c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 1996010500123 19960105 00123 NM 1996 1 5 96FDEA00001 1 19960102 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 512 DENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 THE FUSELAGE SKIN IS DENTED AT BS 512 BETWEEN STR 26 TO 27L. REMOVED DENT AND REPAIRED WITH DOUBLER AT BS 512 BETWEEN S TR 26 TO 27L IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996010500125 19960105 00125 NM 1996 1 5 96FDEA00003 1 19960102 A 5522 657278420 SKIN BOEING 727 7272S2F 1384O81 NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 DUE TO SEVERAL DISCREPANCIES CONSISTING OF CRACKS AND WORN FASTENER HOLES, RT ELEVATOR REQUIRED REPLACEMENT. REMOVED AN D REPLACED RT ELEVATOR PER FEDEX MM 27-30-0, 27-30-01, 27-30-21, 27-30-05, 27-30-11. FUNCTIONAL TEST PER FEDEX MM 27-30 -01 CHECKS GOOD. 2 L 7 3 4F A3WE 1996010500127 19960105 00127 NM 1996 1 5 96FDEA00005 1 19960102 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 CRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148. REPAIRED CRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148, PER FEDEX EA 7-5330-26829. 2 L 7 3 4F A3WE 1996010500130 19960105 00130 NE 1996 1 5 COMA9630001 3 19960102 A 6114 660714200 HUB SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE PROPELLER DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 9725 1445 340A021 DRG705886 WHILE PERFORMING DOWTY SB SF340-61-58 SCAN C, SEVERAL FLAW INDICATION WERE DISCOVERED. PROPELLER WAS DISASSEMBLED AND H UB (S/N 110351) WAS REMOVED FROM SERVICE. 2 L 7 2 4T RT A52EU 6 C P61GL 1996010500133 19960105 00133 EA 1996 1 5 COMA9660003 1 19960101 A 2750 601R93001 FLAP CONTROL CNDAIR CL600 CL6002B19 EA INST PANEL DEFECTIVE A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 941CA 6805 2165 7050 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE FLAP POSITION SELECTOR LEVER ASSY. 2 L 7 2 4F RT A21EA 1996010500347 19960105 00347 NM 1996 1 5 95UAL900365 1 19960102 A 3350 LAMP BOEING 767 767322 1385200 NM LT FUSELAGE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 650UA 25287 THE 6TH EMERGENCY LIGHT ON THE OUTSIDE LEFT SIDE OF THE FUSELAGE WAS INOPERABLE. THE LAMP WAS REPLACED AND THE LIGHT WO RKED NORMALLY DURING AN OPERATIONAL CHECK. 2 L 7 2 4F RT A1NM 1996010500348 19960105 00348 NM 1996 1 5 95UAL900366 1 19960102 A 3350 STRIP BOEING 757 757222 1384956 NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 514UA 24839 EMERGENCY ESCAPE LIGHT STRIP INOP ROW 35. REPLACED LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F RT A2NM 1996010500349 19960105 00349 WP 1996 1 5 95UAL900367 1 19960102 A 3244 TIRE DOUG DC10 DC1010 3022110 WP NR 8 FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 1841U 46634 RETURNED T0 LAX UNDER AMBER ALERT DUE TO BLOWN NR 8 TIRE ON TAKEOFF AND POSSIBLE DAMAGE. NR 7 TIRE BLEW ON TAXI IN, TOW ED TO GATE AND TRIP CANCELLED. REPLACED NR 1 RT SPOILER, RT INBD FLAP, RT INBD FLAP VANE, NR 7 AND 8 TIRES, RT HORIZ ST AB LEADING EDGE AND NR 7 BRAKE. REPAIRED FUSELAGE AND INSPECTED NR 2 ENGINE FOR FOD. FOD TO THE NR 8 TIRE WAS THE CAUS E OF THE INITIAL TIRE FAILURE. 2 L 7 3 4F A22WE 1996010500350 19960105 00350 1996 1 5 9600019763 4 19960101 A 3442 RADAR SYST DOUG DC9 DC941 302207N WP FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 763NW 47396 WEATHER RADAR WOULD NOT PAINT GROUND RETURNS AND BEGAN SPOKING AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER AND INDICATOR WITH NO HELP. DEFERRED RADAR SYSTEM PER MEL 34-19 AND AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500351 19960105 00351 WP 1996 1 5 9600029607 1 19960101 A 3260 LATCH DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 607NW 47232 DURING CLIMB, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. FOLLOWED COCKPIT OP ERATING MANUAL PROCEDURE AND LIGHT EXTINGUISHED AFTER LANDING GEAR WAS EXTENDED FOR LANDING. AIRCRAFT RETURNED TO DTW A ND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR DOOR LATCH AND ROLLER ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996010500352 19960105 00352 WP 1996 1 5 9600039612 1 19960102 A 3260 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP NLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 612NW 47436 DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED LANDING GEAR AND LIGHT REMA INED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED AND OPERATIONALLY CHECKED NOSE LANDI NG GEAR SYSTEM. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500353 19960105 00353 EU 1996 1 5 9600043241 1 19960101 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 341NW 13530 6277 380 DURING LINE MAINTENANCE, THE LEFT EMERGENCY LIGHTS POWER SUPPLY/BATTERY PACK FAILED SYSTEM TEST. REPLACED THE POWER SUP PLY AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996010500354 19960105 00354 EU 1996 1 5 9600053225 1 19960102 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 325US 281 DURING LINE MAINTENANCE, AFT LEFT EMERGENCY LIGHTS BATTERY PACK FAILS COM CHECK. REPLACED BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996010500355 19960105 00355 EU 1996 1 5 96FDEA00006 1 19960101 A 2910 HYD TUBE AIRBUS 310 A310203 EU NR 2 ENGINE LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 413FE 397 SIN - ON CLIMBOUT OF WSSS, LOST YELLOW FLUID TO STAND PIPE AND RETURNED TO WSSS. ON NR 2 ENG TUBE ASSY TO PRESSURE SWIT CH FOUND LEAKING. REMOVED AND REPLACED SAME, (P/N 224-5-12-507). SERVICED YELLOW HYD SYS, LEAK CHECK BY ENG RUN OK. 2 L 7 2 4F RT A35EU 1996010500357 19960105 00357 NM 1996 1 5 DL72L960001 1 19960101 A 3530 PBE BOEING 727 727232 1384082 NM CABIN POPPED INDICATOR A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 501DA 21303 FIRST CLASS COAT CLOSET PBE UNSERVICEABLE, INDICATOR POPPED. REPLACED PBE. 2 L 7 3 4F A3WE 1996010500363 19960105 00363 NM 1996 1 5 DL72S960004 1 19960101 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 21147 RIGHT OVERWING EMERGENCY LIGHT EXIT SIGNS INOP. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 3 4F A3WE 1996010500364 19960105 00364 NM 1996 1 5 DL72S960005 1 19960101 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 21147 RIGHT OVERWING CENTER EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 3 4F A3WE 1996010500371 19960105 00371 NM 1996 1 5 DL757960015 1 19960101 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 625DL 22915 DURING INSPECTION, FOUND THREE EMERGENCY TRACK LIGHTS MISSING. REPLACED LIGHT ASSEMBLIES AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996010500379 19960105 00379 1996 1 5 DLM88960003 4 19960101 A 3417 CADA DOUG MD88 MD88 3023688 NM RIGHT MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 925DL 49712 AT V1, F/O AIRSPEED AND ALT INDICATORS FAILED AND AT LIFT OFF OVERSPEED WARNING CAME ON WITH F/S FAILURE ON BOTH SIDES. GOING TO ALT ON F/O SIDE DID NOT CHANGE OR CADC BOTH ON 1. FLIGHT RETURNED TO EWR. INSTRUMENTS RETURNED TO NORMAL AFT ER LANDING. REPLACED NR 2 CADC (P/N HG28D80) (SN 88111912) AND CADC SWITCH UNIT. 2 L 7 2 4F RT A6WE 1996010500547 19960105 00547 NM 1996 1 5 95UAL900368 1 19960103 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 RAMP PERSONNEL NOTICED EXTERIOR EMERG LIGHTS ON INITIALLY AND THEN WENT OUT. FOUND BOTH ENTRY DOORS AND SERVICE DOORS S LIDE LIGHTS INOPERATIVE. USAIR BATTERY PACK TRIED AND LIGHTS WORKED INITIALLY AND THEN TURNED OFF AND CAME BACK ON. RE PLACED SLIDE BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F A3WE 1996010500548 19960105 00548 WP 1996 1 5 95UAL900369 1 19960103 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1830U 46629 GALLEY LIGHT ASSEMBLY INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY. 2 L 7 3 4F A22WE 1996010500549 19960105 00549 NM 1996 1 5 9600066303 1 19960102 A 3350 900835A BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, THE LEFT UPPER DECK DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK A ND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996010500550 19960105 00550 WP 1996 1 5 9600079982 1 19960102 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996010500551 19960105 00551 WP 1996 1 5 9600089969 1 19960101 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FORWARD OF ROW 4. REPLACED BATTERIES AND OPERATIONAL CHE CK GOOD. 2 L 7 2 4F A6WE 1996010500552 19960105 00552 WP 1996 1 5 9600099923 1 19960101 A 2530 OVEN DOUG DC9 DC932 3022066 WP GALLEY DIRTY A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 927RC 47469 DURING APPROACH, SMOKE ACCUMULATED IN COCKPIT. DECLARED EMERGENCY WITH ATC AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT . FIRE DEPARTMENT MET FLIGHT AND VERIFIED SMOKE CAME FROM OVEN. CLEANED, OPERATIONALLY CHECKED OVEN AND OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500553 19960105 00553 NM 1996 1 5 96UAL900001 1 19960103 A 3230 RETRACT MECH BOEING 747 747238B 1384828 NM NLG MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 WP 29 161UA 21352 NOSE GEAR HAD TO BE EXTENDED BY ALTERNATE SYSTEM, HAD A RED GEAR LIGHT AND NO ALTERNATE NOSE GEAR OPEN LIGHT. GPWS SYST EM GAVE AN AURAL GEAR WARNING, CYCLED GEAR. 2 L 7 4 4F A20WE 1996010500554 19960105 00554 NM 1996 1 5 96UAL900002 1 19960103 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FAILED A UALA K NONE J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 772UA 26930 BACKUP ELECTRICAL SYSTEM EICAS MESSAGE DISPLAYED, INDICATING FAILURE OF BACKUP ELECTRICAL SYSTEM. BACKUP CONVERTER AND LEFTHAND BACKUP GENERATOR WERE REPLACED. VENDOR CONFIRMED FAILURE OF THE PMG STATOR WINDINGS IN THE BACKUP GENERATOR. A LSO, THE BACKUP CONVERTER WAS FOUND TO BE DEFECTIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996010500555 19960105 00555 WP 1996 1 5 ABXA9600002 1 19960104 A 3230 LATCH MECH NIHON YS11 YS11A500 6310416 WP NLG ICED UP A ABXA K NONE J WARNING INDICATION DE DESCENT 1 GL 23 919AX 2113 DURING DESCENT CHECKLIST WITH LANDING GEAR HANDLE PLACED TO NEUTRAL, HYDRAULIC LEVER DEPRESSED AND NOSE LANDING GEAR EXT ENDED. TRIED SEVERAL TIMES AND NOSE GEAR EXTENDED EACH TIME. INSPECTED GEAR, FOUND ICE IN LATCHES. REMOVED ICE FROM G EAR AND LATCHES, CLEANED AREA, LUBED GEAR AND CABLES, INSPECTED SWITCHES AND WIRING HARNESS, NO DAMAGE NOTED. 2 L 7 2 4T A1PC 1996010500556 19960105 00556 SW 1996 1 5 COMA9620001 1 19960102 A 2750 850110 POTENTIOMETER SWRNGN SA227 SA227AC 8780603 SW TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 704C AC704 FLAPS WOULD NOT EXTEND DURING LANDING APPROACH. REPLACED THE FLAP POSITION TRANSMITTER. 1 L 7 2 4T A8SW 1996010500557 19960105 00557 EU 1996 1 5 COMA9630002 1 19960101 A 2612 FIRE DETECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE DIRTY A COMA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 01 358CA 340A047 LEFT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. CLEANED TAIL PIPE FIRE DETECTORS AND FOUND NO DEFECTS. ACFT R ETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996010500558 19960105 00558 EA 1996 1 5 COMA9660004 1 19960102 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT/RT FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 941CA 7050 FLAPS FAIL CAUTION MESSAGE DURING DESCENT. REPLACED THE LT AND RT FLAPS BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996010500565 19960105 00565 EU 1996 1 5 QXEA9600001 1 19960101 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 BOI - EMERGENCY EXIT LIGHT AT ROW 8 INOP RIGHTHAND SIDE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 1996010500567 19960105 00567 EU 1996 1 5 QXEA9600004 1 19960101 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 PDX - FORWARD CABIN EXIT LIGHT INOP. CIRCUIT BOARD WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A20EU 1996010500569 19960105 00569 NM 1996 1 5 VSTA9601001 1 19960102 A 3231 RETRACT MECH BOEING 737 737247 138448D NM RT MLG DOORS MALFUNCTIONED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 308VA 19613 DURING RETRACT OF MLG PER B737 MM 32-32-0 FOR COMPLIANCE WITH VASI EO NR 32-30-1 RT GEAR OPERATION AND FAIRING WAS SATIS FACTORY. ON DOWN SELECTION THE UPPER FLYING DOOR RUBBED HARD ON THE LOWER DOOR JAMMING BOTH DOORS TOGETHER AND CAUSING DOOR RODS AND FITTINGS TRACK. MALFUNCTION BEING INVESTIGATED. DAMAGE ASSESSMENT, REPAIR AND REPLACEMENT IN PROGRESS. 2 L 7 2 4F A16WE 1996011200001 19960112 00001 NE 1996 1 12 95UAL900370 2 19960104 A 7230 COMPRESSOR BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE STALLED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 9071U 19952 655822 ON TAKEOFF AT 90 KNOTS, NR ONE ENGINE HAD A COMPRESSOR STALL. A BRIGHT FLASH WAS OBSERVED ON TAKEOFF, ABORTED TAKEOFF. SUPPLEMENTAL DATA UPDATE: ENGINE WAS BORESCOPED AT THE C-6, C-7, AND C-13 BLADES. BORESCOPE REVEALED EVIDENCE OF SMALL BIRD INGESTION WITH NO BLADE OR VANE DAMAGE. CSD COOLER AND PS3 SCREEN WERE CLEANED. 2 L 7 2 4F 4 F A16WE E2EA 1996011200002 19960112 00002 NM 1996 1 12 95UAL900371 1 19960104 A 2920 69201841 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE FLAP CONTROL LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 356UA 24362 NOTICED A STEADY LOSS OF 'B' SYSTEM HYDRAULIC QUANTITY AFTER REACHING CRUISE. TRIED TO ISOLATE SYSTEMS AND WHEN TURNING OFF THE 'B' SYSTEM SPOILER SWITCH QUANTITY STABILIZED AT 39 PERCENT. REPLACED THE SEAL PLATE BETWEEN THE TRAILING EDGE FLAP CONTROL VALVE AND THE FLAP LOAD LIMITER SOLENOID VALVE. REFERENCE BOEING SERVICE LETTER 737-SL-27-104. 2 L 7 2 4F 4 F RT A16WE E2GL 1996011200003 19960112 00003 WP 1996 1 12 9600109910 1 19960104 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 14 TO 19. REPLACED BATTERIES AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996011200004 19960112 00004 NM 1996 1 12 9600112201 1 19960103 A 3150 T/O WARNING BOEING 727 727251 138408H NM FLIGHT DECK SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 201US 22154 DURING TAKEOFF ROLL WITH FLAPS AT 5 DEGREES, TAKEOFF WARNING HORN ACTIVATED AND TAKEOFF WAS ABORTED. OPERATIONAL CHECK WAS PERFORMED AND SYSTEM INDICATION CHECKED OK. 2 L 7 3 4F A3WE 1996011200005 19960112 00005 WP 1996 1 12 9600129105 1 19960104 A 3260 UNSAFE LIGHT DOUG DC9 DC915 3022036 WP NLG ILLUMINATED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 95S 47205 DURING APPROACH INTO FAR, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EXECUTED GO-AROUND AND RE CYCLED GEAR. ALL INDICATIONS WERE NORMAL AFTER THIRD CYCLE. AIRCRAFT LANDED WITHOUT INCIDENT. CHECKED NOSE GEAR DOWNL OCK SWITCH AND ALL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011200006 19960112 00006 WP 1996 1 12 9600139860 1 19960104 A 3350 60030451 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996011200007 19960112 00007 NM 1996 1 12 96FDEA00013 1 19960104 A 2781 40174 SWITCH BOEING 727 727277 138408S NM NR 5 LE FLAP INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 478FE 21395 AFTER A NORMAL T/O AND FLAP RETRACTION, WE LEVELED AT 5,000 FT AND LEADING EDGE DEVICE LIGHT CAME ON 2 DEGREE SHOWED NR 5 LED UNSAFE. WING ANTI-ICE ON CHECKLIST COMPLETION EXTINGUISHED LIGHT BUT IT CAME ON AGAIN SEVERAL TIMES NO STRUCTURAL LIMITS EXCEEDED. ANTI-ICE CYCLED ON AND OFF WITH NO RESULTS. REPLACED NR 5 L/E KRUEGER FLAP SWITCH. L/E FLAP INDICAT ION OPS CHECK SATISFACTORY ON GROUND TEST. 2 L 7 3 4F RT A3WE 1996011200008 19960112 00008 NM 1996 1 12 96FDEA00014 1 19960105 A 5312 65B07936287 STIFFENER BOEING 747 747245F 1384897 NM BS 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 BS 400 BULKHEAD STIFFENER FOUND WITH CORROSION CRACK AT BWL 118, ADJACENT TO S 42L. STIFFENER REPLACED AS PER FEDEX B74 7 SRM REV 76 51-30-02. 2 L 7 4 4F A20WE 1996011200009 19960112 00009 NM 1996 1 12 96FDEA00015 1 19960105 A 5312 CHORD BOEING 747 747245F 1384897 NM BS 1000 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - BS 1000 BULKHEAD LOWER CHORD FOUND CRACKED AT LBL 9, APPROX 0.75 AND RBL 9, APPROX 0.75. 2 L 7 4 4F A20WE 1996011200010 19960112 00010 NM 1996 1 12 96UAL900003 1 19960104 A 2612 1705 FIRE LOOP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE INOPERATIVE A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 9075U 19956 EXPERIENCED NUMBER ONE ENGINE FIRE WARNING, ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED. REPLACED NUMBER ONE ENGINE LOWER FIRE DETECTION LOOP, BOTH FIRE BOTTLES AND SQUIBS. 2 L 7 2 4F 4 F A16WE E2EA 1996011200011 19960112 00011 WP 1996 1 12 96UAL900004 1 19960104 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1816U 46615 EEL LIGHT INOPERATIVE LT SIDE FORWARD GALLEY. RESEATED LOOSE CONNECTOR. 2 L 7 3 4F A22WE 1996011200012 19960112 00012 NM 1996 1 12 96UAL900005 1 19960104 A 3350 BATTERY BOEING 727 727222 1384073 NM SERVICE DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7457U 21911 LT AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY DUE TO FAILURE. 2 L 7 3 4F A3WE 1996011200013 19960112 00013 NM 1996 1 12 96UAL900006 1 19960104 A 4900 APU BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7457U 21911 WHEN PACKS RAN OFF, APU CABIN HAD BURNT OIL SMELL. 2 L 7 3 4F 4 F A3WE E2EA 1996011200014 19960112 00014 WP 1996 1 12 ABXA9600003 1 19960103 A 3350 1820 BULB DOUG DC8 DC861 3021952 WP OVERHEAD PANEL DEFECTIVE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 849AX 45891 EMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL INOP. RELAMPED EMERGENCY EXIT DISARM LIGHT AND OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200015 19960112 00015 WP 1996 1 12 ABXA9600004 1 19960103 A 3260 H1410051 DN LOCK SWITCH DOUG DC9 DC933F 302207A WP NLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 932AX 47465 NOSE GEAR GREEN DOWN LIGHT WENT OUT WITH GEAR EXTENSION, CYCLED LANDING GEAR, LIGHT FLICKERED OUT AND ON AGAIN. VERIFIE D, FOUND PIN 'C' BROKEN OFF OF NOSE GEAR DOWNLOCK SWITCH. REMOVED BROKEN PIN FROM CONNECTOR PLUG AND REPLACED NOSE GEAR DOWNLOCK SWITCH PER DC-9 MM 32-60-0. SYSTEM GROUND CHECKS GOOD. 2 L 7 2 4F A6WE 1996011200016 19960112 00016 SO 1996 1 12 BIER960029 1 19960104 A 8120 LW18459 ROD SUPPORT PIPER PA31 PA31350 7103110 SO TURBOCHARGER CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3521S 317952107 AT UNRELATED MAINTENANCE, FOUND TURBOCHARGER TOP ROD SUPPORT BRACKET BROKEN AT ENGINE. SUBMITTER STATES SUSPECT MISALIG NMENT OF ROD AND SUPPORT AT INSTALLATION. 1 L 7 2 3O A20SO 1996011200017 19960112 00017 SO 1996 1 12 COMA9610002 1 19960104 A 2750 3075001017 CONTROL BOX EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 1110J 7530 2275 120110 FLAP ASYMMETRY WARNING DURING LANDING ROLL. REPLACED THE FLAP CONTROL BOX. 2 L 7 2 4T RT A31SO 1996011200019 19960112 00019 EU 1996 1 12 COMA9630003 1 19960102 A 7603 C822249 POWER LEVER SAAB SF340 SF340A 7850100 EU RT ENGINE BINDING A COMA O OTHER O OTHER CR CRUISE 1 SO 01 340SF 340A014 WHEN THE RIGHT ENGINE POWER LEVER WAS ADVANCED DURING CRUISE, THE ENGINE SURGED TO 95 PERCENT. REPLACED BINDING RT ENGI NE POWER LEVER CABLE. 2 L 7 2 4T RT A52EU 1996011200020 19960112 00020 EU 1996 1 12 COMA9630004 1 19960102 A 2613 OVERHEAT WARNING SAAB SF340 SF340A 7850100 EU RT ENGINE ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 340SF 340A014 RIGHT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS WERE NORMAL AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011200021 19960112 00021 EU 1996 1 12 COMA9630005 1 19960104 A 3020 9303143005 NOZZLE SAAB SF340 SF340A 7850100 EU LT ENGINE BURNED A COMA K NONE O OTHER CR CRUISE 1 SO 01 347CA 15791 8241 340A028 LEFT ENGINE INLET ANTI-ICE CYCLES ON AND OFF EVERY 15 SECONDS. REPLACED THE INLET PROTECTION DEVICE EXHAUST NOZZLE. 2 L 7 2 4T RT A52EU 1996011200025 19960112 00025 NM 1996 1 12 SWAA960001 1 19960103 A 5610 8300005602 WINDSHIELD BOEING 737 7373H4 1384600 NM RT COCKPIT CRACKED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 309SW 22948 EN ROUTE FROM TUS TO SAN, FIRST OFFICER'S WINDSHIELD BEGAN ARCING, THEN CRACKED. AIRCRAFT DIVERTED TO PHX AND MADE AN U NEVENTFUL LANDING. REPLACED WINDOW ASSEMBLY AND HEAT CONTROLLER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996011200026 19960112 00026 NM 1996 1 12 SWAA960002 1 19960103 A 2730 65445038 ACTUATOR BOEING 737 7372H4 138448C NM ELEV LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 94SW 23053 NOTED A-SYSTEM FLUID LOSS EN ROUTE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED TAIL AREA AND P ERFORMED LEAK CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER PER BOEING M/M. TEST FLOWN WITH NO DEFECTS NOTED. 2 L 7 2 4F A16WE 1996011200027 19960112 00027 WP 1996 1 12 UPS805167 1 19960102 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME HAS .75 INCH LONG CRACK AT FS 80 LONGERON 21R. REPAIRED FRAME PER SR M 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996011200118 19960112 00118 NM 1996 1 12 9600146301 1 19960104 A 3350 900835A BATTERY PACK BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, TWO EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200119 19960112 00119 WP 1996 1 12 9600159967 1 19960105 A 3260 RELAY DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9331 47263 DURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. VISUALLY CONFIRMED LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RELAY R2-28 AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996011200120 19960112 00120 EU 1996 1 12 96FDEA00016 1 19960105 A 3610 DUCT AIRBUS 310 A310203 EU NR 2 ENGINE BLOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 CLIMBING THROUGH 7,000 FT, RECEIVED ECAM AND FIRE HANDLE FIRE WARNING. WHEN THROTTLE MOVED TO IDLE ALL WARNINGS EXTINGU ISHED, TESTED FIRE WARNING SYSTEM AND RETURNED TO EWR, ENG AT IDLE. OPENED UP NR 2 ENG AND FOUND HP RECOUP DUCT BLOWN, (P/N 9345M89-G01) REF IPC 75-00-00 FIG 31 ITEM 150. PERFORMED FIRE WARNING TEST ALL INDICATIONS NORMAL. INSTALLED SERV ICEABLE HP RECOUP AIR DUCT IAW MM 72-00-02. PERFORMED HIGH POWER RUN AS PER JRH, ALL PARAMETERS NORMAL AND A/C OK FOR S ERVICE. 2 L 7 2 4F RT A35EU 1996011200121 19960112 00121 NM 1996 1 12 96FDEA00017 1 19960105 A 3260 H1010153 DN LOCK SWITCH BOEING 727 72722 1384002 NM NLG FAILED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 148FE 19086 NOSE GEAR DID NOT SHOW DOWN AND LOCKED. CYCLED IAW CHECKLIST, SUCCESSFUL 3 DOWN. GEAR HORN SOUNDED CONTINUOUSLY WHEN F LAPS EXTENDED TO 30 DEGREES CONFIRMING GEAR UNSAFE CONDITION. REPLACED NOSE LANDING GEAR LOCK SWITCH IAW MM 32-61-21 AN D OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996011200122 19960112 00122 WP 1996 1 12 96FDEA00018 1 19960106 A 5512 PLANK DOUG DC10 DC1010CF 3023502 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT HORIZ STAB FWD UPPER PLANK CRACKED JUST INBOARD OF CLOSING RIB, FROM FWD EDGE AFT THROUGH FASTENER HOLE 1.5 TOTAL CRA CK CONTINUES PAST HOLE. REMOVED FASTENERS AND TRIMMED OUT CRACKED AREA. NDT AT CRACKED AREA AND OPEN HOLES C/W. COLD WORKED HOLES FINAL REAM. INSTALLED CONCOL WASHER, FABRICATED DOUBLER PER SRM 55-20-00. INSTALLED DOUBLER PER SRM 55-20 -22. 2 L 7 3 4F RT A22WE 1996011200123 19960112 00123 NM 1996 1 12 96FDEA00019 1 19960105 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE, CRACK IN STR 7L STA 970. INSTALLED STR REPAIR PER SRM 53-10-3 PG 5 FIG 3. 2 L 7 3 4F A3WE 1996011200124 19960112 00124 NM 1996 1 12 96FDEA00020 1 19960105 A 5320 DOOR JAMB BOEING 727 727227 1384078 NM BS 416 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 AFT LWR CORNER OF FWD GALLEY DOOR JAMB, AFT SIDE OF FRAME HEAVY CORROSION FOUND STA 416 ABOVE STR 17R. FOUND WITHIN SRM LIMITS. 2 L 7 3 4F A3WE 1996011200125 19960112 00125 NM 1996 1 12 96FDEA00021 1 19960105 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 TOP SURFACE OF FLOORBEAM AT STA 344 CORRODED IN NUMEROUS AREAS FROM LBL 52 TO RBL 38. INSTALLED DOUBLER REPAIR ON TOP C AP OF FLOORBEAM PER DRAWING SR 27-53-007 FROM FEDEX STANDARD REPAIR DRAWING. 2 L 7 3 4F A3WE 1996011200126 19960112 00126 NM 1996 1 12 96FDEA00022 1 19960105 A 5311 BELLFRAME BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN BELL FRAME CRACKED AT RADIUS STA 804.5, JUST ABOVE STA 145. INSTALLED REPAIR PER SRM 51-40-3 PAGE 1 TO 4 REF NR01 41. 2 L 7 3 4F A3WE 1996011200127 19960112 00127 NM 1996 1 12 96FDEA00023 1 19960105 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1996011200128 19960112 00128 NM 1996 1 12 96FDEA00024 1 19960105 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CORROSION ON FLOORBEAM STA 380 RBL 23 TO 51.25 GROUND FASTENER HOLES. FOUND WITHIN SRM LIMITS. 2 L 7 3 4F A3WE 1996011200129 19960112 00129 NM 1996 1 12 96FDEA00025 1 19960108 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 CRACK IN CORNER OF SKIN BS 1223 LBL 16 WL 148. REPAIRED CRACK IN CORNER OF SKIN AT BS 1223 LBL 16 WL 148 PER FEDEX EA 7 -5330-26829. 2 L 7 3 4F A3WE 1996011200130 19960112 00130 NM 1996 1 12 96FDEA00026 1 19960108 A 5320 65453135 STR CLIP BOEING 727 727227 1384078 NM BS 950 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED STR CLIP, BS 950F STR 7L. REMOVED AND REPLACED STR CLIP BS 950F STR 7L PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996011200131 19960112 00131 NM 1996 1 12 96FDEA00027 1 19960108 A 5313 BAC1498144 STRINGER BOEING 727 727227 1384078 NM BS 660 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED STR AT BS 660 STR 7L. REPAIRED DAMAGED STR 7L BS 660 PER FEDEX SRM 53-10-3, BY REMOVING DAMAGED SECTION AND FAB RICATING REPAIR PARTS AND INSTALLING THEM. 2 L 7 3 4F A3WE 1996011200132 19960112 00132 NM 1996 1 12 96FDEA00028 1 19960108 A 5320 65453135 CLIP BOEING 727 727227 1384078 NM BS 660 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01) IN STR AND STR CLIP AT BS 660 STR 3R. REMOVED CORROSION AT STR 3 BS 660 RT. ORIGINAL THICKNESS .045, REMOVED .002, 5 INCH BY 1 INCH AREA WITHIN LIMITS PER FEDEX SRM 53-10-1, ALODINED AND PRIMED AREA. REMOVED STR C LIP AT BS 660 RT DUE TO CRACK. REPLACED STR CLIP PER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996011200133 19960112 00133 NM 1996 1 12 96FDEA00029 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED FRAME AND STR CLIP AT BS 600 RT STR 7. REPAIRED FRAME AT BS 600 STR 7 TO 8R IAW FEDEX SRM 53-10-4. REMOVED DAM AGED STR CLIP AND INSTALLED NEW STR CLIP AT BS 600 STR 7R. 2 L 7 3 4F A3WE 1996011200134 19960112 00134 NM 1996 1 12 96FDEA00030 1 19960108 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01-1) ON FLOORBEAM AT CLIP NUT HOLE BS 360 RBL 12 WL 208. REMOVED CORROSION ON FLOORBEAM BS 360 RBL 12 WL 208 FOUND TO BE OUT OF LIMITS, ORIGINAL .130 AND REMOVED .032 FROM 1 INCH BY 2 INCH AREA. FABRICATED AND INSTALL ED REPAIR ANGLES FOR FLOORBEAM AT BS 360 RBL 12 WL 208 PER FEDEX SRM 53-10-8, ALODINED AND PRIMED. 2 L 7 3 4F A3WE 1996011200135 19960112 00135 NM 1996 1 12 96FDEA00031 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CRACKED IN FRAME BS 560 RT BETWEEN STR 7 AND 8. REPAIRED DAMAGED FRAME BS 560 RT BETWEEN STR 7 AND 8 IAW FEDEX SRM 53-1 0-4. FRAME WAS FOUND NOT TO HAVE INDICATION IAW D6-48875 PT6, 51-00-00 FIG 23. 2 L 7 3 4F A3WE 1996011200136 19960112 00136 NM 1996 1 12 96FDEA00032 1 19960108 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 400 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01-1), ON FLOOR BEAM AT FASTENER HOLE BS 400 RBL 35 WL 207.9. PERFORMED FLOOR BEAM REPAIR AT BS 400 RBL 29 TO 42 WL 207.9 IAW FEDEX SRM 53-10-8, 51-40. 2 L 7 3 4F A3WE 1996011200137 19960112 00137 NM 1996 1 12 96FDEA00033 1 19960108 A 5313 BAC1498144 STRINGER BOEING 727 727227 1384078 NM BS 757-759 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 MECH DAMAGE AND FASTENERS MISSING IN STR 7L BS 757 TO 759. ACCOMPLISHED STR REPAIR AT STA 740 TO 770 STR 7L PER FEDEX S RM 53-10-1, 53-10-2 AND 53-10-3. 2 L 7 3 4F A3WE 1996011200138 19960112 00138 NM 1996 1 12 96FDEA00034 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 380 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 FRAME CRACKED AT STA 380 WL 278 RBL 65. REMOVED DAMAGED SECTION OF FRAME AT BS 380 WL 278 RBL 65. FABRICATED REPAIR AN GLE AND DOUBLERS, ALODINED, PRIMED AND INSTALLED WET. ALL WORK DONE PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996011200139 19960112 00139 NM 1996 1 12 96FDEA00035 1 19960108 A 5754 65162268A LUG BOEING 727 727227 1384078 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 NR 5 K-FLAP O/B LUG O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVE D AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECKED IAW FEDEX MM 27-81-1. 2 L 7 3 4F A3WE 1996011200140 19960112 00140 SO 1996 1 12 COMA9610004 1 19960103 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAPS DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 156CA 1830 120156 RECEIVED TAKEOFF FLAPS AURAL WARNING DURING TAKEOFF AND FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE LT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996011200141 19960112 00141 EU 1996 1 12 COMA9630006 1 19960105 A 3230 RETRACT MECH SAAB SF340 SF340A 7850100 EU LANDING GEAR ICED UP A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 320CA 340A064 LANDING GEAR DID NOT RETRACT FULLY, GEAR CYCLED TWICE WITH SAME RESULT. DE-ICED LANDING GEAR AND RETRACTION CHECK NORMA L. 2 L 7 2 4T RT A52EU 1996011200142 19960112 00142 EU 1996 1 12 COMA9630007 1 19960105 A 2731 DL3827M157 TRIM ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEVATOR DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 356CA 340A034 CONFIGURATION WARNING DURING TAKEOFF ROLL. REPLACED THE LT PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996011200143 19960112 00143 EU 1996 1 12 COMA9630008 1 19960105 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 380CA 340A012 SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERY PACKS. 2 L 7 2 4T RT A52EU 1996011200144 19960112 00144 EA 1996 1 12 COMA9660005 1 19960105 A 2150 PACK CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 924CA 7026 RT COOLING PACK FAULT WARNING. SMOKE IN CABIN AND LAVATORY. SMOKE CLEARED WHEN COOLING PACK SHUTDOWN. PLACED RT COOLI NG PACK ON DEFERRED MAINT LIST. 2 L 7 2 4F RT A21EA 1996011200145 19960112 00145 NM 1996 1 12 DL72K960013 1 19960103 A 5320 FLOOR CHANNEL BOEING 727 727232 1384082 NM BS 1110 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 FOUND ON MV 1, CORROSION ON FLOOR SUPPORT CHANNEL FWD SIDE TOP LEG STA 1110, LBL 9 AROUND FLOOR PANEL HOLE. REPAIRED PE R M/M 53-20-11. 2 L 7 3 4F A3WE 1996011200146 19960112 00146 NM 1996 1 12 DL72K960014 1 19960103 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 360 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 CORROSION FOUND ON FLOORBEAM UPPER ANGLE STA 360 LBL 20 TO RBL 14. INSTALLED REPAIR DOUBLERS PER M/M 53-20-11 PG 802 TO 803. 2 L 7 3 4F A3WE 1996011200147 19960112 00147 NM 1996 1 12 DL72L960016 1 19960103 A 2910 65178494061 HYD LINE BOEING 727 727232 1384082 NM B-HYD SYST CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 509DA 21311 ON T/O, A-SYS HYD QTY DECREASED TO 1.8 GAL. SHORTLY THEREAFTER THE B-SYS STARTED TO DECREASE AND B-HYD PUMPS WERE TURNE D OFF. FOUND THE RIGID HYD LINE FOR THE B-SYS MODULE CRACKED. REPLACED WITH A LIKE LINE, SERVICED SYS AND OPS CK OK. 2 L 7 3 4F A3WE 1996011200155 19960112 00155 NM 1996 1 12 DL72S960027 1 19960104 A 5743 6519296 FITTING BOEING 727 727232 1384082 NM LT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 AT GEAR CHANGE CORROSION WAS FOUND ON THE LEFT MAIN GEAR FWD TRUNNION ATTACH FITTING O/B LOWER HOLE, O/B UPPER HOLE AND INBD LOWER HOLE. ALL CORROSION WAS REMOVED AND FOUND IN LIMITS. THE AREA WAS REPAIRED PER M/M 57-43-0. 2 L 7 3 4F A3WE 1996011200156 19960112 00156 NM 1996 1 12 DL72S960029 1 19960104 A 5744 FITTING BOEING 727 727232 1384082 NM LEFT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 AT GEAR CHANGE THE NR 2 FLAP INBD TRACK SUPPORT FITTING WAS FOUND CORRODED ON THE OUTER FACE. THIS FITTING WAS REPAIRED PER M/M 57-42-0 FIG 805, DAMAGE WAS WITHIN LIMITS FOR THIS REPAIR. 2 L 7 3 4F A3WE 1996011200162 19960112 00162 NM 1996 1 12 DL72S960044 1 19960104 A 2760 MOUNT BOLTS BOEING 727 727232 1384082 NM NR 2 SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 NR 2 SPOILER POWER PACK BOTTOM MOUNT BOLTS ARE LOOSE. REMOVED SPOILER ACTUATOR ATTACH FITTING. REMOVED AND REPLACED AN GLE PER MM 57-42-0 PG 804. INSTALLED POWER PACK, ACTUATOR AND MOUNT FITTING. 2 L 7 3 4F A3WE 1996011200163 19960112 00163 NM 1996 1 12 DL72S960053 1 19960105 A 5240 69562562 HINGE PIN BOEING 727 727232 1384082 NM L 2 SERV DOOR SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 FOUND LEFT AFT SERVICE DOOR WITH SHEARED DOOR HINGE PIN. REPLACED HINGE PIN OPERATION NORMAL. 2 L 7 3 4F A3WE 1996011200165 19960112 00165 NE 1996 1 12 DL733960043 2 19960106 A 7200 ENGINE BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FOD A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 309WA 23442 720673 SHORTLY AFTER T/O, AN ELEC ODOR DEVELOPED IN THE CABIN. COMPLIED WITH CHECKLIST. REMOVED SMALL AMOUNT OF COMPUTER PAPE R FROM NR 2 ENG. RAN ENGINE PER PFHB, NO ODOR PRESENT. RAN ALL ELEC SYS AND A/C PACKS, NO PROBLEM FOUND. INSPECTED EN G PER M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996011200166 19960112 00166 NM 1996 1 12 DL73S960031 1 19960104 A 2740 RELAY 91238056 BOEING 737 737232 1384475 NM STAB TRIM INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 331DL 23103 AT ALTITUDE MAIN STAB TRIM MOTOR WOULD NOT WORK, A/P MOTOR WORKS OK. APPLICABLE C/B WERE CYCLED TO NO AVAIL, RETURNED T O ATL PER DISPATCH. INSPECTED STAB TRIM ACT, CLEANED CONNECTORS, INSPECTED LIMIT SWITHCES, CUTOUT SWITHCES AND ALL CHEC K NORMAL. REPLACED R-66 DUE TO HISTORY AND ALL OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996011200168 19960112 00168 NM 1996 1 12 DL757960028 1 19960104 A 2622 51211 FIRE BOTTLE BOEING 757 757232 1384965 NM FLIGHT CABIN LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 F/C HALON FIRE BOTTLE LEAKING EXTINGUISHING AGENT. 2 L 7 2 4F RT A2NM 1996011200171 19960112 00171 NE 1996 1 12 DL76L960042 2 19960106 A 7261 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 183DN 27110 724146 NR 2 ENG CHANGE DUE TO HIGH OIL CONSUMPTION. 2 L 7 2 4F 4 F RT A1NM E24NE 1996011200172 19960112 00172 NM 1996 1 12 DL76S960008 1 19960102 A 3350 LAMP 387 BOEING 767 767332 1382001 NM 2L DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 00000 23146 SLIDE LIGHT 2L DOOR INOP. RELAMPED, OPN NML. 2 L 7 2 4F RT A1NM 1996011200174 19960112 00174 NM 1996 1 12 DLM11960006 1 19960101 A 2420 WIRE 221W5070511 DOUG MD11 MD11 3023602 NM NR 1 ENGINE DAMAGED A DALA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 805DE 48476 GENERATOR FEEDER CABLES DAMAGED, DUE TO SHORTING IN PYLON. 2 L 7 3 4F RT A22WE 1996011200175 19960112 00175 NM 1996 1 12 DLM11960017 1 19960103 A 3350 TRACK 0105606205 DOUG MD11 MD11 3023602 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 EMERGENCY LIGHT TRACK SHORTED. REPLACED TRACK, OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 1996011200176 19960112 00176 NM 1996 1 12 DLM88960018 1 19960103 A 5755 SPOILER DOUG MD88 MD88 3023688 NM RT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 930DL 49717 FOUND DURING A-2 LETTER CHECK, RIGHT I/B FLIGHT SPOILER DELAMINATED AT T/E. REPAIRED PER SRM 51-70-1B. 2 L 7 2 4F RT A6WE 1996011200178 19960112 00178 NM 1996 1 12 DLM88960052 1 19960106 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908DL 49539 PN PREFLIGHT, L-1 AND R-1 DOOR EMERGENCY EXIT IDENTIFIER LIGHTS FOUND INOP. MTC REPAIRED BROKEN WIRE IN THE RT SIDE F/C FLOOR TRACK AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011200180 19960112 00180 EU 1996 1 12 9600163241 1 19960106 A 3260 848401 PROX SENSOR AIRBUS 320 A320211 3930320 EU LT MLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 341NW 380 DURING CLIMBOUT AFTER THE LANDING GEAR WAS RETRACTED, THREE LANDING GEAR DISAGREEMENT LIGHTS ILLUMINATED. CYCLED LANDIN G GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE LEFT MAIN LANDING GEAR PROXIMITY SENSOR (23GA) AND THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT. OPERATIONAL CH ECK OK. 2 L 7 2 4F RT A28NM 1996011200181 19960112 00181 NM 1996 1 12 9600175529 1 19960108 A 7830 TR UNIT BOEING 757 757251 1384970 NM ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 529US 23844 DURING CLIMB, REVERSER ISOLATION VALVE STATUS MESSAGE AND REVERSER ISOLATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURN ED TO DEPARTURE AIRPORT, NO FUEL WAS DUMPED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEACTIVATED AND STOWED THR UST REVERSER. THRUST REVERSER WAS PLACED ON MEL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1996011200182 19960112 00182 NM 1996 1 12 9600186304 1 19960105 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS IN THE AFT CABIN LEFT AISLE WERE FOUND INOPERATIVE. RECONNECTED LOOS E CONNECTOR IN FLOOR TRACK AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200183 19960112 00183 NM 1996 1 12 9600192284 1 19960105 A 5270 DOOR WARNING BOEING 727 727251 138408H NM CARGO DOOR ACTIVATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 284US 21323 DURING CLIMB, AFT CARGO DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. AFT CARG O DOOR WAS INSPECTED AND FOUND CLOSED AND LOCKED. AFT CARGO DOOR WAS PLACED ON MEL 52-4. 2 L 7 3 4F A3WE 1996011200184 19960112 00184 NM 1996 1 12 9600202704 1 19960107 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND PORTABLE EMERGENCY EXIT LIGHT AT FORWARD GALLEY SERVICE DOOR INOPERATIVE. REPLACED THE LIGHT AS SEMBLY AND BATTERIES, CHECKED OK. 2 L 7 3 4F A3WE 1996011200185 19960112 00185 WP 1996 1 12 9600219923 1 19960108 A 2530 OVEN DOUG DC9 DC932 3022066 WP NR 2 SMOKING A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 927RC 47469 DURING FLIGHT, SMOKE ACCUMULATED IN AIRCRAFT FROM NR 2 OVEN. PILOTS WORE SMOKE GOGGLES AND OXYGEN MASKS UNTIL OVEN COOL ED OFF. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200186 19960112 00186 WP 1996 1 12 9600229916 1 19960108 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200187 19960112 00187 WP 1996 1 12 9600239929 1 19960105 A 3350 BATTERY DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200188 19960112 00188 WP 1996 1 12 9600249929 1 19960108 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200189 19960112 00189 WP 1996 1 12 9600259974 1 19960106 A 3350 BATTERY DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9338 47347 FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200190 19960112 00190 WP 1996 1 12 9600269967 1 19960106 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 WIRING FOR EMERGENCY FLOOR TRACK LIGHTING AT ROW 15 IS LOOSE AND EXPOSED. FOUND WIRE FOR LIGHT AT ROWS 16 AND 18 PULLED OUT OF THE SOCKET. REPAIRED WIRE AND REPLACED SOCKETS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200191 19960112 00191 WP 1996 1 12 9600279989 1 19960106 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING IN TAILCONE AREA INOPERATIVE. REPLACED THE BATTERY PACK AND OPE RATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200192 19960112 00192 WP 1996 1 12 9600289952 1 19960105 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP LT/RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE CHECK, FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED R2-213 AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200193 19960112 00193 WP 1996 1 12 9600299601 1 19960105 A 3231 UPLOCK ASSY DOUG DC9 DC932 3022066 WP LT MLG DOOR LOOSE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 601NW 47038 DURING APPROACH, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. EXECUTED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR DOOR UPLOCK ASSEMBLY LOOSE. RESECURED UPLOCK ASSEMBLY AND RIGGED LANDING GEAR DOOR SPRINGS, OPERATIONAL CHECK GOOD . 2 L 7 2 4F A6WE 1996011200194 19960112 00194 WP 1996 1 12 9600309991 1 19960105 A 3230 UPLATCH ROLLER DOUG DC9 DC932 3022066 WP RT NLG OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8957E 47215 DURING CLIMB, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR D OOR UPLATCH ROLLER AND RIGHT MAIN LANDING STRUT TO BUMPER CLEARANCE OUT OF RIG. RIGGED BOTH SYSTEMS AND OPERATIONAL CHE CK GOOD. 2 L 7 2 4F A6WE 1996011200195 19960112 00195 WP 1996 1 12 9600319106 1 19960107 A 2550 CARGO NET DOUG DC9 DC915 3022036 WP CARGO DOOR OUT OF POSITION A NWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 01 96S 47206 DURING CLIMB CLE-MSP, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, NO HE LP. DIVERTED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE AFT CARGO DOOR WAS NOT FULLY CLOSED AND LATCH ED ON THE AFT SIDE, DUE TO AN UNSECURED CARGO NET AND JAMMED CLIP. THE FORWARD SIDE WAS CLOSED AND LATCHED AND THERE WA S NO ANNUNCIATOR INDICATION. ALSO, FOUND THAT THE DOOR WAS DIFFICULT TO CLOSE. RERIGGED THE DOOR PER 52-31-0, CODE 3. PRESSURE AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011200196 19960112 00196 EU 1996 1 12 96UAL900007 2 19960105 A 7321 SCR501545 ENGINE CONTROL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 916UA 25383 726281 NUMBER ONE ENGINE SURGES AT HIGH POWER SETTINGS WITH AUTO THROTTLE ON AND OFF. ALSO, SURGE WAS NOTICEABLE WITH AIRCRAFT IN YAW, BUT NOT NOTICEABLE AT LOWER POWER SETTINGS. REPLACED MAIN ENGINE CONTROL, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011200197 19960112 00197 NM 1996 1 12 96UAL900008 1 19960105 A 2910 651784528 HYD LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEV PCU LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7266U 21413 RETURNED TO LAX UNDER AMBER ALERT DUE TO LOSS OF A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE IN FLIGHT. REPLACED PRESSURE LINE AT LEFT ELEVATOR POWER CONTROL UNIT DUE TO LEAK. 2 L 7 3 4F 4 F A3WE E2EA 1996011200198 19960112 00198 NM 1996 1 12 96UAL900010 1 19960105 A 3340 LIGHT WIRES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING DAMAGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 7465U 21919 LEFT WING TRAILING EDGE WHITE LIGHT INOPERATIVE. POWER AND GROUND WIRES FOUND BURNT IN VICINITY OF LIGHT. REPLACED WIR ES. CAUSE UNDETERMINED, POSSIBLE LIGHTNING STRIKE. 2 L 7 3 4F 4 F A3WE E2EA 1996011200199 19960112 00199 WP 1996 1 12 96UAL900011 1 19960105 A 3620 FAIL LIGHTS DOUG DC10 DC1010 3022110 WP NR 2 MANIFOLD ILLUMINATED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 1844U 48260 NR 2 PNEUMATIC MANIFOLD 'MANIFOLD FAIL' AND 'TEMP HI' LIGHTS ON. PERFORMED EMERGENCY PROCEDURE, NOW OPERATING WITH SYST EMS 1 AND 3. FAILURE OCCURRED CLIMBING THROUGH 20,000 FEET. 2 L 7 3 4F A22WE 1996011200200 19960112 00200 1996 1 12 96UAL900012 4 19960109 A 2565 SEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 SLIDE REMOVED FROM AIRCRAFT DUE TO INADVERTENT DEPLOYMENT. SLIDE HAS A SEAM LEAK AT THE LT CORNER OF THE SLIDE. REPAIR ED SEAM LEAK, NON-STRUCTURAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996011200201 19960112 00201 NM 1996 1 12 96UAL900013 1 19960108 A 2130 7110024 PANEL BOEING 737 737322 1384676 NM COCKPIT DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 202UA 24717 PRESSURIZATION AUTO FAIL LIGHT CAME ON, WAS UNABLE TO CONTROL PRESSURIZATION IN STANDBY OR MANUAL MODE. CABIN WAS CLIMB ING AT AN UNCONTROLLABLE RATE. REPLACED MAIN OUTFLOW VALVE AND PRESSURIZATION SELECTOR PANEL. FOUND PIN PUSHED IN ON P ANEL, TESTED PRESSURIZATION SYSTEM AND CHECKED OK. 2 L 7 2 4F RT A16WE 1996011200202 19960112 00202 NM 1996 1 12 96UAL900014 1 19960108 A 3350 LAMP SEGMENT BOEING 747 747422 1384935 NM CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT LIGHT INOP AT ROW 1R, LAMP SEGMENT BURNED OUT. REPLACED LAMP SEGMENT AND POWER STRIP. 2 L 7 4 4F RT A20WE 1996011200203 19960112 00203 NM 1996 1 12 96UAL900016 1 19960108 A 2121 36144161 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 568UA 2272 26674 SMOKE IN AFT AND F0RWARD CABIN AFTER LEVEL OFF AT 37,000 FEET. SMOKE BEGAN TO DISSIPATE AT 24,000 FEET IN DESCENT AND C LEAR AT 10,000 FEET. FLIGHT DIVERTED TO PHX. THE APU HAD A SEVERE COOLING FAN FAILURE WHICH CAUSED OIL TO LEAK INTO TH E INLET PLENUM, CONTAMINATING THE AIR CONDITIONING SYSTEM. THE COOLING FAN HAD THE SHROUDED ROTOR. THE APU ALSO SUSTAI NED FOREIGN OBJECT DAMAGE TO THE COMPRESSOR IMPELLERS. PART TOTAL CYCLES, 2,599. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011200204 19960112 00204 NM 1996 1 12 96UAL900018 1 19960109 A 4900 APU BOEING 727 727222 1384073 NM RT MLG WW FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7460U 21914 APU AUTO-SHUTDOWN AND SMOKE CAME OUT OF WHEEL WELL AREA. 2 L 7 3 4F A3WE 1996011200205 19960112 00205 SO 1996 1 12 COMA9610005 1 19960107 A 2910 PRESS LINE EMB 120 EMB120RT SO BLUE HYD SYST FROZEN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 267CA 120259 RT BLUE HYDRAULIC SYSTEM, LOW RESERVOIR PRESSURE, WARNING LIGHT ILLUMINATED. THAWED FROZEN MOISTURE IN RESERVOIR PRESSU RIZATION LINE. 2 L 7 2 4T RT A31SO 1996011200206 19960112 00206 EU 1996 1 12 COMA9630009 1 19960106 A 2432 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU AVIONICS DEFECTIVE A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 320CA 11516 163 340A064 EMERGENCY POWER WARNING LIGHT CAME ON. REPLACED THE EMERGENCY POWER SUPPLY. 2 L 7 2 4T RT A52EU 1996011200207 19960112 00207 EA 1996 1 12 COMA9660006 1 19960106 A 3010 ANTI-ICE DUCT CNDAIR CL600 CL6002B19 EA COCKPIT WARNING A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 912CA 7011 ANTI-ICE DUCT MESSAGE ON EICAS TAKEOFF ABORTED. COULD NOT DUPLICATE DISCREPANCY. SYSTEM CHECKED NORMAL AND ACFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 1996011200208 19960112 00208 NM 1996 1 12 SCNA96001 1 19960103 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE EMERGENCY EXIT LIGHT LOCATED IN THE AFT CABIN WAS FOUND TO BE DIM. REMOVED AND REPLACED BATTERIES IN LIGHT, OPS CHE CKED GOOD PER MM 33-50-101. 2 L 7 3 4F A3WE 1996011200209 19960112 00209 NM 1996 1 12 SCNA96002 1 19960103 A 3350 1102833 LIGHT ASSY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE EMERGENCY EXIT AREA LIGHT AT SEAT ROW 11 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW MM 33 -50-81 AND LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996011200210 19960112 00210 NM 1996 1 12 SCNA96003 1 19960105 A 3350 900835A BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 THE FORWARD EMERGENCY EXIT AREA LIGHT COMES ON AND THEN GOES OUT. REMOVED AND REPLACED BATTERY IAW MM 33-50-71 AND LIGH T TESTED NORMAL. 2 L 7 3 4F RT A3WE 1996011200211 19960112 00211 NM 1996 1 12 UPS205179 1 19960108 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 207UP 21699 YHM - MAINTENANCE REPORTED, L 1 EMERGENCY EXIT LIGHT WILL NOT TEST. LIGHT ASSY REMOVED AND REPLACED AND OPS CHECKED GOO D AS PER MM 33-50-01. 2 L 7 3 4F A3WE 1996011200261 19960112 00261 NM 1996 1 12 9600326304 1 19960107 A 7830 TR SENSOR BOEING 747 747451 1384940 NM NR 2 OUT OF ADJUST A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 664US 23819 DTW - AFTER TAKEOFF, THE NR 2 ENGINE REVERSER AMBER LIGHT ILLUMINATED. NO STATUS, NO EICAS AND NO PRESENT LEG FAULT MES SAGES DISPLAYED. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 135,000 LBS OF FUEL AND DIVERTED FLIGHT TO MSP. MAINTE NANCE VISUALLY INSPECTED NR 2 REVERSER FOR SECURITY AND ADJUSTED TARGET OF LOCK PROXIMITY SENSOR PER MM 78-30-01 PG 501. OPERATIONAL CHECK WAS NORMAL. 2 L 7 4 4F RT A20WE 1996011200262 19960112 00262 NE 1996 1 12 9600336628 2 19960105 A 7250 TURBINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE FAILED A NWAA A E F J UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 628US 22389 02037 DURING CLIMB, THE NR 2 ENGINE FIRE WARNING ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING MANUAL, FIRED BOTTLE, IFSD AND SUBSEQUENTLY DUMPED 147,000 LBS OF FUEL AND RETURNED TO LAX. MAINTENANCE FOUND NR 2 ENGINE TURBINE EXHAUST CASE UNCONTA INED FAILURE. REPLACED NR 2 ENGINE AND CHECK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996011200263 19960112 00263 NM 1996 1 12 9600436625 1 19960110 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 625US 21707 DURING LINE CHECK, FOUND THE STATE ROOM EMERGENCY TRACK LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY PACK A ND FUNCTIONAL CHECK WAS NORMAL. 2 L 7 4 4F A20WE 1996011200264 19960112 00264 EU 1996 1 12 96FDEA00036 1 19960109 A 2750 SOLENOID VALVE AIRBUS 310 A310203 EU FLAP SYST FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 414FE 400 TPE - AFTER T/O, FLAPS WERE VERY SLOW TO RETRACT, FLAPS/SLATS STUCK AT ZERO DEGREES. FOLLOWED EMERGENCY/ABNORMAL PROCED URE AND RETURNED TO TPE. FLAPS RETRACTED TO ZERO DEGREE DETENT ON THE GROUND AND THE FLAP SYS NR 1 FAULT LIGHT ILLUMINA TED. REMOVED AND REPLACED HIGH SPEED SOLENOID VALVE, WORKS OK (P/N 500A000-03), OFF (S/N 03601). BITE TEST ON SFCC NR 1, ALL OK PLACARD REMOVED AND NOTIFIED MOCC. 2 L 7 2 4F RT A35EU 1996011200265 19960112 00265 NM 1996 1 12 96UAL900019 1 19960109 A 3350 BATTERY BOEING 737 737222 1384473 NM COCKPIT DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9045U 19551 FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY AND CHECKS OK. 2 L 7 2 4F A16WE 1996011200266 19960112 00266 NM 1996 1 12 96UAL900020 1 19960109 A 2820 FUEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL SYSTEM IMBALANCE A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 7274U 21421 AIRCRAFT REQUIRES 3 UNITS OF AILERON TRIM FOR LEVEL FLIGHT. FLIGHT DIVERTED TO RAP DUE TO AIRCRAFT DEVELOPED FUEL IMBAL ANCE EN ROUTE. CAUSE OF UNBALANCE UNDETERMINED. MAINTENANCE CHECKED FUEL TANKS WITH DRIPSTICKS AND FOUND A DIFFERENCE OF ONLY 1,000 POUNDS. 2 L 7 3 4F 4 F A3WE E2EA 1996011200267 19960112 00267 WP 1996 1 12 96UAL900021 1 19960109 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 1813U 46612 WHEN BOARDING AIRCRAFT GOT ACRID ODOR APPARENTLY FROM AIR CONDITIONING SYSTEM. WORSE AFTER ENGINE START AND TAKEOFF. A LL GAUGE INDICATIONS NORMAL, COULD NOT DUPLICATE. BURNED OUT PACKS AND REPLACED ALL COALESCER BAGS. 2 L 7 3 4F 4 F A22WE E23EA 1996011200268 19960112 00268 1996 1 12 MWEA96003 4 19960110 A 2565 13621225 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAIL COMPT LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING SERVICE CHECK, FOUND TAIL COMPARTMENT EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED EVAC SLIDE. 2 L 7 2 4F A6WE 1996011200269 19960112 00269 EU 1996 1 12 QXEA9600007 1 19960103 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 GEG - TWO OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A20EU 1996011200270 19960112 00270 EU 1996 1 12 QXEA9600008 1 19960103 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 GEG - TWO 28V CABIN OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1996011200273 19960112 00273 NM 1996 1 12 QXEA9600011 1 19960105 A 3260 864202 SENSOR ELDEC DHAV DHC8 DHC8102 2809003 NM NLG INTERMITTENT A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 825PH 213 SEA - NOSE GEAR RED UNSAFE ADVISORY LIGHT AND GEAR HANDLE LIGHT CYCLED ON AND OFF FOR VARYING LENGTHS OF TIME IN CRUISE. AIRCRAFT LANDED IN SEA WITHOUT FURTHER PROBLEM. AIRCRAFT INSPECTED AND FERRIED TO PDX. NLG DRAG STRUT PROX SENSOR FA ILED AIR/GRO TEST. DRAG STRUT PROX SENSOR REPLACED AND CHECKED GOOD IAW MAINT MANUAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996011200275 19960112 00275 EU 1996 1 12 QXEA9600013 1 19960106 A 3397 WIRE FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 BOI - FLOOR PROXIMITY LIGHTING BETWEEN 6 C, D, E AND 9 C, D, E INOP. REPAIRED BROKEN WIRE AT BATTERY PACK CANNON PLUG. 2 L 7 2 4F RT A20EU 1996011200276 19960112 00276 EU 1996 1 12 QXEA9600014 1 19960107 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 SEA - LIGHT ON EMERGENCY EXIT HANDLE ROW 8 RIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996011200277 19960112 00277 NM 1996 1 12 QXEA9600015 1 19960107 A 3350 321430 BATTERY PACK DORNER DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 330PH 3008 PDX - EXIT SIGN ABOVE SEAT 11A AND RIGHT SIDE AFT EXTERIOR INOP. REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996011200279 19960112 00279 SW 1996 1 12 SWIA95704 1 19960101 A 5210 PRESSURE LINE SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CUT A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 27220 AC718 A/C WOULD NOT PRESSURIZE, CABIN DOOR WAS LEAKING. CABIN DOOR SUPPLY LINE CUT. REMOVED AND REPLACED SUPPLY LINE WITH NE W ONE, OPS CHECKS GOOD. 1 L 7 2 4T A8SW 1996011200280 19960112 00280 SO 1996 1 12 SWIA95705 1 19960104 A 2750 CONNECTORS EMB 120 EMB120ER 3260203 SO LT TE FLAPS LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 AFTER TAKEOFF, TRIED TO RETRACT FLAPS AND THEY ONLY WENT UP TO ABOUT 7 DEGREES, RECEIVED A FLAP DISAGREEMENT WARNING. W E THEN RETURNED FOR LANDING AT SLC. AFTER TOUCHDOWN THE FLAPS RETRACTED. BEFORE TAKEOFF WE GOT DE-ICED WITH FLAPS DOWN 45 DEGREES AS 50P. FOUND DE-ICE FLUID IN CANNON PLUGS ON LT OUTBOARD FLAP ACTUATOR. CLEANED AND SECURED PLUGS, CYCLED FLAPS NUMEROUS TIMES, NO DEFECTS NOTED AND OPS GOOD. 2 L 7 2 4T RT A31SO 1996011200281 19960112 00281 EA 1996 1 12 SWIA95706 1 19960107 A 2421 IDG CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A SWIA K NONE O OTHER CR CRUISE 1 NM 07 409SW 7056 NR 1 IDG CAUTION MESSAGE ILLUMINATED IN FLIGHT. IDG DISCONNECTED PER CHECKLIST. REMOVED AND REPLACED NR 2 IDG ON RIGHT HAND ENGINE. RAN ENGINE, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 1996011200282 19960112 00282 NM 1996 1 12 UPS205183 1 19960109 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 209UP 21698 YHM - MAINTENANCE REPORTED, L-1 EMERGENCY LIGHT IS INOP. RESERVED L-1 EMERGENCY LIGHT ASSY AND ASSY CHECKED SERVICEABLE . 2 L 7 3 4F A3WE 1996011200428 19960112 00428 WP 1996 1 12 IXXA95134 1 19960103 A 3230 GRND SHIFT MECH DOUG DC8 DC862 3021970 WP NLG OUT OF RIG A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 51CX 46027 ON DEPARTURE OUT OF EWR, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'RETRACT' POSITION. THE AIRCRAFT APPEARED TO BE STUCK IN THE 'GROUND' MODE. THE AIRCRAFT RETURNED TO EWR FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FA CILITY WHERE THE NOSE LANDING GEAR WAS DISASSEMBLED, INSPECTED, AND RESEALED, AND THE GROUND SHIFT MECHANISM WAS RIGGED. THE LANDING GEAR WAS OPERATIONALLY CHECKED AND DETERMINED TO BE OPERATING NORMALLY FOLLOWING THE RE-RIG. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996011200518 19960112 00518 WP 1996 1 12 9600349101 1 19960103 A 5320 FITTING DOUG DC9 DC915 3022036 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR UPPER LEFT AND RIGHT STOP FITTINGS. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996011200519 19960112 00519 WP 1996 1 12 9600359610 1 19960103 A 5720 FITTING DOUG DC9 DC932 3022066 WP CTR WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE CENTER WING END FITTING (SECOND STRINGER FROM THE FOR WARD END). REPLACED END FITTING (P/N 3920326-501N) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996011200520 19960112 00520 WP 1996 1 12 9600369941 1 19960103 A 5720 FITTING DOUG DC9 DC932 3022066 WP WS 69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE RIGHT WING LOWER AFT FLANGE FOOT OUTBOARD OF XRS 69 AT STR 18. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996011200521 19960112 00521 WP 1996 1 12 9600371154 1 19960104 A 5320 SPLICE FITTING DOUG DC10 DC1040 3023508 WP FS 1718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON THE STR 52 SPLICE FITTING AT FS 1718. FABRICATED AND INSTALLED PER AFA 7102-1 AND SR M 53-10-00. 2 L 7 3 4F A22WE 1996011200522 19960112 00522 WP 1996 1 12 9600389605 1 19960104 A 5341 FITTING DOUG DC9 DC932 3022066 WP FS 598-620 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT WING TO FUSELAGE ATTACH FITTING BETWEEN STR 22L - 23L, FS 598 - 620. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996011200523 19960112 00523 WP 1996 1 12 9600399938 1 19960106 A 5320 FITTING DOUG DC9 DC931 3022065 WP DOOR STOP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1798U 47369 DURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR RIGHT SIDE STOP FITTING. REPLACED FITTING PER SRM 51-30-0. 2 L 7 2 4F A6WE 1996011200524 19960112 00524 WP 1996 1 12 9600409870 1 19960106 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 701-708 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 29L KEEL FITTING BETWEEN FS 701 - 708. REPLACED FITTING PER SRM 51-10-4 . 2 L 7 2 4F A6WE 1996011200525 19960112 00525 WP 1996 1 12 9600419602 1 19960106 A 5320 FITTINGS DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE INTERCOSTAL SUPPORT FITTINGS FS 996, BETWEEN LONGERONS 27L - 28L AND BETWEEN 27R - 28R. REPLACED FITTINGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996011200526 19960112 00526 WP 1996 1 12 9600429602 1 19960106 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 598-639 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 24R KEEL BEAM FITTING BETWEEN FS 598 - 639 . REPLACED FITTING PER SRM 51-00. 2 L 7 2 4F A6WE 1996011200527 19960112 00527 NM 1996 1 12 9600446307 1 19960110 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 52L TO 58L WERE FOUND INOPERATIVE. RECONNE CTED LIGHT PIN IN FLOOR TRACK. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200528 19960112 00528 EU 1996 1 12 96FDEA00037 1 19960110 A 5101 STRUCTURE AIRBUS 310 A310221 3930310 EU AIR FRAME VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 416FE 288 AFTER TAKEOFF WITH GEAR UP, A/C STARTED VIBRATING. GEAR WAS CYC DOWN & UP WITH NO PROBLEMS. VIB CONTD. LEVEL OFF AT 5 000 FEET. FLAPS/SLATS RETRACTED, VIBRATION STOPPED AT PWR REDUCTION (VIB WAS MOD). RETND FOR LANDING WITH NORMAL SLAT/ FLAP EXTENSION & NO VIB AT REDUCED PWR. PERFORMED WALKAROUND INSP OF RUDDER, LANDING GEAR, STABILIZER, FLAPS AND SLATS, AILERONS, SPOILERS, ELEVATORS ALL CK'D OK FROM GROUND. PERFORMED HI-PWR ENG RUN PER MM 71-00-00, PG A588 IN CONJUNCTIO N WITH A300 FLT MANUAL, REF 5-3-2. PARAM CK'D WITH PUBLISHED LIMITS FOR WEATHER CONDITIONS. 1.489 NR 1 ENG N1=1.2, N2= .6, NR 2 ENG N1=.4, N2=6. VISUALLY INSP ENG SHROUDS, BLADE TIPS, & RUB STRIPS PER MM 72-23-01, PG 601-606, CK'D GOOD. 2 L 7 2 4F RT A35EU 1996011200529 19960112 00529 WP 1996 1 12 ABXA9600005 1 19960104 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 905AX 6864 47147 DURING SERVICE CHECK, IT WAS NOTED EMERGENCY EXIT LIGHTS DO NOT EXTINGUISH WITH SWITCH IN OFF POSITION WHEN AIRCRAFT POW ER IS TURNED OFF. REPLACED EMERGENCY LIGHT'S BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0. 2 L 7 2 4F A6WE 1996011200530 19960112 00530 WP 1996 1 12 ABXA9600006 1 19960103 A 5280 5616307501 DOOR DOUG DC8 DC862 3021970 WP LT MG DAMAGED A ABXA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 803AX 46077 THE GEAR UNSAFE LIGHT ILLUMINATED IN-FLIGHT. RECYCLED GEAR WITH NO EFFECT. DOWN INDICATIONS NORMAL. GEAR DOOR LATCH L IGHTS WERE CHECKED AND LEFT DOOR INDICATED UNLATCHED. FOUND LEFT LANDING GEAR DOOR DAMAGED DUE TO ICE ACCUMULATION. RE PAIRED DOOR IAW ABX REA D825-13919. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW DC-8 MM 32-30-0. 2 L 7 4 4F 4A25 1996011200531 19960112 00531 WP 1996 1 12 ABXA9600007 1 19960109 A 3240 305323001 CONTROL VALVE DOUG DC8 DC861 3021952 WP BRAKE SYST BROKEN A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 847AX 6892 46031 LEFT BRAKES GO FULL TRAVEL WITH NO BRAKING ACTION. BRAKE PRESSURE AND FLUID QUANTITY ARE NORMAL. REPLACED BROKEN BRAKE CONTROL VALVE IAW DC8 MM. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200532 19960112 00532 WP 1996 1 12 ABXA9600008 1 19960110 A 3040 TERMINAL DOUG DC8 DC863 302198A WP WINDSHIELD HEAT DIRTY A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 816AX 46093 DURING CRUISE, ELECTRICAL TYPE FUMES WERE NOTED FROM AREA OF CAPTAIN'S GLARESHIELD. TURNED OFF WINDSHIELD HEAT AND SMEL L SEEMED TO DISSIPATE, BUT THERE WAS A RESIDUAL SMELL LATER. PULLED CIRCUIT BREAKERS FOR FLOOR HEATERS AND SMELL SEEMED TO GO AWAY. INSPECTED THE FLOOR HEATERS AND ELECTRICAL CONNECTORS AND NO DEFECTS WERE NOTED. INSPECTED CAPTAIN'S WIND SHIELD AND TERMINAL BLOCK. FOUND DIRT ON MATING SURFACE BETWEEN WINDSHIELD AND TERMINAL BLOCK THAT CAUSED THE TERMINAL BLOCK TO BECOME HOT. CLEANED MATING SURFACE AND INSTALLED NEW HARDWARE. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200533 19960112 00533 1996 1 12 COMA9610006 4 19960109 A 3413 066500011801 VSI EMB 120 EMB120RT SO LEFT DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 255CA 275 120238 PILOTS VSI TUBE BLANK. REPLACED THE 1VA-81A TA/VS1. 2 L 7 2 4T RT A31SO 1996011200534 19960112 00534 SO 1996 1 12 COMA9610007 1 19960108 A 2751 INDICATION EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 256CA 120245 FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY - ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011200535 19960112 00535 SO 1996 1 12 COMA9610008 1 19960108 A 5753 KRP138112VT ROLLER EMB 120 EMB120RT SO LT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 256CA 120245 FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. REPLACED WORN ROLLERS ON LT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1996011200536 19960112 00536 SO 1996 1 12 COMA9610009 1 19960109 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 269CA 14680 2007 120263 EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 5 IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. 2 L 7 2 4T RT A31SO 1996011200537 19960112 00537 SO 1996 1 12 COMA9610010 1 19960106 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO LT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 266CA 120258 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED LT OUTBOARD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996011200538 19960112 00538 SO 1996 1 12 COMA9610011 1 19960106 A 5753 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 179CA 120179 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE - CLEANED FLAP TRACKS AND ROLLERS AND RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011200539 19960112 00539 SO 1996 1 12 COMA9610013 1 19960109 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 267CA 120259 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED WORN ROLLERS ON RT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1996011200540 19960112 00540 SW 1996 1 12 COMA9620002 1 19960109 A 7712 TQ SIG COND SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE FAILED A COMA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 704C 1937 AC704 44588 RIGHT ENGINE DID NOT ACHIEVE CHARTED TAKEOFF POWER. SWAPPED TORQUE SIGNAL CONDITIONER TO SPARE BRIDGE. ENGINE PERFORMA NCE SATISFACTORY. 1 L 7 2 4T 4 T A8SW E4WE 1996011200541 19960112 00541 EU 1996 1 12 COMA9630010 1 19960108 A 3246 5009237 RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU LT MLG WHEEL SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 344CA 405 OCT910062 340A025 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO MATE FOUND FLAT. DURING INSPECTION, FOUND INNER RACE SPUN. SUB-ASSY HAS BE EN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR AND OVERHAUL. 2 L 7 2 4T RT A52EU 1996011200542 19960112 00542 EU 1996 1 12 COMA9630011 1 19960109 A 3020 NH2466881 INLET SAAB SF340 SF340A 7850100 EU RT ENGINE BURNED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 347CA 5314 4737 340A028 RIGHT ENGINE INLET HEAT FAILED AND LOWER INLET SECTION IS BURNED. REPLACED THE FORWARD LOWER INLET. 2 L 7 2 4T RT A52EU 1996011200543 19960112 00543 EA 1996 1 12 COMA9660007 1 19960109 A 2613 356024310 ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 924CA 7026 LEFT 14TH STAGE DUCT OVERHEAT WARNING IS ON INTERMITTENTLY DURING FLIGHT. REPLACED THE PYLON SECTION OF THE 14TH STAGE BLEED LEAK DETECTION SYSTEM. 2 L 7 2 4F RT A21EA 1996011200544 19960112 00544 EA 1996 1 12 COMA9660008 1 19960110 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 7038 FLAPS ARE STUCK AT ZERO DEGREES. COULD NOT DUPLICATE DISCREPANCY, SYSTEM FUNCTION CHECK NORMAL. ACFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A21EA 1996011200545 19960112 00545 EA 1996 1 12 COMA9660009 1 19960110 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 929CA 882 882 7035 NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996011200546 19960112 00546 EA 1996 1 12 COMA9660010 1 19960110 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 946CA 471 471 7072 THE NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996011200547 19960112 00547 NM 1996 1 12 DHLA720007 1 19960109 A 2780 106081917 SWITCH BOEING 727 727228 NM NR 2 LE FLAP FAILED A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 DURING CLIMB, FLAPS UP LEADING EDGE LIGHT INTERMITTENTLY ON. DURING FLAP EXTENSION, NR 2 L/E FLAP DID NOT LOCK UP. YEL LOW AND GREEN L/E FLAP LIGHTS ON FORWARD PANEL WERE ALTERNATING. CHRISTMAS TREE INDICATED INTERMITTENT YELLOW LIGHT FOR NR 2 L/E FLAP. AT FLAPS 5 DEGREES, ALL GREEN INDICATION. INSPECTED FLAPS. NO DEFECT NOTED. REMOVED AND REPLACED FLA P INDICATING SWITCH. OPS CHECK OK. REF 27-82-1. 2 L 7 3 4F A3WE 1996011200548 19960112 00548 WP 1996 1 12 SCNA96004 1 19960108 A 3234 580500 CONTROL CABLE DOUG DC10 DC1015 3022118 WP COCKPIT OUT OF ADJ A SCNA O OTHER O OTHER CL CLIMB 1 GL 15 152SC 48289 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETRACTED GEAR WITH HANDLE RELEASE BUTTON AND GEA R RETRACTED NORMALLY. ADJUSTED PUSH/PULL CABLE ROD END PER MM 32-21-01, ANTI-RETRACTION OPS CHECKED NORMAL ON GROUND. 2 L 7 3 4F A22WE 1996011200549 19960112 00549 WP 1996 1 12 UPS805189 1 19960110 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED LONGERON 34R ATTACH FITTING AT STA 8.00 CRACKED, EVIDENCE OF CORROSION. WILL REPAIR/REPLACE FITTING PER UPS E.O. DC8 SRM. 2 L 7 4 4F RT 4A25 1996011900001 19960119 00001 WP 1996 1 19 9600451158 1 19960102 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP FUSELAGE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 158US 46767 DURING LINE CHECK, FOUND THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED BITE TEST. REPLACED THE AFT POWER SUPPLY AND BATTE RY PACK. 2 L 7 3 4F A22WE 1996011900002 19960119 00002 WP 1996 1 19 9600469998 1 19960111 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE CHECK, EMERGENCY FLOOR PATH LIGHT AT REAR OF CABIN INOPERATIVE. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900003 19960119 00003 WP 1996 1 19 9600479935 1 19960110 A 3222 SCHRADER VLV DOUG DC9 DC931 3022065 WP NLG STRUT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE AND THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT AND REPLACED SCHRADER VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900004 19960119 00004 EU 1996 1 19 9600483208 1 19960109 A 2611 SMOKE ALARM AIRBUS 320 A320211 3930320 EU CARGO COMPT ACTIVATED A NWAA D F RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 308US 107 DURING TAXI AFT CARGO SMOKE ECAM INDICATION ILLUMINATED AND DISCHARGED EXTINGUISHING AGENT. AIRCRAFT RETURNED TO THE GA TE AND FIRE DEPARTMENT INVESTIGATED SOURCE OF INDICATION. NO DETECTION OF FIRE OR SMOKE NOTED. MAINTENANCE VERIFIED NO EVIDENCE OF FIRE OR SMOKE AND REPLACED THE FIRE EXTINGUISHING BOTTLE. SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A28NM 1996011900005 19960119 00005 NE 1996 1 19 9600492295 2 19960103 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 295US 21506 696495 NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE INSPECTED THE ENGINE AND NO DISCREPANCIES WERE NOTED. AIRCRAFT CONTINUED IN SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996011900006 19960119 00006 NE 1996 1 19 9600509878 2 19960101 A 7320 FUEL CONTL SYST DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 787NC 48149 688767 NR 1 ENGINE WOULD NOT DEVELOP TARGET EPR FOR TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE TRIMMED THE ENGINE AND SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996011900007 19960119 00007 EU 1996 1 19 9600513245 1 19960111 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU PIT PANEL INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 345NW 10254 5008 399 DURING SYSTEM TEST, THE EMERGENCY LIGHT FAILED AT PTT PANEL, COM EMER L FAULT. REPLACED THE POWER SUPPLY AND BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1996011900008 19960119 00008 EU 1996 1 19 9600523245 1 19960109 A 2913 4205400 HYD PUMP AIRBUS 320 A320211 3930320 EU NR 2 ENGINE FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 345NW 9683 399 DURING CLIMB UPON FLAP RETRACTION, LOST YELLOW SYSTEM HYDRAULIC FLUID. FLIGHT RETURNED TO MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE YELLOW PTU PLUG BLOWN OUT AND THE NBR 2 ENGINE DRIVEN HYDRAULIC PUMP INOPERATIVE. REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, 2-WAY HYDRAULIC VALVE, PTU MANIFOLD, AND PRIORITY VALVE. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1996011900009 19960119 00009 WP 1996 1 19 9600531211 1 19960111 A 4900 TSCP7004B APU DOUG DC10 DC1030 3023501 WP TAIL FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 211NW 54569 2234 46868 DURING CLIMB, A STRONG OIL SMELL WAS PRESENT THROUGH OUT THE AIRCRAFT. FLIGHT CREW FOLLOWED SMOKE REMOVAL PROCEDURES, B UT ODOR COULD NOT BE ISOLATED. FLIGHT RETURNED TO DEPARTURE AIRPORT LANDING WITHOUT FURTHER INCIDENT. GROUND PERSONNEL REMOVED AND REPLACED ALL THREE WATER SEPARATOR BAGS AND DETERMINED THAT APU WAS SOURCE OF ODOR. APU PLACED ON MEL. 2 L 7 3 4F A22WE 1996011900012 19960119 00012 1996 1 19 9600569163 4 19960109 A 3454 5224280102 NAV RECEIVER DOUG DC9 DC914 3022034 WP NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8906E 42076 45747 CAPTAIN'S NAV RECEIVER FAILED SHORTLY AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 NAV RECEIVER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900013 19960119 00013 WP 1996 1 19 9600579139 1 19960110 A 3350 60030451 BATTERY PACK DOUG DC9 DC914 3022034 WP RT EXTERIOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 47049 DURING PERIODIC CHECK, RIGHT EXTERIOR EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK AND OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1996011900014 19960119 00014 WP 1996 1 19 9600589180 1 19960108 A 3350 6011779 BATTERY PACK DOUG DC9 DC914 3022034 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3312L 45707 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIO NAL CHECK OK. 2 L 7 2 4F A6WE 1996011900015 19960119 00015 NM 1996 1 19 9600599311 1 19960111 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TWO ROWS OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011900016 19960119 00016 WP 1996 1 19 9600609851 1 19960108 A 3350 CONNECTOR DOUG DC9 DC951 3022051 WP BATTERY PACK CONTAMINATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. CLEANED CANNON PLUG ON BATTE RY PACK. 2 L 7 2 4F A6WE 1996011900017 19960119 00017 NM 1996 1 19 96FDEA00049 1 19960113 A 2780 656021211 MODULE BOEING 727 727225 1384077 NM LE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 467FE 21449 NR 1 LED SLAT, LT WING DID NOT RETRACT WHILE GOING FROM FLAP 5 TO FLAP 2. AMBER LIGHT ON FRONT PANEL WAS ON AND S/O PAN EL IND AMBER, INTRANSIT RED TABS COMPLETED WITH SAME IND. ALSO, WING ANTI-ICE ATTEMPTED. NR 1 SLAT FUNCTIONS NORMAL, P OSITION SWITCH INOPERATIVE. APPLIED HEAT TO NR 1 RETRACT SWITCH, NO HELP. INSTALLED SWITCH CONTACT JUMPER, NO HELP. R EPLACED L/E POS CONTROL MODULE, RAN FLAPS THROUGH NUMEROUS CYCLES AND ALL IND NORMAL. 2 L 7 3 4F A3WE 1996011900018 19960119 00018 NM 1996 1 19 96FDEA00050 1 19960111 A 5320 WEB BOEING 747 747245F 1384897 NM BS 1241 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - CENTER SECTION TANK AFT FACE WEB EXTERIOR FOUND EXFOLIATED AT BS 1241 WL 172, BETWEEN LBL 5 TO 80 AS MARKED. 2 L 7 4 4F A20WE 1996011900019 19960119 00019 NM 1996 1 19 96FDEA00051 1 19960111 A 5320 WEB BOEING 747 747245F 1384897 NM BS 1241 EXFOLIATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 CENTER SECTION TANK AFT FACE WEB EXTERIOR FOUND EXFOLIATED AT BS 1241 WL 172 BETWEEN RBL 80 TO 104. REPAIR CARRIED OUT AS PER ERA B57-10-94. 2 L 7 4 4F A20WE 1996011900020 19960119 00020 NM 1996 1 19 96FDEA00052 1 19960112 A 5280 DOOR DOUG MD11 MD11F 3023600 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LT MLG DOOR HAS 2 INCH CRACK AT UPPER MID HINGE AREA, LWR SKIN. 2 L 7 3 4F RT A22WE 1996011900021 19960119 00021 NM 1996 1 19 96FDEA00053 1 19960112 A 5280 DOOR DOUG MD11 MD11F 3023600 NM CTR GEAR DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CENTERLINE LANDING GEAR DOOR, LT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED LOWER CORNER SECTION LOCATE D NEW FRAME, INSTALLED NEW FRAME PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900022 19960119 00022 NM 1996 1 19 96FDEA00054 1 19960112 A 5280 ANB73872 FRAME DOUG MD11 MD11F 3023600 NM CTR GEAR DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CENTERLINE LANDING GEAR DOOR, RT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900024 19960119 00024 NM 1996 1 19 96FDEA00056 1 19960115 A 5320 65453133 STRINGER CLIP BOEING 727 727227 1384078 NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CRACKED STR CLIP AT BS 440 STR 1L. UPON REMOVAL OF CRACKED STR CLIP FOUND STR NR 1 TO BE DAMAGED AT BS 441. PERFORMED STR REPAIR BS 436 TO 446 STR NR 1 IAW FEDEX SRM 53-10-3 AND INSTALLED NEW STR CLIP BS 440 STR NR 1. 2 L 7 3 4F A3WE 1996011900025 19960119 00025 NM 1996 1 19 96FDEA00057 1 19960115 A 5314 KEEL BEAM BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AT BS 950D PLUS 3, LBL 10. REMOVED CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AND REPAIRED PER FEDEX EA 7-5310-26837. 2 L 7 3 4F A3WE 1996011900026 19960119 00026 NM 1996 1 19 96UAL900022 1 19960110 A 3350 BATTERY BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE GALLEY DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9013U 19051 AFT GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AND CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996011900027 19960119 00027 EU 1996 1 19 96UAL900023 2 19960110 A 7230 COMPRESSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE BIRD STRIKE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN C Y F.O.D. ENGINE STOPPAGE CL CLIMB 1 WP 29 350UA 24301 721649 NUMBER ONE ENGINE FAILED DURING ROTATION. HEAVY FIRST STAGE FAN DAMAGE. A BIRD STRIKE WAS THE CAUSE OF THE ENGINE FAIL URE. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011900028 19960119 00028 EU 1996 1 19 96UAL900024 2 19960110 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 312UA 23673 720804 NUMBER TWO ENGINE WENT TO 935 DEGREES, ABORTED TAKEOFF AT 90 KNOTS. THE ENGINE EXPERIENCED AN EXHAUST GAS TEMPERATURE E XCEEDENCE, DUE TO NORMAL ENGINE PERFORMANCE DETERIORATION. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR. HIGH PR ESSURE TURBINE HARDWARE DID NOT REVEAL ANY OUT OF THE ORDINARY CONDITIONS. THIS ENGINE ACCUMULATED 9049 HOURS SINCE LAS T SHOP VISIT. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011900029 19960119 00029 NM 1996 1 19 96UAL900025 1 19960110 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM AFT ENTRY DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7444U 21898 AFT ENTRY DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996011900030 19960119 00030 NM 1996 1 19 96UAL900026 1 19960111 A 3350 LIGHT BOEING 727 727222 1384073 NM CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7255U 21402 1 LEFT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH LOSS OF ESS POWER. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996011900031 19960119 00031 NE 1996 1 19 96UAL900027 2 19960111 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 610UA 21871 707515 HIGH VIBRATION, NUMBER TWO ENGINE. TROUBLESHOT PROBLEM PER 767-200 MM 71-05-00, PAGES 120 TO 121. REPLACED OIL FILTER, LOOKED AT MAGNETIC CHIP DETECTORS, CHECKED ENGINE INLET AND EXHAUST FOR DAMAGE OR METAL FRAGMENTS. PERFORMED A HIGH PO WER ENGINE RUN AND NO PROBLEMS FOUND. MAXIMUM VIBRATION DURING HIGH POWER RUN WAS 0.5 MILS AT 1.4 EPR, LIMIT IS 5.0 MIL S. PROBLEM HAS NOT BEEN DUPLICATED SINCE ORIGINAL WRITE-UP. 2 L 7 2 4F 4 F RT A1NM E3NE 1996011900032 19960119 00032 NM 1996 1 19 96UAL900028 1 19960111 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7277U 21424 THE AFT CABIN DOOR EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996011900033 19960119 00033 NM 1996 1 19 96UAL900029 1 19960112 A 3350 LAMP BOEING 737 737222 1384473 NM CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9017U 19055 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 12. RELAMPED AND REPLACED COVER, CHECKS OK. 2 L 7 2 4F A16WE 1996011900034 19960119 00034 NM 1996 1 19 96UAL900030 1 19960112 A 2121 36144161 COOLING FAN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE AIR DISTR SYST FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 608UA 2488 21869 61500 AT START OF DESCENT, HEAVY SMOKE FILLED THE CABIN AND COCKPIT. SUPPLEMENTAL DATA UPDATE: THE APU HAD A SEVERE COOLING FAN FAILURE WHICH CAUSED OIL TO LEAK IN THE INLET PLENUM, CONTAMINATING THE AIR CONDITIONING SYSTEM. THE COOLING FAN HA D THE SHROUDED ROTOR. PART TOTAL CYCLES, 2,347. 2 L 7 2 4F 4 F RT A1NM E3NE 1996011900039 19960119 00039 WP 1996 1 19 ABXA9600013 1 19960109 A 5330 592032339 SKIN DOUG DC9 DC932 3022066 WP BS 436 PUNCTURED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 ONE INCH HOLE IN FUSELAGE BETWEEN REAR OF FORWARD BELLY DOOR AREA AND STATIC PORT. THE HOLE WAS CAUSED BY SNOW PLOW MAK ING CONTACT WITH FUSELAGE. FABRICATED AND INSTALLED REPAIR IAW REPAIR ENGINEERING AUTHORIZATION D953-14048-MR. 2 L 7 2 4F A6WE 1996011900047 19960119 00047 SO 1996 1 19 COMA9610014 1 19960111 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO RT MLG DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 4441 226 1217 MECHANIC REMOVED TIRE FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION IN WHEEL SHOP, FOUND DAMAGE TO SUB ASSY AN D KEY INSERTS ANTICIPATE BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR FURTHER INSPECTION A ND EVALUATION. 2 L 7 2 4T RT A31SO 1996011900048 19960119 00048 SO 1996 1 19 COMA9610015 1 19960111 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO RT MLG DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 264CA 4467 497 1256 MECHANIC REMOVED TIRE FROM AIRCRAFT DUE TO TIRE WORN TO LIMITS. DURING INSPECTION OF WHEEL IN WHEEL SHOP, FOUND DAMAGED KEYS DUE TO BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR INSPECTION AND EVALUATION. 2 L 7 2 4T RT A31SO 1996011900049 19960119 00049 SO 1996 1 19 COMA9610016 1 19960112 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 196CA 120196 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. CLEANED THE FLAP TRACKS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011900050 19960119 00050 SO 1996 1 19 COMA9610017 1 19960111 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 247CA 9843 120225 LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1996011900051 19960119 00051 SO 1996 1 19 COMA9610018 1 19960111 A 6120 30005000052 SCU 3000500005 EMB 120 EMB120RT SO LT\RT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 263CA 1572 745 2120 120255 AUTO-FEATHER SYSTEM WILL NOT ARM INTERMITTENTLY. REPLACED THE LT AND RT ENGINE TORQUE SIGNAL CONDITIONER UNITS. 2 L 7 2 4T RT A31SO 1996011900052 19960119 00052 1996 1 19 COMA9610019 4 19960110 A 3418 C818171 AOA EMB 120 EMB120RT SO LEFT DEFECTIVE A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 1110J 13204 4617 120110 STICK SHAKER CAME ON DURING TAKEOFF ROLL. REPLACED THE LT ANGLE OF ATTACK VANE. 2 L 7 2 4T RT A31SO 1996011900053 19960119 00053 EU 1996 1 19 COMA9630012 1 19960111 A 2731 DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEV TRIM DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 359CA 11175 2364 340A053 THE LT ELEVATOR TRIM INDICATION IS INOP. REPLACED THE LT ELEVATOR TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996011900054 19960119 00054 EU 1996 1 19 COMA9630013 1 19960111 A 5270 DOOR WARNING SAAB SF340 SF340A 7850100 EU CARGO COMPT ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 356CA 340A034 CARGO DOOR WARNING CAME ON AFTER TAKEOFF. INSPECTED CARGO DOOR MECHANISM AND WARNING SYSTEM, NO DEFECTS FOUND. ACFT RE TURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900055 19960119 00055 EU 1996 1 19 COMA9630014 1 19960112 A 3260 D494050001 CONTROL BOX SAAB SF340 SF340A 7850100 EU LANDING GEAR DEFECTIVE A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 158CA 21835 372 340A158 LANDING GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION. REPLACED THE LAND GEAR CONTROL BOX. 2 L 7 2 4T RT A52EU 1996011900056 19960119 00056 EA 1996 1 19 COMA9660011 1 19960111 A 4900 38004882 APU CNDAIR CL600 CL6002B19 EA CABIN SMOKING A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 924CA 3539 820 7026 WHILE APU WAS OPERATING AND AC PACKS IN OPERATION, THE CABIN BEGAN TO FILL WITH SMOKE. SEVERAL SECONDS LATER THE APU AU TO-SHUTDOWN OCCURRED. 2 L 7 2 4F RT A21EA 1996011900057 19960119 00057 EA 1996 1 19 COMA9660012 1 19960111 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 940CA 7048 PILOTS WINDSHIELD CRACKED DURING TAXI. REPLACED PILOTS WINDSHIELD. 2 L 7 2 4F RT A21EA 1996011900059 19960119 00059 1996 1 19 MWEA96004 4 19960112 A 2565 13621225 EVAC SLIDE DOUG DC9 DC914 3022034 WP TAILCONE LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING A-CHECK, FOUND TAIL EVAC SLIDE PRESSURE LOW. REPLACED TAIL EVAC SLIDE. 2 L 7 2 4F A6WE 1996011900060 19960119 00060 WP 1996 1 19 MWEA96005 1 19960114 A 2560 3952273501 GIRT BAR LATCH DOUG DC9 DC915 3022036 WP FWD ENTRY DOOR LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 CREW REPORTS, FWD ENTRY DOOR EVAC SLIDE GIRT BAR LATCH SPRING IS WEAK. CLEANED AND LUBED GIRT BAR LATCHES AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996011900061 19960119 00061 NM 1996 1 19 MWEA96006 1 19960114 A 2560 5956953503 SLIDE COVER DOUG MD88 MD88 3023688 NM FWD GALLEY DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 701ME 49760 CREW REPORTS, FWD GALLEY DOOR SLIDE COVER IS LOOSE. RESECURED FWD GALLEY DOOR SLIDE COVER. 2 L 7 2 4F RT A6WE 1996011900062 19960119 00062 1996 1 19 SWAA960003 2 19960109 A 7200 ENGINE BOEING 737 737317 138447P NM NR 2 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 693SW 23174 AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. RE PLACED NUMBER 2 ENGINE PER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996011900063 19960119 00063 NM 1996 1 19 SWAA960004 1 19960108 A 3230 BACR13CG2AB RELAY BOEING 737 7373H4 1384600 NM E/E COMPT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 608SW 27928 AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE. OVERRIDE TRIGGER WAS USED TO RAISE GEAR, CYCLED GEAR NORMALLY. AIRCRAFT RE TURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED RELAY R276, CHECKED AIR SAFETY SENSOR, AND OPS CHECKED PER BOEIN G M/M. 2 L 7 2 4F RT A16WE 1996011900064 19960119 00064 NM 1996 1 19 SWAA960005 1 19960108 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1121 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, BETWEEN S12 AND 13L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900065 19960119 00065 NM 1996 1 19 SWAA960006 1 19960108 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 258/875-883 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 875 TO 883, BETWEEN S1 AND 2L, BETWEEN S1 AND 2R, AT BS 258, S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900066 19960119 00066 NM 1996 1 19 SWAA960007 1 19960108 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1019, BS 340 BETWEEN S17 AND 18L, BS 256 BETWEEN S22 TO 23R A ND AT BS 310, S21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900067 19960119 00067 NM 1996 1 19 SWAA960008 1 19960108 A 5312 BLKHD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BBL 0 WL 185. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900068 19960119 00068 NM 1996 1 19 SWAA960009 1 19960108 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED 2 PLACES AT BS 178, LBL 5 TO 12 AT WL 201 TO 205, LBL 5.7. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900069 19960119 00069 NM 1996 1 19 SWAA960010 1 19960108 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986 WL 208 RBL 5, 24, 32 AND 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900070 19960119 00070 NM 1996 1 19 SWAA960011 1 19960108 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178 LBL 5 WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900071 19960119 00071 NM 1996 1 19 SWAA960012 1 19960108 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 1156 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND O/B CHORD CRACKED AT BS 1156 RBL 23 S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900072 19960119 00072 NM 1996 1 19 SWAA960013 1 19960108 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 360/907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AND SHEAR TIE AT S15 CRACKED AT BS 360 AND BS 907 S4R. REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996011900073 19960119 00073 NM 1996 1 19 SWAA960014 1 19960108 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787, S1L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900074 19960119 00074 NM 1996 1 19 SWAA960015 1 19960108 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161. REPAIRED PER TRAMCO EWO 95-0789. 2 L 7 2 4F RT A16WE 1996011900075 19960119 00075 NM 1996 1 19 UPS205187 1 19960101 A 5230 ANGLE BOEING 727 72730C 1384009 NM AFT CARGO DR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 1 BEAM UPPER I/B L-ANGLE IS CRACKED 1 INCH ON FWD END IN RA DIUS. FABRICATED BEAM L-ANGLE IAW SRM 51-40-3, 52-30-1 AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996011900076 19960119 00076 WP 1996 1 19 RRXA960001 1 19960110 A 3230 47713921 ACTUATOR PIN DOUG DC8 DC871F 302199D WP LT MLG BROKEN A RRXA K NONE J WARNING INDICATION CL CLIMB 1 WP 15 500MH 16396 45812 KPIA-KDAY - FLT 525 - UPLATCH CHECK FAILED ON GEAR RETRACTION OUT OF KPIA. CYCLED GEAR NUMEROUS TIMES AND GEAR UNSAFE A ND GEAR DOOR WARNING LIGHTS ILLUMINATED, N500MH FERRIED TO KMCN. MAINTENANCE FOUND THE LT MLG RETRACT CYLINDER PIN BROK EN. MAINTENANCE INSPECTED THE BOSS AND PIN HOLE AND FOUND SERVICABLE. MAINTENANCE INSTALLED A NEW BOSS PIN IAW SB 32-1 02. THE LEFT HAND MLG OPERATED NORMALLY ON GEAR SWING IAW 32-10-1. 2 L 7 4 4F RT 4A25 1996011900077 19960119 00077 NM 1996 1 19 UPS405206 1 19960113 A 3350 LIGHT BOEING 747 747SR46 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 688UP 20784 MAINTENANCE REPORTED, EMERGENCY LIGHTS UNARMED, LIGHT INOP. RELAMPED, NO HELP. ADJUSTED SOCKET TO MAKE PROPER CONTACT, RELAMPED AND OPS CHECK GOOD. 2 L 7 4 4F A20WE 1996011900078 19960119 00078 EU 1996 1 19 WWMA9600003 1 19960111 A 3222 STRUT SAAB SF340 340B 7860101 EU NLG REQ'D SERVICE A WWMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 306AE 340B306 THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, THE HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO FIELD WITHOUT INC IDENT. MAINTENANCE REPACKED THE LANDING GEAR STRUT DUE TO A FLUID LEAK AND POSSIBLE IMPROPER REPACK OF THE GEAR FROM TH E PREVIOUS NIGHT. THE GEAR WAS SWUNG AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900137 19960119 00137 EU 1996 1 19 VTZA96059 1 19960103 A 7722 HTMAS6F2821SW CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 493UE 7573 1266 805 IAD/WI - FLT 6181 - DURING TAKEOFF AT 0653 HOURS ON 1-3-96, ABORTED TAKEOFF DUE TO RT EGT FLUCTUATING PLUS OR MINUS 50 D EGREES ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03523 IAW M EL 76-2 ON THE RT TTL. MAINTENANCE LATER CLEARED DMI NR 03523 ON 1-4-96 BY CLEANING THE RT ENGINE ZONE 2 CANNON PLUG. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996011900138 19960119 00138 EU 1996 1 19 VTZA96060 1 19960104 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING O N OTHER FALSE WARNING CL CLIMB 1 EA 27 303UE 41015 IAD/MHT - FLT 6207 - DURING CLIMB-OUT AT 2200 HOURS ON 1-4-96, RETURNED TO IAD DUE TO THE RT MLG INTRANSIT LIGHT REMAINI NG ILLUMINATED AFTER GEAR SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT MAIN GEAR UPLOCK SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996011900177 19960119 00177 WP 1996 1 19 9600611154 1 19960102 A 5320 WEB DOUG DC10 DC1040 3023508 WP FS 1908-1921 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION IN THE FLOOR WEB AND DOUBLER AT FS 1908 TO 1921 LBL 88. REPAIRED WEB (P/N AGA 3807-5) P ER EA 11-104450. 2 L 7 3 4F A22WE 1996011900178 19960119 00178 WP 1996 1 19 9600621154 1 19960102 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP FS 1878-1908 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION IN THE MAIN CABIN SEAT TRACK FS 1878 TO 1908 AT LBL 100. REPAIRED TRACK (P/N AFA 7789-5 03) PER EA 11-104452. 2 L 7 3 4F A22WE 1996011900179 19960119 00179 WP 1996 1 19 9600639101 1 19960104 A 5347 SEAT TRACK DOUG DC9 DC915 3022036 WP FS 200-274 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CORROSION ON THE RIGHT INBOARD SEAT TRACK FROM FS 200 TO 274. REPAIRED TRACK (P/N 5910143) PER EA 91-102023. 2 L 7 2 4F A6WE 1996011900180 19960119 00180 WP 1996 1 19 9600649101 1 19960104 A 5315 FLOORBEAM DOUG DC9 DC915 3022036 WP FS 786 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CORROSION ON THE FS 786 FLOORBEAM UPPER SIDE. REPAIRED BEAM (P/N 9912243) PER EA 91-102634. 2 L 7 2 4F A6WE 1996011900181 19960119 00181 WP 1996 1 19 9600651154 1 19960105 A 5312 BULKHEAD DOUG DC10 DC1040 3023508 WP FS 1787 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND VERTICAL CRACKS IN A FS 1787 BULKHEAD STANCHION AT LBL 9, 10 INCHES ABOVE THE CARGO FLOOR LINE. R EPAIRED STANCHION PER EA 11-104463. 2 L 7 3 4F A22WE 1996011900182 19960119 00182 WP 1996 1 19 9600669302 1 19960105 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 237-446 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302RC 48055 DURING H-CHECK, FOUND CORROSION ON THE FOLLOWING FUSELAGE FRAMES; FS 237 AT LONGERON 30, FS 332 AT LONGERON 30 AND FS 44 6 AT LONGERON 29R. REPAIRED ALL FRAMES (P/N 27777930-5) PER EA 93-103399. 2 L 7 2 4F A6WE 1996011900183 19960119 00183 WP 1996 1 19 9600679905 1 19960108 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 775 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE FUSELAGE SKIN AT FS 775 AT LONERON 18R. REPAIRED SKIN PER EA 99-104044. 2 L 7 2 4F A6WE 1996011900184 19960119 00184 WP 1996 1 19 9600681225 1 19960108 A 5320 FITTING DOUG DC10 DC1030 3023501 WP FS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE CENTER GEAR WELL STRINGER FITTINGS AT LBL 21, 14, 7, BL 0, AND RBL 21 FROM BS 150 9 TO 1521. REPLACED STRINGER FITTINGS. 2 L 7 3 4F A22WE 1996011900185 19960119 00185 WP 1996 1 19 9600699601 1 19960109 A 5320 DOOR JAMB DOUG DC9 DC932 3022066 WP AFT CABIN DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE CHECK, FOUND A CRACK IN THE AFT CABIN DOOR JAMB IN THE UPPER LEFT CORNER. REPAIRED JAMB (P/N 5917463-7) PER EA 96-103427. 2 L 7 2 4F A6WE 1996011900186 19960119 00186 WP 1996 1 19 9600709302 1 19960109 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 600-675 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302RC 48055 DURING H-CHECK, FOUND CORROSION ON LONGERON 26L AT FS 600 TO 675. REPAIRED LONGERON (P/N 5936051-501) PER EA 93-103423. 2 L 7 2 4F A6WE 1996011900187 19960119 00187 WP 1996 1 19 9600711154 1 19960110 A 5330 SKIN DOUG DC10 DC1040 3023508 WP FS 1661-1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L AND 51R BENEATH THE ANTI-COLLISION B EACON. REPAIRED SKIN (P/N NFA 6214) PER EA 11-99375. 2 L 7 3 4F A22WE 1996011900188 19960119 00188 WP 1996 1 19 9600721154 1 19960110 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1401-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON LONGERONS 29R TO 31R BETWEEN FS 1401 TO 1521. REPAIRED LONGERONS PER EA 11-104451. 2 L 7 3 4F A22WE 1996011900189 19960119 00189 NM 1996 1 19 9600732298 1 19960110 A 5312 BULKHEAD BOEING 727 727251 138408H NM FS 1183 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1183 BULKHEAD TO STRINGER 30 JACK PAD FITTING. REPLACED THE FITTING PE R SRM 51-10-1. 2 L 7 3 4F A3WE 1996011900190 19960119 00190 WP 1996 1 19 9600749870 1 19960111 A 5320 FITTING DOUG DC9 DC951 3022051 WP DOOR STOP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING H-CHECK, FOUND TWO CRACKS, 2 INCHES AND 2.25 INCHES IN THE AFT ENTRY DOOR UPPER LEFT AND RIGHT DOOR STOP FITTINGS . REPLACED FITTINGS PER EM 5270-01005 AND DWG J060229. 2 L 7 2 4F A6WE 1996011900191 19960119 00191 WP 1996 1 19 9600759605 1 19960111 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 370 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A .5 INCH CRACK IN THE FORWARD CARGO FLOOR SUPPORT FITTING AT FS 370 , LONGERON 28L. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996011900192 19960119 00192 WP 1996 1 19 9600769605 1 19960111 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 756-805 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 30 END FITTING AT FS 756 TO 805. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996011900193 19960119 00193 WP 1996 1 19 9600771154 1 19960112 A 5530 FITTING DOUG DC10 DC1040 3023508 WP VERT STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND A CRACK IN THE NR 4 BANJO FITTING, FORWARD RIGHT FLANGE IN THE RADIUS. REPAIRED PER SRM 55-20-00, SHEETS 1-17. 2 L 7 3 4F A22WE 1996011900194 19960119 00194 NM 1996 1 19 9600786302 1 19960111 A 3350 LIGHT BOEING 747 747451 1384940 NM DOOR 5R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE DOOR 5R EMERGENCY SLIDE LIGHT WAS FOUND INOPERATIVE. REPLACED THE DOOR 5R SLIDE LIGHT ASSEMBLY A ND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900195 19960119 00195 NM 1996 1 19 9600796302 1 19960112 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT BOTH DOOR 2L AND 2R WERE FOUND INOPERATIVE. REPLACED EMERGENCY LIGH T BATTERY PACK AND CHARGE, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900196 19960119 00196 NM 1996 1 19 9600806309 1 19960111 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EXTERIOR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, THE AFT TWO EXTERIOR EMERGENCY LIGHTS LOCATED ON THE RIGHT WING TO BODY FAIRING WERE FOUND INOPERATIV E. REPLACED THE EXTERIOR EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900197 19960119 00197 WP 1996 1 19 9600819854 1 19960111 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 DURING LINE CHECK, FOUND THAT THE TAILCONE DID NOT RELEASE USING THE INTERIOR HANDLE. REPLACED CABLE 301A AND THE UPPER LEFT LATCH SPRING. RERIGGED THE RELEASE SYSTEM PER MM 53-50-3 PG 301 AND OPERATIONAL CHECKS OK. 2 L 7 2 4F A6WE 1996011900198 19960119 00198 WP 1996 1 19 9600829908 1 19960111 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING 'B' CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. REPL ACED THE HANDLE AND CLIPS PER EO 5350-01049. 2 L 7 2 4F A6WE 1996011900199 19960119 00199 NM 1996 1 19 9600832703 1 19960112 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8878Z 21451 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996011900200 19960119 00200 NM 1996 1 19 9600842289 1 19960114 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND THE RIGHT OVERWING MIDDLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK . 2 L 7 3 4F A3WE 1996011900201 19960119 00201 WP 1996 1 19 9600859756 1 19960113 A 3010 PRESS SWITCH DOUG DC9 DC941 302207N WP ANTI-ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 756NW 47180 EN ROUTE DTW-YHZ, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT REMAINED ON DURING WING ANTI-ICE OPERATION. FLIGHT RET URNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE TAIL ANTI-ICE VALVE, NO HELP. REPLACED THE PRESSURE SWITCH AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900202 19960119 00202 WP 1996 1 19 9600869755 1 19960113 A 3260 GEAR LIGHT DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 755NW 47179 NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDEN T. INSPECTED AND CYCLED NOSE GEAR. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900203 19960119 00203 WP 1996 1 19 9600879861 1 19960112 A 3520 90000200712 REGULATOR DOUG DC9 DC951 3022051 WP PASS OXY SYST MALFUNCTIONED A NWAA G O2 MASK DEPLOYED J WARNING INDICATION UK UNKNOWN 1 GL 01 770NC 47758 DURING CHECK OF PASSENGER OXYGEN SYSTEM IN MANUAL POSITION, PRESSURE ROSE TO 60 PSI AND OXYGEN MASKS WERE DEPLOYED THROU GHOUT THE CABIN. REPLACED THE PASSENGER OXYGEN BOTTLE AND REGULATOR, RE-STOWED ALL MASKS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900204 19960119 00204 WP 1996 1 19 9600889101 1 19960113 A 3350 6011779 BATTERY PACK DOUG DC9 DC915 3022036 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996011900205 19960119 00205 NE 1996 1 19 9600891160 2 19960112 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 168US 46769 86185 DURING LANDING WITH REVERSER DEPLOYED, THE NR 1 ENGINE EXPERIENCED A REVERSE STALL. EGT WENT TO 950 DEGREES AND THE ENG INE WAS SHUTDOWN. PERFORMED INSPECTION ON THE INLET AND EXHAUST, INSPECTION WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996011900206 19960119 00206 WP 1996 1 19 9600909902 1 19960111 A 7711 EPR INDICATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 EPR INDICATION WAS BELOW TARGET WITH THE POWER LEVER AGAINST THE FORWARD STOPS. THE TAKEOFF WAS ABORTED AND THE AI RCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996011900207 19960119 00207 WP 1996 1 19 9600919943 1 19960114 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1308T 47615 DURING LINE CHECK, FOUND EMERGENCY LIGHT EXIT SIGN BROKEN AT AFT EXIT DOOR. REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1996011900208 19960119 00208 WP 1996 1 19 9600929975 1 19960112 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LT MLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9339 47382 DURING APPROACH, THE LEFT MAIN LANDING GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR DOWN LIMIT S WITCH AND CANNON PLUG, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900209 19960119 00209 1996 1 19 9600939613 4 19960113 A 3418 9650041027 COMPUTER DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 613NW 1456 539 47438 DURING CLIMB, THE STALL INDICATION FAILURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RE PLACED THE STALL WARNING COMPUTER AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900210 19960119 00210 WP 1996 1 19 9600949935 1 19960112 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQ'D SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE AFTER LANDING GEAR RETRACTION. PULLED CIRCUIT BREAKERS TO PUT AIRCRAFT INTO FLIGHT MODE. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900211 19960119 00211 NE 1996 1 19 9600959902 2 19960114 A 7321 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 ENGINE EPR INDICATION FAILED TO REACH TARGET ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO MAIN TENANCE. THE FUEL CONTROL ASSEMBLY AND THE PT2 PROBE AND NOSE DOME ASSEMBLY WERE REPLACED. THE AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996011900212 19960119 00212 WP 1996 1 19 9600969902 1 19960112 A 7711 EPR IND DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 ENGINE EPR INDICATION FAILED TO REACH TARGET ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER, INDICATOR AND A CRACKED FITTING IN THE PT7 SYSTEM. IN ADDITION, THE EN GINE WAS FIELD TRIMMED PER PWA'S JT8D MAINTENANCE MANUAL. 2 L 7 2 4F 4 F A6WE E2EA 1996011900213 19960119 00213 NE 1996 1 19 9600979852 2 19960110 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 761NC 47116 688802 NR 2 ENGINE FAILED ON CLIMBOUT. THE ENGINE WAS SHUTDOWN AND THE FLIGHT RETURNED MAKING AN UNEVENTFUL OVERWEIGHT LANDING IN DTW. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996011900214 19960119 00214 WP 1996 1 19 9600989977 1 19960115 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9341 47390 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 5 TO 12. REPLACED THE BATTERIES AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011900215 19960119 00215 NM 1996 1 19 96FDEA00040 1 19960112 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01), ON STR FLANGE AT BS 720 STR 4L. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996011900216 19960119 00216 NM 1996 1 19 96FDEA00058 1 19960112 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 804-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE FLOOR, OVER WING AREA CORR ON O/B FLANGE FLOOR TRACK LBL 45 STA 804 TO 848 LT. INSTALLED NEW SEAT TRACK AND CHORD PER SRM 51-10-1. INSTALLATION OF FLOATING SEAT TRACK FROM STA 740 TO 760 COVERED ON NR 1415 LBL 45. 2 L 7 3 4F A3WE 1996011900217 19960119 00217 SO 1996 1 19 COMA9610020 1 19960115 A 5270 DOOR WARNING EMB 120 EMB120RT SO CARGO COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 248CA 120228 CARGO DOOR WARNING SHORTLY AFTER TAKEOFF. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST AND ACFT CONTIN UED SERVICE. 2 L 7 2 4T RT A31SO 1996011900218 19960119 00218 SO 1996 1 19 COMA9610021 1 19960115 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 161CA 120143 TAKEOFF TRIM WARNING DURING TAKEOFF ROLL. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER AND ACFT CONT INUED SERVICE. 2 L 7 2 4T RT A31SO 1996011900219 19960119 00219 SO 1996 1 19 COMA9610022 1 19960114 A 2431 40769 BATTERY EMB 120 EMB120RT SO FUSELAGE FALSE WARNING A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 196CA 8101 301 120196 BATTERY AURAL WARNING SOUNDED AFTER TAKEOFF. BATTERY TEMP GAUGE INDICATED NORMAL. REPLACED THE BATTERY. 2 L 7 2 4T RT A31SO 1996011900220 19960119 00220 SO 1996 1 19 COMA9610023 1 19960112 A 7603 CIRCUIT BREAKERS EMB 120 EMB120RT SO POWER LEVERS TRIPPED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1110J 120110 THE LT AND RT POWER LEVER FLIGHT IDLE STOP SOLENOIDS CIRCUIT BREAKERS WERE TRIPPED. RESET CIRCUIT BREAKERS AND SYSTEM T EST NORMAL. 2 L 7 2 4T RT A31SO 1996011900221 19960119 00221 SO 1996 1 19 COMA9610024 1 19960111 A 3246 118143 BEARING COVER EMB 120 EMB120RT SO LT MLG MISSING A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 269CA 110 120263 RT ANTI-SKID INOP WARNING DURING TAKEOFF ROLL. REPLACED MISSING BEARING COVER ON LT MLG WHEEL. 2 L 7 2 4T RT A31SO 1996011900222 19960119 00222 EU 1996 1 19 COMA9630015 1 19960115 A 3246 5009237 INNER RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU RT MLG SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 158CA 11714 527 JAN920214 340A158 MECHANIC REMOVED WHEEL FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HA S BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2 L 7 2 4T RT A52EU 1996011900223 19960119 00223 EA 1996 1 19 COMA9660013 1 19960114 A 3260 DISAGREE MESSAGE CNDAIR CL600 CL6002B19 EA NLG ACTIVATED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 948CA 7079 NOSE LANDING GEAR DISAGREE MESSAGE, WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE AND NO FAULTS FOUND WITH NLG. 2 L 7 2 4F RT A21EA 1996011900224 19960119 00224 EA 1996 1 19 COMA9660014 1 19960115 A 2120 601R952111 DUCT CNDAIR CL600 CL6002B19 EA AFT EQUIP BAY FAILED A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 949CA 7080 AT 31,000 FEET CABIN STARTED DEPRESSURIZING RAPIDLY. FOUND AIR CONDITIONING DUCT SEPARATED FROM THE WATER SEPARATOR. R EPLACED DUCT. 2 L 7 2 4F RT A21EA 1996011900225 19960119 00225 WP 1996 1 19 MWEA95010 1 19960110 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND FRAME AT STA 1076 LONGERON 20R IS CHAFED FROM LOOSE STANDOFF BRACKET. INSTALLED DOUBLER REPAIR IA W SRM 53-03 FIG 4. 2 L 7 2 4F A6WE 1996011900226 19960119 00226 WP 1996 1 19 MWEA96009 1 19960110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389/408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND FWD CARGO BIN FLOORBEAMS DAMAGED FROM CARGO DOOR AT STA 389 AND 408. INSTALLED ANGLE REPAIR IAW S RM 53-05 PG 289. 2 L 7 2 4F A6WE 1996011900227 19960119 00227 WP 1996 1 19 MWEA96011 1 19960113 A 5320 991556133 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND JACKPAD DOUBLER INSIDE AFT CARGO BIN AT STA 996 CORRODED BEYOND LIMITS. INSTALLED NEW DOUGLAS PAR T IAW SRM 53-01 PG 1 AND 2. 2 L 7 2 4F A6WE 1996011900228 19960119 00228 WP 1996 1 19 MWEA96012 1 19960116 A 3350 6011775 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND LEFT EMERGENCY NACELLE LIGHT INOP. REPLACED NACELLE LIGHT BATTERY PACK AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996011900229 19960119 00229 NM 1996 1 19 SWAA960016 1 19960112 A 5260 T-STRIP BOEING 737 7372H4 138448C NM AIRSTAIR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED MAINT CHECK, FOUND T-STRIP CRACKED ABOVE FWD UPPER AIRSTAIR DOORWAY STOP IN SEVERAL PLACES. REPAIRED T -STRIP PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900230 19960119 00230 NM 1996 1 19 SWAA960017 1 19960114 A 5230 FRAME BOEING 737 7375H4 138449D NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LOWER AFT DOOR STOP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900231 19960119 00231 NM 1996 1 19 SWAA960018 1 19960114 A 5320 PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED MAINT CHECK, FOUND WHEEL WELL LOWER FIXED PANEL BELOW KEEL BEAM CRACKED 1 INCH ON RIGHT SIDE ACROSS FRO M PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900232 19960119 00232 NM 1996 1 19 SWAA960019 1 19960114 A 5240 SKIN BOEING 737 7372T4 1384492 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED MAINT CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900233 19960119 00233 NM 1996 1 19 SWAA960020 1 19960114 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 772 LBL 12.25 RBL 3, RBL 7.5, RBL 8.25 AND RBL 13.25. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900234 19960119 00234 NM 1996 1 19 SWAA960021 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 RBL 4. REPAIRED PER SWA RA 1-253-1420. 2 L 7 2 4F A16WE 1996011900235 19960119 00235 NM 1996 1 19 SWAA960022 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 LBL 10. REPAIRED PER SWA RA 1-253-1419. 2 L 7 2 4F A16WE 1996011900236 19960119 00236 NM 1996 1 19 SWAA960023 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 1006 AFT FLANGE, LBL 15 TO 28. REPAIRED PER SWA RA 1-253-1417. 2 L 7 2 4F A16WE 1996011900237 19960119 00237 NM 1996 1 19 SWAA960024 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORROSION AROUND FASTENER HOLE AND MIGRATING UNDER WEB AT BS 10 16, FWD FLANGE LBL 0 TO 39. REPAIRED PER SWA RA 1-253-1415. 2 L 7 2 4F A16WE 1996011900238 19960119 00238 NM 1996 1 19 SWAA960025 1 19960114 A 5347 SEAT TRACK BOEING 737 7372T4 1384492 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND CABIN SEAT TRACK CRACKED AT SCREW HOLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900239 19960119 00239 NM 1996 1 19 SWAA960026 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FWD GALLEY FLOORBEAM CORROSION UPPER TEE CAP FASTENER BS 294 LBL 11. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996011900240 19960119 00240 NM 1996 1 19 SWAA960027 1 19960114 A 5320 BRACKET BOEING 737 7372T4 1384492 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FWD ENTRY DOOR WEB TO FRAME ATTACH BRACKET CRACKED AT BS 294 S11L. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996011900241 19960119 00241 NM 1996 1 19 SWAA960028 1 19960114 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 910 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN LAP CORRODED AT BS 910 S27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900242 19960119 00242 NM 1996 1 19 SWAA960029 1 19960114 A 5230 SKIN BOEING 737 7372T4 1384492 NM AFT CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO DOOR WEB DAMAGED AT CUTOUT LOWER AFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900243 19960119 00243 WP 1996 1 19 UPS805216 1 19960113 A 5320 FITTING DOUG DC8 DC871 302199A WP AFT BLKHD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 WHILE IN FOR B-CHECK, FOUND FITTING ON STRINGER 32R AT AFT BULKHEAD OF AIRCON COMP IS CORRODED. REMOVED AND REPLACED FI TTING. 2 L 7 4 4F 4A25 1996011900244 19960119 00244 EU 1996 1 19 WWMA9600004 1 19960113 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 320AE 340B320 THE CARGO SMOKE LIGHT ILLUMINATED AND THE CREW DISCHARGED THE NR 1 FIRE BOTTLE. THE AIRCRAFT DIVERTED TO MLU AND LANDED WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. THE DETECTOR OPTIC SENSORS WERE CLEANED AND THE CARGO FIRE EXTINGUISHER SYSTEM WAS DEFERED IAW MEL 26-4. THE AIRCAFT WAS RETURNED TO SERVICE, THE FIRE BOTTLE WAS REPLACED AND THE MEL WAS CLEARED AT THE EARLIEST OPPORTUNITY. 2 L 7 2 4T RT A52EU 1996011900245 19960119 00245 EU 1996 1 19 WWMA9600005 1 19960114 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 15 320AE 340B320 THE CARGO SMOKE LIGHT ILLUMINATED WHILE THE FLIGHT CREW WAS PREFLIGHTING THE AIRCRAFT. MAINTENANCE FOUND NO INDICATION OF SMOKE OR FIRE. THE DETECTOR ELECTRICAL CONNECTORS WERE DISCONNECTED AND THE SMOKE LIGHT STAYED ON. THE CONNECTORS W ERE RECONNECTED AND THE WEU WAS RERACKED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED. 2 L 7 2 4T RT A52EU 1996011900310 19960119 00310 WP 1996 1 19 9600999969 1 19960116 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE CHECK, FOUND COCKPIT AND FORWARD ENTRANCE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900311 19960119 00311 WP 1996 1 19 9601009937 1 19960116 A 3350 LIGHT DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE CHECK, AFT LEFT EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. REPOSITIONED LIGHT AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996011900312 19960119 00312 WP 1996 1 19 9601019945 1 19960116 A 3010 PRESS REG VLV DOUG DC9 DC931 3022065 WP AIRFOIL DE-ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 8925E 45840 DURING FLIGHT, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING WING ANTI-ICE. FOLLOWED COCKPIT OP ERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACE D ICE PROTECTION PRESSURE REGULATOR VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900313 19960119 00313 WP 1996 1 19 9601029933 1 19960116 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1334U 47280 DURING CLIMB, THE NOSE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE. AIRCRAFT RETURNE D TO YUL AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900314 19960119 00314 NM 1996 1 19 96FDEA00059 1 19960116 A 7830 7800152 TR SWITCH BOEING 727 727225 1384077 NM NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 463FE 22551 AFTER ROTATION NR 3 REVERSER OPERATING LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECKLIST AND SHUTDOWN NR 3 ENG. REPLAC ED NR 3 ENG REVERSER SWITCH PER MM 78-30-00. OPS CHECKED NORMAL, PANELS SECURED. 2 L 7 3 4F A3WE 1996011900315 19960119 00315 NM 1996 1 19 96FDEA00060 1 19960117 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE FOREFLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 THERE'S A GOUGE ON THE RT WING FOREFLAP UPPER SURFACE ABOVE THE NR 8 FLAP TRACK. REMOVED AND REPLACED DAMAGE ON O/B RT WING FOREFLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996011900316 19960119 00316 NM 1996 1 19 96FDEA00061 1 19960117 A 5311 FRAME BOEING 727 727233 138408A NM BS 720 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE IN FRAME AT BS 720B LT BETWEEN STR NR 14 TO NR 15, WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-40-3. REMOVED A ND REPLACED FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900317 19960119 00317 NM 1996 1 19 96FDEA00062 1 19960117 A 5311 FRAME BOEING 727 727233 138408A NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160. REPAIRED DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160 PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900318 19960119 00318 NM 1996 1 19 96FDEA00063 1 19960116 A 5311 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 660 LBL 34 TO 46 WL 160. REPAIRED DENTED FRAME BS 660 LBL 34 TO 46 WL 160 IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900319 19960119 00319 WP 1996 1 19 96UAL900031 1 19960115 A 3350 CIRCUIT BREAKER DOUG DC10 DC1030 3023501 WP COCKPIT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1859U 47819 EMERGENCY LIGHTS FLASH ON, THEN OFF INTERMITTENTLY WITH COCKPIT SWITCH IN THE ARMED POSITION. ALL BUSES POWERED. REPLA CED EMERGENCY LIGHTS CONTROL CIRCUIT BREAKER DUE TO DEFECT. 2 L 7 3 4F A22WE 1996011900320 19960119 00320 NM 1996 1 19 96UAL900032 1 19960115 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7444U 21898 EMERGENCY LIGHT JUST FORWARD OF FORWARD GALLEY ON THE CEILING OVER THE AISLE IS INOPERATIVE. REPLACED WEAK BATTERY PACK . 2 L 7 3 4F A3WE 1996011900321 19960119 00321 NM 1996 1 19 96UAL900033 1 19960115 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM CABIN DISCONNECTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 563UA 26665 EMERGENCY LIGHT STRIP INOP AT 13A. DISCOVERED EMERGENCY LIGHT STRIP DISCONNECTED. RECONNECTED, TESTS NORMAL. 2 L 7 2 4F RT A2NM 1996011900322 19960119 00322 NE 1996 1 19 96UAL900037 2 19960116 A 7321 MEC BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE O OTHER CL CLIMB 1 WP 29 365UA 24534 722317 NUMBER ONE ENGINE SURGED DURING CLIMB, N1 WENT FROM A TARGET OF 92 PERCENT TO 94.3 PERCENT. ALSO, HAD A 1,000 POUND INC REASE IN FUEL FLOW, THROTTLE WAS RETARDED AND ENGINE SURGED TWO MORE TIMES BEFORE IT STABILIZED. ENGINE SURGING WAS CAU SED BY AN INTERMITTENT FAILURE OF THE MAIN ENGINE CONTROL ROTARY VARIABLE DIFFERENTIAL TRANSDUCER. THE MAIN ENGINE CONT ROL WAS REPLACED AND CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996011900328 19960119 00328 WP 1996 1 19 ABXA9600026 1 19960111 A 5347 291491311M SEAT TRACK DOUG DC9 DC932 3022066 WP FS 783/872 FAILED A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 901AX 47426 DURING TAKEOFF ROLL, FS 694 SEAT TRACK FAILED PUSHING THE 'C' CONTAINER LOCK OUT OF THE SEAT TRACK. TWO BALLAST PALLETS AND ONE 'C' CONTAINER. TORE THE SEAT TRACK LOCKS FROM THE SEAT TRACKS AT FS 783 AND 872, WHICH WERE IN LOCKING POSITIO N. THE RIGHT PYLON BULKHEAD ABSORBED THE IMPACT, CONTAINERS CAME TO REST AT FS 965. THE CREW SECURED THE FREIGHT AND T HE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. INSPECTED PER REA D953-14079. REPAIRED PER REA D953-14153, D953-14159, D 953-14079 AND THE DC-9 SRM. REFERENCE WORK ORDER NR DMG 454. REA'S D925-14089 THROUGH 14152 WERE ISSUED TO THE DC-9 FL EET TO PROVIDE INCREASED SUPPORT. 2 L 7 2 4F A6WE 1996011900329 19960119 00329 WP 1996 1 19 ABXA9600027 1 19960115 A 3260 7000010101 DNLOCK SW DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A ABXA K NONE P NO WARNING INDICATION CR CRUISE 1 GL 23 900AX 47380 ON GEAR EXTENSION, NOSE WHEEL GREEN LIGHT DID NOT ILLUMINATE. RECYCLED GEAR, NORMAL INDICATIONS. REPLACED NOSE LANDING GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-0. 2 L 7 2 4F A6WE 1996011900330 19960119 00330 WP 1996 1 19 ABXA9600028 1 19960116 A 3260 80801 UPLOCK SW DOUG DC9 DC941 302207N WP MLG DEFECTIVE A ABXA K NONE N FALSE WARNING TO TAKEOFF 1 GL 23 952AX 47615 LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR, LIGHT WENT OUT AFTER TWO MINUTES, THEN ILLUMI NATED BRIEFLY AGAIN. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH IAW DC-9 SUPPLEMENTIAL MM 32-60-1. 2 L 7 2 4F A6WE 1996011900331 19960119 00331 WP 1996 1 19 ABXA9600029 1 19960115 A 7603 406175 BOLT DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE LOOSE A ABXA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 23 823AX 46122 669769 DURING CLIMB, NR 3 ENGINE COULD NOT BE CONTROLLED WITH THROTTLE INPUTS. ENGINE REMAINED AT MAX CONTINUOUS THRUST WITH T HE THROTTLE LEVER PULLED BACK TO IDLE. ENGINE WAS SHUTDOWN AND MAINTAINED A POSITIVE OIL PRESSURE DURING SHUTDOWN PROCE DURES. SECURED AND SAFETIED THE NR 3 ENGINE POWER LEVER LINKAGE AT THE FCU INPUT CLEVIS. GROUND RAN ENGINE, ALL CONTRO LS AND PARAMETERS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1996011900332 19960119 00332 NE 1996 1 19 ABXA9600030 2 19960114 A 7230 739201ABX7 C1 DISK DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 671397 DURING COMPLIANCE OF AD 80-12-51, PRATT AND WHITNEY SB 5136, FOUND CRACK INDICATIONS IN C-1 DISK, FIRST STAGE FAN BLADES . REPLACED C-1 DISK, FIRST STAGE FAN BLADES IAW ABX TEST AND MAINTENANCE RECORD WORK SHEETS, BS374A, BS375A, BS376A AND BS377A. 2 L 7 4 4F 4 F 4A25 1E8 1996011900336 19960119 00336 SO 1996 1 19 BIER960030 1 19960117 A 3297 WIRE PIPER PA31 PA31350 7103110 SO LANDING GEAR BROKEN B BIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 21 27508 317852031 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INVESTIGATION REVEALED BROKEN WIRE GOING TO LEFT GEAR SAFETY SWITCH THERE BY NOT ALLOWING ANTI-RETRACT SOLENOID FROM WORKING. 1 L 7 2 3O A20SO 1996011900337 19960119 00337 NM 1996 1 19 DL72E960069 1 19960111 A 2130 39608831 VALVE BOEING 727 727247 138408F NM RIGHT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 282WA 21484 ON CLIMBOUT THROUGH 29,000 FT, THE CABIN CONTINUED TO CLIMB THROUGH THE PRESET 4,800 CABIN ALITITUDE. DESENCED TO 18,00 0 WHERE THE CABIN STABLIZED AT 10,000. PACK BLEEDS AND OUTFLOW APPEARED OK. REPLACED RT FLOW CONTROL VALVE, LEAK CKS G OOD. PRESSURIZED A/C TO 7 PSI DIFF, ALL SYS NORMAL. 2 L 7 3 4F A3WE 1996011900340 19960119 00340 NM 1996 1 19 DL72E960086 1 19960114 A 5754 651622296 RIB BOEING 727 727247 138408F NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 SLAT NR 6, RIB NR 10 AND 12 CRACKED. REPAIRED PER M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1996011900341 19960119 00341 1996 1 19 DL72L960059 4 19960109 A 2565 SLIDE 146110015 BOEING 727 727232 1384082 NM R1 DOOR LOW PRESSURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 1992 21305 DURING INSPECTION, R-1 DOOR SLIDE PRESSURE FOUND LOW 500 LBS. REPLACED SLIDE. 2 L 7 3 4F A3WE 1996011900342 19960119 00342 NM 1996 1 19 DL72S960054 1 19960109 A 5751 657273434 SKIN BOEING 727 727232 1384082 NM AILERON DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 DURING SHOP INSPECTION, AILERON PANEL UPPER SKIN WAS FOUND DENTED. SPLICED UPPER SKIN PER SRM 57-53-5 FIG 3. 2 L 7 3 4F A3WE 1996011900344 19960119 00344 NM 1996 1 19 DL72S960068 1 19960105 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1110 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 AT MID VISIT 2, FOUND FRAME CRACKED AT STA 1110 ABOVE STR 27L. REMOVED LT FIXED FLOOR PNL FROM 1070 TO 1130 FOR ACCESS. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27 AND INSTALLED REPAIR PER SRM 53-10-4 FIG 27. 2 L 7 3 4F A3WE 1996011900345 19960119 00345 NM 1996 1 19 DL72S960081 1 19960112 A 2780 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 SETUP TO INSPECT THE ATTACH BRACKET FOR THE NR 2 LEADING EDGE FLAP ACTUATOR FOR CONDITION. FOUND ATTACH BRACKET CRACKE D AND REPAIRED PER MM 27-81-22. 2 L 7 3 4F A3WE 1996011900346 19960119 00346 NM 1996 1 19 DL72S960093 1 19960115 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 21582 AFT DOORS SLIDE EMERGENCY LTS INOP. ALSO, FWD CABIN AISLE EXIT SIGN EMERGENCY LIGHT INOP. FWD ENTRY EMERGENCY SLIDE LI GHT INOP. REPLACED BATTERY PACK AT M983, M1085 AND OPN NORMAL. REPLACED L-1 SLIDE REFLECTOR ASSY, OPN NORMAL. 2 L 7 3 4F A3WE 1996011900347 19960119 00347 NM 1996 1 19 DL72W960092 1 19960115 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 DURING C-1 LETTER CHECK, FOUND .5 INCH CRACK AT NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996011900348 19960119 00348 NM 1996 1 19 DL72W960109 1 19960113 A 3220 BUSHING BOEING 727 727247 138408F NM NLG DOOR WORN A DALA O OTHER O OTHER CL CLIMB 1 SO 27 2807W 20579 ON CLIMBOUT FROM RIC AT 360 KTS, THE NOSE WHEEL DOORS WERE SLAMMING OPEN AND SHUT REPEATEDLY. FOUND NLG DOOR OUT OF RIG AND BUSHINGS WORN IN ROD ON FWD QUAD. REPLACED ROD AND RIGGED NLG DOORS. 2 L 7 3 4F A3WE 1996011900349 19960119 00349 NM 1996 1 19 DL72W960112 1 19960109 A 2560 LANYARD BOEING 727 727247 138408F NM R1 DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 ON PREFLIGHT, FOUND R-1 DOOR SLIDE GIRT BAR LANYARD BROKEN. REPLACED LANYARD, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996011900350 19960119 00350 NM 1996 1 19 DL733960062 1 19960110 A 3230 CONTROL CABLE BOEING 737 737347 1384647 NM GEAR HANDLE LOOSE A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 302WA 23182 GEAR DOWN 3 RED AND 3 GREEN LIGHTS. RECYCLED OK 3 GREEN, HAPPENED ON 2 APPROACHS. CORRECTED CABLE TENSION FOR LANDING GEAR ACTUATOR, GEAR SWING NORMAL. 2 L 7 2 4F RT A16WE 1996011900352 19960119 00352 NM 1996 1 19 DL73E960094 1 19960109 A 5330 654688257 SKIN BOEING 737 737247 138448D NM FS 1027 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING OVERHAUL INSPECTION, MAINTENANCE FOUND A 2.5 CRACK UNDER AN EXISTING REPAIR DOUBLER AT APPROXIMATELY FS 1027, BET WEEN S-7L AND S-8L. THE CRACK PROPAGATED IN THE SKIN FROM THE LOWER FORWARD CORNER OF THE DOUBLER. IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 6, THE PREVIOUS CUTOUT UNDER THE REPAIR DOUBLER AND THE NEW DAMAGE WERE INCORPORATED INTO A SIN GLE REPAIR. 2 L 7 2 4F A16WE 1996011900353 19960119 00353 NM 1996 1 19 DL73S960100 1 19960113 A 3230 UPLOCK ACT 654482518 BOEING 737 737232 1384475 NM LT MLG FAILED A DALA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 303DL 2392 23075 LT MLG UNSAFE LIGHT ON IN FLT WITH LT GEAR VIB ALONG WITH UNSAFE INDICATION. JACKED A/C, RAN GEAR AND FOUND UNLOCK ACTU ATOR BYPASSING FLUID. REPLACED SAME, GEAR CKS OK. 2 L 7 2 4F RT A16WE 1996011900354 19960119 00354 NM 1996 1 19 DL757960055 1 19960109 A 3350 BPS73 PWR SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 EMERGENCY LIGHTS INOP AFT LT DOOR AND AFT LT OVERHEAD. REPLACED BATTERY PACK AND PWR SUPPLY. 2 L 7 2 4F RT A2NM 1996011900355 19960119 00355 NM 1996 1 19 DL757960056 1 19960109 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 EMERGENCY LIGHTS INOP AFT LT FLOOR PATH LIGHTS. REPLACED BATT PACK. 2 L 7 2 4F RT A2NM 1996011900356 19960119 00356 NM 1996 1 19 DL757960075 1 19960112 A 3230 257T110314 LEVER MODULE BOEING 757 757232 1384965 NM FLT CABIN MALFUNCTIONED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 673DL 25978 ON APPROACH TO ATL, NOSE GEAR DID NOT EXTEND, EXTENDED NORMALLY ON SECOND ATTEMPT. FOUND ACCUMULATION OF ICE ON NOSE GE AR AND HYD LINES ON AIRCRAFT ARRIVAL. INSPECTED W/W AREA, NOSE GEAR AND MECHANSM FOR DAMAGE AND NONE FOUND. JACKED AIR CRAFT, CYCLED GEAR AND OPS NORMAL. REPLACED LEVER MODULE PER MM, OPS NORMAL. 2 L 7 2 4F RT A2NM 1996011900357 19960119 00357 NM 1996 1 19 DL757960085 1 19960114 A 2530 COFFEE MAKER 811150417 BOEING 757 757232 1384965 NM CABIN SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 674DL 188 25979 ELECTRICAL SMOKE CAME OUT OF NR 1 F/C COFFEE MAKER. C/B PULLED TO STOP SMOKE. REPLACED DISPENSER, OPN NML. 2 L 7 2 4F RT A2NM 1996011900358 19960119 00358 NM 1996 1 19 DL757960090 1 19960115 A 5754 114N300219 TE WEDGE BOEING 757 757232 1384965 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 T/E WEDGE WAS FOUND TO BE DELAMINATED DURING SHOP INSPECTION FOR NR 5 L/E SLAT. THE NOTED T/E WEDGE WAS REPLACED PER SR M 57-43-02. 2 L 7 2 4F RT A2NM 1996011900359 19960119 00359 NM 1996 1 19 DL76S960106 1 19960115 A 2910 LINE BOEING 767 767332 1382001 NM WING ROOT CRACKED A DALA O OTHER K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 120DL 23279 ON APPROACH TO ATL, HAD SMOKE OR BURNING ODOR IN AFT AND MID CABIN. FOUND SLAT PRESSURE HYD LINE CRACKED AT WING ROOT F USELAGE FITTING. REPLACED HYD LINE, NO LEAKS NOTED. REPLACED PRECOOLER FILTERS DUE TO SKYDROL CONTAMINATION. 2 L 7 2 4F RT A1NM 1996011900360 19960119 00360 WP 1996 1 19 DLL10960048 1 19960107 A 3350 079123 LIGHT LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 EMERGENCY LIGHT MISSING AT SEAT 1CD. RELAMPED AND REPLACED, CHECKS GOOD. 2 L 7 3 4F A23WE 1996011900361 19960119 00361 WP 1996 1 19 DLL10960076 1 19960112 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723DA 193C1150 EMERGENCY FLOOR TRACK LIGHT OUT AT SEAT 27 H, J. REPAIRED BROKEN WIRE IN FLOOR TRACK. 2 L 7 3 4F A23WE 1996011900362 19960119 00362 WP 1996 1 19 DLL10960082 1 19960113 A 3230 1516207122 CONTROL VALVE LKHEED 1011 10113851 5265010 WP LEFT W/W MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 733DS 193C1224 AFTER T/O RAISED GEAR HANDLE, ON PILOTS PANEL RSD DOOR AND INTRANSIT LIGHT ON, ALL GREEN LIGHTS OUT. ON S/O PANEL LT GE AR OR DOOR LIGHT ON. CYCLED GEAR, NO CHANGE AND RETURNED TO LAX. REPLACED RT PHASE CONTROL VALVE, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996011900363 19960119 00363 WP 1996 1 19 DLL10960084 1 19960113 A 2750 SCREW JACK 1796062 LKHEED 1011 10113851 5265010 WP RT TE FLAP BROKEN A A DALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 27 722DA 193C1147 ON CLIMBOUT FLAPS EXTENDED 4 TO 6 DEGREES, SLATS UP WITH NO ACTUATION OF FLAP HANDLE. FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES FOR LANDING. GPWS INHIBITED AS PER PROCEDURE. REPLACED RT INBRD FLAP SCREW JACK AND BEARINGS. RIGGED AND OPS CKD GOOD. 2 L 7 3 4F A23WE 1996011900364 19960119 00364 WP 1996 1 19 DLL10960088 1 19960114 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP PWA JT8 JT8D219 52053 NE CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 717DA 62887 193C1096 725754 EMERGENCY LIGHTS IN FIRST CLASS FAILED TO ILLUMINATE DURING LAYOVER TEST. REPLACED POWER SUPPLY. 2 L 7 3 4F 4 F A23WE E9NE 1996011900365 19960119 00365 WP 1996 1 19 DLL13960057 1 19960108 A 5743 1591922 FITTING LKHEED 1011 10113851 5265010 WP LT MLG ACTUATOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 AT HMV, THE LT MLG ACTUATOR ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. TO REMOVE THE CORROSION THE FASTENER HOLE WAS OVERSIZED AND SPOTFACED IN ACCORDANCE WITH INSTRUCTIONS OF THE L1011 SRM FIG 808. THE FITTING WILL BE REPAIRE D PER L1011 SRM 57-14-00 FIG 808. 2 L 7 3 4F A23WE 1996011900366 19960119 00366 WP 1996 1 19 DLL15960067 1 19960110 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752DA 193W1172 ON LAYOVER, FOUND MID CABIN EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY, CHECKS GOOD. 2 L 7 3 4F A23WE 1996011900367 19960119 00367 WP 1996 1 19 DLL17960058 1 19960108 A 5330 1503536 SKIN LKHEED 1011 10113853 5265020 WP FS 1438 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 AT HMV IN ATL, THE FUSELAGE SKIN AT FS 1438, LBL 14 WAS FOUND CORRODED. THE REPAIR CONSISTED OF TRIMMING THE FUSELAGE S KIN AND INSTALLING A REPAIR DOUBLER AND TRIPLER PER DL ERA 272995 REV A. 2 L 7 3 4F A23WE 1996011900369 19960119 00369 NM 1996 1 19 DLM88960060 1 19960109 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DL 49533 FOUND ON D1 LTR CHECK, CORROSION AT MID CARGO DOOR THRESHOLD. REPAIRED PER SRM 53-05 FIG 63. 2 L 7 2 4F RT A6WE 1996011900370 19960119 00370 NM 1996 1 19 DLM88960066 1 19960110 A 5320 JAMB DOUG MD88 MD88 3023688 NM C1 CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 FOUND ON C2 LTR CHECK, CORROSION C1 CARGO DOOR LWR JAMB LONGERON HAS CORROSION. REPAIRED PER SRM 53-05 FIG 44. 2 L 7 2 4F RT A6WE 1996011900371 19960119 00371 NM 1996 1 19 DLM88960070 1 19960112 A 2750 5935973501 DRIVE ARM DOUG MD88 MD88 3023688 NM LT TE FLAP BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 967DL 53116 LEFT TRAILING EDGE FLAP REPORTED WITH EXCESSIVE DROOP. FOUND BROKEN LINK ON LT FLAP ACTUATOR. REMOVED LINK AND ACTUATO R. INSTALLED AFT END OF ARM ASSEMBLY, LINK AND ROD. INSTALLED ACTUATOR AND RECONNECTED LINKS, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011900372 19960119 00372 NM 1996 1 19 DLM88960108 1 19960115 A 3244 TIRE DOUG MD88 MD88 3023688 NM LT MLG BLOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 911DE 49967 AFTER TAKEOFF, RECEIVED LEFT MAIN GEAR UNSAFE LIGHT AND RETURNED FLL. FOUND NR 2 MAIN TIRE BLOWN, WITH WIRING TO SENSOR DAMAGED AND FLAP DAMAGED. REPLACED NR 1, NR 2 WHEELS AND REPAIRED WIRING. FERRIED TO ATL FOR REPAIRS. 2 L 7 2 4F RT A6WE 1996011900373 19960119 00373 NM 1996 1 19 DLM88960111 1 19960114 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM TAIL COMP LEAKING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 939DL 49812 AFTER TAKEOFF, HAD FAINT BURNING ODOR IN CABIN AND LAV SMOKE DETECTOR WENT OFF. FOUND HYDRAULIC LINE LEAKING AT RT THRU ST REV MODULE. INSTALLED APPROVED FLEX LINE FWD TO MCO. 2 L 7 2 4F RT A6WE 1996011900374 19960119 00374 NM 1996 1 19 DLM88960113 1 19960108 A 3231 RETRACT MECH DOUG MD88 MD88 3023688 NM LT MLG DOOR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 999DN 53371 ON LANDING GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR DOOR OPEN LIGHT. AIRCRAFT RETURN ED ATL. CYCLED GEAR, ALL VISUAL NORMAL AND INDICATIONS NORMAL. BLED HYDRAULIC SYSTEM OF AIR, INSPECTED GEAR DOORS AND AREA, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011900375 19960119 00375 WP 1996 1 19 MWEA96013 1 19960116 A 3222 591009505105 STRUT DOUG DC9 DC914 3022034 WP NLG REQD SERVICE A MWEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 31 400ME 45727 MCI - AFTER TAKEOFF, LOST PRESSURIZATION AND TAKEOFF WARNING CAME ON AND AUTO SPOILER DO NOT USE LIGHT ILLUMINATED. AIR CRAFT RETURNED TO MCI. FOUND NOSE GEAR STRUT DEFLATED KEEPING THE A/C IN GROUND MODE. SERVICED STRUT WITH AIR, FOUND N O LEAKS. 2 L 7 2 4F A6WE 1996011900376 19960119 00376 NE 1996 1 19 SWIA95707 2 19960112 A 7261 O-RING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 196SW 120151 LOSS OF OIL PRESSURE EN ROUTE, SHUTDOWN LEFT ENGINE. REPLACED O-RING ON LEFT AUXILIARY GENERATOR AND REPLACED CLAMP. R AN ENGINE, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996011900377 19960119 00377 SW 1996 1 19 SWIA95708 1 19960113 A 2910 HYD LINE SWRNGN SA227 SA227AC 8780603 SW RIGHT CRACKED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 3117S AC603 TOTAL LOSS OF HYDRAULIC PRESSURE. FOUND RIGHT HYDRAULIC PRESSURE LINE CRACKED. REPLACED LINE AND SERVICED HYDRAULIC SY STEM. RAN ENGINES AND OPS, LEAK CHECK GOOD. 1 L 7 2 4T A8SW 1996011900378 19960119 00378 1996 1 19 SWIA95709 4 19960116 A 3425 AHRS COMPUTER EMB 120 EMB120ER 3260203 SO RIGHT LOOSE A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 189SW 120048 FIRST OFFICER'S COMPUTER FLAG COMES ON AND GOES OFF CONTINIOUSLY WHILE AIRBORNE. REPLACED FIRST OFFICER'S AHC-85 AHRS C OMPUTER RETAINING SCREW/NUT. OPS CHECK OF AHC-85 AHRS COMPUTER CHECKS GOOD. 2 L 7 2 4T RT A31SO 1996011900379 19960119 00379 NM 1996 1 19 VSTA9601011 1 19960110 A 5320 65C3372247 CHORD BOEING 737 737247 138448D NM FS 727 CRACKED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 302VA 20126 CRACKED FAIL-SAFE CHORD FS 727 LEFT HAND SIDE. REPAIRED IAW BOEING SB 737-53-1088. REPLACED REPAIRED CHORD IAW EO 53-1 0-3 R1 11/13/95. COMPLETION TERMINATES INSPECTION PER WORK CARD 5364 FOR SIDE REPLACED. MAINTENANCE PERFORMED BY SOUTH WEST AERO TECH NR S5WR702J. 2 L 7 2 4F A16WE 1996011900518 19960119 00518 NE 1996 1 19 9601035514 2 19960117 A 7530 STATOR VANE ACT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A NWAA E D ENGINE SHUTDOWN RETURN TO BLOCK J X WARNING INDICATION ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 01 514US 23202 716370 DURING TAXI OUT, EICAS MESSAGE ENGINE CONTROLS DISPLAYED. THIRTY SECONDS LATER, NR 1 ENGINE SHUT DOWN. AIRCRAFT RETURNE D TO GATE. GROUND MAINTENANCE REPLACED NR 1 ENGINE STATOR VANE ACTUATOR. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011900519 19960119 00519 NM 1996 1 19 9601046305 1 19960116 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, THE FLOOR EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35R TO 42R WERE FOUND INOPERATIVE. RECONNECTED EME RGENCY LIGHT CONNECTOR PIN. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900520 19960119 00520 NM 1996 1 19 9601056625 1 19960117 A 2150 PACK BOEING 747 747251B 1384892 NM NR 1 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 625US 21707 AFTER TAKEOFF AND SUBSEQUENTLY TURNING OFF PACKS, SMOKE FILLED THE ENTIRE AIRCRAFT. WITH ALL PACKS SHOWING NORMAL OPERA TING TEMPERATURE, THE SMOKE DISSIPATED WITHIN A MINUTE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 177,000 POUND S OF FUEL, AND RETURNED TO LAX. FOUND NR 1 PACK FILTER WITH OIL SMELL. NR 2 AND NR 3 PACKS CHECKED OK. DEFERRED NR 1 PACK PER MEL 21-1A. 2 L 7 4 4F A20WE 1996011900521 19960119 00521 NM 1996 1 19 96FDEA00065 1 19960117 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 319 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDE X SRM 51-40-4. 2 L 7 3 4F A3WE 1996011900522 19960119 00522 NM 1996 1 19 96FDEA00066 1 19960118 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 396 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH ARE A. ORIGINAL METAL THICKNESS IS .040 INCH. REMOVED .009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICA TED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3, FIG 2. APPLIED PROTECTIVE FINISHERS. 2 L 7 3 4F A3WE 1996011900523 19960119 00523 NM 1996 1 19 96FDEA00067 1 19960118 A 5753 TE SKIN BOEING 727 72722 1384002 NM RT TE FORE FLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 RIGHT WING INBD FORE FLAP UPPER SURFACE HAS DISBOND ON T/E AREA MARKED. REPAIRED RT WING INBOARD FORE FLAP IAW SRM 51-4 0-6. 2 L 7 3 4F A3WE 1996011900524 19960119 00524 NM 1996 1 19 96FDEA00068 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 720 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14. GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14 WAS FO UND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND WAS REPAIRED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900525 19960119 00525 NM 1996 1 19 96FDEA00069 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22088 DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO RBL 44 WL 160 IAW FEDEX SRM 51-40- 3. 2 L 7 3 4F RT A3WE 1996011900526 19960119 00526 NM 1996 1 19 96FDEA00070 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 580, LBL 37 - LBL 46, WL 160. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 58 0, LB 37 - LB 46, WL 160 PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900527 19960119 00527 NM 1996 1 19 96FDEA00071 1 19960115 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM FS 545 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FORWARD END OF STRINGER 35L CRACKED FROM RIVET HOLE TO FWD END LENGTH. APPROXIMATELY .1250 INCH FS 545 CONFIRMED BY HFE C. FABRICATED STRINGER 35L PER SAMPLE AND INSTALLED STRINGER PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900528 19960119 00528 NM 1996 1 19 96FDEA00073 1 19960115 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM FS 545 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FOUND STRINGER 34L SEVERED FWD OF PREVIOUS SKIN CRACK STATION FS 545. FABRICATED STRINGER 34L PER SAMPLE AND INSTALLED PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900529 19960119 00529 NE 1996 1 19 96UAL900038 2 19960117 A 7200 50G631 BEARING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 183UA 25379 717694 NR 4 ENGINE FAILURE SHORTLY AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO FIELD. REPLACED ENGINE. ANGLE GEARBOX AB-1 BEA RING FAILURE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996011900530 19960119 00530 NM 1996 1 19 96UAL900039 1 19960117 A 2560 25860304 ASPIRATOR ASSY BFGOODRICH 7A110424 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CREW SLIDE INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 4729U G129 19926 CREW SLIDE FOUND WITH LARGE WAD OF PACKING PAPER BLOCKING ASPIRATOR FLAPPER DOORS. REMOVED ASPIRATOR FROM SLIDE AND REM OVED PAPER WAD. PAPER WAS INSTALLED IN THE ASPIRATOR AFTER MANUFACTURE TO PREVENT DOORS FROM OPENING/CLOSING DURING SHI PPING. PAPER NOT REMOVED DURING ORIGINAL INSTALLATION INTO THE SLIDE ASSEMBLY. 2 L 7 4 4F 4 F A20WE E20EA 1996011900531 19960119 00531 NM 1996 1 19 96UAL900040 1 19960117 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 NR 1 LEFT DOOR OUTER EMERGENCY LIGHT INOP. ACCOMPLISHED LIGHT SYSTEM TEST PER MAINTENANCE MANUAL 33-51-00 AND DETERMINE D LIGHT OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011900532 19960119 00532 SO 1996 1 19 COMA9610025 1 19960115 A 3244 314461 TIRE 314461 EMB 120 EMB120RT SO MLG WHEEL SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 9388 225 120262 MECHANIC REMOVED TIRE FROM A/C DUE TO TIRE FLAT AND MATE TO BLOWN TIRE. DURING INSPECTION FOUND TIRE BEAD SEPARATION WI TH WIRE OFF BEAD EXPOSED. REMOVED WHEEL ASSY FROM SERVICE AND SENT WHEEL AND TIRE TO BFG. 2 L 7 2 4T RT A31SO 1996011900533 19960119 00533 SO 1996 1 19 COMA9610026 1 19960115 A 3246 3006031 WHEEL 314461 EMB 120 EMB120RT SO MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 8701 2406 120262 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE BLOWN AND WHEEL DAMAGE. WHEEL SHOP INSPECTED AND FOUND OUTBOARD HALF A SSY P/N 300-603-1 WAS CRACKED. CRACK IN FLANGE APPROXIMATELY 6 INCHES LONG. WHEEL ASSY HAS BEEN REMOVED FROM SERVICE A ND SENT TO BFG. 2 L 7 2 4T RT A31SO 1996011900534 19960119 00534 SO 1996 1 19 COMA9610027 1 19960116 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 268CA 14448 1285 120262 EMERGENCY ESCAPE PATH LIGHTING FROM ROW 8 THROUGH ROW 10 ARE INOPERATIVE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1996011900535 19960119 00535 EU 1996 1 19 COMA9630016 1 19960116 A 3020 NH2466881 INLET HEAT SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 358CA 6742 1168 340A047 LEFT ENGINE INLET HEAT FAIL LIGHT ILLUMINATED. RED GLOW SEEN IN INTAKE. REPLACED THE LEFT LOWER INLET DUCT. 2 L 7 2 4T RT A52EU 1996011900536 19960119 00536 EU 1996 1 19 COMA9630017 1 19960116 A 2720 CONNECTORS SAAB SF340 SF340A 7850100 EU RUDDER LIMITER DIRTY A COMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 347CA 340A028 RUDDER LIMITER OVERRIDE CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. CLEANED WATER FROM WIRING CONNECTIONS AT RUDDER LIM ITER. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900537 19960119 00537 EA 1996 1 19 COMA9660015 1 19960116 A 7732 6233M30A ACCELEROMETER CNDAIR CL600 CL6002B19 1900309 EA LT ENG DEFECTIVE A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 916CA 6411 7014 LEFT ENGINE N2 VIBRATION CAUTION COMES ON AT 87 PERCENT TO 88 PERCENT N2. REPLACED THE LT ENGINE N2 ACCELEROMETER. 2 L 7 2 4F RT A21EA 1996011900538 19960119 00538 NM 1996 1 19 P5CA9600001 1 19960117 A 3241 421897 CONTROL BOX BOEING 747 747123 1384873 NM ANTI SKID SYST FAILED A P5CA K NONE O OTHER LD LANDING 1 WP 23 859FT 20326 DEPARTING KHV, TOWER ADVISED RUBBER LEFT ON RUNWAY. ON ARRIVAL ANC, DISCOVERED NR 11 TIRE BLOWN, HOLE IN WING-BODY FAIR ING, 18 OF CONDUIT MISSING FROM RT BG STRUT. REPLACED ANTI-SKID BOX DUE TO FAILED BITE CHECK IAW MM 32-42-00, 3 TIRES I AW MM 32-45-01. PERFORMED INTERIM REPAIR ON PANEL IAW MA5350-02:01. 2 L 7 4 4F A20WE 1996011900539 19960119 00539 NM 1996 1 19 UPS205219 1 19960116 A 3260 2314152 SWITCH MECH BOEING 727 727185C 138406N NM RT MLG DOOR MISSING A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 940UP 19826 CREW REPORTED, AFTER TAKEOFF, GEAR IN OFF POSITION, GEAR DOOR LIGHT ILLUMINATED, GEAR CYCLED LIGHT REMAINED ON, CONTACTE D MAINTENANCE. REMAINDER OF FLIGHT FLOWN WITH GEAR HANDLE UP, LIGHT GIBSON WAS OFF. FOUND BUSHING, RT MAIN LANDING DOO R SWITCH MECHANISM MISSING. INSTALLED SAME PER 727-MM 32-62-11. 2 L 7 3 4F A3WE 1996012600051 19960126 00051 WP 1996 1 26 USAA960004 1 19960119 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 101 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 37700 49119 PIT - DURING Q-6 CHECK INSPECTION, FOUND A .25 INCH CRACK COMING FROM RIVET AT STA 101, LEFT AFT OF STRAKE IN SKIN. REM OVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11. (X) 2 L 7 2 4F A6WE 1996012600060 19960126 00060 NM 1996 1 26 USAASB96003 1 19960108 A 2133 10612097 OUTFLOW VALVE BOEING 737 7372B7 1384560 NM CABIN STUCK A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 280AU 22892 CLT - FLT 521 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. STOPPED AT 8,000 FEET ABOVE AGL, THEN RETURNED TO CLT. ON DESCENT AT 2,000 FEET, AIRCRAFT STARTED TO PRESSURIZE. MAINTENANCE REPLACED OUTFLOW VALVE DUE TO STICKING. OPS CHECKE D OK. (X) 2 L 7 2 4F A16WE 1996012600062 19960126 00062 WP 1996 1 26 9601069967 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600063 19960126 00063 WP 1996 1 26 9601079909 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600064 19960126 00064 WP 1996 1 26 9601089608 1 19960118 A 3010 39271011 VALVE DOUG DC9 DC932 3022066 WP RT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 608NW 47233 DURING CLIMB, THE RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTA TION VALVE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600065 19960126 00065 WP 1996 1 26 9601099949 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATI ONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600066 19960126 00066 WP 1996 1 26 9601109604 1 19960117 A 3244 TIRES DOUG DC9 DC932 3022066 WP NR 1/2 MLG DAMAGED A NWAA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 GL 01 604NW 47222 DURING TAKEOFF, THE AIRCRAFT WAS SLOW TO ACCELERATE AND A SLIGHT VIBRATION WAS EXPERIENCED. DURING CLIMB, A RUBBER SMOK E SMELL WAS DETECTED AFTER LANDING GEAR RETRACTION. AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. FOUND NR 2 M AIN LANDING GEAR TIRE FLAT-SPOTTED AND FLAT, NR 1 MAIN LANDING GEAR TIRE FLAT-SPOTTED. REPLACED NR 1, NR 2 MAIN LANDING GEAR TIRES AND ANTI-SKID CONTROL BOX. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600067 19960126 00067 WP 1996 1 26 9601119921 1 19960117 A 3010 39271011 VALVE DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 943N 51182 4761 47647 DURING CLIMB, THE LEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTATION VALV E AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600068 19960126 00068 WP 1996 1 26 9601129906 1 19960116 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP NLG DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 956N 47252 GCM - DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. LUBRICATED NOSE LANDING GEAR, CLEANED CANNON PLUG AND SWITCH ON NOSE LANDING GEAR INDICATION SYSTEM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600069 19960126 00069 NM 1996 1 26 9601132710 1 19960112 A 2910 CIRCUIT BREAKER BOEING 727 727225 1384077 NM B-HYD SYST TRIPPED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 820EA 22557 DURING TAKEOFF ROLL, TAKEOFF ABORTED UNDER 80 KTS DUE LOW 'B' SYSTEM PRESSURE 2,000 PSI. RESET 'B' SYSTEM CIRCUIT BREAK ER AND SYSTEM CHECKED NORMAL. 2 L 7 3 4F A3WE 1996012600070 19960126 00070 WP 1996 1 26 9601141161 1 19960119 A 2820 2720121 CONTROLLER DOUG DC10 DC1040 3023508 WP FUSELAGE FAILED A A NWAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 161US 46770 DURING CRUISE, THE TANK OVER FILLED LIGHT ILLUMINATED AND FUEL WAS STREAMING FROM THE LEFT DUMP NOZZLE. DUMPED 92,500 L BS OF FUEL AND RETURNED TO DTW. REPLACED FUEL CONTROLLER. 2 L 7 3 4F A22WE 1996012600071 19960126 00071 WP 1996 1 26 9601159178 1 19960117 A 3222 5910096 STRUT DOUG DC9 DC914 3022034 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3310L 45705 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. LANDING GEAR RETRACTED NORMALLY. FLIGHT RETURN ED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED AND SERVICED NOSE LANDING GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHE CK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600072 19960126 00072 NM 1996 1 26 96FDEA00074 1 19960119 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE FOREFLAP CHAFING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 RT WING I/B FOREFLAP IS CHAFING APPROX 24 INCHES O/B FROM I/B LEADING EDGE. REPAIRED DAMAGE AREA ON RT WING I/B FOREFL AP APPROX 24 INCHES O/B FROM I/B LEADING EDGE. 2 L 7 3 4F A3WE 1996012600073 19960126 00073 NM 1996 1 26 96FDEA00075 1 19960119 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE LIGHTNING STRIKE A FDEA K NONE C F.O.D. IN INSP/MAINT 1 SO 25 169FE 18866 LIGHTNING STRIKES AT BS 706, 793, 824 AND 888 BETWEEN STR 4 AND 5. REPAIRED LIGHTNING STRIKES AT BS 750, 793, 824 BY IN STALLING NEW FASTENERS. REPAIRED BS 888 BY CUTTING OUT DAMAGED AREA AND FABRICATING REPAIR PARTS. INSTALLED IAW 53-30- 3. 2 L 7 3 4F A3WE 1996012600074 19960126 00074 NM 1996 1 26 96FDEA00076 1 19960119 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER EWO N R 96-2043. 2 L 7 3 4F A3WE 1996012600075 19960126 00075 NM 1996 1 26 96FDEA00077 1 19960119 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DURING UT INSP, CRACK IND FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913. 2 L 7 3 4F A3WE 1996012600076 19960126 00076 NM 1996 1 26 96FDEA00078 1 19960118 A 5330 SKIN BOEING 727 72722 1384002 NM BS 875-878 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW ST R 9R PER FEDEX EA 7-5310-26957. 2 L 7 3 4F A3WE 1996012600077 19960126 00077 NM 1996 1 26 96FDEA00079 1 19960123 A 5330 SKIN BOEING 727 727233 138408A NM BS 1073 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1073 STR 19 TO 20L THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600078 19960126 00078 NM 1996 1 26 96FDEA00080 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 1030-1050 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1030 TO 1050 STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050 STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600079 19960126 00079 NM 1996 1 26 96FDEA00081 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 680 LBL 34 TO 45 WL 160. CUT OUT DAMAGE ON FRAME BS 680 LBL 34 TO 45 WL 160, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600080 19960126 00080 NM 1996 1 26 96FDEA00082 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 700 LBL 34 TO 44 WL 160. REMOVED DAMAGE AND FABRICATED REPAIR PARTS PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600081 19960126 00081 NM 1996 1 26 96FDEA00083 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 500 RBL 34 TO 44 WL 160. CUT OUT DAMAGE REPAIRED FRAME BS 500 RBL 34 TO 44 WL 160 PER FEDEX SRM 51-40 -3. 2 L 7 3 4F RT A3WE 1996012600082 19960126 00082 NM 1996 1 26 96FDEA00084 1 19960123 A 5330 SKIN BOEING 727 727233 138408A NM BS 1050-1056 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FIVE DENTS IN SKIN 1050 TO 1056 STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600083 19960126 00083 NM 1996 1 26 96FDEA00085 1 19960119 A 5320 651758866 BEAM BOEING 727 727233 138408A NM BS 268 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-221-01), ON 25G BEAM AT BS 268 LBL 7 WL 08.1. REMOVED AND REPLACED 25G BEAM PER SRM 53-10-01. 2 L 7 3 4F RT A3WE 1996012600084 19960126 00084 NM 1996 1 26 96FDEA00086 1 19960119 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3. 2 L 7 3 4F RT A3WE 1996012600085 19960126 00085 NM 1996 1 26 96FDEA00087 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENT IN FRAME BS 500 LBL 34 TO 46 WL 160. 2 L 7 3 4F RT A3WE 1996012600086 19960126 00086 NM 1996 1 26 96FDEA00088 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENT IN FRAME BS 500 LBL 34 TO 46 WL 160. CUT OUT DENT, FABRICATED REPAIR DOUBLER, CLEANED, TREATED PART AND FRAME. IN STALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600087 19960126 00087 NM 1996 1 26 96FDEA00089 1 19960119 A 5753 SKIN BOEING 727 727233 138408A NM RT TE FOREFLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 RT WING I/B FOREFLAP I/B END HAS DISBONDED RUBSTRIP UPPER SURFACE. REPAIRED PER SRM 51-40-06. 2 L 7 3 4F RT A3WE 1996012600088 19960126 00088 NM 1996 1 26 96FDEA00090 1 19960119 A 5751 TE WEDGE BOEING 727 727233 138408A NM RT AILERON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 RT WING O/B AILERON T/E WEDGE DELAMINATED AT O/B END. REPAIRED PER SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996012600089 19960126 00089 NM 1996 1 26 96FDEA00093 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 360 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FOUND GOUGE IN FRAME STA 360 WL 156 LBL 40, BETWEEN STR 24 TO 25 LT, E-BAY. REMOVED DAMAGE AND FABRICATED PART. REPAIR ED PER SRM 51-40-3 AND 53-10-2. 2 L 7 3 4F RT A3WE 1996012600090 19960126 00090 NM 1996 1 26 96FDEA00094 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 480-560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT TO RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 496 AND 503 BETWEEN STR 26-27R , MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITHIN LIMITS EXCL UDING 2 AREAS. ONE AT STA 500 RBL 14 AND 1 AT STA 490 RBL 22 PER FEDEX SRM 53-30-1, REPAIRED BOTH AREAS PER FEDEX SRM 5 3-30-3. 2 L 7 3 4F RT A3WE 1996012600091 19960126 00091 NM 1996 1 26 96FDEA00095 1 19960119 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-224-01), ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED SECTION OF TRACK, FABRICATED NEW SECTION AND INSTAL LED PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996012600092 19960126 00092 NM 1996 1 26 96FDEA00096 1 19960113 A 5320 FITTING BOEING 747 747245F 1384897 NM BS 1020 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK ATTACH FITTING AT BS 1020 BETWEEN FLOORBEAMS LBBL 72 TO 92 AND 98.58 FOUND 8 INCH CRACK. 2 L 7 4 4F A20WE 1996012600093 19960126 00093 NM 1996 1 26 96FDEA00097 1 19960113 A 5315 FLOOR BEAM BOEING 747 747245F 1384897 NM BS 1000 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 MAIN DECK LBBL 33 TO 99 FLOOR BEAM AT 1000 FOUND CRACKED AT FLOOR BOARD ATTACHMENT HOLE, NOTE PREVIOUS CORROSION BLEND O UT AREA. REPAIR CARRIED OUT AS PER REF SNRM 1654 FOR DETAILS ERA B53-40-27. 2 L 7 4 4F A20WE 1996012600094 19960126 00094 NM 1996 1 26 96FDEA00098 1 19960113 A 5320 INTERCOSTAL BOEING 747 747245F 1384897 NM BS 1020 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK LATERAL INTERCOSTAL AT BS 1020 BETWEEN FLOORBEAMS LBBL 72.92 AND 98.58, FOUND CRACKED ON UPPER SURFACE. 2 L 7 4 4F A20WE 1996012600095 19960126 00095 NM 1996 1 26 96FDEA00099 1 19960113 A 5320 STIFFENER BOEING 747 747245F 1384897 NM BS 1100 MISSING FASTENER A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK LBBL 57 TO 50 FLOORBEAM VERTICAL STIFFENER AT BS 1100, FOUND 4 EA HI-LOK COLLARS MISSING. 2 L 7 4 4F A20WE 1996012600096 19960126 00096 NM 1996 1 26 96FDEA00100 1 19960113 A 5320 BRACKET BOEING 747 747245F 1384897 NM BS 1200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK RBBL 57 TO 50 FLOORBEAM AT BS 1200, FOUND ANGLE BRACKET TO VERTICAL STIFFENER CRACKED. 2 L 7 4 4F A20WE 1996012600097 19960126 00097 NM 1996 1 26 96FDEA00101 1 19960119 A 5754 65162268A K-FLAP BOEING 727 727227 1384078 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 NR 5 K-FLAP O/B LUB O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVE D AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECK IAW FEDEX MM 27-81-1. 2 L 7 3 4F A3WE 1996012600098 19960126 00098 NM 1996 1 26 96UAL900041 1 19960118 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 EMERGENCY ESCAPE LIGHTING INOP AT OVERWING EXIT ROW 17 ABC. RELAMPED DEFECTIVE EMERGENCY ESCAPE LIGHT AT OVERWING EXIT ROW 17 ABC AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600099 19960126 00099 NM 1996 1 26 96UAL900043 1 19960118 A 3350 LEADER LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAV ATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600100 19960126 00100 WP 1996 1 26 96UAL900044 1 19960118 A 2820 ARLO627511 TEE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUEL MANIFOLD RUPTURED A A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 1834U 47966 UNWANTED FUEL TRANSFER INTO NR 2 MAIN TANK WITH FILL VALVE SWITCH IN CLOSED POSITION AND NR 2 MAIN FILL VALVE LIGHT INDI CATING FILL VALVE IS IN CLOSED POSITTION. A WELD FAILED ALLOWING A PRESSURE RELIEF VALVE TO COME OFF THE FUEL MANIFOLD. REPLACED RUPTURED FUEL PUMP TEE ASSEMBLY. 2 L 7 3 4F 4 F A22WE E23EA 1996012600101 19960126 00101 NM 1996 1 26 96UAL900045 1 19960118 A 3350 LEADER LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT LAV FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAV ATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600102 19960126 00102 NM 1996 1 26 96UAL900046 1 19960119 A 4900 APU BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU COMPT SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7289U 21567 CREW REPORTED SMOKE AND FIRE COMING FROM APU ON ARRIVAL. RESET CB AND APU STARTED, NO SMOKE. COULD NOT DUPLICATE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600103 19960126 00103 NM 1996 1 26 96UAL900047 1 19960119 A 2820 69186122 VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK BROKEN A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7286U 21564 WHILE OPERATING ALL OUT OF NR 2 FUEL TANK, THE NR 3 TANK DECREASED SLOWLY IN QUANTITY WITH ONLY THE AFT PUMP OPERATING. LEAKED 1,200 LBS OVER 1 HOUR 15 MINUTES. TURNING OFF BOTH BOOST PUMPS QUANTITY DECREASE STOPPED. FOUND BROKEN VENT TU BE AND REPLACED TUBE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600104 19960126 00104 WP 1996 1 26 96UAL900048 1 19960119 A 2760 APH7201 SPRING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SPEEDBRAKE DRUM FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 1837U 47969 SPOILERS FAILED TO RETRACT AFTER LANDING. HELICAL RETURN SPRING ON SPEEDBRAKE DRUM FOUND BROKEN. REPLACED SPRING. 2 L 7 3 4F 4 F A22WE E23EA 1996012600105 19960126 00105 1996 1 26 96UAL900049 4 19960119 A 2565 SEAM PICO D29835193 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2L SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7441U 16970877 21895 NR 2L EVACUATION SLIDE REMOVED FOR EXPIRATION OF TIME. SHOP FOUND MINOR SEAM LEAK ON THE TUBE DIRECTLY UNDER THE GIRT. REPAIRED SEAM LEAK, NON-STRUCTUAL. 2 L 7 3 4F 4 F A3WE E2EA 1996012600106 19960126 00106 NM 1996 1 26 96UAL900050 1 19960119 A 3350 CONNECTOR BOEING 737 737522 138449F NM CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 904UA 25004 EMERGENCY FLOOR MOUNTED ESCAPE LIGHTING INOP ROWS 15 TO 20. RECONNECTED FLOOR MOUNTED EMERGENCY ESCAPE LIGHTING AT ROWS 15 THROUGH 20 TO POWER SOURCE AND OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1996012600107 19960126 00107 WP 1996 1 26 MWEA96014 1 19960116 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, FWD GALLEY DOOR EVACUATION SLIDE COVER CAME OFF. RESECURED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1996012600108 19960126 00108 WP 1996 1 26 MWEA96015 1 19960118 A 7711 EPR SENSE LINE DOUG DC9 DC914 3022034 WP RIGHT ICED UP A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 600ME 45725 PILOT REPORTS LESS THAN MAX POWER INDICATION, RT ENG WENT TO 1.7 EPR WHILE LT ENGINE JUMPED TO 2.0 EPR AFTER A LAG IN SP OOL UP ON TAKEOFF. THE TAKEOFF WAS ABORTED. INSPECTED ALL EPR SENSE LINES, NO DISCREPANCIES NOTED. RAN BOTH ENGINES T O TAKEOFF POWER. FOUND BOTH INDICATIONS NORMAL WITH ANTI-ICE ON AND OFF. SUSPECT TEMPORARY ICING IN PT2 LINE. RETURNE D A/C TO SERVICE AND NO FURTHER PROBLEMS ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F A6WE 1996012600109 19960126 00109 WP 1996 1 26 MWEA96016 1 19960118 A 4900 GRCP8598D APU DOUG DC9 DC932 3022066 WP AFT ACCESSORY INJESTED SPRAY A MWEA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 204ME 47680 MKE - CREW REPORTS, AFTER LANDING THE LT LAV SMOKE DETECTOR SOUNDED. FLIGHT ATTENDANTS REPORT SMELLING FUEL FUMES AND T HE CABIN SLIGHTLY CLOUDED. RAN BOTH PACKS ON GROUND AND COULD NOT DUPLICATE SMOKE OR FUMES IN CABIN. SMOKE DETECTOR O PS CHECK GOOD. SUBMITTER SUSPECTS SPRAY FROM TAXI INJESTED IN APU. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996012600110 19960126 00110 NM 1996 1 26 P5CA9600002 1 19960118 A 5320 ANGLE BOEING 747 747124 1384874 NM BS 840 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND BROKEN ANGLE AT CONNECTING POINT TO CEILING SUPPORT CHANNEL BS 840 NEAR LBL 33. FABRICATED NEW ANGLE IAW SRM 53-1 0-21 AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600111 19960126 00111 NM 1996 1 26 P5CA9600003 1 19960118 A 5320 DOOR SILL BOEING 747 747124 1384874 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN MAIN DECK SIDE CARGO DOOR SILL AT LOWER AFT END. REPAIRED CRACK IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996012600112 19960126 00112 NM 1996 1 26 P5CA9600004 1 19960118 A 5754 LE FLAP BOEING 747 747124 1384874 NM LT WING BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEADING EDGE FLAP NR 10 OUTBOARD CORNER FOLDED AND BENT. REPAIRED IAW SRM 57-50-03 AND INSTALLED PER SRM 51-30-02 . 2 L 7 4 4F A20WE 1996012600113 19960126 00113 NM 1996 1 26 P5CA9600005 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1336/1364 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING FRONT SPAR BETWEEN STA WS 1336 AND 1364. CORROSION REM OVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600114 19960126 00114 NM 1996 1 26 P5CA9600006 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1392 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING CENTER SPAR AROUND WS 1392. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600115 19960126 00115 NM 1996 1 26 P5CA9600007 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1308/1336 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 1308 AND 1336. REMOVED CORROSION IAW S RM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600116 19960126 00116 NM 1996 1 26 P5CA9600008 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 862-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 862 AND 1000. REMOVED CORROSION IAW SR M 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600117 19960126 00117 NM 1996 1 26 P5CA9600009 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 469.82 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR AT WS 469.82. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600118 19960126 00118 NM 1996 1 26 P5CA9600010 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 586.62 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE AROUND WING CENTER SPAR AT WS 586.62. REMOVED CORROSION IAW SRM 5 1-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600119 19960126 00119 NM 1996 1 26 P5CA9600011 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 323.82 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE BETWEEN STR 26 AND WING CENTER SPAR NEAR WING ROOT, WS 323.82. RE MOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600120 19960126 00120 NM 1996 1 26 P5CA9600012 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1516-1548 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE NEAR FUEL TANK ACCESS BETWEEN WS 1548.20 AND 1516.60. REMOVED COR ROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600121 19960126 00121 NM 1996 1 26 P5CA9600013 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 917-1140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT LOWER WING SURFACE AT FUEL TANK ACCESS BETWEEN WS 917 AND 1140. REMOVED CORROSION IAW SRM 51-10-01, TREATED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600122 19960126 00122 NM 1996 1 26 P5CA9600014 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 642-669.5 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 642 AND 669.50. REMOVED CORROSI ON IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600123 19960126 00123 NM 1996 1 26 P5CA9600015 1 19960118 A 5330 SKIN BOEING 747 747124 1384874 NM FS 1840-1880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT LOWER FUSELAGE BETWEEN BS 1840 AND 1880, STR 49. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600124 19960126 00124 NM 1996 1 26 P5CA9600016 1 19960118 A 5330 PANEL BOEING 747 747124 1384874 NM BS 1780 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND BENT AND LOOSE RIVETS ON AFT CARGO DOOR SWITCH ACCESS PANEL, BS 1780 STR 35 TO 36. FABRICATED AND INSTALLED NEW P ANELS AND FASTENERS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600125 19960126 00125 NM 1996 1 26 P5CA9600017 1 19960118 A 5230 HINGE BOEING 747 747124 1384874 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON FWD DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 560 TO 660. REMOVED CORROSION IAW SRM 51-10 -01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600126 19960126 00126 NM 1996 1 26 P5CA9600018 1 19960118 A 5230 HINGE BOEING 747 747124 1384874 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON AFT CARGO DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 1820 TO 1960. REMOVED CORROSION IAW S RM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600127 19960126 00127 NM 1996 1 26 P5CA9600019 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 917-1364 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE AROUND WING FUEL TANK ACCESS BETWEEN WS 917 AND 1364. REMOVED COR ROSION IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600128 19960126 00128 WP 1996 1 26 RRXA9600002 1 19960118 A 3260 RETRACT MECH DOUG DC8 DC863 302198A WP NLG DOORS MALFUNCTIONED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 964R 46000 KDEN-KADY - FLT 109 - AFTER TAKEOFF, ON GEAR RETRACTION EXCESSIVE VIBRATION WAS FELT FROM NOSE AREA AND LOUD SOUND HEARD . AIRCRAFT RETURNED TO KDEN. MAINTENANCE FOUND THE NOSE GEAR DOORS DOWN. MAINTENANCE SECURED NOSE GEAR DOORS AND NO D EFECTS NOTED. 2 L 7 4 4F 4A25 1996012600129 19960126 00129 NE 1996 1 26 UPS505225 2 19960118 A 7200 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE RIGHT FLAME-OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT AP APPROACH 1 SO 01 434UP 25465 CREW REPORTED, RT ENGINE FLAMED-OUT ON APPROACH. REMOVED AND REPLACED RT ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600130 19960126 00130 NM 1996 1 26 96ZZZX302 1 19960102 A 3610 10610652 DUCT SEAL BOEING 727 727231 1384079 NM NR 3 STRUT FAILED A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 54354 21986 MCI - FLT 469 - DURING CRUISE, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 STRUT DUCT SEAL, MFG PN 10-61065-2. OPERATIONAL CHECK NORMAL. CHECK C-1 - 4-28-95 - MCI. 2 L 7 3 4F A3WE 1996012600133 19960126 00133 WP 1996 1 26 96ZZZX305 1 19960104 A 3350 58222 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 05 935L 47603 STL - FLT 141 - DURING LANDING AND TAXI, THE EGRESS LIGHTS FLICKERED ON AND OFF. FOUND BATTERY PACK, MFG PN 5822-2, WEA K. REPLACED BATTERY PACK AND EGRESS LIGHT, OPERATION CHECKED NORMAL. CHECK C - 8-27-95 - STL. 2 L 7 2 4F A6WE 1996012600134 19960126 00134 WP 1996 1 26 96ZZZX306 1 19960104 A 2170 17946081 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 955U 49427 STL - FLT 99 - DURING APPROACH, SMOKE EMITTED INTO AFT CABIN AND COCKPIT. FOUND LEFT AND RIGHT COALESCER ELEMENTS, MFG PN 179460-8-1, CONTAMINATED. REPLACED LEFT AND RIGHT COALESCER ELEMENTS AND AIR CONDITIONING SYSTEM OPERATION CHECKED N ORMAL. CHECK C-2D - 10-17-95 - MCI. 2 L 7 2 4F A6WE 1996012600135 19960126 00135 WP 1996 1 26 96ZZZX307 1 19960108 A 3610 DUCT DOUG DC9 DC931 3022065 WP NR 1 ENGINE CRACKED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 988Z 47134 STL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED. REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND. OP-15 - 8-21-95 - STL. 2 L 7 2 4F A6WE 1996012600136 19960126 00136 WP 1996 1 26 96ZZZX308 1 19960107 A 2160 BAC18R2A CIRCUIT BREAKER DOUG DC9 DC931 3022065 WP TEMP CONTROL MALFUNCTIONED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 992Z 47095 STL - FLT 298 - DURING CRUISE, HAD AN ELECTRICAL FLASH AND ODOR EMITTED FROM CIRCUIT BREAKER PANEL. FOUND CIRCUIT BREAK ER FOR FLIGHT DECK TEMPERATURE CONTROL WITH INTERNAL MALFUNCTION. REPLACED TEMPERATURE CONTROL CIRCUIT BREAKER, MFG PN BAC18R2A. FLIGHT DECK TEMPERATURE CONTROL CHECKED NORMAL. CHECK C - 6-19-95 - STL. 2 L 7 2 4F A6WE 1996012600137 19960126 00137 WP 1996 1 26 96ZZZX309 1 19960107 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP RT MLG DOOR SW LOOSE A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 993Z 47082 STL - FLT 394 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR OPEN LIGHT REMAINED ON. VISUAL CHECK SHOWED LANDING GEAR DOORS TO BE CLOSED. FOUND PIN PUSHED BACK IN RIGHT GEAR DOOR SWITCH CONNECTOR. SECURED PIN IN RIGH T GEAR DOOR SWITCH CONNECTOR. LANDING GEAR DOOR OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 8-11-95 - STL. 2 L 7 2 4F A6WE 1996012600138 19960126 00138 WP 1996 1 26 96ZZZX310 1 19960107 A 3231 LATCH DOUG DC9 DC931 3022065 WP LT MLG DOOR NOT LATCHED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 993Z 47082 STL - FLT 541 - AFTER TAKEOFF, LANDING GEAR RETRACTION LEFT MLG UNSAFE LIGHT REMAINED ON. CYCLED LANDING GEAR AND LANDI NG GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. FOUND LEFT MLG DOOR LATCH HOOK NOT LATCHING INTO POSITION. RIGGED DOOR L ATCH ROLLER ASSY. LANDING GEAR AND DOOR OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 8-11-95 - STL. 2 L 7 2 4F A6WE 1996012600139 19960126 00139 EU 1996 1 26 96ZZZX311 1 19960110 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 9 414 DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR SIMA960103. 2 H 7 2 4T RT A53EU 1996012600147 19960126 00147 WP 1996 1 26 96ZZZX319 1 19960104 A 3150 SWITCH DOUG DC9 DC932 3022066 WP TAKEOFF WARNING DIRTY A VJ6A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 11 904VJ 47377 PHL/PHL - FLT 545, CREW ADVANCED THROTTLES ON TAKEOFF AND GOT A TAKEOFF WARNING HORN AT APPROXIMATELY 15 KNOTS. CYCLED FLAPS AFTER CLEANING THE TAKEOFF WARNING SWITCH. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996012600152 19960126 00152 NM 1996 1 26 BJNA96101 1 19960111 A 3350 SPLICE BOEING 737 737214 138446R NM CABIN FAILED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 OVERWING SEAT EMERGENCY LIGHT LEFT, INOPERATIVE. REPAIRED SPLICE AND OPS CHECK OK IAW 20-30-12 AND 30-51-0. (X) 2 L 7 2 4F A16WE 1996012600154 19960126 00154 WP 1996 1 26 HAL9601 1 19960102 A 3610 39271012 AUGMENTATION VLV DOUG DC9 DC951 3022051 WP LEFT LEAKING A HALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 13 669HA 10119 P2011 47654 INFORMATION FROM LOG PAGE 126945, 126946. HNL - FLT 534 - AFTER TAKEOFF, TAIL COMP. TEMP HI-LIGHT ON. PERFORMED ABNORM AL CHECK, LIGHT WENT OFF, RETURNED TO HNL. RAN ENGINES AT TAKEOFF POWER, FOUND LEFT AUGMENTATION VALVE LEAKING. NO LEA KS NOTED AT RIGHT AUGMENTATION VALVE. REPLACED LEFT AUGMENTATION VALVE AND CLAMPS. GROUND RUN AT TAKEOFF AND CLIMB POW ER SETTINGS. NO ABNORMAL WARNING LIGHTS ILLUMINATED. NO LEAKS FOUND. OK FOR SERVICE. OPERATIONS CHECK OK. (X) 2 L 7 2 4F A6WE 1996012600163 19960126 00163 WP 1996 1 26 ORJA96001 1 19960101 A 3246 26088911 WHEEL DOUG DC9 DC982 3022082 WP NR 3 MLG BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 5202 49424 REMOVED NR 3 MAIN WHEEL ASSY DUE TO BROKEN TIE BOLT. REPLACED IAW MM 32. (X) 2 L 7 2 4F A6WE 1996012600165 19960126 00165 EU 1996 1 26 SIMA960082 1 19960108 A 3246 5009237 INNER WHEEL HUB 5010488 SAAB SF340 340B 7860101 EU NR 2 WHEEL CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 594MA 175 MAY931232 340B212 LAW - LAW SHOP - MAIN WHEEL ASSY, PN N5010488, SN MAY 93-1232, WAS REMOVED FROM AIRCRAFT FOR TIRE REPLACEMENT. DURING S HOP INSPECTION, 2 CRACKS (APPROX .50 INCH) WERE FOUND RUNNING ACROSS THE TIRE BEAD FLANGE AREA OF INNER HUB ASSY. PN 50 09237, SN AUG89-0900, INNER WHEEL HUB ASSY WAS REMOVED FROM SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600166 19960126 00166 EU 1996 1 26 SIMA960101 1 19960109 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU NR 2 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 112AE 340A112 DFW - FLT 3511 - AFTER TAKEOFF, NR 2 ENGINE GIVES FALSE WARNINGS ON BOTH HANDLE AND CAPTAIN'S WARNING PANEL. AIRCRAFT T URNED BACK. MAINTENANCE INSPECTED AND REPLACED ENGINE FIRE LOOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600167 19960126 00167 EU 1996 1 26 SIMA960102 1 19960109 A 2612 89905202 FIRE CNTRL UNIT SAAB SF340 SF340A 7850100 EU NR 2 ENGINE MALFUNCTIONED A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 112AE 0300 340A112 DFW - FLT 3633 - AFTER TAKEOFF, NR 2 ENGINE WARNING ACTIVATED. CREW RESPONDED BY PULLING THE T-HANDLE AND BLOWING A FIR E BOTTLE, THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE FIRE LIGHT HAD EXTINGUISHED AND NO EMERGE NCY EVACUATION WAS PERFORMED. MAINTENANCE INITIAL INSPECTION SHOWED NO SIGN OF FIRE. REPLACED FIRE BOTTLE AND SQUIBB A ND FIRE CONTROL UNIT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600168 19960126 00168 EU 1996 1 26 SIMA960103 1 19960110 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 0853 414 DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR 96ZZZX311. (X) 2 H 7 2 4T RT A53EU 1996012600169 19960126 00169 EU 1996 1 26 SIMA960111 1 19960111 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 270AT 811 270 OKC - EMERGENCY FLOOR PATH LIGHTING PORTIONS REMAIN ILUMINATED WHEN SYSTEM IS DISARMED. REPLACED EMERGENCY BATTERY PACK 73WL IAW MM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996012600170 19960126 00170 NM 1996 1 26 TWRA9601 1 19960104 A 4930 MA11A1173 FUEL VALVE ACT BOEING 747 747212B 1384886 NM APU INOPERATIVE A TWRA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 616FF 21939 DURING FLIGHT, FUEL VALVE LIGHT ILLUMINATED FOR APU. FLIGHT ATTENDANT AT L5 DOOR NOTICED A FUEL SMELL. UPON LANDING, T HE FUEL VALVE WAS LOCKED OUT. THE ITEM WAS DEFERRED PER DDPG. RETURN FLIGHT TO MIAMI, NO FUEL SMELL WAS NOTICED. ON A RRIVAL AT JFK, INSPECTION CHECKED APU FUEL SHROUD FOR LEAKS, NONE FOUND. MAINTENANCE REPLACED FUEL VALVE ACTUATOR. OPS CHECK AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 4 4F A20WE 1996012600171 19960126 00171 NM 1996 1 26 W8PA960001 1 19960109 A 2740 AR7077M1 TRIM MOTOR BOEING 737 7373L9 1384470 NM EMPENNAGE DEFECTIVE A W8PA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 NM 03 960WP 23331 CREW REPORTED ON APPROACH IN PATTERN AT 400 FEET, HORIZONTAL STABILIZER TRIM CONTINUED TO RUN IN NOSE DOWN POSITION, HAD TO DISCONNECT. MAINTENANCE REPLACED STABILIZER TRIM MOTOR PER MM 27-41-51. OPS CHECKED SYSTEM OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1996012600172 19960126 00172 NM 1996 1 26 W8PA960002 1 19960116 A 2797 WIRE BOEING 737 7373B7 1384580 NM E 3-2 RACK FAILED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 509AU 23384 FOUND CHAFED WIRE, W084-508-24 WHICH HAD ARCED ON 3-2 SHELF RACK. WIRE IS 2B VAC TO AUTOSTAT COMPUTER. REPAIRED WIRE W O84-508-24 AND ADDED ANTI-CHAFE MATERIAL TO WIRE BUNDLE AND EDGE OF E 3-2 RACK. (X) 2 L 7 2 4F RT A16WE 1996012600173 19960126 00173 WP 1996 1 26 9601169759 1 19960116 A 3350 21 BATTERYQXEA96000 DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600174 19960126 00174 WP 1996 1 26 9601179868 1 19960115 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 11 AND 15 INOPERATIVE. REPLACED BATTER IES AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600175 19960126 00175 WP 1996 1 26 9601189868 1 19960117 A 3350 SOCKET DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION FOR FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACE D LIGHT SOCKET AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600176 19960126 00176 WP 1996 1 26 9601199151 1 19960116 A 3350 60030451 BATTERY PACK DOUG DC9 DC914 3022034 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8909E 45770 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ABOVE TAILCONE SLIDE INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600177 19960126 00177 NM 1996 1 26 9601202710 1 19960117 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 820EA 22557 DURING PREFLIGHT, FOUND RED EXIT CUE LIGHT INOPERATIVE AT ROW 17. REPLACED LIGHT MODULE 17D AND CHECKED OK. 2 L 7 3 4F A3WE 1996012600178 19960126 00178 WP 1996 1 26 9601219139 1 19960116 A 3350 113317 BATTERY PACK DOUG DC9 DC914 3022034 WP PAX DOOR SLIDE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 38440 3275 47049 DURING PERIODIC CHECK, EMERGENCY BATTERY PACK FOR MAIN CABIN DOOR EVACUATION SLIDE FAILED TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996012600179 19960126 00179 WP 1996 1 26 9601229753 1 19960117 A 3260 DOOR SWITCHES DOUG DC9 DC941 302207N WP MAIN GEAR DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 753NW 47117 MEM-PHL - DURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED MAIN LANDING GEAR DOOR SWITCHES. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600180 19960126 00180 WP 1996 1 26 9601239967 1 19960120 A 7711 EPR INDICATION DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 9331 47263 657496 AS TAKEOFF POWER WAS APPLIED, THE NR 1 ENGINE EPR INDICATION STARTED DECREASING. THE TAKEOFF WAS ABORTED AND THE AIRCRA FT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND WARMED THE FUEL CONTROL UNIT WITH AN EXTERNAL HEAT SOURCE . NO DISCREPANCIES WERE NOTED AND AIRCRAFT CONTINUED IN SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996012600181 19960126 00181 WP 1996 1 26 96FDEA00103 1 19960120 A 5512 SKIN DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 TWO CRACKS FOUND AT L/E OF LT STABILIZER UPPER SKIN PANEL, AT CLOSING RIB AREA STA XE = 28.426, XFS = 86.616. CRACKS AR E APPROX .25 INCH AND 2.0 INCH IN LENGTH. REPAIRED AS PER EO 8-5510-7-3312 PART 4 AND SRM 55-20-00. 2 L 7 3 4F A22WE 1996012600182 19960126 00182 WP 1996 1 26 96FDEA00104 1 19960118 A 5720 APB70801 ANGLE DOUG DC10 DC1010 3022110 WP WING CENTER SECT CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 L/LT WW FWD BULKHEAD TOP OF WING CENTER BOX SECTION, REMOVABLE PANEL HAS HEAVY CORROSION, APPROX 10 INCHES O/B OF VERTIC AL KEEL BEAM WEB. REMOVED CORRODED ANGLE, CLEANED, TREATED AND PRIMED UPPER WING SURFACE THAT MATES WITH ANGLES REF 51- 00 VOL 11 SRM, OK TO INSTALL ANGLE. INSTALLATION COMPLETED AS PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996012600183 19960126 00183 WP 1996 1 26 96FDEA00105 1 19960120 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CRACK IN HORIZONTAL STABILIZER OUTER RT SECTION, UPPER AFT SPAR CAP AFT BARREL NUT HOLE ADJACENT TO OPERATING BULKHEAD. CRACK MEASURES .3125 INCH INTO HOLE AND THEN PROGRESSES FWD .3750 INCH LONG. CRACK WAS REWORKED PER AN ELLIPTICAL SHAP E AND CALCULATED, AREA EQUALS .387 SQ PER S/B A55118 A MAXIMUM OF .92 IS ALLOWED. 2 L 7 3 4F A22WE 1996012600184 19960126 00184 NM 1996 1 26 96FDEA00106 1 19960108 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 AFT CX COMP STR 29L IS CORRODED ON O/B SIDE AT BELLFRAME STA 950E, AFT SIDE OF BELLFRAME. BEYOND LIMITS PER SRM 53-10-1 , REPAIRED PER FEDEX EA 7-5310-26899. 2 L 7 3 4F A3WE 1996012600185 19960126 00185 NM 1996 1 26 96FDEA00107 1 19960117 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE STR 3L STA 440 CRACKED. INSTALLED REPAIR ON STR 3L STA 440 PER MM 53-10-3 PG 5 WITH FAB PARTS ON SHOP ORDER FE7X, FM7K, FM69. 2 L 7 3 4F A3WE 1996012600186 19960126 00186 NM 1996 1 26 96FDEA00108 1 19960116 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 FWD CARGO FUSELAGE SKIN CORRODED BETWEEN STR 28 LT AND RT STA 720C PLUS 5. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996012600187 19960126 00187 NM 1996 1 26 96FDEA00109 1 19960122 A 5347 BAC1510190 SEAT TRACK BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUTHOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05. 2 L 7 3 4F A3WE 1996012600188 19960126 00188 WP 1996 1 26 ABXA9600036 1 19960119 A 3260 MS25231313 BULB DOUG DC8 DC863 302198A WP GEAR INDICATOR FAILED A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 820AX 46155 DURING LANDING GEAR EXTENSION, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. ABNORMAL LANDING GEAR PROCEDURES WERE C OMPLETED. REPLACED LIGHT BULBS FOR THE LEFT MAIN LANDING GEAR INDICATOR AND THE BULBS ILLUMINATED DURING NEXT LANDING G EAR EXTENSION. 2 L 7 4 4F 4A25 1996012600189 19960126 00189 SO 1996 1 26 COMA9610028 1 19960115 A 2750 3471001001 ANNUNICATOR PNL EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 01 162CA 7659 2083 120150 DURING TAKEOFF, RECEIVED FLAP CONTROL FAULT WARNING. REPLACED THE FLAP ANNUNCIATOR PANEL. 2 L 7 2 4T RT A31SO 1996012600190 19960126 00190 SO 1996 1 26 COMA9610029 1 19960116 A 3230 20885 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 259CA 10790 768 120252 LT MAIN LANDING GEAR A-SYSTEM INTRANSIT INDICATOR REMAINED ON WHEN GEAR SELECTED DOWN. CYCLED GEAR WITH SAME RESULTS. R EPLACED THE LT MLG UPLOCK ACTUATOR. 2 L 7 2 4T RT A31SO 1996012600191 19960126 00191 SO 1996 1 26 COMA9610030 1 19960114 A 6120 8210181 PUMP EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 256CA 4639 1673 120245 LEFT ENGINE PROPELLER WILL NOT UNFEATHER. REPLACED THE PROPELLER OVERSPEED GOVERNOR OIL PUMP. 2 L 7 2 4T RT A31SO 1996012600192 19960126 00192 SO 1996 1 26 COMA9610031 1 19960118 A 5230 12023348005 DOOR SEAL EMB 120 EMB120RT SO CARGO COMPT LOOSE A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 244CA 120217 CABIN PRESSURIZATION FAILED DURING FLIGHT. REPLACED CARGO DOOR SEAL WHICH HAD COME LOOSE. 2 L 7 2 4T RT A31SO 1996012600193 19960126 00193 SO 1996 1 26 COMA9610032 1 19960118 A 2730 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEVATOR DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 TRIM AURAL WARNING SOUNDS WHEN POWER LEVERS ADVANCED. REPLACED THE ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1996012600194 19960126 00194 EU 1996 1 26 COMA9630018 1 19960117 A 2613 004WS00 WEU SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 358CA 12117 223 340A047 DURING TAKEOFF, LEFT ENGINE TAIL PIPE HOT WARNING CAME ON. REPLACED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996012600195 19960126 00195 EA 1996 1 26 COMA9660016 1 19960117 A 3230 16600101 UPLOCK ASSY CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 948CA 853 7079 DURING APPROACH, WHEN LANDING GEAR SELECTED DOWN, THE NLG INDICATED UNSAFE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE NLG UPLOCK ASSY FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996012600196 19960126 00196 WP 1996 1 26 DHL96801007 1 19960118 A 2710 H654 PRESS SWITCH DOUG DC8 DC873 302199C WP AILERON PCU INTERMITTENT A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 AILERON MANUAL CONTROL LIGHT ILLUMINATED AFTER TAKEOFF. ABNORMAL PROCEDURES FOLLOWED. REPLACED AILERON PCU PRESSURE SW ITCH PER M/M 27-10 AND OPS CHECK OK. 2 L 7 4 4F RT 4A25 1996012600197 19960126 00197 WP 1996 1 26 MWEA96017 1 19960119 A 2560 3952273501 GIRT BAR LATCH DOUG DC9 DC915 3022036 WP PAX DOOR LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 CREW REPORTS, AMIN ENTRANCE DOOR GIRT BAR LATCH VERY DIFFICULT TO OPERATE. CLEANED, LUBED LATCHES AND RESHIMMED FOR MOR E CARPET CLEARANCE. 2 L 7 2 4F A6WE 1996012600198 19960126 00198 WP 1996 1 26 MWEA96018 1 19960119 A 2530 50226 OVEN DOUG DC9 DC932 3022066 WP FWD GALLEY MALFUNCTIONED A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, CIRCUIT BREAKER FOR LEFT OVEN POPPED. RESET CB, POPPED AGAIN. F/A REPORTS, SMELLING ELECTRICAL SMOKE. R EPLACED OVEN AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996012600199 19960126 00199 NM 1996 1 26 P5CA9600020 1 19960117 A 2730 CONTROL RODS BOEING 747 747122 1384872 NM ELEVATOR DISCONNECT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DURING GROUND CHECK, FOUND BOTH OUTBOARD ELEVATOR RODS DISCONNECTED. RECONNECTED AND PERFORMED OPERATIONAL CHECK IAW MM 27-31-02. INVESTIGATING TO DETERMINE WHY DISCONNECTED. 2 L 7 4 4F A20WE 1996012600200 19960126 00200 NM 1996 1 26 P5CA9600021 1 19960120 A 3610 69B401186 DUCT BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 854FT 19754 AFTER ENGINE START, WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO BLOCKS. FOUND LEADING EDGE PNEUMA TIC DUCT INBOARD OF NR 2 ENGINE CRACKED. REPLACED DUCT ASSEMBLY, INSPECTED AND LEAK CHECKED IAW MM 36-10-00. 2 L 7 4 4F A20WE 1996012600201 19960126 00201 NE 1996 1 26 P5CA9600022 2 19960120 A 7321 FUEL CONTROL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A P5CA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 WP 23 852FT 19757 662276 NR 4 ENGINE FLAME-OUT AT 29,000 FT, ATTEMPTED ENGINE RESTART, UNSUCCESSFUL. FLIGHT RETURNED TO MIAMI. REPLACED FCU, FU EL PUMP, TT2 SENSOR IAW MM 73-11 01 AND 73-21 01. LEAK CHECK AND RUNUP OK. 2 L 7 4 4F 4 F A20WE E20EA 1996012600202 19960126 00202 NE 1996 1 26 SWAA960030 2 19960113 A 7200 ENGINE BOEING 737 7373G7 1384595 NM GE CFM56 CFM563B1 13802 NE NR 2 FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 671SW 23785 721339 AT 37,000, EXPERIENCED NUMBER 2 ENGINE OIL PRESSURE DROP, THEN ENGINE STOPPAGE. CREW PERFORMED ENGINE SHUTDOWN CHECKLI ST. AIRCRAFT DIVERTED TO TUS AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996012600203 19960126 00203 NM 1996 1 26 SWAA960031 1 19960114 A 3241 39353 ANTI-SKID VALVE BOEING 737 7372H4 138448C NM RT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 81SW 22730 AFTER GEAR RETRACTION, UPON GEAR HANDLE BEING POSITIONED TO OFF, INBOARD GEAR ANTI-SKID LIGHT ILLUMINATED. LIGHT EXTING UISHES WITH HANDLE IN UP OR DOWN POSITIONS. AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING. AT HOU, REPLACED RT INBOARD ANTI-SKID VALVE PER BOEING M/M. 2 L 7 2 4F A16WE 1996012600204 19960126 00204 NM 1996 1 26 SWAA960032 1 19960117 A 5312 BRACKET BOEING 737 7372T4 1384492 NM BS 351.2 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD AT BS 351.2 ATTACH BRACKET CRACKED ON LEFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600205 19960126 00205 NM 1996 1 26 SWAA960033 1 19960117 A 5320 SPLICE BOEING 737 7372T4 1384492 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND STRINGER SPLICE AT S27L CORRODED AT BS 947.5 AND 967. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600206 19960126 00206 NM 1996 1 26 SWAA960034 1 19960117 A 5320 WEB BOEING 737 7372T4 1384492 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND WEB FWD FLANGE TO FRAME CRACKED AT S7L AT BS 294. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600207 19960126 00207 NM 1996 1 26 UPS405244 1 19960119 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 MAINTENANCE REPORTED, CABIN DOOR EMERGENCY LIGHT INOP. CLEANED CONTACTS, OPS CHECK OK. 2 L 7 4 4F A20WE 1996012600277 19960126 00277 NE 1996 1 26 96ZZZX324 2 19960105 A 7200 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RIGHT MALFUNCTIONED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 01 432AW 7374 286 PCE123226 AIRCRAFT DEPARTED GJT. WHEN THE ENGINE BLEEDS WERE SELECTED ON, THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE AI RCRAFT RETURNED TO GJT. AFTER TROUBLESHOOTING AND A TEST FLIGHT, IT WAS DETERMINED THE NR 2 ENGINE WAS LEAKING OIL INTE RNALLY INTO THE BLEED AIR SYSTEM. THE TURBOMACHINE WAS REPLACED. GROUND RUNS AND ANOTHER TEST FLIGHT WERE PERFORMED WI TH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996012600287 19960126 00287 EU 1996 1 26 96ZZZX334 1 19960103 A 3260 INTRANSIT LIGHT BAG JETSTM JETSTM3101 1500215 EU LT MLG MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 838JS 741 FLT 4091 - AFTER TAKEOFF, AFTER LANDING GEAR WAS RETRACTED, LEFT MLG INTRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT RET URNED TO FIELD, LANDED WITHUT FURTHER INCIDENT. PIT MAINTENANCE JACKED THE AIRCRAFT, CONDUCTED A GEAR SWING, UNABLE TO DUPLICATE THE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A21EU 1996012600293 19960126 00293 EU 1996 1 26 96ZZZX340 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 0585 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR AWXA96003, AND NR 96ZZZX341. ( X) 2 L 7 2 4F RT A28NM 1996012600294 19960126 00294 EU 1996 1 26 96ZZZX341 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 6155 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR AWXA96003, AND NR 96ZZZX340. ( X) 2 L 7 2 4F RT A28NM 1996012600308 19960126 00308 EU 1996 1 26 AWXA96003 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 3414 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR 96ZZZX340, AND NR 96ZZZX341. ( X) 2 L 7 2 4F RT A28NM 1996012600321 19960126 00321 NM 1996 1 26 IXKA960001 1 19960102 A 5753 TORQUE TUBE BOEING 727 727251 138408H NM TE FLAPS LOOSE A A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 259US 19978 ATL/MDW - FLT 59 - INBOARD FLAPS WOULD NOT RETRACT ABOVE 15 DEGREES. AIR TURN BACK TO ATL. ON SYSTEM OPS AND INSPECTIO N, FOUND FLAPS IN BYPASS MODE. RESET ASSYMETRY. FOUND LOOSE TORQUE TUBE COUPLING AT OUTBOARD FLAP POWER CONTROL UNIT. SECURED LOOSE TORQUE TUBE COUPLING, RETORQUED SCREWS. OPS CHECK OK PER 27-51-01. (X) 2 L 7 3 4F A3WE 1996012600322 19960126 00322 NM 1996 1 26 P9IA096002 1 19960117 A 4980 4353919M EXHAUST CLAMP BOEING 727 727231 1384079 NM APU FAILED A P9IA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 03 12305 63828 19562 DURING GROUND OPERATION OF APU, THE FIRE WARNING ACTIVATED AND THE APU AUTO SHUT DOWN WITH SMOKE COMING OUT OF THE APU S HROUD. INSPECTION FOUND CLAMP BROKEN FOR INNER EXHAUST DUCT AT SPOT WELD. INSPECTED APU, NO OTHER DAMAGE NOTED. REPLA CED O-RING AND CLAMP. RUN AND OPS CHECKS GOOD, MM 49-00. (X) 2 L 7 3 4F A3WE 1996012600325 19960126 00325 EU 1996 1 26 SIMA960051 1 19960104 A 3350 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 107AE 340A107 ACT - FLT 3906 - FORWARD EMERGENCY SIGN LIGHTS INOPERABLE. FOUND ON CREW PREFLIGHT INSPECTION. REPLACED BATTERY PACK. SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600326 19960126 00326 EU 1996 1 26 SIMA960091 1 19960108 A 3350 3012007 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AT 210 377 DFW - FLT 3819 - CENTER AIRCRAFT EMERGENCY LIGHTS STAYED ON ALL THE TIME. MAINTENANCE REPLACED THE NR 2 BATTERY PACK. O PS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996012600329 19960126 00329 NE 1996 1 26 UIEA9601 2 19960107 A 7261 RR34150G SCAVENGE PUMP BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE FAILED A UIEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 15 508MC 57603 11373 21644 530288 BANKOK/TAIPEI, CI346/07 - EN ROUTE, INCURRED NR 1 ENGINE SHUT DOWN IN FLIGHT-DESCENT PHASE FOR LOSS OF OIL PRESSURE AND N2 RPM. ON ARRIVAL, CHECKED MAIN OIL SCREEN AND CHIP DETECTORS ALL OK. FOUND LUBE AND OIL SCAVENGE PUMP DRIVE SHAFT SH EARED. DRAINED ENGINE OIL, REPLACED SCAVENGE PUMP, SERVICED ENGINE. ENGINE RUN-UP, OPS CHECK OK. (X) 2 L 7 4 4F 4 F A20WE E23EA 1996012600330 19960126 00330 WP 1996 1 26 9601259933 1 19960121 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 133U 47280 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE. RECYCLED LANDING GEAR AND AIRCRAFT SHIFTED INTO FLIGHT MODE. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. SERVICED NOSE GEAR STRUT, CLEANED GROUND SENSING SWITC HES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600331 19960126 00331 WP 1996 1 26 9601269967 1 19960120 A 2421 GENERATOR DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 9331 47263 DURING TAKEOFF, THE GLIDESCOPE, SPEED COMMAND AND COMPASS FLAGS CAME ON. ALSO, THE NR 1 EPR GAUGE INDICATOR STARTED TO DECREASE. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT ENGINE GENERATOR, CONSTANT SPEED DRIVE AND CONST ANT SPEED DRIVE OIL COOLER. FLUSHED AND CLEANED LINES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600332 19960126 00332 1996 1 26 9601279982 4 19960119 A 3418 80098717 AOA TRANSDUCER DOUG DC9 DC932 3022066 WP NR 2 FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 982US 39501 210 45790 DURING CLIMB, THE STALL INDICATION WARNING LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT RE MAINED ILLUMINATED MOMENTARILY, THEN EXTINGUISHED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ANGLE OF ATTACK TRANSDUCER AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600333 19960126 00333 WP 1996 1 26 9601289911 1 19960119 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 961N 47405 DURING TAKEOFF, A VIBRATION WAS DETECTED FROM THE NOSE WHEEL. AIRCRAFT CONTINUED TAKEOFF AND RETURNED TO MSP LANDING WI THOUT INCIDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN. SECURED DOOR AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600334 19960126 00334 WP 1996 1 26 9601299954 1 19960119 A 3230 CONTROL VALVE DOUG DC9 DC931 3022065 WP LANDING GEAR ICED UP A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. FOUND ICE ON L ANDING GEAR CONTROL VALVE. REMOVED ICE AND OPERATIONAL CHECK OF LANDING GEAR SYSTEM GOOD. 2 L 7 2 4F A6WE 1996012600335 19960126 00335 WP 1996 1 26 9601309954 1 19960119 A 3230 SHIFT MECH DOUG DC9 DC931 3022065 WP LANDING GEAR ICED UP A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. FOUND ICE AND SNOW ON GROUND SHIFT MECHANISM. REMOVED SNOW AND ICE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600336 19960126 00336 WP 1996 1 26 9601319994 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8979E 47328 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600337 19960126 00337 WP 1996 1 26 9601329986 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 TO 11. REPLACED BATTERIES AND OPERATIONAL CHEC K GOOD. 2 L 7 2 4F A6WE 1996012600338 19960126 00338 WP 1996 1 26 9601339972 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE CHECK, FOUND CEILING AND MID CABIN EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996012600339 19960126 00339 WP 1996 1 26 9601349957 1 19960121 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT/RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE CHECK, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERAT IONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600340 19960126 00340 WP 1996 1 26 9601359917 1 19960121 A 3350 LIGHT DOUG DC9 DC932 3022066 WP DOOR 1L INTERMITTENT A NWAA K NONE L NO TEST CR CRUISE 1 GL 01 967N 47573 DURING CRUISE, THE FORWARD EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY, BATTERIES AND THE EM ERGENCY EXIT SIGN AT DOOR 1L. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600341 19960126 00341 WP 1996 1 26 9601369907 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE CHECK, FOUND AFT INTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. RESET BATTERY PACK AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996012600342 19960126 00342 WP 1996 1 26 9601379902 1 19960121 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 952N 47073 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600343 19960126 00343 WP 1996 1 26 9601389998 1 19960120 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE CHECK, FOUND AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996012600344 19960126 00344 NM 1996 1 26 9601396601 1 19960119 A 2910 HYD SWIVEL BOEING 747 747151 1384891 NM RT MLG BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 601US 19778 DURING CLIMB, AIRCRAFT LOST HYDRAULIC QUANTITY ON THE NR 4 HYDRAULIC SYSTEM, WHEN THE LANDING GEAR WAS RETRACTED. AIRCR AFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. FOUND BROKEN SWIVEL JOINT ON THE RIGHT WING LANDING GEAR DOWNLOCK ACTU ATOR. REPLACED ADP AND EDP ASSEMBLIES. REPLACED CASE DRAIN AND PRESSURE FILTER FOR ADP/EDP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996012600345 19960126 00345 WP 1996 1 26 9601409876 1 19960118 A 3231 DOOR LINKS DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 785NC 48110 DURING CLIMB, A VIBRATION WAS FELT FROM THE NOSE LANDING GEAR AREA ON GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDE D WITHOUT INCIDENT. REPLACED BOTH NOSE GEAR DOOR LINKS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600346 19960126 00346 WP 1996 1 26 9601419856 1 19960120 A 3350 60030451 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600347 19960126 00347 NM 1996 1 26 9601422761 1 19960120 A 2131 CONTROLLER BOEING 727 7272M7 138407S NM CABIN FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 721RW 21200 DURING FLIGHT, LOST CABIN PRESSURE AT FL 350. AN EMERGENCY DESCENT TO 8,000 FEET WAS MADE, LAST 150 MILES FLOWN AT 8,00 0 FEET. AIRCRAFT LANDED WITHOUT INCIDENT AT MSP. PERFORMED PRESSURIZATION LEAK CHECK. REPLACED AUTO PRESSURE CONTROLL ER AND CONTROL PANEL. PERFORMED FUNCTIONAL CHECK AND SYSTEM OK FOR SERVICE. 2 L 7 3 4F A3WE 1996012600348 19960126 00348 NM 1996 1 26 96FDEA00111 1 19960120 A 5330 SKIN BOEING 727 727233 138408A NM BS 1073 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1973 STR 19 TO 20L, THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AN D INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600349 19960126 00349 NM 1996 1 26 96FDEA00112 1 19960120 A 5330 SKIN BOEING 727 727233 138408A NM BS 1030-1050 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1030 TO 1050, STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050, STR 20 TO 21L IN SKIN. FABRICATED A ND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600350 19960126 00350 NM 1996 1 26 96FDEA00113 1 19960122 A 5330 SKIN BOEING 727 727233 138408A NM BS 1050-1056 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FIVE DENTS IN SKIN STA 1050 TO 1056, STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600351 19960126 00351 NM 1996 1 26 96FDEA00114 1 19960120 A 5313 BAC1498138 STRINGER BOEING 727 727233 138408A NM BS 620 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 MECHANICAL DAMAGE IN HAT SECTION OF STRINGER, AT BS 620 STR 4R. REMOVED DAMAGED SECTION STRINGER 4R BS 620, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996012600352 19960126 00352 NM 1996 1 26 96FDEA00115 1 19960120 A 5313 BAC1498138 STRINGER BOEING 727 727233 138408A NM BS 460 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE ON STRINGER AT BS 460 STR 3R. REMOVED DAMAGED SECTION STR 3R BS 460, FABRICATED AND INSTALLED REPAIR PARTS PER FE DEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996012600353 19960126 00353 NM 1996 1 26 96FDEA00116 1 19960123 A 3610 322861001 VALVE BOEING 727 72725C 138400H NM LT/RT DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 116FE 19298 BOTH LT AND RT PURGE SHUTOFF VALVES PHYSICALLY DAMAGED, ENDS BLOWN OFF. REMOVED AND REPLACED VALVES, LT-12231, RT-C6419 8. 2 L 7 3 4F A3WE 1996012600354 19960126 00354 NM 1996 1 26 96FDEA00117 1 19960108 A 5711 SPAR BOEING 747 747245F 1384897 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 RT WING ROOT ON REAR SPAR LOCATION ATTACHMENT TO CENTER TANK, 4 HOLES IN THE REAR SPAR COMMON TO SPLICE PLATE AND 3 HOLE S IN THE SPLICE PLATE COMMON TO THE REAR SPAR FOUND CRACKED. SPLICE PLATE PLACED AND CRACKED FASTENER HOLES OVERSIZED A ND BUSHING INSTALLED AS PER FEDEX ERA NR B57-10-92 REV 1 65B14528-6, 65B15275-12, 1 EACH 15-5PH-1.250 INCH DIA 1 FT. 2 L 7 4 4F A20WE 1996012600355 19960126 00355 NM 1996 1 26 96UAL900051 1 19960122 A 2781 FLAP INDICATION BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 608UA 21869 LANDED UNDER AMBER ALERT DUE TO IRREGULAR FLAP CONFIGURATION. EICAS MESSAGE LEADING EDGE SLAT ASSYMMETRY DISPLAYED, LEA DING EDGE ILLUMINATED WITH FLAP LEVER, ONE UNIT. PERFORMED PSEU BITE TEST AND NO FAULT. LEADING EDGE AND TRAILING EDGE FLAPS OPERATED NORMAL. UNABLE TO DETECT ANY DEFECTS. 2 L 7 2 4F 4 F RT A1NM E3NE 1996012600356 19960126 00356 NM 1996 1 26 96UAL900052 1 19960122 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7272U 21419 EMERGENCY EXIT ABOVE DOOR 1L IS INOPERATIVE. REPLACED BATTERIES AND GROUND CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996012600357 19960126 00357 NM 1996 1 26 96UAL900053 1 19960122 A 3350 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7467U 21921 EMERGENCY EXIT LIGHT ABOVE DOOR 1 ILLUMINATES WITH POWER, SWITCH AND BATTERY OFF. REPLACED EXIT SIGN LIGHT ASSEMBLY AT DOOR 1L. 2 L 7 3 4F 4 F A3WE E2EA 1996012600358 19960126 00358 NM 1996 1 26 96UAL900054 1 19960122 A 3350 STRIP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9051U 19932 EMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F A16WE E2EA 1996012600359 19960126 00359 NM 1996 1 26 96UAL900055 1 19960122 A 3350 BATTERY BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 367UA 24536 EMERGENCY LIGHTS INOP AT ROWS 1, 10 TO 16, 18 AND DOOR 2 LEFT. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 2 4F RT A16WE 1996012600360 19960126 00360 NM 1996 1 26 96UAL900056 1 19960122 A 3350 STRIP BOEING 737 737522 138449F NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 912UA 25290 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHT STRIP INOP. REPLACED GALLEY LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F RT A16WE 1996012600361 19960126 00361 SO 1996 1 26 COMA9610033 1 19960119 A 3230 2094500102 UPLOCK HOOK EMB 120 EMB120RT SO LT MLG LACK OF LUBE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 200CD 16985 4467 120200 LT MLG WILL NOT RETRACT. FOUND UPLOCK HOOK ASSY TO BE BINDING. CLEANED AND LUBED UPLOCK ASSY AND SYSTEM OPERATES NORMA LLY. 2 L 7 2 4T RT A31SO 1996012600362 19960126 00362 SO 1996 1 26 COMA9610034 1 19960120 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA K NONE O OTHER CL CLIMB 1 SO 01 248CA 120228 RECEIVED FLAP DISAGREEMENT WARNING SHORTLY AFTER TAKEOFF. CLEANED FLAP TRACKS AND SYSTEM OPERATION NORMAL. 2 L 7 2 4T RT A31SO 1996012600363 19960126 00363 SO 1996 1 26 COMA9610035 1 19960121 A 3231 12012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 243CA 120212 WHEN LANDING GEAR RETRACTED, LT MLG INTRANSIT INDICATION REMAINED ON. REPLACED BROKEN LATCH ASSY ON INBD GEAR DOOR. 2 L 7 2 4T RT A31SO 1996012600364 19960126 00364 EU 1996 1 26 COMA9630019 1 19960118 A 3020 NH2466881 INLET HEAT SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 146CA 8365 2132 340A146 RT ENGINE INTAKE HEAT FAILED. REPLACED THE UNDER TEMP THERMISTOR WITH THE SPARE THERMISTOR AND SYSTEM OPERATES NORMAL. 2 L 7 2 4T RT A52EU 1996012600365 19960126 00365 EU 1996 1 26 COMA9630020 1 19960119 A 2910 7229152675 HYD TUBE SAAB SF340 SF340A 7850100 EU RT MLG LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 320CA 340A064 HYDRAULIC FLUID LEAKING FROM RT WHEEL WELL. REPLACED LEAKING BRAKE LINE WHICH WAS CHAFED THROUGH BY WOW HARNESS WIRING. 2 L 7 2 4T RT A52EU 1996012600366 19960126 00366 EU 1996 1 26 COMA9630021 1 19960121 A 5610 7256100502 WINDSHIELD SAAB SF340 SF340A 7850100 EU RT COCKPIT NOT SEALED A COMA K NONE O OTHER CR CRUISE 1 SO 01 358CA 12136 9613 340A047 COPILOTS WINDSHIELD SQUEALS DURING FLIGHT. REPLACED COPILOTS WINDSHIELD. 2 L 7 2 4T RT A52EU 1996012600367 19960126 00367 EA 1996 1 26 COMA9660017 1 19960121 A 3030 102AH2AG TAT PROBE HEAT CNDAIR CL600 CL6002B19 EA FUSELAGE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 7040 TAT PROBE HEAT CAUTION MESSAGE ON EICAS. REPLACED THE TAT PROBE. 2 L 7 2 4F RT A21EA 1996012600368 19960126 00368 EA 1996 1 26 COMA9660018 1 19960121 A 3222 16040101 STRUT CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 914CA 7012 NOSE LANDING GEAR STRUT BOTTOMS DURING TAXI. REPLACED THE NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 1996012600369 19960126 00369 EA 1996 1 26 COMA9660019 1 19960120 A 7714 5071T98P01 AMPLIFIER CNDAIR CL600 CL6002B19 EA RT ENGINE DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 933CA 7040 RT ENGINE WILL NOT ACHIEVE TAKEOFF THRUST. REPLACED THE N1 AMPLIFIER AND ENGINE RUNS NORMAL, ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996012600370 19960126 00370 1996 1 26 COMA9660020 4 19960119 A 3418 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS DEFECTIVE A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 952CA 1931 7092 WOW OUTPUT AND WOW INPUT CAUTION MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 1996012600371 19960126 00371 NM 1996 1 26 DHL96717005 1 19960119 A 3310 106075213 BALLAST BOEING 727 72723 1384004 NM COCKPIT FAILED A T DHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 717DH 19389 MEDIUM AMOUNT OF SMOKE IN COCKPIT FROM UNDER FRONT PANEL RIGHT SIDE. FOUND BALLAST FOR PANEL FLUORESCENT LIGHTS CAUSING SMOKE. DEACTIVATED SYSTEM, DEFERRED PER MEL 33-1. 2 L 7 3 4F A3WE 1996012600372 19960126 00372 NM 1996 1 26 DL72K960128 1 19960105 A 5330 6554590 SKIN BOEING 727 727232 1384082 NM BS 720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT AT THE FWD LT CORNER. THE CORROSION WAS CUTOUT AND REPAI RED WITH AN EXTERNAL AND AN INTERNAL DOUBLER PER FAA/DER FORM 8110-3, DATED 1-5-96. 2 L 7 3 4F A3WE 1996012600373 19960126 00373 NM 1996 1 26 DL72L960115 1 19960116 A 5330 65C20489 SKIN BOEING 727 727232 1384082 NM BS 1005 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 BELLY SKIN WAS CORRODED REQUIRING A 1 INCH BY 4 INCH CUTOUT OF THE SKIN. THE STA 1009 BUTT SPLICE IS AFT OF THE CUTOUT AND FORWARD OF AN EXISTING REPAIR. REPAIRED PER SRM 53-30-3 FIG 3A. 2 L 7 3 4F A3WE 1996012600374 19960126 00374 NM 1996 1 26 DL72L960134 1 19960117 A 5330 6554590 SKIN BOEING 727 727232 1384082 NM FS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 DURING INSPECTION, THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO HAVE CORROSION ON THE ATTACH FLANGE IN THE LT AF T CORNER. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 1-17-96, THE DAMAGE HAS BEEN BLENDED TO 0.59 MINIMUM FLANGE THI CKNESS. 2 L 7 3 4F A3WE 1996012600375 19960126 00375 NM 1996 1 26 DL72S960104 1 19960116 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND DURING E-2 LETTER CHECK, .375 INCH CRACK NR 4 L/E SLAT COVE SKIN LWR ATTACH ANGLE AT O/B END. REPAIRED PER M/M 57 -54-0 PAR 5A. 2 L 7 3 4F A3WE 1996012600376 19960126 00376 NM 1996 1 26 DL72S960105 1 19960116 A 5312 BLKHD WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND ON E2 LETTER CHECK, STA 870 BULKHEAD WEB CRACKED 3 INCHES AT APU LOAD CONTROL VALVE CUTOUT, LWR END IN RT W/W. RE PAIR PER SRM 53-10-9, TIME LIMITED INST. 2 L 7 3 4F A3WE 1996012600377 19960126 00377 NM 1996 1 26 DL72S960110 1 19960116 A 5320 ANGLE BOEING 727 727232 1384082 NM RT WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND ON E2 LETTER CHECK, KEEL BEAM VERT STIFFENER CRACKED .5 INCH FWD INBD RT W/W. TIME LIMITED REPAIR PER SRM 53-10-9 . 2 L 7 3 4F A3WE 1996012600378 19960126 00378 NM 1996 1 26 DL72S960118 1 19960106 A 5320 HINGES BOEING 727 727232 1384082 NM ACCESS DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 FROM MV2 ATL ITEM, CORROSION BEHIND HINGES ON ACCESS DOOR 3448R, LOC RT A/C COMP. REMOVED ACCESS DOOR 3448R, DAMAGE SEC TION OFF ANGLE AND INSTALLED REPAIR PER MM 53-30-1 PG 807. 2 L 7 3 4F A3WE 1996012600379 19960126 00379 NM 1996 1 26 DL72S960129 1 19960111 A 5321 FLOOR PAN BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON MV1 CHECK, LT AND RT LAV FLOOR PAN DITCHING SEAL PANEL CRACKED, VIEWED FROM BAG BIN FWD OF 1183. REPAIRED PER M/M 53-0-11. 2 L 7 3 4F A3WE 1996012600380 19960126 00380 NM 1996 1 26 DL72S960143 1 19960121 A 3350 334701745 LIGHT BOEING 727 727232 1384082 NM LT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 408DA 21152 ON INSPECTION, LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPN CKS NORMAL. 2 L 7 3 4F A3WE 1996012600381 19960126 00381 NM 1996 1 26 DL72S960147 1 19960121 A 3350 BATTERY PACK 20131A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 6800 20752 ON L/O CHECK, FOUND EMERGENCY LIGHTS OUT FROM ROW 27 AFT TO F/A SEAT. REPLACED BATTERY PACK M9027 AND OPS CHECKS NORMAL . 2 L 7 3 4F A3WE 1996012600382 19960126 00382 NM 1996 1 26 DL72S960152 1 19960119 A 2780 BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FROM HMV ATL, NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET CRACKED. INSTALLED REPAIR PER MM 57-20-21 PG 811. 2 L 7 3 4F A3WE 1996012600383 19960126 00383 NM 1996 1 26 DL72S960157 1 19960117 A 3260 H1010154 DNLOCK SWITCH BOEING 727 727232 1384082 NM NLG FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 496DA 21076 ON GEAR EXTENSION RECEIVED RED NOSE GEAR LIGHT, VISUALLY VERIFIED DOWN AND LOCKED. REPLACED NOSE GEAR DOWNLOCK SWITCH A ND NOSE GEAR POSITION SWITCH. ALSO, AS PRECAUTION REPLACED LANDING GEAR ACCESORY UNIT AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996012600384 19960126 00384 NM 1996 1 26 DL72S960160 1 19960116 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 401DA 21145 ON PREDEPARTURE, EMERGENCY TRACK LIGHTS IN FWD CABIN INOP. REPAIRED BROKEN WIRE AT ROW 14 AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996012600385 19960126 00385 NM 1996 1 26 DL72W960116 1 19960114 A 5521 SPAR BOEING 727 7272Q8 138407W NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 THE RIGHT HAND ELEVATOR REAR SPAR HAD A CRACK EMANATING .25 INCH FROM THE INBOARD SIDE OF THE SHEAR PLATE, AT THE THIRD FROM INBOARD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. CRACK WAS WITHIN THE S/B 55-0087 INTERIM REPAIR 0.250 ALLOWABLE LIMIT ON CRACK LENGTH BEYOND THE END OF THE SHEAR PLATE. THE CRACK WAS STOP DRILLED PER THE S/B 55-0087 REV 1. THE S/ B INITIATED THE REQUIRED REPETITIVE INSPECTION AND PERMANENT REPAIR. 2 L 7 3 4F A3WE 1996012600386 19960126 00386 NM 1996 1 26 DL72W960119 1 19960117 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 FOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0. 2 L 7 3 4F A3WE 1996012600387 19960126 00387 NM 1996 1 26 DL72W960127 1 19960119 A 3350 334701744 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 DURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL. 2 L 7 3 4F A3WE 1996012600389 19960126 00389 NM 1996 1 26 DL73E960145 1 19960121 A 3350 081691 SOCKET BOEING 737 737247 138448D NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 382DL 23609 EMERGENCY FLOOR LIGHT AT ROW 2 IS INOP. REPLACED SOCKET, DL (P/N 337201959), (MFG 08169-1), OPS GOOD. 2 L 7 2 4F A16WE 1996012600390 19960126 00390 NM 1996 1 26 DL73E960159 1 19960114 A 3260 DN SWITCH BOEING 737 737247 138448D NM LANDING GEAR FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 376DL 23603 WHEN LANDING GEAR WAS PLACED DOWN, ALL 3 GREEN AND ALL 3 RED LIGHTS ILLUMINATED. REPLACED GEAR HANDLE DOWN SWITCH (S-78 ), OPERATION NORMAL. 2 L 7 2 4F A16WE 1996012600391 19960126 00391 NM 1996 1 26 DL73S960158 1 19960120 A 3240 AV24E1144 VALVE BOEING 737 737232 1384475 NM PARKING BRAKE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 329DL 23101 ON CLIMBOUT, LOST A/B HYDRAULIC SYSTEM PRESSURE. FLIGHT RETURNED MSP. FOUND PARKING BRAKE VALVE LEAKING. REPLACED VAL VE, SERVICED SYSTEM AND OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996012600392 19960126 00392 NM 1996 1 26 DL757960120 1 19960117 A 3350 767 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 620DL 22910 DURING INSPECTION, FOUND EMERGENCY LIGHT AT R-2 DOOR INOP. RELAMPED AND CHECKS GOOD. 2 L 7 2 4F RT A2NM 1996012600393 19960126 00393 NM 1996 1 26 DL757960121 1 19960117 A 3350 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 646DL 24217 R2 DOOR OUTSIDE EMERGENCY LIGHT INOP. EMERGENCY TRACK LIGHT AT ROW 1, 28 INOP. RELAMPED AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996012600394 19960126 00394 NM 1996 1 26 DL757960124 1 19960118 A 5754 114N4004166A TE WEDGE BOEING 757 757232 1384965 NM NR 8 LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 634DL 23615 DURING INSPECTION, NR 8 L/E SLAT TRAILING EDGE WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-07. 2 L 7 2 4F RT A2NM 1996012600395 19960126 00395 NM 1996 1 26 DL757960125 1 19960118 A 3350 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 25142 R2 DOOR EXIT LIGHT DID NOT ILLUMINATE DURING LIGHT TEST. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996012600396 19960126 00396 NM 1996 1 26 DL757960132 1 19960119 A 5610 141T480120 WINDSHIELD BOEING 757 757232 1384965 NM LT FLT DECK FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 680DA 26956 COPILOT WINDSHIELD OUTER PANE SHATTERED, CLIMBING THROUGH 10,000 FT. FLIGHT RETURNED JFK. REPLACED WINDSHIELD. 2 L 7 2 4F RT A2NM 1996012600397 19960126 00397 NM 1996 1 26 DL757960136 1 19960118 A 5754 114N4005157 TE WEDGE BOEING 757 757232 1384965 NM NR 4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING INSPECTION, FOUND THE TRAILING EDGE WEDGE ON THE NR 4 SLAT DELAMINATED IN THE UPPER SKIN. THERE IS A PREVIOUS RE PAIR DOUBLER THAT MEASURES 2 INCHES FORE/AFT AND 10 INCHES WIDE, INSTALLED IN THE DAMAGED REGION. REPAIRED TRAILING EDG E WEDGE IN ACCORDANCE WITH B757 SRM 51-70-10. 2 L 7 2 4F RT A2NM 1996012600398 19960126 00398 NM 1996 1 26 DL767960139 1 19960120 A 3350 BULB BOEING 767 767232 1385132 NM RT OVERWING FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 106DA 22218 RT OVERWING EMERGENCY LIGHT INOP. RELAMPED AND CLEANED CONTACT. 2 L 7 2 4F RT A1NM 1996012600399 19960126 00399 WP 1996 1 26 DLL10960137 1 19960118 A 2150 ACTUATOR 75010304 LKHEED 1011 10113851 5265010 WP NR 2 PACK FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 722DA 2204 193C1147 AFTER TAKEOFF HAD BURNING ODOR AND VISIBLE SMOKE, RETURNED HNL. RAN ALL ENGINES, COULD NOT DUPLICATE. RAN PACKS, ALL N ORMAL. REPLACED NR 3 WATER SEPARATOR BAG. DUE TO HISTORY SUBSEQUENT MAINTENANCE FOUND FAULTY NR 2 PACK RAMA AIR DOOR A CTUATOR. REPLACED ACTUATOR. 2 L 7 3 4F A23WE 1996012600400 19960126 00400 WP 1996 1 26 DLL10960146 1 19960121 A 3350 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 716DA 193C1095 FOUND EMERGENCY TRACK LIGHT AT SEAT 43GH INOP. REPLACED BULB AND EMERGENCY TRACK LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A23WE 1996012600401 19960126 00401 WP 1996 1 26 DLL13960095 1 19960116 A 3233 327003309 ACTUATOR LKHEED 1011 10113851 5265010 WP LT MLG CRACKED A DALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 27 790DL 193A1143 LEFT MLG ACTUATOR CYLINDER LOWER END CRACKED COMPLETELY AND FAILED DURING PREFLIGHT OPERATIONS POST HMV. CAUSED COMPLET E LOSS OF C-SYSTEM HYD FLUID. CYLINDER APPEARS TO NOT HAVE BEEN IDENTIFIED AS BEING MODIFIED PER SB. REPLACED CYLINDER . 2 L 7 3 4F A23WE 1996012600402 19960126 00402 WP 1996 1 26 DLL13960122 1 19960117 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1765 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 DURING HMV INSPECTION, THE FUSELAGE SKIN WAS FOUND SEVERELY CORRODED AT FS 1765, STR 39. THE DAMAGE WAS TRIMMED OUT AND FINAL CUT OUT DIMENSIONS ARE 8.5 INCH BY 7.5 INCH. AN EXTERNAL DOUBLER WILL BE INSTALLED AS A PERMANENT REPAIR PER DL ERA 272931 REV C. 2 L 7 3 4F A23WE 1996012600403 19960126 00403 WP 1996 1 26 DLL13960123 1 19960117 A 5320 1542395 PRESS DECK LKHEED 1011 10113851 5265010 WP BS 359 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 THE NLG PRESSURE DECK CONTAINED CORROSION THAT WAS CUT OUT AT STA 359, LBL 26. THE FINAL CUT OUT DIMENSIONS ARE 4 INCH BY 8 INCH. INSTALLED REPAIR PER DL ERA 273038 R B. 2 L 7 3 4F A23WE 1996012600404 19960126 00404 WP 1996 1 26 DLL15960103 1 19960116 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 54040 193Y1184 OVERHEAD EMERGENCY LIGHTS AT 20AB INOP. REPLACED DEFECTIVE BATTERY PACK AT 22AB OVERHEAD AND LIGHTS CHECK GOOD. 2 L 7 3 4F A23WE 1996012600405 19960126 00405 WP 1996 1 26 DLL17960102 1 19960116 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 56640 193H1202 EMERGENCY LIGHTS AT L-3 DOOR INOP. REPLACED POWER SUPPLY AND EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F A23WE 1996012600406 19960126 00406 NM 1996 1 26 DLM11960140 1 19960120 A 5610 NBA6045501 WINDSHIELD DOUG MD11 MD11 3023602 NM LT COCKPIT CRACKED A DALA K NONE O OTHER DE DESCENT 1 SO 27 801DE 48472 CAPT WINDSHIELD BROKE ON DESCENT THROUGH FL 310. REPLACED CAPT WINDSHIELD PER M/M 56-11-01. ALSO, REPLACED ANTI-ICE CO NTROLLER ON LOG 790446/002. 2 L 7 3 4F RT A22WE 1996012600407 19960126 00407 NM 1996 1 26 DLM11960141 1 19960120 A 3040 9615046004 CONTROLLER DOUG MD11 MD11 3023602 NM LT WINDSHIELD FAILED A DALA K NONE O OTHER DE DESCENT 1 SO 27 801DE 48472 DUE TO CAPT WINDSHIELD CRACK, REPLACING CAPT/LEFT WINDSHIELD ANTI-ICE CONTROLLER. REPLACED LEFT WINDSHIELD ANTI-ICE CON TROLLER. WINDSHIELD REPLACED ON LOG 790446/001. 2 L 7 3 4F RT A22WE 1996012600408 19960126 00408 NM 1996 1 26 DLM88960096 1 19960116 A 3260 BULB DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 SO 27 920DE 53423 ON APPROACH TO CVG, RIGHT MLG DOWNLOCK IND GREEN LIGHT FAILED TO ILLUMINATE. ALL OTHER IND WERE NORMAL, NO HORN AND NO RED LIGHT. CHECKED SENSORS RT GEAR AND PERFORMED BITE CHECK OF PSEV, NO FAULTS. RELAMPED RT GEAR POS IND AND CHECKS GO OD. 2 L 7 2 4F RT A6WE 1996012600409 19960126 00409 1996 1 26 DLM88960126 4 19960118 A 3425 AHARS 4608000307 DOUG MD88 MD88 3023688 NM LT/RT COCKPIT FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 946DL 696 49819 IN FLIGHT BOTH CAPTS AND F/O COMPASSES TUMBLE. AIRCRAFT RETURNED TO DFW. REPLACED BOTH AHARS UNITS AND SYS OPNS NORMAL . 2 L 7 2 4F RT A6WE 1996012600411 19960126 00411 NM 1996 1 26 DLM88960155 1 19960102 A 3232 5939710502 ACTUATOR DOUG MD88 MD88 3023688 NM LT MLG DOOR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 949DL 49880 ON GEAR RETRACTIONS RED LIGHT RT MAIN GEAR EXTENDED 3 GREEN BUT GEAR DOOR OPEN LT ON. FLIGHT RETURNED TO BOS. FOUND BR OKEN TORQUE SHAFT. REPLACED RT GEAR DOOR AND DOOR ACTUATOR. 2 L 7 2 4F RT A6WE 1996012600412 19960126 00412 WP 1996 1 26 MWEA96019 1 19960120 A 5530 ANGLE DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND VERTICAL STAB TO FUSELAGE EXTERIOR ATTACH ANGLE CRACKED ON LT SIDE APPROX 8 INCH FROM AFT END. IN STALLED DOUBLER REPAIR IAW SRM 53-05 FIG 23. 2 L 7 2 4F A6WE 1996012600413 19960126 00413 WP 1996 1 26 MWEA96020 1 19960120 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND ANGLE AT FS 1076 IN AFT ACCESSORY COMPT CRACKED AT LONGERON 16R. FABRICATED AND INSTALLED ANGLE I AW SRM 53-01. 2 L 7 2 4F A6WE 1996012600414 19960126 00414 NM 1996 1 26 P5CA9600023 1 19960123 A 5755 SKIN BOEING 747 747122 1384872 NM NR 9 SPOILER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CORROSION AND SLIGHT BULGING OF PAINT AROUND RIVET HEAD FORWARD OF NR 9 SPOILER. CLEANED AND TREATED PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 1996012600415 19960126 00415 NE 1996 1 26 P5CA9600024 2 19960123 A 7250 SLEEVE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND TURBINE REVERSER SLEEVE CRACKED BETWEEN TWO PREVIOUS REPAIRS. REPAIRED IAW SRM 54-30-03. REPAIR INCLUDES BOTH PR EVIOUS REPAIRS. 2 L 7 4 4F 4 F A20WE E20EA 1996012600416 19960126 00416 NM 1996 1 26 P5CA9600025 1 19960123 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2658 CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND APU COMPT FORWARD BULKHEAD FWD SIDE CHAFED THROUGH AT STA 2658, CAUSED BY IMPROPERLY INSTALLED SHROUD AT BULKHEAD. REPAIRED DAMAGED AREA IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996012600417 19960126 00417 NM 1996 1 26 P5CA9600026 1 19960122 A 2710 ACTUATOR BOEING 747 747121 1384871 NM RT AILERON INOPERATIVE A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 831FT 19648 DURING TAXI OUT, ON FLIGHT CONTROL CHECK, FOUND RT AILERON WOULD NOT UNLOCK FROM HIGH SPEED MODE WITH FLAPS IN TAKEOFF P OSITION. RETURNED TO BLOCKS, APPLIED HEAT TO AILERON LOCKOUT ACTUATOR AND SYSTEM BECAME OPERATIVE. OPERATIONAL CHECK G OOD IAW MM 27-11-00. 2 L 7 4 4F A20WE 1996012600419 19960126 00419 NM 1996 1 26 VSTA9601012 1 19960106 A 5523 6573799501 TAB BOEING 737 737247 138448D NM LT ELEVATOR CRACKED A VSTA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 WP 07 303VA 20125 INTERMITTENT AIRFRAME VIBRATION. LOOSE FASTENERS AT LT ELEVATOR INBOARD HINGE LUG. REPLACED LT ELEVATOR TAB. 2 L 7 2 4F A16WE 1996012600420 19960126 00420 NM 1996 1 26 VSTA9601013 1 19960120 A 5230 57094 SEAL BOEING 737 737204 1384458 NM CARGO DOOR LEAKING A VSTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 312VA 20236 UNABLE TO HOLD PRESSURIZATION IN AIRCRAFT CABIN. AFT CARGO DOOR SEAL LEAKING. REMOVED AND REPLACED DOOR SEAL. 2 L 7 2 4F A16WE 1996012600463 19960126 00463 WP 1996 1 26 HAL9602 1 19960107 A 3260 0080004003 PROX CONTL BOX DOUG DC9 DC951 3022051 WP RT MLG/NLG MALFUNCTIONED A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 2FOR 460 47796 HNL - FLT 516 - INFORMATION FROM LOG PAGE 149767-1. RED NOSE AND RT MAIN UNSAFE LIGHTS AFTER GEAR RETRACTION. RECYCLED , UNABLE TO EXTINGUISH ONE OR BOTH. CHECKED WIRING ON RT MAIN AND NOSE GEAR. FOUND OK. REPLACED PROXIMITY CONTROL BOX . RETRACTION CHECK OK. (X) 2 L 7 2 4F A6WE 1996012600464 19960126 00464 WP 1996 1 26 9601439912 1 19960120 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR TAILCONE HANDLES. REPLAC ED THE CLIPS AND HANDLES PER EO 5350-01049. 2 L 7 2 4F A6WE 1996012600465 19960126 00465 WP 1996 1 26 9601449754 1 19960115 A 5210 CLOSING MECH DOUG DC9 DC941 302207N WP CABIN DOOR MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 754NW 47178 MBS-DTW - UPON ARRIVAL, FOUND THAT THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE RERIGGED THE DOOR PER MM 52-11-0 PG 501 TO 514. REPLACED LOCK ADJUSTMENT AND CRANK ROD ENDS. PRESSURE AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996012600466 19960126 00466 WP 1996 1 26 9601459754 1 19960119 A 5210 BAYONET DOUG DC9 DC941 302207N WP PAX DOOR OUT OF RIG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 754NW 47178 RST-MSP - AFTER ARRIVAL, FOUND THAT THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE RERIGGED THE MAIN C ABIN DOOR PER MM 52-11-00. 2 L 7 2 4F A6WE 1996012600467 19960126 00467 NE 1996 1 26 9601461148 2 19960119 A 7532 SOLENOID DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 148US 46757 86181 DURING LANDING, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. EGT INCREASED TO TOP OF SCALE. CREW FOLLOWED COCKPIT OPE RATING PROCEDURE, SHUT NR 1 ENGINE DOWN AND MOTORED UNTIL EGT IS BELOW 100C. BORESCOPED NR 1 ENGINE AND INSPECTED PER M M 71-00-00. REPLACED RABS SOLENOID AND ALL CHECKS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996012600468 19960126 00468 NM 1996 1 26 9601476601 1 19960120 A 3240 SELECTOR VALVE BOEING 747 747151 1384891 NM BRAKE SYST FAILED A NWAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 GL 01 601US 19778 AFTER TAKEOFF, GEAR AND FLAPS CHECKED UP, NR 4 HYDRAULIC SYSTEM QUANTITY INDICATION ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO NRT. REPLACED RESERVE BRAKE SELECTOR VALVE AND PERFORMED LEAK CHECK. CHECK WAS NOR MAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 1996012600469 19960126 00469 WP 1996 1 26 9601489608 1 19960122 A 3260 BULB DOUG DC9 DC932 3022066 WP NLG MISINSTALLED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 608NW 47233 DURING APPROACH, THE NOSE LANDING GEAR GREEN LIGHT ILLUMINATED. PERFORMED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDEN T. INSTALLED CORRECT BULB FOR NOSE LANDING GEAR INDICATION AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600470 19960126 00470 NM 1996 1 26 9601492292 1 19960120 A 3234 CONTROL VALVE BOEING 727 727251 138408H NM LANDING GEAR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 292US 21503 AFTER TAKEOFF, GEAR WOULD NOT RETRACT AND GEAR HANDLE WOULD NOT RAISE TO THE 'UP' POSITION. AIRCRAFT RETURNED TO MSP AN D LANDED WITHOUT INCIDENT. REPLACED THE LANDING CONTROL VALVE AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996012600471 19960126 00471 NM 1996 1 26 9601506302 1 19960121 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 35 TO 43 WERE FOUND INOPERATIVE. RECONNECTED EMERG ENCY LIGHT CONNECTOR AT SEAT ROW 43 AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600472 19960126 00472 NM 1996 1 26 9601512771 1 19960121 A 2150 MIX VALVE BOEING 727 7272M7 138407S NM RT PACK FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 742RW 21952 DURING FLIGHT, LOSE RIGHT AIR CONDITIONING PACK WITH LOSS OF PRESSURIZATION. AIRCRAFT DROPPED TO 10,000 FEET AND RETURN ED TO MSP. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HAND PACK MIX VALVE AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996012600473 19960126 00473 WP 1996 1 26 9601529601 1 19960121 A 3260 PUSH ROD DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 601NW 47038 DURING APPROACH, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR DOOR SEQUENCE DRIVE ARM PU SH ROD OUT OF RIG. RIGGED PUSH ROD AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600474 19960126 00474 NM 1996 1 26 9601532771 1 19960123 A 3350 POWER SUPPLY BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 742RW 21952 DURING PREFLIGHT, FOUND SECTION OF FLOOR PATH EMERGENCY LIGHTS LEFT SIDE OF CABIN INOPERATIVE. REPLACED POWER SUPPLY AN D BATTERY, CHECKED OK. 2 L 7 3 4F A3WE 1996012600475 19960126 00475 NM 1996 1 26 9601542202 1 19960121 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 202US 22155 DURING PREFLIGHT, FOUND BOTH OVERWING EXIT SIGN EMERGENCY LIGHTS INOPERATIVE ON RIGHT SIDE OF AIRCRAFT. REPLACED BATTER IES IN POWER SUPPLY AND CHECKED OK. 2 L 7 3 4F A3WE 1996012600476 19960126 00476 NM 1996 1 26 96FDEA00119 1 19960116 A 5510 STRINGER BOEING 747 747245F 1384897 NM STA 152.4-184.80 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 RT HORIZ STAB COMP STR 10 BETWEEN STAB STA 152.4 AND 184.80 FOUND CORRODED. MINOR SURFACE CORROSION REMOVED AND AREA RE PROTECTED AS PER SRM FEDEX 51-10-01 AND 51-10-02 REV 76 WITHIN LIMITS AS PER SRM FEDEX 55-10-01 REV 76. 2 L 7 4 4F A20WE 1996012600477 19960126 00477 NM 1996 1 26 96UAL900057 1 19960123 A 3350 BATTERY BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 153UA 20102 EMERGENCY LIGHTS INOP IN THE CEILING AT ROW 38 AND LAVATORY 117. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 4 4F 4 F A20WE E20EA 1996012600478 19960126 00478 NM 1996 1 26 96UAL900058 1 19960123 A 3350 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 FLOOR EMERGENCY ESCAPE LIGHTING INOP AT ROW 13. RECONNECTED FLOOR EMERGENCY ESCAPE LIGHTING AT ROW 13 AND OPERATION CHE CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600479 19960126 00479 NM 1996 1 26 96UAL900059 1 19960123 A 2612 1061096115 FIRE DETECTOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE ENGINE INOPERATIVE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 29 986UA 21748 CREW REPORTS NR TWO ENGINE FIRE WARNING WENT OFF IN CLIMB-OUT. FIRED BOTTLE AND SHUT DOWN ENGINE. REPLACED LOWER FIRE LOOP DETECTOR. TESTED ENGINE FIRE DETECTION SYSTEM. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996012600480 19960126 00480 WP 1996 1 26 ARWA9601001 1 19960117 A 5341 3613917 FITTING DOUG DC8 DC863F 302198F WP LT MLG WW CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LEFT WHEEL WELL FWD BULKHEAD, UPPER OUTER WING ATTACH FORGING AND ADJACENT SKIN HAS LEVEL II CORROSION. CLEANED CORRODE D AREA, CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED DOUBLER, TWO REPAIR STRAPS AND PLUG. IN STALLED IAW DER EO ARW 950173-082, FAA FORM 8110-3 ATTACHED. 2 L 7 4 4F 4A25 1996012600481 19960126 00481 WP 1996 1 26 ARWA9601002 1 19960117 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 454 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LEFT WING STA 454 NEAR CENTER SPAR HAS 5 INCH CRACK INBOARD AND AFT OF HI-LOCK. REMOVED CRACK, FABRICATED PLUG AND DOUB LER. INSTALLED SAME IAW AVITAS ENGINEERING EO 96AROW002D-1, FAA FORM 8110-3 ATTACHED. 2 L 7 4 4F 4A25 1996012600483 19960126 00483 NM 1996 1 26 DL72S960169 1 19960119 A 5313 65564415 STRINGER BOEING 727 727232 1384082 NM FS 950-990 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/ B AND I/B SKIN FLANGES, STRINGER 29L BETWEEN STA 950 AND STA 970. MINIMUM REMAINING FLANGE THICKNESS WAS .100. ALL COR ROSION BLENDS ARE CONSIDERED ACCEPTABLE AS PERMANENT REPAIRS. ALSO, THE STRINGER REQUIRES SPLICING BETWEEN STA 950F AND 970, DUE TO CRACKING AND EXTENSIVE CORROSION BETWEEN STA 970 AND 990. THERE IS AN EXISTING SPLICE LOCATED AT STA 990 P LUS 10. THIS REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DL ERA 303010 REV A. 2 L 7 3 4F A3WE 1996012600484 19960126 00484 NM 1996 1 26 DL72S960170 1 19960119 A 5314 65454414 KEEL BEAM BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, THE OUTBD FLANGE OF THE RT KEEL BEAM, STR 29R WAS FOUND WITH CORROSION AT STA 950. DUE TO INTERFEREN CE ITEMS IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO REMOVE THE CORRODED FLANGE. REPAIR DOUBLERS AND STRAPS WERE INSTA LLED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DATED 01-19-96. 2 L 7 3 4F A3WE 1996012600485 19960126 00485 NM 1996 1 26 DL72S960171 1 19960105 A 5754 651622199 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING INSP, THE FOLLOWING DAMAGE WAS FOUND REQUIRING MRR'S N/R 0058 CRACKS FOUND IN NR 9 AND NR 18 RIB. REPAIRED PER M /M 57-54-0 FIG 805. N/R 0059 CRACKS FOUND IN REPAIR DOUBLERS ON NR 11 AND 12 RIBS. REPAIRED PER M/M 57-54-00. N/R 006 2 CRACK FOUND IN UPPER SKIN AT FENCE MOUNTING HOLE. REPAIRED PER M/M 57-54-0 FIG 813 FOR NR 4 L/E SLAT. 2 L 7 3 4F A3WE 1996012600486 19960126 00486 NM 1996 1 26 DL72S960172 1 19960105 A 5754 651622199 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 CRACK FOUND IN LWR AFT ATTACH ANGLE. REPAIRED PER M/M 57-54-00 FOR NR 4 L/E SLAT. 2 L 7 3 4F A3WE 1996012600488 19960126 00488 1996 1 26 DL72S960178 4 19960123 A 2565 CABLE BOEING 727 727232 1384082 NM L2 DOOR SLIDE BROKEN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 499DA 21143 LEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. R EPLACED DOOR SLIDE PER M/M 25-60-15. 2 L 7 3 4F A3WE 1996012600489 19960126 00489 NM 1996 1 26 DL73E960156 1 19960112 A 5321 FLOOR PANEL BOEING 737 737247 138448D NM FS 777 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING HMV, LT FIXED FLOOR PANEL AT FS 777 FOUND CORRODED BEYOND LIMITS. REPAIRED PER MM 53-21-04 PG 801. 2 L 7 2 4F A16WE 1996012600490 19960126 00490 1996 1 26 DL73S960144 4 19960121 A 3425 DG BOEING 737 737232 1384475 NM NR 1 INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 327DL 23099 AIR TURNBACK, NR 1 COMPASS SYSTEM INTERMITTENTLY INOP, HGD FLAG IN CAPT HSI AND F/O RMI. REPLACED NR 1 DG AND OPS CKS O K. 2 L 7 2 4F RT A16WE 1996012600491 19960126 00491 NM 1996 1 26 DL767960149 1 19960122 A 3260 SENSOR BOEING 767 767232 1385132 NM NLG MALFUNCTIONED A A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 106DA 22218 RETRACTING FLAPS TO UP POSITION AFTER T/O, THE FLAPS AND CONF LIGHT ILLUM WITH ASSOCIATED WARNING. STATUS MSG NOSE A/G DISAGREE STATUS MSG APPEARED. A/C WAS A ATB DUE TO STATUS MSG, NOSE A/G DISAGREE. REPLACED S266 NOSE GEAR COMPRESSED SENSOR. 2 L 7 2 4F RT A1NM 1996012600492 19960126 00492 WP 1996 1 26 DLL10960148 1 19960122 A 5312 1504400 CANTED BLKHD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 715DA 193C1092 WHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRAL\CKS IN THE TYPICAL MANNE R AT LBL 10, RBL 22.5, RBL 22.5 AND RBL 42.5. THE CRACKS WERE CUT OUT AND REPAIR DOUBLERS WERE INSTALLED PER DL ERA 273 149. 2 L 7 3 4F A23WE 1996012600493 19960126 00493 WP 1996 1 26 DLL10960168 1 19960122 A 5312 1504400113 BULKHEAD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 713DA 193C1089 WHILE PERFORMING THE SI 7-70645-12 FS 1212 CANTED BULKHEAD INSPECTION, CRACKS WERE FOUND AT FOUR LOCATIONS. REPAIRED PE R DL ERA 273100 RA. 2 L 7 3 4F A23WE 1996012600494 19960126 00494 WP 1996 1 26 DLL15960151 1 19960122 A 3232 ACTUATOR LKHEED 1011 10113853 5265020 WP RT MLG FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 753DA 193W1189 ON APPROACH INTO ATL, WHEN THE GEAR WAS EXTENDED THE ACFT LOST C-SYST HYD PRESS. ON INSPECTION FOUND RT MLG RETRACT ACT UATOR LOWER END BLOWN OUT AND THE GEAR DOOR WAS TORN OUT AT THE DOOR ACTUATOR ATTACH STRUCTURE. REPLACED DOOR AND ACTUA TOR. 2 L 7 3 4F A23WE 1996012600495 19960126 00495 WP 1996 1 26 DLL17960163 1 19960122 A 5711 1605415101 SPAR CAP LKHEED 1011 10113853 5265020 WP WS 315/329 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 CRACKS WERE DISCOVERED EMANATING FROM TWO EXISTING FASTENER HOLES AT IWS 329 AND IWS 315. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP AND UPPER WING SKIN. THE SUBJECT HOLES WERE OVERSIZED TO REMOVE THE CRACKS IN THE DAMAGED MEMBERS O NLY. REPAIRS ACCOMPLISHED PER DL ERA 273032AD RB. 2 L 7 3 4F A23WE 1996012600496 19960126 00496 WP 1996 1 26 DLL17960164 1 19960122 A 5330 1608990 SKIN LKHEED 1011 10113853 5265020 WP FS 1677/1685 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 THE FUSELAGE SKIN BETWEEN FS 1677 AND FS 1685 WAS BADLY GOUGED/DENTED BELOW THE C3 DOOR FROM S-27 TO S-33. THE REPAIR H AD BEEN PREVIOUSLY REPAIRED ON A TIME LIMITED BASIS. THIS REVISION PROVIDES PERMANENT REPAIR INSTRUCTIONS. ACCOMPLISHE D REPAIRS PER DL ERA 272973 RB. 2 L 7 3 4F A23WE 1996012600497 19960126 00497 NM 1996 1 26 DLM88960165 1 19960122 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM FS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 THE FUSELAGE SKIN IS DENTED AFT OF FS 237, 5 INCHES ABOVE THE L-18L CUSP. THE DENT IS APPROXIMATELY .125 INCH BY 3 INCH BY 2.5 INCH. A TIME LIMITED REPAIR WAS ORIGINALLY INSTALLED. THIS REVISION PROVIDES PERMANENT REPAIR INSTRUCTIONS TO THE REPAIR PER DL ERA 272073 REV B. 2 L 7 2 4F RT A6WE 1996012600498 19960126 00498 NM 1996 1 26 DLM88960166 1 19960122 A 5330 5936003 SKIN DOUG MD88 MD88 3023688 NM FS 636 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 THE FUSELAGE SKIN WAS FOUND WITH EDGE DAMAGE FWD OF THE C2 DOOR. THE DAMAGE WAS TO THE OUTER SKIN ONLY AND AFTER CLEANU P MEASURED APPROX 2 INCH BY 5 INCH. THE PERMANENT REPAIR WILL BE ACCOMPLISHED PER MD88 SRM 53-05 FIG 80 CONFIG 7003. 2 L 7 2 4F RT A6WE 1996012600499 19960126 00499 NM 1996 1 26 DLM88960167 1 19960122 A 5330 5936046 SKIN DOUG MD88 MD88 3023688 NM FS 779-807 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 CORROSION WAS FOUND UNDERNEATH THE FAIRING RUB STRIP BETWEEN FS 779 AND 807. THE CORROSION WAS REMOVED AND BLENDED OUT WITH THE MAXIMUM DEPTH OF DAMAGE .130 OCCURRING AT FS 807. REPAIRED PER DL ERA 273091 RC. 2 L 7 2 4F RT A6WE 1996012600500 19960126 00500 WP 1996 1 26 MWEA96021 1 19960120 A 5312 WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND WEB AT STA 996 AFT PRESSURE BULKHEAD HAD MODERATE CORROSION FROM LONGERON 28L TO 28R AT 6 O'CLO CK POSITION. INSTALLED REPAIR IAW SRM 53-01 FIG 2 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996012600501 19960126 00501 WP 1996 1 26 MWEA96022 1 19960120 A 5312 TEE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND AFT CARGO COMPARTMENT AFT BULKHEAD STA 996 LOWER CENTER SUPPORT TEE ANGLE CORRODED TO EXCESS AT CENTER NUTPLATE LOCATIONS. REMOVED CORROSION AND INSTALLED DOUBLER ANGLE REPAIR IAW SRM 53-01 FIG 2. ACFT RETURNED A/ C TO SERVICE. 2 L 7 2 4F A6WE 1996012600502 19960126 00502 WP 1996 1 26 MWEA96023 1 19960122 A 5320 5917497501 FITTING DOUG DC9 DC932 3022066 WP JACK PAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND AFT JACK PAD SUPPORT FITTING HAS MODERATE CORROSION. MAINTENANCE REPLACED AFT JACK PAD FITTING IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996012600503 19960126 00503 NM 1996 1 26 P5CA9600027 1 19960122 A 5730 SKIN BOEING 747 747122 1384872 NM WS 570-590 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND ONE INCH CRACK ON LOWER FLANGE, MIDPOINT ON LEFT WING LEADING EDGE BETWEEN STA 570 TO 590. REPAIRED CRACK PER SRM 57-40-03. 2 L 7 4 4F A20WE 1996012600504 19960126 00504 NM 1996 1 26 P5CA9600028 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 585/807 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE ABOVE THE CENTER WING SPAR AROUND WS 585.62 AND WS 807. REMOVED CORR OSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600505 19960126 00505 NM 1996 1 26 P5CA9600029 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1084 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE BETWEEN MID AND REAR SPARS AROUND WS 1084. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600506 19960126 00506 NM 1996 1 26 P5CA9600030 1 19960124 A 5330 PANEL BOEING 747 747124 1384874 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT AND PANEL ON LOWER FUSELAGE BS 1000 BETWEEN BL 0 AND RBL 25. REMOVED CORROSI ON IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600507 19960126 00507 NM 1996 1 26 P5CA9600031 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1280-1485 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 1280 TO 1485. REMOVED CORROSION I AW SRM 51-10-01, VERIFIED WITHIN LIMITS OF SRM 57-10-01. 2 L 7 4 4F A20WE 1996012600508 19960126 00508 NM 1996 1 26 P5CA9600032 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATION ON RT WING LEADING EDGE FIBERGLASS PANEL TOP OF WING, NEAR NR 18 AND NR 19 LEADING EDGE. REPAIRED IA W SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600509 19960126 00509 NM 1996 1 26 P5CA9600033 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED TOP PANEL ON RIGHT WING FORWARD OF NR 8 SPOILER. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600510 19960126 00510 NM 1996 1 26 P5CA9600034 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND FIBERGLASS PANEL ON LOWER LEFT WING NEAR NR 3 CANOE CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600511 19960126 00511 NM 1996 1 26 P5CA9600035 1 19960124 A 5532 PANEL BOEING 747 747124 1384874 NM VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEFT SIDE PANEL NR 324AL ON VERTICAL STABILIZER DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600512 19960126 00512 NM 1996 1 26 P5CA9600036 1 19960124 A 5532 SKIN BOEING 747 747124 1384874 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA ON RIGHT STABILIZER UPPER SURFACE AHEAD OF OUTBOARD ELEVATOR AND BEHIND REAR SPAR. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600513 19960126 00513 NM 1996 1 26 P5CA9600037 1 19960124 A 5520 ELEVATOR BOEING 747 747124 1384874 NM LEFT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND INBOARD AFT CORNER OF LEFT HAND INBOARD ELEVATOR CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600514 19960126 00514 NM 1996 1 26 P5CA9600038 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND HOLE ON INBOARD SURFACE OF LOWER FIXED PANEL, RT WING T/E CAVITY. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600515 19960126 00515 NM 1996 1 26 P5CA9600039 1 19960124 A 5751 PANEL BOEING 747 747124 1384874 NM RT OUTBD AILERON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED PANEL BETWEEN TWO INBOARD BALANCE WEIGHTS OF RT OUTBOARD AILERON. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600516 19960126 00516 NM 1996 1 26 P5CA9600040 1 19960124 A 5754 SKIN BOEING 747 747124 1384874 NM RT LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND TOP EDGE CRACKED ON LEADING EDGE FLAPS 19, 23 AND 25 RT WING. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600517 19960126 00517 NM 1996 1 26 P5CA9600041 1 19960124 A 5754 PANEL BOEING 747 747124 1384874 NM LT LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600518 19960126 00518 NM 1996 1 26 P5CA9600042 1 19960124 A 5754 FLAP BOEING 747 747124 1384874 NM NR 6/7 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK ON LOWER EDGE OF LEADING EDGE FLAPS 6 AND 7. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600519 19960126 00519 NM 1996 1 26 P5CA9600043 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 807 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA OVER UPPER WING LEADING EDGE SURFACE ON RT WING APPROX WS 807. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600520 19960126 00520 NM 1996 1 26 P5CA9600044 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED PANEL ON RT WING UPPER SURFACE NEAR NR 2 SPEED BRAKE. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600521 19960126 00521 NM 1996 1 26 P5CA9600045 1 19960124 A 5753 SKIN BOEING 747 747124 1384874 NM LT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN LOWER EDGE ON INBOARD EDGE, AFT T/E FLAP LEFT WING. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600522 19960126 00522 NM 1996 1 26 P5CA9600046 1 19960124 A 5240 ACCESS DOOR BOEING 747 747124 1384874 NM NLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NOSE LANDING GEAR SERVICE INTERPHONE ACCESS DOOR CRACKED. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600523 19960126 00523 NM 1996 1 26 P5CA9600047 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE, BS 860 BETWEEN LBL 40 AND RBL 25. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01. 2 L 7 4 4F A20WE 1996012600524 19960126 00524 NM 1996 1 26 P5CA9600048 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AND CRACKED AIR LOCKS ON FAIRING SUPPORT, LOWER FUSELAGE AT BS 900 BETWEEN BL 0 AND LBL 50. REM OVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01. INSTALLED NEW AIR LOCKS IAW SRM 57-30-02. 2 L 7 4 4F A20WE 1996012600525 19960126 00525 NM 1996 1 26 P5CA9600049 1 19960124 A 5330 PANEL BOEING 747 747124 1384874 NM BS 760-780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AROUND FASTENERS ON LAV SERVICE PANEL, LOWER FUSELAGE BETWEEN BS 760 TO 780. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. INSTALLED NEW FASTENERS/RIVETS. 2 L 7 4 4F A20WE 1996012600526 19960126 00526 NM 1996 1 26 P5CA9600050 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE AT BS 840 RIGHT SIDE NEAR STR 37. REMOVED CORROSION IAW SRM 5 1-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600527 19960126 00527 NM 1996 1 26 P5CA9600051 1 19960124 A 5411 FRAME BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RIGHT SIDE FORWARD CORNER ON SLOT SEAL INST FRAME CRACKED. CRACK REMOVED, PATCH FABRICATED FROM 301 1/2 HARD STAI NLESS STEEL AND INSTALLED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600528 19960126 00528 NM 1996 1 26 P5CA9600052 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RT INTERIOR SKIN LOWER EDGE CHAFED ON NR 2 PYLON, NS 222. PATCHED AND RIVETED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600529 19960126 00529 NM 1996 1 26 P5CA9600053 1 19960124 A 5411 FRAME BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED FRAME AND IMPROPERLY INSTALLED REPAIR DOUBLER ON LEFT HAND SIDE SKIN UPPER MOST OVAL HOLE. OLD REPAIR REM OVED, NEW DOUBLER MANUFACTURED FROM STAINLESS STEEL AND INSTALLED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600530 19960126 00530 NM 1996 1 26 P5CA9600054 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEFT HAND SIDE SKIN NS 180 LOWER CORNER CRACKED ON INTERIOR SIDE. NEW STRAP FIRE SHIELD MANUFACTURED AND INSTALLE D IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600531 19960126 00531 NM 1996 1 26 P5CA9600055 1 19960124 A 5400 STRAP BOEING 747 747124 1384874 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED STRAP ON BOTH SIDES OF NR 3 SKIRT FORWARD EDGE. REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600532 19960126 00532 NM 1996 1 26 P5CA9600056 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN SKIN FRONT SPAR NS 128.5 AT NR 4 PYLON. REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600533 19960126 00533 NM 1996 1 26 P5CA9600057 1 19960124 A 5411 RIB BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN NR 4 PYLON INTERIOR CAVITY RIB NS 163. DEFECTIVE AREA REMOVED AND REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600534 19960126 00534 NE 1996 1 26 P5CA9600058 2 19960124 A 7530 65B975171 VANE BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 4 ENG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662591 FOUND CRACK ON NR 4 ENGINE CASCADE VANE. CRACK TREATED IAW SRM 51-10-02. 2 L 7 4 4F 4 F A20WE E20EA 1996012600535 19960126 00535 NM 1996 1 26 P5CA9600059 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON SKIN ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION AT ACCESS TO DRY BAY, BS 1000 APPROX RBL 98. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600536 19960126 00536 NM 1996 1 26 P5CA9600060 1 19960124 A 5330 SKIN BOEING 747 747124 1384874 NM BS 2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AND SKIN SWELLING ON LOWER FUSELAGE NEAR BS 2200 STR 33. REMOVED CORROSION IAW SRM 51-10-01, FO UND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600537 19960126 00537 NM 1996 1 26 P5CA9600061 1 19960124 A 5730 SPAR CHORD BOEING 747 747124 1384874 NM WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FRONT SPAR UPPER CHORD IN WING CENTER SECTION DRY BAY BS 1000 BETWEEN LBL TO RBL 120. REMOVE D CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600538 19960126 00538 NM 1996 1 26 P5CA9600062 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON CEILING SKIN OF WING CENTER SECTION DRY BAY, BETWEEN FRONT SPAR AND S-28C BETWEEN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600539 19960126 00539 NM 1996 1 26 P5CA9600063 1 19960124 A 5713 STRINGER BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON HORIZONTAL STRINGERS IN CEILING OF WING CENTER SECTION DRY BAY, BETWEEN S-23C AND S-29C BETWE EN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600540 19960126 00540 NM 1996 1 26 P5CA9600064 1 19960124 A 5711 SPAR CHORD BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AROUND RIVET ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 57. REMOV ED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600541 19960126 00541 NM 1996 1 26 P5CA9600065 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON SKIN ABOVE LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 33. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-1. 2 L 7 4 4F A20WE 1996012600542 19960126 00542 NM 1996 1 26 P5CA9600066 1 19960124 A 7110 BRACKET BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 663042 FOUND SKIN SEPARATION WITH SMALL CRACK IN ENGINE FAN COWL TOP BRACKED AFT MOUNT FITTING GROOVE ON NR 2 ENGINE. INSTALLE D NEW SKIN IAW SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 1996012600543 19960126 00543 NM 1996 1 26 P5CA9600067 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662591 FOUND UPPER EDGE CHAFED ON 4R ENGINE SIDE COWL. FABRICATED STRAP AND REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F 4 F A20WE E20EA 1996012600544 19960126 00544 NM 1996 1 26 P5CA9600068 1 19960124 A 5720 BRACKET BOEING 747 747124 1384874 NM LT WING GEAR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED BRACKET IN LT WLG DOOR CUTOUT ON LG SUPPORT BEAM. FABRICATED AND INSTALLED NEW BRACKED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600545 19960126 00545 NM 1996 1 26 P5CA9600069 1 19960124 A 5720 BEAM BOEING 747 747124 1384874 NM LT WING GEAR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LT WING L/G BEAM AFT SIDE STA 1350. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600546 19960126 00546 NM 1996 1 26 P5CA9600070 1 19960124 A 5720 BEAM BOEING 747 747124 1384874 NM LT WING GEAR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON UPPER CHORD OF LT WING L/G BEAM STA 1350. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN L IMITS OF SRM 53-30-01. 2 L 7 4 4F A20WE 1996012600547 19960126 00547 NM 1996 1 26 P5CA9600071 1 19960124 A 5512 PANEL BOEING 747 747124 1384874 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RT STABILIZER PANELS 344HB, 344QB, 344JB DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600548 19960126 00548 NM 1996 1 26 P5CA9600072 1 19960124 A 5350 FAIRING BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS AND HOLES ON FUSELAGE WING BODY FAIRINGS, BS 1475 TO 1540. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600549 19960126 00549 NM 1996 1 26 P5CA9600073 1 19960124 A 5350 FAIRINGS BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS AND HOLES LT UPPER FUSELAGE AT OVERWING FAIRING, BS 1475 TO 1540. 2 L 7 4 4F A20WE 1996012600550 19960126 00550 NM 1996 1 26 P5CA9600074 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 695757 FOUND LOWER AFT CORNER OF NR 3 LT FAN COWL CRACKED, NR 3 RT FAN COWL CRACKED AT OLD REPAIR. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F 4 F A20WE E20EA 1996012600551 19960126 00551 NM 1996 1 26 P5CA9600075 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662320 FOUND CRACK IN OLD REPAIR OF NR 1 RT FAN COWL. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F 4 F A20WE E20EA 1996012600552 19960126 00552 NM 1996 1 26 P5CA9600076 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS ON LEFT WING UPPER SKIN AT T/E BETWEEN SPOILER NR 4 AND INBOARD AILERON AND ON TRIANGLE PANEL IN BOARD TO GATE FITTING. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600553 19960126 00553 NM 1996 1 26 P5CA9600077 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS ON LEFT WING L/E UPPER SKIN BEHIND INBOARD SIDE OF L/E FLAP NR 8 AND NR 10. REPAIRED SAME IAW S RM 51-40-09. 2 L 7 4 4F A20WE 1996012600554 19960126 00554 NM 1996 1 26 P5CA9600078 1 19960124 A 5330 SKIN BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA AND HOLES ON RT UPPER FUSELAGE AT OVERWING FAIRINGS, BS 1475 TO 1540. REPAIRED SAME IAW SRM 51-4 0-09. 2 L 7 4 4F A20WE 1996012600555 19960126 00555 NM 1996 1 26 P5CA9600079 1 19960124 A 5280 FAIRING BOEING 747 747124 1384874 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LT WLG STRUT DOOR FAIRING CRACKED ON FWD AND AFT CORNERS. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600556 19960126 00556 NM 1996 1 26 P5CA9600080 1 19960124 A 5720 TIP BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND PANEL DELAMINATED ON RT WING TIP UPPER SURFACE. REPAIRED SAME IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600557 19960126 00557 NM 1996 1 26 P5CA9600081 1 19960124 A 5311 FRAME BOEING 747 747124 1384874 NM BS 2200 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND FRAME LOWER CHORD STA 2200 STR 44 RT SIDE CRACKED. REINFORCED AND REPAIRED SAME IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996012600558 19960126 00558 NM 1996 1 26 P5CA9600082 1 19960124 A 5512 PANEL BOEING 747 747124 1384874 NM HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED PANELS 334DB, 334HB, 334KB ON LEFT HORIZONTAL STABILIZER. REPAIRED SAME IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600559 19960126 00559 NM 1996 1 26 P5CA9600083 1 19960124 A 2710 EYE BOLTS BOEING 747 747124 1384874 NM CCA ASSY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND ALL EYE BOLTS ON PUSH-PULL RODS ON CCA PROGRAMMER CORRODED, RT W/G WHEEL WELL. REMOVED CORROSION IAW SRM 53-10-01 , PAINTED IAW CP 20-40-00. 2 L 7 4 4F A20WE 1996012600560 19960126 00560 NE 1996 1 26 SCNA96005 2 19960119 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE MALFUNCTIONED A SCNA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 15 275AF 22092 DURING CLIMBOUT, THE NUMBER 3 ENGINE FAILED AT FL 210. NO ATTEMPT TO RESTART ENGINE IN FLIGHT WAS MADE. MAINTENANCE EN GINE RUN WAS ACCOMPLISHED PER MM 71-00-30 PAGE 216 AND NO DEFECTS WERE NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996012600561 19960126 00561 NE 1996 1 26 SCNA96006 2 19960120 A 7260 GEARBOX BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE MALFUNCTIONED A SCNA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 275AF 22092 700821 THE NR 3 ENGINE SHUT DOWN ON TAXI OUT. FOUND NR 3 ENGINE TO HAVE A GEARBOX PROBLEM, SUN COUNTRY WILL UPDATE THIS REPORT WHEN SHOP FINDINGS ARE AVAILABLE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600562 19960126 00562 NM 1996 1 26 SCNA96007 1 19960121 A 3260 H1010153 SWITCH BOEING 727 727259 138408J NM NLG FAILED A SCNA K NONE N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. REPLACED THE NOSE GEAR LOCK SWITCH PER MM 32-61-01 PAGE 404. PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSTMENT AND TEST PER MM 32-61-71 PAGE 501. 2 L 7 3 4F A3WE 1996012600563 19960126 00563 NM 1996 1 26 SCNA96008 1 19960121 A 3260 MS2500111 SWITCH BOEING 727 727259 138408J NM NLG LACK OF LUBE A SCNA K NONE N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. JACKED NOSE OF THE AIRCRAFT, SWUNG GEAR , LUBED AND CLEANED THE DOWNLOCK SWITCH. INDICATION CHECKED NORMAL. 2 L 7 3 4F A3WE 1996012600564 19960126 00564 NM 1996 1 26 SCNA96009 1 19960122 A 3260 H1010154 SWITCH BOEING 727 727259 138408J NM NLG CORRODED A SCNA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. FOUND THE LANDING GEAR POSITION SWITCH ( S93) CORRODED AND HANGING UP. REMOVED AND REPLACED SWITCH AND CANNON PLUG (D300). INDICATION CHECKED GOOD PER B727, MM 32-61-71. 2 L 7 3 4F A3WE 1996012600565 19960126 00565 NM 1996 1 26 UPS405284 1 19960109 A 5711 SPAR BOEING 747 747123 1384873 NM WS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 AMS - WHILE IN FOR C-CHECK, CORROSION ON LWR FRONT SPAR CHORD BBSTA 1000 NEAR STA 38L. REMOVED CORROSION PER SRM 57-10- 01 FIG 1, OUT OF LIMIT. REWORKED CORROSION SPOT PER KLM DFX 96-001 BOEING APPROVAL. 2 L 7 4 4F A20WE 1996012600628 19960126 00628 SO 1996 1 26 C2XA96IA001 1 19960104 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT FORWARD UPPER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REP LACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600629 19960126 00629 SO 1996 1 26 C2XA96IA002 1 19960104 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT FORWRAD UPPER SEAT TRACK CORRODED AT FWD END. MAINTENANCE REMOVED AND REPLACED T HE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600630 19960126 00630 SO 1996 1 26 C2XA96IA003 1 19960104 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT FORWARD LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPL ACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600631 19960126 00631 SO 1996 1 26 C2XA96IA004 1 19960104 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT AFT LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600634 19960126 00634 SO 1996 1 26 C2XA96IA007 1 19960105 A 5720 12061341607 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATE D 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1996012600635 19960126 00635 SO 1996 1 26 C2XA96IA008 1 19960105 A 5720 12061341607 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATE D 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1996012600636 19960126 00636 SO 1996 1 26 C2XA96IA009 1 19960105 A 5720 12061341611 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 5TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRFT APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1996012600637 19960126 00637 SO 1996 1 26 C2XA96IA010 1 19960105 A 5720 12061341613 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1996012600638 19960126 00638 SO 1996 1 26 C2XA96IA011 1 19960105 A 5720 12061341615 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1996012600639 19960126 00639 SO 1996 1 26 C2XA96IA012 1 19960105 A 5720 12061341617 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 2ND AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600640 19960126 00640 SO 1996 1 26 C2XA96IA013 1 19960105 A 5720 12017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 16. THE SKIN SUPPORT IS LOCATED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600670 19960126 00670 WP 1996 1 26 IXXA9569 1 19960103 A 3040 CONNECTOR DOUG DC8 DC863F 302198F WP RT WINDSHIELD LOOSE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 784AL 46135 BETWEEN KNGU AND BIKF, AN ELECTRICAL SMELL AND A SMALL AMOUNT OF SMOKE WERE NOTED COMING FROM THE FIRST OFFICERS WINDSHI ELD AREA. IN KNGU, NO SOURCE COULD BE IDENTIFIED FOR THE SMELL. THE WINDSHIELD HEAT WAS PRECAUTIONARILY DEFERRED FOR F URTHER TROUBLESHOOTING. FURTHER TROUBLESHOOTING REVEALED A LOOSE ELECTRICAL CONNECTOR AT THE FIRST OFFICERS WINDOW HEAT SENSOR. THE LOOSE CONNECTION WAS SECURED, AND THE WINDSHIELD HEAT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996012600672 19960126 00672 WP 1996 1 26 IXXA9594 1 19960103 A 3230 UPLATCH CABLE DOUG DC8 DC871 302199A WP LT MLG DOOR OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 824BX 45946 ON TAKEOFF FROM TOL TO ONT, THE CREW REPORTED AN UNSAFE GEAR AND DOOR LIGHT AFTER GEAR RETRACTION. THE AIRCRAFT RETURNE D TO TOL FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR LANDING GEAR SYSTEM INSPECTION AND RI G CHECK. A RIG CHECK OF THE LANDING GEAR MECHANICAL CONTROL SYSTEM WAS ACCOMPLISHED. AN INITIAL GEAR TEST SHOWED THE L EFT MLG DOOR UPLATCH OUT OF RIG. THE LEFT MLG DOOR UPLATCH CABLE AND DOOR ROLLER MECHANISM WERE RIGGED. FINAL LANDING GEAR OPERATIONAL CHECK WAS NORMAL, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996012600744 19960126 00744 EU 1996 1 26 SIMA960021 1 19960102 A 2620 E0052R8B3ASWE CONNECTOR AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE DIRTY A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 424MQ 045 ORD - FLT NR 4100 - ENGINE FIRE BOTTLE DISCHARGE LIGHTS ILLUMINATED DURING TAXI, RETURNED TO GATE. RAI'D CANNON PLUG ON FIRE BOTTLE NR 1 SQUIB ON THE NR 1 ENGINE, OPS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996012600755 19960126 00755 NM 1996 1 26 9601702291 1 19960120 A 2780 RETRACT MECH BOEING 727 727251 138408H NM LE FLAPS OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 01 291US 21379 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT. RESET FLAP TRIM. SECOND TAKE OFF WAS SUCCESSFUL. REPLACED THE LEADING EDGE SWITCHES S311 AND S312 AND RIGGED FOLLOW-UP DRUM. PERFORMED TAKEOFF WARN ING TEST. CHECKED OK. 2 L 7 3 4F A3WE 1996012600756 19960126 00756 NM 1996 1 26 9601712286 1 19960120 A 3260 BULB BOEING 727 727251 138408H NM RT MLG FAILED A NWAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 01 286US 21325 DURING APPROACH INTO MSP, NO GEAR DOWN AND LOCKED ON RIGHT LANDING GEAR. AIRCRAFT MADE A GO-AROUND AND LANDED ON SECOND APPROACH WITHOUT INCIDENT. REPLACED THE LIGHT BULB. CHECKED OK. 2 L 7 3 4F A3WE 1996012600757 19960126 00757 WP 1996 1 26 9601729871 1 19960123 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 780NC 48102 DURING LINE CHECK, FOUND WIRING FOR RIGHT OVERHEAD EMERGENCY EXIT LIGHTS BROKEN. REPAIRED WIRES. OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A6WE 1996012600758 19960126 00758 WP 1996 1 26 9601739866 1 19960124 A 3260 PROX SWITCH DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 775NC 47785 DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE AND THE LIGH T REMAINED ILLUMINATED. AIRCRAFT CONTINUED TO DESTINATION AND ACCOMPLISHED TOWER FLYBY AND LANDED WITHOUT INCIDENT. RE PLACED THE NOSE LANDING GEAR DOWNLOCK PROXIMITY SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600759 19960126 00759 WP 1996 1 26 9601749912 1 19960120 A 3230 UPLOCK HOOK DOUG DC9 DC931 3022065 WP LT MLG OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 962N 47406 DURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR U PLOCK HOOK HINGE BOLT TOO TIGHT. RETORQUED BOLT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600760 19960126 00760 NE 1996 1 26 9601751162 2 19960122 A 7260 GEAR BOX DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE LEAKING A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 162US 46771 86168 AFTER TAKEOFF, THE NR 2 ENGINE OIL DECREASED RAPIDLY. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO MSP. R EPLACED STARTER DRIVE SEAL, BOTH HYDRAULIC PUMP DRIVE SEALS, GEAR BOX, AND BREATHER VALVE. PERFORMED LEAK CHECK. ENGIN E RUN-UP WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996012600761 19960126 00761 NM 1996 1 26 9601762703 1 19960124 A 3350 POWER SUPPLY BOEING 727 727225 1384077 NM DOOR 1L INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8878Z 21451 DURING PRE-FLIGHT, FOUND EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED THE POWER SUPPLY. CHECKED OK. 2 L 7 3 4F A3WE 1996012600762 19960126 00762 NM 1996 1 26 9601775513 1 19960124 A 3350 BPS73 POWER SUPPLY BOEING 757 757251 1384970 NM DOOR 3R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 513US 23201 DURING OVERNIGHT MAINTENANCE, FOUND DOOR 3R EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996012600763 19960126 00763 EU 1996 1 26 9601783223 1 19960122 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 323US 272 DURING APPROACH INTO LAS AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWN LOCKED MESSAGE. CYCLED LANDING GEAR H ANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO DISCREPANC IES. 2 L 7 2 4F RT A28NM 1996012600764 19960126 00764 WP 1996 1 26 9601799601 1 19960123 A 3231 59164605509 SELECTOR VALVE DOUG DC9 DC932 3022066 WP MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 601NW 451 47038 DURING APPROACH INTO DSM, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOOR ACTUATOR WITH NO HELP. REPLACE D THE MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600765 19960126 00765 WP 1996 1 26 9601809154 1 19960122 A 3350 BATTERY DOUG DC9 DC914 3022034 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING PRE-FLIGHT CHECK, COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE EMERGENCY LIGHT BATTERIES. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600766 19960126 00766 NM 1996 1 26 9601816301 1 19960124 A 3350 CONNECTOR BOEING 747 747451 1384940 NM UPPER DECK LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE UPPER DECK FLOOR PATH EMERGENCY LIGHTS AT SEAT ROWS 77 TO 79 WERE FOUND INOPERATIVE. RECONNECT ED LIGHT ASSEMBLY PIN AT SEAT 77. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600767 19960126 00767 NM 1996 1 26 9601826308 1 19960124 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING PRE-FLIGHT CHECK, THE CEILING MOUNTED EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED THE BATTER Y PACK. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600768 19960126 00768 NM 1996 1 26 9601836310 1 19960124 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK (TPE), THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 24R TO 31R WERE FOUND INOPERATIVE. RECONNECT ED LOOSE LIGHT ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600769 19960126 00769 NM 1996 1 26 9601846301 1 19960124 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 25L TO 35L WERE FOUND INOPERATIVE. RECONNECTED LIG HTS ASSEMBLY PIN AT SEAT 25. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600770 19960126 00770 NM 1996 1 26 96FDEA00120 1 19960124 A 2750 163087 TRANSMITTER BOEING 727 72722 1384002 NM TE FLAPS WORN A A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 191FE 19084 AFTER TAKEOFF DURING FLAP RETRACTION. THE OUTBOARD FLAPS BECAME ASYMMETRICAL BETWEEN THE ZERO AND 2 DEGREE INDICATOR, R EPEAT WRITE UP. FOUND RT OUTBOARD TRANSMITTER SECURING COLLAR LOOSE, ADJUSTED TRANSMITTER AND TIGHTENED COLLAR PER MM 2 7-52-12. RAN FLAPS SEVERAL TIMES, OPS CK GOOD. SUGGEST REPLACING RT OUTBOARD FLAP TRANSMITTER AND LOCKING COLLAR DUE T O POSSIBILITY OF COLLAR AND/OR TRANSMITTER SHAFT WORN. 2 L 7 3 4F A3WE 1996012600771 19960126 00771 NE 1996 1 26 96FDEA00121 2 19960124 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 OIL LOSS A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 482FE 21464 AT APPROXIMATELY FLIGHT LEVEL 220, NR 3 LOW OIL PRESSURE/FILTER BYPASS LIGHT FLASHED ON AND OFF. CONFIRMING LOW PRESSUR E ZERO QUANTITY AND RED LINE OIL TEMPERATURE. ENGINE WAS SHUT DOWN, LANDING ACCOMPLISHED DFW. REPLACED NR 3 ENGINE PER WORK CARDS 70T0001, 70T0003, 70T0301, AND C/W FEC-M-0485 ENGINE RUN FORM, ALL OPS AND LEAK CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996012600772 19960126 00772 WP 1996 1 26 96FDEA00122 1 19960124 A 5512 SKIN DOUG DC10 DC1010 3022110 WP LT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CRACK INDICATION ON LT STAB L/E AT UPPER FWD TANG. CRACK EXTENDS ITSELF ACROSS FASTENER HOLE APPROX 1.25 INCH IN LENGTH . CRACK LOCATION IS 5 INCHES I/B OF CLOSURE RIB AREA. REPAIRED CRACK IN REF TO SRM 55-20-00 FIG 9 AND 10. ALSO, PER E A 8-5510-21035A. 2 L 7 3 4F A22WE 1996012600773 19960126 00773 WP 1996 1 26 96FDEA00123 1 19960125 A 3260 ARG7531 TARGET SENSOR DOUG DC10 DC1010F 3022111 WP LT MLG BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 40061 46973 LEFT MAIN GEAR INDICATION ON BOTH PANELS REMAINED RED AFTER RETRACTION. RAN CHECK LIST PROCEDURES WITHOUT SUCCESS. SUB MITTER FEELS THE GEAR IS RETRACTING AND EXTENDING OK, BUT LIGHTS STAY RED. FOUND TARGET SENSOR ON MAIN GEAR DOOR BROKEN . REPLACED TARGET SENSOR PER MM 32-6. 2 L 7 3 4F A22WE 1996012600804 19960126 00804 WP 1996 1 26 ABXA9600071 1 19960123 A 2910 AE2460001J0630 HYD HOSE DOUG DC8 DC861 3021952 WP NR 2 ENGINE FAILED A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 843AX 46017 DURING CRUISE, HYDRAULIC QUANTITY DROPPED TO STANDPIPE LEVEL. FOUND HYDRAULIC PRESSURE LINE BLOWN ON NR 2 ENGINE. REPL ACED PRESSURE LINE AND THE NR 2/NR 3 HYDRAULIC PUMPS IAW DC8 MM, CHAPTER 29-10-12. OPS CHECK AND LEAK CHECK WERE GOOD. 2 L 7 4 4F 4A25 1996012600805 19960126 00805 SO 1996 1 26 COMA9610036 1 19960124 A 3260 PROX SENSOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 268CA 120262 LANDING GEAR DID NOT EXTEND WHEN SELECTED TO DOWN. PLACED THE B-SYSTEM PROXIMITY SENSOR ON DEFERRED MAINTENANCE LIST AN D ACFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996012600806 19960126 00806 SO 1996 1 26 COMA9610037 1 19960123 A 3411 PITOT SYST EMB 120 EMB120RT SO RIGHT CONTAMINATED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 156CA 120156 COPILOT'S AIR SPEED INDICATOR FAILED DURING FLIGHT. CLEANED MOISTURE FROM COPILOT'S PITOT SYSTEM. ACFT RETURNED TO SER VICE. 2 L 7 2 4T RT A31SO 1996012600807 19960126 00807 SO 1996 1 26 COMA9610038 1 19960123 A 7931 SEDLOC4BC OIL PRESS GAUGE EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 462CA 12382 4164 120264 RIGHT ENGINE OIL PRESSURE INDICATES ZERO. REPLACED THE RT ENGINE OIL PRESSURE GAUGE. PART TOTAL CYCLES, 12,823. 2 L 7 2 4T RT A31SO 1996012600808 19960126 00808 EU 1996 1 26 COMA9630022 1 19960124 A 3020 ND00752200 CONTROLLER SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 359CA 3886 226 340A053 RIGHT ENGINE INLET HEAT FAILED. REPLACED THE INLET HEAT CONTROLLER AND LOAD MONITOR. PART TOTAL CYCLES, 4566. 2 L 7 2 4T RT A52EU 1996012600809 19960126 00809 NE 1996 1 26 COMA9630023 2 19960123 A 7320 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTIONED A A COMA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 01 340SF 13783 340A014 367108 LEFT ENGINE SHUT DOWN IN-FLIGHT. TORQUE WAS ERRATIC FOR 3 SECONDS AND THEN SHUT DOWN BY ITSELF. PROBLEM COULD NOT BE D UPLICATED. ENGINE WAS INSPECTED AND NO DEFECTS NOTED. THE ELECTRONIC CONTROL UNIT WAS REPLACED AS A PRECAUTIONARY MEAS URE. PART TOTAL CYCLES, 15,108. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996012600810 19960126 00810 EU 1996 1 26 COMA9630024 1 19960124 A 3060 666000094 BRUSH BLOCK SAAB SF340 SF340A 7850100 EU LT PROP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 361CA 340A056 LEFT PROPELLER DEICE IS INOPERATIVE. REPLACED THE PROPELLER DEICE BRUSH BLOCK ASSY. 2 L 7 2 4T RT A52EU 1996012600811 19960126 00811 EA 1996 1 26 COMA9660021 1 19960119 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 924CA 7026 PASSENGER DOOR OUTER HANDLE WARNING MESSAGE ON EICAS. PROBLEM COULD NOT BE DUPLICATED. OPERATION OF CABIN DOOR AND IND ICATION SYSTEM WERE NORMAL. 2 L 7 2 4F RT A21EA 1996012600812 19960126 00812 NM 1996 1 26 P5CA9600084 1 19960124 A 2820 COUPLING BOEING 747 747122 1384872 NM NR 1 PYLON LOOSE A A P5CA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 WP 23 851FT 19756 ON BLOCK IN, GROUND PERSONNEL SAW TAILPIPE FIRE, NR 1 ENGINE. CREW DISCHARGED FIRE BOTTLE AND MOTORED ENGINE, PUT OUT F IRE. INSPECTED ENGINE AND PYLON FOR DAMAGE, NO STRUCTURES FOUND DAMAGED. FOUND AFT-MOST FUEL FEED LINE COUPLING LOOSE AND FUEL LEAK IN NR 1 PYLON. FOUND SAFETY WIRE BROKEN AT PIG TAIL. REPLACED O-RING AND TIGHTENED COUPLING IAW MM 28-22 -07, OPS AND LEAK CHECK OK. PYLON CONDUCTIVITY INSPECTION OK. 2 L 7 4 4F A20WE 1996012600813 19960126 00813 NM 1996 1 26 P5CA9600085 1 19960123 A 5320 65B108651 SUPPORT BEAM BOEING 747 747122 1384872 NM WS 432.65 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND SUPPORT BEAM CRACKED IN PREVIOUS REPAIR. REPAIRED PER SRM 51-40-03, WEB REPLACED WITH 2024-T3.040 MATERIAL. 2 L 7 4 4F A20WE 1996012600814 19960126 00814 NM 1996 1 26 P5CA9600086 1 19960123 A 5743 SUPPORT FTG BOEING 747 747122 1384872 NM LT WING MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 DURING SSID INSPECTION, NOTED INDICATION OF CRACK ON OUTBOARD WING GEAR SUPPORT FITTING. REMOVED FITTING AND REPAIRED P ER S/B 747-57-2244. BORED TO FIRST OVERSIZE, MAG PART INSP COMPLETED, FITTING REINSTALLED. 2 L 7 4 4F A20WE 1996012600815 19960126 00815 NM 1996 1 26 P5CA9600087 1 19960123 A 5751 65B022332 FITTING BOEING 747 747122 1384872 NM RT INBD AILERON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND BOTH FORWARD AND AFT INBOARD FAIL-SAFE FITTINGS ON RT INBOARD AILERON DUE TO LOOSE RIVETS IN PREVIOUS REPAIR. REM OVED FITTINGS, REPAIRED WEB, REINSTALLED NEW BUSHINGS AND FITTINGS IAW SRM 57-51 02A-001A AND 57-42-14-001. 2 L 7 4 4F A20WE 1996012600816 19960126 00816 SO 1996 1 26 SWIA95710 1 19960118 A 3230 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 LANDING GEAR COULD NOT COME UP. INSTALLED TWO NEW HARNESSES ON RIGHT MAIN GEAR FOR A+ AND B+ INTRANSIT LIGHT. SET GAP TO PROPER SETTING PER MAINTENANCE MANUAL. SWUNG GEAR SEVERAL TURNS AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996012600817 19960126 00817 NM 1996 1 26 UPS205300 1 19960119 A 5320 INTERCOSTAL BOEING 727 72721C 138400M NM BS 682 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 682, RBL 10 - LBL 10, WL 152. REPLACED STRUCTUR E LBL 10 - RBL 10, STA 682, WL 152 I/A/W SRM 51-29-1. 2 L 7 3 4F A3WE 1996020200001 19960202 00001 WP 1996 2 2 9601551225 1 19960103 A 5330 SKIN DOUG DC10 DC1030 3023501 WP RADIO ALT MOUNT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE MOUNTING RINGS FOR ALL 4 RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS (P/N AYB 7022-1; AYB 7053-1, -501) PER EA 12-103877. 2 L 7 3 4F A22WE 1996020200002 19960202 00002 WP 1996 2 2 9601569139 1 19960108 A 5311 FRAME DOUG DC9 DC914 3022034 WP FS 58 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE FS 58 FRAME AT THE 12 O'CLOCK POSITION. REPAIRED FRAME (P/N 9911502-3) PER EA 91-102024. 2 L 7 2 4F A6WE 1996020200003 19960202 00003 WP 1996 2 2 9601579139 1 19960108 A 5320 SUPPORT DOUG DC9 DC914 3022034 WP FS 230-260 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND CORROSION ON THE CENTERLINE FLOOR SUPPORT FS 230 TO 260. REPAIRED SUPPORT (P/N 5910137-7) PER EA 91-102025. 2 L 7 2 4F A6WE 1996020200004 19960202 00004 NM 1996 2 2 9601585506 1 19960109 A 5320 SILL BOEING 757 757251 1384970 NM CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD. REPAIRED CHORD (P/N 146N8522-51), PER EA 55-104364. 2 L 7 2 4F RT A2NM 1996020200005 19960202 00005 WP 1996 2 2 9601599139 1 19960109 A 5240 DOUBLER DOUG DC9 DC914 3022034 WP FWD SERV DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND A CRACK ON THE FORWARD SERVICE DOOR JAMB, LOWER AFT CORNER. REPAIRED DOUBLER (P/N 5911407-33), PE R EA 91-104980. 2 L 7 2 4F A6WE 1996020200006 19960202 00006 WP 1996 2 2 9601601225 1 19960110 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FS 1950-1958 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1950 TO 1958, LONGERON 50L TO 52. REPAIRED SKIN (P/N AGA 7418-1 ) PER EA 12-104396. 2 L 7 3 4F A22WE 1996020200007 19960202 00007 NM 1996 2 2 9601612298 1 19960112 A 5320 ANGLE BOEING 727 727251 138408H NM FS 1263 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND A CRACK IN THE VERTICAL STAIRWELL TORQUE BOX, RIGHT SIDE BS 1263 FRAME CHORD ANGLE. REPAIRED ANGL E PER EA 22-103436. 2 L 7 3 4F A3WE 1996020200008 19960202 00008 EU 1996 2 2 9601623214 1 19960112 A 5313 LONGERON AIRBUS 320 A320211 3930320 EU FS 14300-14834 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 314US 160 DURING 1C1 CHECK, FOUND CORROSION ON FUSELAGE STRINGERS 41R, 43R AND 44 EACH BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER S PER EA 32-105085, -105086 AND -105087. 2 L 7 2 4F RT A28NM 1996020200009 19960202 00009 NM 1996 2 2 9601632298 1 19960115 A 5313 LONGERON BOEING 727 727251 138408H NM FS 1000 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND CORROSION ON STR 29L AT BS 1000. REPAIRED STRINGER (P/N 65-56144-3), PER EA 22-103431. 2 L 7 3 4F A3WE 1996020200010 19960202 00010 NM 1996 2 2 9601642298 1 19960115 A 5210 FRAME BOEING 727 727251 138408H NM PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING P-CHECK, FOUND A CRACK IN THE MAIN CABIN DOOR FRAME AT THE UPPER HINGE RELIEF. REPAIRED DOOR (P/N 50-7945-177), PER EA 22-103435. 2 L 7 3 4F A3WE 1996020200011 19960202 00011 NM 1996 2 2 9601652298 1 19960116 A 5313 LONGERON BOEING 727 727251 138408H NM FS 623 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND CORROSION ON STR 27R AT BS 623. REPAIRED STRINGER (P/N 65-56236), PER EA 22-103428. 2 L 7 3 4F A3WE 1996020200012 19960202 00012 WP 1996 2 2 9601661157 1 19960118 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 157US 46766 DURING L-CHECK, FOUND CORROSION ON THE RBL 7 LONGERON FITTING FROM FS 1509 TO 1521 IN THE CENTER GEAR WHEEL WELL. REPLA CED THE FITTING PER SRM 51-00-00 FIG 2. 2 L 7 3 4F A22WE 1996020200013 19960202 00013 WP 1996 2 2 9601679606 1 19960118 A 5320 CASTING DOUG DC9 DC932 3022066 WP FS 70 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT DIAGONAL WEB ATTACH CASTING IN THE NOSE LANDING GEAR WHEEL WELL FS 70. REPLACED CASTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996020200014 19960202 00014 NM 1996 2 2 9601686719 1 19960119 A 5320 FITTING BOEING 747 747251F 1384898 NM FS 1264-1268 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING P-CHECK, FOUND CORROSION ON THE INNER KEEL BEAM BOX FITTING BS 1264 TO 1268 RBL 4 TO RBL 8. REPLACED FITTING PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996020200015 19960202 00015 WP 1996 2 2 9601699154 1 19960121 A 5755 FITTING DOUG DC9 DC914 3022034 WP SPOILER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND A CRACK IN THE RIGHT WING INBOARD SPOILER CENTER HINGE FITTING. REPLACED SPOILER (P/N 591055-5 16), PER MM 27-61-1 PG 401 TO 406. 2 L 7 2 4F A6WE 1996020200016 19960202 00016 WP 1996 2 2 9601859865 1 19960122 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 674 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 DURING H-CHECK, FOUND A CRACK IN THE FS 674 FLOORBEAM RIGHT SIDE END FITTING. REPLACED FITTING (P/N 3912075-2N), PER SR M 51-30-1 AND -5. 2 L 7 2 4F A6WE 1996020200017 19960202 00017 NM 1996 2 2 9601866730 1 19960122 A 5320 FITTING BOEING 747 7472J9F 1384806 NM FS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING PERIODIC CHECK, FOUND A CRACK IN THE SEAT TRACK SUPPORT FITTING AT BS 400, RBL 11. REPLACED FITTING (P/N 65B1483 1-2). 2 L 7 4 4F RT A20WE 1996020200018 19960202 00018 WP 1996 2 2 9601879871 1 19960123 A 5313 LONGERON DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 21R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996020200019 19960202 00019 WP 1996 2 2 9601889871 1 19960123 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 225 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE LONGERON 25R SPLICE FITTING AT FS 225. REPLACED FITTING PER SRM 51-1 0-3. 2 L 7 2 4F A6WE 1996020200020 19960202 00020 NM 1996 2 2 9601896719 1 19960119 A 5320 SPLICE PLATE BOEING 747 747251F 1384898 NM FS 1920 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1920 FLOORBEAM SPLICE PLATE FROM LBL 98 TO LBL 105. REPLACED PLATE (P/ N 65B17953-2), PER SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1996020200021 19960202 00021 WP 1996 2 2 9601909151 1 19960125 A 7711 EPR INDICATOR DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8909E 45749 666810 NR 2 ENGINE EPR INDICATION WAS LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996020200022 19960202 00022 NM 1996 2 2 9601915503 1 19960125 A 3350 BPS73 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 503US 23192 DURING MAINTENANCE, FOUND AFT RIGHT SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY M736 AND B ATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996020200023 19960202 00023 WP 1996 2 2 9601929930 1 19960124 A 3260 BULB DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 89S 47042 YEG - DURING APPROACH, RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. CREW CONFIRMED VISUALL Y THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OU T ON STANDBY AS A PRECAUTION. CLEANED RIGHT MAIN GEAR DOWNLOCK SWITCH CONNECTOR AND RELAMPED INDICATOR LIGHTS. OPERATI ONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200024 19960202 00024 WP 1996 2 2 9601939975 1 19960124 A 3260 DN/UPLOCK SW DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 9339 47382 DURING CLIMBOUT FROM CMH, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEA R UPLOCK AND DOWNLOCK SWITCHES. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200025 19960202 00025 WP 1996 2 2 9601949601 1 19960125 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPP LY AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200026 19960202 00026 WP 1996 2 2 9601959986 1 19960124 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200027 19960202 00027 WP 1996 2 2 9601969917 1 19960124 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN FORWARD CABIN AND AT LEFT FORWARD DOOR EMERGEN CY EXIT. REPLACED BLOWN FUSE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200028 19960202 00028 NM 1996 2 2 96FDEA00124 1 19960125 A 3270 1U1169 ACTUATOR BOEING 727 727227 1384078 NM TAIL SKID FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 485FE 21488 AFTER T/O, THE LANDING GEAR HAD TO BE RECYCLED TO EXTINGUISH THE TAIL SKID LIGHT. DURING THE SECOND ATTEMPT IT TOOK 10 SECONDS FOR THE LIGHT TO GO OUT. REPLACED TAIL SKID ACTUATOR PER MM 32-71-12 AND ADJ PER MM 32-71-01, GROUND CHECKS OK. 2 L 7 3 4F A3WE 1996020200029 19960202 00029 NM 1996 2 2 96FDEA00126 1 19960126 A 3230 SPINDLE/ARM BOEING 727 7272D4 138407U NM LT MLG BROKEN A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 288FE 21850 WHEN MANUALLY CRANKING THE L/GEAR A SNAP WAS HEARD AND THE MECHANICAL POINTER STOPPED MOVING. THE SNAP WAS HEARD BEFORE REACHING THE MECHANICAL STOP, GEAR DID EXTEND BUT NO FURTHER POINTER MOVEMENT WAS VISIBLE. FOUND MANUAL EXTENSION INDI CATOR SPINDLE BROKEN AND FOLLOWER ARM BENT. REPLACED SPINDLE AND ARM AS PER MM 32-34-71. PERFORMED ADJ AND TEST LANDIN G GEAR MANUAL EXTENSION SYSTEM AS PER MM 32-34-81. ALL CHECKED GOOD, OK FOR SERVICE AND REQUIRED ITEM INSPECTION COMPLI ED WITH. 2 L 7 3 4F A3WE 1996020200030 19960202 00030 NM 1996 2 2 96FDEA00127 1 19960122 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO 44 WL 160 IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996020200031 19960202 00031 NM 1996 2 2 96FDEA00128 1 19960126 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 14 9 IAW FEDEX SRM 53-10-2 AND 53-10-3. 2 L 7 3 4F RT A3WE 1996020200032 19960202 00032 NM 1996 2 2 96FDEA00129 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 480-560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 498 AND 503 BETWEEN STR 26 TO 27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITH LIMITS EX CLUDING TWO AREAS. ONE AT STA 500 RBL 14 AND ONE AT STA 490 RBL 22 PER FEDEX SRM 53-30-1. REPAIRED BOTH AREAS PER FEDE X SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996020200033 19960202 00033 NM 1996 2 2 96FDEA00130 1 19960125 A 5530 STRINGER BOEING 727 727233 138408A NM VERT FIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 VERTICAL FIN STA 110, STR 8L IS CRACKED, BAY NR 6. REPAIRED CRACKED STRINGER PER SRM 55-30-4. 2 L 7 3 4F RT A3WE 1996020200034 19960202 00034 NM 1996 2 2 96FDEA00131 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 520 LBL 37 TO 46 WL 160. DENTS IN FRAME AT BS 520 LBL 37 TO 46 WL 160 WERE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996020200035 19960202 00035 NM 1996 2 2 96FDEA00132 1 19960126 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-11-01 AND -3), ON LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1130 FROM RBL 50 TO LBL 38 WL 200. REMOV ED CORROSION, FABRICATED REPAIR ANGLE PER EA 7-5310-26949. 2 L 7 3 4F RT A3WE 1996020200036 19960202 00036 NM 1996 2 2 96FDEA00133 1 19960126 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 460 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IA W FEDEX EA 7-5310-26943. 2 L 7 3 4F RT A3WE 1996020200037 19960202 00037 NM 1996 2 2 96FDEA00134 1 19960125 A 5330 SKIN BOEING 727 727233 138408A NM BS 710 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 710 LBL 6 WL 149 FOUND DEEP GOUGE AT FASTENER HOLE ON EXTERIOR SKIN WHILE WORKING NR 0413. REMOVED DAMAGE, FABRICATE D REPAIR PARTS AND INSTALLED PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996020200038 19960202 00038 NM 1996 2 2 96FDEA00135 1 19960126 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 360-368 DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DELAMINATION OF SKIN LAP STRINGER 19L BS 360 TO 368. REMOVED FASTENERS IN SKIN LAP AT STR 19L. UPON REMOVAL OF FASTENE RS FOUND NO FURTHER INDICATIONS OF DELAMINATION. INSTALLED NEW STR TIE AND INSTALLED STR 19 SPLICE. ALL WORK DONE IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200039 19960202 00039 NM 1996 2 2 96FDEA00136 1 19960126 A 5530 65678961 FITTING BOEING 727 72722 1384002 NM VERT FIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FIT TING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907. 2 L 7 3 4F A3WE 1996020200040 19960202 00040 NM 1996 2 2 96FDEA00137 1 19960126 A 5320 69239022 FITTING BOEING 727 72722 1384002 NM BS 360 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON STR TO FRAME TIE AT BS 360 STR 20L. REMOVED AND REPLACED STR TIE AT BS 360 20L, DUE TO CORROSION OUT OF LI MITS. 2 L 7 3 4F A3WE 1996020200041 19960202 00041 NM 1996 2 2 96UAL900060 1 19960124 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MID LAV INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 EMERGENCY EVACUATION LIGHTING AT FORWARD MID LAVATORY AREA INOP. REPLACED EMERGENCY EVACUATION LIGHTING STRIP AT MID LA VATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200042 19960202 00042 NE 1996 2 2 96UAL900061 2 19960124 A 7250 2810194 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE LEAKING A UALA D RETURN TO BLOCK K FLUID LOSS IN INSP/MAINT 1 WP 29 512UA 24809 FUEL LEAK ON NR 2 ENGINE COMING FROM CORE ACCESSORY DRAIN DURING ENGINE OPERATION. NO FUEL LEAK AFTER SHUTDOWN. *S/D* REPLACED THE LPT CASE COOLING VALVE AND THE HPT CASE COOLING VALVE, CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200043 19960202 00043 NM 1996 2 2 96UAL900062 1 19960124 A 2760 PCA TRANSFORMER GM69375600 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 4 SPOILER MALFUNCTIONED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 542UA 25276 SPOILER HANDLE GOES TO FULL EXTEND AS SOON AS HANDLE IS ARMED. SUPPLEMENTAL DATA UPDATE: NR 3 FAULT ON THE SPOILER CON TROL MODULE. REPLACED NR 4 SPOILER PCA TRANSFORMER (RVDT). CLEARED FAULT, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200044 19960202 00044 NM 1996 2 2 96UAL900063 1 19960125 A 2131 PRESS CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7461U 21915 AT 31,000 FT CABIN ALT OBSERVED AT 9,000 FT SWITCHED TO STANDBY AND CABIN CONTINUED TO CLIMB. WENT TO MANUAL AND FLIGHT RETURNED TO DEN. MAINTENANCE REPLACED PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 1996020200045 19960202 00045 NM 1996 2 2 96UAL900064 1 19960125 A 2420 IDG CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE SHORTED A UALA O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC DE DESCENT 1 WP 29 605UA 21866 DESCENDING THROUGH 18,000 FEET, LOST RIGHT MAIN AC BUS, GENERATOR WOULD NOT RESET. BUS REMAINED OFF FOR REMAINDER OF FL IGHT. APU GENERATOR WOULD NOT POWER BUS. PASSENGERS REPORTED SPARKS FROM RIGHT ENGINE WHEN LIGHTS WENT OUT. A SHORTED IDG FEEDER CABLE ON THE RIGHT ENGINE CAUSED THE RIGHT MAIN AC BUS TO SHORT THE CIRCUIT BREAKER. THE FEEDER CABLE WAS R EPAIRED AND REPOSITIONED TO PREVENT FURTHER CHAFING. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200046 19960202 00046 NM 1996 2 2 96UAL900065 1 19960125 A 3232 S273N1016 ACTUATOR DOWTY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG WORN A UALA O OTHER J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 29 534UA 25129 EICAS LANDING GEAR DISAGREE INDICATION. LANDING GEAR DOORS AND LANDING GEAR LIGHTS ON SIMULTANEOUSLY. CONDITION OCCURR ED AFTER TAKEOFF WITH GEAR HANDLE UP. VIBRATION ACCOMPANIED OCCURRENCE. APPROXIMATELY 45 SECONDS LATER ABNORMALITIES C LEARED. SUPPLEMENTAL DATA UPDATE: NOSE LANDING GEAR DOOR ACTUATOR RETRACTION CYCLE WAS NOT OPERATING NORMALLY WHICH CA USED THE EICAS MESSAGE. REPLACED NOSE GEAR DOOR ACTUATOR. REMOVED ACTUATOR WAS FOUND TO HAVE WORN SEALS. ACTUATOR WAS OVERHAULED, TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200047 19960202 00047 WP 1996 2 2 MWEA96024 1 19960124 A 2120 AIR DISTR DOUG DC9 DC932 3022066 WP CABIN ODOR A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 502ME 48132 F/A REPORTS, AN ELECTRICAL SMELL NEAR THE EMERGENCY EXIT ROWS. NO SMOKE REPORTED AND IT DISAPPEARED AFTER 10 MIN. LOWE RED PSU DOORS AT EMERGENCY EXIT ROWS, NO DEFECTS NOTED AND COULD NOT DUPLICATE. RETURNED A/C TO FLIGHT AND NO FURTHER D ISCREPANCIES ON THIS OR SUBSEQUENT FLIGHTS. 2 L 7 2 4F A6WE 1996020200048 19960202 00048 NM 1996 2 2 P5CA9600088 1 19960123 A 5320 CHORD BOEING 747 747122 1384872 NM BS 1351 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEVEL 1 CORROSION AT STATION 1350 PRESSURE DECK TOP CHORD. CORROSION REMOVED, FOUND WITHIN LIMITS IAW SRM 53-10-0 1. 2 L 7 4 4F A20WE 1996020200049 19960202 00049 NM 1996 2 2 UPS205316 1 19960126 A 3260 INDICATION SYST BOEING 727 727247 138408F NM LANDING GEAR MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 208UP 21701 CREW REPORTED, ON GEAR RETRACTION RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR, NORMAL DOOR INDICATION EXTENSI ON AND RETRACTION. THREE GROUND LIGHTS ON EXTENSION AND NO RED LIGHT ON RETRACTION. RED NOSE LIGHT CAME BACK ON AND FL UCTUATED IN INTENSITY. OCCASIONALLY GROUND NOSE LIGHT CAME ON DIM AND WENT OUT WHILE RED LIGHT STAYED ON. 2 L 7 3 4F A3WE 1996020200050 19960202 00050 WP 1996 2 2 UPS805315 1 19960125 A 3230 TRIGGER DOUG DC8 DC871F 302199D WP NLG NOT LOCKED A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 798UP 45895 CLIMBING THROUGH 25K AT 340IAS, NOSE GEAR DOOR POSSIBLY FELL OPEN, CONFIRMED BY LOUD COCKPIT NOISE AND VIBRATION. IMMED IATELY DECLARED AN EMERGENCY AND RAN GEAR DOOR UNLOCKED CHECKLIST IN THE QRH. RECTIFIED THE PROBLEM. NOSE GEAR LINK RE LEASE TRIGGER WAS NOT FULLY LOCKED. 2 L 7 4 4F RT 4A25 1996020200051 19960202 00051 WP 1996 2 2 UPS805317 1 19960126 A 3260 DNLOCK SWITCH DOUG DC8 DC871F 302199D WP NLG FAILED A IPXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 703UP 45939 CREW REPORTED, NOSE LANDING GEAR DID NOT GIVE A GROUND INDICATION. COMPLETED CHECKLIST DID FLYBY AND DECLARED EMERGENCY . LANDED AFTER MAINTENANCE AND TOWER VISUALLY CHECKED GEAR DOWN. 2 L 7 4 4F RT 4A25 1996020200062 19960202 00062 CE 1996 2 2 96ZZZX397 1 19960105 A 3213 161500L STRUT LEAR 24 24 5170302 CE LT MLG GROOVE FAILED A VLLA K NONE O OTHER IN INSP/MAINT 1 GL 05 710TV 8381 4863 78020 24159 LEFT LANDING GEAR STRUT SNAP-RING GROOVE FAILED. SUSPECT CAUSE - EXTREME ROUGHNESS ON RUNWAY. 2 L 7 2 4J A10CE 1996020200087 19960202 00087 NE 1996 2 2 96ZZZX454 2 19960104 A 7314 706800 FUEL PUMP BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE MALFUNCTIONED A TWAA O OTHER O OTHER AP APPROACH 1 CE 05 603TW 22566 STL - FLT 721 - DURING APPROACH, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. COMPLETED APPROACH AND LANDING. F OUND FUEL PUMP, MFG PN 706800, MALFUNCTION. REPLACED ENGINE FUEL PUMP AND ENGINE FUEL CONTROL, MFG PN 773333-21. ENGIN E OPERATION THEN CHECKED NORMAL. CHECK C-1C - 12-28-95 - LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200088 19960202 00088 NE 1996 2 2 96ZZZX455 2 19960108 A 7310 3035681 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT ENGINE DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 425JS 3037 FLT 4194 - DURING CRUISE, THE FLIGHT CREW WAS ALERTED BY AN AMBER FUEL FILTER BYPASS CAS MESSAGE. EICAS FUEL SYSTEM PAG E INDICATED THE LEFT ENGINE HP FUEL FILTER IMPENDING BYPASS INDICATION. AIRCRAFT RETURNED TO PIT, LANDED WITHOUT FURTHE R INCIDENT. PIT MAINTENANCE REMOVED AND REPLACED LEFT ENGINE HP FUEL PUMP FILTER IAW MM 73-10-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996020200089 19960202 00089 EU 1996 2 2 96ZZZX456 1 19960106 A 3260 622800200 UPLOCK SWITCH ROTOL BAG JETSTM JETSTM3101 1500215 EU LT/RT MLG DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 854JS 735 FLT 4178 - AFTER LANDING GEAR WAS RETRACTED, THE LEFT MLG INTRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR SEVERA L TIMES WITH NO SUCCESS. AIRCRAFT RETURNED TO FIELD, AND LANDED WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE CLEA NED THE LEFT AND RIGHT UPLOCK MICROSWITCHES IAW STD MAINTENANCE PRACTICES. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A21EU 1996020200090 19960202 00090 NM 1996 2 2 96ZZZX457 1 19960110 A 3250 2304000001 SERVO VALVE MESSIER DORNER DO32 DO328100 2996000 NM NLG STEERING DEFECTIVE A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 3033 FLT 4194 - WHILE TAXIING ON THE RUNWAY IN PREPARATION FOR TAKEOFF, CREW WAS ALERTED BY A NOSE WHEEL STEERING FAIL CAS ME SSAGE. DAY MAINTENANCE UNABLE TO CORRECT DISCREPANCY IN CMH. AIRCRAFT WAS FERRIED FROM CMH TO CAK. CAK MAINTENANCE RE MOVED AND REPLACED NOSE WHEEL STEERING SERVO VALVE IAW MM 32-51-00. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996020200091 19960202 00091 NE 1996 2 2 96ZZZX458 2 19960112 A 7210 PT61916B GEARBOX FOKKER F27 F27MK500 4990629 EU RROYCE DART DART5327R 54509 NE LT ENGINE FAILED A MTNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 722FE 1202 10472 13307 RIC - ON CLIMB-OUT, THE LEFT ENGINE INDICATED A POWER LOSS (RPM DROPPED TO 13,800 AT MAX). THE CREW DECLARED AN EMERGEN CY AND RETURNED TO RIC. DURING DESCENT, LEFT GENERATOR LIGHT, LEFT ALTERNATOR LIGHT, AND LEFT GEARBOX OIL PRESSURE LIGH T CAME ON. ALL TEMPERATURES WERE NORMAL. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. AFTER TROUBLESHOOTING, MECHA NIC FOUND INTERNAL FAILURE IN THE LEFT GEARBOX. 2 H 7 2 4T 4 T A817 E297 1996020200092 19960202 00092 CE 1996 2 2 96ZZZX459 1 19960102 A 7120 12991003279 TRUSS BEECH 1900 1900C 1154161 CE RT ENGINE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 130UE 1678 UC130 SPI - DURING VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-12-18, A CRACK WAS FOUND. THE RIGHT ENGINE TRUSS WAS R EPLACED WITH SERVICEABLE. 2 L 7 2 4T RT A24CE 1996020200094 19960202 00094 SW 1996 2 2 MALA964791 1 19960101 A 2460 JGZA RELAY SWRNGN SA227 SA227AC 8780603 SW RT CONSOLE SHORTED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 433MA AC714 MSP - FLT 3230 - INBOUND, CREW NOTED ALL OF THE RT ENGINE INSTRUMENTS WERE INOPERATIVE. THE AIRCRAFT CONTINUED TO MSP A ND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT BUS TIE RELAY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200095 19960202 00095 NE 1996 2 2 MALA964794 2 19960102 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE FAILED A MALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 15 865MA 364 BEH - FLT 3488 - AFTER TAKEOFF, THE NR 2 ENGINE BEGAN TO SURGE IN RPM AND TORQUE. THE CREW REDUCED POWER, BUT THE ENGIN E CONTINUED TO SURGE. THE CREW ELECTED TO PERFORM A PRECAUTIONARY SHUT DOWN AND RETURNED TO BEH WITHOUT INCIDENT. THE PROBLEM COULD NOT BE DUPLICATED IN BEH, SO THE AIRCRAFT WAS FERRIED TO DTW FOR FURTHER TROUBLESHOOTING. MAINTENANCE PER SONNEL REPLACED THE HMU. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1996020200096 19960202 00096 SW 1996 2 2 MALA964795 1 19960107 A 5400 2735112 ATTACH ANGLE SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT INBOARD LOWER WING TO NACELLE ATTA CH ANGLE. THEY STOP DRILLED A CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) 1 L 7 2 4T A8SW 1996020200097 19960202 00097 SW 1996 2 2 MALA964796 1 19960107 A 5753 2731141001 DOUBLER SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED EXCESSIVE WEAR ON THE LEFT FLAP WALKING BEAM ROLLER DOU BLER. THEY REPLACED THE DOUBLER AND INSTALLED A REINFORCEMENT IAW FAC SRM 57-90-10. (X) 1 L 7 2 4T A8SW 1996020200098 19960202 00098 SW 1996 2 2 MALA964797 1 19960107 A 5753 2731141001 DOUBLER SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED EXCESSIVE WEAR ON THE RIGHT FLAP WALKING BEAM ROLLER DO UBLER. THEY REPLACED THE DOUBLER AND INSTALLED A REINFORCEMENT IAW FAC SRM 57-90-10. (X) 1 L 7 2 4T A8SW 1996020200099 19960202 00099 SW 1996 2 2 MALA964798 1 19960107 A 2730 2744026007 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RT HORIZ STAB CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED CORROSION IN THE RIGHT ELEVATOR TORQUE TUBE. THEY REPL ACED THE TORQUE TUBE IAW WITH FAC SRM 51-00-00. (X) 1 L 7 2 4T A8SW 1996020200100 19960202 00100 SW 1996 2 2 MALA964799 1 19960107 A 2730 2744026007 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW LT HORIZ STAB CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEUDLED INSPECTION, MAINTENANCE PERSONNEL NOTED CORROSION IN THE LT ELEVATOR TORQUE TUBE. THEY REPLACE D THE TORQUE TUBE IAW FAC SRM 51-00-00. (X) 1 L 7 2 4T A8SW 1996020200101 19960202 00101 SW 1996 2 2 MALA964800 1 19960107 A 5400 2735112 ANGLE SWRNGN SA227 SA227AC 8780603 SW LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LT LOWER INBOARD WING TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) 1 L 7 2 4T A8SW 1996020200102 19960202 00102 SW 1996 2 2 MALA964801 1 19960106 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 445MA AC687 BRD - FLT 3236 - AFTER TAKEOFF, THE NLG RED INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR RETRACTION. THE AIRCRAFT CONTI NUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT NLG UPLOCK SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200103 19960202 00103 SW 1996 2 2 MALA964802 1 19960105 A 3230 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA O OTHER O OTHER CL CLIMB 1 GL 15 445MA AC687 GFK - FLT 3253 - AFTER DEPARTURE, THE NOSE GEAR WOULD CYCLE IN THE GEAR WELL AFTER RETRACTION. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THE CYCLING STOPPED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONN EL ADJUSTED THE RIGGING OF THE NLG POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200104 19960202 00104 NM 1996 2 2 MALA964803 1 19960105 A 3350 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 MSP - FLT 3231 - DURING PRE-FLIGHT INSPECTION, CREW NOTED THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANC E PERSONNEL REPLACED ALL SIX BATTERY PACKS, PN 61-078-1 AND DASH 9. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996020200105 19960202 00105 NM 1996 2 2 MALA964804 1 19960106 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 822MA 326 DTW - FLT 3120 - DURING A POST-FLIGHT INSPECTION, CREW NOTED THE CABIN EMERGENCY LIGHTS WOULD SHUT OFF AFTER ONLY FIVE S ECONDS OF OPERATION. MAINTENANCE PERSONNEL REPLACED THREE EMERGENCY LIGHT BATTERY PACKS. ALL SYSTEMS OPERATED SATISFAC TORILY. (X) 2 H 7 2 4T RT A13NM 1996020200106 19960202 00106 SW 1996 2 2 MALA964805 1 19960105 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 26906 AC654B BRD - FLT 3462 - AFTER TAKEOFF, THE RED NOSE GEAR INTRANSIT LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. THE AIRCRA FT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT NOSE LANDING GEAR UPLOCK SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200107 19960202 00107 NM 1996 2 2 MALA964806 1 19960105 A 3260 82410315001 SOCKET ASSY DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 827MA 331 DTW - FLT 3432 - DURING A PRE-FLIGHT INSPECTION, CREW NOTED THE NOSE GEAR AND LT MAIN GEAR ALTERNATE DOWN AND LOCKED LIG HTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE MAIN GEAR EMERGENCY DOWNLOCK INDICATOR SOCKET AND REPAIRED A B ROKEN WIRE FOR THE NOSE GEAR LIGHT. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996020200108 19960202 00108 SW 1996 2 2 MALA964807 1 19960104 A 3233 2751016003 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW RT MLG MALFUNCTION A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 426MA AC645 BEH - FLT 3485 - DURING APPROACH, THE RT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE CREW RECYCLED THE GEAR AND THE LIGHT ILLUMINATED NORMALLY. THE AIRCRAFT CONTINUED TO BEH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT MLG ACTUATOR, PN 27-51016-003. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200113 19960202 00113 WP 1996 2 2 9601979941 1 19960108 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 69-91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STRINGER 15 BETWEEN XRS 69 TO 91. REPAIRED STRINGER PER EA 99-104039. 2 L 7 2 4F A6WE 1996020200114 19960202 00114 WP 1996 2 2 9601989941 1 19960108 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON RIGHT WING STRINGERS 14 AND 15, XRS 58 TO 137 AND ON 20 AND 21, XRS 69 TO 91. REPAIRED STRINGERS PER EA 99-104038. 2 L 7 2 4F A6WE 1996020200115 19960202 00115 WP 1996 2 2 9601999941 1 19960109 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND A .75 INCH CRACK IN THE FUSELAGE SKIN AT FS 200, LONGERON 13L. REPAIRED SKIN (P /N 5911406-59) PER EA 99-104036. 2 L 7 2 4F A6WE 1996020200116 19960202 00116 WP 1996 2 2 9602009155 1 19960124 A 5320 FITTING DOUG DC9 DC914 3022034 WP FS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 DURING H-CHECK, FOUND CORROSION IN THE FORWARD SERVICE DOOR JAMB FLOOR TO FRAME SUPPORT FITTING, FS 200. REPLACED FITTI NG PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996020200117 19960202 00117 WP 1996 2 2 9602019962 1 19960125 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 155 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 914RW 47362 DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE LONGERON 11R END FITTING AT FS 155. REPLACED FITTING ANGLES PER SRM 53-05 FIG 100. 2 L 7 2 4F A6WE 1996020200118 19960202 00118 1996 2 2 9602029760 4 19960126 A 3416 2050011RC ALTIMETER DOUG DC9 DC941 302207N WP LT COCKPIT FAILED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 760NW 30723 28147 47288 DURING CLIMB, CAPTAIN'S ALTIMETER OFF FLAG CAME ON. RESET CIRCUIT BREAKER AND ALTIMETER CAME ON MOMENTARILY, THEN OFF F LAG RETURNED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S ALTIMETER AND OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020200119 19960202 00119 WP 1996 2 2 9602039153 1 19960121 A 5350 CLIPS DOUG DC9 DC914 3022034 WP TAILCONE OUT OF ADJUST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8912E 45829 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HAN DLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR RELEASE H ANDLE FROM THE CLIPS. ADJUSTED THE INTERIOR AND EXTERIOR CLIPS. 2 L 7 2 4F A6WE 1996020200120 19960202 00120 WP 1996 2 2 9602049877 1 19960123 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAIL CONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 786NC 48148 DURING EO 5350-01032 TAIL CONE FUNCTION CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HAND LE FROM THE CLIPS. ALSO, FOUND THAT THE TAIL CONE DID NOT DROP FROM THE AIRCRAFT, BUT HUNG UP ON THE UPPER LOCKPINS. R ERIGGED THE TAIL CONE PER MM 53-50-3, PAR 4 AND CITEXT 09-5350-1-0024, CHECKED OK. 2 L 7 2 4F A6WE 1996020200121 19960202 00121 WP 1996 2 2 9602059880 1 19960125 A 7711 PT2 PROBE DOUG DC9 DC951 3022051 WP LT/RT ENGINES ICED UP A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 675MC 47651 EPR INDICATION LOW ON BOTH ENGINES DURING TAKEOFF. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTE NANCE CLEARED ICE DEPOSITS FROM BOTH PT2 PROBES. ENGINE INDICATION RETURNED TO NORMAL ON SUBSEQUENT RUNUP. 2 L 7 2 4F A6WE 1996020200122 19960202 00122 NM 1996 2 2 96FDEA00138 1 19960119 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1072-1090 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 1072 TO 1090 STR 7R DAMAGE TO STRINGER INSIDE U-CHANNEL ABOVE SKIN RIVETS. INSTALLED REPAIR DOUBLER IAW B OEING SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200123 19960202 00123 NM 1996 2 2 96FDEA00139 1 19960119 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 757-759 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 BS 757 TO 759 STR 7L DAMAGE INSIDE STRINGER ABOVE RIVETS THROUGH SKIN. REPLACED STR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200124 19960202 00124 NM 1996 2 2 96FDEA00140 1 19960118 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 882-889 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 882 TO 889 STR 7R DAMAGED TO STR INSIDE U-CHANNEL ABOVE SKIN RIVETS. REMOVE DAMAGED STR 7R FROM BS 872 TO 898, FABRICATED PARTS 1, 2, 3 AND 4. DRILLED AND INSTALLED PER SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996020200125 19960202 00125 NM 1996 2 2 96FDEA00141 1 19960118 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 885-888 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 885 TO 888 STR 7L, DAMAGE TO STRINGER INSIDE U-CHANNEL. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICA TED FILLER, REPAIRED PARTS 1, 2, 3. LOCATED AND DRILLED ALL HOLES, TREATED AND PRIMED ALL PARTS AND INSTALLED PER SRM 5 3-10-3 PAGES 5 TO 8 FIG 3. 2 L 7 3 4F A3WE 1996020200126 19960202 00126 NM 1996 2 2 96UAL900066 1 19960126 A 5210 65331601 SEAL BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE PAX DOOR LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9023U 19061 CREW REPORTS, UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. MAINTENANCE FOUND AIR LEAKING FROM FORWARD AIRSTAIRS DOOR SE AL. STOPPED LEAK BY PUTTING ALUMINUM FILLED EPOXY RESIN UNDERNEATH AIRSTAIRS DOOR SEAL. AIRCRAFT PRESSURIZES NORMALLY. 2 L 7 2 4F 4 F A16WE E2EA 1996020200127 19960202 00127 NM 1996 2 2 96UAL900067 1 19960126 A 2460 26930017 CIRCUIT BREAKER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU E/E COMPT DEFECTIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 338UA 24242 LOST CAPTAIN'S AND FIRST OFFICER'S INSTRUMENTS. RESTORED POWER TO FIRST OFFICER'S INSTRUMENTS BUT NEVER REGAINED CAPTAI N'S INSTRUMENTS. THE NUMBER ONE ELECTRICAL BUS CIRCUIT BREAKER AND THE NUMBER TWO GENERATOR BREAKER AUXILIARY CONTACTS WERE FOUND DEFECTIVE. BOTH PARTS WERE REPLACED AND WIRING CHECKS ACCOMPLISHED AS A PRECAUTIONARY. TWO VERIFICATION FLI GHTS WERE ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 1996020200129 19960202 00129 WP 1996 2 2 ABXA9600072 1 19960104 A 3231 522103 BUSHING DOUG DC9 DC933F 302207A WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR ARTICULATING DOOR LINKAGE WORN. REPLAC ED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200130 19960202 00130 WP 1996 2 2 ABXA9600073 1 19960104 A 3231 3923166501 FITTING DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200131 19960202 00131 WP 1996 2 2 ABXA9600074 1 19960104 A 3231 NB3218600 BUSHING DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGES WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200132 19960202 00132 WP 1996 2 2 ABXA9600075 1 19960111 A 5610 575468827 DOUBLER DOUG DC9 DC932 3022066 WP LT EYEBROW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3; EAAD 56-3956MA, FOUND DOUBLER CRACKED AT UPPER AFT CORNER OF LEFT EYEB ROW WINDOW FRAME. REPLACED DOUBLER IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996020200153 19960202 00153 WP 1996 2 2 ABXA9600096 1 19960111 A 5280 5913433504 HINGE DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR H INGE WORN. REPLACED HINGE IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 1996020200155 19960202 00155 WP 1996 2 2 ABXA9600098 1 19960104 A 5330 591141622 SKIN DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND A 1.4 INCH CRACK IN THE SKIN AT STA 617, AT LONGERON 18R. REPAIRED IAW ABX REA D953-13 873-MR. 2 L 7 2 4F A6WE 1996020200156 19960202 00156 WP 1996 2 2 ABXA9600099 1 19960103 A 5311 9919613502 FRAME DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND FRAME 617 CRACKED BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-13907-MR. 2 L 7 2 4F A6WE 1996020200157 19960202 00157 WP 1996 2 2 ABXA9600100 1 19960105 A 5753 5912168502 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING FORWARD MOVEABLE VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-02. 2 L 7 2 4F A6WE 1996020200158 19960202 00158 WP 1996 2 2 ABXA9600101 1 19960103 A 5753 5910042504 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND RIGHT FLAP CENTER FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-3. 2 L 7 2 4F A6WE 1996020200163 19960202 00163 WP 1996 2 2 ABXA9600106 1 19960125 A 3260 7000010101 SWITCH DOUG DC8 DC863 302198A WP LT MLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 820AX 46155 ON GEAR EXTENSION LEFT MAIN GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE. RECYCLED LANDING GEAR AND DOWNLOCK LIGHT DID NOT IL LUMINATE. DOWNLOCK LIGHT CAME ON DURING LANDING. CLEANED LEFT MAIN GEAR DOWNLOCK SWITCH CANNON PLUG AND REPLACED DOWNL OCK SWITCH. GEAR RETRACTION AND GEAR INDICATION CHECK WAS GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 1996020200164 19960202 00164 WP 1996 2 2 ABXA9600107 1 19960125 A 3231 DOOR DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 818AX 46075 ON GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ALSO, RIGHT GEAR DOOR UNLATCH LIGHT ILLUMINATED. RECYC LED GEAR AND HAD NO CHANGE. ADJUSTED DOOR LATCH ASSEMBLY TO OBTAIN PROPER CLEARANCE AND OPS CHECKED GOOD IAW DC-8 MM CH APTER 32-31-4. 2 L 7 4 4F 4A25 1996020200165 19960202 00165 WP 1996 2 2 ABXA9600108 1 19960126 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 905AX 47147 EMERGENCY BATTERY PACK INTERMITTENT OPERATION. REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1996020200167 19960202 00167 WP 1996 2 2 ARWA9601003 1 19960127 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 288-297 CRACKED A ARWA K NONE O OTHER UK UNKNOWN 1 SO 19 802BN 45909 DURING POST FLIGHT INSPECTION, AN 8.5 FUSELAGE SKIN PUNCTURE WAS NOTED AT FS 288.00 TO 297.00 AT LONGERON 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I/A/W SRM 53-2-1 FIG 7. SEALED AREA I/A/W SRM 51-1-11. 2 L 7 4 4F 4A25 1996020200168 19960202 00168 SO 1996 2 2 COMA9610039 1 19960125 A 6120 711JOMRL731P8 SEAL EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 162CA 120150 RIGHT ENGINE NP FLUCTUATES. REPLACED PROPELLER TRANSFER TUBE SEALS. 2 L 7 2 4T RT A31SO 1996020200169 19960202 00169 SO 1996 2 2 COMA9610040 1 19960125 A 2913 MPEV30082B PUMP HYD EMB 120 EMB120RT SO RIGHT FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 255CA 16470 231 120238 RT ELECTRIC HYDRAULIC PUMP IS INOP. REPLACED THE RT ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1996020200170 19960202 00170 SO 1996 2 2 COMA9610041 1 19960125 A 2752 3203001011 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 164D 256 120164 FLAP ASYMMETRY WARNING AFTER LANDING. REPLACED THE RT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996020200171 19960202 00171 SO 1996 2 2 COMA9610042 1 19960127 A 3260 922AA2YA6P2722 SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 196CA 120196 AFTER LANDING GEAR RETRACTED, A RUMBLING SOUND WAS HEARD AS IF GEAR DOORS WERE OPEN. FOUND LT MLG UPLOCK PROXIMITY SENS OR, SYSTEM-A DEFECTIVE. DEFERRED SYSTEM PER EMB SNL 32-015 AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200172 19960202 00172 SO 1996 2 2 COMA9610043 1 19960128 A 3060 78614423 LEAD WIRE EMB 120 EMB120RT SO LT PROP BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 259CA 120252 LEFT PROPELLER DE-ICE IS INOP. REPLACED BROKEN DE-ICE LEAD WIRE AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200173 19960202 00173 EU 1996 2 2 COMA9630025 1 19960125 A 3620 M2001542 SWITCH 211C119136A SAAB SF340 SF340A 7850100 EU RT BLEED AIR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 357CA 11888 4889 M236 340A044 RT BLEED AIR FAULT CAUTION LIGHT ILLUMINATED DURING CLIMB. REPLACED THE BLEED AIR PRESSURE SWITCH AND THE BLEED AIR OVE RTEMP SWITCH FOR TROUBLESHOOTING. PROBLEM DID NOT DUPLICATE IN MAINTENANCE. 2 L 7 2 4T RT A52EU 1996020200174 19960202 00174 WP 1996 2 2 MWEA96025 1 19960126 A 3350 1001191 PIN DOUG DC9 DC932 3022066 WP FWD GALLEY LOOSE A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 502ME 48132 CREW REPORTS, EMERGENCY FLASHLIGHT RETAINING PIN WILL NOT STAY IN SOCKET. REPLACED FLASHLIGHT ASSEMBLY AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200175 19960202 00175 WP 1996 2 2 MWEA96026 1 19960126 A 5730 SKIN DOUG DC9 DC914 3022034 WP WS 80 LE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LT WING LEADING EDGE DENTED STA XRS 80. INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 2 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200176 19960202 00176 WP 1996 2 2 MWEA96027 1 19960127 A 3350 SOCKET DOUG DC9 DC914 3022034 WP CABIN DIRTY A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 700ME 45696 DURING C-CHECK, SEVERAL OVERHEAD CENTER AISLE EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. CLEANED AND TIGHTENED SO CKET. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200177 19960202 00177 NM 1996 2 2 P5CA9600089 1 19960125 A 7711 613116 PT7 LINE BOEING 747 747122 1384872 NM NR 4 ENGINE BROKEN A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 23 851FT 19756 ON TAKEOFF, LOST NR 1 AND NR 4 EPR INDICATION AND NR 3 AND NR 4 GENERATOR. TAKEOFF WAS ABORTED. REPLACED NR 3 GCU, GRO UND CHECK OK. FOUND NR 4 GCR RACK PLUG LOOSE, SECURED AND GROUND RUN CHECK OK. FOUND NR 4 ENGINE PT7 LOOP LINE BROKEN AT ONE O'CLOCK POSITION. REPLACED LINE, GROUND RUN OK IAW MM 77-11-15. DEFERRED REPAIR OF NR 1 EPR. 2 L 7 4 4F A20WE 1996020200178 19960202 00178 NM 1996 2 2 P5CA9600090 1 19960127 A 2710 INDICATOR BOEING 747 747121 1384871 NM RT AILERON INOPERATIVE A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 830FT 19642 RETURNED TO RAMP DUE TO IMPROPER RT OUTBOARD AILERON INDICATION. FUNCTIONAL CHECK OF ALL CONTROL SURFACES NORMAL, ALL C OCKPIT INDICATIONS NORMAL IAW MM 27-00-00. 2 L 7 4 4F A20WE 1996020200179 19960202 00179 NM 1996 2 2 P5CA9600091 1 19960127 A 3244 TIRE BOEING 747 747122 1384872 NM NR 10 BLOWN A P5CA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 23 854FT 19754 BLEW NR 10 TIRE ON TAKEOFF FROM HONG KONG. RETURNED TO HONG KONG, MADE UNEVENTFUL LANDING. REMOVED AND REPLACED TIRE I AW MM 32-45-01. 2 L 7 4 4F A20WE 1996020200180 19960202 00180 NM 1996 2 2 UPS205319 1 19960124 A 5753 652466858 WEDGE BOEING 727 72721C 138400M NM RT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996020200181 19960202 00181 NM 1996 2 2 UPS205320 1 19960119 A 5753 652163327 MID SPAR BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR AFT SIDE 54 AND 58 O/B OF THE I/B END OF MID SPAR. REPLACED ON NRC 368443. 2 L 7 3 4F A3WE 1996020200182 19960202 00182 NM 1996 2 2 UPS205321 1 19960119 A 5753 652163327 MID SPAR BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR UPPER INTERIOR SURFACE AFT SIDE 49 AND 5 5 I/B OF THE O/B END OF MID SPAR. REPLACED ON NRC 368443. 2 L 7 3 4F A3WE 1996020200183 19960202 00183 NM 1996 2 2 UPS205322 1 19960119 A 2750 652163327 FITTING BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT F ITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443. 2 L 7 3 4F A3WE 1996020200184 19960202 00184 NM 1996 2 2 UPS205323 1 19960119 A 2750 652163327 FITTING BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT F ITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443. 2 L 7 3 4F A3WE 1996020200185 19960202 00185 NM 1996 2 2 UPS205324 1 19960119 A 2711 6521773501 FITTING BOEING 727 72721C 138400M NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON TAB HINGE FITTINGS CORRODED, 3 EA. REMOVED AND REPLACED LT AI LERON TAB FITTINGS IAW SRM 51-30-2 AND MM 27-10-0. 2 L 7 3 4F A3WE 1996020200186 19960202 00186 NM 1996 2 2 UPS205325 1 19960119 A 2710 6524646501 HINGE ARM BOEING 727 72721C 138400M NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE ARM IS CORRODED AROUND BOLT HOLE. REMOVED AND RE PLACED HINGE ARM IAW MM 27-10-01 AND 27-10-0. 2 L 7 3 4F A3WE 1996020200187 19960202 00187 NM 1996 2 2 UPS205326 1 19960123 A 2711 6521773501 HINGE TAB BOEING 727 72721C 138400M NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/ B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0. 2 L 7 3 4F A3WE 1996020200188 19960202 00188 NM 1996 2 2 UPS205327 1 19960123 A 2710 65849505 ROD END BOEING 727 72721C 138400M NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILER ON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00. 2 L 7 3 4F A3WE 1996020200189 19960202 00189 NM 1996 2 2 UPS205328 1 19960122 A 2710 6593155264 HINGE FITTING BOEING 727 72721C 138400M NM RT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND RE PLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-20-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996020200190 19960202 00190 NM 1996 2 2 UPS205329 1 19960123 A 5754 ANGLE BOEING 727 72721C 138400M NM NR 7 SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51 -30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1. 2 L 7 3 4F A3WE 1996020200191 19960202 00191 NM 1996 2 2 UPS205330 1 19960123 A 5754 BONDING JUMPER BOEING 727 72721C 138400M NM NR 6 K-FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00. 2 L 7 3 4F A3WE 1996020200192 19960202 00192 NM 1996 2 2 UPS205331 1 19960123 A 5754 SLAT BOEING 727 72721C 138400M NM NR 5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IA W MM 27-81-11. 2 L 7 3 4F A3WE 1996020200193 19960202 00193 NM 1996 2 2 UPS205332 1 19960123 A 5511 650174313 RIB BOEING 727 72721C 138400M NM HORZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT EN D. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996020200194 19960202 00194 NM 1996 2 2 UPS205333 1 19960125 A 5530 MID SPAR BOEING 727 72721C 138400M NM VERT FIN CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRE D PER UPS EO 727-55-0309. 2 L 7 3 4F A3WE 1996020200195 19960202 00195 NM 1996 2 2 UPS405318 1 19960125 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM BS 1060 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 WHILE IN FOR C-CHECK AMS MAINTENANCE REPORTED, FLOORBEAM UPPER CHORD CORRODED AT BS 1580 LBL 0. REMOVED AND REPLACED FL OORBEAM IAW SRM 51-40-04. 2 L 7 4 4F A20WE 1996020200196 19960202 00196 NM 1996 2 2 UPS405334 1 19960112 A 5314 KEEL BEAM BOEING 747 747123 1384873 NM BS 1242 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 WHILE IN FOR C CHECK AT AMS, MAINTENANCE, FOUND CORROSION ON CENTERLINE KEELBEAM WEB INSIDE BSTA 1242. REPAIRED AS REQU IRED PER SRM 51-10-01, AND KLM DTZ 96-011. 2 L 7 4 4F A20WE 1996020200197 19960202 00197 NM 1996 2 2 UPS405342 1 19960126 A 2560 69B515751 RELEASE HANDLE BOEING 747 747121 1384871 NM ESCAPE SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 MAINTENANCE REPORTED, ESCAPE SLIDE RELEASE HANDLE CLIP BROKEN AND PAWL BROKEN MAKING ESCAPE SLIDE ARMED AND NOT SAFE. R EMOVED AND REPLACED RELEASE HANDLE CLIP AND PAWL. SLIDE SECURED AND OPERATES FROM SAFE TO ARM NORMALLY. 2 L 7 4 4F A20WE 1996020200198 19960202 00198 WP 1996 2 2 UPS805335 1 19960104 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK AT FLOORBEAM TO WING L-ATTACH ANGLE LBL 40 FS 760. REPLACED ANGLE PER SRM 51-2-20D. 2 L 7 4 4F RT 4A25 1996020200199 19960202 00199 WP 1996 2 2 UPS805336 1 19960103 A 5510 5654500 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT HORIZ STAB LEADING EDGE I/B SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200202 19960202 00202 WP 1996 2 2 UPS805339 1 19960109 A 5713 STRINGER DOUG DC8 DC871F 302199D WP WS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, STRINGER 54 LOWER CRACKED AT STA XW 485. REPAIRED IAW UPS EO DC8-57 10-7184. 2 L 7 4 4F RT 4A25 1996020200203 19960202 00203 WP 1996 2 2 UPS805340 1 19960109 A 5711 SPAR DOUG DC8 DC871F 302199D WP NR 1 MAIN TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, NR 1 MAIN TANK O/B SECTION CRACKED LOWER CENTER SPAR AND WEB THROUGH ACCESS PNL 506A. REPAIRED IAW UPS EO DC8-5710-7895A. 2 L 7 4 4F RT 4A25 1996020200204 19960202 00204 WP 1996 2 2 UPS805341 1 19960109 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT FRAME STA 781 BETWEEN LONG 18 AND 19 CRACKED. REPAIRED IAW UPS EO DC8-53- 1553 AND TIMCO REO 01764. 2 L 7 4 4F RT 4A25 1996020200205 19960202 00205 WP 1996 2 2 UPS805343 1 19960128 A 5754 5751184505 FITTING DOUG DC8 DC871F 302199D WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 MAINTENANCE REPORTED, FLAP FITTING CRACKED ON O/B FLAP I/B FITTING. REMOVED AND REPLACED FITTING. 2 L 7 4 4F RT 4A25 1996020200206 19960202 00206 WP 1996 2 2 UPS805344 1 19960104 A 5320 SUBFLOOR WEB DOUG DC8 DC873F 302199F WP FS 45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON SUBFLOOR WEB FWD ENTRY DOOR FS 45. REPAIRED PER SRM 53-2- 0 AND SRM 51-1-2. 2 L 7 4 4F RT 4A25 1996020200207 19960202 00207 WP 1996 2 2 UPS805345 1 19960108 A 5315 3774605C01 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FLOORBEAM FS 55 LBL 37. REPLACED PER UPS EO DC8-53-1547. 2 L 7 4 4F RT 4A25 1996020200210 19960202 00210 WP 1996 2 2 9602069301 1 19960124 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP ELEC HYD PUMP FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 301RC 48054 ON APPROACH INTO BIL, THE RIGHT HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. ACTUATED EMERGENCY GEAR EXTENSION HANDLE, NO HELP. LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. INITIATED LEFT HIGH G-TURN, SECURED DOWN AND LOCKED INDICATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC SYSTEM AND FOUND BAD HYDRAULIC LINE AT ELECT RIC PUMP. REPLACED LEFT MAIN LANDING GEAR EMERGENCY EXTENSION CABLE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200211 19960202 00211 NM 1996 2 2 9602076719 1 19960127 A 3240 SHUTTLE VALVE BOEING 747 747251F 1384898 NM NR 15 BRAKE FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 619US 21321 DURING CLIMB AFTER LANDING GEAR RETRACTION, THE NR 4 HYDRAULIC QUANTITY WENT FROM 8 GALLONS TO 2 GALLONS AND THE LOW QUA NTITY LIGHT ILLUMINATED. THE NR 2 HYDRAULIC QUANTITY WENT FROM 5 GALLONS TO 8 GALLONS. AIRCRAFT DIVERTED TO SEA AND LA NDED WITHOUT INCIDENT. REPLACED THE NR 15 BRAKE SHUTTLE VALVE AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996020200212 19960202 00212 NM 1996 2 2 9602086627 1 19960126 A 3830 DRAIN BOEING 747 747251B 1384892 NM FS 800 CLOGGED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 627US 21709 DURING CLIMB, WATER OVERFLOWED FROM THE FIRST CLASS LAVATORY AND NR 2 GALLEY. AIRCRAFT RETURNED TO NRT AND LANDED WITHO UT INCIDENT. CLEANED AND PURGED CLOGGED DRAIN AT STATION 800 AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996020200213 19960202 00213 EU 1996 2 2 9602093245 1 19960127 A 3230 664700500A4B CONTROL UNIT AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 345NW 13299 9444 399 DURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT. CYCLED THE LANDING GEAR HANDLE AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT AND SYSTEM TESTED OK. 2 L 7 2 4F RT A28NM 1996020200214 19960202 00214 WP 1996 2 2 9602109953 1 19960128 A 2822 O-RING DOUG DC9 DC931 3022065 WP RT BOOST PUMP SPLIT A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 918RW 47158 DURING CLIMB AFTER CENTER TANK WAS EMPTY, THE RIGHT FUEL PRESSURE LOW LIGHT ILLUMINATED. RIGHT FUEL INDICATION DID NOT DECREASE AND THE LEFT FUEL INDICATION WAS DECREASING AT THE RATE OF EQUAL TO BOTH ENGINE BURNS. ACCOMPLISHED COCKPIT OP ERATING MANUAL PROCEDURES AND FUEL LOW PRESSURE LIGHT EXTINGUISHED WITH CROSSFEED ON. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. RIGHT FUEL INDICATION DID DECREASE ON DESCENT. REPLACED O-RING AT RIGHT AFT FUEL BOOST PUMP PRESSUR E LINE. ALSO, REPLACED THE LEFT ENGINE LOW PRESSURE FUEL FILTERS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F A6WE 1996020200215 19960202 00215 WP 1996 2 2 9602119989 1 19960127 A 2923 405016 AUX HYD PUMP DOUG DC9 DC931 3022065 WP LANDING GEAR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8945E 47181 LANDING GEAR WAS VERY SLOW TO RETRACT AFTER TAKEOFF. NOSE GEAR RED UNSAFE LIGHT EXTINGUISHED AT 3,500 FEET AND BOTH MAI NS AT 4,500 FEET. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR ALTERNATE HYDRAULIC PU MP DUE TO INTERNAL BYPASSING. OPERATIONAL CHECK NORMAL ON GEAR SWING AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200216 19960202 00216 NE 1996 2 2 9602129984 2 19960125 A 7220 NOSE BULLET DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE ICED UP A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 677MC 47756 688231 NR 1 ENGINE EPR INDICATION WAS ABNORMALLY HIGH DURING POWER APPLICATION ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND TH E AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED ICE DEPOSITS FROM THE ENGINE NOSE BULLET AND PT2 PROBE. ENGINE IN DICATIONS RETURNED TO NORMAL ON SUBSEQUENT RUNUP. 2 L 7 2 4F 4 F A6WE E2EA 1996020200217 19960202 00217 EU 1996 2 2 9602133215 1 19960128 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 315US 171 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED 'L/G GEAR NOT UPLOCKED' AND 'L/G DOORS NOT CLOSED' MESSAGES. CY CLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCI DENT. CORRECTIVE ACTION WILL BE ACCOMPLISHED DURING 'C' CHECK. 2 L 7 2 4F RT A28NM 1996020200218 19960202 00218 EU 1996 2 2 9602143223 1 19960128 A 3231 RETRACT MECH AIRBUS 320 A320211 3930320 EU NLG DOORS OUT OF RIG A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 323US 272 DURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED THE LANDING GEAR HANDLE AND GEAR EXTENDED NORMALLY. ACCOMPLIS HED A MISSED APPROACH. DURING SECOND APPROACH ATTEMPT, LANDING GEAR FUNCTIONED NORMALLY. AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE RIGGED THE NOSE LANDING GEAR DOORS AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996020200219 19960202 00219 WP 1996 2 2 9602151154 1 19960128 A 3234 HANDLE DOUG DC10 DC1040 3023508 WP LANDING GEAR LACK OF LUBE A NWAA O OTHER J WARNING INDICATION LD LANDING 1 GL 01 154US 46763 DURING GEAR EXTENSION, THE GEAR HANDLE BUTTON STUCK IN PLACE IN DOWN POSITION WITH AN UNSAFE GEAR INDICATION. RECYCLED GEAR AND MANUALLY PUSHED HANDLE IN AND GOT NORMAL GEAR INDICATIONS. LUBED GEAR HANDLE RELEASE BUTTON AND GEAR HANDLE PI VOTS. 2 L 7 3 4F A22WE 1996020200220 19960202 00220 WP 1996 2 2 9602169967 1 19960127 A 3260 GEAR LIGHT DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9331 47263 DURING APPROACH INTO MSP, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS CHECKED NO RMAL. DISCREPANCY COULD NOT BE DUPLICATED. CLEANED SWITCHES AS A PRECAUTION AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200221 19960202 00221 WP 1996 2 2 9602179917 1 19960128 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED FUSE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200222 19960202 00222 NM 1996 2 2 9602182275 1 19960126 A 2133 OUTFLOW VALVE BOEING 727 727251 138408H NM CABIN DIRTY A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 275US 21154 AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCID ENT. FOUND OUTFLOW VALVES VERY DIRTY. CLEANED OUTFLOW VALVES AND INSPECTED PLUMBING TO CONTROLLER. PERFORMED PRESSURI ZATION TEST, CHECKED OK. 2 L 7 3 4F A3WE 1996020200223 19960202 00223 NM 1996 2 2 9602192769 1 19960128 A 2612 FIRE LOOP BOEING 727 7272M7 138407S NM NR 2 ENGINE MALFUNCTIONED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 01 729RW 21742 DURING CLIMB, THE NR 2 ENGINE FIRE BELL AND LIGHT ACTIVATED. ENGINE SHUT DOWN, AIRCRAFT RETURNED TO ORD AND LANDED WITH OUT INCIDENT. REPLACED THE NR 2 FIRE DETECTION UNIT AND ENGINE FIRE LOOP. 2 L 7 3 4F A3WE 1996020200224 19960202 00224 WP 1996 2 2 9602209913 1 19960130 A 5350 RELEASE HANDLE DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HA NDLE FROM THE CLIPS DURING THE FIRST TWO ATTEMPTS. THE FORCE REQUIRED DURING THE THIRD ATTEMPT WAS WITHIN LIMITS. NO F URTHER ACTION WAS TAKEN. 2 L 7 2 4F A6WE 1996020200225 19960202 00225 NM 1996 2 2 96UAL900068 1 19960129 A 2780 RETRACT MECH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 516UA 24860 UNABLE TO MOVE FLAPS NORMALLY, LEADING EDGE LIGHT ON AND FLAP ASYMMETRY MESSAGE. FLAPS RECYCLED IN ALT OK, BUT STILL LO CKED OUT IN NORMAL. BITE CHECK ON NR 1 FSEU SHOWS SLAT LOSS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200226 19960202 00226 NM 1996 2 2 96UAL900069 1 19960129 A 3350 TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 EMERGENCY EXIT LIGHTS FLOOR TRACK LENS AT ROWS 1 THROUGH 2 ARE DAMAGED. REPLACED EMERGENCY EXIT LIGHTS FLOOR TRACK COVE R. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200227 19960202 00227 NM 1996 2 2 96UAL900070 1 19960129 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY EXIT LIGHT STRIP DAMAGED AND LOOSE. SECURED THE EMERGENCY EXIT LIGHT STRIP TRACK TO FLOOR USING TAPE AND LEAV ING THE EMERGENCY EXIT LIGHT STRIP ELEMENT VISIBLE. NEEDS TO BE CLEANED UNDERNEATH TRACK AND RESECURED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200228 19960202 00228 NM 1996 2 2 96UAL900071 1 19960129 A 2780 FSEU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 527UA 24995 ON APPROACH, EICAS MESSAGE DISPLAYED, LEADING EDGE ASYMMETRY MESSAGE AND LEADING EDGE WARNING LIGHT. FLAPS STUCK AT 25 DEGREES AND NO ADVERSE CONTROL WHEEL FORCES - LANDED WITH FLAPS AT 25 DEGREES. REPLACED NR 1 FSEU AND SWITCHES S10338 AND S10340 PER MM. CYCLED FLAPS SEVERAL TIMES AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200229 19960202 00229 NM 1996 2 2 96UAL900072 1 19960129 A 3231 27464 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR MALFUNCTIONED A UALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 WP 29 534UA 25129 ON TAKEOFF, NOSE GEAR RETRACTION DOORS LIGHT REMAINED ON WITH NOTICEABLE VIBRATION AND WIND NOISE. GEAR DISAGREE LIGHT ON EICAS. NOSE GEAR DOORS WOULD NOT FULLY CLOSE DUE TO A MALFUNCTIONING NOSE GEAR DOOR ACTUATOR. REPLACED NOSE GEAR AC TUATOR, SYSTEM CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200230 19960202 00230 NM 1996 2 2 96UAL900073 1 19960129 A 2781 285T004953 FSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 608UA 21869 AFTER TAKEOFF WITH FLAP RETRACTION, LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE APPEARS AND AMBER WARNING PRESENT. FLAPS APPEAR TO BE VISUALLY RETRACTED. AIRCRAFT RETURNED TO MIA. SUPPLEMENTAL DATA UPDATE: THE LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE AND AMBER WARNING WERE FALSE FLAP SLAT ELECTRONIC UNIT (FSEU) INDICATIONS. THE FSEU WAS REPLACED PER MM 2 7-51-01. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200231 19960202 00231 NM 1996 2 2 96UAL900074 1 19960129 A 2560 3A34991 VALVE FLANGE BFGOODRICH 7A14793 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA G421 25158 DURING SLIDE OVERHAUL, FOUND RIGHT HAND INFLATE/DEFLATE RUBBER MOUNTING FLANGE CRACKED. PROBABLE CAUSE WAS BENDING OF T HE VALVE DURING SLIDE PACKING. REPLACED RUBBER INFLATE/DEFLATE VALVE FLANGE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996020200232 19960202 00232 NM 1996 2 2 96UAL900075 1 19960129 A 2130 FLOW CONTL VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RADIO RACK MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7257U 21404 AIRCRAFT RETURNED, UNABLE TO MAINTAIN PRESSURE. CABIN WOULD NOT HOLD MORE THAN 1 DIFFERENTIAL PRESSURE CLIMBING THROUGH 10K FEET, CABIN WAS 8,000 FEET. ACCOMPLISHED PRESSURE CONTROL SYSTEM CHECK, NO DEFECTS FOUND. RAN ENGINES AND DUCT PR ESSURE NORMAL. AIRCRAFT PRESSURIZED OKAY. RADIO RACK FLOW CONTROL VALVE OFF SCHEDULE AT RENO. REPLACED RADIO RACK FLO W CONTROL VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1996020200233 19960202 00233 WP 1996 2 2 96UAL900076 1 19960129 A 2120 AIR DISTR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 1831U 46630 NOXIOUS OILY FUMES FROM AIR CONDITIONING SYSTEM ON GROUND AND IN THE AIR. SOME PASSENGERS AND FLIGHT ATTENDANTS WERE NA USEATED. FUMES REALLY STRONG WHEN IN RAINY CONDITIONS. SUPPLEMENTAL DATA UPDATE COULD NOT FIND SOURCE OF ODOR OR DUPLI CATE PROBLEM. REPLACED COALESCER BAGS AS A PRECAUTIONARY ACTION. 2 L 7 3 4F 4 F A22WE E23EA 1996020200234 19960202 00234 WP 1996 2 2 96UAL900077 1 19960129 A 5620 9F122891 SEAL DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN WINDOW SEPARATED A UALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 29 1810U 46609 WINDOW AT 12J, ANACOUSTICAL PANE AND RETAINER FOR PANE MISSING. SUPPLEMENTAL DATA UPDATE REPLACED ANACOUSTICAL PANE AT 12J. ON 1/16/96 1T WAS REPORTED THAT WINDOW 12J SEAL WAS COMING OFF. RESET THE SEAL IN THE WINDOW TRACK. SUBMITTER SU GGEST, THE PROBABLE CAUSE OF THE PANE SEPARATION IS THAT THE SEAL MAY HAVE BEEN INSTALLED INCORRECTLY. 2 L 7 3 4F 4 F A22WE E23EA 1996020200235 19960202 00235 1996 2 2 96UAL900078 4 19960129 A 3417 4061100901 ADC BOEING 737 737322 1384676 NM LEFT INOPERATIVE A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 310UA 23671 ON TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR AND BOTH FLIGHT MANAGEMENT COMPUTERS INOP. NUMBER ONE AIR DATA COMPUTER SHOWED BARO REFERENCE NUMBER TWO, OUT OF LIMIT IN FAULT MEMORY. REPLACED NUMBER ONE AIR DATA COMPUTER, CHECKS OK. 2 L 7 2 4F RT A16WE 1996020200236 19960202 00236 NM 1996 2 2 96UAL900079 1 19960129 A 2740 69394131 BRAKE PLATE BOEING 737 737322 1384676 NM HORIZ STAB CHIPPED A UALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 203UA 24718 CREW REPORTS THAT THE HORIZONTAL STABILIZER TRIM IS JAMMED AND CANNOT BE TRIMMED MANUALLY OR ELECTRONICALLY. JACKSCREW ASSEMBLY WAS JAMMED, ASSEMBLY WAS REMOVED FROM AIRCRAFT AND ROUTED TO THE SHOP. DURING DISASSEMBLY A BRAKE PLATE WAS FO UND CHIPPED. CHIP SHOWED SIGNS OF WEAR AND AN IMPACT MARK. 2 L 7 2 4F RT A16WE 1996020200237 19960202 00237 NM 1996 2 2 96UAL900080 1 19960129 A 3350 CONNECTOR BOEING 737 737322 1384676 NM CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 320UA 23952 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 TO ROW 18. RESEATED CONNECTOR ON POWER CABLE, CHECKS OK. 2 L 7 2 4F RT A16WE 1996020200238 19960202 00238 SO 1996 2 2 COMA9610044 1 19960126 A 2435 23080013 STARTER GEN EMB 120 EMB120RT SO LT ENGINE FAILED A COMA E D ENGINE SHUTDOWN RETURN TO BLOCK M Y OVER TEMP ENGINE STOPPAGE TX TAXI/GRND HDL 1 SO 01 189CA 5986 118 120189 DURING LEFT ENGINE START, T6 EXCEEDED 900 DEGREE CELSIUS. START WAS ABORTED AND DURING DRY MOTOR, THE STARTER FAILED. R EPLACED THE STARTER/GENERATOR AND START CONTACTOR. 2 L 7 2 4T RT A31SO 1996020200239 19960202 00239 SO 1996 2 2 COMA9610045 1 19960128 A 3150 80055711 AURAL WARN UNIT EMB 120 EMB120RT SO AVIONICS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 255CA 11394 2242 120238 TAKEOFF AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE AURAL WARNING UNIT. 2 L 7 2 4T RT A31SO 1996020200240 19960202 00240 SO 1996 2 2 COMA9610046 1 19960128 A 2750 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO INST PANEL DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 205CA 7650 491 120205 TAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT. 2 L 7 2 4T RT A31SO 1996020200241 19960202 00241 EU 1996 2 2 COMA9630026 1 19960129 A 7712 TQ INDICATION SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 358CA 340A047 THE RT ENGINE TORQUE INDICATOR WENT FULL DEFLECTION DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY DURING MAINTENANCE RUNS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996020200242 19960202 00242 NM 1996 2 2 DHL96742005 1 19960130 A 2611 302842 SMOKE DETECTOR BOEING 727 727225 1384077 NM NR 3 MALFUNCTIONED A T DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 742DH 21290 CARGO SMOKE LIGHT ILLUMINATED DURING CRUISE FLT. INSPECTED CARGO AREA FOR SMOKE AND INSPECTED NR 1, 2 AND 3 SMOKE DETEC TORS AND AMP. OPS CHECKED 3 TIMES, TEST OK. RAN PROVISION CHECK AND AIR CONDITION CK PER JRH, NO FAULT FOUND. 2 L 7 3 4F A3WE 1996020200244 19960202 00244 NM 1996 2 2 DL72S960173 1 19960123 A 3320 036405 BALLAST BOEING 727 727232 1384082 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 536DA 22049 CEILING POWER FWD C/B ON P18-3 PNL POPPED FOLLOWED BY AN ACRID ELECTRICAL SMELL IN THE FWD PART OF THE AIRCRAFT. PULLED AND COLLARED FWD CONT C/B AND FWD CEILING PWR C/B. PULLED C/P ON CEILING LIGHT AT RT ROW 24 AND LT 17. FOUND BURNED B ALLAST, REPLACED BALLAST AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996020200245 19960202 00245 NM 1996 2 2 DL72S960176 1 19960123 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 FOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996020200246 19960202 00246 NM 1996 2 2 DL72S960177 1 19960123 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 FOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M /M 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996020200247 19960202 00247 NM 1996 2 2 DL72S960180 1 19960124 A 2120 BOEING 727 727232 1384082 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 420DA 39986 21273 ON TAKEOFF, COCKPIT AND CABIN FILLED WITH SMOKE, DID NOT SMELL LIKE ELECTRICAL. FLIGHT RETURNED TO SEA. MAINT INSPECTE D ENGINES INLETS AND EXHAUST APU AREA AND RAM AIR DOORS, NO DISCREPANCY FOUND. RAN APU WITH A/C PACKS AND ENGS WITH PAC KS. SUSPECT ANTI-ICE FLUID FUMES CAUSED TROUBLE. ALL ELECT SYSTEMS OPERATED NORMAL AND ACFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996020200248 19960202 00248 NM 1996 2 2 DL72S960187 1 19960119 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FROM HMV ATL, THE LOWER SKIN ON THE LT HORIZ STAB IS GOUGED AND CRACKED I/B END. ACCOMPLISHED REPAIRS PER SRM 55-10-3 F IG 3. 2 L 7 3 4F A3WE 1996020200249 19960202 00249 NM 1996 2 2 DL72S960198 1 19960125 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 FOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE, ADJACENT TO O/B TRACK. REPAIRED P ER M/M 57-54-0. 2 L 7 3 4F A3WE 1996020200251 19960202 00251 NM 1996 2 2 DL72S960202 1 19960125 A 5320 DECK BOEING 727 727232 1384082 NM BS 940-950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING MIDVISIT, TWO 1 INCH CRACKS WERE FOUND IN THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK BETWEEN STATIONS 940 AND 950, BETWEEN LBL 50 AND 60. MODIFICATION INSTALLED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 727-53-0149, REVISION 4. 2 L 7 3 4F A3WE 1996020200252 19960202 00252 NM 1996 2 2 DL72S960204 1 19960126 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND ON A-2 LETTER CHECK, .375 INCH CRACK IN TORQUE BOX LIGHTENING HOLE AT STA 1303 RIGHT SIDE 48 SECTION. REPAIRED PE R MM 53-11-0. 2 L 7 3 4F A3WE 1996020200253 19960202 00253 NM 1996 2 2 DL72S960206 1 19960126 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOOR AREA CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND DURING A-2 LETTER CHECK, .75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LWR HINGE CUTOUT. REPAIRED PER ERA 303079-1 4 AND M/M 53-30-0. 2 L 7 3 4F A3WE 1996020200254 19960202 00254 NM 1996 2 2 DL72W960212 1 19960127 A 2160 COOLING VALVE BOEING 727 727247 138408F NM PWA 2037 PW2037 NE EE COMP FAILED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 2817W 20873 716548 DISPATCHED WITH ONE PACK, MIX VLV INOP. ACFT WOULD NOT HOLD THE CABIN WITH CARGO HEAT OUTFLOW CLOSED AND OUTFLOW VLV FU LL CLOSED. REPLACED EQUIP COOLING VLV IN E/E COMP, PRESS ACFT TO 3 PSI AND OPERATION CKS OK. 2 L 7 3 4F 4 F A3WE E17NE 1996020200255 19960202 00255 NM 1996 2 2 DL73E960188 1 19960123 A 2460 TRANS RELAY BOEING 737 737247 138448D NM EE COMPT FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 238WA 23186 AT CRUISE 33,000 FT, ALT LOST ALL ELECT POWER AND CAPT INSTRUMENTS WERE COMPLETELY OUT FOR APPROX 20 MIN. RECOVERED F/O INSTR AND EVENTUALLY CAPT INSTRUMENTS RETURNED. REPLACED NR 1 TXFR RLY R-3 CPN 243201020. FOUND NR 2 ALT TXFR BUS C/B POPPED AND WOULD NOT RESET. REPLACED SAME. REPLACED NR 1 GEN BRKR CPN 243001013 S/N TF7130. ALSO, REPLACED NR 1 BTB S/N 172A CPN 243001008 AND BUS PROT PANEL S/N 6836 CPN 243001013. OPERATION NOW NORMAL. 2 L 7 2 4F A16WE 1996020200256 19960202 00256 NM 1996 2 2 DL757960161 1 19960123 A 3231 SOLENOID 96005011 BOEING 757 757232 1384965 NM RT MLG DOOR FAILED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 642DL FAH0504 23996 RIGHT MAIN GEAR WOULD NOT EXTEND NORMALLY, USED ALT EXTENSION AND GOT NORMAL INDICATION. REPLACED RT GEAR DOOR INTERLOC K SOLENOID AND OPS NORMAL. 2 L 7 2 4F RT A2NM 1996020200258 19960202 00258 NM 1996 2 2 DL757960214 1 19960128 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 673DL 25978 POWER SUPPLY FUSES OPEN, TRACK LIGHTS INOP IN AFT CABIN. REPLACED POWER SUPPLY AND OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996020200259 19960202 00259 NE 1996 2 2 DL76L960185 2 19960124 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 180DN 25985 724685 ENGINE COMPRESSOR STALLED AS POWER WAS ADDED FOR T/O. BELIEVED TO BE LT ENGINE, NO EXCEEDENCE, ENGINE WAS REPLACED AND ROUTED TO SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1996020200260 19960202 00260 NM 1996 2 2 DL76L960186 1 19960124 A 2560 SLIDE RELAY BOEING 767 767332 1382001 NM E4 RACK DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 ON ALL CABIN SERVICE AND ENTRY DOORS, THE SLIDE ARMED LIGHT WILL NOT FLASH IN ARMED MODE WITH THE HANDLE SLIGHTLY PULLED . REPLACED DEFECTIVE RELAY, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996020200261 19960202 00261 NM 1996 2 2 DL76L960192 1 19960125 A 5754 114T310022A SLAT BOEING 767 767332 1382001 NM NR 7 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE NR 7 SLAT TRAILING EDGE WEDGE LOWER SKIN WAS FOUND WITH A HOLE. THE HOLE IS .5 INCH IN DIAMETER AND IS LOCATED 42 I NCHES INBOARD FROM THE OUTBOARD EDGE AND 4 INCHES FOWARD OF THE AFT EDGE. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, TYPE 4.1-25. ACCOMPLISHED REPAIRS PER DL ERA 273 086-14AD. 2 L 7 2 4F RT A1NM 1996020200262 19960202 00262 WP 1996 2 2 DLL10960101 1 19960116 A 3230 BUSHING LS100203A7 LKHEED 1011 10113851 5265010 WP LT GEAR NOT INSTALLED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 733DS 193C1224 ON GEAR RETRACTION, RED DOOR AND INTRANS WITH LEFT GEAR OR DOOR ON S/O PANEL. CYCLED GEAR, SAME INDICATIONS. FOUND PHA SE CONTROL VALVE INCORRECTLY INSTALLED DUE TO OMITTED BUSHING ON THE TWO ACTUATING ROD/S TWO LUGS. INSTALLED MISSING BU SHING, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996020200263 19960202 00263 WP 1996 2 2 DLL10960190 1 19960123 A 5312 1504400 BULKHEAD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 712DA 193C1088 WHILE PERFORMING INSPECTION SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH A 12 INCH LONG VERTICAL CRACK AT R BL 22.5. THE SUBJECT WEB IS M/F .050 7075 T6 CLAD SHEET. ACCOMPLISHED REPAIRS PER DL ERA 273152-14. 2 L 7 3 4F A23WE 1996020200264 19960202 00264 WP 1996 2 2 DLL10960191 1 19960125 A 5320 1553017 FITTING LKHEED 1011 10113851 5265010 WP FS 792 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 BOTH THE FWD AND AFT FITTINGS ON THE FWD FRAME FS 792 ARE REQUIRED TO BE MFG'D TO ACCOMMODATE A FRAME REPAIR INSTALLED B Y ER/A 271917-14. SUBJECT FITTINGS ARE M/F 7075-T6 DIE FORGINGS, APPROVAL PER DL ERA 271918-14 REV B. 2 L 7 3 4F A23WE 1996020200265 19960202 00265 WP 1996 2 2 DLL10960195 1 19960125 A 5312 1505220 WATERLINE LKHEED 1011 10113851 5265010 WP FS 1363 ELONGATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 WHILE ACCOMPLISHING THE CENTER WEB SPLICE ON THE FS 1363 BKHD PER SI 7-69959-14AD, OPN 0319, THE POTABLE WATER LINE CUTO UT WAS DAMAGED AND ELONGATED THROUGH THE WEB AND FWD MOD SPLICE STRAP. THE ORIGINAL CUTOUT WAS A 1.25 DIA HOLE. THE EL ONGATED CUTOUT HAS A MAX WIDTH OF 1.5 AND CAUSES A SHORT EDGE DISTANCE CONDITION OF .22 MIN ON 4 ADJACENT FASTENERS. TH E ORIGINAL WEB IS MADE FROM .065 THICK 7075-T6 CLAD SHEET. THE FWD MOD SPLICE STRAP IS MADE FROM .080 THICK 7075-T6CLAD SHEET. ACCOMPLISHED REPAIRS PER DL ERA 272019-14 REV A. 2 L 7 3 4F A23WE 1996020200266 19960202 00266 WP 1996 2 2 DLL13960193 1 19960125 A 5312 STRAP LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 THE BULKHEAD SPLICE STRAP AT FS 1363 LBL 42.5 WAS FOUND CRACKED. THE SUBJECT STRAP IS M/F 0.100 7075-T6 CLAD. ACCOM PLISHED REPAIRS PER DL ERA 272789-14AD. 2 L 7 3 4F A23WE 1996020200267 19960202 00267 NM 1996 2 2 DLM88960179 1 19960123 A 3340 LIGHT LENS DOUG MD88 MD88 3023688 NM RT WING LIGHTNING STRIKE A DALA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 905DL 49536 AIRCRAFT INCURRED LIGHTNING STRIKE ON APPROACH AND SMOKE WAS SMELLED IN CABIN AND COCKPIT. THE SMOKE OCCURED 5 TO 8 MIN AFTER STRIKE AND DISSIPATED AFTER 10 MIN. INSPECTED AIRCRAFT PER M/M 05-53-00 PG 601. FOUND RT AFT TAIL LIGHT LENS SH ATTERED AND NO OTHER DAMAGE NOTED. REPLACED LENS, RAN PACKS AND NO ODORS OR SMOKE. 2 L 7 2 4F RT A6WE 1996020200268 19960202 00268 NM 1996 2 2 DLM88960182 1 19960124 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA K NONE J WARNING INDICATION LD LANDING 1 SO 27 919DE 53422 NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OP 4703, JACKED A/C, CYCLED NOSE GEAR AND ALL IND NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1996020200269 19960202 00269 NM 1996 2 2 DLM88960189 1 19960124 A 3220 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 919DE 53422 NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OPN 4703, JACKED AN CYCLED NOSE GEAR AND ALL INDICATIONS NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1996020200270 19960202 00270 NM 1996 2 2 DLM88960205 1 19960126 A 2913 PUMP DOUG MD88 MD88 3023688 NM LT MLG WW FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 923DL 49705 AFTER T/O, SMOKE IN CABIN AND COCKPIT WITH SMOKE ALARMS ON FURTHER INSP FOUND HYD TRANSFER PUMP CASE DRAIN LINE HAD FILL ED ITS OVERFLOW CONTAINER. WHICH IN TURN HAD BEEN RUNNING INTO THE APU INTAKE. REPLACED HYD TRANSFER PUMP, DUMPED AND CLEANED DRAIN CAN. APU WILL HAVE TO BE CLEANED TO PREVENT FURTHER CONTAMINATION OF AIR CONDITIONER SYSTEMS. 2 L 7 2 4F RT A6WE 1996020200271 19960202 00271 WP 1996 2 2 MWEA96028 1 19960126 A 5311 FRAME DOUG DC9 DC914 3022034 WP LT MLG WW GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DURING D-CHECK, FOUND FWD FRAME OF LT WHEEL WELL OPENING HAS A DEEP GOUGE 4 INCHES LONG. INSTALLED DOUBLER REPAIR IAW S RM 53-01 FIG 2 SHEET 4. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200272 19960202 00272 NM 1996 2 2 VSTA9601014 1 19960128 A 2810 106121061N FUEL CELL BOEING 737 737204 1384458 NM NR 2 DAMAGED A VSTA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 312VA 20236 FUEL LEAKING FROM CENTER DRAIN MAST. REPLACED CENTER TANK NR 2 FUEL BLADDER AND REPAIRED VENT BOX. LEAK CHECKS NORMAL. 2 L 7 2 4F A16WE 1996020200273 19960202 00273 NM 1996 2 2 VSTA9601015 1 19960128 A 5610 BAC008632 WINDOW BOEING 737 737247 138448D NM R1 WINDOW CRACKED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 302VA 20126 R1 WINDOWS OUTER PANE CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER. 2 L 7 2 4F A16WE 1996020200346 19960202 00346 NM 1996 2 2 96ZZZM102 1 19960103 A 3350 3314030 LIGHT BOEING 727 727227 1384078 NM CABIN INOP A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 769AT 028715 21998 EMERGENCY EXIT LIGHT ABOVE RIGHT FORWARD SERVICE DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT. 2 L 7 3 4F A3WE 1996020200350 19960202 00350 NE 1996 2 2 96ZZZM106 2 19960103 A 7261 ENGINE OIL 2380 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RIGHT REQ'D SERV A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 429JS 3043 FLT NR 4005 - EN ROUTE FROM CVG TO PHL, CAPTAIN NOTICED A FLUCTUATION IN THE RIGHT ENGINE OIL PRESSURE INDICATION. AIRC RAFT DIVERTED TO PIT WHERE MX SERVICED THE RIGHT ENGINE WITH FOUR QUARTS OF TURBINE OIL. GROUND CHECKED GOOD AIRCRAFT T O SERVICE. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 1996020200428 19960202 00428 NM 1996 2 2 AALA960002 1 19960101 A 3350 A3060720101 CONDUCTOR DOUG MD11 MD11 3023602 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE FROM L2 DOOR TO PAX SEAT ROW 15B INOPERATIVE. REPLAC ED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR AFT OF L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996020200429 19960202 00429 EU 1996 2 2 AALA960010 1 19960103 A 3260 200392605 BUFFER FOKKER F28 F28MK0100 4990807 EU LT MLG NEED ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1431B 11416 BNA - FLT 2079 - AFTER TAKEOFF BNA, WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR MFDU WARNING DISPLAYED. RECYCLE D LANDING GEAR WITH SAME RESULTS. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEA R DOOR BUMPER AND INSTALLED LOCK PIN AND SAFETY WIRE. ACCOMPLISHED LANDING GEAR RETRACTON CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996020200430 19960202 00430 WP 1996 2 2 AALA960017 1 19960107 A 3350 A3030398101 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 76201 53291 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 1 THROUGH 4 IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996020200431 19960202 00431 WP 1996 2 2 AALA960018 1 19960107 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996020200443 19960202 00443 EU 1996 2 2 C2XA96IA014 1 19960111 A 2820 1153000 PRESS SWITCH AEROSP ATR42 ATR42320 8680930 EU RT NACELLE LEAKING A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 17810 093 IAH - DURING 4A CHECK INSPECTION, FOUND RT FUEL SHUTOFF VALVE PRESSURE SWITCH LEAKING, LOCATED BEHIND RIGHT ENGINE AFT U PPER COWLING, FORWARD OF FRONT WING SPAR. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200444 19960202 00444 EU 1996 2 2 C2XA96IA015 1 19960112 A 2710 2S711009100200 BELLCRANK BRG AEROSP ATR42 ATR42320 8680930 EU LT AILERON RUSTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING 1A CHECK INSPECTION, FOUND LEFT AILERON CONTROL SYSTEM BELLCRANK BEARING BINDING AND RUSTY. BELLCRANK LOCA TED AT LEFT WING RIB 24, ACCESS THROUGH LOWER WING PANEL 523AB. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK ASSEMBLY . AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200445 19960202 00445 EU 1996 2 2 C2XA96IA016 1 19960112 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING 1A CHECK INSPECTION, THE PASSENGER DOOR/STAIR EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. LOCATED O N THE INTERIOR OF THE DOOR, LOWER SIDE OF THE SECOND STEP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. AIRCRAFT A PPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200446 19960202 00446 EU 1996 2 2 C2XA96IA017 1 19960112 A 5320 ANGLE AEROSP ATR42 ATR42320 8680930 EU WING/FUS CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING 4C CHECK INSPECTION, FOUND A CRACKED ATTACHMENT ANGLE ON RIGHT WING TO FUSELAGE FAIRING SUPPORT FRAME NR 29 . MAINTENANCE REMOVED AND REPLACED ATTACHMENT ANGLE. (M) 2 H 7 2 4T RT A53EU 1996020200447 19960202 00447 EU 1996 2 2 C2XA96IA018 1 19960112 A 5730 S5241053600000 ACCESS PANEL AEROSP ATR42 ATR42320 8680930 EU LT WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING 4C CHECK INSPECTION, FOUND LEFT WING ACCESS PANEL NR 522CT TO HAVE CORROSION ON MATING SURFACES. MAINTENAN CE REMOVED AND REPLACED THE PANEL. (M) 2 H 7 2 4T RT A53EU 1996020200448 19960202 00448 SO 1996 2 2 C2XA96IA019 1 19960114 A 2550 PE710261 TIE DOWNS EMB 120 EMB120RT SO CARGO FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C1 CHECK I