20030328000012003032800001CE 2003 3 28 CA030212004 120030212A2910124K0016CL0150 HOSE CESSNA500 550 2076604CE PWA JT15 JT15D4 52112NE BRAKE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) WHEEL WELL FOUND SOAKED WITH HYDRAULIC FLUID , AFTER LAST FLIGHT OF THE DAY. FOUND BRAKE FLUID RESEVOIR DEPLETED. TOPPED OFF BRAKE FLUID RESEVOIR BUT WAS UNABLE TO DETECT LEAK UNTIL THE A/C WAS ON JACKS. WE HAVE HAD 2 PRIOR OCCURRENCES AND DETERMINED THAT WITH THE GEAR EXTENDED THE FLEX LINE IS TAUT. THIS IS REQUIRED IN ORDER TO CLEAR THE WHEEL WELL ON RETRACTION. THERE IS QUITE A LOAD JUST BEHIND THE LOWER FITTING. 1L72 4F4 F A22CE E1NE 20030328000032003032800003NM 2003 3 28 CA030212006 120030206A3230DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 HYD SYS LEAKING W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA 3867538675 (CAN) AFTER DEPARTURE DURING GEAR UP SELECTION, LOSS OF NR 2 HYDRAULIC QUANTITY AND FAILURE OF GEAR TO RETRACT . AIRCRAFT RETURNED FOR NORMAL LANDING . MAINTENANCE INSPECTION FOUND NLG DOWNLOCK ACTUATOR FLEX LINE CRACKED/LEAKING . TEMPORARTY FLEX LINE INSTALLED AND HYDRAULIC SYSTEM RE-FILLED. LINE DSC252B4-0124 DOM 9-95 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030328000052003032800005NE 2003 3 28 CA030212009 120030207A62106117020201067 BLADE SKRSKYS61 S61N 8142104NE GE CT58 CT581402 30011NE MAIN ROTOR CRACKED W BA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) INBOUND FROM RIG, 'BIM' LIGHT ILLUMINATED. EMERGENCY CHECKLIST C/W. AIRCRAFT DIVERTED TO SABLE ISLAND FOR PRECAUTIONARY LANDING. COMM CENTRE ADVISED.POST S/D CHECK CONFIRMED PRESSURE BELOW LIMITS. 2G72 4U4 U 1H15 1E3 20030328000072003032800007EA 2003 3 28 CA030213003 220030210A7230 CASE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA COMPRESSOR PUNCTURED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) PIN SIZE HOLE LOCATED ON NR 2 PT6T-3 POWER SECTION GAS GENERATOR CASE AT APPROXIMATELY 7 O'CLOCK POSITION 3 3/4 INCHES AFT OF FIRST CIRCUMFIRENTIAL SEAM WELD (BY P3 AIR BOSS SUPPLYING AIR TO TORQUEMETER CLUTCH SEAL) WHILE PERFORMING VISUAL INSPECTION OF GAS GENENERTOR CASE. SILIGHT AIR LOSS FROM HOLE BUT NOT AFFECTING POWER ASSURANCE FIGURES (APPROXIMATELY +1.7 TO 1.9 PERCENT N1). POWER SECTION CHANGED. 1G71 4U4 U H4SW E22EA 20030328000112003032800011 2003 3 28 CA030214005 420030207A2340301 SWITCH BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA PUSH/TALK FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) PUSH TO TALK SWITCH REPLACED AFTER FAILURE. NEW PUSH TO TALK SWITCH FAILED WITH 4.7 HOURS USED. SWITCH COMPLETELY BROKEN TO PIECES. ONLY CREW ACTION WAS TO USE HAND MICROPHONE AND HAVE CAPTAIN SIDE DO THE MAJORITY OF COMMUNICATION. 2L72 4T4 TRTA24CE E4EA 20030328000152003032800015EU 2003 3 28 CA030214009 120030210A1430NAS1351N412 BOLT AIRBUS310 A310300 3930305EU GE CF6 CF680C2A5 NE BRAKE ACCUM LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE A-01 CHECK, RT MAIN LANDING GEAR, EMERGENCY BRAKE MANIFOLD WAS SUSPECTED TO BE LEAKING. INSPECTION FOUND THE ALTERNATE BRAKE RETURN ACCUMULATOR LOOSE ON THE MANIFOLD, DUE TO THE FACT THAT THE BOLTS INSTALLED TO SECURE THE ACCUMULATOR WERE NOT WIRE LOCKED. T 2L72 4F4 FRTA35EU E13NE 20030328000162003032800016WP 2003 3 28 CA030214010 120030205A8097 WIRE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524* NE NR 1 PYLON CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING NR 1 ENGINE START, THE ENGINE START VALVE SWITCH LIGHT DID NOT ILLUMINATE. INSPECTION FOUND WIRES DAMAGED DUE TO CHAFING. THE FOLLOWING WIRES WERE FOUND MELTED, BURNED AND SOLDERED. THE LOCATION OF WIRES WERE ON THE ENGINE NR 1 PYLON, UNDER PANEL 452 AT, TOWARD THE FWD OF PANEL UNDER THE LT HINGE OUTBOARD COVER UNDER AND FWD OF THE PHENOLIC ROLLER GUIDE, CAUSED THE CHAFING. WIRE WAS FOR THE START VALVE INDICATION AND WIRE WAS FOR THE DISCHARGE BOTTLE INDICATION. THIS PREVENTED THE INDICATION IN THE FLIGHT COMPARTMENT. THE WIRES WERE REPAIRED IAW WD STANDARD PRACTICE MANUAL 20-15-04. 2L73 4F4 F A23WE E12EU 20030328000172003032800017SW 2003 3 28 CA030217001 120030214A5510206020121010 FITTING BELL BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL HORIZONTAL STAB CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) CRACKS FROM RIVIT HOLE IN 0.125 INCH STAMPED ATTACHMENT FLANGE COMPLETELY ACROSS FLANGE SEPARATING IT INTO TWO PIECES. (NOTE) THERE IS NO DANGER OF STABILIZER SEPARATION FROM THE AIRCRAFT AS THE FLANGE ISSTILL RIVITED TO THE INBOARD RIB IN 5 OTHER PLACES, THE STABILIZER IS CLAMPED TO THE SPAR IN 4 PLAC ES AND THERE IS A STOP ASSEMBLY TO PREVENT SEPARATION AS WELL. THIS PROBLEM HAS BEEN WITH US A LONG TIME BUT WHAT BRINGS THIS ONE TO LIGHT IS WE HAVE FOUND SIX (6) CRACKS ON 5 AIRCRAFT IN TWO MONTHS. RECOMMEND CREWS BE MORE VIGILENT ON INSPECTIONS SO TO DETECT CRACKS BEFORE THEY HAVE A CHANCE TO GROW. 1G71 3U3 U H2SW E4CE 20030328000202003032800020EU 2003 3 28 CA030218005 120030216A3260ABS012110 PROXIMITY SENSOR AIRBUS320 A320212 3930322EU CFMINTCFM56 CFM565A3 NE NLG FAILED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) AFTER TAKE-OFF AND GEAR RETRACTION, 'NLG DOOR OPEN' MESSAGE APPEARED ON ECAM. GEAR CYCLED, BUT MESSAGE REPEATED. AIRCRAFT RETURNED FROM FLIGHT. POST FLIGHT REPORT INDICATED NOSE GEAR DOOR PROX. SENSORS 30GA AND 31 GA FAILED. BOTH SENSORS REPLACED, AND SYSTEM CHECKED SERVICEABLE. AIRCRAFT RELEASED TO SERVICE. 2L72 4F4 FRTA28NM E29NE 20030328000212003032800021SW 2003 3 28 CA030218006 120030205A321121949 TUBE BBAVIA7 7GCBC 1220601SW LYC O360 O360C2E 41514EA MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT HAS OVER 2,700 HOURS OF TOWING GLIDERS OFF A GRASS STRIP. DEFECT WAS FOUND DURING RECOVERING OF FUSELAGE. VERTICAL CRACK ON BOTH SIDES OF LT REAR GEAR 'U' BOLT BUSHING IN 'U' BOLT ATTACH TUBE. 1H71 3O3 ONCA759 E286 20030328000242003032800024NM 2003 3 28 0300626632 120030324A2197DM553 CONNECTOR BOEING747 747251B 1384892NM GASPER FAN BROKEN A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL01632US 23112 DURING APPROACH A STRONG ELECTRICAL FUME EMITTED BETWEEN THE NR 2 AND NR 3 CABIN COMPARTMENT. PULLED THE NR 2 AND NR 3 GALLEY CIRCUIT BREAKERS AND THE FLIGHT LANDED WITHOUT INCIDENT. REPAIRED BROKEN GASPER FAN WIRE PINS NR 4 AND NR 5 ON ELECTRICAL PLUG DM553. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20030328000262003032800026NM 2003 3 28 03084428 120030325A3350 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27428FJ 3193 DURING MAINTENANCE INSPECTION, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030328000282003032800028EU 2003 3 28 03FDEA00353 120030328A5530A5357000800600 PANEL AIRBUS310 A310 EU VERTICAL STAB DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 VERTICAL STAB. LE PANEL 321AL DELAMINATED 2L72 4F RTA35EU 20030328000292003032800029EU 2003 3 28 2003F00157 120030326A290012TW13 SWITCH SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D1 NE COLLECTIVE INTERMITTENT E S4WAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 WP074027Q3202 2904 9456 DURING CRUISE FLIGHT THE PILOT FELT THE CONTROLS GET "HARD" LIKE A HYDRAULIC SYSTEM FAILURE, BUT AIRCRAFT STILL FLYABLE. PILOT OPTED TO DO PRECAUTIONARY LANDING IN AN OFF-AIRPORT AREA WITH NO INCIDENT REGARDING PERSONNEL OR AIRCRAFT. AFTER INSPECTING SYSTEM FOUND HYDRAULIC CUTOFF SWITCH ON PILOT'S COLLECTIVE TO BE INTERMITTENT AND PUTTING SYSTEM INTO BYPASS AND LOCKING THE CONTROL SERVOS. AFTER REPLACING THE SWITCH THE AIRCRAFT OPERATED NORMALLY. 1G71 3U3 U H9EU E19EU 20030328000302003032800030EU 2003 3 28 49201 120030325A7120 MOUNT AMD FALC20FALCON200 2730150EU GARRTTATF3 ATF3* 29002WP ENGINE CRACKED E ERYAK NONE O OTHER ININSP/MAINT 1 CE07412AB5261 492 P20138 DURING THE PERFORMANCE OF A 600 ENGINE INSPECTION, FOUND CRACKS AROUND ENGINE MOUNTING PADS IN THE MID-FRAME. A LOANER ENGINE IS BEING INSTALLED, WHERE THE AFFECTED ENGINE IS BEING SENT TO GARRETT FOR EVALUATION. 2L72 4F4 FRTA7EU E7WE 20030328000312003032800031 2003 3 28 811AV032403 420030324A34257011702933 CONTROL PANEL AMD FALC90FALCON900EX 2730009EU GARRTTTFE731TFE73160 NE COCKPIT SMOKE C O OTHER O OTHER NRNOT REPORTED 1 EA25811AV 64 74 DURING CLIMB, CREW SMELLED A BURNING ODOR AND SMOKE IN THE VICINITY OF FLIGHT GUIDANCE CONTROL PANEL. CREW TURNED OFF BACK LIGHTING TO PANEL, SMOKE AND ODOR DISIPATED. FLIGHT CONTINUED TO DESTINATION UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL PART NUMBER 7011702933. OPERATIONAL CHECKED GOOD. (P) 2L73 4F4 FRTA46EU E1NM 20030328000322003032800032EU 2003 3 28 ASOA03088 120030304A5412S5421230500100 FIREWALL AEROSPATR72 ATR72 EU PWA PW120 PW127 NE LT NACELLE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11630AS 336 DURING HANGER MAINTENANCE IN MCN, THE LEFT NACELLE UPPER FIREWALL WAS FOUND TO BE CRACKED WITH MATERIAL FALLING OUT. MAINTENANCE REPAIRED THE CRACKED NACELLE FIREWALL BY INSTALLING A DOUBLER IAW SRM. 2H72 4T4 TRT E20NE 20030328000382003032800038SO 2003 3 28 C2XA03TY023 120030210A532014522459003 ANGLE EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE RAMP ANGLE AT THE FWD CENTER OMEGA BEAM WAS CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000392003032800039SO 2003 3 28 C2XA03TY024 120030210A531014522460013 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE LT OMEGA BEAM AND RAMP ANGLE WERE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA; FAB FILLER, SHIM, EXTERNAL LT RAMP ANGLE IAW EMB 135/145 SRM 53-21-10. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000402003032800040SO 2003 3 28 C2XA03TY025 120030210A531314521725001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND CHAFING ON STRINGERS 19L-19R AT FRAME 53. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED BOTH AREAS IAW EMB 135/145 SRM 53-24-02. ALODINED AND PRIMED IAW EMB 135/145 CPM51-21-04;05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000412003032800041SO 2003 3 28 C2XA03TY026 120030210A322014524475003 BRACE EMB 145 EMB145LR 3260212SO NLG CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION MAINT FOUND CORROSION ON THE LT AND RT NLG BRACE CAPS. MAINTENANCE REMOVED AND REPLACED BOTH CAPS IAW EMB 135/145 AMM 32-20-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000422003032800042SO 2003 3 28 C2XA03TY027 120030210A531014525480003 SILL EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION THE CARGO DOOR SILL WAS FOUND CORROCDED. MAINTENANCE REMOVED DOOR, REMOVED THE COVER SILL, LOCATED, DRILL NEW DOOR SILL, INSTALLED DOOR PROTECTIVE STRIPS AND INSTALLED DOOR. PRESSURE CHECK WAS GOOD IAW 135/145 SRM 53-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000432003032800043SO 2003 3 28 C2XA03TY028 120030210A534714530641011 SEAT TRACK EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2715980 145202 DURING A SCHEDULED 2-C INSPECTION, MULTIBLE SEAT TRACKS HAD CORROSION. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IN THE CABIN IAW EMB 145MM-53-01-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000532003032800053NM 2003 3 28 C8GA20030005 120030227A32601061226211 DOWNLOCK BOEING727 727223 1384074NM MLG DEFECTIVE A C8GAO OTHER J WARNING INDICATION APAPPROACH 1 SO15708AA 22465 FLIGHT 705 FROM KMSP TO KTOL. ON APPROACH INTO TOLEDO, THE LEFT HAND MAIN GEAR INDICATED UNSAFE RED LIGHT ON. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL CHECKLIST A-06-4. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE LEFT HAND GEAR DOWNLOCK CARD IN THE LANDING GEAR ACCESSORY UNIT WAS REPLACED. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 32-09-121 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030328000542003032800054NM 2003 3 28 C8GA20030007 120030305A27512061121 INDICATOR BOEING727 7272A1 138407FNM TE FLAP DEFECTIVE A C8GAA UNSCHED LANDING O OTHER CLCLIMB 1 SO15286SC10 21601 FLT 723 FROM ROC TO TOL. AFTER DEPARTURE, DURING FLAP RETRACTION THE OUTBOARD FLAP INDICATOR INDICATED ASYMMETRY BETWEEN THE FLAP FIVE DEGREE AND TWO DEGREE POSITION. ACCOMPLISHED THE APPROPRIATE CHECKLIST AND RETURNED TO ROC AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND THE OUTBOARD FLAP POSITION INDICATOR WAS REPLACED. OPERATIONAL CHECKS WERE ACCOMPLISHED IAW MM 27-52-21 AND THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 20030328000592003032800059NM 2003 3 28 CALA0300095 120030303A5311 FRAME BOEING737 737924 13848A1NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0937409 30126 THE GROUND POWER CABLE CONNECTOR SHORTED TO THE FUSELAGE STRUCTURE AT THE RECEPTACLE CUTOUT. THE FRAME WEB AT STA 235.8, WL 180 WAS FOUND TO HAVE HEAT DAMAGE. THE AREA WAS REPAIRED IAW ECRA 5311-01146. 2L74 4F RTA16WE 20030328000602003032800060NM 2003 3 28 CALA0300098 120030216A5320 PAN BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917309 23360 INSPECTION FOUND LAV FLOOR PAN FASTENER CORRODED AT STA 1016, RBL 13. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-20-02. 2L72 4F RTA16WE 20030328000612003032800061NM 2003 3 28 CALA0300105 120030307A335020121 CHARGER BOEING757 757224 1384958NM CABIN INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW0918112 27302 INSPECTION FOUND EMERGENCY LIGHTS AT SEATS 12-16 INOPERATIVE. THE EMERGENCY LIGHT BATTERY CHARGER WAS REPLACED AND THE LIGHTS TESTED GOOD. 2L72 4F RTA2NM 20030328000622003032800062 2003 3 28 CALA0300106 420030308A2565100503115 LIGHT DOUG DC9 DC982 3022082WP TAILCONE SLIDE INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW091781242094 49250 THE TAILCONE SLIDE LIGHT FAILED BATTERY TEST. THE SLIDE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 25-62-01. 2L72 4F A6WE 20030328000632003032800063WP 2003 3 28 CALA0300107 120030308A5350 CABLE DOUG DC9 DC982 3022082WP TAILCONE OUT OF RIG A CALAK NONE O OTHER ININSP/MAINT 1 SW0917812 49250 THE TAILCONE FAILED TO DROP WITHIN SPECIFICATIONS AT ALL THREE POSITIONS DURING FUNCTIONAL TEST. THE PULL EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW 53-53-00. 2L72 4F A6WE 20030328000642003032800064NM 2003 3 28 CALA0300110 120030310A335020121 CHARGER BOEING737 737524 1384721NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914605 27318 INSPECTION FOUND FIRST CLASS CABIN SEATS WITH EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE DURING "A" CHECK. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-02. 2L72 4F RTA16WE 20030328000652003032800065NM 2003 3 28 CALA0300112 120030312A3397 WIRE BOEING757 757224 1384958NM ROW 16 LEFT BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0933103 27293 INSPECTION FOUND EMERGENCY PATH LIGHTS FROM ROW 8-26 INOPERATIVE. MAINTENANCE FOUND WIRING BROKEN AT ROW 16 LEFT AND FUSES BLOWN AT BATTERY PACK ROW 9 RT. THE DAMAGED WIRING WAS REPAIRED IAW WDM 33-51-15 AND 33-51-14. REPLACED BLOWN FUSES ON M736 AND M10919. ALLWIRING REPAIRED IAW STANDARD PRACTICES CHAPTER 20. OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-00. 2L72 4F RTA2NM 20030328000662003032800066NM 2003 3 28 CALA0300118 120030314A5542 SKIN BOEING737 7373T0 1384582NM RUDDER DEBONDED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916310 23361 INSPECTION FOUND LT RUDDER T/E SKIN DISBONDING IN THIRD LAYER OF EXISTING REPAIR 28 INCHES FROM LOWER END. A REPAIR WAS INSTALLED IAW ECRA 5540-01163. 2L72 4F RTA16WE 20030328000672003032800067NM 2003 3 28 CALA0300133 120030320A5321 PRESSURE PANEL BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW2712313 23364 INSPECTION FOUND A 1 INCH CRACK IN RT PRESSURE DECK AT STA 664. REPAIRED IAW SRM 53-60-51. 2L72 4F RTA16WE 20030328000682003032800068WP 2003 3 28 CALA0300134 120030321A5311 FRAME DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914840 49580 INSPECTION FOUND A 1/2 INCH CRACK IN CANTED FRAME CAP AT STA 1446, L3R. REMOVED AND REPLACED CAP IAW SRM 51-30-2. 2L72 4F A6WE 20030328000692003032800069NM 2003 3 28 CALA0300135 120030321A5320 SUPPORT BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 INSPECTION FOUND LT AFT LAV FORWARD WALL SUPPORT HAT SECTION CORRODED AT NUT PLATES. INSTALLED A NEW SECTION OF WALL SUPPORT HAT SECTION IAW SRM 51-40-01. 2L72 4F RTA16WE 20030328000702003032800070NM 2003 3 28 CALA0300142 120030325A5311 FRAME BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 208. 2L72 4F RTA16WE 20030328000712003032800071NM 2003 3 28 CALA0300143 120030325A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED IN TWO LOCATIONS: STABILIZER STATION 107.5 AND 289.1. THE AREAS WERE REPAIRED IAW SRM 55-10-1, FIGURE 203, SHEETS 1 & 2. 2L72 4F RTA16WE 20030328000722003032800072NM 2003 3 28 CALA0300144 120030326A5230 SKIN BOEING737 737524 1384721NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916618 27331 INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN DENTED. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030328000742003032800074NM 2003 3 28 CH1A200381009 120030323A3350 COVER BOEING727 7272S7 138407ZNM EMERGENCY LIGHT MISSING A C1HAK NONE O OTHER ININSP/MAINT 1 GL15681CA 22020 EMERGENCY EXIT LIGHT IN OVERWING EXIT IS MISSING COVER A/C LEFT 2L73 4F A3WE 20030328000752003032800075NE 2003 3 28 CH1A200382005 220030324A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A C1HAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 GL15682CA 22019 ON APPROACH TO LAS AT 500FT, NR 2 ENGINE COMPRESSOR STALLED. DID NOT USE NR 2 REVERSER. FLT ATTND REPORTED COMP STALL ON ROLL OUT 2L73 4F4 F A3WE E2EA 20030328000802003032800080 2003 3 28 CNMA200300001 420030117A25655WD230100201 SLIDE DOUG DC10 DC1030 3023501WP CABIN DISLODGED A CNMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0759083 20760 47926 WHILE AT GATE FLIGHT ATTENDANT OPENED R-1 DOOR WITHOUT DISARMING DOOR. SLIDE CAME OUT OF ITS CONTAINER AND LANDED ON TOP OF CATERING TRUCK AWAITING TO DELIVER. APPARENTLY SLIDE DID NOT FALL FAR ENOUGH TO ACTIVATE DEPLOYMENT MECHANISM. SLIDE WAS REMOVED AND REPLACED, SLIDE BEING SENT IN TO CHECK AND OVERHAUL. (P) 2L73 4F A22WE 20030328000912003032800091EA 2003 3 28 COMA0360164 120030321A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002B19 1900309EA E&E BAY DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01960CA 7117 FLIGHT 9492 AVIONICS DOOR CAUTION MESSAGE AT 8000 FT. ADJUSTED THE AVIONICS DOOR PROXIMITY SENSOR. 2L72 4F RTA21EA 20030328000922003032800092EA 2003 3 28 COMA0370009 120030322A291067075296001 LINE CNDAIRCL600 CL6002C10 1390015EA NR 2 HYD SYS LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01354CA930 10064 FLIGHT 5741 - NR 2 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPAIRED CHAFED HYDRAULIC TUBING IN AFT EQUIP BAY. 2L72 4F RTA21EA 20030328000972003032800097EU 2003 3 28 CX7A194J29 120030203A26131734362450 SENSOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03302CE 340B193 TAILPIPE HOT CWP ON LEFT ENGINE DURING T/O ROLL. ABORTED T/O. 2L72 4T RTA52EU 20030328000982003032800098EU 2003 3 28 CX7A194J30 120030203A26131734362450 SENSOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A CX7AC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03300CE 340B184 RT TAILPIPE HOT OCCURRED ON TAKEOFF AT APPROX 150 FEET AGL. DID AIR RETURN. 2L72 4T RTA52EU 20030328000992003032800099EU 2003 3 28 CX7A194J31 120030222A26121734362450 SENSOR SAAB SF340 340B 7860101EU RT TAILPIPE CONTAMINATED A CX7AEC ENGINE SHUTDOWN ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL03306CE 340B203 RT ENGINE TAIL PIPE HOT WARNING CAME ON SHORTLY AFTER T/O REMAINED ON AFTER ENGINE SHUTDOWN 2L72 4T RTA52EU 20030328001002003032800100EU 2003 3 28 CX7A194J32 120030304A26121734362450 SENSOR SAAB SF340 340B 7860101EU LT TAILPIPE CONTAMINATED A CX7ACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL03306CE 340B203 LT TAILPIPE HOT LIGHT DURING T/O AT 200 FT REPORTED BY CREW 2L72 4T RTA52EU 20030328001052003032800105EU 2003 3 28 DHL2003362002 120030113A2612 CONNECTOR AIRBUS300 A300B4203 3930306EU NR 2 ENGINE FAILED A DHLAK NONE N FALSE WARNING ININSP/MAINT 1 SO01362DH 84 ENGINE NR 2 LOOP A-LIGHT ILLUMINATED ON PREFLIGHT. RERACKED DETECTOR CONNECTOR PLUG ON CONTROL UNIT IAW A300 M/M 26-12-11. CLEANED LOOP-B AND LOOP A-FAN CASE CONNECTORS IAW A300 M/M 26-12-12. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030328001062003032800106EU 2003 3 28 DHL2003362003 120030113A2612 CONNECTOR AIRBUS300 A300B4203 3930306EU NR2 FIRE LOOP LOOSE A DHLAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO01362DH 84 ENGINE NR 2 LOOP A-LIGHT ILLUMINATED INTERMITTENTLY ON GROUND AFTER LANDING. CLEANED ALL A-LOOP CONNECTOR PLUGS ON FAN, CORE, AND PYLON ON NR 2 ENGINE. FOUND LOOP CLAMP ON LOOP UNFASTENED. REFASTEN CLAMP. OPS CHECKED GOOD IAW 26-12-00 PAGE 6. 2L72 4F RTA35EU 20030401000012003040100001EU 2003 4 1 00086 120030326A33109993 CONTROL PANEL AMD FALC20FALCONE 2720305EU COCKPIT FAILED E HAEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW05285TW 285 PILOT REPORTED DURING CLIMB AT FL290 ELECTRICAL SMOKE IN COCKPIT REQUESTED RETURN TO DEPARTURE AIRPORT ADS, ISOLATED NR 1 ELECTRICAL SYSTEM AND SMOKE DECREASED, REMAINDER OF FLIGHT UNEVENTFUL. WILL UPDATE THIS REPORT AFTER MAINTENANCE. REMOVED AND REPLACED FAILURE WARNING PANEL. OPS CHECK GOOD. 2L72 4F A7EU 20030331000082003033100008EA 2003 3 31 03086628 120030327A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK AT SEAT ROW 1 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CONNECTOR FOR THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030331000102003033100010EU 2003 3 31 03FDEA00355 120030328A7830 PANEL AIRBUS310 A310 EU THRUST REVERSER PEELING A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 1 ENGINE OUTBOARD THRUST REVERSER TRANSLATING PANEL UPPER SLIDER TEFLON PEELING UP, AND SLIDER DAMAGED. 2L72 4F RTA35EU 20030625001292003062500129EU 2003 6 25 03FDEA00356 120030328A5410 PANEL AIRBUS310 A310 EU NR 2 NACELLE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 2 ENG I/B TRANSLATING COWL UPPER T- TRACK SLIDER CRACKED OFF. INSTALLED NEW UPPER SLIDER WITH NEW TRANSLATING SLEEVE W/C NOO193 2L72 4F RTA35EU 20030625001252003062500125EU 2003 6 25 03FDEA00357 120030321A5510 SPAR CAP AIRBUS310 A310 EU HORIZONTAL STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 LT HORIZONTAL UPPER AFT SPAR CAP CORRODED APPROX. 4FT. FROM FUSELAGE. UNDER MAE W/O NO. 13350. REPAIRED AFT SPAR CAP IAW SRM 55-13-11 AND SRM 51-41-01. 2L72 4F RTA35EU 20030331000112003033100011EU 2003 3 31 03X03038751 120030310A27201379013E401 ARM BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RUDDER CRACKED A O3XAK NONE O OTHER ININSP/MAINT 1 SO03875AE19935400 875 DURING A SCHEDULED INSPECTION THE RUDDER QUADRANT DRIVE ASSEMBLY WAS FOUND CRACKED AT THE RUDDER FEEL SPRING ATTACH ARM. THE FEEL SPRING ATTACH ARM IS ATTACHED IN TWO SECTIONS TO THE RUDDER QUADRANT, ONE SECTION WAS CRACKED ALL THE WAY THROUGH. IF THE ATTACH FEEL CONTROL ARM CONTINUED TO CRACK THE REMAINING WAY THROUGH, THIS CONDITON COULD CAUSE LOSS OF YAW CONTROL. 2L72 4T4 TRTA56EU E4WE 20030331000132003033100013EU 2003 3 31 136821 120030330A3246175K882 TIRE SAAB SF340 SF340A 7850100EU NLG WORN A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL1719XS 340A019 FLT 4511 DURING TAKEOFF ROLL PILOT REPORTED THAT THE NOSE WHEELS HAD SEVERE VIBRATION TAKE OFF ABORTED AIRCRAFT RETURNED TO GATE MAINTENANCE INSPECTED NOSE GEAR AND FOUND NO DEFECTS TIRES WERE FLAT SPOTTED AND REPLACED PER SF340 M/M AIRCRAFT RELEASED FOR SERVICE 2L72 4T RTA52EU 20030331000152003033100015EA 2003 3 31 2003F00167 120030213A270060093000103 CONTROL UNIT CNDAIRCL600 CL6002B16 1900305EA RT WING INTERMITTENT A O2GAO OTHER F FLT CONT AFFECTED LDLANDING 1 NE03601VH 5043 FLAPS STOPPED AT 2 DEGREES POSITION WHEN FLAPS SELECTED TO 20 DEGREES. RESET CONVETERS AT FLAP CONTROL UNIT. FLAPS OPERATED NORMALLY FOR REMAINDER OF FLIGHT. CHANGED FLAP BDU. AIRCRAFT RETURNED TO SERVICE WITH NO PROBLEMS. (M) 2L72 4F RTA21EA 20030331000172003033100017EA 2003 3 31 A6WA200340023 120030106A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 OBLIQUE ANGLE AT FS 625 LT SIDE IS CRACKED ONE INCH IN RADIUS. REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 LT SIDE WITH NEW. 2L72 4F RTA21EA 20030331000182003033100018EA 2003 3 31 A6WA200340024 120030106A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 HYDRAULIC BRACKET AT FS 656 LT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED, REPAIRED, AND INSTALLED BRACKET. NDT PERFORMED, NO INDICATIONS NOTED. 2L72 4F RTA21EA 20030331000212003033100021EA 2003 3 31 A6WA200340027 120030106A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 OBLIQUE ANGLE AT FS 625 RT SIDE IS CRACKED 1 INCH IN RADIUS REMOVED AND REPLACED CRACKED OBLIQUE ANGLE AT FS 625 RIGHT SIDE. 2L72 4F RTA21EA 20030331000292003033100029WP 2003 3 31 AALA20030036 120030108A3260833703 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A AALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW21241AA 49254 ORD - FLT 357 - EN ROUTE LGA-ORD, UNSAFE NOSE GEAR INDICATION DURING APPROACH TO ORD. GEAR WAS DOWN 3 GREEN LIGHTS ALL MECHANICAL VISUAL INDICATION AGREE, ON SHORT FINAL. RECEIVED AUDIO LANDING GEAR ALONG WITH A RED LIGHT IN THE NOSE GEAR. THIS HAPPENED 304 TIMES WITH A QUICK FLASH OF THE RED LIGHT. DID A GO-AROUND AND CYCLED THE GEAR, ALL INDICATIONS WERE NORMAL AND THE NOSE GEAR FLASHED RED ONE TIME. LANDED ORD WITHOUT INCIDENT. SENSOR BAD, REPLACED NOSE GEAR DOWNLOCK SENSOR. SWUNG GEAR 4 TIMES. NO FAULTS NOTED. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000302003033100030WP 2003 3 31 AALA20030037 120030108A3260 DOWNLOCK SENSOR DOUG DC9 DC982 3022082WP MLG DEFECTIVE A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW21465A 49595 ORD - FLT 854 - EN ROUTE FLL-ORD, ON APPROACH ORD, AFTER PUTTING LANDING GEAR HANDLE DOWN. RGHT GEAR WARNING LIGHT ILLUMINATED. USED MANUAL GEAR EXTENSION TO EXTEND LANDING GEAR. GEAR SHOWED DOWN AND LOCKED. LANDED ORD WITHOUT INCIDENT. REPLACED D1-27 SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000312003033100031WP 2003 3 31 AALA20030038 120030112A2822 SCREW DOUG DC9 DC983 3022083WP BOOST PUMP LOOSE A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW2176202 53292 EN ROUTE LGB-DFW, AT 24,000 FEET SMALL FUEL LEAK NOTICED. NO DISCREPANCY IN FUEL BURN OR IMBALANCE. CLIMBED TO 33,000 FEET AND LEAK INCREASED TO A STEADY STREAM. DECLARED EMERGENCY, DIVERTED TO ELP AND LANDED WITHOUT INCIDENT. RETORQUED BOOST FUEL PANEL SCREWS TO BOOST PUMP. PANEL UNDER HEATER BLANKET. LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000322003033100032WP 2003 3 31 AALA20030039 120030108A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21463AA 49593 DURING OVERNIGHT MAINTENANCE, FORWARD LT AND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000332003033100033WP 2003 3 31 AALA20030040 120030109A3397 WIRE DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW217521A 49898 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN SEATS 8F AND 12F INTERMITTENT. CLEANED AND SECURED EMERGENCY EXIT LIGHT GROUND WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000342003033100034WP 2003 3 31 AALA20030042 120030109A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21487AA 49680 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000352003033100035WP 2003 3 31 AALA20030045 120030112A212160529042 FAN DOUG DC9 DC982 3022082WP ACM BAY FAILED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21454AA 49559 EN ROUTE DEN-DFW, ON TAKEOFF ROLL, HEAR A FAN TYPE NOISE SIMILAR TO INSTRUMENT COOLING FAN CYCLING ON/OFF SEVERAL TIMES. PAST V1 HAD BLAST OF AIR AND SAW SMOKE (GRAY) IN COCKPIT WITH PACK FLOW OFF. TURNED LEFT PACK OFF, SMOKE STOPPED IMMEDIATELY. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. INSPECTED COCKPIT, CABIN AND TAIL SECTION OF AIRCRAFT. NO SMOKE OR ODOR DETECTED. REPLACED LT PACK HEAT EXCHANGER COOLING FAN. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000362003033100036WP 2003 3 31 AALA20030060 120030114A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21476AA 49651 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS OVER WALKWAY IN TAIL COMPARTMENT INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT BATTERY FOR TAILCONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000372003033100037WP 2003 3 31 AALA20030061 120030114A335060030451 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21205AA 49155 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING SIGN AT ROW 21 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000412003033100041WP 2003 3 31 AALA20030184 120030208A21205953625521 DUCT DOUG DC9 DC982 3022082WP TAIL CRACKED A AALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW21203AA 49145 EN ROUTE MIA-IAH, ON CLIMB-OUT, PASSING 14,000 FT, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LEVELED AIRCRAFT AT 16,000 FT AND ACCOMPLISHED PROCEDURE. WITH HIGH PRESSURE BLEED OFF, THE LIGHT EXTINGUISHED. RETURNED MIA WITHOUT INCIDENT. AFTER LANDING, IT WAS NOTED THAT THE GROUND INSTRUMENT COOLING FAN WAS NOT IN OPERATION. REPLACED WATER SEPARATOR DUCT. PERFORMED LEAK CHECK, NO LEAKS NOTED. PERFORMED OPERATIONS CHECK OF TAIL COMPARTMENT OVERHEAT SYSTEM. NO FAULTS NOTED. ALSO, ACCOMPLISHED GROUND CHECK OF INSTRUMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000452003033100045WP 2003 3 31 AALA20030199 120030216A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21475AA 49650 DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS OVER SEATS 21-27 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000462003033100046WP 2003 3 31 AALA20030200 120030216A3350 CONTACTOR DOUG DC9 DC982 3022082WP CABIN DIRTY A AALAK NONE L NO TEST ININSP/MAINT 1 SW21476AA 49651 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT L2 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000472003033100047WP 2003 3 31 AALA20030209 120030219A3350 BALLAST DOUG DC9 DC982 3022082WP CABIN BURNED OUT A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21249AA 49269 EN ROUTE MIA-CLT, IMMEDIATELY AFTER TAKEOFF, NR 1 FLIGHT ATTENDANT CALLED AND SAID THE CABIN WAS FILLING UP WITH SMOKE. CREW CHECKED BOTH LAVATORIES AND THOUGHT SMOKE WS COMING FROM UPPER SIDEWALL VENTS. SHUT OFF BOTH PACKS AND RECIRCULATION FAN. SMOKE SEEMED TO DISSIPATE. RETURNED AND LANDED MAI IMMEDIATELY. NR 1 FLIGHT ATTENDANT COULD NOT SEE PAST ROW 14 FROM AT FORWARD ENTRY DOOR. PASSENGERS SAID IT SMELLED LIKE ELECTRICAL. SMOKE SEEMED TO BE COMING FROM AROUND ROW 29B. REPLACED LIGHT BALLAST. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000492003033100049WP 2003 3 31 AALA20030212 120030218A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21403A 49314 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000502003033100050WP 2003 3 31 AALA20030222 120030223A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21490AA 49683 DURING OVERNIGHT MAINTENANCE, ALL EMERGENCY EXIT LIGHTS AT TAIL CONE AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000512003033100051WP 2003 3 31 AALA20030229 120030222A2612 WARNING SYSTEM DOUG DC9 DC983 3022083WP E&E BAY DEFECTIVE A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW21571AA 49353 EN ROUTE ACA-ORD, DURING CLIMB, RECEIVED INTERMITTENT APU AURAL WARNING, NO LIGHTS. WARNING STOPPED BUT AFTER LEVEL OFF AT 29,000 FT WARNING STARTED AGAIN. RECEIVED RT ENGINE FIRE WARNING (AGAIN NO LIGHTS). LANDED MEX WITHOUT INCIDENT. INSPECTED AND CHECKED ENGINE AND APU FIRE DETECTION SYSTEM, NO FAULTS NOTED. REPLACED CENTRAL AURAL WARNING UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000522003033100052WP 2003 3 31 AALA20030230 120030221A2163 SENSOR DOUG DC9 DC982 3022082WP ACM BAY LEAKING A AALAG O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW21418AA 49329 AT CRUISE AT 33,000 FT, CREW SELECTED TAIL DE-ICE CABIN PRESSURE WOULD START TO DESCEND AT ABOUT 300 FT PER MINUTE. CREW RAN CHECKLIST AND WERE ABLE TO CORRECT PROBLEM. CABIN STARTED TO CLIMB AT ABOVE 1,000 FT PER MINUTE. AGAIN CREW WENT THROUGH CHECKLIST AND WERE ABLE TO STOP CLIMB BY TIME CABIN WAS PASSING 8,000 FT. CREW DECLARED AN EMERGENCY AND DEPLOYED OXYGEN MASKS. AIRCRAFT DESCENDED TO 9,000 FT AND CREW WAS ABLE TO CONTROL CABIN AND CLIMBED BACK UP TO 15,000 FT. LANDED TPA WITHOUT INCIDENT. REPLACED LT AIR CONDITIONING SUPPLY HIGH TEMP SENSOR AND GASKET. ACCOMPLISHED AIRFOIL ANTI-ICE TEST. ACCOMPLISHED CABIN DECAY TEST AND FOUND TO BE WITHING LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)2L72 4F A6WE 20030331000532003033100053WP 2003 3 31 AALA20030244 120030225A3397 CONNECTOR DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 4D INOPERATIVE. INSERTED EMERGENCY EXIT LIGHT PIN IN CONNECTOR ON PLUG TO SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000552003033100055WP 2003 3 31 AALA20030249 120030227A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21474 49649 DURING OVERNIGHT MAINTENANCE, AFT TAIL CONE EMERGENCY EXIT LIGHTS INOPERATIVE. REATTACHED EMERGENCY EXIT LIGHT BATTERY FOR TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000562003033100056NE 2003 3 31 ABXA030120 220030318A7200 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 DEFECTIVE A ABXAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 GL23818AX2148 46075 671350 ON CLIMBOUT, THE NR 4 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 4 OIL PRESSURE NOTED TO BE 32 PSI. WHEN POWER REDUCED, OIL PRESSURE WAS 20 PSI. SHUT DOWN THE NR 4 ENGINE AT 1036Z. WINDMILLING OIL PRESSURE 8-10 PSI IN CLIMB AND CRUISE. AIRCRAFT FERRIED TO ILN WHERE MAINTENANCE REPLACED THE NR 4 ENGINE IAW JOB CARD 8090507 AND DC-8 MM. TRIMMED ENGINE IAW DC8-8A AND 8B. 2L74 4F4 F 4A25 1E8 20030331000572003033100057CE 2003 3 31 AMWA17 120030305A5346 FINGER DOUBLER BEECH 1900 1900D 1154162CE RT ENG TRUSS CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07237YV UE237 WHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030331000582003033100058CE 2003 3 31 AMWA18 120030305A5346 PLATE BEECH 1900 1900D 1154162CE LT ENG TRUSS DAMAGED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07237YV UE237 WHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE PER THE STANDARD REPAIR MANUAL 57-95-02. NO TEARDOWN REPORT WILL BE REQUIRED. 2L72 4T RTA24CE 20030331000652003033100065NE 2003 3 31 ASOA03089 220030306A7261 O-RING AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE LT ENGINE FAILED A ASOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11532AS 458 DURING CLIMB OUT, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE QRH, SHUT THE LT ENGINE DOWN AND DECLARED AN EMERGENCY. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE OIL FILTER O-RING ON THE LT ENGINE AND ADDED THREE QUARTS OF OIL. ALSO, THE REDUCTION GEAR BOX AND MAIN OIL TANK CHIP DETECTORS WERE PULLED FOR POSSIBLE FOREIGN OBJECT DAMAGE. NO DAMAGE WAS FOUND. THE ENGINE RUN AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT OK FOR SERVICE. 2H72 4T4 TRTA53EU E20NE 20030331000662003033100066EA 2003 3 31 ASOA03090 120030307A21707536893 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE ACM ODOR A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11880AS 200108160 7606 DURING DESCENT INTO MOB, AFTER STARTING THE AUXILLARY POWER UNIT AND SWITCHING THE BLEEDS, A FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN. THE FUEL ODOR DISSIPATED AFTER SHUTTING THE AUXILIARY POWER UNIT DOWN. THE AIRCRAFT SAFELY IN MOB. MAINTENANCE REMOVED AND REPLACED BOTH COALESCER BAGS ON THE AIR CYCLE MACHINE. ALSO, BOTH ENGINES WERE RAN WITH THE ENGINE BLEEDS CYCLED ON AND OFF, AND THE AUXILIARY POWER UNIT WAS SHUT DOWN AND RE-STARTED WITH THE ENGINES RUNNING. NO FUEL ODOR WAS NOTED. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030331000672003033100067EA 2003 3 31 ASOA03091 120030308A2750 SEAL CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE WING CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11874AS SBRJ614 7551 DURING HANGAR MAINTENANCE, THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE IAW SRM. 2L72 4F4 FRTA21EA E15NE 20030331000682003033100068EA 2003 3 31 ASOA03092 120030308A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE FUSELAGE CRACKED A ASOAO OTHER O OTHER NRNOT REPORTED 1 SO11874AS 7551 DURING HANGER MAINTENANCE, THE LT ANGLE BRACKET UNDER THE ENGINE SUPPORT BEAM FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ANGLE BRACKET UNDER THE ENGINE SUPPORT BEAM FRAME IAW SRM. 2L72 4F4 FRTA21EA E15NE 20030331000692003033100069EA 2003 3 31 ASOA03093 120030308A2120 ODOR CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* NE CABIN DETECTED A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11880AS 7606 DURING DESCENT, A STRONG FUEL ODOR OCCURRED IN THE COCKPIT AND CABIN WHEN THE BLEEDS WERE SWITCHED FROM THE ENGINE TO THE AUXILIARY POWER UNIT. THE AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTED THE AUXILIARY POWER UNIT FOR LEAKS AND RAN BOTH ENGINES WHILE TRANSFERRING THE RT ENGINE BLEEDS TO THE AUXILIARY POWER UNIT SEVERAL TIMES. THE FUEL ODOR DID NOT REOCCUR. OPERATIONAL CHECKS GOOD. AIRCRAFT, OK FOR SERVICE. 2L72 4F4 FRTA21EA E15NE 20030331000742003033100074EU 2003 3 31 AWXA200300317 120030313A5315D53472075000 FLOORBEAM AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 DURING C-03 CHECK CORROSION WAS FOUND AT 6 EACH NUT PLATES ON LOWER SURFACE OF FLOORBEAM BETWEEN FR 66+10 AND FR 68, LBL 57, Y1732. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED AREA OF FLOORBEAM BETWEEN FR 66+10 AND FR 68, LBL 57, Y1732; FABRICATED 2 EACH FILLERS AND A REPAIR ANGLE; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, PG. 202-213, FIG. 201. 2L72 4F RTA28NM 20030331000752003033100075EU 2003 3 31 AWXA200300318 120030326A5210FE1740011 DAMPER AIRBUS320 A320231 3930325EU PAX DOOR LEAKING A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW42143 082 DURING C-03 CHECK THE L-2 DOOR DAMPER ASSEMBLY WAS FOUND LEAKING. MAINTENANCE REMOVED AND REPLACED THE L-2 DAMPER ASSEMBLY IAW AMM TASK 52-13-14-400-001, OPERATIONAL CHECK WAS GOOD. VENDOR CONFIRMED FAILURE OF DAMPER CYLINDER ASSEMBLY S/N 280 FINDING LEAKAGE THE FRONT AND REAR CUPS DUE TO WORN SEALS. DETERIORATED SEALS WERE ALSO FOUND ON THE PERCUSSION AND BOTTLE ASSEMBLY. REPLACED ALL WORN PARTS AND COMPLIED WITH S/B'S FE174-52-2 & 3R1, P/N CHANGED TO FE174-004. 2L72 4F RTA28NM 20030331000762003033100076NM 2003 3 31 AWXA200300319 120030327A2910R291206EE0250T HOSE BOEING737 7373Q8 1384670NM RT MLGWW BURST A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28327AW 23507 ON CLIMB OUT FROM DEN EN ROUTE FOR PHX, THE RT MAIN LANDING GEAR INDICATED BOTH RED AND GREEN, ACCOMPANIED BY HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS. DECLARED EMERGENCY AND TURNED BACK TO DEN, LANDED WITHOUT FURTHER EVENT. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND RT MAIN LANDING GEAR PRESSURE LINE RUPTURED. AWA MAINTENANCE TECHNICIANS DISPATCHED FROM PHX. 2L72 4F RTA16WE 20030331000772003033100077NM 2003 3 31 AWXA200300320 120030317A5312651630086 FRAME BOEING737 7373S3 1384711NM 178 BULKHEAD CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON LT SIDE FRAME OF 178 BULKHEAD, WL 195. MAINTENANCE REMOVED DAMAGED SIDE FRAME, 178 BULKHEAD, WL 195; FABRICATED A NEW REPLACEMENT SIDE FRAME PER DWG 65-16300; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG. 3 & 6. 2L72 4F RTA16WE 20030331000782003033100078NM 2003 3 31 AWXA200300321 120030324A53206545834551 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030331000792003033100079NM 2003 3 31 AWXA200300322 120030315A5320651630534 ANGLE BOEING737 7373S3 1384711NM FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK CORROSION WAS FOUND ON ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW. MAINTENANCE REMOVED CORRODED ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65-16305; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12. 2L72 4F RTA16WE 20030331000802003033100080NM 2003 3 31 BJNA030220 120030228A5730 SKIN BOEING737 737282 13844ATNM LT WING CORRODED A BJNAO OTHER O OTHER NRNOT REPORTED 1 WP11789TM46481 23046 DURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE LT WING OUTBOARD BOOST PUMP CUTOUT AREA. BLENDED OUT THE CORROSION, HOWEVER THE REMAINING MATERIAL THICKNESS WAS BELOW MINIMUM REQUIRED, AND THE CUT OUT OF MATERIAL WAS BEYOND SRM LIMITS. FABRICATED AND INSTALLED REPAIR FILLERS IAW SRM. 2L72 4F RTA16WE 20030331000862003033100086SO 2003 3 31 C2XA03SH063 120030329A531014521721005 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE RT BUTT STRAP AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000872003033100087SO 2003 3 31 C2XA03SH064 120030329A531014521721005 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE CENTER BUTT STRAP BETWEEN FRAMES 14 AND 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 53-20-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000882003033100088SO 2003 3 31 C2XA03SH065 120030329A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 SHV-DURING C-CHECK, REPAIR DOUBLER ON T-REINFORCEMENT ON STRINGER 19 RIGHT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000892003033100089SO 2003 3 31 C2XA03SH066 120030329A531314528737001 STRINGER EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, REPAIR DOUBLER ON TEE REINFORCEMENT ON STRINGER 19 LT WAS FOUND TO HAVE A GOUGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000962003033100096NM 2003 3 31 CALA0300145 120030327A5230 SKIN BOEING737 7373T0 1384582NM CARGO DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND AFT CARGO DOOR SKIN DENTED BETWEEN STA 816 AND 819. REPAIRED DOOR IAW SRM 52-00-01, FIGURE 203. 2L72 4F RTA16WE 20030331000972003033100097NM 2003 3 31 CALA0300146 120030327A5512 SKIN BOEING737 7373T0 1384582NM HORIZONTAL STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED IN FOUR PLACES FROM STA 231-272. THE SKIN WAS REPAIRED IAW SRM 55-10-01, FIGURE 203. 2L72 4F RTA16WE 20030331000982003033100098NM 2003 3 31 CALA0300147 120030327A5320 FLOOR SUPPORT BOEING737 737524 1384721NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917619 27332 INSPECTION FOUND A 4 INCH CRACK IN FLOOR SUPPORT AT STA 344, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-40-3. 2L72 4F RTA16WE 20030331000992003033100099NM 2003 3 31 CALA0300148 120030327A3260 CABLE BOEING737 737524 1384721NM RT MLG OUT OF RIG A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0918622 27526 THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM EWR. APPROPRIATE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN GEAR AIR/GROUND SENSE TELEFLEX CABLE OUT OF ADJUSTMENT DURING MAIN GEAR SAFETY SENSOR CHECK. THE TELEFLEX CABLE WAS ADJUSTED IAW MM 32-09-01 AND 27-62-51. GROUND SPOILERS CHECKED GOOD. ALL CONNECTIONS WERE LUBRICATED. SYSTEM OPERATIONS CHECKS WERE GOOD. GEAR RETRACTION WAS GOOD IAW MM 32-32-00. 2L72 4F RTA16WE 20030331001002003033100100 2003 3 31 CALA0300149 420030327A25655262100 ACTUATOR BOEING767 767224 1385170NM SLIDE INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW097615110116 30430 THE FORWARD AND AFT DOOR ACTUATORS FOR THE RT SIDE OFF-WING SLIDE DOOR WERE FOUND EXPENDED. THE DOOR ACTUATORS WERE REMOVED AND REPLACED IAW MM 25-65-10. 2L72 4F RTA1NM 20030331001012003033100101NE 2003 3 31 CH1A200381010 220030327A7200 ENGINE BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 STALLED A C1HAC ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 GL15681CA 22020 ON TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED NR 2 EPR DROPPED TO 1.2 AUTO PACK TRIP SYSTEM ACTIVATED 2L73 4F4 F A3WE E2EA 20030331001052003033100105EU 2003 3 31 DHL2003362007 120030211A2611 CONTROL PANEL AIRBUS300 A300B4203 3930306EU SMOKE DETECT INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01362DH 84 ON S/O'S PANEL, AND CARGO SMOKE DETECTION PANEL, THE AFT FAULT MAGNETIC INDICATOR IS AMBER. DUCT WON'T TEST. DEFERRED IAW MEL 26-11-01-2. PLACARD INSTALLED. CONTROL 11968. REF DMI 11968 ON S/O PANEL, THE ELEC CARGO SMOKE DETECTION PANEL. THE AFT DUCT FAULT M1 IS AMBER, IT WON'T TEST. RE-RACKED THE ELECTRIC AND CARGO SMOKE DETECTOR AMPLIFIER. SYSTEM OPS CHECKED GOOD IAW A300 26-14-04. THIS CLEARS DMI 11968. PLACARD REMOVED. 2L72 4F RTA35EU 20030331001062003033100106EU 2003 3 31 DHL2003362008 120030321A2497 BUSS AIRBUS300 A300B4203 3930306EU WARNING PANEL DAMAGED A DHLAO OTHER J WARNING INDICATION APAPPROACH 1 SO01362DH 84 ON APPROACH INTO LICZ, WE HAD A ELECTRIC LIGHT ILLUMINATED ON THE MASTER WARNING PANEL AND SINGLE STROKE CHIME ASSOCIATED WITH A/C BUSS NR 1 OFF ILLUMINATED ON S/O PANEL COMPLETED ABNORMAL PROCEDURES. FOUND NR 1 A/C BUSS WARNING CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. SELECTED NR 1 A/C BUSS. BUSS POWERED TO 115VAC 400 HZ. PERFORMED CHECK OF NR 1 A/C BUSS DISTRIBUTION IAW A-300 M/M 24-50-00. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030331001072003033100107EU 2003 3 31 DHL2003362500 120030207A5311 FRAME AIRBUS300 A300B4203 3930306EU FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01362DH 84 DENT (CREASE) IN FRAME 24 BETWEEN STRINGER 8 AND 9. REMOVED WALL PANEL FOR ACCESS. CUT OUT DAMAGED AREA FROM FRAME. FABRICATED DOUBLER. INSTALLED DOUBLER 0.50, CLEANED AREA. REINSTALLED WALL PANEL. ALL WORK DONE PER A 300 SRM 53-10-10 PG 269-270. 2L72 4F RTA35EU 20030331001092003033100109EU 2003 3 31 DHL2003363002 120030326A3242C200601004 BRAKE AIRBUS300 A300B4203 3930306EU MLG FAILED A DHLAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO01363DH 85 AFTER T/O & NORMAL GEAR RETRACTION, HOT BRAKE LIGHT ILLUMINATED. (200 DEG AND CLIMBING) FELT VIBRATION DURING EXTENSION. FOUND NR 2 TIRE BLOWN. R & R NR 1 TIRE ASSY IAW 12-37-32 (MATED TIRE). R & R NR 2 MAIN WHEEL ASSY IAW M/M 12-37-32. PERFORMED OPS CHECK OF ANTI-SKID SYSTEM IAW M/M 32-42-72. OPS CHECKED GOOD. REPLACED FAN DEBRIS GUARD AND BRAKE FAN OPS CHECKED GOOD IAW M/M 32-48-11. OK FOR SERVICE. 2L72 4F RTA35EU 20030331001102003033100110EU 2003 3 31 DHL2003364001 120030124A3240 BRAKE ASSY AIRBUS300 A300B4203 3930306EU MLG DISCHARGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01364DH 141 RT BRAKE PEDAL SOFT. BRAKES GRAB SUDDENLY. CHECKED AND FOUND RIGHT SIDE LOW PRESSURE BRAKE SYSTEM NEEDED REPLENISHED. REPLENISHED RIGHT SIDE PER M/M 12-12-32. CHECKED NORMAL. 2L72 4F RTA35EU 20030331001112003033100111EU 2003 3 31 DHL2003364003 120030202A2612 FIRE LOOP AIRBUS300 A300B4203 3930306EU NR 2 ENGINE CHAFED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01364DH 141 ENGINE NR 2 LOOP-A LIGHT ILLUMINATED. ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURES COMPLETED. DEFERRED PER MEL 26-12-01-1, DMI 11849 ASSIGNED. REF DMI 11849 - ENGINE NR 2 LOOP-A LIGHT ILLUMINATED. ENGINE OR APU LOOPS LIGHT ILLUMINATED ABNORMAL PROCEDURES COMPLETED. TROUBLESHOT FOUND WIRE BUNDLE RUBBING AGAINST A-LOOP IN HOT SECTION. REPAIRED AND SECURED WIRE BUNDLE. INSPECTED A-LOOP. NO DEFECTS NOTED RAN ENGINE AT CRUISE T/O POWER AND SYSTEM OPS CHECKED GOOD PER M/M 26-12-00. DMI CLEARED. 2L72 4F RTA35EU 20030331001132003033100113EU 2003 3 31 DHL2003367001 120030201A2710 STRUCTURE AIRBUS300 A300B4203 3930306EU AILERON VIBRATION A DHLAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO01367DH 265 CONTINUOUS MODERATE AIRFRAME VIBRATION WHEN ABOVE FLIGHT LEVEL 200 AND 250 KIAS. EMERGENCY DECLARED. RETURNED TO LAX. SUSPECT ALL-SPEED AILERONS. PERFORMED ADJUSTMENTS ON BOTH ALL-SPEED AILERONS IAW 27-10-00. GROUND OPS CHECKED GOOD AT THIS TIME. RT FUEL JETTISON VALVE FAILED TO OPEN ON PRIMARY SYSTEM. VALVE OPENED USING SECONDARY SYSTEM. CHECKED PER M/M 28-31-00. NO DEFECTS NOTED. OK FOR SERVICE. OVERWEIGHT LANDING AT 298,000 LBS. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-11. NO DEFECTS NOTED. 2L72 4F RTA35EU 20030331001172003033100117NM 2003 3 31 DHL2003720003 120030325A3231 DOOR BOEING727 727228 1384083NM MLG LACK OF LUBE A DHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01720DH 19544 NOSE GEAR WOULD NOT EXTEND ACCOMPLISHED ABNORMAL PROCEDURE AND NOSE GEAR EXTENDED. LUBRICATED ALL DOOR LATCHES AND PERFORMED GEAR SWING NUMEROUS TIMES IAW B-M/M 32-30-00. NO DEFECTS NOTED. 2L73 4F RTA3WE 20030331001212003033100121NM 2003 3 31 DHL2003740501 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD CARGO FRAME HAS 2 DENTS INTO THE RADIUS AT BS 700 STR 23 AT 24R. REMOVED FASTENERS FOR ACCESS PER SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER (7075-T6 .063 PER SRM 53-10-2 FIG 11 AND 51-40-0 FIG 1. ALODINED AND PRIMED PER SRM 51-10-2 AND INSTALLED REPAIR PER SRM 51-40-3 PG 1. 2L73 4F RTA3WE 20030331001222003033100122NM 2003 3 31 DHL2003740502 120030213A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FWD CARGO FRAME HAS 3 DENTS AT BS 700 STR 38 L. REMOVED FASTENERS FOR ACCESS PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 57-40-3. FABRICATED REPAIR 7075-T6 .063 PER SRM 53-10-3 FIG 3. ALODINED AND PRIMED PER SRM 51-10-2, INSTALLED REPAIR PER SRM 57-40-3 FIG 1. 2L73 4F RTA3WE 20030331001232003033100123NM 2003 3 31 DHL2003740503 120030204A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FUESLAGE UPPER MAIN DECK CARGO DOOR FUSLAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACH TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABRICATED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .063 PER SRM 53-10-4 FIG 1. PARTS TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-4, FIG 1 AND 51-30-2. 2L73 4F RTA3WE 20030331001242003033100124NM 2003 3 31 DHL2003740504 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 FUSELAGE FRAME AT STA 600 IS DENTED AND CRACKED BETWEEN STR 16R-17R. CUT OUT DAMAGED FRAME AND FABRICATED REPAIR FROM 7075-T6 .063. CLEANED, TREATED AND PRIMED AND INSTALLED REPAIR PER SRM 51-40-1. 2L73 4F RTA3WE 20030331001382003033100138NM 2003 3 31 DHL2003740519 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH IN FWD CARGO FRAME HAS A DENT INTO THE RADIUS AT BS 680 STR 24 LT. REMOVED FASTENERS AT FRAME BS 680 STR 24L PER SRM 57-30-2. CUT OUT DAMAGED FRAME AREA PER SRM 57-40-3 FIG 1. FABRICATED FRAME REPAIR FROM 7075-T6 0.063 (12.5 X 6 INCH) PER SRM 51-40-3 FIG 1. TREATED AND PRIMED PER SRM 57-10-2, INSTALLED REPAIR PER SRM 57-40-3 FIG 1. 2L73 4F RTA3WE 20030331001392003033100139NM 2003 3 31 DHL2003740525 120030221A5310 DOOR FRAME BOEING727 7272Q9 138448MNM CARGO BAY CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT, C-2 DOOR LOWER CUTOUT LOWER FRAME IS CORRODED AND CRACKED IN 3 AREAS. REMOVED THRESHOLD MOUNT FITTINGS FROM C-DOOR FOR ACCESS IAW SRM 51-30-2. REMOVED 2 EA PREVIOUS REPAIRS SPLICE PLATES FROM LWR TEE CHORD IAW SRM 51-30-2. REMOVED FWD AFT, MIDDLE SEAL RETAINERS AND MOUNTS FOR ACCESS IAW SRM 51-30-2. REMOVED LWR T-CHORD FOR REPLACEMENT IAW SRM 51-30-2. FABBED NEW LWR T-CHORD USING 60-9794 PO 301733 DIM 4 INCH X 57.5 INCH IAW SRM 53-10-2 FIG 5 & 51-20-1. ALODINED AND PRIMED T-CHORD IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30-2. REINSTALLED C-2 DOOR THRESHOLD MOUNTS AND RETAINERS IAW SRM 57-30-2. 2L73 4F RTA3WE 20030331001402003033100140NM 2003 3 31 DHL2003740526 120030221A5310 DOOR FRAME BOEING727 727200 138407ENM FUSELAGE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 AFT CARGO COMPT, C-2 DOOR LOWER CUTOUT UPPER DOOR FRAME IS CORRODED AROUND NUT PLATES ON INBOARD FLANGE LOWER SURFACE BETWEEN STA 950E-990 STR 27R. REMOVED NUT PLATES FROM UPPER DOOR FRAME I/B SIDE FOR CORROSION REMOVAL IAW SRM 51-10-2. REMOVED CORROSION FROM UPPER DOOR FRAME IAW SRM 51-10-6 WITH A MATERIAL LOSS OF OVER 50 PERCENT AND IS OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED NEW UPPER DOOR FRAME DIMENSIONS 94 INCHES X 2 INCHES USING 60-20317 PO 3017135 IAW SRM 53-10-2 FIG 5. ALODINED AND PRIMED NEW PIECE IAW SRM 51-10-2 AND INSTALLED UPPER DOOR FRAME IAW SRM 51-30-2. INSTALLED NUT PLATES ON UPPER DOOR FRAME IAW SRM 51-30-2. 2L73 4F RTA3WE 20030331001412003033100141NM 2003 3 31 DHL2003740527 120030226A5521 SPAR BOEING727 7272Q9 138448MNM RT ELEVATOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH 21930 RT ELEVATOR TAB HAS 3 O/B HINGES LOOSE AT ELEVATOR REAR SPAR ATTACH POINT, CHECK FOR SPAR CRACKS PER S/B 55-0089. REMOVED DAMAGED SPAR AND INSTALLED NEW SPAR (P/N 65C30825-24) PO 301742 IAW S/B 727-55-0089 FIG 6 AND SUPPORT FITTINGS. 2L73 4F RTA3WE 20030401000022003040100002NM 2003 4 1 03087403 120030328A3350362624 LIGHT DORNERDO32 DO328300 NM CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27403FJ 3149 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA55NM 20030401000042003040100004EA 2003 4 1 03088628 120030329A3350 BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27628BR 7240 DURING MAINTENANCE INSPECTION, THE CABIN DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000052003040100005EU 2003 4 1 03089312 120030330A33506134051 BATTERY PACK JETAIRJETSTMJETSTM4101 1500501EU CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27312UE 41025 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE FWD EMERGENCY BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030401000092003040100009EA 2003 4 1 03090668 120030331A33501317 BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27668BR 7544 DURING MAINTENANCE INSPECTION, THE OVERHEAD CABIN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000112003040100011 2003 4 1 250TR0008 420030323A2230L6901 TRANSMITTER BOEING737 7372K5 138448XNM AUTOTHROTTLE MALFUNCTIONED A PIDAO OTHER O OTHER CRCRUISE 1 SO05250TR 22597 AUTO THROTTLE KEEPS DISCONNECTING DURING FLIGHT. REPLACED LT. ENGINE THRUST LEVER POSITION TRANSMITTER PER MM 22-31-81. OPS CHECKED OK. 2L72 4F RTA16WE 20030401000122003040100012NM 2003 4 1 250TR0009 120030326A33501000679 LIGHT BOEING737 7372K5 138448XNM CABIN MALFUNCTIONED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05250TR 22597 EMERGENCY EXIT LIGHT COMES ON WHEN POWER IS SWITCHED OFF AND EMERGENCY EXIT SWITCH IS IN OFF POSITION. REPLACED RT FWD EMERGENCY EXIT LIGHT ASSY AND OPS CHECK PER MM 33-51-11. 2L72 4F RTA16WE 20030401000132003040100013NM 2003 4 1 372PA0018 120030325A3350362624 LIGHT BOEING737 737306 13844BGNM CABIN BURNED OUT A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05372PA 23546 AFT SECTION OF CABIN FLOOR EMERGENCY STRIP LIGHTING OUT. FOUND DIRTY SOCKETS AT INVERTER STRIP, CLEANED SAME. REMOVED AND REPLACED AFT SECTION OF FLOOR LIGHTS PER MM 33-51-21. OPS CHECK GOOD PER MM 33-51-02. 2L72 4F RTA16NE 20030328000102003032800010EA 2003 3 28 CA030214004 220030205A7414 POINTS PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA MAGNETO LOOSE W O OTHER R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CA BO19607FR (CAN) LT ENGINE WILL NOT START. REMOVED LEFT MAGNETO AND DISASSEMBLED, FOUND RETARD POINTS NOT OPENING, FOLLOWER PLASTIC AND FELT RIVETS LOOSE AND NOT OPENING POINTS PROPERLY. 1L72 3O3 O A20SO E14EA 20030328000122003032800012SO 2003 3 28 CA030214006 120030214A57200062061002 SKIN PIPER PA28 PA28140 7102802SO LYC O320 O320E3D 41508EA WINGS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THE DOUBLERS ON THE BOTTOM OF THE WING WALK SKINS JUST OUTBOARD OF THE INBOARD STAMPED STIFFENERS WERE SEVERELY CRACKED. THE AFT SKIN CRACK WAS 42CM IN LENGTH. THE FORWARD SKIN HAD 3 CRACKS 5CM IN LENGTH. THIS AREA IS NOT NORMALLY ACCESSIBLE BUT THIS AIRCRAFT HAD AN EXTRA INSPECTION HOLE INSTALLED FROM A PREVIOUS SB. THIS AREA SHOULD BE INSPECTED WITH A BORESCOPE ESPECIALLY ON HIGHER TIME AIRCRAFT. 1L71 3O3 O 2A13 E274 20030328000182003032800018CE 2003 3 28 CA030218001 120030203A5711101110367 SPAR CAP BEECH 200 B200C 1152924CE PWA PT6 PT6A42 52043NE WING CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) CORROSION ON UPPER RIGHT AND LEFT FORWARD WING SPAR CAPS BETWEEN WS 223 & 236 AND WS 122 & 132. CORROSION IS BEYOND LIMITS, WINGS TO BE REMOVED AND SPARS TO BE REPLACED AS DIRECTED BY BEECHCRAFT ENGINEERING. 1L72 4T4 T A24CE E4EA 20030401000142003040100014WP 2003 4 1 AALA20030001 120030103A3350 LIGHT DOUG DC9 DC982 3022082WP EXTERIOR INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21293AA 49305 DURING OVERNIGHT MAINTENANCE, RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RT EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000172003040100017WP 2003 4 1 AALA20030031 120030107A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21266AA 49291 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS AT ROW 7-11 INOPERATIVE. RESEATED CEILING EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000192003040100019WP 2003 4 1 AALA20030220 120030223A3350 CONNECTOR DOUG DC9 DC983 3022083WP EMERGENCY LIGHT CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21567AM 53293 DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHTS IN FORWARD GALLEY AND FLIGHT DECK INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT BATTERY CONNECTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030401000202003040100020WP 2003 4 1 AALA20030221 120030223A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21437AA 49455 DURING OVERNIGHT MAINTENANCE, WALL MOUNTED EMERGENCY EXIT LIGHT ACROSS FROM FORWARD LAVATORY IN AISLE INOPERATIVE. REPLACED WALL MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030401000212003040100021WP 2003 4 1 AALA20030227 120030227A3350 LIGHT DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21454AA 49559 DURING OVERNIGHT MAINTENANCE, OVERHEAD CEILING EMERGENCY EXIT LIGHT FORWARD OF AFT EXIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000222003040100022WP 2003 4 1 AALA20030236 120030224A3350 WIRE DOUG DC9 DC982 3022082WP EMERGENCY LIGHT LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2170401 49312 DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT AISLE SEAT LIGHT AT SEAT 26D INOPERATIVE. PLUGGED EMERGENCY EXIT LIGHT WIRE IN TO RECEPTACLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030401000242003040100024EA 2003 4 1 ASOA03044 120030206A2751 SENSOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS OUT OF RIG A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11914EV 7752 DURING APPROACH INTO ATL FROM DAL, APPROXIMATELY 5,000 FT AND 250 KIAS, THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW SELECTED AN 8 DEGREE FLAP SETTING WITH NO NOTABLE FLAP CHANGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE RE-RIGGED BOTH BRAKE POSITION SENSOR UNITS, RESET AND RAN THE FLAPS THROUGH FIFTEEN CYCLES. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000252003040100025EA 2003 4 1 ASOA03045 120030206A3350BM10006002 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11832AS 7243 DURING A GROUND INSPECTION IN DFW, THE LEFT FORWARD UPPER EXTERIOR EMRGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD UPPER EXTERIOR EMERGENCY LIGHT. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000272003040100027EU 2003 4 1 ASOA03047 120030207A33507012210 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11636AS 375 DURING A GROUND INSPECTION IN VPS, THE FORWARD EMERGENCY EXIT LAMPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXT LIGHT LAMPS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030401000282003040100028EA 2003 4 1 ASOA03048 120030207A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11848AS 7339 DURING DESCENT INTO MLB FROM ATL, AS THE AUXILIARY POWER UNIT WAS POWERED UP EXTREME JET FUEL FUMES OCCURRED IN THE CABIN THROUGH THE ENVIROMENTAL CONTROL SYSTEM. THE CREW SHUT DOWN THE AUXILIARY POWER UNIT AND THE AIRCRAFT LANDED SAFELY IN MLB. MAINTENANCE REMOVED AND REPLACED THE AUXILIARY POWER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000292003040100029EA 2003 4 1 ASOA03049 120030208A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11874AS 7551 DURNG A GROUND INSPECTION IN DFW, THE FORWARD PASSENGER DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD PASSENGER DOOR EXTERNAL EMERGENCY LIGHT LAMP. (M) 2L72 4F RTA21EA 20030401000302003040100030EA 2003 4 1 ASOA03050 120030209A3350OL3071BPEGPL LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11857AS 7411 DURING A GROUND INSPECTION IN MGM, THE CEILING EMERGENCY EXIT LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A LAMP IN THE CEILING EMEGENCY EXIT LIGHT AT ROW 10. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030625001232003062500123NM 2003 6 25 AWXA200300327 120030328A2730S251N2062 ACTUATOR BOEING757 757225 1384959NM ELEVATOR WORN A AWXAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 WP28913AW17255 22207 DURING CLIMBOUT FL 200 RECEIVED EICAS STATUS ELEV ASYM, TURNED BACK. ON SHORT FINAL AT POWER REDUCTION FOR LANDING (10 FT ABOVE GROUND LVL), VIOLENT CONTROL COLUMN SHAKING OCCURRED (NOT STICK SHAKER). MX TROUBLESHOT & FOUND FAULT BALL FOR ELEV ASYM LIMIT ACTUATOR TRIPPED ON RT ELEV ASYM LIMIT MODULE. RESET MODULE & PERFORMED BITE CHECK ON LT & RT ELEV ASYM MODULES. BITE CHECK GOOD. PERFORMED ELEVATOR CONTROL SYSTEM TEST PER T/C F1B27623, TEST WAS GOOD. PERFORMED ELEV TEST WITH EACH INDIVIDUAL HYD SYS, NO FAULTS NOTED. AS PRECAUTION REPLACED ELEV ASYM ACTUATOR, OPS CHECK GOOD. *S/D* VENDOR TEARDOWN OF ELEV ASYM LINEAR ACTUATOR S/N 194 ONLY FOUND INDICATION OF NORMAL WEAR. UNIT REPAIRED & TESTED. 2L72 4F RTA2NM 20030401000402003040100040SO 2003 4 1 C2XA03BT045 120030328A323414532170401 LEVER EMB 145 EMB145 3260210SO MLG FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2727962 145110 CREW REPORTED "AFTER TAKEOFF FROM PHL ENROUTE TO CLE, LANDING GEAR WOULD NOT RETRACT. HANDLE WORKED FINE. (DIVERTED TO EWR, LANDED UNEVENTFULLY) POST FLIGHT INSPECTION REVEALED NO GEAR PINS IN LANDING GEAR." AIRCRAFT MAINTENANCE FERRIED TO BTV GEAR DOWN, MAINTENANCE REMOVED AND REPLACED LT NR 2 MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 AMM, REMOVED AND REPLACED LGEU IAW EMB145 AMM AND REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM. OPS. CHECKED LANDING GEAR GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030401000462003040100046SO 2003 4 1 C2XA03SH082 120030331A531014521725013 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK FOWARD SILL HAS CORROSION BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED DAMAGE AND MADE A DOUBLER REPAIR ON AFFECTED SILL IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401000502003040100050EU 2003 4 1 CA030220005 120030219A5520 BALANCE WEIGHT STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE HARTZLHCB5M HCB5MP3 GL ELEVATOR SEPARATED W O OTHER FD FLT CONT AFFECTED INFLIGHT SEPARATION LDLANDING 1 CA 21093 (CAN) AIRPORT PERSONNEL APPROACHED MAINT WITH PIECE OF METAL THAT HAD BEEN FOUND ON RUNWAY. SUSPECTED IT WAS OURS DUE TO COLOR. IDENTIFIED AS A BALANCE WEIGHT ASSY FROM ELEVATOR TRIM TAB ON A SHORTS SD3-60. CHECKED A/C AT THE RAMP, FOUND THAT A/C HAD TAB WITH MISSING BALANCE WEIGHT. IT HAD APPARENTLY BROKEN AWAY UPON LANDING. PILOT RECEIVED NO INDICATION THAT PART HAD SEPARATED DURING LANDING PHASE. A/C RETURNED TO MAINT, REPLACEMENT TAB WAS INSTALLED. AREA OF SEPARATION IS IMPOSSIBLE TO SEE. TAB CONTROL ROD MUST BE DISCONNECTED SO TAB CAN BE DEFLECTED ENOUGH TO GIVE BALANCE WEIGHT A GOOD WIGGLE TO CHECK FOR POSSIBLE SEPARATION. 2H72 4T4 T A41EU E4EA 6 CP44GL 20030401000512003040100051NM 2003 4 1 CA030220007 120030212A56107560001 WINDOW BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE COCKPIT CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA 60204 (CAN) DURING CLIMB, CAPTAINS NR 2 WINDOW CRACKED DUE ELECTRICAL ARCING. AIRCRAFT RETURNED TO BASE. NR 2 WINDOW REPLACED AND CHECKED SERVICEABLE. TIME 60204.19 CYC.58513. 2L72 4F4 F A16WE E2EA 20030401000522003040100052NM 2003 4 1 CA030220009 120030217A2910BACH8B04NN0202T HOSE BOEING737 737* NM PWA JT8 JT8D17 52049NE HYD SYSTEM RUPTURED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER SELECTING LANDING GEAR UP ON CLIMB, WARNING RED/GREEN NOSE GEAR LIGHTS ILLUMINATED. CONTACTED MCC AND WERE ADVISED TO LOWER GEAR AND CONTINUE TO MAINT BASE. FUEL REMAINING WAS NOT SUFFICIENT AND ELECTED TO RETURN. NOTICED SYSTEM "A" HYDRAULICS QUANTITY HAD DEPLETED TO ZERO. ATC ADVISED AND CFR WAS CALLED. A/C LANDED IAW 'LOSS OF SYSTEM 'A' FLUIDS NON NORMAL CHECKLIST WITH NO INCIDENTS TO REPORT. MAINTENANCE INSPECTION REVEALED NOSE GEAR LOCK ACTUATOR - LOCK PORT HOSE FOR GEAR UP FOUND RUPTURED HOSE. REPLACED HOSE AND HYDRAULICS SERVICED. SYSTEM GROUND CHECKED, SERVICEABLE WITH NO LEAKS . AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2L72 4F4 FRTA16WE E2EA 20030401000582003040100058NM 2003 4 1 CA030224003 120030220A2612 FIRE LOOP BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE APU MALFUNCTIONED W FA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA 34247 (CAN) CREW REPORTED, AT CRUISING ALTITUDE, 20 MINUTES OUT OF YLW THEY EXPERIENCED A VIBRATION FOLLOWED BY AN APU FIRE WARNING. CREW SHUTDOWN APU WITH THE FIRE HANDLE AND APU FIRE BOTTLES WERE DISCHARGED. A/C COMPLETED AN (ABNORMAL LANDING CONFIGURATION) IN YLW WITH CFR ON STANDBY NO EMERGENCY WAS DECLARED. A/C LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION FOR EVIDENCE OF FIRE AND EXTERNAL INTEGRITY OF THE APU REVEALED NO SIGNS OF FIRE. THE APU AND APU FIRE SHUT OFF SYSTEM WAS PLACED ON MEL (49-1 AND 26-7-1). MAINTENANCE HAS SINCE REPLACED APU FIRE LOOP WARNING HARNESS AND PLAN TO REPLACE EGT WIRING PRIOR TO MEL EXPIRING 02 MAR.03. AIRCRAFT HAS RETURNED TO SERVICE WITH NO FURTHER INCIDENTS TO REPORT. 2L72 4F4 F A16WE E2EA 20030401000592003040100059NM 2003 4 1 CA030224004 120030219A492038042816 APU BOEING737 737217 1384464NM PWA JT8 JT8D17A 52049NE APU BAY FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN) PRIOR TO PUSH BACK, AIRCRAFT RAPIDLY FILLED CABIN WITH SMOKE, AIRCRAFT DEPLANNED. CAUSED BY THE BLEED FROM THE APU (BURNED OIL CONTAMINATION) APU CHANGED AND COLLESTER BAGS REPLACED. AC SERVICEABLE 2L72 4F4 F A16WE E2EA 20030401000602003040100060WP 2003 4 1 CA030225001 220030221A7314307085063 PUMP LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP FUEL FAILED W C ABORTED TAKEOFF XJ ENGINE FLAMEOUT WARNING INDICATION TOTAKEOFF 1 CA 10877 (CAN) AIRCRAFT WAS AT 70 KNOTS ON TAKE-OFF ROLL WHEN LT ENGINE FLAMED OUT. CREW REJECTED TAKE OFF. TROUBLESHOOTING FOUND LT ENGINE DRIVEN PUMP AT 30 PSI. AMM STATE MINIMUM 300 PSI. PUMP REPLACED. AIRCRAFT RETURN TO SERVICE. 2L72 4F4 F A10CE E6WE 20030401000612003040100061EU 2003 4 1 CA030225002 120030220A5520SD3316213XB BRACKET STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE HARTZLHCB5M HCB5MP3 GL ELEVATOR TRIM CRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 31865 (CAN) BRACKET WAS INSPECTED AS PART OF A FLEET CAMPAIGN INITIATED IN-HOUSE. BRACKET WAS FOUND TO HAVE A .7500 INCH CRACK AND A .2500 INCH CRACK FROM THE OUTSIDE EDGES MOVING INWARD. THE TRIM TAB WAS REMOVED AND REPLACED WITH A SERVICEABLE TRIM TAB. THE REMOVED BRACKET AND THE MASS BALANCE WEIGHT HAVE BEEN SENT TO MFG FOR ANALYSIS. 2H72 4T4 T A41EU E4EA 6 CP44GL 20030401000632003040100063EA 2003 4 1 CA030225008 120030215A3230 DRAG BRACE CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE NLG CRACKED W O OTHER E VIBRATION/BUFFET LDLANDING 1 CA (CAN) THE AIRCRAFT LANDED NORMALLY AND SHORTLY AFTER, THE NLG TOUCH DOWN, THE CREW REPORTED AN IMPACT FOLLOWED BY A NOISE AND THE NLG COLLAPSED. THE NLG COLLAPSE DUE TO THE DRAG BRACE CRACKED. THE CREW MENTIONNED ALSO A PROBABLE IMPACT WITH A SNOW BANK FOR SEVERAL REASONS: RUNWAY SNOW CONTAMINATION INCONSISTENT (CLEAR , 4 FT AND SNOW BANKS) SIDE OF THE RUNWAY CLEAR FROM SNOW- SNOW GSE ACTIVITY AT A RUNWAY TEE INTERSECTION (JUST AFTER THE LANDING AREA) THE NLG COLLAPSE DUE TO THE DRAG BRACE CRACK. 2L72 4F4 FRTA21EA E15NE 20030401000642003040100064NE 2003 4 1 CA030226001 220030224A7230 COMPRESSOR BOEING767 767375 1385217NM GE CF6 CF680C2B6F 30025NE LT ENGINE STALLED W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 CA (CAN) REJECTED TAKE OFF AFTER COMPRESSOR STALL ON THE LT ENGINE AND RISE IN TEMP AT 155 KNOTS, ALL 8 TIRES WENT FLAT (FUSES BLOWED OUT). 2L72 4F4 FRTA1NM E13NE 20030401000702003040100070NM 2003 4 1 CA030228013 120030219A2740651948220 GEARBOX BOEING727 727225 1384077NM PWA JT8 JT8D7B 52053NE STAB TRIM FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING COLD WEATHER, PRE-DEPARTURE CHECK BY MAINTENANCE PERSONNEL, THE STABILIZER TRIM SYSTEM WAS OPERATED. DURING OPERATION A VIBRATION AND NOISE WAS NOTICED. UPON INVESTIGATION IT WAS FOUND THAT THE BRAKE ASSEMBLIES IN THE STABILIZER TRIM GEARBOX WERE NOT FUNCTIONING CORRECTLY, CAUSING THE VIBRATION AND NOISE. THE STABILIZER TRIM GEARBOX AND JACKSCREW ASSEMBLY WAS REPLACED WHICH RECTIFIED THE DEFECT. INVESTIGATION OF PRIOR FLIGHTS DID NOT SHOW ANY PREVIOUS PROBLEMS. 2L73 4F4 F A3WE E2EA 20030401000722003040100072NE 2003 4 1 CA030304002 220030227A7200 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE NR2 STALLED W E ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 CA (CAN) NR 2 ENGINE STALL IN LEVEL FLT. ECAM MSG NR 2 ENGINE STALL THEN NR 2 ENGINE SHUT DOWN. ECAM ACTIONS CARRIED OUT. CHANGED NR 2 ENGINE IAW AMM. 2L72 4F4 FRTA28NM E29NE 20030401000742003040100074NM 2003 4 1 DHL2003741500 120030331A5330 SKIN BOEING727 727200 138407ENM FUSELAGE CANNING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING C CHECK, FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT, REMOVED FASTENER AT FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM. APPROX. 2 X 1 INCH IAW B-727 SRM 53-30-2. 2L73 4F RTA3WE 20030401000762003040100076NM 2003 4 1 DHL2003741502 120030323A5311 FRAME BOEING727 727200 138407ENM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DISCREPANCY AS FOLLOWS DURING C CHECK, B.S. 1030 CIRCUM. IS CRACK LT SIDE 3" ABOVE FLOOR. REMOVED FASTENER AT BS 1030 CIRCUM LT SIDE 3 INCH ABOVE FLOOR IAW B-727 SRM 51-30-2. 2L73 4F RTA3WE 20030401000812003040100081NM 2003 4 1 DHL2003745003 120030123A3260 SWITCH BOEING727 727224 1384076NM MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01745DH 20665 AFTER GEAR RETRACTION UPON MOVING GEAR HANDLE FROM UP TO OFF POSITION. S/O RT GEAR DOOR LIGHT ILLUMINATED, AND FRONT PANEL DOOR LIGHT ILLUMINATED. BROUGHT LEVER BACK TO UP AND ALL DOOR LIGHTS EXTINGUISHED. TROUBLESHOT SYSTEM, FOUND DEBRIS AT RT MLG WARNING SWITCH. CLEANED AND RESECURED. PERFORMED OPERATIONAL SYSTEM TEST, NO DEFECTS NOTED REF M/M 32-62-11. 2L73 4F A3WE 20030401000822003040100082NM 2003 4 1 DHL2003745005 120030205A261210607723 WARNING SYSTEM BOEING727 727224 1384076NM FIRE WARNING MALFUNCTIONED A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01745DH 20665 FIRE WARNING BELL IS MAKING STRANGE NOISE AND NO BELL. REPLACED AURAL WARNING BOX. OPS CHECKED GOOD IAW B727 M/M 31-26-0. 2L73 4F A3WE 20030401000902003040100090NM 2003 4 1 DHL2003747001 120030125A2612 FIRE LOOP BOEING727 727224 1384076NM NR 1 OUT OF POSITION A DHLAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01747DH 22253 ON P6-3 CIRCUIT BREAKER PANEL NR 1 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED NR 1 GROUND FAULT DETECTION SYSTEM TO DMI 11753 IAW MEL 26-9. PLACARD INSTALLED. RE; DMI 11753 - NR 1 GROUND FAULT ILLUMINATED. REPOSITIONED FIRE LOOP THAT WAS TOUCHING COWL, CHECKED GOOD PER 26-11-0. CLEARS DMI 11753. PLACARD REMOVED. 2L73 4F A3WE 20030401000932003040100093NM 2003 4 1 DHL2003748003 120030304A3350 LIGHT BOEING727 727225 1384077NM CABIN INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01748DH 22440 FORWARD ENTRY EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING STANDBY POWER CHECK. CLEANED AND RE-SECURED EMERGENCY EXIT LIGHT ASSEMBLY IAW B727 M/M 33-50-71. OPS CHECKED SERVICEABLE IAW B727 M/M 33-50-91. 2L73 4F A3WE 20030401000952003040100095NM 2003 4 1 DHL2003751005 120030205A2120 ODOR BOEING727 727264 138408MNM CABIN DETECTED A DHLAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01751DH 22982 AFTER CLOSING MCD ON TAXI OUT IN MCI, AN ACRID ODOR BECOMES PRESENT IN COCKPIT, AFTER TURNING ON PACKS, ODOR REMAINS FOR 5-10 MINUTES. RETIGHTENED GROUND INTERCONNECT LINES, RAN PACKS FOR 30 MINUTES, NO ODOR DETECTED, OPS CHECKED NORMAL IAW M/M 21-21-0 & 20-80-01. 2L73 4F A3WE 20030401001072003040100107WP 2003 4 1 DHL2003803004 120030320A5347 SEAT TRACK DOUG DC8 DC873 302199CWP COCKPIT LACK OF LUBE A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01803DH 46123 S/O'S SEAT DIFFICULT TO MOVE FORE AND AFT. LUBED F/O'S AND S/O'S SEAT TRACKS AND CHECKED MOVEMENT. OK PER M/M 25-11-1. 2L74 4F RT4A25 20030401001102003040100110WP 2003 4 1 DHL2003804501 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 766.500. REMOVED FASTENERS PER SRC2 PG 1. STOP DRILLED CRACK PER SRM 57-20 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001112003040100111WP 2003 4 1 DHL2003804502 120030120A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 422.750. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE DOUBLER PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001122003040100112WP 2003 4 1 DHL2003804503 120030116A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING CTR L/E FORMER UPPER PART WITH 1 INCH CRACK AT STA XFS 416.500. REMOVED FASTENERS PER SRM 51-1-21 PG 1. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFORCEMENT ANGLE (2024-T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001132003040100113WP 2003 4 1 DHL2003804504 120030110A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING CTR L/E FORMER PART WITH 2 INCH CRACK AT STA XFS 521.250. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED DOUBLER ANGLE (2024.T3 AL 0.063) PER SRM PG 9-10. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED DOUBLER PER SRM 57-2-0 PG 9-10. 2L74 4F RT4A25 20030401001232003040100123WP 2003 4 1 DHL2003804515 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER LOWER PART WITH 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001242003040100124WP 2003 4 1 DHL2003804516 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN AT XFS 610.000 (LT O/B WING). REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001252003040100125WP 2003 4 1 DHL2003804517 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED 1/2 IN AT XFS 434.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001282003040100128WP 2003 4 1 DHL2003804520 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT OUTER WING L/E FORMER UPPER PART HAS A 1 IN CRACK AT STA XFS 797.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001292003040100129WP 2003 4 1 DHL2003804521 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 622.500. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10. CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001302003040100130WP 2003 4 1 DHL2003804522 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 641.250. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030625001182003062500118NM 2003 6 25 DHL2003743006 120030401A2612 BRACKET BOEING727 727225 1384077NM NR 1 FIRE LOOP BROKEN A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01743DH 22438 AFTER PRE-DEPARTURE CHECK FOUND NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. DEFERRED PER MEL 26-9 CAT-C DMI 12419. REF DMI 12419; NR 1 FIRE WARNING GROUND FAULT TEST LIGHT INOPERATIVE. FOUND BROKEN BRACKET ON B-FLANGE, REPLACED, RE-SECURED FIRE LOOP, OPS CHECKED NORMAL IAW M/M 26-11-01 & 26-11-12. THIS CLEARS DMI 12419, PLACARD REMOVED. 2L73 4F A3WE 20030401001412003040100141WP 2003 4 1 DHL2003804549 120030206A57205769859U164 FITTING DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT ZEE PAN WING ZEE PAN FITTING CRACKED 2.00STA. XW 223.000 CORR: REMOVED FITTING ZEE PAN(CRACKED CONDITION)IAW SRM51-3-0 PG. 1 CLEANED , TREATED, & PRIMED AREA IAW SRM51-1-8B , INSTALLED NEW FITTING ZEE PAN ON RH WING L/E , STA. XW 233.000 IAW SRM51-3-0 PG. 1 2L74 4F RT4A25 20030401001442003040100144WP 2003 4 1 DHL2003804553 120030203A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 "A" CARGO DOOR LOWER EXT. SKIN SHOWS WEAR (FS.280.000-340.000) PERFORMED MAJOR REPAIR IAW SRM52-1-0 PG. 1 , SRM51-9-0 FIG 68A, SRM 52-4-1 PG. 2 FIG. 1. REMOVED DAMAGED SKIN FROM "A" CARGO DOOR IAW SRM51-1-21 PG. 1 , SRM51-1-20D PG. 21. FABRICATED NEW SKIN (7075T6.050) IAW SRM 52-4-1 PG. 2 FIG 1 . CLEANED , TREATED AND PRIMED IAW SRM51-1-8B, INSTALLED NEW SKIN IAW SRM52-4-1 PG. 2 FIG.1 , SRM51-1-21 PG. 1 , SRM51-1-20D PG.9 , SRM51-1-15 PG. 1REFER TO N/R 0243 FOR "A" CARGO DOOR REMOVAL AND INSTALLATION. 2L74 4F RT4A25 20030401001462003040100146WP 2003 4 1 DHL2003804556 120030215A57305769589505 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E UPPER SKIN CORRODED BETWEEN STA. XFS291.5000 AND XFS 304.000 CORR: PERFORMED MAJOR REPAIR IAW EO DHL 030108 , ED-3214. REMOVED FASTNERS IAW SRM51-1-21 PG. 1 REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM57-2-0 PG 16 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EO DHL 030108 , ED-3214. FABRICATED A REPAIR DOUBLER (7075T6AL.071) AND THREE FILLERS (7075T6AL.063) IAW EO DHL030108 , ED-3214. CLEANED , TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B APPLIED PRC TO ALL FAYING SURFACES IAW SRM 51-1-15 PG. 1 INSTALLED DOUBLERS AND FILLERS AT LH L/E UPPER SKIN WITH NEW FASTNERS IAW EO DHL 030108, ED-3214, SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001472003040100147WP 2003 4 1 DHL2003804557 120030210A57105769933183 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING OUTBD VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO58.000 PERFORMED MAJOR REPAIR IAW EO DHL 030109 ED-3222 . REMOVED FASTNERS IAW SRM 51-1-21 PG 1 TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AL.063) AND INTERNAL DOUBLER (7075T6AL.050) IAW EO DHL030109 , ED-3222 . CLEANED TREATED , & PRIMED INNER SURFACE IAW SRM51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG. 1 INSTALLED FILLERS AND DOUBLERSAT LH WING OUTBD VANE SLOT UPPER SKIN WITH NEW FASTNERS IAW EO DHL 0-30109 , ED-3222, SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001482003040100148WP 2003 4 1 DHL2003804558 120030202A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E UPPER SKIN CORRODED BETWEEN STA 422.750 AND XFS 427.000 PERFORMED MAJOR REPAIR IAW SRM57-2-1 PAGE 2 FIG. 38 REMOVED CORROSION ON L/E UPPER SKIN IAW SRM51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG.16. CUT OUT CORRODED AREA IAW SRM 57-2-1 PG. 2, FIG.38 CLEANED , TREATED, AND PRIMED FILLER & DOUBLER INNER PART IAW SRM 51-1-8B. INSTALLED FILLER & DOUBLER ON LT WING STA. XFS 422.750-XFS 427.000 AND APPLIED PRC SEALANT IAW SRM 57-2-1 PG. 2 FIG 38, SRM51-1-21 PG. 1 SRM51-1-15 PG 1, FOR REMOVAL AND RE-INSTALLATION OF CENTER L/E SEE N/R0318. 2L74 4F RT4A25 20030401001492003040100149WP 2003 4 1 DHL2003804559 120030307A552257025792 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVAL / INSTALLATION OF THE RT ELEVATOR GEAR TAB DUE TO DELAMINATION ON UPPER SKIN. R & R RT ELEVATOR GEAR TAB IAW MM 27-30-3 PG. 201-206 REFER TO N/R 0607 FOR OPS CHECK. 2L74 4F RT4A25 20030401001512003040100151WP 2003 4 1 DHL2003804661 120030212A5210 SKIN DOUG DC8 DC873F 302199FWP PAX DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD PASSENGER DOOR INTERIM REPAIR AT AFT LWR JAMB CORNER STA. 55.00 LT PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 15 REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG. 1 CUT OUT DAMAGED AREA IAW SRM 53-2-0 FIG , FABRICATED FILLER & DOUBLER (7075 T6 0.63) & TRIPLER (7075T6 .080) IAW SRM53-2-0 FIG 15 . CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. ISTALLED FILLER , DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG. 15 , SRM 51-1-21 PG. 1 , SRM 51-1-20D PG. 9 , SRM51-1-15 PG 1 2L74 4F RT4A25 20030401001532003040100153WP 2003 4 1 DHL2003804663 120030207A533056544401 PANEL DOUG DC8 DC873F 302199FWP LT WING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING NR 718 CENTERWING LOWER PANEL EXTERNAL SKIN DELAMINATED STA 730.000-STA 779.000 R & R NR 718 CENTERWING LOWER PANEL ON LT WING , STA 730.000-STA. 779.000 IAW SRM 51-3-0 2L74 4F RT4A25 20030401001542003040100154WP 2003 4 1 DHL2003804664 120030309A53305654693404 PANEL DOUG DC8 DC873F 302199FWP CENTERWING DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LOWER FUSELAGE 723 RT CENTERWING LOWER PANEL INNER SKIN DELAMINATED CORR: R/R RH LOWER PANEL 723 IAW SRM51-3-0 PG. 1 2L74 4F RT4A25 20030401001552003040100155WP 2003 4 1 DHL2003804665 120030116A57105769933184 VANE DOUG DC8 DC873F 302199FWP RT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT OUTBD SLOT VANE AT STA XS 520.000 HOLES ELONGATED. PERFORMED MAJOR REPAIR IAW EO DHL 030101 , ED-3211. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1, TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030101 , ED-3211 , FABRICATED REPAIR DOUBLER, A FILLER (7075T6AL-0.063) AND INTERNAL DOUBLER IAW EO DHL 030101 , ED -3211. CLEANED , TREATED AND PRIMED INNER SURFACE IAW SRM51-1-8B. APPLIED PRC SEALANT AND DOUBLERS AT RT OUTBD SLOT VANE STA. XS 520.000 MKI 2L74 4F RT4A25 20030401001562003040100156WP 2003 4 1 DHL2003804666 120030202A53403750257U1 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 AFT CARGO COMPT. SPLICE FITTING CRACKED 3.000 INCH BETWEEN STA. 1040.000-1060.000 , L31R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PAGE 1 AND FAX BOEING -SEU-LIM - 03-00003H DATE 20TH 2003. REMOVED CRACKED FITTING IAW SRM 51-1-20D PAGE 21. CLEANED , TREATED AND PRIMED AREA IAW SRM51-1-8B. INSTALLED NEW FITTING ON AFT CARGO COMPT. BTWN STA. 1040.000 AND STA. 1060.000 , L31R IAW SRM51-1-20D PG. 9 2L74 4F RT4A25 20030401001572003040100157WP 2003 4 1 DHL2003804667 120030204A5710576998592 VANE DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING L/E INBD. VANE SHOWS HOLES ELONGATED , XS247.000 PERFORMED MAJOR REPAIR IAW EO DHL 030104 , ED-3208. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EA DHL 030104, ED-3208 FABRICATED REPAIR DOUBLER. A FILLER 7075T6 AL 0/063 AND INTERNAL DOUBLER IAW EO DHL 030104 , ED-3208. CLEANED , TREATED AND PRIMED INTERIOR SURFACES IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED FILLER AND DOUBLERS IN RT WING L/E VANE WITH NEW FASTNERS IAW EO DHL 030104 , ED-3208, SRM51-1-21 PG 1. 2L74 4F RT4A25 20030401001582003040100158WP 2003 4 1 DHL2003804668 120030117A57005769584502 DOOR DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING L/E OUTBD. SLOT DOORS SHOW .5000 CRACKS ON THREE SECTIONS BETWEEN STA. 435.789 - XS520.168 REMOVED DAMAGED L/E SLOT DOORS IAW MM 27-80-2 PG. 201-203 PERFORMED NEW HOLESAND COUNTERSUNK IAW SRM 51-1-22 FIG. 476 . INSTALLED NEW SLOT DOORS ON THE THREE SECTIONS BETWEEN STA. XS 435.789 AND XS520.168 IAW MM. 2L74 4F RT4A25 20030401001592003040100159WP 2003 4 1 DHL2003804669 120030208A5522 SKIN DOUG DC8 DC873F 302199FWP RT ELEVATOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT ELEVATOR UPPER SKIN SURFACE DENTED ( STA. 44.907 - 50.000) PERFORMED MAJOR REPAIR IAW EO DHL 030102, ED-3219 . REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 REMOVED DAMAGED SKIN SEGMENT IAW EO DHL 030102 , ED-3219. CLEANED TREATED AND PRIMED NEW SKIN INTERIOR IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED NEW SKIN SEGMENT ONRT ELEVATOR TOP SURFACE WITH NEW FASTNERS IAW EO DHL 030102 , ED-3219 AND SRM 51-1-21 PG. 1 SEE N/R 2052 FOR RT. ELEVATOR REMOVAL AND INSTALLATION. SEE N/R 2645 FOR WEIGHT AND BALANCE 2L74 4F RT4A25 20030401001602003040100160WP 2003 4 1 DHL2003804767 120030212A573057695831N PANEL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING L/E OUTBD SLOT UPPER DOOOR SHOWS FOUR .250 CRACKS BTWN STA XS484.895 AND XS520.168 CORR: R & R LT WING OUTBD SLOT UPPER DOOR BETWEEN XS484.895 AND XS520.168 IAW MM. 2L74 4F RT4A25 20030401001632003040100163WP 2003 4 1 DHL2003804772 120030304A55435644220501 TAB DOUG DC8 DC873F 302199FWP RUDDER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 REMOVAL /INSTALLATION OF RUDDER TAB REQUIRED DUE TO DELAMINATION IN BOTH SIDES OF SKIN. R & R RUDDER TAB IAW MM 27-21-2 PG. 201-204 ADJUSTED RUDDER TAB IAW MM 27-21-2 PG. 204-207 REFER TO N/R 0607 FOR OPS CK 2L74 4F RT4A25 20030401001662003040100166WP 2003 4 1 DHL2003804775 120030212A535056563501 FILLET DOUG DC8 DC873F 302199FWP WING TO BODY DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING, WING TO FUSELAGE FILLET INNER SKIN DELAMINATED , STA 826.000 - STA. 912.000. R & R PANEL ON LT WING, WING TO FUSELAGE STA. 826.000-STA. 912.000 IAW SRM 51-3-0 PG. 1 2L74 4F RT4A25 20030401001672003040100167WP 2003 4 1 DHL2003804776 120030211A53307075T6 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD. SERVICE DOOR- AFT LOWER JAMB CORNER CRACKED 1.562 STA. 190.000. PERFORMED MAJOR REPAIR IAW SRO8530021 , REMOVED FASTNERS IAW SRM 51-1-20D PG. 21 CUT - OUT DAMAGED AREA IAW DWG SR8530021. FABRICATED FILLER AND DOUBLER (7075T6 .063 &TRIPLER (7075T6.080) IAW DRAWING SR08530021. CLEANED TREATED AND PRIMED FILLER ,DOUBLER & TRIPLER IAW SRM 51-1-8B. INSTALLED FILLER , DOUBLER AND TRIPLER WITH NEW FASTNERS IAW DWG SR08530021 , SRM 51-1-20D PG. 9 , SRM51-1-15 PG. 1. 2L74 4F RT4A25 20030401001682003040100168WP 2003 4 1 DHL2003804778 120030214A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 FWD ACCESSORY BAY FRAME CRACKED 1.00 INCH, STA. 55.000 L23R. PERFORMED MAJOR REPAIR IAW 53-2-0 PG. 20/21 FIG. 2 (SHEET 2)., REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 , SRM51-1-20D PG 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 PG. 20/21 SHEET 2 . FABRICATED NEW FRAME SEGMENT & SLICES IAW SRM53-2-0 PG. 20/21 FIG. 2 SHEET 2. HEAT TREATED IAW SRM 51-1-1 PG. 1-17 , SRM51-1-4, PG.1-3, DPS1-05.3, CLEANED , TREATED AND PRIMED IAW SRM53-2-0 PG.20/21 SHEET 2 , SRM51-1-21 PG. 1 , SRM51-1-20D PG. 9 FOR PNUE. DUCT R/R AND LEAK CK. SEE N/R 1834 2L74 4F RT4A25 20030401001722003040100172WP 2003 4 1 DHL2003804782 120030215A5754 ANGLE DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING CENTER L/E FORMER AND ANGLE DOUBLER UPPER PART CRACKED.500 INCH. AT XFS 420.000. REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21 PG. 1 , SRM 51-1-20D PG. 21 STOP DRILLED FORMER CRACK IAW SRM 57-2-0 PG. 9-10 FERFORMED HEAT TREATMENT IAW SRM 51-1-1 PG. 1-17 , SRM 51-1-4 PG. 1-3 AND DPS1-05.3. CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ABNGLES DOUBLER IAW SRM57-2-0 PG. 9-10 AND SRM 51=1=21 PG 1 SRM 51=1=20D PG. 9 2L74 4F RT4A25 20030401001732003040100173WP 2003 4 1 DHL2003804873 120030216A57305611002502 SKIN DOUG DC8 DC873F 302199FWP RT WING TE DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER PANEL SKIN DELAMINATED ( STA XW 5.000-47.000) R & R RT WING UPPER T/E PANEL (STA. XW5.000-47.000) IAW SRM 51-3-0 PG. 1 2L74 4F RT4A25 20030401001822003040100182WP 2003 4 1 DHL2003873004 120030307A2611 SMOKE DETECTOR DOUG DC8 DC873F 302199FWP CARGO BAY MALFUNCTIONED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01873SJ 46091 NR 6 POSITION SMOKE DETECTOR SELECT DOES NOT ILLUMINATE DURING TEST. MAY BE INOPERATIVE PER MEL 26-6-2 DMI NR 12210 PLACARD INSTALLED. REF. DMI NR 12210 NR 6 POSITION ON SMOKE DETECTOR SELECT DOES NOT ILLUMINATE DURING TEST. PERFORMED OPERATIONAL TEST OF NR 6 CARGO SMOKE DETECTOR PER DC-8 M/M 26-10-00. OPS CHECKED GOOD. THIS CLEARS DMI #12210. 2L74 4F RT4A25 20030401001842003040100184CE 2003 4 1 DIN2003F00000 120030210A242030B10719A GENERATOR LEAR 55 55LEAR 5170702CE GARRTTTFE731TFE731* 01518WP NR 1 ENGINE FAILED B DINRO OTHER O OTHER NRNOT REPORTED 1 EA13127GT 625 067 SHAFT SHEARED ON GENERATOR WITH RELATIVITY LOW TIME SINCE OVERHAUL. SHAFT SHEARED .5000 INCH FROM DRIVE SPLINE, SLIGHT CORROSION CAN BE SEEN AT FAILURE POINT. PERHAPS A MORE THOROUGH NDI DURING THE LAST OVERHAUL COULD HAVE FOUND THIS DEFECT. THE GENERATOR WAS SENT OUT FOR REPAIRS, THE SHAFT WAS REPLACED, NO OTHER DEFECTS WERE NOTED AND IT IS BACK IN SERVICE. NORMAL SCHEDULED MAINTENANCE ON THESE GENERATORS IS, 1050 HOURS TSO A BEARING CHANGE IS REQUIRED, AND AT 2000 HOURS TSO, OVERHAUL IS REQUIRED. (W) 2L72 4F4 F A10CE E6WE 20030402000052003040200005SO 2003 4 2 2003F00178 120030401A3297 WIRE PIPER PA32 PA32R300 7103213SO MLG BROKEN A UDPAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP23 32R7680084 SELECTED GEAR UP AND IT OPERATED NORMALLY. ABOUT 1/2 WAY THROUGH FLIGHT, THE PILOT NOTICED THE LANDING GEAR CIRCUIT BREAKER HAD TRIPPED. IT WOULD NOT RESET. RESET THE BREAKER AND THE GEAR OPERATED NORMALLY. A BROKEN WIRE WAS DISCOVERED IN THE LEFT WHEEL WELL THAT OPERATED THE SQUAT SWITCH AND IT HAD ELECTRICALLY SHORTED. THE WIRE WAS REPAIRED AND THE GEAR OPERATED NORMALLY ON JACKS. FAR 43.9 WAS COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L71 3O A3SO 20030402000122003040200012EU 2003 4 2 030903292 120030331A33501317 BULB JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY LIGHTSBURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27329UE 41097 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT FWD EXIT SIGN WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030402000142003040200014EA 2003 4 2 03091620 120030401A33500L6839BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA EMERGENCY SIGN BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27620BR 7179 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT EMERGENCY EXIT SIGN WAS INOPERATIVE.MAINTENANCE PERSONNEL REPLACED LAMP IN THE EMERGENCY EXIT SIGN OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030402000152003040200015EA 2003 4 2 03091623 120030401A335059257 INVERTER CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT INOPERATIVE A VTZAK NONE O OTHER ININSP/MAINT 1 EA27623BR 7192 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CENTER EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE PERSONNEL REPLACED AN INVERTERIN THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE 2L72 4F RTA21EA 20030408000692003040800069NM 2003 4 8 03FDEA00359 120030304A5740ARC050214 HINGE BRACKET DOUG MD11 MD11 3023602NM ZONE 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 RT WING, O/B FLAP, I/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2 EACH CORRODED. WINGS - RIGHT O/B FLAP, I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORROSION REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740- 68589. 2L73 4F RTA22WE 20030403000262003040300026NM 2003 4 3 03FDEA00360 120030401A5330 SKIN BOEING727 727200 138407ENM DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 N00175 EXTERIOR SKIN IS DENTED AT STA. 702F STR-4R. DENT AT 702F+15 STR 4R WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1, PG 2A, DETAIL II. CUT OUT DAMAGED SKIN 1 INCH DIAMETER AND REPAIRED IAW SRM 53-30-3. 2L73 4F RTA3WE 20030403000272003040300027NM 2003 4 3 03FDEA00361 120030401A5315 FLOORBEAM BOEING727 727200 138407ENM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CORROSION ON FLOORBEAM BS 1070 RBL 1 RBL 44, WL 201 AT FASTENER HOLES. REMOVED CORROSION ON LOWER FLOORBEAM BS 1070 RBL 1-44 AT FASTENER HOLES. ORIGINAL THICKNESS .130 REMOVED .010 MAX MATERIAL IN A 1 X 1 AREA RBL 1-RBL 26 & RBL 31-44 IN LIMITS PER SRM 53-10-1. REMOVED CORROSION ON BS 1070 FLOORBEAM RBL 27-30. ORIGINAL THICKNESS .130 REMOVED .053 MAX IN A 1.25 X 2.25 AREA OUT OF LIMITS PER SRM5 3-10-1. REMOVED DAMAGE RBL 27-31. FABRICATED AND DRILLED UP REPAIR PARTS. INSTALLED REPAIR PARTS AND FASTENERS WET WITH SEALANT ALL WORK ACCOMPLISHED IAW 727 SRM 51-10-8, FIG 8 AND 51-10-2. 2L73 4F RTA3WE 20030402000202003040200020EU 2003 4 2 0300643221 120030330A2910 O-RING AIRBUS320 A320211 3930320EU PTU MANIFOLD LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01321US 262 RECEIVED YELLOW SYSTEM HYDRAULIC RESERVOIR LOW LEVEL WARNING. ECAM INDICATED ZERO QUANTITY IN YELLOW SYSTEM RESERVOIR. DEACTIVATED YELLOW HYDRAULIC SYSTEM PER COM AND LANDED UNEVENTFULLY. REPLACED O-RING AT THE PTU MANIFOLD AND LEAK CHECKED OK. SERVICED YELLOW HYDRAULIC SYSTEM. RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA28NM 20030402000232003040200023NM 2003 4 2 03091405 120030401A3350 BULB DORNERDO32 DO328300 NM EMERGENCY LIGHT BURNED OUT A VTZAK NONE O OTHER ININSP/MAINT 1 EA27405FJ 3155 DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY EXIT SIGN LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REPLACED LIGHTS IN THE EMERGENCY EXIT SIGNS, AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUTED SERVICE 2H72 4T RTA55NM 20030625001342003062500134NM 2003 6 25 03FDEA00367 120030401A5330 SKIN BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 CONVEX DENT IN SKIN AT BS 1020, JUST ABOVE STR 26L CONVEX DENT IN SKIN AT BS 1020 JUST ABOVE STRINGER 26L, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 2A, DETAIL II. REMOVED DENT 1 INCH DIAMETER X .063. FABRICATED REPAIR AND INSTALLED IAW SRM 53-30-3 FIG. 24 USING .063 2024-T3 2L73 4F RTA3WE 20030408000712003040800071NM 2003 4 8 03FDEA00368 120030401A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 B/S 600 FRAME DENT STR 23L. DENT IN FRAME AT BS 600 STR 23L FOUND TO BE OUT OF LIMITS. REPAIRED PER FED-EX EA 7-5310-54458. 2L73 4F RTA3WE 20030403000302003040300030NM 2003 4 3 03FDEA00369 120030401A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25266FE 21672 MECHANICAL DAMAGE TO FRAME BS 420 BETWEEN STR 6 RT AND 7 RT. INSTALLED REPAIR CHANNEL ON FRAME PER SRM 53-10-4. 2L73 4F RTA3WE 20030402000262003040200026EU 2003 4 2 1140311144 120030114A2910109072924119 TRANSDUCER AGUSTAA109 A109E 0260119EU NR 2 HYD SYS INOPERATIVE A NXTAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SW19144CF12 11144 DURING PATIENT FLIGHT, NR 2 MAIN HYDRAULICS PRESSURE QUICKLY FELL INTO THE CAUTION RANGE. IN ANTICIPATION OF TOTAL LOSS NR 2 SYSTEM. I SLOWED BELOW VIE, EXTENDED GEAR ( 3 GREEN) CONTINUING TO SLOW TO 90 KNOTS. DECLARED AN EMERGENCY, MADE AN UNEVENTFUL PRECAUTIONARY LANDING. SLOW TO VIE, EXTEND LANDING GEAR, LANDED AT NEAREST AIRPORT. 1G72 3U RTH7EU 20030402000282003040200028NM 2003 4 2 2003UALA00235 120030301A2780755299B ACTUATOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE SLAT WORN A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29571UA3530035300 26681 SLAT DISAGREE INDICATION CAME ON AFTER TAKE-OFF. INHIBITED SLAT MOVEMENT DUE TO FAULTED NR 11 LEADING EDGE SLAT ACTUATOR. REMOVED AND REPLACED THE SUBJECT LEADING EDGE SLAT ACTUATOR WITH NEW SERVICEABLE ACTUATOR 2L72 4F4 FRTA2NM E17NE 20030402000412003040200041NM 2003 4 2 2003UALA00318 120030325A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN BODY FRAME STRINGER CLIP IS CRACKED AT BS 706, STR 4R. MAJOR REPAIR ACCOMPLISHED. NEW CLIP INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030402000422003040200042NM 2003 4 2 2003UALA00319 120030325A5313 STRINGER CLIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 CABIN BODY FRAME STRINGER CLIP IS CRACKED AT BS 639, STR 4RT. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP. 2L72 4F4 FRTA16WE E2GL 20030402000442003040200044NM 2003 4 2 2003UALA00321 120030325A5313 STRINGER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 STRINGER AT STA 500 TO 520 LEFT SIDE OF FUSELAGE DAMAGED. MAJOR REPAIR ACCOMPLISHED WITH STRINGER SPLICE 2L72 4F4 FRTT0001SE E46NE 20030402000452003040200045NM 2003 4 2 2003UALA00322 120030325A5330 SKIN BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29789UA 26935 SKIN AND STRINGER S38-L DAMAGED BETWEEN STA 508 AND 529. MAJOR REPAIR ACCOMPLISHED. DOUBLER APPLIED ON FUSELAGE SKIN LOCATED LEFT SIDE BELOW STR 38 LT BETWEEN STA 508 AND 529. 2L72 4F4 FRTT0001SE E46NE 20030402000462003040200046NM 2003 4 2 2003UALA00323 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT AT STA 1340 BETWEEN STR 25L AND 26L, TOP OF FRAME IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20030402000472003040200047NM 2003 4 2 2003UALA00324 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1420 BETWEEN STR 25L AND 26L, UPPER FRAME FLANGE DENTED MAJOR REPAIR ACCOMPLISHED. PERFORMED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20030402000492003040200049NM 2003 4 2 2003UALA00326 120030322A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29553UA 25277 AFT PIT STA 1360 ABOVE STR 26L, TOP OF FRAME FLANGE IS DENTED MAJOR REPAIR ACCOMPLISHED. COMPLETED FRAME REPAIR 2L72 4F4 FRTA2NM E17NE 20030402000532003040200053NM 2003 4 2 2003UALA00330 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 847, STR 9R, FRAME WEB IS CRACKED AT FASTENER HOLE MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT, DOUBLER INSTALLED 2L72 4F4 FRTA16WE E2GL 20030402000542003040200054NM 2003 4 2 2003UALA00331 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 847, STR 8L FRAME WEB IS CRACKED AT FASTENER HOLE MAJOR REPAIR ACCOMPLISHED. CRACK REMOVED, REPAIR DOUBLER INSTALLED 2L72 4F4 FRTA16WE E2GL 20030402000552003040200055NM 2003 4 2 2003UALA00332 120030325A335020131 BATTERY PACK BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29917UA 25384 EMERGENCY ELECTRICAL LIGHTING (EEL) ADJACENT TO ROW 18 INOPERATIVE. REPLACED EEL BATTERY PACK AND FEEDER STRIP. 2L72 4F4 FRTA16WE E2GL 20030402000562003040200056NM 2003 4 2 2003UALA00333 120030327A5755 WARNING LIGHT BOEING747 747422 1384935NM PWA 4056 PW4056 NE SPOILER INOPERATIVE A UALALA ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION LDLANDING 1 WP29180UA 25224 A/C RECEIVED NO RIGHT SPOILER INPUT/RESPONSE ON APPROACH INTO LAX 2L74 4F4 FRTA20WE E24NE 20030402000582003040200058NM 2003 4 2 2003UALA00335 120030327A5347 SEAT TRACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 SEAT TRACK CORRODED, BS 800-808, LBL 52. MAJOR REPAIR ACCOMPLISHED. REPAIRED SEAT TRACK WITH SPLICE SECTION AND FILLERS. 2L72 4F4 FRTA1NM E24NE 20030402000592003040200059NM 2003 4 2 2003UALA00336 120030307A5754114W41113 SKIN BOEING777 777222 1385219NM NR 1 SLAT CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29785UA 26954 NR 1 SLAT, OTBD LOWER L/E SKIN CRACKED. MAJOR REPAIR ACCOMPLISHED. CRACK REPAIRED W/EXTERNAL DOUBLER. 2L72 4F RTT0001SE 20030402000632003040200063NM 2003 4 2 2003UALA00340 120030305A5754114W424011 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 6 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED 2L72 4F4 FRTT0001SE E46NE 20030402000662003040200066NM 2003 4 2 2003UALA00343 120030303A5754114W42102 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 14 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 26919 T/E WEDGE DELAMINATED - NR 14 SLAT, WITH BULB SEAL FOAM CORE SECTION IS MISSING. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030402000672003040200067NM 2003 4 2 2003UALA00344 120030316A5754114W413016 WEDGE BOEING777 777222 1385219NM SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 T/E WEDGE, SLAT ASSEMBLY, DELAMINATED. MAJOR REPAIR ACCOMPLISHED. T/E WEDGE WAS REPAIRED. 2L72 4F RTT0001SE 20030402000722003040200072NM 2003 4 2 A6WA200330005 120030304A3260DOLN1076B CONNECTOR DORNERDO32 DO328100 2996000NM GROUND MATRIX INTERMITTENT A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31331MX 3074 PROXY SYSTEM FAIL MESSAGE IN FLT. FOUND INTERMITTENT CONNECTION AT GROUND MATRIX 80VPNV. CLEANED AND RERACKED GROUND MATRIX. OPS CHECK GOOD AT THIS TIME. (IPC REF: 24-50-01-1-370) 2H72 4T RTA45NM 20030403000252003040300025NM 2003 4 3 03013 120030331A5210 STRUCTURE BOEING747 747132 1384882NM PAX DOOR TORN A KCSAK NONE O OTHER ININSP/MAINT 1 GL23709CK 20247 ON THRU FLIGHT INSPECTION, FOUND L-2 DOOR FORWARD LOWER EDGE BELOW BOTTOM HINGE TO LOWER "R" STRAP PULLED LOOSE AND TORN. APPROX. SIZE 10 INCH ON FRONT; BOTTOM BROKE LOOSE APPROX. 6 INCH AFT; SHEET METAL IS TORN UPWARD APPROX. 6 INCHES. 2L74 4F A20WE 20030403000312003040300031NM 2003 4 3 03FDEA00373 120030401A3110 WARNING LIGHT BOEING727 727200 138407ENM WINDSHEAR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25207FE 22929 DURING INITIAL CLIMB PASSING 800-1000 FT WE EXPERIENCED A RED WINDSHEAR WARNING AND AURAL WARNING. WE PERF THE EMERGENGY ESCAPE MANUVER AND IMMEDIATELY FIREWALL ALL THRUST LEVERS. WARNING LASTED 5 SECONDS. THRUST LEVERS WERE THEN RETARDED TO MAX POWER. #1 EPR READ 2.15 WITH MAX ON T.O.L.D CARD 1.94. WE DID HAVE DECREASING A/S INITIALLY. DIVERSION FLIGHT TIME WAS 31 MINUTES AT 14000 FEET PERF INLET AND EXHAUST INSPECTION. PERF ANALYTICAL ANALYSIS WORKSHEET ON ALL THREE ENGINES PER JRH FIREWALL AND OR EMERGENCY ESCAPE CHECK ON PAGE 6-38 AND 6-38A PREF BITE TEST OF GPWS PER 32- 52-000-1. NO FAULTS ANNUNCIATED C/W INSPECTION PROCEDURES PER E.A. 78-7100-69076. 2L73 4F RTA3WE 20030403000322003040300032EU 2003 4 3 148891 120030402A3220 LANDING GEAR SAAB SF340 SF340A 7850100EU NLG VIBRATION A UHLAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 GL17149SZ 340A149 FLIGHT 4507 CRW-PIT. A/C EXPERIENCED SEVERE NOSEWHEEL SHIMMY AT ABOUT 40-45 KNOTS DURING INITIAL TAKE-OFF ROLL. CREW ABORTED TAKE-OFF AND RETURNED TO GATE. CREW DID NOT EXPERIENCE ANY SHIMMY DURING NORMAL TAXIING. A/C TAKEN OUT OF SERVICE 4-2-03 AT1519. 2L72 4T RTA52EU 20030403000352003040300035 2003 4 3 249TR0016 420030331A2220 WARNING LIGHT BOEING737 7372K5 138448XNM MACH TRIM ILLUMINATED A PIDAO OTHER N FALSE WARNING CRCRUISE 1 SO05249TR 22598 MACH TRIM FAIL LIGHT ILLUMINATED DURING FLIGHT. UNABLE TO DUPLICATE. PERFORMED BITE TEST VIA PDCS CDU, NO FAULTS NOTED. 2L72 4F RTA16WE 20030403000362003040300036EU 2003 4 3 46831 120030402A2422 WARNING LIGHT SAAB SF340 SF340A 7850100EU MAIN INVERTER ILLUMINATED A UHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL17108CQ 340A108 FLIGHT 4536 PIT-HGR. JUST AFTER TAKE-OFF FROM PIT DURING CLIMB THE MAIN INVERTER FAIL LIGHT ILLUMINATED. CREW FOLLOWED QRH AND SWITCHED TO THE STANDBY INVERTER. TRANSFER WAS GOOD WITH NO SYSTEM FAILS. A/C TURNED AROUND AND RETURNED TO GATE AT PIT. A/C WAS TAKEN OUT OF SERVICE. 2L72 4T RTA52EU 20030403000392003040300039NM 2003 4 3 AMTA200300254 120030222A335020131A BATTERY PACK BOEING757 75723N 1384973NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11519AT 27975 FOUND ROW 1-4 BULLNOSE EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 DOOR BATTERY PACK IAW AMM 33-51-07, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 20030403000432003040300043NM 2003 4 3 AMTA200300259 120030223A3350 FUSE BOEING757 75723N 1384973NM POWER SUPPLY BLOWN A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11524AT 30233 ROW 23 EMERGENCY EXIT AISLE LIGHT INOPERATIVE. REPLACED POWER SUPPLY FUSE AT POWER SUPPLY M733 PER 33-51-07-2. OP SCHECK GOOD AT THIS TIME. (M) 2L72 4F RTA2NM 20030403000442003040300044NM 2003 4 3 AMTA200300285 120030227A28226075504 PUMP BOEING757 75728A 1384976NM FUEL BOOST INOPERATIVE A AMTAO OTHER O OTHER NRNOT REPORTED 1 GL11521AT 24368 RIGHT AFT FUEL BOOST PUMP C/B POPPED. PERFORMED INSULATION RESISTANCE AND BONDING CHECKS PER MM 28-22-03. OPS CHECKED OK. REFERENCE LP 543952 FOR RIGHT AFT BOOST PUMP REMOVED AND REPLACED. (M) 2L72 4F RTA2NM 20030403000462003040300046NM 2003 4 3 AMTA200300305 120030304A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 EPL RED LIGHT 1 EACH AT ROW 29 INOPERATIVE. FOUND DISCONNECTED EPL WIRE AND 32D, CIRCUIT TO RED LIGHT AT 29 VERIFIED OPERATIVE. (M) 2L72 4F RTA2NM 20030403000642003040300064SO 2003 4 3 ASOA03056 120030211A541012039731001 FRAME EMB 120 EMB120ER 3260203SO NACELLE CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11266AS 120188 DURING A HANGAR CHECK IT TXK, THE LOWER AFT SECTION NACELLE HALF-FRAME WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER AFT SECTION NACELLE HALF-FRAME IAW SRM 54-20-04. (M) 2L72 4T RTA31SO 20030403000652003040300065EU 2003 4 3 ASOA03058 120030213A33502275941249 LIGHT AEROSPATR72 ATR72212 8680945EU CABIN INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11635AS 372 DURING A HANGAR CHECK IN MCN, THE FLOOR EMERGENCY LIGHT AT SEATS 14 A-B WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A FLOOR EMERGENCY LIGHT GROUND WIRE AT SEATS 14 A-B. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2H72 4T RTA53EU 20030403000662003040300066NM 2003 4 3 AWXA200300328 120030330A2730285T0015116 COMPUTER BOEING757 757225 1384959NM STAB TRIM MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28913AW 22207 ON CLIMB OUT, RECEIVED EICAS MESSAGE "ELEV ASYM", NO ADVERSE CONTROL FEEL, TURNED BACK FOR REPAIR. MAINT R & R LT STAB TRIM AILERON LOCKOUT COMPUTER, OPERATIONAL TEST GOOD. PERFORMED TEST FLT TO VERIFY SYS INTEGRITY; PRIOR TO FIRST TAKEOFF PULLED RT ADC CIRCUIT BREAKER TO DEFAULT TO LT STAB TRIM AILERON COMPUTER, A/C FLEW WITHOUT EVENT. RESET RT ADC CIRCUIT BREAKER AND PULLED LT BREAKER TO ISOLATE RT STAB TRIM AILERON COMPUTER. ON CLIMB AT APPROX 230 KTS RECEIVED EICAS MESSAGE "ELEV ASYM", CLEARED PRIOR TO LANDING. INSPECTED BOTH STAB TRIM AILERON COMPUTERS, NO FAULTS NOTED. VERIFIED ELEVATOR ASYM ACT MOVES FROM HIGH SPEED & RETURNS TO NORMAL. R & R RT STAB TRIM AILERON L/O COMPUTER, OPS TEST GOOD. 2L72 4F RTA2NM 20030403000672003040300067NM 2003 4 3 AWXA200300329 120030324A5320654860713 WEB BOEING737 7373G7 1384595NM WING-BODY FAIRINCRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON RT WING TO BODY FAIRING LOWER STRUCTURE WEB, BS 530. MAINTENANCE CUTOUT DAMAGED SECTION OF R/H WING TO BODY FAIRING LOWER STRUCTURE WEB AT BS 530; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-13, FIG. 1, PG. 1-3. 2L72 4F RTA16WE 20030403000702003040300070NM 2003 4 3 AWXA200300332 120030326A53206517684642 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 DURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON FORWARD OUTBOARD CORNER OF INTERCOSTAL, JUST FORWARD OF L-1 DOOR AT BS 294 TO BS 303, STR 7 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 294 TO BS 303, STR 7 L/H; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-17684; INSTALLED REPAIR PART IAW B737-300 SRM 51-10-02, PG. 12 2L72 4F RTA16WE 20030328000042003032800004NM 2003 3 28 CA030212008 120030212A323282970018011 CYLINDER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG DOOR UPLOCK CORRODED W O OTHER O OTHER NRNOT REPORTED 1 CA LI0021 (CAN) DURING SCHEDULED AIRCRAFT INSPECTION MLG DOOR UPLOCK ACTUATOR FOUND LEAKING. COMPONENT REMOVED AND SENT TO SHOP, SHOP INSPECTION FOUND SEVERE CORROSION IN THE UPLOCK PISTON ROD BORE AND PISTON RETAINING NUT . PART DETERMINED BEYOND ECONOMICAL REPAIR. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030328000062003032800006EA 2003 3 28 CA030213001 120030208A792128E997 OIL COOLER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE ENGINE LEAKING W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN) NR 1 ENGINE OIL COOLER FOUND LEAKING FROM LOWER COOLING FINS. OIL COOLER REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20030328000092003032800009NE 2003 3 28 CA030214003 220030207A8520LW13923 BUSHING PIPER PA60 PA60602P 7106015NM LYC O540 IO540AA1A 41532NE CONNECTING ROD CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA (CAN) DURING INSPECTION OF AN ENGINE IN FOR CRANKCASE REPAIR AND AD 2002-20-51, 4 OUT OF 6 CONNECTING ROD BUSHINGS WERE FOUND CRACKED OR BROKEN. SOME BUSHINGS HAD ROTATED IN THE CONNECTING ROD, PROBABLY AFTER CRACKING.NO HISTORY OF OVERBOOST, OVERSPEED, OR DETONATION REPORTED. 1M72 3O3 ORTA17WE 1EA 20030328000192003032800019SW 2003 3 28 CA030218004 120030212A6510206040106001 SPRING BELL BELL 206 206L 1181522SW ALLSN 25OC 250C20R GL DRIVESHAFT BROKEN W O OTHER O OTHER NRNOT REPORTED 1 CA AMN10022 (CAN) SPRING BROKE, TURNED SIDEWAYS AND CHAFED SPHERICAL COUPLING AND PLATE. 1G71 3U3 U H2SW E4CE 20030328000232003032800023EU 2003 3 28 2003FA0000327 120030320A4930160353500 LINE BRAERODH125 BAE125800A 1500285EU APU FUEL LEAKING C O OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL0774NP 1286 NA0440 AFTER APU SHUTDOWN PILOT OBSERVED SMOKE COMING FROM TAILCONE JUST PROIR TO ATTEMPTING REFUEL. REFUEL PROCESS ABORTED AND REARBAY ACCESS DOOR OPENED TO INVESTIGATE. CREW MEMBER OBSERVED DENSE WHITE SMOKE COMING FROM REAR BAY. FURTHER INVESTIGATION REVEALED A SPLIT IN THE FUEL MANIFOLD FOR THE APU. SBT62T49108 ADDRESSES THIS PROBLEM, HOWEVER IT IS ONLY AN OPTIONAL BULLETTIN. 2L72 4F RTA3EU 20030328000252003032800025EU 2003 3 28 03084302 120030325A3350 LIGHT JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27302UE 41013 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WAS INOPERATIVE. MAINTENANCE PERSONNEL SECURED A LOOSE CONNECTOR FOR THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA41NM 20030328000442003032800044SO 2003 3 28 C2XA03TY030 120030226A531014525480003 SILL EMB 145 EMB145ER 3260211SO CARGO DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714938 145029 DURING A SCHEDULED 3C INSPECTION THERE WAS EVIDENCE OF CORROSION UNDER THE CARGO DOOR SILL PROTECTIVE PLATE. MAINTENANCE DRILL OUT THE RIVETS IN SILL, REMOVED CORRODED PARTS, FAB NEW BRACKETS AND INSTALL ALONG WITH A NEW CARGO SILL IAW EMB 135/145 SRM 51-40-02; SRM 51-30-01 AND EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030328000452003032800045SO 2003 3 28 C2XA03TY031 120030226A5530145207350003 HOUSING EMB 145 EMB145LR 3260212SO VERTCAL STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716981 145208 DURING A SCHEDULED 2C INSPECTION THE LT AND RT VERT STAB SPHERICAL BEARING HOUSING HAD LITE CORROSION. MAINTENANCE REWORKED BOTH VERTICAL BEARING HOUSINGS IAW EC 5510-01052 AND EMB 145 AMM 51-50-01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000462003032800046SO 2003 3 28 C2XA03TY034 120030313A531014521699003 BEAM EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2716911 145446 DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM AT FRAME 20 WAS CORRODED. MAINTENANCE CUT OUT DAMAGED AREA, FAB, ALODINE, PRIME, PAINTED AND INSTALLED REPAIRED DOUBLER, FILLER AND SHIMS IAW EMB 135/145 SRM 53-21-10, 51-40-02;CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK. 2L72 4T RTT00011AT 20030328000582003032800058NM 2003 3 28 CALA0300094 120030221A5320 STRUCTURE BOEING737 7373T0 1384582NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912313 23364 MAINTENANCE FOUND THE AFT CARGO DOOR LOWER BEAM TEE CHORD CRACKED. TWO CRACKS WERE EMANATING FROM A RIVET HOLE. THE CRACKS WERE 0.4 INCH LONG AND 0.8 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5230-01715. A DIP WAS ISSUED TO ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS. 2L72 4F RTA16WE 20030328000852003032800085EA 2003 3 28 COMA0360067 120030131A5530600210615 BUSHING CNDAIRCL600 CL6002B19 1900309EA VERTICAL STAB LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01989CA12093 7215 THE LT VERTICAL STABILIZER LUG BUSHING WAS MIGRATED .025 INCH AT THE HORIZONTAL STABILIZER PIVOT POINT. REMOVED THE MIGRATED BUSHING. PERFORMED NDT/LP1 TO ENSURE NO DAMAGE TO LUG BORE. MACHINED AND INSTALLED A 1ST OVERSIZED BUSHING I/A/W REO 601R-55-31-044. 2L72 4F RTA21EA 20030328000932003032800093CE 2003 3 28 CWQ2003F00002 120030122A21206512072101 DUCT CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE NACA SCOOP MISOVERHAULED B CWQRO OTHER O OTHER NRNOT REPORTED 1 GL05309QS 5600509 DURING INSPECTION, LOOKED INTO DORSAL NACA SCOOPS,MATERIAL MISSING FROM AIR VANES PN 6512072-11, 6512072-12 LOCATED IN TRANS DUCT MISSING MATERIAL LOCATION WAS A CONCERN BECAUSE ITS ONLY ROUTE WAS TO END UP IN VENT J-BOX (AIR MIXING BOX) WHERE IT WOULD HAVE PASSED CABIN PRESS, FRESH AIR CHECK VALVE (POSSIBLY WEDGING VALVE OPEN) THIS WOULD HAVE NOT ALLOWED A/C TO HOLD PRESS. 1ST PIECE WAS FOUND WEDGED IN CHECKVALVE (VALVE COULD NOT SEAL) 2ND PIECE WAS FOUND PAST OVERHEAD BLOWER WEDGED IN DUCT WORK (NO DAMAGE TO BLOWER CAGE). LOCATED BROKEN PARTS REMOVED, REPLACED BROKEN PARTS WITH NEW. CLOSED UP CABIN INTERIOR AND DUCT WORK. REASSEMBLED TAILCONE DUCTING. CHECKVALVE WAS SERVICEABLE REINSTALLED. 2L72 4F4 FRTA22CE E25EA 20030328001012003032800101EU 2003 3 28 CX7A194J33 120030302A61208210172 GOVERNOR SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE OVERSPEED DEFECTIVE A CX7ACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL03301CE 340B191 IMMEDIATELY AFTER T/O NOTICED AN UNUSUAL YAW, NOTED LEFT PROP RPM WAS ERRATIC. IT WOULD NOT EXCEED 1340 RPM. T/M LOCKOUT HAD NO AFFECT PER CHECKLIST. ALL OTHER ENGINE INDICATIONS NORMAL. 2L72 4T RTA52EU 6 CP11NE 20030328001022003032800102CE 2003 3 28 DBC2003F00001 120030225A3260H1113071 UPLOCK SWITCH CESSNA650 650 2076802CE GARRTTTFE731TFE731* 01518WP LT MLG FAILED E DBCAO OTHER N FALSE WARNING CLCLIMB 1 GL1316SU 6500025 AFTER DEPARTING PBI PILOT SELECTED LANDING GEAR UP. LANDING GEAR RETRACTED AND HANDLE IN-TRANSIT LIGHT EXTINGUISHED. A COUPLE OF SECONDS LATER, LANDING GEAR HANDLE IN TRANSIT LIGHT ILLUMINATED FOLLOWED BY IN TRANSIT LIGHT EXTINGUISHING AND LEFT MAIN DOWN AND LOCKED LIGHT ILLUMINATING. PILOTS SELECTED GEAR DOWN AND RETURNED TO PBI. LANDING GEAR WAS UNEVENTFUL. AIRCRAFT WAS PLACED ON JACKS AND A RETRACTION TEST WAS PERFORMED. IT WAS DETERMINED THE UPLOCK SWITCH HAD FAILED WHICH PREVENTED SOLENOID VALVE FROM OPENING AND APPLYING HYDRAULIC PRESSURE TO UPLOCK ACTUATOR. UPLOCK SWITCH REPLACED. OPERATIONS CHECKED GOOD. 2L72 4F4 F A9NM E6WE 20030328001032003032800103CE 2003 3 28 DEBA391MT0103 120030124A304010138402522 WINDSHIELD BEECH 300 300BEECH 1152930CE COCKPIT CRACKED E DEBAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03391MT844 FA111 CO-PILOTS WINDSHIELD INNER PANE SHATTERED IN FLIGHT. WINDSHIELD HEAT WAS NOT TURNED ON AT THE TIME. 2L72 4T A24CE 20030331000162003033100016EA 2003 3 31 A6WA200340022 120030106A5320 BRACKET CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 HYDRAULIC BRACKET AT FS 656 RT SIDE AT STRINGER 9 HAS AN ELONGATED THRU HOLE AT HYDRAULIC PRESSURE LINE REMOVED BRACKET, REPAIRED, AND REINSTALLED. PERFORMED NDT WITH NO INDICATIONS NOTED. 2L72 4F RTA21EA 20030331000192003033100019EA 2003 3 31 A6WA200340025 120030106A5311 FRAME CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 FS FRAME 718 IS CRACKED .25 INCHES AT TOP RIVET HOLE AT STRINGER 11 LT SIDE, INCORPORATED MFG REO 601R-53-61-193 REV A. 2L72 4F RTA21EA 20030331000202003033100020EA 2003 3 31 A6WA200340026 120030105A5320 ACCESS PANEL CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DAMAGED A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31404AW 7294 RT BOOST PUMP ACCESS HOLE HAS FAILED FASTENER HOLE AT 1:00 O`CLOCK POSITION PERFORMED REPAIRS NR 1 AND NR 2 OF REO 601R-57-21-169 BY OPENING UP HOLE. FABRICATING BUSHING AND INSTALLING BUSHING. 2L72 4F RTA21EA 20030331000382003033100038WP 2003 3 31 AALA20030086 120030121A335060030451 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW2176200 53290 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHTS IN AFT GALLEY AREA INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY FOR AFT GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030331000422003033100042WP 2003 3 31 AALA20030189 120030209A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21228AA 49178 SAN - DURING OVERNIGHT MAINTENANCE, AFT HALF OF SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY. SYSTEM GROND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000442003033100044WP 2003 3 31 AALA20030192 120030212A3350P4010049 BATTERY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21456AA 49561 DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN AFT ACCESSORY COMPARTMENT INOPERATIVE. RESEATED EMEGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 20030331000702003033100070EU 2003 3 31 ASOA03094 120030216A5310 THRESHOLD AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, PASSENGER DOOR DRAIN GUTTER THRESHOLD BETWEEN FRAMES 36L TO 39L WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED PASSENGER DOOR DRAIN GUTTER THRESHOLD BETWEEN FRAMES 36L TO 39L IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000712003033100071EU 2003 3 31 ASOA03095 120030216A5320S5367800821600 ANGLE AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE RIGHT Z-ANGLE BETWEEN FRAMES 39R TO 41R WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT Z-ANGLE BETWEEN FRAMES 39R TO 41R IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000722003033100072EU 2003 3 31 ASOA03096 120030216A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE SEAT TRACK BETWEEN FRAMES 31R TO 36R, WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK BETWEEN FRAMES 31R TO 36R, IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000732003033100073EU 2003 3 31 ASOA03097 120030216A5347 SEAT TRACK AEROSPATR72 ATR72212 8680945EU PWA PW120 PW127 NE FUSELAGE CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO11533AS 460 DURING C-CHECK INSPECTION, THE SEAT TRACKS BETWEEN FRAMES 36R TO 39R AND 39L TO 41L WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS BETWEEN FRAMES 36R TO 39R AND 39L TO 41L IAW SRM. 2H72 4T4 TRTA53EU E20NE 20030331000902003033100090SO 2003 3 31 C2XA03SH075 120030329A532014524131009 SUPPORT BRACKET EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE PASSENGER DOOR THRESHOLD SUPPORTS WHERE FOUND TO BE CORRODED BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT BRACKETS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000912003033100091SO 2003 3 31 C2XA03SH076 120030330A531013500322001 SILL EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT SILL BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000922003033100092SO 2003 3 31 C2XA03SH077 120030330A531014522460015 BUTT STRAP EMB 145 EMB145LR 3260212SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT BUTT STRAP BETWEEN FRAMES 17 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331000932003033100093SO 2003 3 31 C2XA03SH078 120030330A532014524199401 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK, THE LT OUTBOARD FLOOR SUPPORT AT FRAME 18 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20030331001032003033100103EA 2003 3 31 COMA0360165 120030326A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 1900309EA LEFT FAILED A COMAO OTHER O OTHER CRCRUISE 1 SO01971CA15030 7145 FLT 5016 PILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW. 2L72 4F RTA21EA 20030331001042003033100104EA 2003 3 31 COMA0360166 120030326A3350 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT DAMAGED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01937CA 7044 FLIGHT 5214, 1ST SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERATIVE. SECURED WIRING CONNECTOR ON FLOOR STRIP LIGHTING. 2L72 4F RTA21EA 20030331001152003033100115EU 2003 3 31 DHL2003368001 120030114A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU LAVATORY MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01506TA 207 LAV SMOKE DETECTOR SOUNDED HAD TO BE DISCONNECTED. OPS CHECKED SMOKE DETECTOR IAW M/M 26-17-00. OPS CHECKED GOOD. 2L72 4F RTA35EU 20030331001162003033100116NM 2003 3 31 DHL2003704508 120030203A5311 FRAME BOEING727 727200 138407ENM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 520 IS DENTED BETWEEN STR 16-R AND 17-R. ROUTED CRACK AREA APPROX 730 X 1.210. FABRICATED REPAIR DOUBLER FROM 7075-T6 .063. TREATED AND PRIMED AND INSTALLED PER SRM 51-40-1 FIG 1. 2L73 4F RTA3WE 20030331001342003033100134NM 2003 3 31 DHL2003740515 120030203A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH AFT CARGO COMPT AFT PIT FLOORBEAM AT RBL 15 IS CRACKED AT NUT PLATE STA 950E. REMOVED FASTENERS PER SRM 51-30-2. FABRICATED DOUBLER ANGLES (2024-T3 .050) PER SRM 51-40-3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 51-30-2. 2L73 4F RTA3WE 20030331001352003033100135NM 2003 3 31 DHL2003740516 120030204A5311 FRAME BOEING737 7372Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH UPPER MAIN DECK CARGO DOOR FUSELAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACHED TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABBED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .050 PER SRM 53-10-4 FIG 11. PARTS TREATED AND DRILLED PER SRM 51-10-2. INSTALLED REPAIR PER SRM 53-10-4 AND 51-30-2. 2L72 4F A16WE 20030331001362003033100136NM 2003 3 31 DHL2003740517 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO015311 FUESLAGE FRAME AT STA 540 IS DENTED BETWEEN STR 16R-17R. CUT OUT DENTED AREA AND FABRICATED REPAIR PER SRM 51-40-3. TREATED AND PRIMED REPAIR PARTS AND INSTALLED PER SRM 51-40-1 FIG 1. 2L73 4F RTA3WE 20030331001372003033100137NM 2003 3 31 DHL2003740518 120030203A5311 FRAME BOEING727 7272Q9 138448MNM FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH FUSELAGE FRAME AT STA 580 IS DENTED AND CRACKED BETWEEN STR 16R-17R. REMOVED DAMAGED AREA, NO CRACK FOUND. FABRICATED REPAIR PART FROM 7075-T6 .063 AL PER SRM 51-40-3. TREATED, PRIMED AND INSTALLED PER SRM 51-40-3 FIG 1. 2L73 4F RTA3WE 20030401000072003040100007EA 2003 4 1 03089664 120030330A33502013BR BATTERY PACK CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27664BR 7528 DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FWD EMERGENCY FLOOR TRACK LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE #2 EMERGENCY BATTERY PACK. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000082003040100008EA 2003 4 1 03090647 120030331A33503071BPEGPL BULB CNDAIRCL600 CL6002B19 1900309EA CABIN BURNED OUT A VTZAK NONE L NO TEST ININSP/MAINT 1 EA27647BR 7399 DURING MAINTENANCE INSPECTION, AN EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20030401000182003040100018WP 2003 4 1 AALA20030219 120030220A3350P4010049 BATTERY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21438AA 49456 DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 12-17 AISLE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 20030401000342003040100034EA 2003 4 1 ASOA03054 120030210A33501317 LIGHT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO11846AS 7328 DURING A GROUND INSPECTION IN DFW, THE RIGHT SIDE AFT EMERGENCY LIGHT OVERWING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT SIDE AFT EMERGENCY LIGHT LAMP. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA21EA 20030401000362003040100036NM 2003 4 1 AWXA200300323 120030328A3397BMS13311122 WIRE BOEING737 737277 1384570NM SEAT ROW 2 LT BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030401000372003040100037NM 2003 4 1 AWXA200300324 120030328A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT ROW 8 LT BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28151AW 23219 FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030401000412003040100041GL 2003 4 1 C2XA03CL079 220030325A724023074735 COMBUSTION LINER EMB 145 EMB145 3260210SO ALLSN AE300 AE3007A GL NR 2 ENGINE WRONG PART A C2XAK NONE O OTHER ININSP/MAINT 1 SW27111091066 145657 CAE312285 3/25/03 EXPRESS JET AIRLINES WAS NOTIFIED BY ROLLS ROYCE THAT AIRCRAFT 11109, NR 2 ENGINE HAD THE WRONG P/N COMBUSTION LINER INSTALLED AT THE FACTORY. THE AIRCRAFT WAS FERRIED TO CLEVELAND FOR A ENGINE CHANGE. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030401000452003040100045SO 2003 4 1 C2XA03SH081 120030331A533014527605003 SKIN EMB 145 EMB145LR 3260212SO FUSELAGE GOUGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2714953 145071 DURING C-CHECK SKIN WAS FOUND GOUGED UNDER GPU ACCESS PANEL BETWEEN FRAMES 6 AND 8. MAINTENACE REMOVED DAMAGE AND REPAIRED SKIN IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20030401000492003040100049EA 2003 4 1 CA030219003 120030218A2932ACA3581D71 CHECK VALVE CNDAIRCL600 CL600* EA LYC ALF502ALF502L2C NE HYD SYSTEM INADEQUATE W K NONE N FALSE WARNING ININSP/MAINT 1 CA (CAN) NR 2 HYDRAULIC MANIFOLD EDP (ENGINE DRIVEN PUMP) CHECK VALVE BACKS OUT, O-RING AND BACKUP RING SHEAR ALLOWING PRESSURE INTO THE EDP PRESSURE SWITCH WHEN THE ELECTRIC PUMP IS ON AND ENGINE IS SHUT DOWN. RECURRING DEFECT DUE TO IMPROPER LOCKING DEVICE ON THE CHECK VALVE. MFG FIELD SERVICE REP. NOTIFIED. NO ACTION TAKEN BY MANUFATURER. 2L72 4F4 FRTA21EA E6NE 20030401000552003040100055EA 2003 4 1 CA030221005 120030217A5610NP1393213 WINDSHIELD CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343A1 30015NE COCKPIT BROKEN W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 11696 (CAN) WHILE TAXIING, CAPTAINS WINDSHIELD SHATTERED. TEMP -26, THIS WAS THE ORIGINAL WINDSHIELD. WINDSHIELD TOTAL TIME 11,696 2L72 4F4 FRTA21EA E15NE 20030401000922003040100092NM 2003 4 1 DHL2003747003 120030129A2612 FIRE DETECTOR BOEING727 727224 1384076NM NR 1 ILLUMINATED A DHLAO OTHER J WARNING INDICATION NRNOT REPORTED 1 SO01747DH 22253 FIRE PROTECTION DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED, NR 1. PLACED ON MEL 26-9-1 DMI 11789. PLACARDS INSTALLED. REF DMI NR 11789 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. OPS CHECK NR 1 ENG FIRE DETECTOR, NO DEFECTS NOTED PER MM 26-11-001. THIS CLEARS DMI 11789. 2L73 4F A3WE 20030401000942003040100094NM 2003 4 1 DHL2003751004 120030131A2612 FIRE DETECTOR BOEING727 727264 138408MNM NR 1 ENGINE INOPERATIVE A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01751DH 22982 NR 1 ENGINE FIRE DETECTION A-SYSTEM INOP. NR 1 ENGINE FIRE DETECTION A-SYSTEM MAYBE INOP AND DEFERRED PER MEL 26-6. ASSIGNED DMI 11822 PLACARD INSTALLED. REF DMI 11822 NR 1 ENGINE FIRE DETECTION A-SYSTEM INOP. REF DMI 11822 NR 1 ENGINE FIRE DETECTION A-SYSTEM TESTED IAW M/M 26-11-0. OPS CHECKED NORMAL. NO DEFECTS NOTED. THIS ACTION CLEARS DMI 11822. PLACARDS REMOVED. 2L73 4F A3WE 20030401001022003040100102NM 2003 4 1 DHL2003780004 120030327A3350 BATTERY BOEING727 727223 1384074NM EMERGENCY LIGHT DISCHARGED A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01780DH 22006 BOTH EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES, OPS CHECKED NORMAL IAW M/M 33-50-71. 2L73 4F A3WE 20030401001032003040100103NM 2003 4 1 DHL2003782001 120030318A2611 CONNECTOR BOEING727 727227 1384078NM SMOKE DETECTOR DIRTY A DHLAK NONE L NO TEST ININSP/MAINT 1 SO01769AT 21998 MAIN CARGO SMOKE DETECTION SYSTEM NR 2 LIGHT FLASHES WHEN TEST SWITCH PRESSED. CLEANED AND RESEATED CONNECTOR PLUG. OPS CHECKED GOOD IAW M/M 26-17-01. 2L73 4F A3WE 20030401001182003040100118WP 2003 4 1 DHL2003804510 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER LOWER PART CRACKED AT 1/2 IN STA XFS 460.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001192003040100119WP 2003 4 1 DHL2003804511 120030117A5754 FRAME DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 RT WING CENTER L/E FORMER UPPER PART CRACKED AT XFS 454.000. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED REINFOCING ANGLE (2024.T3 AL 0.032) PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001262003040100126WP 2003 4 1 DHL2003804518 120030125A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 603.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED ANGLE DOUBLER (2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001272003040100127WP 2003 4 1 DHL2003804519 120030115A5754 FRAME DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH 46124 LT WING I/B L/E FORMER CRACKED 1 IN STA XFS 653.750. REMOVED FASTNERS PER SRM 51-1-21 PG 1.STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10.FABRICATED REINFOCING ANGLE(2024.T3 AL 0.032)PER SRM 57-2-0 PG 9-10.CLEANED TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 PG 9-10 AND 51-1-21 PG 1. 2L74 4F RT4A25 20030401001432003040100143WP 2003 4 1 DHL2003804552 120030212A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 RT WING T/E UPPER SKIN SURFACE WITH 1/2 INCH CRACK IN IT. (XRS285.000-305.000) CUT OUT DAMAGED AREA IAW SRM57-2-0 FIG. 2 FABRICATED FILLER (2024T3,032) & DOUBLER (2024T3.050) IAW SRM57-2-0 FIG. 2. CLEANED , TREATED AND PRIMED FILLER & DOUBLER INNER SURFACE IAW SRM51-1-8B INSTALLED FILLER AND DOUBLER IAW SRM 57-2-0 FIG2 , SRM51-1-21 PG. 1 2L74 4F RT4A25 20030401001502003040100150WP 2003 4 1 DHL2003804660 120030228A57303889713 PANEL DOUG DC8 DC873F 302199FWP LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING LOWER SKIN SURFACE HAS 1.5 INCH CRACK AT STA XRS 455.000, BETWEEN S-63L AND S-64-L PERFORMED MAJOR REPAIR IAW EO DHL 030115, ED-3216 , REMOVED FASTNERS IAW IAW SRM 512-1-20D PG. 21 TRIMMED OUTDAMAGED SKIN SEGMENT IAW EO DHL 030115 , ED-3216. FABRICATED REPAIR DOUBLER (7075T6AL 0.100) & TRIPLER (7075T6AL 0.125) & FILLER (7075 T6 AL 0.211) & SHIM (7075T6AL 0.025)IAW EO DHL 030115 , ED-3126. CLEANED TREATED AND PRIMED INNER SURFACE OF REPAIR DOUBLER , TRIPLER , FILLER, SHIM , SHIM. IAW SRM 51-1-8B APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM51-1-15 PG. 1 INSTALLED DOUBLER , TRIPLER , FILLER , SHIM WITH NEW FASTNERS IAW EO DHL 030115, ED-3216, SRM51-1-20D PG. 9 FOR LEAK CHECK SEE N/R 2591 2L74 4F RT4A25 20030401001522003040100152WP 2003 4 1 DHL2003804662 120030210A57305769933183 VANE DOUG DC8 DC873F 302199FWP LT WING DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 LT WING OUTBOARD FLAP VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO67.000. PERFORMED MAJOR REPAIR IAW EO DHL 030109 , ED-3222 REMOVED FASTNERS IAW SRM 51-1-21 PG. 1. TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AL .071) A FILLER ( 7075T6AL .063) AND INTERNAL DOUBLER (075T6AL .050) IAW EO DHL030109 , ED-3222. CLEANED TREATED AND PRIMED INNER SURFACE IAW SRM 51-1-8B , APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-15 PG 1 . INSTALLED FILLERS & DOUBLERS AT LT WING OUTBD VANE SLOT UPPER SKIN WITH NEW FASTNERS IAW EO DHL 030109, ED-3222 AND SRM 51-1-21 PG 1. 2L74 4F RT4A25 20030401001612003040100161WP 2003 4 1 DHL2003804770 120030122A5347S2772660 CARGO TRACK DOUG DC8 DC873F 302199FWP FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 MAIN CARGO TRACK WORN IN VARIOUS LOCATIONS . CUT OUT DAMAGED TRACKS IAW SRM 53-2-3 PG 17 , CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED NEW PLUGS AND CHANNEL OR INSTALLED NEW TRACK SECTION IAW SRM 53-2-3 PG. 49-50 2L74 4F RT4A25 20030401001652003040100165WP 2003 4 1 DHL2003804774 120030227A575556551672 SKIN DOUG DC8 DC873F 302199FWP NR 3 SPOILER DELAMINATED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01804DH77866 46124 R & R OF RT SPOILER NR 3 DUE TO DELAMINATION ON UPPER SURFACE. R & R NR 3 RT SPOILER IAW M/M 27-61-1 PG. 201-207 REF: N/R 0607 FOR OPS CHECK 2L74 4F RT4A25 20030401001802003040100180WP 2003 4 1 DHL2003873002 120030226A3510 HOSE DOUG DC8 DC873F 302199FWP OXYGEN MASK KINKED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 FIRST OBSERVERS 02 MASK DOES NOT ALLOW O2 TO FLOW IN NORMAL ONLY IN EMERGENCY. FOUND O2 MASK HOSE KINKED BEHIND REGULATOR. UNKINKED AS REQUIRED. FIRST OBSERVERS 02 MASK OPS CHECKED NORMAL IAW DC8 M/M 35-10-8. 2L74 4F RT4A25 20030401001812003040100181WP 2003 4 1 DHL2003873003 120030227A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT STUCK A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01873SJ 46091 F/O'S SLIDING WINDOW WILL NOT OPEN. FOUND WINDOW JAMMED. UNSTUCK WINDOW. OPS CHECKED GOOD PER M/M 56-10-3. 2L74 4F RT4A25 20030402000212003040200021EU 2003 4 2 0300653226 120030331A2121 FAN AIRBUS320 A320211 3930320EU E/E BAY BURNED OUT A NWAAA UNSCHED LANDING EB VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01326US 282 DURING CRUISE EXPERIENCED RUMBLING/VIBRATION SEEMING TO COME FROM AVIONICS COMPARTMENT. ALSO EXPERIENCED ELECTRICAL BURING ODOR (NO SMOKE). DIVERTED TO BHM AND LANDED UNEVENTFULLY. VERIFIED AVIONICS BLOWER FAN FAULTY AND APPLIED MEL PROVISIONS. RAN PACK AND VERIFIED ABSENCE OF ODOR AND SMOKE. RETURNED A/C TO SERVICE. 2L72 4F RTA28NM 20030402000272003040200027NM 2003 4 2 2003UALA00212 120030226A282260721011 PUMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE FUEL BOOST DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29199UA7154 28717 A/C RECEIVED RT-STAB FUEL PUMP EICAS INDICATION. RT HST TRANSFER PUMP FAILED TO OPERATE. THIS A/C WAS OPERATING UNDER THE CERTIFICATE LIMITATIONS OF AD 2002-24-52 AMOC LETTER 140S-02-384 DATED 12/6/02. THIS LIMITATION DID NOT ALLOW THE CREW TO SELECT THE LT TX PUMP ON WHEN THE RT PUMP FAILED. A FLIGHT MANUAL BULLETIN WAS ADOPTED TO ALLOW THE CREW TO SELECT THE LT PUMP ON IF THE RH PUMP FAILS. THE PUMP SENSE PORT THREADS WERE STRIPPED. IT IS UNLIKELY THAT THIS CAUSED THE EICAS MESSAGE WITHOUT CREATING A LARGE FUEL LEAK. IT PASSED THE BENCH CHECKS AND STATOR X-RAY INSPECTION. 2L74 4F4 FRTA20WE E24NE 20030402000302003040200030NM 2003 4 2 2003UALA00237 120030305A261267410413294 MODULE BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT SHORTED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29556UA 26650 A/C RECEIVED WHEEL WELL FIRE INDICATION. WHEEL WELL FIRE INDICATION FOUND TO BE CAUSED BY P-3 WHEEL WELL FIRE ANNUNCIATOR L445. ANNUNCIATOR MODULE REPLACED AND OPERATED NORMAL. REMOVED PART TO BE EVALUATED BY VENDOR. 2L72 4F4 FRTA2NM E17NE 20030402000322003040200032NM 2003 4 2 2003UALA00290 120030317A335058781 LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN CONTAMINATED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29350UA 24301 EMERGENCY ELECTRICAL LIGHTING FIXTURE INOPERATIVE FROM ROW 15 TO THE BACK OF AIRCRAFT. FOUND RIBBON CABLE FOR THE EEL LIGHTS SOAKED WITH WATER. REMOVED CABLE AND CHECKED INDIVIDUAL LIGHTS. REPLACED POWER STRIP CABLE, OPS NORMAL. 2L72 4F4 FRTA16WE E2GL 20030402000332003040200033NM 2003 4 2 2003UALA00308 120030322A7830 RELAY BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE ISOLATION VALVE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP29669UA 30025 A/C RECEIVED REVERSER ISOLATION VALVE INDICATION BEFORE ETOPS ENTRY POINT. THE REV ISLN VLV LIGHT IS INHIBITED IN FLIGHT. THE ONLY SINGLE FAILURE THAT WOULD CAUSE THIS MESSAGE IN FLIGHT IS FAILURE OF K10359 OR K206 RELAYS, REF WDM 78-36-21 PG 4 SH 1. THESE RELAYS WERE REPLACED ALONG WITH THE PRESSURE SWITCHES AND ANOTHER RELAY. A CONTRIBUTING FACTOR FOR THIS TURNBACK WAS THE A/C FLIGHT MANUAL 7-26 FOR IRREGULARS GIVES A CAUTION THAT ADDITIONAL SYSTEM FAILURE MAY CAUSE INFLIGHT DEPLOYMENT. THIS IS NO LONGER TRUE WITH THE CHANGES MADE DURING SYNC LOCK INST. THIS CAUTION IS GOING TO BE CHANGED TO REFLECT CHANGES POST SYNC LOCK INSTALLATION. 2L72 4F4 FRTA1NM E24NE 20030402000342003040200034NM 2003 4 2 2003UALA00309 120030323A3230 SWITCH BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE MLG MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29310UA 23671 AIRCRAFT RETURNED TO FIELD WHEN THE LANDING GEAR FAILED TO RETRACT. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED AND THE LANDING GEAR EXTENDED AND RETRACTED NORMAL. 2L72 4F4 FRTA16WE E2GL 20030402000352003040200035NM 2003 4 2 2003UALA00310 120030321A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 CABIN RT SIDE STA 616 FRAME CRACKED BELOW CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR 2L72 4F4 FRTA16WE E2GL 20030402000362003040200036NM 2003 4 2 2003UALA00311 120030322A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29378UA 24653 CABIN LT SIDE STA 616 FRAME CRACKED BELOW CREASE BEAM. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND FILLER. 2L72 4F4 FRTA16WE E2GL 20030402000372003040200037NM 2003 4 2 2003UALA00312 120030323A5313 STRINGER BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE FUSELAGE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29954UA 26739 FUSELAGE STR S21-R DAMAGED BETWEEN BS 887 AND BS 907. MAJOR REPAIR ACCOMPLISHED. PERFORMED ANGLE REPAIR. 2L72 4F4 FRTA16WE E2GL 20030402000402003040200040NM 2003 4 2 2003UALA00317 120030324A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 827, STR 9R FRAME WEB IS CRACKED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DOUBLER WAS INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030402000522003040200052NM 2003 4 2 2003UALA00329 120030326A5311 FRAME BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STA 867, STR 9R FUSELAGE FRAME WEB CRACKED AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT, DOUBLER INSTALLED. 2L72 4F4 FRTA16WE E2GL 20030402000652003040200065NM 2003 4 2 2003UALA00342 120030301A5754114W423012 WEDGE BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 12 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29767UA 26918 T/E WEDGE DELAMINATED - NR 12 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F4 FRTT0001SE E46NE 20030402000682003040200068NM 2003 4 2 2003UALA00345 120030314A5754114W416021 WEDGE BOEING777 777222 1385219NM NR 6 SLAT DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29206UA 30212 T/E WEDGE DELAMINATED - NR 6 SLAT MAJOR REPAIR ACCOMPLISHED. T/E WEDGE REPAIRED. 2L72 4F RTT0001SE 20030408000732003040800073NM 2003 4 8 03FDEA00372 120030402A3220 BUSHING BOEING727 727200 138407ENM ZONE 700 MISSING A FDEAO OTHER J WARNING INDICATION CRCRUISE 1 SO25484FE 21466 TEST FLIGHT. UPON RAISING LANDING GEAR, NOSE GEAR RED LIGHT AND RED DOOR LIGHT STAYED ON. AIR CREW COULD HEAR SOMETHING STILL IN AIRSTREAM. LOG BOOK ENTRY REQ. UPON FURTHER INVESTIGATION, FOUND BUSHING FROM LOCK & POSITION SWITCH CONTROL ARM TO BE MISSING. INSTALLED BUSHING IN CONTROL ARM. PERFORMED OPERATIONAL TEST ON NLG IAW FED-EX M/M 32-61-071-5. FUNCTIONAL CHECKED GOOD. 2L73 4F RTA3WE 20030403000472003040300047NM 2003 4 3 AMTA200300306 120030304A3397 WIRE BOEING757 75723N 1384973NM EMERGENCY LIGHT DISCONNECTED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11516AT 27972 EPW WHITE LIGHT, THREE EACH, AT ROWS 30 AND 31 INOPERATIVE. REF ITEM 4 THIS PAGE 558241 FOR ADDITIONAL INFORMATION, ONCE WIRE FOR 32D WAS RECONNECTED WHITE EPL LIGHTS AT 30 AND 31 CHECK GOOD. (M) 2L72 4F RTA2NM 20030403000712003040300071SO 2003 4 3 C2XA03BT046 120030320A7500 O-RING EMB 145 EMB145ER 3260211SO ALLSN AE300 AE3007A GL NR 2 ENGINE LEAKING A C2XAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW2714940 145033 CREW REPORTED, "BLEED NR 2 LEAK IN FLIGHT" CREW PREFORMED PRECAUTIONARY ENGINE SHUTDOWN. MAINTENANCE FOUND LEAKING FAN AIR VALVE THERMOSTAT O-RINGS, REMOVED AND REPLACED FAN AIR VALVE THERMOSTAT O-RINGS. OPS.CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20030403000722003040300072SO 2003 4 3 C2XA03CL081 120030331A2730 CONTROL CABLE EMB 135 EMB135ER 3260203SO ELEVATOR LOOSE A C2XAO OTHER O OTHER APAPPROACH 1 SW2725504 145186 CLE FLT 2828 THE CREW REPORTED ELEVATOR LOST EFFECTIVENESS ON FINAL AT 130-125 KIAS. ELEVATOR FEELS SLOPPY ON GROUND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX ADJUSTED CABLE TENSIONS AND REMOVED AND REPLACED CAPTAINS ELEVATOR CABLE TENSIONER/REGULATOR OPERATIONAL CHECKS AND TEST FLIGHT WAS GOOD. 2L72 4F RTT00011AT 20030403000732003040300073SO 2003 4 3 C2XA03CL082 120030401A3260W001089224 WIRE EMB 145 EMB145ER 3260211SO WARNING SYS SHORTED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2714943 145040 CLE FLT 2224 THE CREW REPORTED THAT THE LANDING GEAR AURAL WARNING SOUNDED ON TAKEOFF WITH THE GEAR SELECTED AND INDICATING UP. AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED SHORTED WIRE BEHIND AURAL WARNING RACK W001-0892-24. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20030403000762003040300076SO 2003 4 3 C2XA03TY045 120030402A531014521699003 BEAM EMB 135 EMB135LR 3260305SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2717524 145399 DURING A SCHEDULED 1-C INSPECTION THE OMEGA BEAM WAS FOUND CORRODED. MAINT CUT OUT CORRODED AREA, FAB. ANGLE, FILLER, SHIMS AND INSTALLED IAW 135/145/SRM-53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK. 2L72 4F RTT00011AT 20030403000772003040300077NM 2003 4 3 CALA0300150 120030328A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND PASSENGER CABIN FLOORBEAM CORRODED AT BS 294.5, LBL 20 TO RBL 23. THE UPPER FLOORBEAM WAS REPLACED IAW SRM 53-10-51, FIGURE 205. 2L72 4F RTA16WE 20030403000782003040300078NM 2003 4 3 CALA0300151 120030328A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND STRINGER 25R CORRODED AT BS 364 AND S24R WAS CORRODED AT BS 360. REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030403000792003040300079NM 2003 4 3 CALA0300152 120030328A5313 STRINGER BOEING737 7373T0 1384582NM FUSELAGE PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND STRINGER 24R PUNCTURED AT BS 363. REPAIRED IAW SRM 53-00-03, FIGURE 201. 2L72 4F RTA16WE 20030403000882003040300088 2003 4 3 COMA0360168 420030325A2210 CLUTCH CNDAIRCL600 CL6002B19 1900309EA AUTOPILOT OUT OF TOLERANCEA COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01915CA7490 7013 FLIGHT 5847 A/P TRIM CAUTION MESSAGE - AILERONS FELT NOTICABLE STIFF. COULD NOT DUPLICATE DISCREPANCY, FOUND THE AUTO PILOT SERVO SLIP-CLUTCH OUT OF TOLERANCE, ADJUSTED SLIP CLUTCH TO PROPER VALVE. 2L72 4F RTA21EA 20030403000902003040300090EA 2003 4 3 COMA0360171 120030330A335020131A BATTERY CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01984CA14949 7171 FLIGHT 5132 EMERGENCY FLOOR PATH LIGHTING ROWS 1 THRU 5 IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY. 2L72 4F RTA21EA 20030403000912003040300091EA 2003 4 3 COMA0360172 120030330A2621385000183 BOTTLE CNDAIRCL600 CL6002B19 1900309EA FIRE EXTING DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA11696 7241 FLIGHT 5198 CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES. 2L72 4F RTA21EA 20030403000922003040300092EA 2003 4 3 COMA0360173 120030330A2621346000371 FIRE BOTTLE CNDAIRCL600 CL6002B19 1900309EA CABIN DISCHARGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01710CA11622 7241 FLGIHT 5198 - CARGO FIRE BOTTLE "LOW" CAUTION MESSAGE. REPLACED THE CARGO FIRE BOTTLES 2L72 4F RTA21EA 20030403000942003040300094EA 2003 4 3 COMA0360175 120030330A2750860D10018ABCD COMPUTER CNDAIRCL600 CL6002B19 1900309EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01868CA3118 7427 FLIGHT 5928 FLAPS FAIL CAUTION DURING LANDING. REPLACED THE FECU. 2L72 4F RTA21EA 20030403000962003040300096EU 2003 4 3 DHL2003367002 120030327A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU MALFUNCTIONED A DHLAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO01367DH 265 BATT. SMOKE LIGHT AND SMOKE LIGHT ON MWP ILLUMINATED. EMERGENCY CHECKLIST COMPLETED. RETURNED TO GSO. REMOVED AND REPLACED BATT. SMOKE DETECTOR, IAW A300 M/M 26-11-11. REMOVED AND REPLACED ELECTRIC SMOKE DETECTOR BOX IAW A300 M/M 26-11-11 & SMOKE DETECTOR SYSTEM OPS CHECKED GOOD IAW A300 M/M 26-11-00. 2L72 4F RTA35EU 20030403000972003040300097NE 2003 4 3 DJFA200300001 220030105A7200 BEARING BEECH MU300 400A 1155402CE PWA JT15 JT15D5 52112NE NR 1 ENGINE FAILED E DJFAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA23731TA RK273 PCEJA0316 AIRCRAFT IN CRUISE AT 410 FT LOST OIL PRESSURE ON NR 1 ENGINE AND ENGINE SHUTDOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT DESCENDED AND LANDED AT SRQ. PRELIMINARY REPORT INDICATES BEARING FAILURE. 2H72 4F4 FRTA16SW E25EA 20030403000992003040300099NE 2003 4 3 DL72S030110 220030129A7200 WARNING LIGHT BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE ILLUMINATED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27523DA63607 21583 700319 NR 1 ENG OIL FILTER BYPASS LIGHT PER POM SHUT ENGINE DOWN. CLEANED CONNECTOR FOR MASTER DIM AND TEST MODULE AND PERFORMED ENGINE WINDMILL INSP PER M/M. 2L73 4F4 F A3WE E2EA 20030403001002003040300100NM 2003 4 3 DL72S030143 120030211A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27410DA 21222 UPPER SKIN OF LT ELEVATOR WAS FOUND WITH OVERSIZED COUNTER SINKS IN ATTACHMENT HOLES COMMON TO THE REAR SPAR. REPAIR PER ER/A 417786-14AD. 2L73 4F A3WE 20030403001012003040300101NM 2003 4 3 DL72S030148 120030210A5330 SKIN BOEING727 727225A 1384077NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO278875Z 21293 TWO EXISTING SMALL REPAIR DOUBLERS WERE INSTALLED ON THE AIRCRAFT AT THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. ONE REPAIR WAS FOR A SMALL CRACK IN THE SKIN AT THE EDGE OF THE DOOR AND THE OTHER FOR A BLENDOUT OF A LIGHTNING STRIKE. BOTH REPAIR WERE TEMPORARY AND WERE REMOVED. BOTH DAMAGE CUTOUT LOCATIONS WERE INSPECTED AND REPAIRED WITH A SINGLE EXTERNAL REPAIR DOUBLER PER ER/A 384476-14, REV A. 2L73 4F RTA3WE 20030403001032003040300103NM 2003 4 3 DL72S030194 120030225A33501000679REVAC LIGHT BOEING727 727225A 1384077NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO278890Z 21859 L-1 EXIT SIGN INOPERATIVE IN EMERGENCY MODE. REPLACED LIGHT ASSY. 2L73 4F RTA3WE 20030403001042003040300104 2003 4 3 DL72S030208 420030303A3421344003685 INDICATOR BOEING727 727225A 1384077NM COCKPIT MALFUNCTIONED A DALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO27805EA 22436 CAPTS ATTITUDE INDICATOR INTERMITTENT. ROLLS TO 45/90 DEGS WITH AFF FAIL FLAG AND A COMPARITOR ROLL LIGHT. REPLACED CAPTS ADI AND VG PER M/M. SYS CHECKS NORMAL. 2L73 4F RTA3WE 20030403001092003040300109NM 2003 4 3 DL72S030279 120030326A5753 FAIRING BOEING727 727225A 1384077NM RT WING LOOSE A DALAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO278882Z 21579 AT FL300 SPEED .78/285KTS THE AIRCRAFT HAD MODERATE TO SEVERE VIBRATION IN AIRCRAFT AND CONTROLS. FOUND INBOARD RT FLAP ELEPHANT EAR AND CANOE LOOSE. REPAIRED SAME. 2L73 4F RTA3WE 20030403001122003040300112NM 2003 4 3 DL72W030105 120030128A3350 LIGHT BOEING727 727247 138408FNM CABIN INOPERATIVE A DALAO OTHER L NO TEST NRNOT REPORTED 1 SO27297WA 22534 LT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED RACK M964 AND BATTERY, RELAMPED SIGNS, EXERCISED NO SMOKING SWITCH AND NOW CHECKS NORMAL. 2L73 4F A3WE 20030403001132003040300113NE 2003 4 3 DL72W030192 220030224A7314 PUMP BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 FUEL FAILED A DALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27297WA 22534 700301 AIR TURNBACK, NR 1 ENGINE. REPLACED FUEL PUMP AND CONTROL. 2L73 4F4 F A3WE E2EA 20030403001142003040300114NE 2003 4 3 DL72W030196 220030225A7261 O-RING BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE LEAKING A DALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27297WA48183 22534 700301 NR 1 ENG OIL LOSS. REPLACED FUEL PUMP SHAFT O-RING. 2L73 4F4 F A3WE E2EA 20030403001162003040300116NM 2003 4 3 DL733030081 120030123A2530255001852 COFFEEMAKER BOEING737 737347 1384647NM 2L AFT GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27306WA 23347 FLT ATTENDANT VERBAL REPORT, LT AFT GALLEY COFFEEMAKER HAS ELECTRIC ODOR. REPLACED COFFEEMAKER, OPS CHECK NORMAL. NO ODOR. 2L72 4F RTA16WE 20030403001172003040300117NM 2003 4 3 DL733030088 120030124A33500201820001 LIGHT BOEING737 7373B7 1384580NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952WP 23378 EMERGENCY LIGHT ASSY IS BROKEN BY THE R-1 DOOR. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS NORMAL. 2L72 4F RTA16WE 20030403001182003040300118NM 2003 4 3 DL733030089 120030124A3350 LIGHT BOEING737 7373B7 1384580NM SEAT 17 DEF BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27952WP 23378 EMERGENCY LIGHT ASSY DAMAGE AT SEAT ROW 17 DEF (IN THE SEAT WHITE LIGHT). REPLACED EMERGENCY LIGHT ASSY, CHECKS NORMAL. 2L72 4F RTA16WE 20030403001192003040300119NM 2003 4 3 DL733030129 120030205A5610 WIRE BOEING737 737347 1384647NM COCKPIT ARCED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27303WA 23183 CO-PILOTS FRONT WINDSHIELD POWER WIRE IN UPPER RT CORNER ARCED. C/BS PULLED TO REMOVE POWER. REPLACED TERMINAL END AND HARDWARE. REPAIRED SAME. 2L72 4F RTA16WE 20030403001202003040300120NM 2003 4 3 DL733030142 120030210A3350 LIGHT BOEING737 737347 1384647NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27312WA 23598 EMERGENCY EXIT LIGHTING INOP AT ROW 22 AND 25. REPLACED LIGHT SOCKET AT ROW 22 AND REATTACHED WIRES AT ROW 25. BOTH EMERGENCY EXIT LIGHTS NOW CHECK NORMAL. 2L72 4F RTA16WE 20030403001212003040300121NM 2003 4 3 DL733030144 120030211A2612 CONTROL MODULE BOEING737 737347 1384647NM APU FIRE DETECT FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27304WA 23345 35523C AT 8000 FT APU FIRE LIGHT AND BELL SOUNDED, C/W PROC LIGHT STILL ON. AIR TURNBACK TO OAK. REPLACED FIRE DETECTOR CONTROL MODULE. 2L72 4F RTA16WE 20030403001242003040300124NM 2003 4 3 DL733030151 120030213A2612 FIRE LOOP BOEING737 737347 1384647NM APU UNSERVICEABLE A DALAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO27304WA37986 23345 35523C DURING PUSHBACK APU FIRE WARNING CAME ON APU SHUTDOWN AND INDICATION EXTINGUISHED APPROXIMATELY 2 MINUTES LATER. FIRE INDICATION RETURNED AND REMAINED ON. CREW FIRED APU EXTINGUISHER BOTTLE AND FIRE LIGHT DID NOT GO OUT. INSPECTED APU AND COMPARTMENT AREA NO EVIDENCE OF FIRE NO EVIDENCE OF FIRE DETECTED BY GROUND OR FIRE RESPONSE PERSONNEL. DEFERRED APU FIRE DETECTION AND EXTINGUISHING SYSTEM TO MEL, APU INOPERATIVE. TESTED FIRE LOOP SYSTEM, UNABLE TO DUPLICATE PROBLEM. 2L72 4F RTA16WE 20030403001252003040300125GL 2003 4 3 DL733030162 220030218A7310S332A0041 HOSE BOEING737 737347 1384647NM CFMINTCFM56 CFM563B1US GL NR 2 ENGINE LEAKING A DALAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO27304WA 23345 72071 ON ARRIVAL DEN FOUND FUEL LEAKING FROM RT ENGINE. INSP FOUND MAIN FUEL LINE FROM PYLON TO ENG FUEL PUMP LEAKING AT SWEDGED END / PYLON SIDE. REPLACED SAME. 2L72 4F4 FRTA16WE E2GL 20030403001262003040300126NM 2003 4 3 DL733030266 120030322A7830 PROXIMITY SENSOR BOEING737 7373B7 1384580NM NR 2 ENGINE T/R MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27951WP 22951 NR 2 T/R LIGHT ILLUMINATED CLIMBING THROUGH 12,000 FT. RETURN TO SLC QRH PROCEDURES COMPLIED WITH. REVERSER LIGHT ON OVERHEAD PANEL. ATB. CLEANED SIX PROXIMITY SENSORS FOR THE LEFT AND RIGHT T/R HALVES. CLEANED CANNON PLUGS FOR RIGHT AND LEFT SYNC LOCKS. REPLACE ENG ASSESSORY UNIT PER MM 78-34-06-4. NR 2 T/R SYSTEM CHECKS GOOD. NO REVERSER FAULT LIGHT NOTED. 2L72 4F RTA16WE 20030403001272003040300127NM 2003 4 3 DL733030275 120030324A33500201991008 LIGHT BOEING737 7373B7 1384580NM 24 DEF DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27951WP 22951 FOUND CABIN EMERGENCY EXIT LIGHT INOP AT SEAT 24DEF. REPLACED WIRE CONNECTORS AT LIGHT ASSY. OPS CHECKS NORMAL. 2L72 4F RTA16WE 20030403001302003040300130NM 2003 4 3 DL733030314 120030329A53306545767132 SKIN BOEING737 737347 1384647NM FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27309WA 23442 THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 470 BETWEEN STRINGERS 22L & 23L. THE DENT WAS REMOVED WITH A 7 INCHES CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384681-14, REV A. 2L72 4F RTA16WE 20030403001312003040300131NM 2003 4 3 DL738030136 120030209A4920 APU BOEING737 737832 13844CFNM APU BAY CONTAMINATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO273741S5232 P5846 30487 P5846 ON THE GROUND AT GATE IN MSP, DEICING FLUID WAS APPLIED TO TAIL SECTION WITHOUT PRIOR COORDINATION WITH FLIGHT CREW. SMOKE FILLED COCKPIT, STARTED TO FLOW INTO CABIN. PAX EVAC THROUGH 1L DOOR. SMOKE REM PROC FOLLOWED. DEICE FLUID INJESTED INTO APU INLET, CAUSED FUMES IN CABIN. RAN PACKS AT GATE AND CLEARED CABIN. ALL CHECKS NORMAL, AC OK FOR SERVICE. 2L72 4F RTA16WE 20030404000012003040400001NM 2003 4 4 372PA0017 120030324A335094145 LIGHT BOEING737 737306 13844BGNM CABIN INOPERATIVE A PIDAO OTHER L NO TEST NRNOT REPORTED 1 SO05372PA 23546 EMERGENCY FLOOR LIGHTING INOP FROM 21 AFT. REPLACED AFT SECTION EMERGENCY LITE STRIP PER MM 25-61-01. OPS CHECK OK. 2L72 4F RTA16NE 20030404000032003040400003NM 2003 4 4 373PA0008 120030402A335086210066 BATTERY PACK BOEING737 7373Y0 1384671NM EMERGNENCY LIGHTDISCHARGED A PIDAK NONE L NO TEST ININSP/MAINT 1 SO05373PA 23749 EMERGENCY EXIT FLOOR PATH LIGHT SEAT 6 AND SEAT 11 DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-51. 2L72 4F RTA16WE 20030404000052003040400005WP 2003 4 4 ABXA030122 120030313A53103926783507 SUPPORT DOUG DC9 DC932F 3022067WP CARGO DOORWAY CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 THE AFT LOWER CARGO DOOR JAMB, FORWARD LATCH PIN MOUNT WAS CRACKED. REPLACED THE FORWARD LATCH PIN SUPPORT IAW DC-9 SRM. 2L72 4F A6WE 20030404000062003040400006WP 2003 4 4 ABXA030123 120030313A5330591143267 SKIN DOUG DC9 DC932F 3022067WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 FUSELAGE SKIN WAS CRACKED AT STA. 1096, BETWEEN LONGERON 2 LEFT AND LONGERON 3 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01. 2L72 4F A6WE 20030404000072003040400007WP 2003 4 4 ABXA030124 120030317A53209922042506AX SUPPORT DOUG DC9 DC932F 3022067WP AFT CARGO CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 FS 851 RIGHT VERTICAL FLOOR SUPPORT FITTING CRACKED. INSTALLED NEW STRUT SUPPORT IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 20030404000082003040400008WP 2003 4 4 ABXA030125 120030317A5320991555047 INTERCOSTAL DOUG DC9 DC932F 3022067WP FUSELAGE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 CORROSION AROUND INTERCOSTAL NUTPLATES UPPER AND LOWER SURFACE, BETWEEN LONGERON 28 LEFT AND LONGERON 27 LEFT, F.S. 979 - 996. REPLACED INTERCOSTAL IAW DOUGLAS DRAWING 9915550 AND DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 20030404000092003040400009WP 2003 4 4 ABXA030126 120030324A53103924028501N FITTING DOUG DC9 DC932F 3022067WP KEEL AREA CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 LONGERON END CRACKED, LEFT CANTED KEEL AREA, JUST AFT OF FORWARD "P" DOME, LONGERON 29 LEFT. REPLACED LONGERON 29 LEFT END CAP IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20030404000112003040400011NM 2003 4 4 AWXA200300333 120030402A2560P4010021 BATTERY BOEING737 737277 1384570NM FLASHLIGHT DISCHARGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE FORWARD LT EMERGENCY FLASHLIGHT HAD NO BLINKING LIGHT. MAINTENANCE REMOVED AND REPLACED THE FORWARD LT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA16WE 20030404000132003040400013SO 2003 4 4 C2XA03TY046 120030403A213122250NO30201 CONTROLLER EMB 135 EMB135LR 3260305SO CABIN ERRATIC A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2717524 145399 PILOTED WAS IN A CLIMB OUT OF TYS WHEN THE PRESSURIZATION ICIAS MESSAGE WENT INOPERATIVE. THE CREW RETURN TO TYS AND MAINT. R & R THE PRESSURE CONTROLLER, OPS CHECK WAS GOOD IAW EMB 145 MM 21-31-00. AIRCRAFT WAS REL. AND NO FURTHER PROBLEMS OCCURED. 2L72 4F RTT00011AT 20030404000162003040400016NM 2003 4 4 CALA0300163 120030401A5241 SKIN BOEING737 7373T0 1384582NM GALLEY DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND R-2 DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-00-01. 2L72 4F RTA16WE 20030404000172003040400017NM 2003 4 4 CALA0300164 120030401A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 INSPECTION FOUND TOP SURFACE OF TOP CAP OF LATERAL FLOORBEAM AT STA 1016 CORRODED AT LT SIDE AREA UNDER LAV TANK. REPAIRED IAW ECRA 5310-03851. 2L72 4F RTA16WE 20030404000202003040400020NM 2003 4 4 DHL2003726002 120030404A5347 SEAT TRACK BOEING727 727228 1384083NM COCKPIT DAMAGED A DHLAO OTHER O OTHER NRNOT REPORTED 1 SO01726DH 20409 S/O'S SEAT WILL NOT LOCK INTO RAIL FOR SIDEWAY MOVEMENT. CLEANED AND LUBRICATED SEAT RAILS AND LOCKING MECHANISM PER M/M 2510. OPS NORMAL. 2L73 4F RTA3WE 20030404000262003040400026WP 2003 4 4 DHL2003873007 120030401A5610 WINDOW DOUG DC8 DC873F 302199FWP COCKPIT LACK OF LUBE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01873SJ 46091 F/O'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED F/O'S SLIDING WINDOW AND LUBRICATED ACTUATING ASSEMBLY AS REQUIRED. OPS CHECKED GOOD IAW M/M 56-10-3. 2L74 4F RT4A25 20030404000282003040400028NM 2003 4 4 DL738030280 120030326A2750 WARNING LIGHT BOEING737 737832 13844CFNM FLAPS ILLUMINATED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO27380DA 30266 AT CRUISE - FL 390 - YAW DAMPER DISENGAGED AND WAS RESET. LEADING EDGE IN TRANSIT LIGHTS WERE OBSERVED ON OVERHEAD. FOLLOWED BY L/E LIGHTS ON FWD PANEL WITH T/E. FLAPS INDICATING 1/2 DEG. DESCENT INITIATED AND FLAPS RETRACTED FULLY ON THEIR OWN. CHECKED SYSTEM PER FIM AND TESTED FSEU WITH NO VCM MSGS. ALL FLAP AND PROX SWITCHES TEST NORMALLY. ENTIRE SYSTEM TESTS PER FIM 27-81/806. FDAU SHOWS FLAP HANDLE INPUT TO THE NR 1 DETENT. PERFORMED PHASE 1 OVERSPEED INSPECTION PER M/M 05-51-08-2. 2L72 4F RTA16WE 20030404000292003040400029NM 2003 4 4 DL73K030117 120030130A5330654576988 SKIN BOEING737 737247 138448DNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27379DL 23606 THE FUSELAGE SKIN AT FS 480 WAS GOUGED AND CRACKED BY GROUND EQUIPMENT JUST BELOW THE STRINGER 26R SKIN LAP JOINT. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384498-14. 2L72 4F A16WE 20030404000322003040400032WP 2003 4 4 03FDEA00376 120030402A2620 CONTROLLER DOUG MD10 MD1010F WP FIRE EXTING INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25392FE 46626 IN CRUISE (FL330) RECIEVED CARGO FIRE INDICATION WITH MASTER WARNING AND AFT 1 FLASHING DISCHARGE LIGHT. COMPLIED W/ APPROPRIATE PROCEDURES. DIVERT TO STL. ONLY FIRED BOTTLE NR 1. REPLACED LOWER CARGO COMP FIRE EXT CONTAINER NR 1, DISCHARGE HEADS AND DISCHARGE CARTRIDGES. R & R MISC. SYS. CONTROLLER PRECAUTIONARY PER MD10 MM 31-42-01. R&R CARGO FIRE CONTROL PANEL PER MD10 AMM 26-14-10-4 PANEL OPS CK OK, PER MD10 AMM 26-14-01 PG501. PERFORMED FIRE EXTINGUISHER CIRCUITS TEST PER M/M 26-22-01. PERFORMED OPS CHECK ON MSC PER M/M 31-42-01. CARGO FIRE TEST OPS CHECKS GOOD PER M/M 26-14-01. OK FOR SERVICE. 2L73 4F RTA22WE 20030404000332003040400033NM 2003 4 4 03FDEA00377 120030402A5597 WIRE HARNESS DOUG MD11 MD11 3023602NM ZONE 300 BURNED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25585FE 48481 HORIZONTAL STABILIZER CENTER SECTION TOP- WIRE BUNDLE AT THE RT INBOARD SIDE, INSIDE THE AFT FUSELAGE COMPT, FOUND BURNED AND DAMAGED DURING FSC RETURN-TO-SERVICE TEST. 2L73 4F RTA22WE 20030625001242003062500124EU 2003 6 25 03FDEA00378 120030403A78307065M93G10 PANEL AIRBUS310 A310 EU THRUST REVERSER DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 1 ENGINE O/B T/R TRANSLATING COWL, LWR AFT LINER DELAMINATED. REMOVED AND REPLACED NR 2 ENGINE T/R TRANS COWL IAW MM 78-32-11-4-B. 2L72 4F RTA35EU 20030404000342003040400034EU 2003 4 4 03FDEA00379 120030403A7830 FILLET AIRBUS310 A310 EU NR 2 ENG T/R TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25443FE 283 NR 2 ENG I/B THRUST REVERSER CORE UPPER AFT FILLET PANEL TORN. R/R FILLET PANEL PER IAW SRM 51-40- 2. 2L72 4F RTA35EU 20030404000372003040400037NM 2003 4 4 DL73K030274 120030323A3233654462514 ACTUATOR BOEING737 737247 138448DNM NLG BROKEN A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO27243WA 23517 ON APPROACH INTO MCO NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. OK ON SECOND ATTEMP AND LANDED WITH OUT INCIDENT. AMT FOUND LOCK ACTUATOR FAILED CAUSING 1 INCH DIAMETER HOLE IN FWD PRESS BULKHEAD NOSE WHEEL WELL. 2L72 4F A16WE 20030404000422003040400042NM 2003 4 4 DL73S030113 120030129A5312 BULKHEAD BOEING737 737232 1384475NM FUSELAGE CANNING A DALAK NONE O OTHER ININSP/MAINT 1 SO27314DA 23086 INSPECTION OF THE AFT P-DOME REVEALED A 10 X 8 X .25 INCH OIL CAN IN THE LOWER WEB AREA OF NEAR BL 0. THE OIL CAN WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOULBER PER BAC S/B 737-53A1075 AND ER/A 384318-14AD. 2L72 4F RTA16WE 20030404000432003040400043NM 2003 4 4 DL73S030191 120030224A7120 SUPPORT FITTING BOEING737 737232 1384475NM ENGINE MOUNT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27305DL 23077 FWD ENGINE MOUNT SUPPORT FITTING ASSY WAS FOUND WITH O/S MOUNT HOLES. REPAIR PER ER/A 422119-14AD. 2L72 4F RTA16WE 20030404000442003040400044NM 2003 4 4 DL757030067 120030116A2120 ODOR BOEING757 757232 1384965NM CABIN DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27618DL 22908 FLT ATTENDANTS REPORTED AN ODOR SIMILAR TO HOT PLASTIC IN THE REAR OF THE AFT CABIN THAT THE APPARENT CAUSE OF HEADACHES FOR SEVERAL PASSENGERS AND FLT ATTENDANTS. AIRCRAFT WAS IN CRUISE. ANTI ICE WAS NOT IN USE. ODOR DID NOT INCREASE WHEN USING ANTI ICE IN DESCENT. OPERATED AIR CONDITION SYSTEM FOR 30 MINS. COULD NOT DUPLICATE ANY SMELL OR ODOR. 2L72 4F RTA2NM 20030404000452003040400045NM 2003 4 4 DL757030094 120030124A5310143N85121 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 THE OUTBOARD STRUCTURE OF THE LOWER SILL BEAM OF THE C1 DOOR OPENING WAS FOUND CORRODED. TO REMOVE THE CORROSION, THE OUTER STRUCTURE AND WEB OF THE FS 620 FRAME WERE CUT BETWEEN STRINGERS 25R & 26R AND THE LOWER SECTIONS REMOVED. THE SILL STRUCTURE WAS REPLACED AND THE FRAME AND WEB SECTIONS SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED PER ER/A 384357-14, REV A. 2L72 4F RTA2NM 20030404000462003040400046NE 2003 4 4 DL757030100 220030128A7261PW2037RTC ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO27698DL44277 29911 716511 RT ENGINE FAILURE ON CLIMBOUT, APPROX 18,000FT. EICAS STATUS PAGE RT ENGINE SEC SEL-RT ENGINE LOW N1-RT ENGINE OIL PRESS-RT ENGINE FUEL ON SOL. EPCS PAGE OIL PRESS RED NO OTHER FAULTS RECORDED. REPLACED ENGINE. 2L72 4F4 FRTA2NM E17NE 20030404000472003040400047NM 2003 4 4 DL757030101 120030128A2560 PLACARD BOEING757 757232 1384965NM CABIN WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27693DL 29725 THE 3 RT RAFT SURVIVAL KIT HAS DIRECTIONS PLACARDS THAT IS HARD TO READ. REMOVED AND REPLACED 3 RIGHT SURVIVAL KIT. 2L72 4F RTA2NM 20030404000482003040400048NM 2003 4 4 DL757030115 120030128A5330143N347111 SKIN BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27685DA 27588 THE FUSELAGE SKIN WAS GOUGED BY TOOLING AT FS 500, JUST BELOW THE STRINGER 26R SKIN LAP JOINT. THE GOUGE WAS REMOVED FROM THE SKIN WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384441-14, REV A. 2L72 4F RTA2NM 20030404000492003040400049NM 2003 4 4 DL757030167 120030220A2120 ODOR BOEING757 757232 1384965NM A/C DUCTING DETECTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO27678DL 25983 ODOR IN COCKPIT COMING FROM OVERHEAD AIR CONDITIONING DUCT. FOUND TO BE RIGHT RECIRCULATION FAN THE CAUSE. DEACTIVATED FAN AND FWD TO MCO/PLAC PER MEL 21-25-01A. 2L72 4F RTA2NM 20030404000502003040400050NE 2003 4 4 DL757030182 220030222A7320DPN736001778 EEC BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE UNSERVICEABLE A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO27653DL 24393 716363 LT ENGINE PRIMARY CONTROL STATUS MSG, LT ENGINE FAILED. REPLACED NR 1 ENGINE EEC. PERFORMED WINDMILL INSPECTION ON ENGINE. NO DEFECTS NOTED. 2L72 4F4 FRTA2NM E17NE 20030404000512003040400051NM 2003 4 4 DL757030184 120030223A3350 BATTERY BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27608DA 22815 EMERGENCY LIGHTS AFT OF SEAT 38 INOP. REMOVED AND REPLACED LIGHT PACK AND BATTERY ASSEMBLY. 2L72 4F RTA2NM 20030404000522003040400052NM 2003 4 4 DL757030188 120030221A5315146N51116 FLOORBEAM BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 THE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH MULTIPLE AREAS OF CORROSION. THE UPPER CAP FLANGE WAS TRIMMED OFF FROM END TO END (LBL 61 - RBL 61). A NEW CAP WAS FABRICATED FROM ALUMINUM EXTRUSION AND INSTALLED ON THE FLOORBEAM. THE REPAIR WAS ACCOMPLISHED PER ER/A 384525-14, REV A. 2L72 4F RTA2NM 20030404000542003040400054NM 2003 4 4 DL757030190 120030221A5310143N85121 DOOR FRAME BOEING757 757232 1384965NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27652DL 24392 THE OUTER CAP OF THE LOWER SILL BEAM OF THE C1 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION. TO REMOVE THE OUTER STRUCTURE, THE OUTER STRUCTURE AND WEB OF THE FS 620 FRAME WERE CUT AND THE LOWER SECTIONS REMOVED. A NEW SILL STRUCTURE WAS THEN INSTALLED AND THE LOWER SECTIONS OF FRAME CHORD AND WEB SPLICED BACK IN PLACE WITH ALUMINUM REPAIR DOUBLERS PER ER/A 384501-14, REV A. 2L72 4F RTA2NM 20030404000592003040400059NM 2003 4 4 DL757030223 120030307A2913291702437 PUMP BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27618DL 22908 716514 LOST RT HYD SYSTEM QUANTITY WHILE HOLDING SHORT OF RUNWAY FOR TAKEOFF. FOUND RT ENGINE DRIVEN HYD PUMP HOUSING CRACKED. REPLACED RT ENGINE DRIVEN HYD PUMP, CASE DRAIN FILTER AND PRESURE FILTER. ALL LEAKED CHECKED GOOD. SERVICED HYD SYSTEM TO FULL. 2L72 4F4 FRTA2NM E17NE 20030404000602003040400060NM 2003 4 4 DL757030237 120030312A3040 DEICE SYSTEM BOEING757 757232 1384965NM COCKPIT WINDOW BURNED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO276714Q 30485 ELEC FUMES IN FLT DECK AND LEFT ENG GEN DROPPED OFF LINE. NO ASSOC STATUS MSGS. DIVERTED TO GSO. LEFT ENG GEN CONFIRMED FAILED. PLACED ON MCO PER MEL. FOUND EVIDENCE OF FUMES WHILE STANDBY POWER CHECK WAS PERFORMED. REPLACED MAIN BATTERY, CHARGER AND INVERTER AS PRECAUTIONARY. DURING CONTINUED T/S, FOUND BURNED TERMINALS ON 3L WINDOW HEAT TERMINAL. THE 3L WINDOW HEAT DEACTIVATED PER MEL. IT IS SUSPECTED THAT THE 3L WINDOW WAS SOURCE OF SMELL THE ENTIRE TIME. 2L72 4F RTA2NM 20030404000612003040400061NM 2003 4 4 DL757030246 120030316A3350 BATTERY PACK BOEING757 757232 1384965NM EMERGENCY LIGHT UNSERVICEABLE A DALAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO27662DN 24991 REPLACED BATTERY PACK ON F/C CHARGER FOR SEAT PATH LIGHT