20030331000812003033100081EU 2003 3 31 BMAC010001 120011205A3200622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU MLG MALFUNCTIONED A B16AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05529PA 771 LANDING GEAR INTRANSIT LIGHT STAYED ON LT. COULD NOT DUPLICATE. PRECAUTIONARY REPLACEMENT OF UPLOCK AND DOWNLOCK SWITCHES PER SB32-891142, PERFORMED ON LEFT MAIN GEAR. (M) 2L72 4T RTA21EU 20030505000482003050500048EA 2003 5 5 A6WA200340043 120010622A2420761341 GCU CNDAIRCL600 CL6002B19 1900309EA ADG INOPERATIVE A A6WAO OTHER O OTHER NRNOT REPORTED 1 GL31406AW2933 7402 COMPLY WITH ADG INFLIGHT DEPLOYMENT IAW TASK 024/24/220/701. ADG FUNCTIONAL CHECK FAILED. REMOVED AND REPLACED GCU, S/N 0290. FLIGHT OPERATIONAL TEST OF ADG AUTO DEPLOYMENT SUCCESSFUL. GCU COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF). 2L72 4F RTA21EA 20030505002282003050500228NM 2003 5 5 S01227042 120011222A5753 STRUCTURE BOEING BOEING747 747209B NM PWA JT9 JT9D7R4G2 52054NE TE FLAP CORRODED W SAJFO OTHER O OTHER LDLANDING 1 WP03 87500 22299 I/B FLAPS FAILED TO EXTEND BEYOND 10 UNIT. ALT EXTENSION FAILED. GRD CK FOUND RT I/B FORE & MID FLAP DAMAGE & NR 5 MAIN CARRIAGE SPINDLE BROKEN. REPLACED RT I/B FORE/MID FLAP. REPLACED NR 5 MAIN CARRIAGE. PERFORM I/B FLAP ADJ/TEST. REPLACED DFDR. NR 6 CARRIAGE REMOVED & FOUND CORROSION PITTING. CARRIAGES REPLACED. FRACTURED CARRIAGE SENT TO BOEING. FRACTURE INITIATED FROM CORROSION PITTING OD SURFACE & PROPAGATED. PRESENCE OF HIGH CONCENTRACTION OF CHLORINE ELEMENT FOUND ON FRACTURE SURFACE MIGHT HAVE CONTRIBUTED TO STRESS CORROSION CRACKING. ALL OVERHAUL PROCEDURES & SHOP WORKSHEETS REVIEWED & REVISED TO COMPLY W/OHM. T/E FLAP CARRIAGE MUST BE REPEAT OVERHAULED NOT TO EXCEED 30000 FH OR 8 YRS. 2L74 4F4 FRTA20WE E3NE 20030507001182003050700118EA 2003 5 7 CA030417008 120010919A5741 BUSHING CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF343B1 NE WING ATTACHMENT LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS. 2L72 4F4 FRTA21EA E15NE 20030530000562003053000056NM 2003 5 30 2003F00333 120011227A575365413175 FLAP TRACK BOEING727 72721 1384003NM TE FLAPS CRACKED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX 19261 LEFT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELAGE IS CRACKED IN SEVERAL PLACES AT WBL 70.5. REMOVED AND REPLACED ROLLER BEARING TRACK. (M) 2L73 4F A3WE 20030530000582003053000058NM 2003 5 30 2003F00335 120011229A571165162003 SPAR BOEING727 72721 1384003NM LEFT WING CORRODED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX34220 19261 LEFT WING FRONT SPAR UPPER CAP, LOWER LEG, HAS CORROSION AT WS 222.0 AND 224.5. CORROSION FOUND OUT OF LIMITS. REPAIRED SPAR PER DRAWING RFB275710-122601. (M) 2L73 4F A3WE 20030530000572003053000057NM 2003 5 30 2003F00334 120011228A57536521630173 SKIN BOEING727 72721 1384003NM TE FLAP DELAMINATED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX 19261 LEFT INBOARD FORE FLAP DELAMINATED AT TRAILING EDGE JUST ABOVE MIDDLE TRACK. REMOVED FLAP, REPAIRED IAW B727 MM 27-51-11. REINSTALLED FLAP. (M) 2L73 4F A3WE 20010111044822001011104482WP 2001 1 11 TWAA0100101 120010101A3350MISC0639 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05983Z 47411 THE LEFT NACELLE LIGHT WAS INOPERATIVE ON THE EMERGENCY LIGHT CHECK. REPLACED THE LEFT OVERWING EMERGENCY BATTERY PACK. CHECK-C 12-14-99. 2L72 4F A6WE 20010111029012001011102901NM 2001 1 11 DL72W010003 120010101A3610BACC10DU350ABE CLAMP BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE STRETCHED A DALAO OTHER J WARNING INDICATION CLCLIMB 1 SO272820W 21058 700535 AT 60 KTS ON T/O ROLL, LEFT STRUT PNEUMATIC DUCT PRESSURE WENT TO 6 O'CLOCK POSITION. ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENGINE THROTTLE BROUGHT TO IDLE. LIGHT EXTINGUISHED. FOUND WORN DUCT CLAMP ON ENG BLEED SUPPLY DUCT. REPLACED SAME. RAN ENG. STRUT OVERHEAT STAYED OUT 2L73 4F4 F A3WE E2EA 20010111045302001011104530NM 2001 1 11 UPS01234577 120010101A3350 BULB BOEING727 72725C 138400HNM COCKPIT MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01931UP 19858 INSPECTION TYPE:N/A COCKPIT DOOR EMERGENCY EXIT LIGHT HAS ONE DIM BULB RELAMPED EMER. LIGHT OVER FLIGHT DECK ENTRY DOOR, OPS CHECK GOOD 2L73 4F A3WE 20010111023072001011102307NM 2001 1 11 AWXA0001166 120010102A53306545765 SKIN BOEING737 7373S3 1384711NM FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 UPPER EXTERNAL FUSELAGE STA 230 LBL 7 - LBL 9 LIGHTNING STATIC DMG WENT OUT OF LIMITS. CUTOUT DMG; FABED FILLERS & DOUBLERS; INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 201. 2L72 4F RTA16WE 20010111005782001011100578NM 2001 1 11 AWXA0001167 120010102A3397BMS13131122 WIRE BOEING737 7373G7 1384595NM SEAT 2B BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28160AW 23782 EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B INOP. REPAIRED BROKEN WIRE; LIGHT OPS CHECKS GOOD 2L72 4F RTA16WE 20010111023082001011102308NM 2001 1 11 AWXA0001169 120010102A33501012721 LIGHT BOEING737 7373G7 1384595NM SEAT 3C INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 EMERGENCY ESCAPE PATH LIGHT INOP @ SEAT 3C. REPLACED LIGHT ASSY 2L72 4F RTA16WE 20010111023092001011102309EU 2001 1 11 AWXA0001170 120010102A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28631AW3034325917 077 EXIT SIGNS OVER DOOR 1L & 1R AND FIRST CLASS OVERHEAD DO NOT ILLUMINATE WHEN NO SMOKING SIGN IS OFF. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-38; OPS CHECKED GOOD 2L72 4F RTA28NM 20010111023102001011102310NM 2001 1 11 AWXA0001171 120010102A335020121 CHARGER BOEING737 737375 13844BNNM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28336AW 23707 EMERGENCY LIGHTS INOP ROW 13-18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER ASSY; LIGHTS OPS CHECKED GOOD. 2L72 4F RTA16WE 20010111061372001011106137NM 2001 1 11 PCAA0101001 120010101A561007802 WINDSHIELD DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13831EX10554 160 LGA-ALB FLIGHT 3551. LEFT WINDSCREEN SHATTERED IN FLIGHT. AIRCRAFT LANDED IN ALB. MAINTENANCE REPLACED CAPTAINS WINDSHIELD AND 15 NUTPLATES ALONG BOTTOM OF WINDOW SILL IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 56-10-11, RAN AIRCRAFT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010111041742001011104174NM 2001 1 11 F3LA200100001 120010101A21332888 GASKET BOEING737 7373Q8 1384670NM OUTFLOW VALVE INOPERATIVE A F3LAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03318FL 709 26301 AIR TURN BACK. FLIGHT CREW REPORTED AUTO PRESSURIZATION INOPERATIVE. RETURNED TO ATL WITHOUT INCIDENT. REPLACED OUTFLOW VALVE HEATER GASKET AND CHECKED OKAY. 2L72 4F RTA16WE 20010111006182001011100618NM 2001 1 11 SCNA01001 120010101A3397 WIRE BOEING727 7272J4 1384006NM CABIN BROKEN A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 THE OVERHEAD EMERGENCY LIGHT AT SEAT 24 STAYED ON AFTER THE POWERR IS WAS REMOVED AND THE SWITHC WAS TURNED OFF. REPAIRED BROKEN DISARM WIRE ON OVERHEAD EMERGENCY LIGHT AT SEAT 24, OPERATIONAL CHECKS GOOD. 2L73 4F RTA3WE 20010111037402001011103740WP 2001 1 11 ERKR200100012 120010104A523099211661 FITTING DOUG DC9 DC933F 302207AWP CARGO DOOR CRACKED B ERKRO OTHER O OTHER ININSP/MAINT 1 WP07933F 47191 CRACK ON MAIN CARGO DOOR LOWER FITTING AT STATION 413.062 2L72 4F A6WE 20010111023302001011102330NM 2001 1 11 AWXA0001176 120010103A531365528941 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 INTERCOSTAL UPPER FLANGE CRACKED AT SCREW HOLE BS 540 LBL 2. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02 2L72 4F RTA16WE 20010111023312001011102331NM 2001 1 11 AWXA0001177 120010103A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 CABIN SEAT TRACK CRACKED AT RBL 45 & FS 727B. REMOVED GUSSET IAW SRM 51-40-02; FABED REPAIR PLATE AND SHIM IAW 51-70-13 FIG 1; INSTALLED REPAIR PLATE AND SHIM IAW 51-70-13; INSTALLED GUSSET IAW 51-40-02. 2L72 4F RTA16WE 20010111023332001011102333NM 2001 1 11 AWXA0001179 120010103A53206720381 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 FS 178 LT INTERCOSTAL CRACKED WL 195 LBL 24. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 2L72 4F RTA16WE 20010111037412001011103741WP 2001 1 11 ERKR200100014 120010104A522059101597 DOUBLER DOUG DC9 DC933F 302207AWP EMERGENCY EXIT CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 FABRICATION OF A DOUBLER TO BE INSTALLED AT THE EMERGENCY EXIT DOOR AT STATION 669.0 COMMON TO THE INNER SKIN TO REPAIR A CRACK IN THE FORWARD LOWER CORNER. REPAIRED PER ECRA 933-52-054-2 REV. B 2L72 4F A6WE 20010111021872001011102187EU 2001 1 11 RAIA0101001 120010102A24358260121 STARTER GEN AEROSPATR72 ATR72202 8680940EU NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03721TE1673 528 217 7158-STL-DURING CLIMB #1 DC GENERATOR FELL OF LINE AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED #1 STARTER GENERATOR IAW J41 MAINTENANCE MANUAL. 2H72 4T RTA53EU 20010111023372001011102337NM 2001 1 11 AWXA0001184 120010103A55126554821 SKIN BOEING737 7373G7 1384595NM HORIZONTAL STAB DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 LT HORIZ STABILIZER L.E. SKIN DENTED OUT OF LIMITS AT LES 24.0.: REMOVED, FABED REPLACEMENT, AND INSTALLED REPLACEMENT LE SKIN IAW BOEING DWG 65-54821 AND SRM 51-40-02 2L72 4F RTA16WE 20010111023382001011102338NM 2001 1 11 AWXA0001185 120010103A532165458336 WEB BOEING737 7373G7 1384595NM CABIN FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. REMOVED FLOOR WEB IAW SRM 51-40-02; FABED REPLACEMENT PART IAW DWG 65-45833; INSTALLED REPLACEMENT PART IAW 51-40-02. 2L72 4F RTA16WE 20010111023412001011102341NM 2001 1 11 AWXA0001187 120010103A531265163006 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 CENTER WEB CRACKED FS 178 LBL 5.0 WL 198 (1.0L) AND WL 202 (1.0L). REMOVED DAMAGED AREA OF WEB; NDT VERIFIED NO CRACKS; FABED REPAIR PARTS AND INSTALLED IAW SRM 53-10-08 FIG 209 AT FS 178 LBL 5.0 WL 200. 2L72 4F RTA16WE 20010111023482001011102348NM 2001 1 11 AWXA0001194 120010103A5410313A138017 ANGLE BOEING737 7373G7 1384595NM NACELLE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 LT WING O/B PYLON SKATE ANGLE HAS ELONGATED NR 3 FASTENER HOLE. REMOVED DAMAGE; FABED AND INSTALLED REPAIR AND INSTALLED SKATE ANGLE IAW SRM 51-40-02 AND 51-70-11; INSTALLED REPAIR ANGLES, 2 EA, AND 3 EA FILLERS IAW B737 SRM 51-70-11 AND 54-50-71; FABED ANGLES, MILLED AND HEAT TREATED, 3 EA FILLERS AND 3 SHIMS IAW 51-30-01 FIG 10 2L72 4F RTA16WE 20010111023492001011102349NM 2001 1 11 AWXA0001195 120010103A5310651758351 STIFFENER BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 VERTICAL STIFFENER ANGLE CRACKED FS 178 LBL 5.7 WL 180 (1.5 INCH L). REMOVED COMPONENTS TO GAIN ACCESS; CUTOUT DMGD AREA; NDT VERIFIED NO CRACKS; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 205; REINSTALLED COMPONENTS IAW TASK CARD 01A53006, C1A53006 2L72 4F RTA16WE 20010111023502001011102350NM 2001 1 11 AWXA0001196 120010103A532065176889 INTERCOSTAL BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 AT LT LAV. STR 16 FS 300, FOUND INTERCOSTAL WEB TO HAVE CRACK AT RADIUS. REMOVED DAMAGE IAW SRM 51-70-13 AND 51-70-11; NDT CONDUCTED HFEC IAW B737 NDTM PT.6, 51-00-00 FIG 23, NO CRACKS NOTED; FABED ANGLE AND FILLER REPAIR IAW SRM 53-10-15 FIG 1 AND 51-70-11; INSTALLED REPAIR IAW SRM 51-70-11 AND 51-40-02. 2L72 4F RTA16WE 20010111023662001011102366NM 2001 1 11 AWXA0001200 120010103A5320 BRACKET BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 ANGLE BRACKET CRACKED STA 616 LBL 60. REMOVED DAMAGED AREA; FABED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW ER 03-5310-0035-JS1A 2L72 4F RTA16WE 20010111023682001011102368EU 2001 1 11 AWXA0001202 120010103A3260 LANDING GEAR AIRBUS320 A320231 3930325EU MAIN MALFUNCTIONED A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28627AW 66 ON LANDING GEAR EXTENSION THE NOSE GEAR SHOWED NOT DOWN/LOCKED; THE PILOT JIGGLED THE HANDLE AND ABOUT 10 SEC LATER THE GEAR THEN SHOWED DOWN AND LOCKED; CREW MADE AN EMERGENCY LANDING. THE PROBLEM WAS TROUBLESHOT IAW TSM 32-31-00 PG.A212 & A213; NO FAULTS WERE FOUND AND NO ASSOCIATED FAULTS WERE NOTICED ON PREVIOUS FLIGHT REPORTS; THE AIRCRAFT WAS RELEASED IAW TSM 00-INTRO: PG 28 (2)(B)2 2L72 4F RTA28NM 20010111023692001011102369NM 2001 1 11 AWXA0001203 120010103A323065446916 MODULE BOEING737 7373Y0 1384671NM NLG WW MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28330AW38862 23499 LAS - AIR TURNBACK - UPON GEAR RETRACTION, RED TRANSIT NOSE GEAR LIGHT WOULD NOT EXTINGUISH IN GEAR UP POSITION; VIBRATION AND NOISE PRESENT; IN OFF POSITION GREEN AND RED NOSE GEAR LIGHT ON; ALL 3 GEAR GREEN LIGHTS WERE ON FOR LANDING. MAINTENANCE TROUBLESHOT AND REPLACED THE NOSE GEAR HYDRAULIC MODULE; FUNCTIONAL CHECKS WERE GOOD. 2L72 4F RTA16WE 20010111039702001011103970WP 2001 1 11 ERKR200100015 120010104A523099211583 STRAP DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 354 FRAME OF THE MAIN CARGO DOOR BELOW TRACE LL "J". THE REPAIR CONSISTS OF DRILLING OUT THE DAMAGE INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSHING AND REPLACING THE INNER SKIN. PER ECRA 933-52-059-2 REV. B. 2L72 4F A6WE 20010111023392001011102339NM 2001 1 11 AWXA0001186 120010103A52106545871 SKIN BOEING737 7373G7 1384595NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 R1 DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. CUT OUT DAMAGE AND REPAIRED IAW SB737-52-1096 FIG 6 DETAIL II AS PER AWA EO 52-00-02 AND SRM 51-40-02 2L72 4F RTA16WE 20010111015852001011101585EU 2001 1 11 XNA00023 120010103A2611 SMOKE AIRBUS300 A300B4203 3930306EU CARGO BAY DETECTED A TC8AO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 GL23474AS 219 ON APPROACH TO DAY A & B LIGHTS ON MID1, MID2 & AFT CARGO ILLUMINATE ACCOMPONIED WITH SMOKE AND ODER. 2L72 4F RTA35EU 20010111013882001011101388NE 2001 1 11 CALA0100001 220010102A7261 ENGINE BOEING737 737524 1384721NM GE CFM56 CFM563B1 13802NE NR 2 LEAKING A CALAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW0914604 27317 856781 SHORTLY AFTER TAKEOFF FROM EWR SMOKE ENTERED THE CABIN AND THE LAV SMOKE DETECTORS ACTIVATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. THE SMOKE DISSIPATED RAPIDLY ONCE ON THE GROUND. THE AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND OIL IN THE NR 2 ENGINE BLEED DUCTS. THE NR 2 ENGINE WAS REMOVED AND REPLACED. BOTH COALESCER BAGS WERE REPLACED. THE ENGINE WAS RUN AND OPERATIONAL CHECKS WERE GOOD. 2L72 4F4 FRTA16WE E2GL 20010111014042001011101404NM 2001 1 11 CALA0100003 120010102A7110301A10805 COWLING BOEING737 7373Q8 1384670NM NR 2 ENGINE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0919382 26311 INSPECTION FOUND RT ENGINE NOSE COWL DENTED. THE RT ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 71-11-01. 2L72 4F RTA16WE 20010111039722001011103972WP 2001 1 11 ERKR200100017 120010104A523099211595 STRAP DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF THE DOUBLE-DRILLED HOLE TO THE INNER CHORD OF THE STATION 354 AND 373 FRAME OF THE MAIN CARGO DOOR BELOW TRACE L5L. THE REPAIR CONSISITS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSHING AND REPLACING THE INNER SKIN. PER ECRA 933-52-062-2 REV.A 2L72 4F A6WE 20010111044982001011104498EU 2001 1 11 UPS01134582 120010103A3260BDM3003 DETECTOR AIRBUSA300 A300F4622R 3930360EU MLG FAILED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01124UP 0808 INSPECTION TYPE:N/A AFTER TAKEOFF, LDG GEAR WOULD NOT RETRACT ON SYS 1. SWITCHED TO SYS 2 AND GEAR RETRACTED NORMALLY. R&R POSITION DETECTOR UNIT PER MEL 32-31-71, OPS CK OK. THIS CLEARS M206586. 2L72 4F RTA35EU 20010111045352001011104535NM 2001 1 11 UPS01234586 120010103A3350 BATTERY BOEING727 72727C 138400JNM COCKPIT FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01908UP 19114 INSPECTION TYPE:N/A EMERGENCY LIGHT AT ENTRY DOOR INOP LIGHT SWITCH LEFT ON. REPLACED BATTERIES. OPS CK OK 2L73 4F A3WE 20010111045612001011104561WP 2001 1 11 UPS01834585 120010103A3350 BATTERY DOUG DC8 DC871F 302199DWP CABIN FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01707UP 45907 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP, SWITCH APPEARS TO BE AT FAULT R & R 'D A/C MAIN BATTERY PER MM 24-30-01 AND 33-50-01 OPS CK GOOD 2L74 4F RT4A25 20010111036222001011103622NM 2001 1 11 C1HA200194001 120010101A3350 SIGN BOEING727 727290 138408WNM CABIN DISLODGED A C1HAO OTHER O OTHER TOTAKEOFF 1 GL15294AS 22146 AFT EMERGENCY EXIT SIGN FELL OFF ON TAKE OFF. RESECURED SIGN OPS NORMAL. 2L73 4F A3WE 20010111037942001011103794SO 2001 1 11 SWIA972241 120010101A3150 WARNING SYSTEM EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT FALSE ACTIVATIONA SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07584SW 120352 WHILE APPLYING TAKEOFF POWER RAN BOTH ENGINES. COULD NOT DUPLICATE. CHECKED ENGINE CONTROL CHIME WITH EECS OFF. CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20010111037962001011103796SO 2001 1 11 SWIA972243 120010103A3150 WARNING SYSTEM EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE COCKPIT MALFUNCTIONED A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07218SW 120287 ON TAKE OFF ROLL, GOT TRIM AURAL WARNING WITH TRIM SET IN GREEN RANGE. ABORTED TAKEOFF. PERFORMED AURAL WARNING RESET PROCEDURES, CHECKS GOOD IAW MM 31-63-00 2L72 4T4 TRTA31SO E20NE 20010111045252001011104525NE 2001 1 11 TWAA0100301 220010102A7200 ENGINE BOEING757 7572Q8 1384972NM PWA 2037 PW2037 NE NR 1 FAILED A TWAAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 CE05701TW 28160 4906 IN CRUISE A LOUD BANG WAS HEARD FROM THE LEFT ENGINE AND IT SPOOLED DOWN. MADE AN UNSCHEDULED LANDING AT MSP. THE ENGINE WAS REPLACED. CHECK-C 12-5-00 LAX. 2L72 4F4 FRTA2NM E17NE 20010111038692001011103869WP 2001 1 11 ERKR200100024 120010105A523059211653 FITTING DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 ADDRESSES REPAIR OF SEVERAL EXTRA HOLES AND OVERSIZE HOLES COMMON TO THE MAIN CARGO DOOR HINGES AND FITTING ASSEMBLY. PER ECRA 933-52-086-2 2L72 4F A6WE 20010111038702001011103870WP 2001 1 11 ERKR200100025 120010105A5230992115943 SKIN DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF CHAFE DAMAGE TO THE EXTERNAL SKIN OF THE MAIN CARGO DOOR STATION 370.06 THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER AND A EXTERNAL AREO-CHAMFERED DOUBLER. PER ECRA 933-52-088-2 REV. B 2L72 4F A6WE 20010111051922001011105192EA 2001 1 11 JBXA000233 120010105A3230601R509675 CONTROL PANEL CNDAIRCL600 CL6002B19 EA MLG FAILED A JBXAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SO05589ML 7376 DISCREPANCY: FLT. 371 RDU/RDU AFTER TAKEOFF WITH GEAR HANDLE SELECTED UP HAD GEAR DISAGREE MESSAGE. AIRCRAFT RETURNED TO RDU. CORRECTIVE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW CL-65 MM 32-31-01. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW MM 32-30-00. 2L72 4F RTA21EA 20010111038712001011103871WP 2001 1 11 ERKR200100026 120010105A5330592176469 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 ADDRESSES REPLACEMENT OF DAMAGED SKIN PANEL LOCATED BETWEEN STATION 229 AND 301, L11-L18, LEFT HAND SIDE. ADDITIONALLY THE DAMAGED SINGLE SKIN PANEL WILL BE REPLACED WITH TWO (2) NEW SECTIONS DUE TO MATERIAL AVAILABILLY. PER ECRA 933-53-051-2 REV.A 2L72 4F A6WE 20010111058392001011105839WP 2001 1 11 MWEA010024 120010104A335060030451 BATTERY PACK DOUG DC9 DC932 3022066WP FUSELAGE DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31401ME 47133 FORWARD BANK OF EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHEN POWERING DOWN THE AIRCRAFT. -- MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. 2L72 4F A6WE 20010111038722001011103872WP 2001 1 11 ERKR200100027 120010105A53115920338501 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 737 & 756 FRAMES, L6L & L6R. CONSISTS PLUGGING DISCREPANT HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-055-2 REV.A 2L72 4F A6WE 20010111041752001011104175NM 2001 1 11 F3LA200100002 120010102A7110 FAIRING BOEING737 737228 13844AGNM NR 2 ENGINE CRACKED A F3LAK NONE O OTHER ININSP/MAINT 1 NM03234TR 3086 23004 DURING C-7 CHECK, INSPECTION REPORTED A 1/2 INCH CRACK ON INSIDE AFT CORNER OF NR 2 ENGINE INBOARD FIXED FAIRING. MAINTENANCE REMOVED DAMAGED GUSSET AND "L" ANGLE AND FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 54-10-2, 51-10-2 AND 51-30-2. 2L72 4F RTA16WE 20010111025222001011102522NM 2001 1 11 DHL2001720001 120010104A5270 WARNING SYSTEM BOEING727 727228 NM CARGO DOOR ACTIVATED A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01720DH 19544 CLIMBING THROUGH 12.0, 5.0. ANNUNCIATOR PANEL "CARGO DOOR" LIGHT ILLUM. DOOR LIGHT BY ARMING SWITCH DID NOT ILLUM. AND NO PRESSURIZATION CHANGES NOTED. CABIN DIFF. AND CABIN NET WAS ABOUT 1800". (CORRECTIVE ACTION) ADJUSTED SWITCH ON 3RD LOCK AND OPS CHECKED SYSTEM TO 6 PSI DIFF. ALL INDICATIONS OPS CHECK GOOD. 2L73 4F A3WE 20010111025232001011102523 2001 1 11 DHL2001720002 420010104A34202588369905 ADI BOEING727 727228 NM COCKPIT UNSERVICEABLE A DHLAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SO01720DH 19544 ON DEPARTURE, F.O.'S ADI TUMBLED BECAME INOP - SWITCHING F.O. TO AUX V.G. WAS OF NO HELP - STILL INOP. (CORRECTIVE ACTION) SWAPPED NR 2 V.G. TO AUX V.G. AND R & R NR 2 ADI OPS CHECK GOOD PER M.M. CH 34-62-11 & M.M. CH 34-22-21. 2L73 4F A3WE 20010111009022001011100902NM 2001 1 11 01FDEA00002 120010104A531465561111 KEELBEAM BOEING727 727233 138408ANM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 CORROSION ON LT KEELBEAM AT BS 960 O/B FLANGE AROUND FASTENERS. ** S/D ** COMING 2L73 4F RTA3WE 20010111009032001011100903NM 2001 1 11 01FDEA00003 120010104A5313BAC1498140 STRINGER BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 NR 319 TEN OPEN FASTENER HOLES ON SIDE OF STRINGER 24 LT AT BS 480. ** S/D ** R&R & FAB PER FEDEX SRM 53-10-3, 53-10-3. 2L73 4F RTA3WE 20010111009182001011100918NM 2001 1 11 01FDEA00004 120010104A531365562362 STRINGER BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 CRACK AT STR 15 LT SIDE BS 720C-4 AFT OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20010111016282001011101628 2001 1 11 XNA01001 420010105A3418 COMPUTER AIRBUS300 A300B4203 3930306EU COCKPIT MALFUNCTIONED A TC8AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23370PC 134 ON CLIMB OUT SLATS RETRACTED 210 KTS. STICK SHAKER CAME ON. ICING WAS REPORTED, ALL OTHER CONDITIONS SEEMED NORMAL. ACTION TAKEN:FOUND SEVERAL PUSHED PINS BEHIND MASTER WARNING COMPUTER AT RECEPTICAL. RESUCURED PINS. MASTER WARNING SYSTEM OPS CHECK GOOD. STALL WARNING SYSTEM OPS CHECK GOOD I/A/W A300 MM CH 27-36-00. 2L72 4F RTA35EU 20010111009192001011100919NM 2001 1 11 01FDEA00005 120010104A5313655457512 STRINGER BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 NR 419 CRACK AT STR 15 LT SIDE BS 720D+4 FWD OF EXT LIGHT. ** S/D ** R&R PER IAW FEDEX SRM 53-10-3 FIG 1. 2L73 4F RTA3WE 20010111045622001011104562WP 2001 1 11 UPS01834587 120010104A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:N/A CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE APPROX 6 FT FWD OF OVERPRESS SAFETY VALVE CRACK LENGTH IS 3/4 INCH IN THE UPPER DIRECTION AND 1/2 INCH IN THE LOWER DIRECTION ALL.FERRY. FLIGHT.PROCEDURES.HAVE.BEEN.ACCOMPLISHED.AND.ACFT. IS.IN.SAFE.OPERATING.CONDITION.FOR.FERRY.FLIGHT..UPS AUTHORIZATION.J.WRIGHT.-.MGR.AMC 2L74 4F RT4A25 20010111046802001011104680WP 2001 1 11 UPS01834588 120010102A3350 BATTERY DOUG DC8 DC871F 302199DWP CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01707UP 45907 INSPECTION TYPE:IN EMERGENCY LIGHTS INOP. SWITCH APPEARS TO BE AT FAULT. R&R'D A/C MAIN BATTERY. 2L74 4F RT4A25 20010301002102001030100210EU 2001 3 1 SABA010002 120010102A3260 PIN BAG JETSTMJETSTM3201 1500217EU MLG DOWNLOCK LACK OF LUBE A SABAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO33957AE 957 AIRCRAFT 957 ON FLIGHT 5132 FROM CLT TO OAJ. WHEN THE LANDING GEAR WAS SELECTED DOWN FOR LANDING THE NOSE SAFE INDICATION WOULD NOT ILLUMINATE. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AND TAXIED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE CLEANED AND LUBED THE DOWNLOCK PIN AND HOOK FOR FULL TRAVEL TO THE LOCK POSITION. OPS CHEC WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA56EU 20010111058412001011105841WP 2001 1 11 MWEA010026 120010103A2913AS19593B PUMP DOUG DC9 DC932 3022066WP HYD SYSTEM INOPERATIVE A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31215ME 47744 RIGHT HYDRAULIC PRESSURE AND FLUID SHOWED ZERO AFTER TAKE OFF. -- REPLACED BROKEN HYDRAULIC LINE FROM AUX GEAR PUMP. REPLACED AUXILIARY ELECTRIC PUMP AND ENGINE DRIVEN PUMP. 2L72 4F A6WE 20010111058642001011105864WP 2001 1 11 MWEA010027 120010103A52105910081137 SKIN DOUG DC9 DC982 3022082WP PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31804ME 48030 FOUND 3/8 INCH CRACK ON LOWER FORWARD CORNER OF PASSENGER DOOR. -- INSTALLED DOUBLER IAW MD80/DC9 SRM (STRUCTURAL REPAIR MANUAL). 2L72 4F A6WE 20010111058182001011105818WP 2001 1 11 MWEA010004 120010105A5313591141217 LONGERON DOUG DC9 DC914 3022034WP FUSELAGE TOOL DAMAGE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 LONGERON 27R HAS DRILL MARKS BETWEEN STATION 427-446. -- FABRICATED AND INSTALLED LONGERON. 2L72 4F A6WE 20010111058192001011105819WP 2001 1 11 MWEA010005 120010105A532059114087 SPLICE DOUG DC9 DC914 3022034WP FUSELAGE GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 GOUGE IN RADIUS OF LONGERON SPLICE AT LONGERON 4 RIGHT, STATION 229. -- FABRICATED AND INSTALLED LONGERON SPLICE. 2L72 4F A6WE 20010111039312001011103931WP 2001 1 11 ERKR200100034 120010105A5330591970735 DOUBLER DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 INSPECTION REVEALED AN EXISTING BLENDED SKIN LOCATED BETWEEN RT STATION 917-937 AND LONGERON 28-30. THIS PROVIDES INSTRUCTIONS TO FABRICATE AND INSTALL A REPAIR AND FINGER DOUBLER.PER ECRA 933-53-069-2. 2L72 4F A6WE 20010111023512001011102351NM 2001 1 11 AWXA0001197 120010104A53126552878 BULKHEAD BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 BS 178 FWD PRESSURE BULKHEAD CENTER WEB RBL 5.7 HAS 1/2 INCH CRACK; WL 198-200 RBL 5.7 HAS 3/8 INCH CRACK UNDER STIFFENER. REMOVED DAMAGE AND INSTALLED DOUBLER AND REPAIR FILLERS IAW SRM 53-10-08 FIG 209; NDT VERIFIES CRACKS COMPLETELY REMOVED. 2L72 4F RTA16WE 20010111023712001011102371NM 2001 1 11 AWXA0001205 120010104A53206720381 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28314AW 23733 INTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. CUT OUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08 FIG 207; HFEC - NO CRACKS NOTED; FABED REPAIR PARTS IAW 53-10-08 FIG 207; TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW 51-40-02 2L72 4F RTA16WE 20010111023722001011102372NM 2001 1 11 AWXA0001208 120010104A531265C380902 SPLICE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 SIDE CHORD CRACKED FS 178 WL 207 RBL 26 AND WL 195 RBL 24. CUT OUT DAMAGED SECTION OF SIDE CHORD; DRILLED NEW CHORD; DRILLED NEW SPLICE ANGLE; FABED UPPER REPAIR SPLICE STRAP & INSTALLED IAW BOEING SB 737-53A1173 AND ER #03-5311-00340-JS2; HFEC INSPEC IAW B737 NTM PT.6, 51-00-00 FIG 23 - NO CRACKS NOTED ABOVE OR BELOW CUTLINE. 2L72 4F RTA16WE 20010111023752001011102375NM 2001 1 11 AWXA0001212 120010104A53306545765 SKIN BOEING737 7373S3 1384711NM FUSELAGE GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 EXT. FUSELAGE STA 395 BTW STR 5L & 6L SKIN HAS 2 LONG GOUGE. CUTOUT DAMAGED AREA IAW SRM 53-00-01; HFEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED REPAIR DOUBLER IAW SRM 53-00-01 FIG 202; INSTALLED REPAIR DOUBLER IAW 53-00-01 FIG 202. 2L72 4F RTA16WE 20010111024702001011102470NM 2001 1 11 AWXA0001213 120010104A5512BACR15CE5D SKIN BOEING737 7373S3 1384711NM HORIZONTAL STAB GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 LT HORIZ STABILIZER L/E UPPER SURFACE AT STA 166.30 HAS A DENT WITH A GOUGE (APPROX. 2.5 X 1.5). BLENDED GOUGE OUT OF LIMITS IAW SRM 51-10-02; CUTOUT DMGD AREA IAW 55-10-01; FABED SHIMS, FILLER AND DOUBLER; TREATED AND PRIMED PARTS AND INSTALLED PARTS IAW 51-40-02. 2L72 4F RTA16WE 20010111024712001011102471NM 2001 1 11 AWXA0001214 120010104A53106518420 WINDOW POST BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 3/8 INCH CRACK BETWEEN FLIGHT DECK WINDOW POST 1 & 2 FS 211.8. CUT OUT CRACK; FABED FILLER; INSTALLED FILLER AND BOEING P/N 69-71947-7 DOUBLER IAW SRM 53-10-01 FIG 210. 2L72 4F RTA16WE 20010111024722001011102472NM 2001 1 11 AWXA0001215 120010104A531065C25229 SHEAR TIE BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 UPON OPEN UP, FOUND CRACK AT STA 727D RIGHT ON FRAME/SHEAR TIE. CUT OUT DAMAGED PORTION AT STA 727D STR 27R IAW SRM 53-00-07; FABED REPAIR PARTS IAW 53-00-07 FIG 203; INSTALLED REPAIR PARTS IAW 51-40-02. 2L72 4F RTA16WE 20030416000862003041600086WP 2003 4 16 AALA20021761 120010425A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FUSELAGE GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW21453AA 49558 TUL - FOUND CABIN FLOOR BEAM IS GOUGED STATION 389. BLENDED AREA PER SRM 51-10-3, BEYOND LIMITS. REPAIRED PER AARD 53-20-00-21. (M) 2L72 4F A6WE 20030530000592003053000059NM 2003 5 30 2003F00336 120011220A5753652919510 FLAP TRACK BOEING727 72721 1384003NM LT WING CRACKED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX34220 19261 LEFT WING NR 4 FLAP TRACK FAIRING OUTBOARD TRACK, BEARING GUIDE, CRACKED. REMOVED AND REPLACED TRACK IAW B727 SRM 51-10-01. (M) 2L73 4F A3WE 20030530001042003053000104EA 2003 5 30 CA030416004 120011101A2742C3CF2907 ACTUATOR DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A135 52043NE HARTZLHCB3T HCB3TN3 GL HOROZONTAL STAB FAILED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) FROM TSB A01A0112, FOLLOWING TAKE OFF OF A FLOAT EQUIPPED DHC 3T, THE CONTROL COLUMN PITCHED VIOLENTLY FORWARD AND BACK BEFORE RETURNING TO A NEUTRAL POSITION. THE AIRCRAFT THEN PITCHED DOWN AND CONTACTED THE WATER IN A NOSE DOWN, WINGS LEVEL ATTITUDE. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE AND SANK. THE OCCUPANTS ESCAPED WITHOUT SERIOUS INJURY. INVESTIGATION REVEALED THE CABLE-OPERATED JACKSCREW JAMMED DUE TO INTERNAL CORROSION OF THE JACKSCREW. ONCE JAMMED, THE RIVET SECURING THE FORK END TO THE ACTUATOR SHEARED RESULTING IN A FREE FLOATING HORIZONTAL STABILIZER. 1H71 3R4 T A815 E4EA 6 CP15EA 20030530000642003053000064NM 2003 5 30 2003F00339 120011229A575365413176 FLAP TRACK BOEING727 72721 1384003NM RT WING CRACKED A XP0BO OTHER O OTHER NRNOT REPORTED 1 SO35727PX 19261 RIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK ON FUSELGE IS CRACKED AT WBL 70.597. REMOVED AND REPLACED RIGHT WING TRAILING EDGE INBOARD FLAP UPPER ROLLER BEARING TRACK. (M) 2L73 4F A3WE 20010111028412001011102841NM 2001 1 11 DLM88010002 120010101A5200 DOOR DOUG MD88 MD88 3023688NM LEFT FUSELAGE LOOSE A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27983DL 53247 AFTER TAKEOFF PASSING 15000. FELT AND HEARD BANG. PAX IN ROW 10 ABC FELT VIBRATION IN SEATS AND FLOOR. SLOWED A/C VIB WENT AWAY. INCREASED SPEED VIB RETURNED - REPLACED GROUND A/C DOOR ON LEFT SIDE OF AIRCRAFT AT ROW 13 FOR WEAR 2L72 4F RTA6WE 20010116012122001011601212NM 2001 1 16 AWXA0001165 120010102A21317638102 CONTROLLER BOEING737 7373G7 1384595NM CABIN PRESSURE FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28308AW362343490 24710 *S/D* PDX - AIR TURNBACK - AUTO PRESSURIZATION PREVIOUSLY PLACED ON MEL 21-14 (12/28/2000); AFTER TAKEOFF FROM PDX, STANDBY PRESSURIZATION FAILED AND CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN NORMAL MODE; THE AIRCRAFT RETURNED TO PDX. IN PDX PRESSURIZATION INTEGRITY CHECK WAS PERFORMED PER AWA TASK CARD F1B21006 AND NO FAULTS NOTED; THE CABIN PRESSURE CONTROLLER WAS REPLACED AND FUNCTIONAL CHECKS WERE GOOD; MEL 21-14 WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE, NO FURTHER FAULTS HAVE BEEN REPORTED AS OF 1/12/01. 2L72 4F RTA16WE 20010111005792001011100579NM 2001 1 11 AWXA0001168 120010102A3397BMS13131122 WIRE BOEING737 73733A 1384673NM SEAT 2B BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B FAILED TO ILLUMINATE DURING TEST. FOUND BROKEN WIRE AT SEAT 2B; SPLICED THE WIRE AND LIGHT OPS CHECKED GOOD 2L72 4F RTA16WE 20010111005802001011100580NM 2001 1 11 AWXA0001172 120010102A3397BMS13131122 WIRE BOEING737 73733A 1384673NM SEAT 3C CHAFED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 EMERGENCY LIGHTING INOP ROWS 3-7. REPAIRED WIRING AT SEAT 3C 2L72 4F RTA16WE 20010111023282001011102328NM 2001 1 11 AWXA0001173 120010102A335020121 CHARGER BOEING737 737301 1384611NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28326AW 23258 RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER; LIGHT CHECKS GOOD 2L72 4F RTA16WE 20010111009012001011100901WP 2001 1 11 01FDEA00001 120010103A7830 TRANSMITTER DOUG DC10 DC1010F 3022111WP NR 2 ENGINE T/R FAILED A FDEAO OTHER J WARNING INDICATION LDLANDING 1 SO25053FE 47807 NR 2 ENGINE THRUST REVERSER FAILED TO CLOSE AFTER LANDING, REVERSER UNLOCK & REVERSER 2 VALVE OPEN CAUTION LIGHTS ILLUMINATED. C/W RED TABS PROC. ** S/D ** R&R THRUST REVERSER. SYS CK GOOD. 2L73 4F A22WE 20010111045342001011104534NM 2001 1 11 UPS01234584 120010102A3350 BATTERY BOEING727 727247 138408FNM COCKPIT FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01208UP 21701 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR INOP R&R BATTERIES ON EMERGENCY LIGHT. SYS OP CKS GOOD 2L73 4F A3WE 20010111014332001011101433EU 2001 1 11 QXEA0100001 120010101A3350 SIGN FOKKERF28 F28MK4000 4990810EU CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09491US 11156 GEG - THE FORWARD CENTER ISLE EXIT SIGN WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20010111051282001011105128 2001 1 11 GLBA9191 420010102A3416066030620008 ALTIMETER BEECH 1900 1900D 1154162CE COCKPIT INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01179GL2312 UE179 RETURN TO BLOCK - #1 ALTIMETER FLAGGED ON CLIMB OUT, R/R ALTIMETER OPS CHECKED SYSTEM GOOD 2L72 4T RTA24CE 20010111020942001011102094EU 2001 1 11 RAIA0012060 120010102A24358260121 STARTER GEN AEROSPATR72 ATR72202 8680940EU NR 1 ENGINE FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03721TE1673 528 217 7158-STL-DURING CLIMB #1 DC GENERATOR FELL OF LINE AND WOULD NOT RESEST. MAINTENANCE REMOVED AND REPLACED #1 STARTER GENERATOR IAW J41 MAINTENANCE MANUAL. 2H72 4T RTA53EU 20010111020952001011102095EU 2001 1 11 RAIA0012061 120010102A3240S2728117820000 SPRING AEROSPATR42 ATR42300 8680920EU BRAKE SYSTEM FAILED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03421TE 102 7330-STL-LEFT HAND BRAKE GRABS FULL LOCKED WHEN PEDAL IS BARELY PUSHED IN WITH HYDRAULICS OFF. THE LEFT PEDAL GOES DOWN VERY EASILY AS IF NO SPRING TENSION. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT HAND PEDAL ARTIFITIAL FEEL SPRING IAW ATR42 MAINTENANCE MANUAL. 2H72 4T RTA53EU 20010111024752001011102475NM 2001 1 11 AWXA0001218 120010104A53206545614 TIE CLIP BOEING737 7373S3 1384711NM FUSLEAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 STR TIE CLIP CRACKED ON LOWER END OF BOTH FLANGES FS 312 BL 0. REMOVED STR TIE CLIP IAW SRM 51-40-02; FABED SHEAR CLIP IAW 55-10-04; INSTALLED SHEAR CLIP IAW 51-40-02 2L72 4F RTA16WE 20010111024772001011102477NM 2001 1 11 AWXA0001220 120010104A531165C3760716 FRAME BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 BS 178 FWD PRESS. BLKHD AFT SIDE LBL 5.7 WL 185 1 1/2 CRACK IN RADIUS OF VERT. CHORD O/B SIDE. REMOVED DAMAGED SECTION IAW SRM 53-10-08; FABED REPAIR PARTS, FILLERS IAW 53-10-08; REMOVED AND REINSTALLED ADJACENT STRUCTURE IAW 51-40-02; REINSTALLED REPAIR PARTS. 2L72 4F RTA16WE 20010111024782001011102478NM 2001 1 11 AWXA0001221 120010104A531165163006301 FRAME BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 SIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.4L) & WL 195 LBL 24 (1.4L). CUTOUT DAMAGED SECTION OF SIDE CHORD; DRILLED NEW SPLICE ANGLE AND NEW CHORD; FABED UPPER FRAME SPLICE STRAP AND INSTALLED IAW BOEING SB 737-53A1173 AND ER 03-5311-00340-JS2. 2L72 4F RTA16WE 20010111024792001011102479NM 2001 1 11 AWXA0001222 120010104A53206937253 BEAM BOEING737 7373S3 1384711NM SUB FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 CABIN FLOOR STA 685 LBL 46 FLOOR BEAM WEB HAS CRACK. REMOVED CRACKED STUB BEAM; FABED NEW STUB BEAM IAW DWG BAC69-37253 AND INSTALLED IAW BAC DWG 65-46543. 2L72 4F RTA16WE 20010111025182001011102518NM 2001 1 11 AWXA0001223 120010104A53306545765 SKIN BOEING737 7373S3 1384711NM FUSELAGE DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 UPPER EXT. FUSELAGE STA 230 LBL 7 - LBL 9 SKIN STATIC DAMAGE WENT OUT OF LIMITS. CUTOUT DAMAGE; FABED FILLER AND DOUBLERS AND INSTALLED REPAIR PARTS IAW SRM 53-00-01 FIG 201 2L72 4F RTA16WE 20010111007062001011100706NM 2001 1 11 AWXA0001228 120010104A3397BMS13131122 WIRE BOEING737 7373G7 1384595NM ROW 23L BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28306AW 24633 ROW 23 EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT ROW 23L. 2L72 4F RTA16WE 20010111030022001011103002EU 2001 1 11 AWXA0001229 120010104A3350 CIRCUIT BREAKER AIRBUS320 A320231 3930325EU EMERGENCY LIGHTSTRIPPED A AWXAO OTHER O OTHER CRCRUISE 1 WP28626AW 65 EMERGENCY LIGHT CIRCUIT BREAKER POPPED IN FLIGHT. PHX MAINTENANCE PER FOR RESET OF CIRCUIT BREAKER; EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD; CIRCUIT BREAKER REMAINED ENGAGED AND NO FURTHER FAULTS NOTED. 2L72 4F RTA28NM 20010111039322001011103932WP 2001 1 11 ERKR200100035 120010105A53119923405501 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE GOUGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF A DISCREPANT HOLE, AND A GOUGE TO THE INNER CHORD OF STATION 617 FRAME BETWEEN L15L & L16L. CONSISTS OF TRIMMING OUT THE DAMAGE AND INSTALLING A REINFORCEMENT STRAP.PER ECRA 933-53-070-2. 2L72 4F A6WE 20010111037032001011103703WP 2001 1 11 ERKE200100036 120010105A53119923408502 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF STATION 680 FRAME, AT L6L AND BETWEEN L11R & L15R. CONSISTS OF PLUGGING HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-071-2. 2L72 4F A6WE 20010111041762001011104176NM 2001 1 11 F3LA200100003 120010104A5610 WINDOW BOEING737 737228 13844AGNM COCKPIT LOOSE A F3LAA UNSCHED LANDING O OTHER CLCLIMB 1 NM03237TR 23007 AIR TURN BACK. FLIGHT CREW REPORTED PRESSURIZATION LEAK AT R-1 WINDOW, WHICH HAD BEEN REPLACED THE PREVIOUS NIGHT. RETURNED TO ELP WITHOUT INCIDENT. MAINTENANCE RETORQUED AND RESEALED R-1 WINDOW. 2L72 4F RTA16WE 20010111039332001011103933WP 2001 1 11 ERKR200100037 120010105A531199115411 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF STATION 699 FRAME AT L6R & L6L. CONSISTS OF PLUGGING DISCREPANT HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS.PER ECRA 933-53-072-2 2L72 4F A6WE 20010111058682001011105868NM 2001 1 11 MWEA010031 120010102A53129951888111 BULKHEAD DOUG MD88 MD88 3023688NM FUSELAGE TORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 BULKHEAD WEB HAS A TEAR APPROXIMATELY 2 INCHES ABOVE FLOOR AT APPROXIMATELY LONGERON 29 LEFT. -- INSTALLED DOUBLER IAW DC9/MD80 STRUCTURAL REPAIR MANUAL. 2L72 4F RTA6WE 20010111039352001011103935WP 2001 1 11 ERKR200100039 120010107A53119923412502 FRAME DOUG DC9 DC933F 302207AWP 658 DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 658 FRAME BETWEEN L8R & L15R. CONSISTS OF PLUGGING DISCREPANT HOLES AND INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS. PER ECRA 933-075-2 REV. B 2L72 4F A6WE 20010111039372001011103937WP 2001 1 11 ERKR200100041 120010107A53119921594501 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO STATION 434 & 439 FRAMES L5L & L18L. CONSISTS OF PLUGGING AND TRIMMING OUT DISCREPANT HOLES AND INSTALLING REPAIR BUSHINGS, REINFORCEMENT STRAPS AND GUSSETS.PER ECRA 933-53-090-2. 2L72 4F A6WE 20010111043772001011104377WP 2001 1 11 ERKR200100044 120010107A53119911504 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DAMAGED STATION 76, 89 & 95 FRAMES BETWEEN Z=-10 & Z=8 LHS. CONSISTS OF REMOVING AND REPLACING THE DAMAGED FRAME SECTIONS AND INSTALLING SPLICES TO REJOIN THE REPLACEMENT AND EXISTING SECTIONS. PER ECRA 933-53-092-2. 2L72 4F A6WE 20010111044142001011104414WP 2001 1 11 ERKR200100046 120010107A5311 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE MISDRILLED B ERKRK NONE W INADEQUATE Q C ININSP/MAINT 1 WP07933F 47191 REPAIR OF MISDRILLED HOLE DAMAGE; LOCATED BETWEEN STATIONS 294 & 301, L10L TO L18L; FRAME AND CLOSEOUT WEB. CONSISTS OF REMOVING AND REPLACING THE DAMAGED LOWER PORTION OF THE FRAME AND INSTALLING A SPLICE TO JOIN THE EXISTING AND REPLACEMENT SECTIONS, INSTALLING A REPAIR BUSHING IN THE INNER CHORD OF THE FRAME ABOVE THE SPLICE AND FINALLY ADDING A DOUBLER TO THE INBD SIDE OF THE CLOSEOUT WEB. PER ECRA 933-53-095-2. 2L72 4F A6WE 20010111044842001011104484WP 2001 1 11 ERKR200100047 120010107A5347 SEAT TRACK DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF CORROSION DAMAGE TO DOUBLE SEAT TRACK LBL 27 BETWEEN STATIONS 398.5 AND 476.5. CONSISTS OF CUTTING OUT, REMOVING AND REPLACING THE DAMAGED PORTION OF SEAT TRACK BETWEEN 398.5 AND 476.5 AND INSTALLING SPLICES TO JOIN THE EXISTING AND REPLACEMENT SECTIONS. PER ECRA 933-53-097-2. 2L72 4F A6WE 20010111044862001011104486WP 2001 1 11 ERKR200100049 120010107A5311 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE MISDRILLED B ERKRK NONE W INADEQUATE Q C ININSP/MAINT 1 WP07933F 47191 REPAIR OF MISS-DRILLED HOLE DAMAGE TO FRAME AND CLOSEOUT WEB AT STATION 207, L11L. CONSISTS OF DRILLING OUT THE MISS-DRILLED HOLES IN THE FRAME AND THE WEB AND INSTALLING REINFORCEMENT STRAPS.PER ECRA 933-53-100-2. 2L72 4F A6WE 20010111044872001011104487WP 2001 1 11 ERKR200100050 120010107A5320991007811 ANGLE DOUG DC9 DC933F 302207AWP FUSELAGE ELONGATED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF AN ELONGATED IN THE LOWER CUSP ANGLE P/N 9910078-11 AT STATION 207, LHS. CONSISTS OF DRILLING OUT THE DAMAGE AND INSTALLING A FILLER AND REINFORCEMENT STRAP. PER ECRA 933-53-101-2. 2L72 4F A6WE 20010111025242001011102524NM 2001 1 11 DHL2001720003 120010104A5270 SWITCH BOEING727 727228 NM OUT OF ADJ OUT OF ADJ A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01720DH 19544 CLIMBING THRU 12.0 S/O ANNUNCIATOR PANEL(CARGO DOOR)LIGHT ILLUM. DOOR LIGHT BY ARMING SWITCH DID NOT ILLUM, AND NO PRESSURAZATION CHANGES NOTED.CABIN DIFF AND CABIN ALT WAS ABOUT 1800. ADJUSTED SWITCH ON 3RD LOCK AND OPS CHK SYSTEM TO 6 PSI DIFF.ALL IND GOOD. 2L73 4F A3WE 20010111044882001011104488WP 2001 1 11 ERKR200100051 120010108A5315 FLOORBEAM DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF CRACKED FLOOR BEAM UPPER CHORD FORWARD FLANGE AT STATION 389, RBL 54.5. CONSISTS OF TRIMMING OUT THE DAMAGE AND INSTALLING A NET FIT FILLER AND NESTED LAYERED REPAIR ANGLES. PER ECRA 933-53-102-2. 2L72 4F A6WE 20010111025252001011102525 2001 1 11 DHL2001720004 420010104A34202588369905 ADI BOEING727 727228 NM COCKPIT UNSERVICEABLE A DHLAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SO01720DH 19544 ON DEPARTURE F/OS ADI TUMBLED AND BECAME INOP SWITHING F/O TO AUX VG WAS OF NO HELP, STILL INOP. SWAPPED NR 2 VG TO AUX VG AND R&R NR 2 ADI. OPS CHKED OK PER M/M 34-22-21 2L73 4F A3WE 20010111045862001011104586WP 2001 1 11 ERKR200100056 120010108A533099216961 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF A CRACK IN 9921696-1 SKIN ( INNER WEB )AT STATION 306, L4L. CONSISTS OF TRIMMING OUT THE CRACK AND INSTALLING DOUBLERS. PER ECRA 933-53-110-2. 2L72 4F A6WE 20010111019582001011101958EA 2001 1 11 COMA0160044 120010104A532060034017595 ANGLE CNDAIRCL600 CL6002B19 EA FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01914CA18259 7012 PERFORMED A MAJOR REPAIR AT F.S. 280.00 AFT "J" ANGLE IS CRACKED AT THE TWO CENTER NUT PLATES. REPAIRED CRACKED AFT "J" ANGLE F.S. 280 BETWEEN LBL9 AND RBL 9 IAW WVAC E.O. 601R-53-2081A. 2L72 4F RTA21EA 20010111045872001011104587WP 2001 1 11 ERKR200100057 120010108A541499577434 SKIN DOUG DC9 DC933F 302207AWP PYLON DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 INSPECTION REVEALED DAMAGE TO THE RIGHT HAND PYLON TRAILING EDGE UPPER SURFACE SKIN, THIS DOCUMENT PROVIDES MATERIAL SUBSTITUTION INSTRUCTIONS TO USE DMS1592 IN LIEU OF DMS1536 PER ECRA 933-54-068-2 REV. A. 2L72 4F A6WE 20010111045882001011104588WP 2001 1 11 ERKR200100058 120010108A553259121665 SKIN DOUG DC9 DC933F 302207AWP VERTICAL STAB GOUGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF GOUGE DAMAGE TO THE SKIN AND FINGER DOUBLER OF THE VERTICAL STABILLIZER REMOVABLE TIP FAIRING AT YV248, ZV141, R/H, L/H. THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND ADDING A REPAIR DOUBLER BEHIND THE SKIN AND FINGER DOUBLER. PER ECRA 933-55-080-2 REV B. 2L72 4F A6WE 20010111057342001011105734NE 2001 1 11 NACA200100002 220010105A8530356994 CYLINDER PWA R2800CB3 DOUG DC6 DC6A 3021706WP PWA R2800 R2800CB3 52026NE NR 3 ENGINE CRACKED A NACAEA ENGINE SHUTDOWN UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL0343872218 218 P32304 533294 P32304 DISCREPANCIES: M.I. @ 03:15Z, SHUT DOWN #3 ENGINE DUE TO RAPID BACKFIRE.CORRECTIVE ACTION: REPLACED #3 CYLINDER ON #3 ENGINE. 2L74 4R4 R 6A3 5E8 20010111045892001011104589WP 2001 1 11 ERKR200100059 120010108A57309919377504 PANEL DOUG DC9 DC933F 302207AWP WING DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 ADDRESSES REPAIR OF TWO (2) EXISTING TRIM-OUTS COMMON TO THE REFUEL DOOR LAND OF THE RH WING LEADING EDGE SPAR LOCATED BETWEEN XFS 258 AND XFS 280. PER ECRA 933-57-052-2 REV.A. 2L72 4F A6WE 20010111045902001011104590WP 2001 1 11 ERKR200100060 120010108A573099193711 SKIN DOUG DC9 DC933F 302207AWP WING DENTED B ERKRO OTHER O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DENT AND DING DAMAGE TO THE LHS L/H WING SKIN BETWEEN XIS 189 AND XOS 194. THIS CONSISTS OF TRIMMING AND DRILLING OUT THE DAMAGE AND INSTALLING FILLERS AND AN EXTERNAL DOUBLER. PER ECRA 933-57-082-2. 2L72 4F A6WE 20010111051202001011105120CE 2001 1 11 GLBA2001002 120010106A3350GE1864 BULB BEECH 1900 1900D 1154162CE CABIN BURNED OUT A GLBAK NONE L NO TEST ININSP/MAINT 1 CE01254GL UE254 EMERGENCY LIGHT INOP - R/R LIGHT BULB OPS CHECKED GOOD 2L72 4T RTA24CE 20010111051212001011105121CE 2001 1 11 GLBA2001003 120010107A243423078019 GENERATOR BEECH 1900 1900D 1154162CE NR 2 INOPERATIVE A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01169GL5842 1452 UE169 RETURN TO BLOCK - RIGHT GEN FELL OFF LINE WOULD NOT RESET, R/R STARTER-GEN SYSTEM OPS CHECKED GOOD 2L72 4T RTA24CE 20010111046062001011104606WP 2001 1 11 ERKR200100061 120010108A574499193012 FITTING DOUG DC9 DC933F 302207AWP WING MISDRILLED B ERKRK NONE W INADEQUATE Q C ININSP/MAINT 1 WP07933F 47191 THIS REPAIR OF MISS-DRILLED HOLE DAMAGE TO RHS WING # 1 SLAT OUTBOARD FITTING P/N 9919301-2 AT STATION XIS 137.921. CONSISTS OF PLUGGING THE DISCREPANT MISS-DRILLED HOLES AND INSTALLING A REINFORCEMENT FITTING. PER ECRA 933-57-096-2. 2L72 4F A6WE 20010111051222001011105122CE 2001 1 11 GLBA2001004 120010107A7700 WARNING LIGHT BEECH 1900 1900D 1154162CE LT ENGINE ILLUMINATED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE0194UX UE94 RETURN TO BLOCK - LEFT ENGINE BLEEDAIR FAIL INDICATION, RESEATED PCB OPS CHECKED SYSTEM GOOD RETURNED TO SERVICE 2L72 4T RTA24CE 20010111058422001011105842WP 2001 1 11 MWEA010034 120010104A3010983810564 RELAY DOUG DC9 DC914 3022034WP COCKPIT FAILED A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL3180ME 45795 WHILE USING AIRFOIL ANTI-ICE LEFT HAND ICE PROTECTION TEMPERATURE HI ANNUNCIATOR ILLUMINATED. AFTER SECURING SYSTEM, RH ICE PROTECTION TEMP. HI ILLUMINATED. SECURED THE SYSTEM. -- PERFORMED SYSTEM TESTS ON RIGHT HAND AND LEFT HAND SIDES. ALL TESTS WERE WITH-IN SPECIFIED LIMITS. ALL TEMPERATURES CHECK NORMAL. SYSTEM OPERATIONALLY CHECK GOOD. REMOVED AND REPLACED RELAY R2-664. 2L72 4F A6WE 20010111019732001011101973EA 2001 1 11 COMA0160047 120010101A32445010598 TIRE CNDAIRCL600 CL6002B19 EA NLG FAILED A COMAC ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 SO01868CA660 7427 NLG TIRE BLEW OUT DURING T/O. REPLACED NLG WHEEL ASSY. 2L72 4F RTA21EA 20010111045562001011104556NM 2001 1 11 TWAA0100504 120010107A3350 LIGHT BOEING757 757231 1384950NM CABIN CONTAMINATED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05714P 28482 THE EGRESS LIGHT STRIP IN FIRST CLASS WAS INOPERATIVE. DRIED MOISTURE FROM LIGHT TRACK IN FIRST CLASS. CHECK-C 8-16-00 LAX. 2L72 4F RTA2NM 20010111020192001011102019EA 2001 1 11 COMA0160051 120010102A5270 WARNING SYSTEM CNDAIRCL600 CL6002B19 EA PAX DOOR FALSE ACTIVATIONA COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01812CA 7381 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. DOOR LATCH MECHANISM OPERATES NORMALLY. 2L72 4F RTA21EA 20010111020332001011102033EA 2001 1 11 COMA0160054 120010102A2750855D1007 BPSU CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01936CA10327 7043 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU. 2L72 4F RTA21EA 20010111020352001011102035 2001 1 11 COMA0160056 420010103A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01964CA 7129 STALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020362001011102036EA 2001 1 11 COMA0160057 120010103A781022855030113 NOZZLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT ENGINE DEPARTED A COMAO OTHER DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 SO01933CA 7040 807441 VIBRATION FELT DURING FLIGHT, VIBRATION STOPPED DURING DECENT. POST FLIGHT INSP FOUND LEFT ENGINE TAILPIPE AND EXHAUST FAIRING HAD DEPARTED ACFT.REPLACED LEFT ENGINE. 2L72 4F4 FRTA21EA E15NE 20010111020382001011102038 2001 1 11 COMA0160059 420010103A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01403CA 7428 STALL FAIL CAUTION MESSAGE DURINT T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020622001011102062EA 2001 1 11 COMA0160062 120010103A5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA COCKPIT FAILED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01924CA12337 7026 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20010111020642001011102064EA 2001 1 11 COMA0160064 120010104A2750855D1009 BPSU CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01915CA3700 7013 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20010111020652001011102065 2001 1 11 COMA0160065 420010105A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01969CA 7141 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER 2L72 4F RTA21EA 20010111014542001011101454EU 2001 1 11 QXEA0100007 120010104A498038075412 APU FOKKERF28 F28MK4000 4990810EU AFT TAIL MALFUNCTIONED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09487US34556163 11238 LAX- CABIN FILLED WITH SMOKE WITH APU AND CABIN PACK ON. REMOVED AND REPLACED APU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20010111014362001011101436EU 2001 1 11 QXEA0100004 120010104A33505515800106 SIGN FOKKERF28 F28MK4000 4990810EU CABIN MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09484US 11234 SEA- EXIT LIGHT OVER ISLE MID CABIN FACING AFT IS DIM. REMOVED AND REPLACED MID CABIN AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20010111014532001011101453EU 2001 1 11 QXEA0100006 120010102A3350551590004 CIRCUIT BOARD FOKKERF28 F28MK4000 4990810EU CABIN MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09490US 11152 SEA- EXIT SIGN MID CABIN OVERHEAD AISLE FACING AFT IS DIM. REPLACED EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20010111031012001011103101SO 2001 1 11 SWIA972251 120010103A27513015001007 FCU EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FLAPS MALFUNCTIONED A SWIAK NONE N FALSE WARNING DEDESCENT 1 NM07195SW 120127 DURING DESCENT, FLAP CONTROL FAULT LIGHT ILLUMINATES WITHOUT SELECTING ANY FLAPS, INBOARD PAIR FLASHING PANEL. QRH PROCEDURE CLEARED FAULT. REMOVED AND REPLACED FCU DUE TO UNCOMMAND FLAPS FAULTS INBOARD. AFTER CYCLING FLAPS SEVERAL TIMES WITH OUT DUPLICATING PROBLEM IAW EMB 120 MM 27-50-06. PN ON 307500-1007 SN ON 0102 SN OFF 0169 2L72 4T4 TRTA31SO E20NE 20010111031232001011103123SO 2001 1 11 SWIA972252 120010102A2751 CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT FLAP CONTAMINATED A SWIAK NONE J WARNING INDICATION APAPPROACH 1 NM071105G 120105 FLAP ASSYMETRY INDICATION OUTBOARD SECTION ON APPROACH. AIRCRAFT REMAINED CONTROLLABLE, LANDED UNEVENTFULLY. FOUND ANTI-ICING FLUID IN RIGHT OUTBOARD FLAP ELECTRICAL CONNECTOR. CLEANED CONNECTOR. CYCLED FLAPS NUMEROUS TIMES. GROUND OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20010111031242001011103124SO 2001 1 11 SWIA972253 120010105A2752 ACTUATOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE FLAP FAILED A SWIAK NONE J WARNING INDICATION DEDESCENT 1 NM07190SW 120050 INBOARD FLAP CONTROL FAULT INFLIGHT. NO FLAP HANDLE MOVEMENT. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. CYCLED FLAPS NUMEROUS TIMES OPS CHECKS GOOD. RII 27-307PN ON 320300-1005 SN ON 0030 SN OFF 0421 2L72 4T4 TRTA31SO E20NE 20010125001672001012500167NM 2001 1 25 01FDEA00014 120010109A53116515929 FRAME BOEING727 727233 138408ANM FUSELAGE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 FRAME IS DENTED AT BS 520, STRINGER 22 RT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3. 2L73 4F RTA3WE 20010111046932001011104693WP 2001 1 11 UPS01834595 120010102A532037502571N FITTING DOUG DC8 DC871F 302199DWP FWD CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01713UP 46014 INSPECTION TYPE:C2 STA. 600 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3750257,AND SRM. 51-1-20D 2L74 4F RT4A25 20010111046952001011104695WP 2001 1 11 UPS01834597 120010103A5330575032219 DOUBLER DOUG DC8 DC871F 302199DWP AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01713UP 46014 INSPECTION TYPE:C2 STA. 1340 LONG. 31L FINGER DOUBLER IS CRACKED AND CORRODED REMOVED,FABRICATED,AND REPLACED FINGER DOUBLER I.A.W. DWG. 5750322, AND SRM.51-1-20D,51-1-21 2L74 4F RT4A25 20010111046962001011104696WP 2001 1 11 UPS01834598 120010101A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01713UP 46014 INSPECTION TYPE:C2 STA. 325 BL.0 SEAT TRACK IS WORN BEYOND LIMITS. REPAIRED SEAT TRACK I.A.W. SRM. 53-2-3 FIG.8 2L74 4F RT4A25 20010111020672001011102067EA 2001 1 11 COMA0160067 120010105A3350 LIGHT CNDAIRCL600 CL6002B19 EA CABIN INOPERATIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01785CA 7326 EMERGENCY LIGHTS AFT OF ROW 9 ARE INOPERABLE. AFTER AIRCRAFT WARMED, COULD NOT DUPLICATE, EMERGENCY LIGHTS OPERATE NORMAL. 2L72 4F RTA21EA 20010111020872001011102087 2001 1 11 COMA0160074 420010105A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01956CA 7105 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020882001011102088EA 2001 1 11 COMA0160075 120010105A5210 LATCH CNDAIRCL600 CL6002B19 EA PAX DOOR OUT OF ADJ A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01917CA 7017 CABIN DOOR CAUTION MESSAGE DURING FLIGHT. ADJUSTED DOOR LATCH MECHANISM. 2L72 4F RTA21EA 20010111020892001011102089EA 2001 1 11 COMA0160076 120010106A499038760016 SWITCH CNDAIRCL600 CL6002B19 EA APU MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01785CA 7326 APU OIL PRESSURE MESSAGE. REPLACED APU LOW OIL PRESSURE SWITCH. 2L72 4F RTA21EA 20010111020902001011102090EA 2001 1 11 COMA0160077 120010105A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 EA MLG ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01960CA 7117 NLG DISAGREE MESSAGE,NLG DID NOT INDICATE UP. COULD NOT DUPLICATE. LANDING GEAR RETRACT CHECKS WERE NORMAL. 2L72 4F RTA21EA 20010111051792001011105179WP 2001 1 11 IXXX0100002 120010108A32307000010101 SWITCH DOUG DC8 DC862 3021970WP RT GEAR DEFECTIVE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11799AL684611178 45922 ENROUTE FROM OKO TO QPG, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGH CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT RETURNED TO OKO FOR AN UNEVENTFUL LANDING. MAINTEANCE INSPECTED THE LANDING GEAR LOCATING A DEFECTIVE RIGHT MAIN GEAR UPLATCH SWITCH. MAINTENANCE REPLACED THE SWITCH AND PERFORMED A SUCCEFUL OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 20010111009442001011100944WP 2001 1 11 CALA0100008 120010108A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916807 49261 INSPECTION FOUND INTERCOSTAL AND AFT ATTACH ANGLE IN MID PIT CORRODED BETWEEN STA 709 AND 788, L27R TO L28R. THE INTERCOSTAL AND ANGLE WERE REMOVED AND A NEW INTERCOSTAL AND ANGLE WERE INSTALLED IAW SRM 51-30-2, 51-30-3, 51-30-4, AND 51-30-5. 2L72 4F A6WE 20010111024872001011102487EU 2001 1 11 DHL2001364007 120010104A2611 WARNING SYSTEM AIRBUS300 A300B4203 3930306EU SMOKE DETECTION MALFUNCTIONED A DHLAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01364DH IN FLIGHT THE MAIN BAY SMOKE LIGHT ILLUMINATED WITH THE MWP SMOKE LIGHT AND CHIME. LIGHT BECAME INTERMITTENT AND EXTINGUISHED PRIOR TO INITIATING EMERGENCY CHECKLIST. LIGHT REMAINED EXTINGUISHED AND ALL INDICATIONS WERE NORMAL. DIVERTED TO DEN FOR SAFETY REASONS. PERFORMED VISUAL INSPECTION OF MAIN BAY AND FOUND NO INDICATION OF SMOKE OR DAMAGE. PERFORMED OPERATIONAL CHECK OF ELECTRONIC SMOKE DETECTION SYSTEM PER M/M REF 26-11-00 AND SYSTEM OPS CHECKS GOOD OK TO CONTINUE. 2L72 4F RTA35EU 20010111024912001011102491NM 2001 1 11 DHL2001715001 120010103A2611 BULB BOEING727 727155C 138404ZNM SMOKE DETECTOR BURNED OUT A DHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01715DH 19618 UPPER MAIN CARGO SMOKE DETECTORS NOT VISIBLE. RELAMPED UPPER SMOKE DETECTOR. OPS CHECK GOOD I.A.W 26-17-01 2L73 4F A3WE 20010111021452001011102145WP 2001 1 11 DHL2001805001 120010103A2760 CURRENT LIMITER DOUG DC8 DC873F 302199FWP SPOILERS FAILED A DHLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01805DH 46125 ON TAXI OUT NOTED NO SPOILER PRESSURE. RAN ABNORMAL PROCEDURES STILL NO SPOILER PRESS. REPLACED ALL THREE CURRENT LIMITERS OPS CHECKS GOOD I.A.W. 27-00-00 2L74 4F RT4A25 20010111037372001011103737WP 2001 1 11 ERKR200000010 120010104A523099211662 FITTING DOUG DC9 DC933F 302207AWP CARGO DOOR CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 MAIN CARGO DOOR AT STA 389 LOWER CLOSE OUT WEB ( INTERIOR DOOR ) BETWEEN LONGERON 16L AND 17L FRAME CRACKED. 2L72 4F A6WE 20010111037392001011103739WP 2001 1 11 ERKR200100011 120010104A523099211662 FITTING DOUG DC9 DC933F 302207AWP CARGO DOOR CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 CRACK ON MAIN CARGO DOOR LOWER FITTING AT STA.409.062 2L72 4F A6WE 20010111037382001011103738WP 2001 1 11 ERKR200100010 120010104A523099211662 WEB DOUG DC9 DC933F 302207AWP FITTING CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 MAIN CARGO DOOR AT STA 389 LOWER CLOSE OUT WEB ( INTERIOR DOOR ) BETWEEN LONGERON 16L AND 17L FRAME CRACKED. 2L72 4F A6WE 20010111044382001011104438WP 2001 1 11 ERKR200100013 120010104A5230NPN FITTING DOUG DC9 DC933F 302207AWP 428.062 CRACKED B ERKRO OTHER O OTHER ININSP/MAINT 1 WP07933F 47191 crack on main cargo door lower fitting at station 428.062 2L72 4F A6WE 20010111023322001011102332NM 2001 1 11 AWXA0001178 120010103A53476546815 SEAT TRACK BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28154AW 23776 SEAT TRACK CRACKED AT RBL 25 & FS 727B. REMOVED GUSSET IAW SRM 51-40-02; FABED ABD INSTALLED REPAIR PLATE AND SHIM IAW 51-70-13; REINSTALLED GUSSET IAW 51-40-02 2L72 4F RTA16WE 20010111023342001011102334NM 2001 1 11 AWXA0001180 120010103A5312651630086 FRAME BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 SIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.3L). REMOVED DAMAGED SECTION OF CHORD; INSTALLED NEW SECTION OF CHORD, SPLICE ANGLE, AND SPLICE PLATE IAW E.R. 03-5311-00342-JS2 2L72 4F RTA16WE 20010111023352001011102335NM 2001 1 11 AWXA0001181 120010103A52106545871 SKIN BOEING737 7373G7 1384595NM PAX DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 R1 DOOR SKIN CRACKED AT UPPER HINGE CUT OUT. CUT OUT DAMAGE AND REPAIRED IAW SB 737-52-1096 FIG 6 DETAIL 1, AWA EO 52-00-02, AND SRM 51-40-02 2L72 4F RTA16WE 20010111021882001011102188EU 2001 1 11 RAIA0101002 120010102A3240S2728117820000 SPRING AEROSPATR42 ATR42300 8680920EU BRAKE SYSTEM DAMAGED A RAIAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03421TE 102 7330-STL-LEFT HAND BRAKE GRABS FULL LOCKED WHEN PEDAL IS BARELY PUSHED IN WITH HYDRAULICS OFF. THE LEFT PEDAL GOES DOWN VERY EASILY AS IF NO SPRING TENSION. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS LEFT HAND PEDAL ARTIFITIAL FEEL SPRING IAW ATR42 MAINTENANCE MANUAL. 2H72 4T RTA53EU 20010111023422001011102342NM 2001 1 11 AWXA0001188 120010103A531265163006 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 CENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.0L) AND WL 202 (1.0L). REMOVED DAMAGED AREA OF WEB; NDT VERIFIED NO CRACKS; FABED REPAIR PARTS AND INSTALLED PARTS IAW SRM 53-10-08 FIG 209 AT FS 178 RBL 5.0 WL 200 2L72 4F RTA16WE 20010111023432001011102343NM 2001 1 11 AWXA0001189 120010103A531265163006 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 CENTER WEB CRACKED FS 178 LBL 0.7 WL 187. CUT OUT DAMAGE; FABED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203 2L72 4F RTA16WE 20010111023442001011102344NM 2001 1 11 AWXA0001190 120010103A531265163006 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 BS 178 FWD PRESSURE BULKHEAD CENTER WEB CRACKED 2 EA 1/2 INCH LONG O/B SIDE OF LBL 5.7 AT WL 216 AND WL 214 UNDER STIFFENER. REMOVED DAMAGED AREA OF WEB AT WL 214 LBL 7.0; FABED REPAIR PARTS; INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209. 2L72 4F RTA16WE 20010111023452001011102345NM 2001 1 11 AWXA0001191 120010103A531265163006 BULKHEAD BOEING737 7373G7 1384595NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 BS 178 FWD PRESSURE BULKHEAD CENTER WEB CRACKED 2 EA 1/2 INCH LONG O/B SIDE OF RBL 5.7 AT WL 216 AND WL 214 UNDER STIFFENER. REMOVED DAMAGED AREA OF WEB AT WL 214 LBL 7.0; FABED REPAIR PARTS; INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209 2L72 4F RTA16WE 20010111023462001011102346NM 2001 1 11 AWXA0001192 120010103A5512657378351 SKIN BOEING737 7373G7 1384595NM HORIZONTAL STAB DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW25070 23776 LT HORIZ STABILIZER L/E AT L/E STA 122.39 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-10-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPLACEMENT RIB IAW 55-10-01; INSTALLED PARTS IAW SRM 55-10-01 FIG 203. 2L72 4F RTA16WE 20010111023472001011102347NM 2001 1 11 AWXA0001193 120010103A5512657378351 SKIN BOEING737 7373G7 1384595NM FUSELAGE DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 23776 LT HORIZ STABILIZER L/E AT L/E STA 233.59 HAS DENT OUT OF LIMITS. REMOVED FASTENERS AND RIB AND CUT OUT DMG IAW SRM 55-10-01; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 - NO CRACKS NOTED; FABED DOUBLER AND FILLER IAW 55-10-01; FABED REPLACEMENT RIB IAW 55-10-01; INSTALLED PARTS IAW SRM 55-10-01 FIG 203. 2L72 4F RTA16WE 20010111023672001011102367NM 2001 1 11 AWXA0001201 120010103A575365C252752 BEAM BOEING737 7373G7 1384595NM WING CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28154AW 23776 RT WING LOWER T/E METAL SEAL FWD OF AILERON IS CRACKED. REMOVED AND REPLACED BEAM ASSY IAW SRM 51-40-02, 51-40-05 AND 51-10-02 2L72 4F RTA16WE 20010111014342001011101434NM 2001 1 11 QXEA0100002 120010102A3350 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09825PH 213 PDX - FOUND LEFT HAND SIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010111021892001011102189NE 2001 1 11 RAIA0101004 220010103A732031055016 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE FALSE INDICATIONA RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03560HK9758 9758 41076 76082 7494-STL-DURING TAKE OFF RIGHT HAND IEC CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND P2 SENSOR IAW GARRETT TPE 331 MAINTANACE MANUAL. 2L72 4T4 TRTA41NM E18NE 20010111039712001011103971WP 2001 1 11 ERKR200100016 120010104A52309921583 STRAP DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF THE DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 373 FRAME OF THE MAIN CARGO DOOR ABOVE TRACE LL "G". THE REPAIR CONSISITS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT STRAP AND REPAIR BUSHING AND REPLACING THE INNER SKIN. PER ECRA 933-52-060-2 REV.A 2L72 4F A6WE 20010111014032001011101403WP 2001 1 11 CALA0100002 120010101A5543 TAB DOUG DC9 DC982 3022082WP RUDDER LOOSE A CALAK NONE O OTHER ININSP/MAINT 1 SW0916807 49261 INSPECTION FOUND RUDDER TAB T/E METAL TAB LOOSE ON RT SIDE. THE RUDDER TRIM TAB WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-20-02, PARAGRAPH B & C. 2L72 4F A6WE 20010111039732001011103973WP 2001 1 11 ERKR200100018 120010104A523099211585 ANGLE DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 411 AND 430 FRAMES OF THE MAIN CARGO DOOR BELOW TRACE L5L. THE REPAIR CONSISTS OF DRILLING OUT THE DAMAGE, INSTALLING A REINFORCEMENT ANGLE AND REPAIR BUSHING AND REPLACING THE INNER SKIN. PER ECRA 933-52-063-2 REV.A 2L72 4F A6WE 20010116011852001011601185WP 2001 1 16 UPS01834583 120010103A2710 CONTROL VALVE DOUG DC8 DC873F 302199FWP RT AILERON BINDING A IPXAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO01866UP 45966 INSPECTION TYPE:N/A AILERON BINDING, DURING CONTROL CHECKS AILERON WOULD NOT RETURN TO NEUTRAL ON ITS OWN AFTER BEING DISPLACED TO THE RIGHT. RTB *S/D* REMOVED AND REPLACED RT AILERON POWER CYLINDER/CONTROL VALVE UP TO STEP B2 AGE 204 MM 27-11-06. OPS CK LEAK CK GOOD. 2L74 4F RT4A25 20010111037952001011103795EA 2001 1 11 SWIA972242 120010103A2751 POTENTIOMETER CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT OUT OF ADJ A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07423SW 7456 ON TAXI OUT FLAPS WERE SET TO 20 DEGREES AND EICAS INDICATION IS 18 DEGREES. ADJUSTED LEFT AND RIGHT FLAP INDICATION POTENTIOMETERS PER CRJ MM 27-55-01. RAN FLAPS EICAS INDICATIONS NORMAL. FECU INDICATION OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 20010111047082001011104708WP 2001 1 11 ERKR200100019 120010104A532099211513 ANGLE DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE TO THE INNER FLANGE OF THE STATION 364 AND STATION 379.5 FRAMES OF THE MAIN CARGO DOOR BETWEEN L5L AND L6L. THE REPAIR FOR EACH LOCATION, CONSISTS OF TRIMMING OUT THE DAMAGE AND NESTING A SET OF REPAIR ANGLES BEHIND THE INNER FLANGE OF THE FRAME. PER ECRA 933-52-066-2. 2L72 4F A6WE 20010111047092001011104709WP 2001 1 11 ERKR200100020 120010104A523099211514 ANGLE DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE DAMAGE TO THE INNER FLANGE OF THE STATION 347 FRAME OF THE MAIN CARGO DOOR BETWEEN L5L AND L6L . THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE AND NESTING A SET OF REPAIR ANGLES BEHIND THE INNER FLANGE OF THE FRAME.PER ECRA 933-52-067-2 REV.A 2L72 4F A6WE 20010111047102001011104710WP 2001 1 11 ERKR200100021 120010104A523099211445 STRAP DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 392 FRAME OF THE MAIN CARGO DOOR BELOW TRACE LL "H". THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER, REINFORCEMENT ANGLE AND STRAP. PER ECRA 933-52-078-2 REV.A 2L72 4F A6WE 20010111045262001011104526WP 2001 1 11 TWAA0100302 120010103A4990 SMOKE DOUG DC9 DC982 3022082WP CABIN DETECTED A TWAAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE05919TW 49368 ON SHORT FINAL SMOKE APPEARED IN THE CABIN WHEN ANTI-ICE WAS TURNED ON. ACCOMPLISHED PACK BURN OUT AND DEACTIVATED APU PER MEL. CHECK-C 5-12-00 MCI. 2L72 4F A6WE 20010111028702001011102870WP 2001 1 11 EFKR200100022 120010104A523099211445 STRAP DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF DOUBLE-DRILLED HOLE DAMAGE TO THE INNER CHORD OF THE STATION 411 FRAME OF THE MAIN CARGO DOOR BELOW LL "H". THE REPAIR CONSISTS OF TRIMMING OUT THE DAMAGE, INSTALLING A FILLER ANGLE, AND STRAP. PER ECRA 933-52-083-2 REV.A 2L72 4F A6WE 20010111045582001011104558WP 2001 1 11 TWAA0100601 120010108A3350 LIGHT DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05939AS 49657 THE FWD OVERWING EMERGENCY EXIT SIGN LH AND RH HAND, THE FWD ENTRY PORTABLE EMERGENCY LIGHT, EGRESS LIGHTS ROW 5 THRU 7, AND EGRESS LIGHTS ROW 22 THRU 27 WERE INOPERATIVE. REPLACED BATTERY IN THE BATTERY PACK PN 41B030CF00101 FOR THE EXIT SIGN AND FOR THE ENTRY LIGHT, REPLACED A LIGHT MODULE PN 0105606-005 FOR FWD CABIN EGRESS LIGHTS, AND ADJUSTED BATTERY CONTACTS FOR THE AFT CABIN EGRESS LIGHTS. CHECK-C 11-16-99 MCI. 2L72 4F RTA6WE 20010111045712001011104571WP 2001 1 11 TWAA0100606 120010104A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT CABIN SEAT TRACK NR 3, SEAT TRACK HAD CORROSION UNDER THE FWD LAVATORY. REMOVED CORROSION IN TRACK AREA. REPAIRED PER SRM 53-05 PAGE 10G AND 10H. REPLACED SECTION OF TRACK. 2L72 4F RTA6WE 20010111045742001011104574WP 2001 1 11 TWAA0100608 120010105A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT IN THE FWD CARGO BILGE, FROM STA 370 TO 427, RBL 9 INCHES, FLOOR SUPPORT AT DOOR ENTRANCE HAD CORROSION AROUND NUT PLATE HOLES. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01. 2L72 4F RTA6WE 20010111045752001011104575WP 2001 1 11 TWAA0100609 120010106A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT WAS CORRODED FROM STA 157 TO 201, RBL 44 INCHES. FABRICATED NEW FROM EXTRUSION. REPLACED PER SPM 6-70-01. 2L72 4F RTA6WE 20010111045762001011104576WP 2001 1 11 TWAA0100610 120010106A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT CABIN FLOOR SUPPORT WAS CORRODED AT STA 177, RBL 9 TO 42. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-30-2. 2L72 4F RTA6WE 20010111059762001011105976NE 2001 1 11 ANCF200100001 220010105A7200 BLADE BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE RT ENGINE FAILED W ANCFA UNSCHED LANDING CJ F.O.D. WARNING INDICATION TOTAKEOFF 1 SW99321LF 26269 31233 DURING T/O IN MIA, AFTER LIFTOFF SOME BIRDS WERE INGESTED BY RIGHT ENGINE, ENGINE FAILED. AIRCRAFT RETURNED TO MIA WITHOUT FURTHER PROBLEM.CORRECTIVE ACTIONACCOMPLISHED AS PER EWO 75-72-4226PERFORMED FIM PROCEDURE AFTER BIRD STRIKE IAW FIM 71-00-00, THEN PERFORMED AN INSPECTION TO ALL LPC BLADES IAW AMM 72-31-13, REMOVED 6 BLADES DAMAGED, ALSO APPLY DRY FILM LUBRICANT TO LPC BLADES IAW AMM 72-31-13 AND LPC ROTOR DISC IAW AMM 72-31-13, PERFORMED FAN TRIM BALANCE IAW AMM 72-31-13, ALL TEST WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E12EU 20010126000732001012600073NM 2001 1 26 01FDEA00010 120010109A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 FOUND CORROSION ON INNER SKIN AT LAP BS 720B + 10 INCHES, STR 26R, RBL 22. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-30-3 FIG 6. 2L73 4F A3WE 20010111009232001011100923NM 2001 1 11 01FDEA00012 120010106A3233731414 ACTUATOR BOEING727 72722 1384002NM RT MLG FAILED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25186FE 18872 01-002 DURING CLIMBOUT, LANDING GEAR SELECTOR IN OFF POSITION. RED DOORS LIGHT ILLUMINATED, WITH AMBER RT MLG DOOR LIGHT. REPLACED DOOR ACTUATOR PER B727 MM 32-32-081-4. LEAK & OPS CK OK. REMOVED GEAR PINS. 2L73 4F A3WE 20010111009242001011100924NM 2001 1 11 01FDEA00013 120010109A2612894120 FIRE DETECTOR BOEING727 7272S2F 1384O81NM NR 1 ENGINE FALSE ACTIVATIONA FDEAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO25204FE 22926 01-003 NR 1 ENGINE FIRE INDICATION ON T/O ROLL ABOUT 70 KNOTS. DISCHARGE BOTH BOTTLES, LIGHT STAYED ON. ** S/D ** R&R SENSING ELEMENT & BOTH BOTTLES PER IAW MM 26-11-012-4, 2627-071-4. ALL SYS CK GOOD. 2L73 4F A3WE 20010111036152001011103615WP 2001 1 11 ABXA010001 120010108A3230 HANDLE DOUG DC8 DC863 302198AWP MLG MALFUNCTIONED A ABXAO OTHER O OTHER CLCLIMB 1 GL23813AX 46136 LANDING GEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. PRESSURIZATION WAS NORMAL AND THERE WAS NO WARNING HORN. CREW PUSHED IN THE ANTI-RETRACT LATCH AND LANDING GEAR CAME UP NORMALLY. ON DESCENT INTO ILN, CREW RE-CYCLED LANDING GEAR. THE LANDING GEAR OPERATED NORMALLY. MAINTENANCE INSPECTED AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION ADJUSTMENT AND TEST PROCEDURE, IAW DC-8 MM 32-30-00. NO DEFECTS WERE NOTED. INSPECTED NOSE GEAR AND GROUND SHIFT MECHANISM. NO DEFECTS WERE NOTED. 2L74 4F 4A25 20010111036162001011103616WP 2001 1 11 ABXA010002 120010109A561059124262 WINDOW DOUG DC8 DC863 302198AWP COCKPIT STUCK A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 FIRST OFFICERS CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. MAINTENANCE INSPECTED AND OPERATED THE FIRST OFFICERS CLEARVIEW WINDOW SEVERAL TIMES. THE WINDOW OPERATED NORMALLY IAW DC-8 MM 56-10. 2L74 4F 4A25 20010111027362001011102736NM 2001 1 11 SCNA001005 120010107A324226011825 BRAKE ASSY BOEING727 727282 138408TNM MLG FAILED A SCNAO OTHER O OTHER LDLANDING 1 GL15281SC 888 21949 DURING LANDING THE NUMBER ONE MAIN TIRE FAILED. THE NUMBER ONE BRAKE WAS FOUND LOCKED UP AND DAMAGED THE NUMBER ONE TIRE. REMOVED AND REPLACED THE NUMBER ONE BRAKE AND THE NUMBER ONE AND TWO TIRES. OPERATIONAL CHECKS GOOD. 2L73 4F RTA3WE 20010111028212001011102821NM 2001 1 11 SCNA01006 120010109A3350 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 DURING A MAINTENANCE LINE CHECK THE THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPAIRED THE WIRING AND REMOVED AND REPLACED SELF CONTAINED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. 2L73 4F A3WE 20010111027832001011102783NM 2001 1 11 SCNA01004 120010104A33501000679 LIGHT BOEING727 7272J4 1384006NM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 21438 DURING A MAINTENACE "A" CHECK THE R1 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT, OPERATIONAL CHECKS GOOD. 2L73 4F RTA3WE 20010111009252001011100925NM 2001 1 11 01FDEA00015 120010110A2613 DETECTOR BOEING727 727232 1384082NM NR 3 ENGINE ACTIVATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO25497FE 20866 01-004 AT 5000 FT ON CLB OUT NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. NO IRREGULARITIES NOTED. CLEANED OVERHEAT DETECTION ELEMENT. RAN NR 3 ENGINE IAW JET RUN HANDBOOK, NO LEAKS NOTED. OK FOR SERVICE. 2L73 4F A3WE 20010111047112001011104711WP 2001 1 11 ERKR200100023 120010104A523099211449 FRAME DOUG DC9 DC933F 302207AWP CARGO DOOR DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 AUTHORIZES THE REPAIR OF MISS-DRILLED HOLE DAMAGE, IN THE AREA OF STATION 316, LL "C" TO THE INNER WEB AND DOUBLER OF THE MAIN CARGO DOOR. THE REPAIR CONSISTS OF PLUGGING THE DAMAGED SKIN AND LOWER WEB, BLENDING OUT THE DAMAGE TO THE FRAME. PER ECRA 933-52-085-2 REV.A 2L72 4F A6WE 20010111058152001011105815WP 2001 1 11 MWEA010001 120010102A7921548003 COOLER DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE RT ENGINE LEAKING A MWEAC ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL31216ME 47740 665323 RIGHT HAND OIL PRESSURE ON TOP END OF RED LINE QUANTITY AT 2 QTS. -- REPLACED TOP AFT FUEL OIL COOLER "B" NUT PACKING, SERVICED OIL. 2L72 4F4 F A6WE E2EA 20010111058172001011105817WP 2001 1 11 MWEA010003 120010104A53135911412123 LONGERON DOUG DC9 DC914 3022034WP FUSELAGE MISDRILLED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 LONGERON 27 LEFT AT STATION 351 HAS A DOUBLE DRILLED HOLE. -- FABRICATED AND REPAIRED SPLICE. 2L72 4F A6WE 20010111058382001011105838 2001 1 11 MWEA010023 420010103A2565113317 CLIP DOUG DC9 DC981 3022081WP ESCAPE SLIDE MISSING A MWEAK NONE O OTHER ININSP/MAINT 1 GL31807ME 48033 FORWARD SERVICE DOOR SLIDE COVER RIGHT SIDE KEEPS COMING OFF. -- MAINTENANCE REATTACHED LOWER SLIDE COVER LANYARD CLIP. 2L72 4F A6WE 20010111038732001011103873WP 2001 1 11 ERKR200100028 120010105A53439957975501 ANGLE DOUG DC9 DC933F 302207AWP NOSE GEAR WW DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 VISUAL INSPECTION REVEALED DAMAGE TO THE NOSE GEAR SUPPORT BEAM ON THE LEFT AND RIGHT HAND SIDES. THIS CONSISTS OF TRIMMING OUT THE DAMAGE AREA AND INSTALLING THE REPAIR SPLICE ANGLES AND THE REPAIR CAP. PER ECRA 933-53-056-2. 2L72 4F A6WE 20010111038992001011103899WP 2001 1 11 ERKR200100029 120010105A531159203381 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORD OF THE STATION 718 FRAME, L6L & L6R. CONSISTS OF PLUGGING DISCREPANT HOLES, INSTALLING REPAIR BUSHINGS AND REINFORCEMENT STRAPS AND REPLACING EXISTING GUESSETS AND FILLERS.PER ECRA 933-53-058-2. 2L72 4F A6WE 20010111051192001011105119CE 2001 1 11 GLBA2001001 120010103A21205238001 ELEMENT BEECH 1900 1900D 1154162CE CABIN TEMP FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01226GL UE226 RETURN TO BLOCK - DUAL ENVIROMENTAL FAILURE, REPLACED TEMP SENSOR AND PRECOOLER BYPASS VALVE SYSTEM OPS CHECKED GOOD RETURNED TO SERVICE 2L72 4T RTA24CE 20010111039022001011103902WP 2001 1 11 ERKR200100030 120010105A532099100789 WEB DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF CORRODED UPPER CUSP ANGLE P/N 9910078-9. CONSISTS OF CUTTING THE UPPER CUSP ANGLE AT STATION 179, REPLACING THE CORRODED PORTION AFT OF THE CUT, AND INSTALLING A SPLICE TO JOIN THE EXISTING AND REPLACEMENTS PORTIONS, ADDITIONALLY, DAMAGE TO THE LOWER CUSP ANGLE WILL BE TRIMMED OUT AND A NESTED ANGLES INSTALLED. PER ECRA 933-53-064-02 REV. B 2L72 4F A6WE 20010111009202001011100920NM 2001 1 11 01FDEA00006 120010104A531365562362 STRINGER BOEING727 727233 138408ANM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 NR 420 CRACK AT STR 15 RT SIDE BS 720B+4 FWD OF EXT LIGHT. ** S/D ** COMING 2L73 4F RTA3WE 20010111009212001011100921NM 2001 1 11 01FDEA00007 120010105A5320655989634 SUPPORT BOEING727 727232 1384082NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 NR 842 CORROSION ON WEB SUPPORT BS 572 - 580, RBL 54, WL 200. ** S/D ** R&R & FAB PER IAW FEDEX SRM 51-10-6, 51-10-2, 51-30-2, AND 51-30-5 BAC SPEC 5300, AND FEDEX DRWG 65-59896. 2L73 4F A3WE 20010111009222001011100922NM 2001 1 11 01FDEA00008 120010105A53116516330 FRAME BOEING727 727232 1384082NM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 NR 397 DOUBLE HOLE IN FRAME AT BS 870 JUST O/B OF STRINGER 3R. ** S/D ** R&R PER IAW FEDEX EA 7-5310-56211. 2L73 4F A3WE 20010111039032001011103903WP 2001 1 11 ERKR200100031 120010105A531299579061 BULKHEAD DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 INSPECTION REVEALED DAMAGE TO THE FORWARD CLOSE OUT WEBS. STATION 362-370 AND 427-435 THE REPAIR CONSISTS OF FABRICATE THE REPLACEMENT WEB AND RING DOUBLERS, AND INSTALLED. PER ECRA 933-53-065-2 2L72 4F A6WE 20010111039052001011103905WP 2001 1 11 ERKR200100033 120010105A531299577391 BULKHEAD DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE FRAME WEB AND SPLICE AT STATION 945 BETWEEN L9L AND L10L. CONSISTS OF INSTALLING A REPAIR BUSHING, REPLACING THE SPLICE AND INSTALLING A SPLICE DOUBLER. PER ECRA 933-53-057-2 REV. A. 2L72 4F A6WE 20010116011842001011601184NM 2001 1 16 UPS01534589 120010105A275018196918 FLAP BOEING757 75724APF 1384969NM WING MALFUNCTIONED A IPXAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01412UP 23852 INSPECTION TYPE:N/A DIVERTION - FLAP DISAGREE MSG. REMOVED AND REPLACED FLAP POSITION TRANSMITTER IAW MM 27-58-03. OPS CHK FLAP TRAVEL AND BITE CHK FSEU ALL NORMAL. P/N ON/OFF 18-1969-18, S/N ON -0750B, S/N OFF 0533B. 2L72 4F RTA2NM 20010111006642001011100664NM 2001 1 11 TWAA0100401 120010103A3397 WIRE BOEING767 7673Y0 NM GALLEY DISCONNECTED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05639TW 26208 THE EGRESS LIGHTS WERE INOPERATIVE ON THE LT SIDE OF THE FWD GALLEY. FOUND WIRES DISCONNECTED. RECONNECTED THE WIRING. CHECK-C 2-10-00. 2L72 4F RTA1NM 20010111058652001011105865WP 2001 1 11 MWEA010028 120010104A335060030451 BATTERY PACK DOUG DC9 DC981 3022081WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31809ME 48071 AFT EMERGENCY LIGHT AT STATION 1308 AND 1336 REMAINED ON WITH APU POWER AND BATTERY POWER REMOVED. -- MAINTENANCE TROUBLESHOT AND VERIFIED BAD BATTERY PACK AND REPLACED B5-27. 2L72 4F A6WE 20010111037982001011103798SO 2001 1 11 SWIA972245 120010104A2163 SENSOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE A/C PACK FAILED A SWIAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 NM07288SW 120316 NOTICED HOT AIRCRAFT BEFORE TAKEOFF. AFTER TAKEOFF FA SMELLED SMOKE AND SMOKE DETECTOR IN LAV WENT OFF. RETURNED TO LAX. INSTALLED NEW LEFT PAC DUCT TEMP SENSOR. CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 20010111007022001011100702SO 2001 1 11 SWIA972247 120010104A2751 WIRE EMB 120 EMB120RT 3260202SO PWA 118 PW118 NE FLAP ACTUATOR GROUNDED A SWIAK NONE F FLT CONT AFFECTED APAPPROACH 1 NM07200CD 120200 ON APPROACH SELECTED FLAPS 25 THE RT OUTBOARD WENT 1 LIGHT BAR PAST FLAPS 25 AND CAUSED AN ASYMETRY. WE LANDED, PERFORMED THE QRH, THEN SELECTED FLAPS UP AND THE LT OUTBOARD DID NOT MOVE AND THE RT OUTBOARD WENT 2 LIGHT BARS UP AND CAUSED ANOTHER ASYMETRY. FOUND RT OUTBOARD FLAP ACTUATOR POTENTIOMETER WIPER WIRE GROUNDING TO AIRFRAME. ISOLATED TO SOLDER SLEEVE AT CANNON PLUG OF ACTUATOR. REPAIRED WIRING AND SOLDER SLEEVE W602-0023-22DR. OPS CHECK GOOD 2L72 4T4 TRTA31SO E20NE 20010111023362001011102336NM 2001 1 11 AWXA0001182 120010104A53126552878 BULKHEAD BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 CENTER WEB BULKHEAD 178 WL 200 LBL 537 HAS CRACK 3/8 INCH. REMOVED DAMAGE AND INSTALLED REPAIR IAW 53-10-08 FIG 209 2L72 4F RTA16WE 20010111023522001011102352NM 2001 1 11 AWXA0001198 120010104A5312654583340 WEB BOEING737 7373S3 1384711NM CABIN FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28315AW 23734 FLOOR WEB CRACKED FS 180 WL 207 LBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND BOEING DWG #65-45833 2L72 4F RTA16WE 20010111023652001011102365NM 2001 1 11 AWXA0001199 120010104A5321654583340 WEB BOEING737 7373S3 1384711NM CABIN FLOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 FLOOR WEB CRACKED AT FS 180 WL 207 RBL 26. FABED AND INSTALLED FLOOR WEB IAW SRM 51-10-02 AND DWG 65-45833 2L72 4F RTA16WE 20010111023702001011102370NM 2001 1 11 AWXA0001204 120010104A53206720382 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 INTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. CUT DAMAGED SECTION OF INTERCOSTAL IAW SRM 53-10-08; FABED REPAIR ANGLE, RADIUS BLOCK FILLER, AND FILLER IAW SRM 53-10-08 FIG 207; TREATED AND PRIMED PARTS IAW 51-20-01; INSTALLED PARTS IAW 51-40-02. 2L72 4F RTA16WE 20010111023732001011102373NM 2001 1 11 AWXA0001209 120010104A53106520722 DOOR FRAME BOEING737 7373S3 1384711NM FUSELAGE DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 FWD. CARGO DOOR, FWD DOOR FRAME DENTED 3 PLACES AT LOWER INSIDE END. REMOVED DAMAGED WEB IAW SRM 51-70-13 FIG 1; FABED REPLACEMENT PART IAW 51-70-13 FIG 1; INSTALLED REPLACEMENT PART IAW 51-70-13 FIG 1. 2L72 4F RTA16WE 20010111023742001011102374NM 2001 1 11 AWXA0001210 120010104A53126545409245 PRESSURE PANEL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 LT MLG WW STA 663 LBL 30 CEILING PRESSURE DECK HAS A CRACK. REMOVED DAMAGED AREA IAW ER 03-5310-99288-EY1; FABED REPAIR PARTS IAW ER 03-5310-99288-EY1; INSTALLED REPAIR PARTS IAW ER 03-5310-99288-EY1. 2L72 4F RTA16WE 20010111024732001011102473NM 2001 1 11 AWXA0001216 120010104A53136942159 INTERCOSTAL BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 STA 312 BL 0 INTERCOSTAL, JUST FWD OF E&E DOOR CRACKED. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02; FABED REPAIR PARTS IAW 51-40-02 AND ENGINEERING SUPPORT; INSTALLED PARTS IAW 51-40-02. 2L72 4F RTA16WE 20010111024742001011102474NM 2001 1 11 AWXA0001217 120010104A53126545614 BULKHEAD BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 CENTER WEB CRACKED FS 178 WL 187 RBL 0.7 (1.1L). CUTOUT DAMAGED SECTION OF WEB; HFEC - NO CRACKS NOTED; FABED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 FIG 203. 2L72 4F RTA16WE 20010111024762001011102476NM 2001 1 11 AWXA0001219 120010104A531169878671 FRAME BOEING737 7373S3 1384711NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28314AW 23733 BS 178 FWD PRESS. BULKHEAD AFT SIDE LBL 5.7 WL 185 1 CRACK IN RADIUS OF VERT. CHORD I/B SIDE. REMOVED DAMAGED AREA IAW SRM 53-10-08; INSTALLED NEW REPAIR PARTS IAW 53-10-08 FIG 205; FABED 5 EA. FILLERS AND INSTALLED SAME IAW 51-40-02. 2L72 4F RTA16WE 20010111025192001011102519EU 2001 1 11 AWXA0001224 120010104A33501013081 LIGHT AIRBUS320 A320231 3930325EU CABIN DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28643AW 315 FWD LEFT BLKHD EMERGENCY LIGHT INOP AND COVER MISSING. REMOVED AND REPLACED EMERGENCY LIGHT AT FWD LEFT BULKHEAD; LIGHT OPS CHECKS GOOD. 2L72 4F RTA28NM 20010111025202001011102520NM 2001 1 11 AWXA0001225 120010104A335020121 CHARGER BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28903AW 23323 FWD. AIRCRAFT EMERGENCY ISLE LIGHTING INOP. REMOVED AND REPLACED FWD BATTERY PACK AND FWD BATTERY CHARGER; EMERGENCY LIGHTS OPS CHECK GOOD. 2L72 4F RTA2NM 20010111025212001011102521NM 2001 1 11 AWXA0001226 120010104A3350 LIGHT BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 SEAT EMERGENCY LIGHT AT SEAT 21C INOP. RESECURED LOOSE WIRE; LIGHT OPS CHECKS GOOD 2L72 4F RTA16WE 20010111058442001011105844 2001 1 11 MWEA010036 420010108A34144057800901 INDICATOR DOUG MD88 MD88 3023688NM COCKPIT INOPERATIVE A MWEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL31701ME 49760 FIRST OFFICERS AIRSPEED INDICATOR FLAGGED. -- VERIFIED DISCREPANCY. REMOVED AND REPLACED FIRST OFFICERS AIRSPEED INDICATOR. 2L72 4F RTA6WE 20010116011612001011601161WP 2001 1 16 MWEA010014 120010108A532099576703 INTERCOSTAL DOUG DC9 DC914 3022034WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 OPEN FASTENER HOLES ON INTERCOSTAL AT LONGERON 8 RIGHT, BETWEEN STATION 566 AND 544. FABRICATED AND INSTALLED DOUBLER AND INTERCOSTAL. 2L72 4F A6WE 20010116011622001011601162WP 2001 1 16 MWEA010015 120010108A532099576673 INTERCOSTAL DOUG DC9 DC914 3022034WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 OPEN FASTENER HOLES ON INTERCOSTAL AT LONGERON 18 LEFT, BETWEEN STATION 566 AND 544. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20010116011632001011601163WP 2001 1 16 MWEA010017 120010108A5310991224319 SHEAR TIE DOUG DC9 DC914 3022034WP FUSELAGE MISDRILLED A MWEAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31500ME 45711 SHEAR TIE AT STATION 786 RIGHT HAND BETWEEN LONGERONS 9 AND 13 HAS MISDRILLED HOLES. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE. 2L72 4F A6WE 20010116011682001011601168WP 2001 1 16 MWEA010021 120010108A533059114003 SKIN DOUG DC9 DC914 3022034WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 DENT IN EXTERNAL SKIN AT LEFT SIDE STATION 76, JUST FORWARD OF EXTERNAL POWER RECEPTACLE. FABRICATED AND DRILLED DOUBLER. 2L72 4F A6WE 20010116011702001011601170WP 2001 1 16 0100061152 120010104A5244 DOOR DOUG DC10 DC1040 3023508WP ACCESSORY BAY UNSECURE A NWAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL01152US 46761 AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMBOUT OF MCO. FLIGHT RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ACCESSORY DOOR UNSECURED. ACCESSORY DOOR WARNING SWITCH INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN WIRE AND SECURED ACCESSORY DOOR. OPERATIONAL CHECK GOOD. 2L73 4F A22WE 20010116011802001011601180NM 2001 1 16 UPS01534601 120010110A5230 HANDLE BOEING757 75724APF 1384969NM CARGO DOOR OUT OF ADJ A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01465UP 28269 INSPECTION TYPE:N/A, AIR TURNBACK DUE TO: EICAS MSG FWD CARGO DOOR DISPLAYED AND CARGO DOORS OPEN LIGHT ILLUM AFTER TAKEOFF. ADJUSTED FWD DOOR HANDLE FLUSHNESS PER M/M 52-34-22. OPS NORMAL. 2L72 4F RTA2NM 20010116012062001011601206NM 2001 1 16 QXEA0100014 120010109A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A QXEAO OTHER L NO TEST NRNOT REPORTED 1 NM09822PH9872 525 106 PDX - FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED OVERHEAD EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010116012422001011601242EU 2001 1 16 0100033269 120010105A2910NAS161212 PACKING AIRBUS320 A320212 EU HYD MANIFOLD LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01369NW 1011 DURING CLIMB, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING O-RING ON PTU QUICK DISCONNECT COUPLING. LEAK CHECK OK. 2L72 4F RTA28NM 20010116012442001011601244NM 2001 1 16 0100056729 120010102A26122156646 FIRE DETECTOR BOEING747 747251F 1384898NM MAIN CARGO BAY FALSE INDICATIONA NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01629US5138 1038 22388 DURING CRUISE, THE MAIN DECK FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO YWG AND LANDED WITHOUT INCIDENT. REPLACED THE MAIN DECK 1B FIRE DETECTOR AND TEST SWITCH. OPERATIONAL CHECK GOOD. 2L74 4F A20WE 20010116012622001011601262EU 2001 1 16 0100113208 120010110A5311 FRAME AIRBUS320 A320211 3930320EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-181432. 2L72 4F RTA28NM 20010116012802001011601280NM 2001 1 16 CALA0100009 120010109A5315 FLOORBEAM BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917316 23367 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 10. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV A. 2L72 4F RTA16WE 20010116012812001011601281NM 2001 1 16 CALA0100010 120010109A5210 INTERCOSTAL BOEING737 7373T0 1384582NM PAX DOOR GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917316 23367 INSPECTION FOUND L-1 DOOR INTERCOSTAL GOUGED BELOW UPPER SPIGOT BUSHING. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-2. 2L72 4F RTA16WE 20010116012822001011601282NM 2001 1 16 CALA0100011 120010110A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917316 23367 INSPECTION FOUND A GOUGE IN INTERIOR SKIN AT CENTER BAY FOR L-1 TORQUE TUBE AT STA 303, STRINGER 11L. A NEW SECTION OF SKIN PANEL WAS INSTALLED IAW SRM 51-10-02. 2L72 4F RTA16WE 20010116012832001011601283NM 2001 1 16 CALA0100013 120010111A5315 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914381 26310 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 344, LBL 25. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. 2L72 4F RTA16WE 20010116012862001011601286NM 2001 1 16 QXEA0100015 120010110A6123 CONTROLLER DHAV DHC8 DHC8102 2809003NM AUTOFEATHER SYS WILL NOT TEST A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09825PH 213 LWS - AUTOFEATHER WILL NOT TEST. CYCLED POWER LEVERS AND CONDITION LEVERS FULL TRAVEL NUMEROUS TIMES. TEST NORMAL. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010116012872001011601287NM 2001 1 16 QXEA0100016 120010111A6123 CONTROLLER DHAV DHC8 DHC8202 2809007NM FEATHER SYSTEM MALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM09828PH 526 IDA - NR 2 PROP WILL NOT COME OUT OF FEATHER. GROUND RUN, COULD NOT DUPLICATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010116013522001011601352WP 2001 1 16 MWEA010016 120010108A532099115451 FLOOR SUPPORT DOUG DC9 DC914 3022034WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 FRAME STATION 256 CENTERLINE FLOOR SUPPORT HAS .30 DIAMETER HOLE THRU UPPER LEG OF FLOORBEAM. FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS. 2L72 4F A6WE 20010116014722001011601472EA 2001 1 16 SWIA972256 120010107A2731 TRIM SWITCH CNDAIRCL600 CL6002B19 EA HORIZONTAL STAB MALFUNCTIONED A SWIAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 NM07416SW 7089 INFLIGHT THE STAB TRIM AND MACH TRIM DISCONNECTED AND WOULD RESET ONLY AFTER THE F/O TRIM DISCONNECT WAS CYCLED 4 OR 5 TIMES. POWER DOWN AIRCRAFT. OPERATIONAL CHECK OF HSTCU. OPS CHECKS GOOD IAW MM 27-41-01. RAN HORIZONTAL STABILIZER IAW MM 27-40-00 STAB TRIM AND MACH TRIM OPS CHECKS GOOD. UNABLE TO DUPLICATE DISCREPANCY. 2L72 4F RTA21EA 20010116014732001011601473SO 2001 1 16 SWIA972258 120010108A2752 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07162CA 120150 CONTROL FAULT ON FLAP DURING RETRACTION ON GROUND. PRESS RESET AS PER QRH, FAULT CLEARED BUT REOCCURS WHEN RESELECTING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT NACELLE ACTUATOR AS PER RII 27-307. OPS CHECK. P/N ON 308200-1007, S/N ON 0195, S/N OFF 0402. 2L72 4T4 TRTA31SO E20NE 20010116014762001011601476SO 2001 1 16 SWIA972261 120010109A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA PW118 PW118B NE TE FLAPS CONTAMINATED A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07188SW 120039 FLAP DISAGREEMENT ON SELECTION OF FLAP 45 DEGREES (OUTBOARD FLAPS WOULD NOT EXTEND BEYOND LAST LIGHT BAR ON FLAP ANNUNCIATOR PANEL). FOUND GLYCOL IN LEFT OUTBOARD CANNON PLUG. CLEANED PLUG. OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20010116014792001011601479WP 2001 1 16 MWEA010007 120010105A531359164411 LONGERON DOUG DC9 DC914 3022034WP FUSELAGE DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 STATION 279 HAS HOLE IN LONGERON 29 LEFT JUST ABOVE FORWARD ANNTENA. FABRICATED AND INSTALLED NEW LONGERON. 2L72 4F A6WE 20010116015072001011601507SO 2001 1 16 SWIA972246 120010104A2930 WARNING LIGHT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE HYD SYSTEM ILLUMINATED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07284YV 120284 AFTER TAKEOFF GREEN SYSTEM HYDRAULIC FILTER LIGHT AND HYDRAULIC MAP LIGHT ILLUMINATED AFTER GEAR RETRACTION. RETURNED TO LAX. REMOVED GREEN SYSTEM ENGINE PUMP RETURN FILTER AND INSPECTED NO PARTICLES NOTED. INSTALLED NEW FILTER AND RESET BYPASS INDICATOR PIN. RUN UP FOR OPS AND LEAK CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 20010119000072001011900007NM 2001 1 19 2001UALA00003 120010102A3350 TRANSFORMER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE CABIN INOPERATIVE A UALAO OTHER L NO TEST UKUNKNOWN 1 WP29207UA 30213 TWO ADJACENT EEL LIGHTS INOP ON SEAT 2E. REPLACED EEL TRANSFORMER AND LIGHTS CHECK GOOD. 2L72 4F4 FRTT0001SE E46NE 20010119000092001011900009NM 2001 1 19 TWAA0100801 120010111A335085 LAMP BOEING757 7572Q8 1384972NM COCKPIT INOPERATIVE A TWAAK NONE O OTHER ININSP/MAINT 1 CE05702TW 28162 THE EGRESS SYSTEM SWITCH LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-17-99 LAX. 2L72 4F RTA2NM 20010119000112001011900011NM 2001 1 19 SPAA0100041 120010109A33501000679 LIGHT BOEING737 7372T4 1384492NM L-2 DOOR INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP28703S 22529 DURING ACCOMPLISHMENT OF PRE-FLIGHT CHECK FOUND EMERGENCY EXIT LIGHT AT L-2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B737 MM 33-51-101. OPERATIONAL CHECK GOOD. 2L72 4F A16WE 20010119000122001011900012NM 2001 1 19 AWXA0001242 120010111A5312672036 WEB BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW42277 23747 CRACKED LIGHTENING HOLE ON VERT SUPPORT WEB AT WL 195 RBL 17 FS 180. CUT OUT DAMAGE; HFEC SHOWS NO CRACKS; FABED REPAIR DOUBLER AND INSTALLED IAW SRM 51-70-13; HFEC COMPLIED WITH B737 NTM PT 6 51-00-00 FIG 23. 2L72 4F RTA16WE 20010119000142001011900014NM 2001 1 19 AWXA0001240 120010111A5312651758351 STRUCTURE BOEING737 7373Y0 1384671NM PREESURE BLKHD CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW 23747 STA 178 WL 190 FWD PRESSURE BULKHEAD AFT SIDE CRACK 1.25 INCH VERT CORD LEFT O/B SIDE. REMOVED DAMAGED; FABED AND INSTALLED ANGLE AND FILLERS IAW SRM 51-40-02, 53-10-08 FIG 205. 2L72 4F RTA16WE 20010119000162001011900016NM 2001 1 19 AWXA0001239 120010111A533065C33930 SKIN BOEING737 7373Y0 1384671NM GRND A/C RECPT. GOUGED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW 23747 LWR FUSELAGE SKIN DOUBLER GOUGED AND TORN AT GROUND A/C RECEPTACLE. REMOVED EXISTING DOUBLER IAW SRM 51-40-02; INSTALLED CONICAL WASHERS IAW 51-40-08; FABED REPAIR DOUBLER; TREATED AND PRIMED DOUBLER AND SKIN IAW 51-20-01; INSTALLED DOUBLER IAW 51-40-02. 2L72 4F RTA16WE 20010119000172001011900017NM 2001 1 19 AWXA0001238 120010111A531369353506 TIE CLIP BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW 23747 STRINGER TIE CLIP CRACKED FS 500A STR 16R. REMOVED CRACKED TIE CLIP IAW SRM 51-40-02; FABED STRINGER TIE CLIP IAW DWG 69-35350; TREATED AND PRIMED IAW 51-20-01; INSTALLED IAW DWG 69-35350. 2L72 4F RTA16WE 20010111007052001011100705NM 2001 1 11 AWXA0001227 120010104A3397BMS13131122 WIRE BOEING737 7373B7 1384580NM ROW 18 BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28328AW 23377 AFT SECTION OF EMERGENCY TRACK LIGHTING SYSTEM DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT ROW 18; REPAIRED WIRE; EMERGENCY LIGHT OPS CHECK NORMAL. 2L72 4F RTA16WE 20010111058662001011105866NM 2001 1 11 MWEA010029 120010102A53209951888121 BRACKET DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 BULKHEAD LOWER SUPPORT BRACKET AT APPROXIMATELY LONGERON 28 LEFT CRACKED. -- REMOVED AND REPLACED SUPPORT BRACKET 2L72 4F RTA6WE 20010111058672001011105867NM 2001 1 11 MWEA010030 120010102A5312995188889 BULKHEAD DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 BULKHEAD TEE AT FLOOR LEVEL BETWEEN LONGERON 28 LEFT AND 28 RIGHT HAS CRACK AT APPROXIMATELY LONGERON 29 LEFT. -- REMOVED AND REPLACED TEE. 2L72 4F RTA6WE 20010111058692001011105869NM 2001 1 11 MWEA010032 120010102A5312995188835 STRUT DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 BULKHEAD VERTICLE STRUT AT LONGERON 29 LEFT CRACKED APPROXIMATELY 6 INCHES ABOVE FLOOR. -- INSTALLED DOUBLE ANGLE IAW DC9/MD80 STRUCTURAL REPAIR MANUAL. 2L72 4F RTA6WE 20010111058702001011105870NM 2001 1 11 MWEA010033 120010102A53209951888169 ANGLE DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 BULKHEAD LOWER FLOOR SUPPORT ANGLE BETWEEN LONGERONS 28 LEFT AND 28 RIGHT CRACKED AT APPROXIMATELY LONGERON 29 LEFT. -- REMOVED AND REPLACED SUPPORT ANGLE. 2L72 4F RTA6WE 20010111039342001011103934WP 2001 1 11 ERKR200100038 120010105A53119957686503 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF DISCREPANT HOLE DAMAGE TO THE INNER CHORDS OF STATION 639 & 617 FRAMES, L6R, L6L,L9R & L9L. CONSISTS OF PLUGGING, OR TRIMMING OUT, DISCREPANT AND EXTRANEOUS HOLES AND INSTALLING REPAIR BUSHINGS, REINFORCEMENT STRAPS AND ANGLES. PER ECRA 933-53-073-2. 2L72 4F A6WE 20010111039362001011103936WP 2001 1 11 ERKR200100040 120010107A5730 ACCESS DOOR DOUG DC9 DC933F 302207AWP WING CORRODED B ERKRO OTHER O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF CORROSION DAMAGE TO CENTER TANK LT S ACCESS DOOR LANDING. CONSISTS OF BLENDING OUT THE DAMAGE. PER ECRA 933-53-081-2. 2L72 4F A6WE 20010111043752001011104375WP 2001 1 11 ERKR200100042 120010107A5321592240125 FLOOR PANEL DOUG DC9 DC933F 302207AWP CABIN CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 ADDRESSES THE REPAIR OF CRACKED FLOOR PANEL LOCATED BETWEEN STATION 503-775, X=37-45 LEFT HAND SIDE.CONSISTS OF TRIMMING OUT THE DAMAGE FLOOR PLANK AND INSTALLING A SPLICE DOUBLER AND ANGLE.PER ECRA 933-53-091-2 REV.A. 2L72 4F A6WE 20010111043762001011104376WP 2001 1 11 ERKR200100043 120010107A533059114004 SKIN DOUG DC9 DC933F 302207AWP MGL WW IMPROPER PART B ERKRK NONE W INADEQUATE Q C ININSP/MAINT 1 WP07933F 47191 REPAIR OF THE R/H 5911400-4 SKIN PANEL ABOVE NOSE WHEEL WELL FS 68 TO 79 RT PER OBSOLETE DOUGLAS DC-9 SRM 53-04, FIGURE 14,SHEET 2 WITH THE FOLLOWING DEVIATION: CLAD 2024-T3 WILL BE USED IN LIEU OF CLAD 2014-T6 FOR ALL REPAIR PARTS. PER ECRA 933-53-093-2 REV. A. 2L72 4F A6WE 20010111043782001011104378WP 2001 1 11 ERKR200100045 120010107A531259203371 FRAME DOUG DC9 DC933F 302207AWP FUSELAGE MISDRILLED B ERKRK NONE W INADEQUATE Q C ININSP/MAINT 1 WP07933F 47191 REPAIR OF MISS-DRILLED HOLE AND DRILL START DAMAGE TO INNER CHORD AND WEB, OF STATION 598 FRAME SECTIONS, AT L18L, L11R & L6R. CONSISTS OF PLUGGING DISCREPANT HOLES AND BLENDING OUT DRILL STARTS. PER ECRA 933-53-094-2. 2L72 4F A6WE 20010111044852001011104485WP 2001 1 11 ERKR200100048 120010107A5320 INTERCOSTAL DOUG DC9 DC933F 302207AWP FUSELAGE CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF CRACKED INTERCOSTAL LOCATED AT L12R BETWEEN STATION 149 & 160. CONSISTS OF INSTALLING A NESTED REINFORCEMENT ANGLE. PER ECRA 933-53-099-2. 2L72 4F A6WE 20010111051932001011105193EA 2001 1 11 JBXA000234 120010106A32307179015 CONTROL PANEL CNDAIRCL600 CL6002B19 EA MLG FAILED A JBXAA UNSCHED LANDING JO WARNING INDICATION OTHER CLCLIMB 1 SO05572ML 7224 DISCREPANCY: UPON GEAR LEVER SELECTION UP, HAD THE FOLLOWING MESSAGES PARKING BRAKE SOV, ANTI SKID INBD, AND GEAR DISAGREE. ALL OCCURRED WITH GEAR REMAINING DOWN AND LOCKED. CORRECTIVE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL PANEL I-A-W AMM 32-30-00 OPS CHECK GOOD. 2L72 4F RTA21EA 20010111045822001011104582WP 2001 1 11 ERKR200100052 120010108A5315995821223 FLOORBEAM DOUG DC9 DC933F 302207AWP FUSELAGE ELONGATED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF ELONGATED HOLE DAMAGE TO STATION 756 FLOORBEAM UPPER CAP FROM LBL 40 OUTBD. CONSISTS OF TRIMMING OFF, REMOVING AND REPLACING THE DAMAGED OUTBD MOST END OF THE FLOORBEAM UPPER CAP AND INSTALLING A SPLICE ( AT LBL 40 ) TO JOIN THE EXISTING AND REPLACEMENT SECTIONS. PER ECRA 933-53-104-2. 2L72 4F A6WE 20010111045832001011104583WP 2001 1 11 ERKR200100053 120010108A5330 SKIN DOUG DC9 DC933F 302207AWP FUSELAGE CORRODED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF 2 INSTANCES OF CORROSION DAMAGE TO SKIN BETWEEN L28R AND L30R AT STATIONS 427 AND 370. CONSISTS OF TRIMMING OUT THE DAMAGE AND INSTALLING AN INTERNAL AND EXTERNAL DOUBLER.PER ECRA 933-53-105-2. 2L72 4F A6WE 20010111045842001011104584WP 2001 1 11 ERKR200100054 120010108A531599234361 FLOORBEAM DOUG DC9 DC933F 302207AWP FUSELAGE ELONGATED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF ELONGATED HOLE DAMAGE TO FLOOR BEAM / FRAME SPLICE FITTINGS AT STATION 718 CONSISTS OF DRILLING OUT THE DAMAGE AND INSTALLING REPAIR BUSHINGS. PER ECRA 933-53-106-2. 2L72 4F A6WE 20010122000012001012200001NM 2001 1 22 SWAA010024 120010101A53126516300 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD WEB CRACKS AT RBL 4.7, WL 213.25 - WL 213.75 & RBL 6.7, WL 213.25 - 213.75. REPAIRED BULKHEAD PER SRM. 2L72 4F RTA16WE 20010122000332001012200033NM 2001 1 22 DL72L010009 120010102A3350900542 BATTERY BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27501DA 21303 ON LAYOVER FOUND OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP. CABIN AT FWD GALLEY IN AISLE. L1021 FWD LOWERED CEILING SIGN. FOUND ALL 6 VOLT 328 LAMPS BAD. RELAMPED, NO HELP. FOUND M1085 BATTERY CHARGER MODULE BAD. REPLACED M1085 MODULE AND BATTERY PACK. LIGHT NOW OPS NORMAL. 2L73 4F A3WE 20010122000342001012200034NM 2001 1 22 DL72S010015 120010104A5755 FITTING BOEING727 727232 1384082NM NR 4 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27538DA 22076 FOUND ON F1 LETTER CK, NR 4 SPOILER ACTUATOR I/B MOUNT FITTING IS CRACKED. REPAIRED PER MM 57-42-000-8. 2L73 4F A3WE 20010122000352001012200035NM 2001 1 22 DL757010020 120010105A3350P4010021 BATTERY BOEING757 757232 1384965NM 2L DOOR DISCHARGED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO276707A 30395 EMERGENCY FLASHLIGHT AT 2L INOP. REPLACED BATTERY AND BULB CHECKS OK. 2L72 4F RTA2NM 20010122000362001012200036WP 2001 1 22 DLL14010026 120010106A3340 POWER SUPPLY 672320101 LKHEED1011 1011385115 5265015WP R1 DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27740DA 60848 193C1244 R1 EXTERIOR DOOR LIGHT DID NOT ILLUMINATE. REPLACED R1 POWER SUPPLY. 2L73 4F A23WE 20010122000372001012200037NM 2001 1 22 DL767010034 120010106A5330143T3211 SKIN BOEING767 767232 1385132NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27104DA 22216 THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR WHICH WAS INSTALLED BETWEEN FS 500 & 521 AND BETWEEN STRINGERS 33L & 39L. THE UPPER PORTION OF THE REPAIR WAS REMOVED AND THE ADDITIONAL SKIN DAMAGE REMOVED WITH AN ADDITIONAL CUTOUT. A NEW ALUMINUM SKIN DOUBLER WAS INSTALLED AND INCORPORATED INTO THE EXISTING REPAIR PER ER/A 379697-14, REV B. 2L72 4F RTA1NM 20010122000442001012200044NM 2001 1 22 AWXA0001232 120010111A5320672038502 INTERCOSTAL BOEING737 7373Y0 1384671NM FUSELAGE CRACKED A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW 23747 STA 178 FWD PRESSURE BULKHEAD AFT SIDE CRACK 1.5 INCH LONG INTERCOSTAL RT SIDE WL 195. REMOVED AND REPLACED INTERCOSTAL RT SIDE IAW SRM 51-40-02. 2L72 4F RTA16WE 20010122000452001012200045NM 2001 1 22 AWXA0001231 120010111A533065457683 SKIN BOEING737 7373Y0 1384671NM FUSELAGE LIGHTNING STRIKEA AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW42277 23747 LIGHTNING DISCHARGE MARK, FUSELAGE RT SIDE JUST ABOVE FWD CARGO DOOR BETWEEN FS 460 AND FS 480. REMOVED DAMAGED AREA PER SRM 53-00-01; NDT CONDUCTED HFEC INSP PER B737 NDTM PT 6, 51-00-00 FIG 23. NO CRACKS NOTED AROUND CUTOUT; FABED FILLER AND DOUBLER AND INSTALLED REPAIR PER 53-00-01 FIG 202. 2L72 4F RTA16WE 20010122000462001012200046NM 2001 1 22 AWXA0001233 120010111A5320693535214 TIE CLIP BOEING737 7373Y0 1384671NM AFT CARGO BAY BENT A AWXAK NONE O OTHER UKUNKNOWN 1 WP28331AW 23747 AFT CARGO COMPT STA 727C STR 24L FRAME CLIP BENT. REMOVED AND REPLACED FRAME CLIP IAW SRM 51-40-02. 2L72 4F RTA16WE 20010122000472001012200047NM 2001 1 22 AWXA0001230 120010111A2730MS2764837 BEARING BOEING BOEING737 737277 1384570NM ELEV.TORQUE TUBEWORN A AWXAK NONE F FLT CONT AFFECTED LDLANDING 1 WP28185AW 22652 ON LANDING FLARE IN SFO THE ELEVATOR CONTROL WAS STIFF. PERFORMED OPERATIONAL AND VISUAL INSPECTION OF ELEV CONTROL SYSTEM, NO DEFECTS NOTED. DUE TO PRIOR REPORT OF STIFF ELEV; BOEING WAS CONSULTED; PER THEIR RECOMMENDATION THE ELEV TORQUE TUBE BEARINGS WERE LUBRICATED AND THE AIRCRAFT MAINTENANCE FERRIED TO PHX FOR FURTHER TROUBLESHOOTING AND BEARING REPLACEMENT. IN PHX FURTHER TROUBLESHOOTING WAS PERFORMED AND THE ELEV ACT INPUT TORQUE TUBE BEARINGS WERE REPLACED; ONE BEARING WAS DRY AND WHEN ROTATED WAS ROUGH. AFTER REPLACEMENT A VERIFICATION FLIGHT WAS PERFORMED AND THE ELEV OPERATION WAS NORMAL. 2L72 4F RTA16WE 20010122000522001012200052NM 2001 1 22 DL738010008 120010102A213171211997101AC CONTROLLER BOEING737 737832 13844CFNM E/E BAY INOPERATIVE A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27376DA 29624 ON TAKEOFF FROM CVG A/C DID NOT PRESSURIZE IN AUTO. NOT ABLE TO PRESSURIZE A/C WITH ALTERNATE MODE. FOUND NR 1 DCPC FAIL. T/S PER FIM 21-31 TASK 823-824 AND FIM21-31 TASK 825. REPLACED NR 1 DCPC, CKS GOOD PER FIM 21-31 TASK 825, PRESSURIZED A/C, SYSTEM NORMAL. 2L72 4F RTA16WE 20010122000532001012200053NM 2001 1 22 DL72S010010 120010102A5754 ANGLE BOEING727 727232 1384082NM NR8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 FOUND ON MV2 CHECK, .75 INCH CRACK NR 8 SLAT COVE SKIN ANGLE BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-000-8. 2L73 4F A3WE 20010122000542001012200054WP 2001 1 22 DLL14010011 120010102A3350 POWER SUPPLY 5165744 LKHEED1011 1011385115 5265015WP L3 DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO271739D UNK 193C1237 L-3 DOOR EXT EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, CHECKS GOOD. 2L73 4F A23WE 20010122000552001012200055NM 2001 1 22 DL73K010012 120010102A5330654580026 SKIN BOEING737 737232 1384475NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27313DL 23085 A 1 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE LOWER AFT CORNER OF THE L1 DOOR. THE DAMAGE WAS REPAIRED PER BACO DWG 65C27257 AND BACO S/B 737-53-1083. THE DAMAGE WAS FOUND AT HMV. 2L72 4F RTA16WE 20010131002192001013100219 2001 1 31 USAABB01001 420010104A3460 FMC BOEING767 767201 1385125NM EE BAY FAILED A USAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA19646US 23898 CLT - FLT 192 - FLIGHT RETURNED TO CLT DUE TO DUAL FMC FAILURE. (M) 2L72 4F RTA1NM 20010131002202001013100220WP 2001 1 31 USAAD01001 120010102A3350MISC0639 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19967VJ 47375 IND - THE RIGHT NACELLE EMERGENCY LIGHT AND THE SERVICE DOOR EVACUATION SLIDE ACTIVATED EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE RIGHT NACELLE AND SERVICE DOOR EMERGENCY LIGHTS. (M) 2L72 4F A6WE 20010131002222001013100222WP 2001 1 31 USAAD01002 120010104A3350MISC0639 BATTERY PACK DOUG DC9 DC931 3022065WP CARGO BAY DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19991VJ 47310 IND - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PROGRAMMED THE RIGHT NACELLE EMERGENCY LIGHT BATTERY FOR REPLACEMENT DUE TO THE PART NOT IN STOCK. THE AIRCRAFT WAS RELEASED FOR FLIGHT UNDER MEL PROCEDURES. (M) 2L72 4F A6WE 20010131002372001013100237WP 2001 1 31 AALA016001 120010104A2170 COALESCER BAG DOUG DC9 DC983 3022083WP AC BAY DIRTY A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21879RA 53185 LAX - WHEN PACK CONTROL TEMP SELECTOR WAS MOVED TOWARD WARM, CABIN RAPIDLY FILLED WITH SMOKE. MAINTENANCE CHANGED COALESCER BAGS, ACCOMPLISHED PACK BURN OUT, NO SMELL OR SMOKE IN CABIN. SJC- AT GATE SMELLED BURNED DUSTY SMELL WITH ONLY RIGHT PACK RUNNING, SWITCHED TO LEFT PACK AND SLOWLY CABIN FILLED WITH SMOKE AND SAME BURNT SMELL. MAINTENANCE FOUND TEMP SWITCHES IN FULL HOT. RETURNED TO NORMAL OPERATING RANGE. CHANGED COALEESCER BAGS AND CHANGED THE 130 DEGREES TEMP SENSOR. PERFORMED OPS CHECK, NO LEAKS NOTED, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 20010201000952001020100095NE 2001 2 1 EIA2001001 220010101A7230809402 CASE BOEING747 747SR46 NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE WORN A EIAAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM09478EV 21033 AIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INITIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENANCE CHECK AND INSPECTION FOUND PRIMARY VIBRATION CAUSED BY NR 3 AND NR 4 ENGINE FAN CASE WEAR. REPLACED NR 3 AND NR 4 ENGINE FAN CASES. ALL CHECKS NORMAL ON ENGINE RUNS. REPLACED FROZEN RIGHT W/W WSIB TOP PULLEYS, RIGHT W/W AILERON CABLE AA TOP PULLEY AND LEFT W/W/ AA/AB PULLEYS (P/N''''S BACP30M3). REPAIRED AILERON PULLEY BRACKET PER ECRA 478-27-105-1 PART 1. AILERON RIG, OPERATIONAL CHECKS, AND RII INSPECTIONS ACCOMPLISHED. (M) 2L74 4F4 F A20WE E20EA 20010201000962001020100096NE 2001 2 1 20010131SG006 220010101A7230809788 CASE BOEING747 747SR46 NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE WORN A EIAAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM09478EV 21033 AIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INITIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENANCE CHECK AND INSPECTION FOUND PRIMARY VIBRATION CAUSED BY NR 3 AND NR 4 ENGINE FAN CASE WEAR. REPLACED NR 3 AND NR 4 ENGINE FAN CASES. ALL CHECKS NORMAL ON ENGINE RUNS. REPLACED FROZEN RIGHT W/W WSIB TOP PULLEYS, RIGHT W/W AILERON CABLE AA TOP PULLEY AND LEFT W/W/ AA/AB PULLEYS (P/N''S BACP30M3). REPAIRED AILERON PULLEY BRACKET PER ECRA 478-27-105-1 PART 1. AILERON RIG, OPERATIONAL CHECKS, AND RII INSPECTIONS ACCOMPLISHED. REF EIA2001001. (M) 2L74 4F4 F A20WE E20EA 20010906003202001090600320WP 2001 9 6 EIA2001003 120010104A3222 STRUT DOUG DC9 DC915F 3022037WP NLG LEAKING A EIAAO OTHER K FLUID LOSS TOTAKEOFF 1 NM09915F 47061 DURING HIGH SPEED PHASE OF TAKEOFF ROLL, LOUD BANGING NOISE HEARD FROM NOSEGEAR. AFTER TAKEOFF AIRCRAFT REMAINED IN GROUND MODE. INSPECTION AND SERVICED NOSE STRUT, NO DEFECTS/LEAKS NOTED. AT DEPARTURE, NLG SHOCK STRUT LEAKED FLUID AND DEFLATED. SERVICED NOSE STRUT PER ECRA 915-32-048-1 PART 1. (M) 2L72 4F A6WE 20010202001042001020200104EA 2001 2 2 COMA0160141 120010122A532060034017351 ANGLE CNDAIRCL600 CL6002B19 EA FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01915CA18100 7013 FWD J ANGLE AT FS 280.00 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED AND REPLACED FWD J ANGLE IAW WVAC EO 601R-53-2101. 2L72 4F RTA21EA 20010202001052001020200105SO 2001 2 2 C2XA01IA037 120010119A33507287580501 LIGHT EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2716954 145072 IAH - DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT TWO OF THE AISLE PATH EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTIONS OF LIGHT STRIP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20010202001062001020200106SO 2001 2 2 C2XA01IA038 120010122A3260852701 PROXIMITY SWITCH EMB 145 EMB145LR SO LT MLG OUT OF ADJ A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716951 145063 IAH - FLIGHT 3929, THE CREW REPORTED THAT ON CLIMB-OUT A LANDING GEAR AIR GROUND FAIL MESSAGE APPEARED ON THE EICAS. THE CREW VERIFIED NORMAL OPERATION OF THE GEAR AND CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20010202001072001020200107SO 2001 2 2 C2XA01IA039 120010120A32331959520006 ACTUATOR EMB 120 EMB120ER 3260203SO RT MLG OUT OF ADJ A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2715730 120187 IAH - FLIGHT 3490, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATOR TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE AFFECTED ACTUATOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTA31SO 20010202001102001020200110WP 2001 2 2 ABXA0100017 120010119A2740591096235 JACKSCREW DOUG DC9 DC941 302207NWP STABILIZER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX3421134211 47780 CORROSION WAS LOCATED ON THE STABILIZER JACKSCREW THREADS, RIGHT HAND SIDE. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSY AND ACME NUT IAW DC-9 MM 27-40-01. 2L72 4F A6WE 20010202001132001020200113WP 2001 2 2 ABXA0100020 120010119A57554925721502 FITTING DOUG DC9 DC941 302207NWP SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS FOUND CRACKED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 20010202001142001020200114WP 2001 2 2 ABXA0100021 120010119A53305912864 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23963AX 47780 FUSELAGE SKIN WAS CRACKED FORWARD OF STATION 1072, BELOW LONGERON 14R. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39613. 2L72 4F A6WE 20010202001172001020200117NM 2001 2 2 F3LA200100009 120010119A33506013211 CHARGER BOEING737 7372Y5 1384554NM ESCAPE SLIDE INOPERATIVE A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03921WA 23039 L-1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED L-1 DOOR SLIDE LIGHT ASSY, BATTERY AND CHARGER PER MM 33-51-71. 2L72 4U RTA16WE 20010202001182001020200118NM 2001 2 2 AWXA0001252 120010118A3230D3231007000100 GEARBOX AIRBUSA319 A319132 NM ZONE 123 OUT OF ADJ A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28801AW 889 DURING POST MAINTENANCE FLIGHT TEST THE LANDING GEAR WAS EXTENDED USING MANUAL EXTENSION AND THE NOSE GEAR FAILED TO EXTEND, LGCIU 1 & 2 FAULTS WERE PRESENT. THE GEAR WAS RESET AND GEAR WAS EXTENDED HYDRAULICALLY AND ALL GEAR EXTENDED NORMALLY. MAINTENANCE TROUBLESHOT PER THE TSM. THE NLG VENT VALVE WAS REPLACED WHICH DID NOT HELP. THE FREE FALL CABLE RIGGING WAS CHECKED, WHICH CHECKED GOOD. THE ALTERNATE EXTENSION REDUCTION GEARBOX WAS REMOVED AND FOUND BOTH SHEAR PINS SHEARED. THE SHEAR PINS WERE REPLACED AND THE GEARBOX REINSTALLED. AFTER INSTALLATION, FOUND THE GEARBOX STOP BOLTS OUT OF ADJUSTMENT. AFTER REPLACEMENT OF THE SHEAR PINS AND ADJUSTMENT OF THE STOP BOLTS. 2L72 4F RTA28NM 20010111045852001011104585WP 2001 1 11 ERKR200100055 120010108A5310592032339 STRUCTURE DOUG DC9 DC933F 302207AWP FUSELAGE GOUGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 ADDRESSES REPAIR OF EXISTING GOUGE IN THE WATER SERVICE DOOR CUTOUT LOCATED BETWEEN STATION 446-465, LONGERON 21-22, RIGHT HAND SIDE. PER ECRA 933-53-107-2 REV. A 2L72 4F A6WE 20010111039042001011103904NM 2001 1 11 ERKR200100032 120010105A531165B01843 FRAME BOEING747 747132 1384882NM FUSELAGE CRACKED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07479EV 19898 CRACKED INNER CHORD AT STA 1265. REPAIRED PER ECRA 479-53-146-2. THIS REPAIR IS A TIME LIMITED, IT PROVIDES AMOC FOR SB 747-53A2416 AND IS VALID FOR A PERIOD OF NOT MORE THAN 1000 FLIGHT CYCLES BEYOND 01-05-01. 2L74 4F A20WE 20010111027822001011102782NM 2001 1 11 SCNA01003 120010103A2910 CHECK VALVE BOEING727 7272J4 1384006NM HYD SYSTEM FAILED A SCNAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL15288SC 20765 DURING TAKEOFF FROM MKE THE AIRCRAFT FILLED WITH SMOKE IN BOTH THE CABIN AND COCKPIT. THE FLIGHT CREW ABORTED THE TAKEOFF. THE AIRCRAFT WAS FERRIED TO MSP, THE ODOR RETURNED BUT NO SMOKE. THE NUMBER ONE ENGINE 13TH STAGE HYDRAULIC RESERVOIR CHECK VALVE WAS FOUND TO HAVE FAILED. REMOVED AND REPLACED BOTH NR 1 AND NR 2 CHECK VALVES AND BOTH COALESOR BAGS. RAN ALL THREE ENGINES AT DIFFERENT POWER SETTINGS SEVERAL TIMES, NO FURTHER FAULT FOUND. 2L73 4F RTA3WE 20010111019572001011101957EA 2001 1 11 COMA0160043 120010104A532060154103077 SPLICE CNDAIRCL600 CL6002B19 EA FUSELAGE MISMANUFACTURED A COMAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO01914CA 7012 TWO SPLICE PLATES 601R31030-77 WERE FABRICATED INCORRECTLY BY MANUFACTURER. FABRICATED DOUBLER PLATE, REWORKED SPLICE PLATES AND INSTALLED I/A/W W.V.A.C. E.O. 601R-53-2076. 2L72 4F RTA21EA 20010111019562001011101956NE 2001 1 11 COMA0160042 220010102A7240NAS6303U9 BOLT CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE EXHAUST NOZZLE MISSING A COMAO OTHER K FLUID LOSS ININSP/MAINT 1 SO01 807539 WE WERE REMOVING THE QEC KIT FROM ENGINE 807539 THAT WAS INSTALLED ON A PORTABLE ENGINE STAND. WHEN IT CAME TIME TO REMOVE THE EXHAUST NOZZLE P/N 228-55030-11J WE FOUND 7 BOLTS (OUT OF 30) MISSING. FOUR OF THE BOLTS (P/N NAS6303U4 AND NAS 6303U9) WERE LOCATED NEXT TO EACH OTHER WITH TWO OF THEM IN THE 6 O'CLOCK DELTA BRACKET WHICH HOLDS THE EXHAUST FAIRING.THE OTHER 3 BOLTS WERE MISSING AT THE 7 AN 11 O'CLOCK POSITION.NO ACTION TAKEN. THE EXHAUST HARDWARE REMAINING WAS DISCARDED AS IS STANDARD PRACTICE ON OUR QEC CHANGES. 2L72 4F4 FRTA21EA E15NE 20010111046072001011104607WP 2001 1 11 ERKR200100062 120010108A575359202168 FITTING DOUG DC9 DC933F 302207AWP FLAP CARRIAGE DAMAGED B ERKRK NONE O OTHER ININSP/MAINT 1 WP07933F 47191 REPAIR OF RIGHT HAND SIDE WING INBD FLAP CARRIAGE FITTING WEAR MARKS. CONSISTS OF BLENDING OUT THE WEAR MARKS.PER ECRA 933-57-103-2. 2L72 4F A6WE 20010207001662001020700166NM 2001 2 7 UPS01634590 120010107A5720 ATTACH FITTING BOEING767 76734AF 1385212NM LT WING TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01302UP 27240 INSPECTION TYPE:PFLT LEFT WING, LEFT O/B FLAP, PANEL (WING) ABOVE O/B FITTING HAS AN 18 INCH CRACK THRU AND 24 INCH CRACK THRU THE PANEL. (SEE ITEM 1, PG 534960) MARKED THE UPPER SURFACE. REMOVED PANEL AND ACCOMPLISHED INTERIM REPAIR IAW B767-5750-13691A INSPECT EA W/E CK AND PERMANENT REPAIR AT NEXT C-CK. 2L72 4F RTA1NM 20010111045372001011104537NM 2001 1 11 UPS01634591 120010107A5730 PANEL BOEING767 76734AF 1385212NM LT WING CRACKED A IPXAO OTHER O OTHER NRNOT REPORTED 1 SO01302UP 27240 INSPECTION TYPE:PFLT LT O/B WING PANEL CRACKED 18 INCH AND 24 INCH AT FLAP TRACK. ***MRR FILED AS OPEN*** 2L72 4F RTA1NM 20010116011862001011601186 2001 1 16 UPS01834592 420010106A2565 SLIDE DOUG DC8 DC871F 302199DWP PAX DOOR LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 INSPECTION TYPE:N/A, ESCAPE SLIDE LOOSE. *S/D* RESECURED ESCAPE SLIDE AS NEEDED PER MM 25-60. 2L74 4F RT4A25 20010222001472001022200147WP 2001 2 22 UPS01834599 120010104A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 INSPECTION TYPE:DURING PREFLIGHT, CRACKS MIGRATING FROM RIVET AT STATION 1480 ON LEFT SIDE OF FUSELAGE . APPX 6 IN. FWD OF OVERPRESS SAFETY VALVE. CRACK LENGTH IS .750 IN. THE UPPER DIRECTION & .500 IN. THE LOWER DIRECTION. REMOVED DAMAGED SKIN AT STA 1480, FABRCATED, DRILLED & FINISHED REPAIR. DFRL D206716 CLEARED ON LP 462587. 2L74 4F RT4A25 20010111051712001011105171WP 2001 1 11 IXXA0000045 120010105A3260 CONNECTOR DOUG DC8 DC871F 302199DWP WHEEL WELL LOOSE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11826BX82733621 45998 ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR LOCATION A LOOSE CANNON PLUG ON THE LEFT MAIN GEAR DOOR SWITCH. MAINTENANCE SECURED THE CANNON PLUG AND PERFORMED PERFORMED AN OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20010111051782001011105178WP 2001 1 11 IXXA0100001 120010105A3230 CONNECTOR DOUG DC8 DC871F 302199DWP WHEEL WELL LOOSE A IXXAO OTHER J WARNING INDICATION CLCLIMB 1 SW11826BX82733621 45998 !ENROUTE FROM RDU TO TOL, THE GEAR DOOR WARNING LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR LOCATION A LOOSE CANNON PLUG ON THE LEFT MAIN GEAR DOOR SWITCH. MAINTENANCE SECURED THE CANNON PLUG AND PERFORMED PERFORMED AN OPERATIONAL CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F RT4A25 20010111019742001011101974EA 2001 1 11 COMA0160048 120010102A27507455001 CONTROL UNIT CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01409CA492 7441 FLAPS FAIL MESSAGE. REPLACED THE FLAP SELECTOR ASSY. 2L72 4F RTA21EA 20010111019752001011101975 2001 1 11 COMA0160049 420010102A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01420CA 7451 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111045532001011104553WP 2001 1 11 TWAA0100501 120010105A215020495054 ACM DOUG DC9 DC982 3022082WP AC BAY CONTAMINATED A TWAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05911TW 49182 FUMES WERE REPORTED IN THE CABIN. OIL WAS FOUND IN THE LT ACM DUCTS. REPLACED THE ACM, CHANGED WATER SEPERATERS, AND ACCOMPLISHED PACK BURN OUT. CHECK-C 8-20-00 STL. 2L72 4F A6WE 20010111002742001011100274NM 2001 1 11 TWAA0100502 120010107A2497 WIRE BOEING757 757231 1384950NM RELAY PANEL DAMAGED A TWAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE05719TW 28487 DURING TROUBLESHOOTING RT ENGINE PROBE HEAT MALFUNCTION, ATTEMPT WAS MADE TO REPLACE RELAY K10479. AS RELAY PANEL OPENED SPARKS CAME FROM WIRE BUNDLE. REMOVED POWER FROM THE AIRCRAFT AND FOUND WIRE 6092-20 WAS BURNED THRU, REFERENCE WIRING DIAGRAM MANUAL 30-24-12. SPLICED IN A NEW PIECE OF WIRE. TAPED AND SECURED WIRE BUNDLE. CHECK-C 12-19-00 LAX. 2L72 4F RTA2NM 20010111045542001011104554NM 2001 1 11 TWAA0100503 120010106A33500202175007 LIGHT BOEING767 7673Q8 NM CABIN INOPERATIVE A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05635TW 28207 THE EGRESS LIGHTS WERE INOPERATIVE ON THE LEFT SIDE OF THE CABIN FROM ROW 30 AFT, AND EMERGENCY LIGHTS WERE INOPERATIVE ON THE AFT FUSELAGE AND THE RT SIDE NR 4 SLIDE LIGHT. CORRECTED EGRESS LIGHTS BY SECURING CONTACTS AT ROWS 41 LEFT AND 42 LEFT, AND REPLACED THE LIGHT ASSEMBLY, PN 0202175-007, AT THE AFT FUSELAGE AND R4 DOOR SLIDE LIGHT. CHECK-C 4-7-98. 2L72 4F RTA1NM 20010111019762001011101976EA 2001 1 11 COMA0160050 120010102A2611PU90421R3 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA LAVATORY FALSE INDICATIONA COMAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SO01812CA 7381 SMOKE TOILET CAUTION MESSAGE, F/A REPORTS SMOKE AND ELECTRIC SMELL IN CABIN.COULD NOT DUPLICATE. REPLACED LAV SMOKE DETECTOR. 2L72 4F RTA21EA 20010111020312001011102031 2001 1 11 COMA0160052 420010102A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01739CA 7273 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020322001011102032EA 2001 1 11 COMA0160053 120010103A2752853D10012 ACTUATOR CNDAIRCL600 CL6002B19 EA TE FLAPS JAMMED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936CA2329 7043 FLAPS FAILED WHEN SELECTED TO 45 DEGREES. REPLACED THE RT NR 3 FLAP ACTUATOR. 2L72 4F RTA21EA 20010111020372001011102037 2001 1 11 COMA0160058 420010104A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01962CA 7123 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020392001011102039EA 2001 1 11 COMA0160060 120010103A2150601R951213 FITTING CNDAIRCL600 CL6002B19 EA ACM CLOGGED A COMAA UNSCHED LANDING OS OTHER AFFECT SYSTEMS CLCLIMB 1 SO01416CA 7450 WHEN AIR CONDITIONING BLEED AIR TRANSFERRED FROM APU TO ENGINES, REVERBERATIONS COULD BE HEARD AND FELT IN CABIN. UNCLOGGED WATER SEPERATOR DRAIN LINES. 2L72 4F RTA21EA 20010111020402001011102040 2001 1 11 COMA0160061 420010103A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01975CA 7150 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020632001011102063EA 2001 1 11 COMA0160063 120010104A2750855D1009 BPSU CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01936CA6495 7043 FLAPS FAILED AT 41 DEGREES. REPLACED THE RT BPSU. 2L72 4F RTA21EA 20010111020342001011102034 2001 1 11 COMA0160055 420010102A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01420CA 7451 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111014352001011101435EU 2001 1 11 QXEA0100003 120010104A33505515800106 SIGN FOKKERF28 F28MK4000 4990810EU COCKPIT MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09484US 11234 SEA- FORWARD EXIT LIGHT OVER COCKPIT DOOR IS DIM. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 20010111014372001011101437EU 2001 1 11 QXEA0100005 120010102A33505515900004 CIRCUIT BOARD FOKKERF28 F28MK4000 4990810EU COCKPIT MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09490US 11152 SEA- EXIT SIGN OVER COCKPIT DOOR IS DIM. REPLACED EXIT LIGHT CIRCUIT BOARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETRUNED TO SERVICE. 2L72 4F RTA20EU 20010111041772001011104177NM 2001 1 11 F3LA200100004 120010105A2612 FIRE DETECTOR BOEING737 7372L9 1384497NM APU MALFUNCTIONED A F3LAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM03271FL 22734 FLIGHT CREW REPORTED APU FIRE WARNING ILLUMINATED IN FLIGHT FROM PHX TO DEN. THE APU FIRE BOTTLE WAS DISCHARGED AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT WAS DIVERTED TO ABQ AND LANDED WITHOUT INCIDENT.AN INSPECTION REVEALED NO SIGNS OF OVERHEATING OR FIRE. PLACARDED APU FIRE DETECTION SYSTEM PER MEL 26-8.1. SUPPLEMENTAL INFORMATION TO FOLLOW WHEN REPAIR IS ACCOMPLISHED. 2L72 4F RTA16WE 20010111031282001011103128EA 2001 1 11 SWIA972254 120010106A2760 PCU CNDAIRCL600 CL6002B19 EA SPOILER FAILED A SWIAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 NM07408SW 7055 SPOILERONS FAULT MESSAGE CAME ON INFLIGHT. REMOVED AND REPLACED LEFT INBOARD PCU ON LEFT SPOILERON IAW MM 27-26-01. OPS CHECK LEAK CHECK GOOD AT THIS TIME. PN ON 2700-7 SN ON MAL0581 SN OFF MAL0474 2L72 4F RTA21EA 20010111031312001011103131SO 2001 1 11 SWIA972255 120010106A27523203001007 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE T/E FLAP FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07162CA 120150 AFTER SELECTING FLAPS 45 DEGREES DISAGREEMENT ILLUMINATED OUTBOARD PAIRS WERE AFFECTED WITH 4 LIGHT PAIRS NOT ILLUMINATED. DID NOT FIX ITSELF. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE ACTUATOR. PN ON 320300-1007 SN ON 0780 SN OFF 0954 2L72 4T4 TRTA31SO E20NE 20010202001192001020200119NM 2001 2 2 AWXA0001253 120010112A3350900542 BATTERY PACK BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28182AW 22649 DURING SCHEDULED INSPECTION FOUND EMERGENCY LIGHTS OUT IN THE FIRST CLASS CABIN. REPLACED POWER SUPPLY FOR THE FIRST CLASS CABIN EMERGENCY LIGHTS. OPS CHECK OK. 2L72 4F RTA16WE 20010202001222001020200122NM 2001 2 2 EIA20001004 120010104A2510 SMOKE BOEING747 747273C 1384896NM COCKPIT CONSOLE DETECTED A EIAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09470EV 20653 AT FL340, EXPERIENCED SMOKE IN THE COCKPIT COMING FROM AFT END OF CENTER CONSOLE. ACCOMPLISHED FIRE/SMOKE PROCEDURES AND RETURNED TO HNL. (M) 2L74 4F A20WE 20010202001322001020200132NM 2001 2 2 GAIA01009OP 120010111A3242211473 BRAKE BOEING727 7272J0 138407ENM RT MLG FIRE A GAIAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SW07281KH 21105 FLT 718 - TOL-ELP - AFTER LANDING AND COMING TO REST AT THE PARKING SPOT AT ELP, THE RIGHT GEAR BRAKES CAUGHT FIRE. GROUND CREWS IMMEDIATELY EXTINGUISHED THE BRAKES FIRES. NR 1 BRAKE OVERTEMPED BUT DID NOT CATCH ON FIRE. APPROXIMATELY 20 MINUTES LATER, NR 1, NR 3, AND NR 4 TIRES THERMAL PROTECTION PLUGS BLEW. NO OTHER DIFFICULTIES OCCURRED. AFTER A SIGNIFICANT COOL DOWN PERIOD, THE TIRES AND BRAKES WERE REMOVED AND ASSOCIATED GEAR COMPONENTS WERE INSPECTED PER CONSIDERATION IN GMM CHAPTER 14, PAGE 4. NO OTHER DEFECTS WERE NOTED. REPLACED ALL WHEELS AND BRAKES. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F RTA3WE 20010202001332001020200133NM 2001 2 2 GAIA01088OP 120010110A3230656021132 ACCESSORY UNIT BOEING727 727251 138408HNM EE BAY MALFUNCTIONED A GAIAK NONE J WARNING INDICATION APAPPROACH 1 SW07279US 21158 FLT 708 - OKC-PHX - DURING APPROACH TO PHX, THE CREW NOTED ON GEAR EXTENSION THREE RED LIGHTS AND THREE GREEN LIGHTS ILLUMINATED. THE LANDING GEAR WAS RECYCLED AND ONLY THE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT CONTINUED ITS APPROACH AND LANDED SAFELY AT PHX WITHOUT ANY FURTHER DIFFICULTIES. REMOVED, REPLACED AND TESTED LANDING GEAR ACCESSORY UNT IAW BOEING MM. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20010202001352001020200135NM 2001 2 2 GAIA01002OP 120010104A3350 SOCKET BOEING727 727251 138408HNM L1 DOOR CORRODED A GAIAK NONE L NO TEST ININSP/MAINT 1 SW07279US 21158 DURING NON-ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. CLEANED CORROSION FROM LIGHT SOCKET PINS AND CLEANED SOCKET RECEPTACLE. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 20010202001692001020200169EU 2001 2 2 SIMA0033 120010103A3350BE1317 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21238AE 340B238 JFK - FLT 5198 - OVERHEAD EMERGENCY LIGHT AT SEAT 3C IS INOPERATIVE. PUT ON MEL AT THIS TIME. REMOVED AND REPLACED BULB AT SEAT 3C IAW AMM 33-50-00. OPS CHECK GOOD. RESTORED MEL. (M) 2L72 4T RTA52EU 20010202001712001020200171EU 2001 2 2 SIMA00310 120010103A335066363 LIGHT SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAK NONE L NO TEST UKUNKNOWN 1 SW21394AE 340B394 DFW - FLT 3415 - EMERGENCY EXIT FLOOR LIGHTING AT ROW 9A IS INOPERATIVE. MAINTENANCE REPLACED FLOOR LIGHTING STRIP AT ROW 9A. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 20010202001722001020200172EU 2001 2 2 SIMA0071 120010107A33206510732 BALLAST SAAB SF340 340B 7860101EU CABIN MALFUNCTIONED A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21358RZ 340B358 BOS - FLT 5122 - FLIGHT ATTENDANT NOTICED SMOKE IN CABIN SMELLS LIKE ELECTRIAL FIRE OR BURNING PLASTIC. REMOVED AND INSTALLED BALLAST OVER 9A IAW SAAB AMM CH 33-21-00. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. (M) 2L72 4T RTA52EU 20010202001732001020200173EU 2001 2 2 SIMA0073 120010107A2611 SMOKE WARNING SAAB SF340 340B 7860101EU AVIONICS ACTIVATED A SIMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW21340RC 340B340 BOS - FLT 4608 - AVIONICS SMOKE WARNING ILLUMINATED DURING TAXI IN BOS. RETURNED TO GATE AND EVACUATED AIRCRAFT. MEL 26-3 AML PAGE 1293877. (M) 2L72 4T RTA52EU 20010202001742001020200174EU 2001 2 2 SIMA0099 120010109A3350MS274061 SWITCH SAAB SF340 340B 7860101EU CABIN FAILED A SIMAK NONE L NO TEST TXTAXI/GRND HDL 1 SW21394AE 340B394 SGF - FLT 3617 - FLIGHT ATTENDANT ARMED LIGHT SWITCH INTERMITTENT, SGF MAINTENANCE WENT AOG FOR BULB NO FIX. FERRIED AIRCRAFT TO DFW. REMOVED AND REPLACED SWITCH IAW AMM. OPS CHECK GOOD. (M) 2L72 4T RTA52EU 20010202001762001020200176SO 2001 2 2 SIMA0091 120010109A2611FDS765A2 SMOKE DETECTOR EMB 135 EMB135ER 3260203SO LAVATORY MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SW21700LE 145156 ORD - FLT 4433 - CREW REPORTED THAT AFTER TAKEOFF LAV SMOKE WARNING CAME ON EICAS. CREW FOLLOWED AOM PROCEDURE AND RETURNED TO ORD. LAV SMOKE WARNING LIGHT WENT OUT DURING APPROACH, BUT NOTED NO BURNING SMELL IN LAV AREA. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK GOOD. (M) 2L72 4F RTT00011AT 20010205000012001020500001SO 2001 2 5 COMA0110017 120010112A531012027289501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01267CA21508 120259 THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2. 2L72 4T RTA31SO 20010205000022001020500002SO 2001 2 5 COMA0110018 120010112A531012027289501 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01267CA21508 120259 THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 1671-2. 2L72 4T RTA31SO 20010205000032001020500003SO 2001 2 5 COMA0110019 120010112A531112022616001 FRAME EMB 120 EMB120RT SO FUSELAGE NICKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01267CA21508 120259 THE AIRCRAFT''S FRAME 46A HAS A NICK IN THE UPPER FRAME FLANGE AT A PREVIOUSLY INSTALLED ANGLE. THE FRAME WAS REPAIRED BY REMOVING THE OLD ANGLE, DRESSING AND BLENDING THE NICK AND INSTALLING A SERVICEABLE ANGLE IN ACCORDANCE WITH AERODESIGN REPORT NR 2400-4. 2L72 4T RTA31SO 20010220002732001022000273NE 2001 2 20 01FDEA00042 220010124A7250 TURBINE DOUG MD11 MD11F 3023600NM GE CF6 CF680C2D1F 30025NE NR 1 ENGINE DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25616FE 48747 702349 ON T/O, NR 1 ENG HAD SEVERE VIBRATION AND EVM TURBINE INDICATIONS. NO REDUCTION WITH REDUCED POWER, SECURED NR 1 ENGINE AND RETURNED TO PEK. MX FOUND METAL IN TAILPIPE AND LAST STAGE TURBINE SEVERELY DAMAGED. *S/D* REMOVED AND REPLACED NR 1 ENG PER WORK CARD MD11 71T07 C1. COWLING OPEN AND CLOSE PERF PER MM 7-13-00. 2L73 4F4 FRTA22WE E31N3 20010111025282001011102528NM 2001 1 11 DHL2001741001 120010109A3222 STRUT BOEING727 7272Q9 138448MNM NLG UNDERSERVICED A DHLAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01741DH 21931 ON TAXI-OUT LOUD BANGING NOISE FROM NOSE WHEEL AREA ESPECIALLY WHEN TAXING OVER SMALL BUMPS. SERVICED NOSE STRUT WITH 5606 AND NITROGEN PER M/M CHPT 32 2L73 4F RTA3WE 20010111024922001011102492 2001 1 11 DHL2001717001 420010109A342025883024 GYRO BOEING727 72723 1384004NM COCKPIT UNSERVICEABLE A DHLAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01717DH 19389 CAPT HSI FAILED ON TAXI OUT. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO PER M/M 34-21-21,SYS OPS CHK GOOD 2L73 4F A3WE 20010111018832001011101883EU 2001 1 11 A6WA200000082 120010104A2150 A/C PACK BAG BAE146BAE146300A 1500267EU NR 2 ODOR A A6WAH DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL31616AW E3145 SMOKY SMELL IN CABIN AFTER TAKEOFF, CREW SHUT OFF APU AIR AND SWITCHED TO ENGINE AIR, OPERATED ON NR 2 PACK AND SMOKY SMELL DISSIPATED. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURE COULD NOT DUPLICATE SMELL, SYSTEM OPERATES NORMALLY ON ALL ENGINES AND APU AIR. 2H74 4F RTA49EU 20010111041612001011104161WP 2001 1 11 0100019935 120010105A5330 SKIN DOUG DC9 DC931 3022065WP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011332U 47404 A fuselage crack was found on the skin at the 1 left door aft of the #4 doorstop. Repaired per EA.96-167022. Reference Logpage 1312704. 2L72 4F A6WE 20010126001002001012600100NM 2001 1 26 01FDEA00011 120010108A5320 DOUBLER BOEING727 727233 138408ANM DOOR FRAME GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25273FE 22038 MAIN CARGO DOOR AFT FRAME BS 620 IS GOUGED AT PREVIOUS REPAIR. INGD RADIUS APPROX 21 INCHES UP FROM THE BOTTOM EDGE. *S/D* REMOVED, REPLACED AND FAB PER IAW FEDEX SRM 51-40-3. PREVIOUS REPAIR. INSTALL REPAIR DOUBLER PER IAW FEDEX SRM 51-30-2. 2L73 4F RTA3WE 20010111041622001011104162EU 2001 1 11 0100023212 120010105A5315 FLOORBEAM AIRBUS320 A320211 3930320EU FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01312US 152 DURING "L" CHECK FOUND CORROSION ON FLOORBEAMS IN AFT GALLEY AREA AT Y765 AND Y1162.5/Y1292. REPAIRED PER EA 32-181716. 2L72 4F RTA28NM 20010111058432001011105843WP 2001 1 11 MWEA010035 120010106A215020495055 ACM DOUG DC9 DC981 3022081WP AFT ACCESSORY LACK OF LUBE A MWEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31809ME 48071 CLEANERS REPORTED SMOKE IN CABIN. UPON MAINTENANCE ARRIVAL AT AIRCRAFT, SMOKE STILL FLOATING IN CABIN WITH BURNING SMELL. NOTED RIGHT AIRCONDITIONING PACK SWITCH LEFT IN HP BLEED OFF, APU AIR SWITCH ON AND APU RUNNING WITH CORSS FEEDS OPEN. AIRCRAFT MAIN BUSSES SWITHCED OFF WITH ONLY GROUND SERVICE ON. SUSPECT RIGHT AIRCONDITIONING PACK OVERHEAT/SHUTDOWN. -- MAINTENANCE INSPECTED RIGHT ACM TURBINE, OIL SERVICED. OPERATED RIGHT ACM SYSTEM FOR APPROXIMATELY 1 HOUR. PRESSURE AND TEMPS NORMAL. RIGHT A/C ACM SYSTEM OK FOR FURTHER SERVICE. SUSPECT RIGHT ACM OVERTEMPED AND SHUT DOWN PRIOR TO ANY DAMAGE. 2L72 4F A6WE 20010111046812001011104681WP 2001 1 11 UPS01834593 120010103A531337585931 LONGERON DOUG DC8 DC871F 302199DWP AFT CARGO CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01713UP 46014 INSPECTION TYPE:C2 STA.1350 LONG. 35R IS CRACKED REMOVED AND REPLACED LONGERON ST. 1270-1350 I.A.W. DWG. 3758593,AND SRM. 51-1-20D 2L74 4F RT4A25 20010111020662001011102066 2001 1 11 COMA0160066 420010105A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01946CA 7072 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020682001011102068EA 2001 1 11 COMA0160068 120010105A3010 WARNING LIGHT CNDAIRCL600 CL6002B19 EA WING DEICE ILLUMINATED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01739CA 7273 LEFT WING ANTI-ICE CAUTION DURING T/O. COULD NOT DUPLICATE. SYSTEM TEST SATISFACTORY. 2L72 4F RTA21EA 20010111017822001011101782 2001 1 11 COMA010069 420010105A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01868CA 7427 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111020702001011102070EA 2001 1 11 COMA0160070 120010101A5610601R3303310 WINDSHIELD CNDAIRCL600 CL6002B19 EA COCKPIT FAILED A COMAO OTHER O OTHER APAPPROACH 1 SO01430CA19 7461 COPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20010111020712001011102071EA 2001 1 11 COMA0160071 120010103A5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA COCKPIT FAILED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01943CA3999 7062 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 20010111020722001011102072EA 2001 1 11 COMA0160072 120010105A7830 WARNING LIGHT CNDAIRCL600 CL6002B19 EA THRUST REVERSER ILLUMINATED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01916CA 7014 RT THRUST REVERSER UNLOCK MESSAGE. SECURED T/R AND DEFERRED MAINTENANCE PER M.E.L. 2L72 4F RTA21EA 20010111020862001011102086EA 2001 1 11 COMA0160073 120010105A3260 WARNING LIGHT CNDAIRCL600 CL6002B19 EA NLG ILLUMINATED A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01962CA 7123 NLG DISAGREE MESSAGE. NO FAULT CODES IN PSEU, COULD NOT DUPLICATE, RETRACTION CHECKS WERE NORMAL. 2L72 4F RTA21EA 20010111020912001011102091 2001 1 11 COMA0160078 420010106A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01971CA 7145 STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010205000112001020500011NM 2001 2 5 2001UALA00008 120010105A2131 CONTROLLER BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN PRESSURE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP297458U 21912 UNABLE TO CONTROL CABIN PRESSURIZATION DURING CLIMB TO 31,000 FEET. AIRCRAFT DIVERTED TO ATL. *S/D* SUSPECTED PRESSURE CONTROLLER. REPLACED PRESSURE CONTROLLER. 2L73 4F4 F A3WE E2EA 20010205000122001020500012NM 2001 2 5 2001UALA00009 120010108A282291318506 CONTACTOR 3823002 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE FUEL BOOST FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP297460U 21914 ALL NR 2 FUEL BOOST PUMP TANK CIRCUIT BREAKERS POPPED DURING CRUISE. AIRCRAFT RETURNED TO DEN. *S/D* SPECIFIC CAUSE COULD NOT BE DETERMINED. REPLACED NR 2 RT AFT BOOST PUMP, AND NR 3 ESSENTIAL POWER CONTACTOR R110. 2L73 4F4 F A3WE E2EA 20010205000132001020500013NM 2001 2 5 2001UALA00010 120010108A3260189915 DOWNLOCK SENSOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT MLG FAILED A UALAO OTHER N FALSE WARNING LDLANDING 1 WP297289U 21567 AIRCRAFT EXPERIENCED AN AMBER ALERT LANDING DUE TO RIGHT GEAR RED LIGHT LOCK DOWN INDICATION. *S/D* FOUND RIGHT MAIN GEAR DOWNLOCK SENSOR BAD. REPLACED SENSOR. OPS CHECK OK. 2L73 4F4 F A3WE E2EA 20010205000202001020500020NM 2001 2 5 2001UALA00012 120010103A2822 PUMP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 FUEL BOOST FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP297453U 21907 DURING CRUISE, THE NR 1 TANK FUEL BOOST PUMP FAILED. AIRCRAFT DIVERTED TO DSM. *S/D* RAN NR 1 AFT FUEL BOOST PUMP TO RUN APU FOR APPROXIMATELY .5 HR, RAN NR 1 ENGINE FOR 20 MINUTES. BOOST PUMP OPERATED NORMALLY. 2L73 4F4 F A3WE E2EA 20010205000442001020500044NM 2001 2 5 UPS01234755 120010102A5312 PRESSURE PANEL BOEING727 72722C 138400FNM NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 INSPECTION TYPE:C CK, NOSE LANDING GEAR WHEEL WELL SIDEWALL RIGHT BS 290 TO LWR HAS CRACK INDICATION MIGRATING FROM PREVIOUS REPAIR ABOUT 1 INCH LONG. INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 51-40-2. 2L73 4F A3WE 20010205000482001020500048WP 2001 2 5 TWAA0101108 120010111A5347 GALLEY TRACK DOUG DC9 DC983 3022083WP CABIN CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT IN THE FWD CABIN, LIGHT CORROSION WAS ON GALLEY TIE DOWN ANGLE APPROX STA 210, RBL 10, AT NUT PLATE RIVETS. PART REMOVED AND REPLACED WITH NEW PART PER SPM 6-70-01. PAINTED WHITE PER SRM 51-10-03. INSTALLED NEW FASTENERS PER SRM 51-30-02. SEALED AREA PER SRM 51-20-0 PAGE 2. 2L72 4F RTA6WE 20010205000492001020500049EU 2001 2 5 MALA010128 120010121A27507DE CONNECTOR SAAB SF340 SF340A 7850100EU FLAP INDICATOR DAMAGED A MALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL1599XJ 099 IN FLIGHT NOTICED LT FLAP INDICATOR BETWEEN 7-15 DEGREE WITH FLAP HANDLE AT 0 DEGREES, RAN ORH AND DID NOT NOTICE YAW. ON APPROACH INTO DTW WHEN SELECTING FLAPS, FLAPS REMAINED AT 0 DEGREES. MAINTENANCE REPLACED CANNON PLUG 7-DE, AT FLAP IND TRASNIMTTER IAW SF 340MM, ALL CHECKS GOOD AT THIS TIME. 2L72 4T RTA52EU 20010205000512001020500051WP 2001 2 5 ARWA0010101 120010118A2910 HYDRAULIC LINE DOUG DC8 DC8F54 3021926WP NR 2 ENGINE LEAKING A ARWAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO1957FB 45669 DURING DESCENT AT THE INITIAL PHASE OF THE APPROACH LOSS HYDRAULIC FLUID AND PRESSURE. INITIATED PHASE I AND ABNORMAL IAW PROCEDURES. AFTER CLEARING THE ACTIVE DURING TAXI, LOSS HYDRAULIC BRAKE PRESSURE. AIR BRAKE PRESSURE APPLIED. FOUND PRESSURE LINE TO ENGINE NR 2 HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED PRESSURE LINE; SYSTEM CHECK NORMAL IAW 29-10-12. SERVICED AIR BRAKE BOTTLE AND BLED HYDRAULIC BRAKE SYSTEM IAW MM 32-18-0 AND 29-0. SYSTEM OPERATION NORMAL, NO LEAKS NOTED. 2L74 4F 4A25 20010205000622001020500062WP 2001 2 5 TWAA0101501 120010123A4990 APU DOUG DC9 DC983 3022083WP APU BAY CONTAMINATED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE059302B 49528 DURING SHORT FINAL CREW NOTICED SMELL OF SMOKE. AFTER LANDING SMELL WENT AWAY. AFTER EXTENSIVE CHECKS CAUSE NOT DETERMINED. DID CLEAN SOME OIL FROM APU INLET SO APU OIL MAY HAVE BEEN OVERSERVICED. CHECK-C 10-16-00 STL. 2L72 4F RTA6WE 20010205000642001020500064WP 2001 2 5 TWAA0101504 120010121A5313 STRINGER DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON STRINGER 23L, STA 1021 TO 1041, AFT CARGO COMPT. INSTALLED NEW SECTION OF STRINGER AND 2 SPLICES PER SRM 53-02, FIG 18 SHEET 4. 2L72 4F RTA6WE 20010205000662001020500066WP 2001 2 5 TWAA0101506 120010122A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 1174 TO 1212, RBL 58 INCHES. REMOVED CORROSION PER SRM 51-10-2. REPLACED MEMBRANE PER SRM 51-30-1, 51-30-02, AND 51-30-5. 2L72 4F RTA6WE 20010205000672001020500067WP 2001 2 5 TWAA0101507 120010125A5313 LONGERON DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05998R 47030 DURING CHECK-C MAINT LONGERON 3R AT STA 658 WAS CRACKED AT LOWER FLANGE .25 INCH LONG. REPAIRED PER SRM 53-02 AND DRAWING SRO 9530128. 2L72 4F A6WE 20010205000712001020500071NM 2001 2 5 QXEA0100032 120010114A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE GOUGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS MISSING MATERIAL AND GOUGED UPAT STATION X434.500. REPAIRED IAW DHC-8 RD8-53-1339. 2H72 4T RTA13NM 20010205000722001020500072NM 2001 2 5 QXEA0100033 120010112A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X300.400. REPAIRED IAW DHC-8 RD8-53-1339 AND HORIZON AIR EA 9-53-588. 2H72 4T RTA13NM 20010205000732001020500073NM 2001 2 5 QXEA0100034 120010110A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM FUSELAGE CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09824PH 157 PDX- RIGHT HAND INBOARD SEAT TRACK HAS PITTING ON TOP SIDE AT STATION X264.100. REPAIRED IAW DHC-8 RD8-53-1339. 2H72 4T RTA13NM 20010111020922001011102092EA 2001 1 11 COMA0160079 120010107A3230601R751461 VALVE CNDAIRCL600 CL6002B19 EA NLG MALFUNCTIONED A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01721CA5693 7259 LANDING GEAR DISAGREE MESSAGE, NLG NOT DOWN AND LOCK.REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 20010111020692001011102069 2001 1 11 COMA0160069 420010105A3418 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING MALFUNCTIONED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01868CA 7427 STALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER. 2L72 4F RTA21EA 20010111003472001011100347NM 2001 1 11 CALA0100004 120010106A3397 WIRE BOEING737 7373T0 1384582NM CABIN DAMAGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914325 23455 INSPECTION FOUND ROW 14-21 SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE UNDER SEAT 19B. THE WIRE WAS REPAIRED IAW MM 20-10-13 AND OPERATION CHECKED GOOD. 2L72 4F RTA16WE 20010111008902001011100890NM 2001 1 11 CALA0100005 120010107A3350D71702001 POWER SUPPLY BOEING737 737824 13844BZNM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0937255 30610 THE FIRST SIX ROWS OF COACH PATH EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING TEST. THE EMERGENCY LIGHT POWER SUPPLY AT BS 500C WAS REMOVED AND REPLACED. OPERATION CHECKED GOOD IAW MM 33-51-06. 2L72 4F RTA16WE 20010111008912001011100891NM 2001 1 11 CALA0100006 120010107A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917316 23367 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 312, S20R. THE DENTED AREA OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-51, FIGURE 202. 2L72 4F RTA16WE 20010111008922001011100892NM 2001 1 11 CALA0100007 120010108A3230 FUSE BOEING737 737724 NM NLG INOPERATIVE A CALAO OTHER O OTHER APAPPROACH 1 SW0915710 28780 THE NOSE GEAR FAILED TO EXTEND NORMALLY ON APPROACH TO CLE. ALTERNATE EXTENSION WAS USED TO EXTEND THE GEAR AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE NLG EXTENSION FUSE AT FAULT. THE NLG EXTENSION FUSE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. THE NLG WAS SWUNG SEVERAL TIMES AND ALL OPERATION WAS NORMAL IAW MM 32-33-71. 2L72 4F RTA16WE 20010111045592001011104559 2001 1 11 TWAA0100602 420010108A2565100504205 SLIDE DOUG DC9 DC982 3022082WP L1 DOOR UNSERVICEABLE A TWAAK NONE O OTHER ININSP/MAINT 1 CE05940AS 49825 ON PREFLIGHT THE LEFT SIDE FWD CABIN DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS READING ZERO. REPLACED THE SLIDE ASSEMBLY. CHECK-C 7-18-00 STL. 2L72 4F A6WE 20010111045702001011104570WP 2001 1 11 TWAA0100605 120010102A5320 WEB DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT CORROSION WAS FOUND ON LT FLOOR MEMBRANE AT STA 1174, AFT CARGO COMPT. FABRICATED AND INSTALLED DOUBLER . 2L72 4F RTA6WE 20010111045722001011104572WP 2001 1 11 TWAA0100607 120010105A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059420D 49824 DURING CHECK-C MAINT THE NR 1 SEAT TRACK, GALLEY TIE DOWN HOLE HAD CORROSION AT STA 1117. FABRICATED NEW CHAIR TRACK AND INSTALLED PER SPM 6-70-01 PAGE 1 PARA 4, FROM STA 1030 TO 1136. 2L72 4F RTA6WE 20010111024892001011102489NM 2001 1 11 DHL2001702001 120010106A3150 WARNING SYSTEM BOEING727 72730C 1384009NM COCKPIT ACTIVATED A DHLAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO01702DH 19793 RTO BECAUSE OF FALSE T/O WARNING HORN-RECYCLED FLAPS, WARNING DID NOT SOUND WHEN T/L ADVANCED. PREFORMED T/O WARNING TEST,FOUND NORMAL OPS PER M/M 34-00 AND 31-00 2L73 4F A3WE 20010111059792001011105979 2001 1 11 ANCF200100002 420010107A3414 INDICATOR BOEING767 767259 1385136NM PWA 4056 PW4056 NE AIRSPEED FAILED W ANCFC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW99985AN 24618 DURING TAKE OFF CAPTAIN AIRSPEED INDICATOR GOT STUCK AT 100 KNTS. TAKE OFF WAS ABORTED AT 116 KNTS. DEFERRED AIRSPEED INDICATOR INOPERATIVE PER MEL 34-13-1 ITEM 199 CAT C, ALSO CHECKED EFIS AIRSPEED INDICATOR ON CAPTAIN SIDE, IT WORKS NORMALLY. 2L72 4F4 FRTA1NM E24NE 20010111061382001011106138NM 2001 1 11 PCAA0101002 120010109A3350 BULB DHAV DHC8 DHC8102 2809003NM CABIN FAILED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13835EX 289 BGM FLIGHT 3555. ROW 1 RIGHT SIDE EMERGENCY LIGHT INOP ONE BULB. MAINTENANCE REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 20010111045772001011104577WP 2001 1 11 TWAA0100701 120010108A335058222 POWER SUPPLY DOUG DC9 DC983 3022083WP CABIN MALFUNCTIONED A TWAAK NONE O OTHER CRCRUISE 1 CE059303K 49529 THE EGRESS LIGHTS CAME ON IN FLIGHT FROM ROW 15 TO 25. REPLACED THE POWER SUPPLY. CHECK-C 12-24-2000. 2L72 4F RTA6WE 20010111045362001011104536NM 2001 1 11 UPS01234600 120010109A33501000679 LIGHT BOEING727 72731C 1384011NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01922UP 19231 INSPECTION TYPE:N/A ON SHUTDOWN, DISCOVERED COCKPIT EMER