N137AA

Part: ENGINE — STALLED (NR 1) · airframe 31,511 hrs · 12,465 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SMF DUE TO THE FLIGHT CREW REPORTING MULTIPLE BIRD STRIKES DURING CLIMB OUT ALONG WITH A #1 ENGINE STALL / SURGE AND THE ENGINE THEN CAME BACK. THE AIRCRAFT LANDED SAFELY AT SMF AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE ACCOMPLISHED A BORESCOPE INSPECTION ON THE HPC AND FOUND DAMAGE THAT EXCEEDED LIMITS REQUIRING THE ENGINE TO BE CHANGED. MAINTENANCE REPLACED THE #1 ENGINE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TASK CARD 26L40071004.

Part: ENGINE — STALLED (NR 1) · airframe 31,511 hrs · 12,465 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SMF DUE TO THE FLIGHT CREW REPORTING MULTIPLE BIRD STRIKES DURING CLIMB OUT ALONG WITH A #1 ENGINE STALL / SURGE AND THE ENGINE THEN CAME BACK. THE AIRCRAFT LANDED SAFELY AT SMF AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE ACCOMPLISHED A BORESCOPE INSPECTION ON THE HPC AND FOUND DAMAGE THAT EXCEEDED LIMITS REQUIRING THE ENGINE TO BE CHANGED.

Part: BATTERY — NO TEST (ZONE 200) · airframe 31,295 hrs · 12,378 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT 3L TEST LIGHT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 30,811 hrs · 12,176 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-22-00.

Part: BATTERY — NO TEST (ZONE 200) · airframe 29,188 hrs · 11,505 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202503213679) AND BATTERY (AALA202503216414) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 29,188 hrs · 11,505 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAULT MESSAGE DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202503213679) AND BATTERY (AALA202503216414) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 27,010 hrs · 10,566 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 12C AISLE EMERGENCY LIGHTING WIRING PULLED OUT OF PLUG/CONNECTOR. RECONNECTED WIRING TO SEAT 12C FOR EMERGENCY LIGHTING.

Part: LIGHT — INOPERATIVE (ROW 12ABC) · airframe 26,703 hrs · 10,440 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY ESCAPE PATH LIGHT IN ROW 12ABC INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHT IN ROW 12 ABC.

Part: DOOR LATCH — STICKING (COCKPIT) · airframe 26,376 hrs · 10,301 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR LATCH STICKS, DIFFICULT TO OPEN. MAINTENANCE LUBRICATED FLIGHT DECK DOOR LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 25,137 hrs · 9,762 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO A #2 ENGINE STALL ECAM MESSAGE DURING CLIMBOUT. FLIGHT CREW REDUCED #2 ENGINE POWER TO FLIGHT IDLE AND POWER WAS SLOWLY RESTORED. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT FOR AALA202312124534: MAINTENANCE REPLACED THE #2 ENGINE PER TASK CARD 26L40071004 AND 26L40071003. ** (CLOSED)

Part: ENGINE — STALLED (ZONE 400 - NAC/P) · airframe 25,137 hrs · 9,762 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO A #2 ENGINE STALL ECAM MESSAGE DURING CLIMBOUT. FLIGHT CREW REDUCED #2 ENGINE POWER TO FLIGHT IDLE AND POWER WAS SLOWLY RESTORED. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DOOR LATCH — INOPERATIVE (ZONE 900 - LAV/G) · airframe 24,266 hrs · 9,409 cycles

AIRCRAFT WAS NOT GROUNDED: UNABLE TO OPEN MID LAVATORY DOOR FROM INSIDE. MAINTENANCE REPLACED LAVATORY DOOR LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LATCH — LACK OF LUBE (ZONE 900 - LAV/G) · airframe 23,752 hrs · 9,196 cycles

AIRCRAFT WAS NOT GROUNDED: L2 LAVATORY DOOR LATCH DIFFICULT TO CLOSE/OPEN. LUBRICANTED L2 LAVATORY DOOR LATCH AS NEEDED.

Part: MASK — DEPLOYED (ZONE 200 - FUSE) · airframe 2,247 hrs · 8,655 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE O2 MASKS DEPLOYED ROW 33ABC,36ABC,11DEF. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPACKED O2 MASKS PER AMM 35-21-43-550-801-A AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF MANUAL MASK RELEASE PER AMM 35-23-00-710-001-A.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 22,471 hrs · 8,654 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAILED SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202302091092) AND BATTERY (AALA202302093470). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLKISHED PER AMM 33-51-00.

Part: BATTERY — NO TEST (ZONE 200 - FUSE) · airframe 22,471 hrs · 8,654 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAILED SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 10WL (AALA202302091092) AND BATTERY (AALA202302093470). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLKISHED PER AMM 33-51-00.

Part: STRUT — UNDERSERVICED (ZONE 700 - GEARS) · airframe 20,997 hrs · 8,052 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR WOULD NOT RETRACT ALONG WITH A SHOCK ABSORBER FAULT MESSAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAX WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE: NOTED THAT BOTH LANDING GEAR CONTROL INTERFACE UNITS SHOWED THE NOSE LANDING GEAR SHOCK ABSORBER FAULT AND FULLY SERVICED THE NOSE LANDING GEAR STRUT PER AMM 12-12-32. A SATISFACTORY RETRACTION CHECK OF THE NOSE LANDING GEAR WAS ACCOMPLISHED PER AMM 32-30-00 WITH NO FAULTS NOTED.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 20,781 hrs · 7,968 cycles

AIRCRAFT WAS NOT GROUNDED: 4R DOOR DAMPER PRESSURE TOO LOW, FOUND TO BE AT 1400 PSI AT 80 DEGREES F. SERVICED 4R DOOR DAMPER PER AMM 52-10-00.

Part: NONE — NONE (ZONE 100 - FUSE) · airframe 20,178 hrs · 7,722 cycles

AIRCRAFT WAS GROUNDED; "VENT AVNCS SYS FAULT" ECAM MESSAGE CAME ON. LEVELED OFF AT 10,000 FEET, DECLARED AN EMERGENCY AND RETURNED TO BOS LANDING SAFELY. REPLACED SKIN AIR OUTLET VALVE PER AMM 21-26-53, ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — INOPERATIVE (ZONE 100 - FUSE) · airframe 19,067 hrs · 7,246 cycles

AIRCRAFT WAS GROUNDED: SMOKE FORWARD CARGO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. FORWARD CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. FLIGHT DECLARED EMERGENCY AND DIVERTED TO ILM. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED ALL FORWARD CARGO SMOKE DETECTORS PER AMM 26-16-15. (AALA202112217589), (AALA202112220893), AND (AALA202112225455). REMOVE AND REPLACED FORWARD CARGO FIRE BOTTLE (AALA202112222667) PER AMM 26-23-41.

Part: SMOKE DETECTOR — INOPERATIVE (ZONE 100 - FUSE) · airframe 19,067 hrs · 7,246 cycles

AIRCRAFT WAS GROUNDED: SMOKE FORWARD CARGO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. FORWARD CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. FLIGHT DECLARED EMERGENCY AND DIVERTED TO ILM. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED ALL FORWARD CARGO SMOKE DETECTORS PER AMM 26-16-15. (AALA202112220893), (AALA202112225455), AND (AALA202112226604). REMOVE AND REPLACED FORWARD CARGO FIRE BOTTLE (AALA202112222667) PER AMM 26-23-41.

Part: SMOKE DETECTOR — INOPERATIVE (ZONE 100 - FUSE) · airframe 19,067 hrs · 7,246 cycles

AIRCRAFT WAS GROUNDED: SMOKE FORWARD CARGO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. FORWARD CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. FLIGHT DECLARED EMERGENCY AND DIVERTED TO ILM. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED ALL FORWARD CARGO SMOKE DETECTORS PER AMM 26-16-15. (AALA202112217589), (AALA202112220893), AND (AALA202112226604). REMOVE AND REPLACED FORWARD CARGO FIRE BOTTLE (AALA202112222667) PER AMM 26-23-41.

Part: SMOKE DETECTOR — INOPERATIVE (ZONE 100 - FUSE) · airframe 19,067 hrs · 7,246 cycles

AIRCRAFT WAS GROUNDED: SMOKE FORWARD CARGO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. FORWARD CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. FLIGHT DECLARED EMERGENCY AND DIVERTED TO ILM. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED ALL FORWARD CARGO SMOKE DETECTORS PER AMM 26-16-15. (AALA202112217589), (AALA202112225455), AND (AALA202112226604). REMOVE AND REPLACED FORWARD CARGO FIRE BOTTLE (AALA202112222667) PER AMM 26-23-41.

Part: FIRE BOTTLE — DISCHARGED (ZONE 100 - FUSE) · airframe 19,067 hrs · 7,246 cycles

AIRCRAFT WAS GROUNDED: SMOKE FORWARD CARGO ELECTRONIC CENTRALIZED AIRCRAFT MONITOR. FORWARD CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. FLIGHT DECLARED EMERGENCY AND DIVERTED TO ILM. AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. REMOVED AND REPLACED ALL FORWARD CARGO SMOKE DETECTORS PER AMM 26-16-15. (AALA202112217589), (AALA202112220893), (AALA202112225455), AND (AALA202112226604). REMOVE AND REPLACED FORWARD CARGO FIRE BOTTLE PER AMM 26-23-41.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 18,998 hrs · 7,221 cycles

AIRCRAFT WAS NOT GROUNDED: DURING CIDS TEST, EMERGENCY POWER SUPPLY UNIT 14WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 14WL PER AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 18,998 hrs · 7,221 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS TEST OF EMERGENCY POWER SUPPLY UNIT 11WL INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38.

Part: DOOR — MALFUNCTIONED (LAVATORY E) · airframe 17,801 hrs · 6,705 cycles

AIRCRAFT NOT GROUNDED: LAVATORY E DOOR DOES NOT CLOSE AUTOMATICALLY, JAMS IN CLOSED POSITION. (OPEN)

Part: HOOK — DISENGAGED (LAVATORY DOOR) · airframe 17,801 hrs · 6,705 cycles

AIRCRAFT NOT GROUNDED: LAVATORY E DOOR DOES NOT CLOSE AUTOMATICALLY, JAMS IN CLOSED POSITION. **SUPPLEMENTAL REPORT FOR AALA202107238381: MAINTENANCE FOUND THAT RESISTANCE HINGE WAS NOT ENGAGED TO HOOK. REMOVED AND RE-INSTALLED DOOR WITH RESISTANCE HINGE ENGAGED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-45-19. ** (CLOSED)

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,123 hrs · 6,436 cycles

AIRCRAFT IN BASE MAINTENANCE: FOUND EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 4 ELEVATOR LEFT AMM 55-16-42-400-001-A STEP4.B AND AMM 55-16-48-400-001-A STEP 4C

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 3 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 3 ELEVATOR LEFT PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 6 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 6 ELEVATOR LEFT PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 5 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 5 ELEVATOR LEFT PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 2 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 2 ELEVATOR LEFT PER AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (LT ELEVATOR) · airframe 17,123 hrs · 6,436 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 1 ELEVATOR ON LEFT HORIZONTAL STABILIZER. INSTALLED NEW HINGE ARM END FITTING 1 ELEVATOR LEFT IAW AMM 55-16-42-400-001-A.

Part: CYLINDER — NO TEST (PAX DOOR DAMPER) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNCTIONAL CHECK. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14-400-001-B .

Part: BOTTLE — FAILED (PAX DOOR DAMPER) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FAILED DAMPING FUNCTIONAL CHECK. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14-400-001-B .

Part: SHEAR PLATE — CORRODED (FRMS 69-70 S23R) · airframe 15,461 hrs · 5,811 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE LOCATED BETWEEN FR69 AND FR70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11-801 AND DRAWING D53474180.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SHEAR PLATE LOCATED BETWEEN STA FR 69 TO FR 70, STR 23L. L = 1.236 INCHES. REPLACED SHEAR PLATE AND FASTENERS LOCATED BETWEEN FR 69 AND FR 70 AT LEVEL OF STR 23L AT AFT GALLEY AREA PER SRM 51-42-11-801.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA LOWER SILL LOCATED AT S23R AND FR68. REPAIRED PER SRM 53-41-14-300-001.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,461 hrs · 5,811 cycles

AIRCRAFT IN BASE MAINTENANCE: L=1.086 INCH, W=0.530 INCH, D=0.025 INCH CORRODED AREA ON FLOOR BEAM -Y254 AT LEVEL OF FR16. PERFORMED PERMANENT REPAIR OF FLOOR BEAM -Y254 AT LEVEL OF FR16.

Part: SUPPORT — CORRODED (FRM 68 S23L) · corrosion level 2 · airframe 15,461 hrs · 5,811 cycles

AIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON LOWER SILL AT STR 23L FR 68 L=0.594 INCHES, W=0.392 INCHES, D=0.032 INCHES. PERFORMED PERMANENT REPAIR CATEGORY A, REINFORCEMENT (NESTED ANGLES), ON LOWER SILL AT LEVEL FR 68, STR 23L AFT GALLEY AREA PER SRM 53-41-14-300-001.

Part: FITTING — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 15,461 hrs · 5,811 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA CENTER FITTING LOCATED BETWEEN FR66 AND FR68 AT S23L. L=8.265 INCHES, W=0.675 INCHES, D=0.015 INCHES. REPLACED CENTER FITTING PER SRM 51-42-11-801, 51-72-11-911-001 AND DWG D53480505.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,220 hrs · 6,472 cycles

AIRCRAFT IN BASE MAINTENANCE: L=0.700 INCH, W=0.595 INCH, D=0.045 INCH CORRODED AREA ON FLOOR BEAM -Y254 AT LEVEL OF FR 20. PERFORMED PERMANENT REPAIR OF FLOOR BEAM -Y254 AND AT LEVEL OF FR 20.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 17,118 hrs · 6,434 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT WL14 FAULT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT POSITION WL14 PER AMM 33-51-38.

Part: SLIDE — FAULTED (R1 DOOR) · airframe 16,825 hrs · 6,324 cycles

AIRCRAFT WAS GROUNDED: BITE FAILED. R1 SLIDE FAULTING. REPLACED SLIDE PER JOB CARD 26L00025011.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 15,917 hrs · 5,982 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE REPLACING THE L2 DOOR EMERGENCY ESCAPE SLIDE FOR A SCHEDULED TIME CHANGE MAINTENANCE FOUND THE REPLACEMENT SLIDE TO BE DEFECTIVE AND UNSERVICEABLE. MAINTENANCE REINSTALLED THE ORIGINAL SLIDE PER AMM 25-62-47 AND TASK CARD 1604.

Part: SLIDE — NO TEST (EMERGENCY LIGHT) · airframe 14,781 hrs · 5,530 cycles

AIRCRAFT IN BASE VISIT: R1 DOOR SLIDE NEEDS REPLACED FOR EMERGENCY LIGHT TEST FAILURE. REMOVED AND REPLACED R1 DOOR SLIDE IAW J/C 26L00025011.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 14,781 hrs · 5,530 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR SLIDE NEEDED TO BE REPLACED. MAINTENANCE REPLACED SLIDE DOOR PER JOB CARD 26C00033004.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 14,484 hrs · 5,411 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 DOOR DAMPER PRESSURE LOW. SERVICED DOOR DAMPER TO PROPER PRESSURE PER STANDARD PRACTICES.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 14,396 hrs · 5,377 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 151RF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-42-14.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 13,937 hrs · 5,213 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS DURING CIDS TEST EPSU 14WL FAULT. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-58. OPS CHECK NORMAL.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 13,937 hrs · 5,213 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS DURING CIDS TEST EPSU 15WL FAULT. MAINTENANCE REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-58.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 13,937 hrs · 5,213 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS DURING CIDS TEST EPSU 10WL FAULT. REPLACED EPSU BATTERY 10WL IAW AMM 33-51-58, OPS CHECK NORMAL.

Part: FAN — FAILED (EXTRACTION) · airframe 13,503 hrs · 5,036 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER GATE ARRIVAL COULD FEEL VIBRATION IN FORWARD GALLEY FLOOR. STARTED GETTING SMOKE, TURNED BLOWER AND EXTRACT OFF, TURNED APU OFF AND VIBRATION STOPPED. MAINTENANCE REPLACED AVIONICS EXTRACTION FAN IAW AMM 21-26-51-400-001-A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 13,390 hrs · 4,988 cycles

AIRCRAFT IN BASE VISIT: R1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 13,390 hrs · 4,988 cycles

AIRCRAFT IN BASE VISIT: R2 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 13,013 hrs · 4,833 cycles

AIRCRAFT WAS NOT GROUNDED: R1 PASSENGER DOOR EMERGENCY ASSIST CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 12,830 hrs · 4,756 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER PRESSURE LOW. MAINTENANCE SERVICED DAMPER TO PROPER PRESSURE PER AMM 52-10-00.

Part: ASSIST ASSY — LOW PRESSURE (R1 DOOR) · airframe 12,626 hrs · 4,679 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSISTOR PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSISTOR PRESSURE TO PROPER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 12,528 hrs · 4,644 cycles

AIRCRAFT WAS NOT GROUNDED: 1R EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (SERVICE DOOR) · airframe 11,952 hrs · 4,426 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND FORWARD SERVICE DOOR ACCUMULATOR LOW ON PRESSURE. MAINTENANCE SERVICED DORR ACCUMULATOR PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 11,838 hrs · 4,385 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST ACTUATOR PRESSURE WAS LOW. MAINTENANCE SERVICED ACTUATOR PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — UNKNOWN (CABIN) · airframe 9,508 hrs · 3,510 cycles

DOOR AND CEILING EMERGENCY LIGHTS DID NOT ILLUMINATE DURING FLIGHT. ACCOMPLISHED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTS, TESTED OK , IAW MM 33-51-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 9,069 hrs · 3,353 cycles

EMERGENCY POWER SUPPLY 14WL FAILED ON A CIDS TEST. REPLACED EPSU IAW 33-51-00.

Part: HANDLE — DETACHED (L4 DOOR) · airframe 7,992 hrs · 2,962 cycles

L4 DOOR ASSIST HANDLE LOWER FRONT DETACHED. MAINTENANCE REPLACED THE ASSIST HANDLE IAW AMM 25-23-46 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 7,838 hrs · 2,905 cycles

ON GATE ARRIVAL, OPENED THE L1 DOOR AND SLIDE FELL OUT OF PACK. DOOR ASSIST BOTTLE DEPLOYED. SLIDE DID NOT DEPLOY. REPLACED THE SLIDE IAW AMM 25-62-44.

Part: BOTTLE — DISCHARGED (DOOR ASSIST) · airframe 7,838 hrs · 2,905 cycles

ON GATE ARRIVAL OPENED THE L1 DOOR AND SLIDE FELL OUT OF PACK. DOOR ASSIST BOTTLE DEPLOYED. SLIDE DID NOT DEPLOY. REPLACED L1 DOOR ASST BOTTLE PER AMM 52-11-14.

Part: UNKNOWN — MALFUNCTIONED (AUTOFLIGHT SYS) · airframe 7,774 hrs · 2,882 cycles

DURING APPROACH INTO BGI, AROUND 500 FEET, AIRCRAFT EXPERIENCED A NOSE DOWN PITCH AT THE SAME TIME THE AUTO THROTTLE BECAME UNRESPONSIVE. THE FLIGHT CREW INTERVENED AND DISCONNECTED THE AUTOPILOT AND AUTO THROTTLES TAKING MANUAL CONTROL. AIRCRAFT EXPERIENCED TAIL STRIKE. ACCOMPLISHED AFS OPERATIONAL TEST IAW AMM 22-96-00-710-001A AND EA 273523, NO FAULTS NOTED, ILS OPERATIONAL TEST IAW AMM 34-36-00-710-003-A AND EA 273523, NO FAULTS NOTED. MAINTENANCE REPLACED THE NR 1 FMGC IAW AMM 22-83-34. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 7,328 hrs · 2,712 cycles

AIRCRAFT WAS GROUNDED. DELAMINATION ON FORWARD CARGO FLOOR BOARD PANEL 131EF. REPLACED FORWARD CARGO FLOOR BOARD PANEL 131EF PER MM 52-22-14.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO BAY) · airframe 7,328 hrs · 2,712 cycles

DELAMINATION ON FORWARD CARGO FLOOR PANEL 131AF. REPLACED FWD CARGO FLOOR PANEL 131AF IAW AMM 53-22-14. AIRCRAFT WAS GROUNDED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 7,328 hrs · 2,712 cycles

AIRCRAFT WAS GROUNDED. DELAMINATION ON AFT CARGO FLOOR PANEL 151LF. REPLACED FLOOR PANEL 151LF PER MM 53-22-14.

Part: BATTERY — FAILED (CABIN) · airframe 5,599 hrs · 2,059 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT 12WL FAILED TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. OPERATIONAL CHECK GOOD.

Part: ANGLE — CORRODED (BS 859-899)

TUL - CORROSION ON LOWER FORWARD SUPPORT ANGLE. REPAIR COVERED ON ESO 7349 DATE 11-9-99. REMOVED CORROSION AND REPAIRED PER ESO 7349, S/N 47847, DATED 11-8-99. TST: 101,286.36 HOURS. CYCLES: 18,805. (X)

Part: BEAM — CORRODED (BS 1000)

TUL - CORROSION ON ANGLE BEAM ON AFT FORWARD CARGO DOOR FRAME. REPAIR COVERED BY ESO 7349. BLENDED OUT CORROSION PER SRM 51-21-01 VOL II. TST: 101,286.36 HOURS. CYCLES: 18,805. (X)

Part: LIGHT — INOPERATIVE (ROW 12H)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 12H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INLET — FOD (NR 3 PACK)

DFW - FLT T0005 - DURING CRUISE, FLIGHT ATTENDANTS IN AFT CABIN REPORTED SMOKE IN AFT GALLEY AREA. FLIGHT CREW TURNED OFF RECIRCULATION FANS AND SMOKE DISSIPATED. FLIGHT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DEBRIS IN NR 3 PACK INLET. MAINTENANCE CLEARED DEBRIS FROM NR 3 PACK INLET. GROUND RAN ALL THREE ENGINES AND PACKS WITH NO SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: LIGHT — BROKEN (ROW 4B)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT PASSENGER SEAT 4B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT PASSENGER SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACM — MALFUNCTIONED (NR 1 PACK)

DFW - FLT 5 - DURING LEVEL OFF FL310, FLIGHT ATTENDANT REPORTED SMOKE THROUGHOUT CABIN. FIRST OFFICER INVESTIGATED AND REPORTED IT SMELLED LIKE ELECTRICAL SMOKE. CREW ACCOMPLISHED CHECKLIST AND RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE. TROUBLE SHOOTING FOUND NR 1 PACK AS SOURCE OF ODOR. REPLACED NUMBER ONE AIR CYCLE MACHINE AND AS A PRECAUTIONARY, REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT WAS RETURNED TO SERVICE AFTER SUCCESSFUL FUNCTIONAL CHECK FLIGHT. (M)

Part: FRAME — CORRODED (CARGO DOORWAY)

TUL - CORROSION ON CENTER CARGO DOOR CUT-OUT FORWARD LOWER CORNER OF JAMB STA 1701, L43R. INSTALLED DOUBLER STRAP OVER BLENDED AREA PER ESO7349 DATED 6-10-98. TST: 96,680.24 HOURS. CYCLES: 18,100. (X)

Part: BRACKET — CORRODED (WS 736)

TUL - CORROSION IN 2 EACH BOLT HOLES AND ON FACE OF OUTBOARD FLAP, OUTBOARD HINGE BRACKET SIDE LOAD SUPPORT BOSS. RE-WORKED OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD SUPPORT BOSS BORES PER CMM 57-44-09 AND ESO'S 7327 AND 7349 DATED 6-10-98. TST: 96,680.24 HOURS. CYCLES: 18,100. (X)

Part: ANGLE — CORRODED (BS 1977)

TUL - FRAME ANGLE FORWARD SIDE HAS CORROSION STA 1977 FROM LONGERON 48L TO LONGEORN 52. REPAIRED PER ESO 7349, DATED 6-8-98. TST: 96,680.24 HOURS. CYCLES: 18,100. (X)

Part: FRAME — CORRODED (BS 1997)

TUL - FRAME ANGLE AFT SIDE OF FRAME 1997 HAS HEAVY CORROSION BETWEEN LONGER 47L AND 48R. SPLICED IN NEW SECTION OF 'J' ANGLE PER SRM 53-30-00 VOL 11. (M)

Part: SKIN — CORRODED (BS 1997-2005)

TUL - FUSELAGE BELLY SKIN HAS CORROSION 2 PLACES ON SIDES OF LONGERON 44L STATION 2000 TO 2005. REPAIRED AREA PER ESO 7349, DATED 05/28/98 AND SRM 51-21-01 VOL 2. (M)

Part: FRAME — CORRODED (BS 1841)

TUL - FRAME AT STATION 1841 BETWEEN LONGER 43L AND 42L HAS CORROSION. INSTALLED REPAIR AFTER CORROSION REMOVAL, PER SRM 53-30-00 PAGE 14. (M)

Part: SHEAR TIE — CORRODED (BS 1967)

TUL - SHEAR TIE IS ONE PIECE FROM 47L-47R EACH TIE TO SKIN HAS CORROSION. REMOVED AND REPLACED SHEAR TIE STRIP PER AARD 51-01-00-05. (M)

Part: TRUNNION — CORRODED (BS 1461)

TUL - FOUND CORROSION ON LEFT AND RT AFT TRUNNION BOLT SPOT FACE SURFACES, TOP SIDES. REMOVED CORROSION, CASTING BEYOND LIMITS. REPAIRED PER ESO 7349, DATE 6-5-98. (M)

Part: SPLICE — CORRODED (BS 1853)

TUL - FOUND LONGERON SPLICE FITTING CORRODED BETWEEN STATION 1853-1871 AT LONGERON 48L. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-00 PAGE 9. (M)

Part: SKIN — CORRODED (WS 433)

TUL - FOUND CORROSIN ON LOWER WING SKIN AROUND CASTNER AT REAR SPAR NEAR STATION XORS 433. REPAIRED PER ESO 7349, DATED 6-2-98. (M)

Part: TIE DOWN — CORRODED (BS 840-860)

TUL - FOUND CORROSION AT AFT GALLEY TIE DOWN LUGS. NEW SECTION INSTALLED PER ESO 7349, DATED 5/28/98. (M)

Part: FLOORBEAM — CORRODED (BS 840-860)

TUL - G5 GALLEY CENTER SUPPORT AND BEAM HAS SURFACE CORROSION. REMOVED CORROSION PER SRM 51-21-01, TREATED AND PRIMED PER SRM 51-21-01. (M)

Part: INTERCOSTAL — CORRODED (BS 1967)

TUL - INTERCOSTAL CORRODED BETWEEN LONGERON 47R TO LONGERON 48R AND BET STATION 1967 TO STATION 1977. REMOVED AND REPLACED INTERCOSTAL PER AARD 51-01-00-05. (M)

Part: ROLLER TRAY — CORRODED (BS 1666)

TUL - FOUND CORROSION IN ROLLER TRAY NR 1 AT ROLLER BRAKE LOCATION STATION 1666. REMOVED AND REPLACED NR 1 ROLLER TRAY FROM STATION 1621 TO STATION 1781 PER SRM 51-01-00-05. (M)

Part: SILL — CORRODED (BS 939)

TUL - FOUND CORROSION UNDER OMNI ROLLER SUPPORT CASTING AROUND BOLT HOLES ON DOOR SILL. PERFORMED REPAIR PER ESO DATED 6-1-98. SPOT FACED HOLES TO REMOVE CORROSION AND PLUGGED WITH SHIMS. (M)

Part: FRAME — CORRODED (BS 1741)

TUL - FOUND CORROSION ON FRAME 1741 FROM LONG 51L TO 51R. MANUFACTURED A REPAIR DOUBLER FOR FRAME J-CHANNEL PER AARD 51-01-00-05 AND INSTALLED ON FRAME 1741 LONG 51L TO 51R. (M)

Part: SUPPORT — CORRODED (BS 1887-1897)

TUL - CORROSION ON AFT END OF LAVATORY F SUPPORT. INSTALLED FABRICATED LUG PER SRM 53-60-01 AND DOUBLER PER SRM 53-60-01. TST: 96,680.24 HOURS. CYCLES: 18,100. (X)

Part: FLOOR SUPPORT — CORRODED (BS 1887)

TUL - FOUND CORROSION ON FLOORBOARD SUPPORT JUST AFT OF LAV F STATION 1887. INSTALLED FABRICATED REPAIR PER SRM 53-60-01 TO FLOORBOARD SUPPORT. (M)

Part: ANGLE — CORRODED (BS 2003-2007)

TUL - FOUND CORROSION ON T-ANGLE AT AFT END NR 4 GALLEY SUPPORT. REPAIRED T-ANGLE AT STATION 2007-2003 AND AFT NR 4 GALLEY SUPPORT PER ESO 7349 DATED 05-28-98. (M)

Part: SUPPORT — CORRODED (BS 1887-1897)

TUL - FLOORBOARD SUPPORT HAS CORROSION AT 1887-1897 APPROXIMATELY 40 INCHES RIGHT OF CENTERLINE. INSTALLED FABRICATED REPAIR PER SRM 53-60-01 AND DOUBLER PER SRM 53-60-01. TST: 96,680.24 HOURS. CYCLES: 18,100. (X)

Part: SUPPORT — CORRODED (BS 1853-1996)

TUL - GALLEY SUPPORT NR 3 HAS CORROSION AT 3 GALLEY MOUNTS. INSTALLED REPLACEMENT PART PER AARD 51-10-00-1, TREATED, PRIMED AND PAINTED. (M)

Part: FLOORBEAM — CORRODED (BS 808)

TUL - C-5 GALLEY RT FORWARD AND AFT SUPPORTS AND BEAM HAS HEAVY CORROSION. FABRICATED AND INSTALLED A SECTION OF A FLOORBOARD GALLEY SUPPORT PER AARD 51-01-00-05 PAGE 1. (M)

Part: SKIN — CORRODED (BS 1868)

TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER L48L STATION 1868 STRINGER 48L. INSTALLED EXTERNAL REPAIR DOUBLER PER ESO 7349, DATED 6/1/98. (M)

Part: LONGERON — CORRODED (BS 1977)

TUL - LONGERON 38L CORRODED AT STATION 1977. REPLACED SECTION OF LONGERON PER SRM 53-10-00. (M)

Part: DUCT CLAMP — LOOSE (NR 3 ENG)

DFW - FLT 123 - AT ROTATIO DURING T/O, FIRE WARN AND RT HYD TEMP HIGHT LIGHTS ILLUMINATED FOR NR 3 ENG. ACCOMPLISHED SHUTDOWN OF NR 3 ENG AND FIRE WARNING LIGHT EXTINGUISHED. A/C DUMPED FUEL AND RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED NR 3 ENG. ACCOMPLISHED LEAK AND GROUND CHECKS WITH NO DEFECTS FOUND. A LOOSE CLAMP ON A STARTER DUCT JOINT LED TO JOINT FAILURE RESULTING IN HIGH UNDER COWL TEMP AND A FIRE WARNING. SUBSEQUENT FAN CASE ABRADABLE SHROUD MATERIAL DISBONDING OCCURED DUE TO IMPINGING HOT AIR FROM THE FAILED STARTER DUCT JOINT. ENGINE PROCESSED THROUGH SHOP FOR RETURN TO SERVICE. (M)

Part: DOOR — MISSING (LT MLG)

HNL - FLT 73 - ON ARRIVAL HNL, DURING MAINTENANCE WALK AROUND FOUND LEFT MAIN LANDING GEAR DOOR OUTER DOOR PANEL MISSING. DEFERRED DUE TO NO PARTS AVAILABLE, INSPECTED AIRCRAFT FOR AIRWORTHINESS OF FLIGHT. NO OTHER DISCREPANCIES NOTED. AIRCRAFT RELEASE FOR MAINTENANCE FERRY FLIGHT TO TUL ACCOMPLISHED FERRY FLIGHT TO TUL. REPLACED MAIN LANDING GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DOOR — MISSING (LT MLG)

HNL - FLT 73 - AFTER GATE ARRIVAL DURING WALK AROUND, LT MAIN LANDING GEAR DOOR OUTER DOOR PANEL DISCOVERED MISSING WITH SLIGHT DAMAGE TO LEFT INBOARD FLAP ACCESS PANEL. ACCOMPLISHED TEMPORARY REPAIR TO FLAP ACCESS PANEL AND AIRCRAFT MAINTENANCE FERRY HNL/TUL. REPLACED LEFT MAIN LANDING GEAR DOOR OUTER DOOR PANEL. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ANGLE — CRACKED (BS 2007)

TUL - FOUND UPPER CAP ANGLE (TEE) CRACKED AT 2007 PRESS BULKHEAD AT ATTIC FLOOR LINE 18 INCHES INBOARD OF STRINGER 13 LEFT. REPAIRED PER ESO 7349. (M)

Part: ENGINE MOUNT — CORRODED (RT ENGINE)

TUL - BOLT HOLE HAS PITTS IN RIGHT PYLON FORWARD ENGINE MOUNT OUTBOARD BOLT HOLE. REWORKED BOLT HOLE PER ESO 7349 DATED 08-20-96. (M)

Part: SUPPORT — CORRODED (BS 401-422)

TUL - FOUND GALLEY NR 2 STRUCTURE SUPPORT HAS CORROSION AROUND MOUNTING HOLE AND AT END ATTACHMENT. REMOVED AND REPLACED SUPPORT STRUCTURE WITH NEWLY FABRICATED PART PER SRM 53-00-01 TREATED AND PAINTED AREA PER SRM 51-21-01. (M)

Part: SHEAR TIE — CORRODED (BS 1119)

TUL - FOUND SHEAR TIE HAS SURFACE CORROSION BETWEEN STRINGER 46L AND 47L AT FRAME 1119 FORWARD AND BACK SIDE. INSTALLED SHEAR CLIP SPLICE REPAIR PER SRM 53-30-00 PG 35 FIG 10. (M)

Part: SUPPORT — CORRODED (NR 2 GALLEY)

TUL - FOUND CORROSION IN GALLEY SUPPORT BEYOND LIMITS. REPLACED NR 2 GALLEY CENTER SUPPORT WITH NEW PART. (M)

Part: FLOOR SUPPORT — CORRODED (BS 422)

TUL - FOUND FLOOR SUPPORT AFT OF G2 BETWEEN INBOARD AND OUTBOARD GALLEY MOUNTS CORRODED AT BOTH ENDS. REMOVED AND FABRICATED NEW FLOOR SUPPORTS PER SRM 53-00-01, INSTALLED SAME AND TREATED AND PAINTED PER SRM 51-21-01. (M)

Part: STRUT — REQ'D SERV (NLG)

DFW - FLT NR 102 - DURING APPROACH TO DFW, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR EXPERIENCED LOUD CLUNK AND RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME RESULTS. CONFIRMED NOSE LANDING GEAR DOWN AND LOCKED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SEALS AND SERVICED NOSE STRUT WITH OIL AND NITROGEN. ALSO, REPLACED LANDING GEAR PROXIMITY SWITCH CONTROL UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (NLG)

HNL - FLT NR 0005 - AFTER TAKEOFF HNL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH SLIGHT VIBRATION NOTED. RECYCLED LANDING GEAR AND RED LIGHT AGAIN ILLUMINATED WITH NO VIBRATION. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO HNL, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SENSORS. ACCOMPLISHED BITE CHECK OF LANDING GEAR PROXIMITY SWITCH CONTROL UNIT AND ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)