N9008U
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 1969-11-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
71 reports on file, 1995-05-26 – 2026-07-08.
Part: ACTUATOR — FAULT MESSAGE (ZONE 100) · airframe 34,164 hrs · 16,671 cycles
AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A BURNING WIRE SMELL FOR LESS THAN FIVE SECONDS IN FLIGHT DECK AND FORWARD GALLEY WHEN AN AIR PACK NR 1 OVERHEAT AND AN AIR PACK NR 1 REGUL FAULT MESSAGES DISPLAYED. MAINTENANCE FOUND A FAULT MESSAGE IN SKYWISE FOR THE PACK 1 AIR INLET FLAP ACTUATOR AND REPLACED IT PER AMM 21-61-51. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES OR SMELLS NOTED.
Part: CYLINDER — LOW PRESSURE (ZONE 800) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: DOOR 1L DAMPER LOW PRESSURE. MAINTENANCE PERFORMED CHARGING OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER FE240-202OF THE PASSENGER CREW DOOR 831 IAW AMM 52-10-00-614-001-A.
Part: FLASHLIGHT — NOT SEATED (ZONE 200) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: FWD JUMP SEATS FLASH LIGHT TEST INOPERATIVE. MAINTENANCE INSTALLED CORRECTLY FWD JUMP SEATS FLASH LIGHT TEST IS OK IAW AMM 25-65-00-0001 STEP 5.B.
Part: CYLINDER — LOW PRESSURE (ZONE 800) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: DOOR 1R DAMPER LOW PRESSURE. PERFORMED CHARGING OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER P/N:FE240-206 OF THE PASSENGER CREW DOOR 841 IAW AMM 52-10-00-614-001-A.
Part: FITTING — CRACKED (ZONE 800) · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON INTERCOSTAL FITTING LOCATED AT LEVEL DOOR STOP N7 ON FR 16RH AT FWD GALLEY AREA. MEASURE IS D=0.087 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED AT LEVEL DOOR STOP #7 AT FR16 RH SIDE IAW A319 SRM 51-42-11-801 A319 SRM 51-72-11-801 AND DRAWING D53114223.
Part: FRAME — CRACKED (ZONE 200) · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 1 IN UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 11 OCLOCK, AT FWD GALLEY AREA, HOLE 1 L=0.246 INCH. MAINTENANCE ACCOMPLISHED TIME LIMIT REPAIR ON FR16 RH BTW STR5 TO STR 10 FWD GALLEY AREA (PARTIAL FRAME REPLACEMENT) IAW EA 374012 AND REPAIR DRAWING R53113279.
Part: BONDING PLATE — CRACKED (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK ELEVATOR HINGE ARM 2 BONDING PLATE ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 BONDING PLATE ON LH HORIZONTAL IAWA319 SRM 51-42-11-801, DWG-D55182712 AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #3 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: BONDING PLATE — BROKEN (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: BROKEN BONDING PLATE HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED BONDING PLATE HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER IAW A319 SRM 51-42-11-801, DWG D55182732.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE ARE L= 0.9540 INCHES W= 0.900 INCHES D=0.010 INCHES. MAINTENANCE REPLACED SHEAR PLATE LOCATED STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53474180 AND IAW A320FAM AMM 38-31-36- 400-001-A STEP 4.A(6) THRU 4A(11) L1 THRU L3.
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 67 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.
Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION SHEAR PLATE STR 23 L BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE OF CORROSION IS L= 2.494 INCH W= 0.539 INCH D= 0.015 INCH. MAINTENANCE REPLACED SHEAR PLATE LOC. AT STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53474180.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LOC. BTW FR67 +5 IN. AT LEVEL STR23 R AT AFT GALLEY AREA (CPCP 534136-01). MEASURES ARE L=0.992 IN, W= 0.297 IN, D= 0.091 IN. MAINTENANCE REPLACED CENTER FITTING LOC AT STRG 23R AND BTW FR66 AND FR68. IAW A319 SRM 51-42-11-801 AND DWG D53480505.
Part: HINGE FITTING — EXCESS PLAY (ZONE 200) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 2 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 5 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 4 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON RH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: DUMMY RAIL — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,773 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION RAIL DUMMY Y503.2 BTW FR12 AND FR16 AT FWD GALLEY AREA. CORRODED ARE IS L=1.083 INCH, W=0.821 INCH, D=0.089 INCH. MAINTENANCE REPLACED RAIL DUMMY Y503.2 BTW FR12 AND FR16 AT FWD GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-001, DWG-D53114410 AND DWG-D53114411.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 33,774 hrs · 16,455 cycles
AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON LH HORIZONTAL STABILIZER I.A.W A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
Earlier reports · 1995–2024 · 46 reports
2024
Part: DOOR — STUCK (ZONE 800) · airframe 30,314 hrs · 14,541 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT AFT LAV DOOR WILL NOT OPEN PER THE FA'S. MAINTENANCE ADJUSTED AND OPS CKD LAV DOOR IAW AMM 25-40-00.
Part: O-RING — LEAKING (HYD SYSTEM) · airframe 29,753 hrs · 14,214 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING AT CRUISE A BLUE HYDRAULIC SYSTEM RESERVOIR LOW LEVEL ECAM MESSAGE AND THE LOSS OF ALL BLUE HYDRAULIC SYSTEM FLUID. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE BLUE HYDRAULIC SYSTEM PRESSURE SWITCH 2074GJ LEAKING DUE TO A BROKEN O-RING. MAINTENANCE REPLACED THE O-RING AND ACCOMPLISHED A SATISFACTORY LEAK/OPERATIONAL CHECK.
2023
Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 27,188 hrs · 12,811 cycles
AIRCRAFT WAS NOT GROUNDED: AFT CABIN MEGAPHONE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE MEGAPHONE AND ACCOMPLISED A SATISFACTORY OPERATIONAL CHECK.
Part: CONNECTOR — BROKEN (ZONE 200 - FUSE) · airframe 26,559 hrs · 12,451 cycles
AIRCRAFT WAS GROUDED: SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR BROKEN AND REPAIRED IT PER AMM 33-51-08. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: WIRE HARNESS — DEFECTIVE (ZONE 200 - FUSE) · airframe 26,559 hrs · 12,451 cycles
AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT ROW 21 INOPERATIVE. REPLACED WIRE HARNESS BETWEEN SEAT ROWS 20 AND 21 FOR EMERGENCY ESCAPE LIGHT PER ASM 33-51-00** (CLOSED)
Part: CONNECTOR — BROKEN (ZONE 200 - FUSE) · airframe 26,559 hrs · 12,451 cycles
AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE FOUND EMERGENCY LIGHT CONNECTOR BROKEN AND REPAIRED IT PER AMM 33-51-08. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 26,559 hrs · 12,451 cycles
AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT ROW 21 INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
2022
Part: PROXIMITY SWITCH — FALSE INDICATION (AFT CABIN DOOR) · airframe 25,152 hrs · 11,801 cycles
AIRCRAFT WAS GROUNDED: AFT CABIN DOOR SLIDE INDICATION DOOR PAGE DISAGREES WITH SLIDE ARM STATUS IN FLIGHT. ON GROUND ALL FOUR DOORS INDICATE ARMED 2L DOOR IN FLIGHT DISAGREES WITH ARMED STATUS. MAINTENANCE REPLACED LEFT AFT ESCAPE SLIDE PROXIMITY SWITCH 7WN1 PER AMM 52-73-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-71-00.
Part: INDICATOR — FALSE INDICATION (L3 DOOR) · airframe 25,096 hrs · 11,776 cycles
AIRCRAFT WAS GROUNDED: 3L DOOR SHOWS NOT ARMED DURING FLIGHT INTERMITTENTLY. MAINTENANCE REPLACED 3L DOOR SLIDE ARMED INDICATOR LIGHT ASSEMBLY PER AMM 52-73-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: RELAY — DEFECTIVE (ZONE 100 - FUSE) · airframe 25,071 hrs · 11,764 cycles
AIRCRAFT WAS GROUNDED: DURING FLIGHT L3 DOOR SLIDE DISPLAYS DISARMED. FLIGHT ATTENDANT VERIFIED ARMED. ALSO L1 DOOR WAS INTERMITTENT AS WELL DURING FLIGHT. MAINTENANCE REPLACED POWER SUPPLY SWITCH OVER RELAY 12WN PER TSM 52-11-00. A SATISFATORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 24,665 hrs · 11,560 cycles
AIRCRAFT WAS GROUNDED: RIGHT HAND AFT DOOR ASSIST BOTTLE LOW PRESSUER. SERVICED DOOR ASSIST BOTTLE PER AMM 25-62-00.
Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 24,665 hrs · 11,560 cycles
AIRCRAFT WAS GROUNDED: LEFT HAD AFT EMERGENCY POWER SUPPLY UNIT 13WL FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 24,665 hrs · 11,560 cycles
AIRCRAFT WAS GROUNDED: LEFT HAND AFT DOOR ASSIST BOTTLE LOW PRESSUER. SERVICED DOOR ASSIST BOTTLE PER AMM 25-62-00.
Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 23,832 hrs · 11,148 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT DOOR ASSIST BOTTLE REQUIRES SERVICING SERVICED RIGHT HAND AFT DOOR ASSIST BOTTLE PER AMM 52-10-0
Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 23,832 hrs · 11,148 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT DOOR ASSIST BOTTLE REQUIRES SERVICING SERVICED LEFT HAND AFT DOOR ASSIST BOTTLE PER AMM 52-10-0
Part: WIRE — BROKEN (ZONE 200 - FUSE) · airframe 23,727 hrs · 11,101 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT ROW 13C EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRES FOR SEAT ROW 13C EMERGENCY LIGHT PER ESPM 20-43-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-51-00.
Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 23,280 hrs · 10,893 cycles
AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT AT SEAT ROW 21 ABC IS INOPERATIVE. MAINTENANCE FOUND DAMAGED WIRES AT LIGHT ASSEMBLY SHORT HARNESS AND REPLACED THE LIGHT ASSEMBLY PER AMM 33-51-19. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: FIRE BOTTLE — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 22,855 hrs · 10,715 cycles
AIRCRAFT WAS GROUNDED: APU AGENT DISCHARGE LIGHT ILLUMINATED. REPLACED APU FIRE EXTINGUISHER BOTTLE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-22-41
Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 22,778 hrs · 10,688 cycles
AIRCRAFT WAS NOT GROUNDED: LEFT AFT DOOR EMERGENCY ACCUMULATOR NEEDS SERVICING. PERFORMED ACCUMULATOR CHARGING PER AMM 52-10-00.
Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 22,778 hrs · 10,688 cycles
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT DOOR EMERGENCY ACCUMULATOR NEEDS SERVICING. PERFORMED ACCUMULATOR CHARGING PER AMM 52-10-00.
2021
Part: LIGHT — MALFUNCTIONED (SEAT 14DEF) · airframe 19,689 hrs · 9,333 cycles
AIRCRAFT WAS NOT GROUNDED. EXIT C06181 N210 SIGN AT 14 DEF LIT UP AFTER LANDING UNCOMMANDED LIGHTING. ACCOMPLISHED CABIN INTERCOMMUNICATION DATA SYSTEM RESET, PER AMM 23-73-00, NO FAULTS NOTED.
2020
Part: SPRING — DIRTY (GIRT BAR) · airframe 19,079 hrs · 9,058 cycles
AIRCRAFT WAS GROUNDED: 1L DOOR IS DIFFICULT TO ARM AND DISARM. CLEANED AND GREASED GRIT BAR TRIGGER SPRING IAW AMM 12-22-52 STEP 4 SECTION (A) STEP 5.
Part: HINGE FITTING — WORN (PAX DOOR) · airframe 18,990 hrs · 9,008 cycles
AIRCRAFT WAS GROUNDED: FORWARD PASSENGER L1 DOOR GUST LOCK DOES NOT ENGAGE WITH DOOR FULLY OPEN. FOUND HINGE FITTING BUSHINGS BENT/MIGRATED. REPLACED THE UPPER HINGE FITTING (AALA202009169001) AND THE LOWER HINGE FITITNG (AALA202009169011), PER AARD 51-00-00-3.
Part: HINGE FITTING — WORN (L1 DOOR) · airframe 18,990 hrs · 9,008 cycles
AIRCRAFT WAS GROUNDED: FORWARD PASSENGER L1 DOOR GUST LOCK DOES NOT ENGAGE WITH DOOR FULLY OPEN. FOUND HINGE FITTING BUSHINGS BENT/MIGRATED. REPLACED THE UPPER HINGE FITTING (AALA202009169001) AND THE LOWER HINGE FITITNG (AALA202009169011), PER AARD 51-00-00-3.
2019
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 17,107 hrs · 8,114 cycles
AIRCRAFT WAS NOT GROUNDED: EXIT LIGHT LENS COVER MISSING AT DOOR 1R. MAINTENANCE REPLACED LIGHT LENS COVER PER STANDARD PRACTICES.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 16,703 hrs · 7,910 cycles
AIRCRAFT IN BASE VISIT: BATTERY PACK FAILING AT ESPU 12WL, RH SIDE OF ESCAPE HATCH. REMOVED AND REPLACED ESPU 12WL IAW AMM 33-51-38, OPS CHECK GOOD.
Part: COVER — OUT OF ALIGNMENT (LT OVRWING SLIDE) · airframe 16,703 hrs · 7,910 cycles
AIRCRAFT IN BASE VISIT: LH OFF-WING ESCAPE SLIDE ENCLOSURE IS NOT FLUSH WITH THE OUTER SURFACE OF THE ESCAPE SLIDE. REMOVED AND REPLACED LH OFF-WING ESCAPE SLIDE IAW WORK CARD 1621.
Part: SUPPORT ANGLE — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 16,703 hrs · 7,910 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT, LEFT HAND SIDEWALL TO FLOOR SUPPORT ANGLE BETWEEN FR 53 AND FR 54 AT S38L. REPLACED FLOOR SUPPORT ANGLE PER SRM 51-42-11.
Part: DOOR SILL — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 16,703 hrs · 7,910 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT -Y1290. REPLACED LOWER SILL PER SRM 51-42-11.
Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 16,703 hrs · 7,910 cycles
AIRCRAFT IN BASE VISIT: L2 DOOR DAMPER / EMER CYLINDER LOW PRESSURE. SERVICED L2 DOOR OPERATING CYLINDER IAW AMM 52-10-00-614-001-A.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 16,055 hrs · 7,605 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS ON DECENT AT APROX 5000' AUTOPILOT AND AUTOTHRUST ON TURBULENCE (LIGHT) CAUSED AIRSPEED TO RAPIDLY INCREASE FROM SELECTED 180KTS TO APROX 205KTS THEN BACK TO 170 KTS THEN BACK TO 200 KTS OVERSPEED WARNING OCCURED. MAINTENANCE REPORTS FLT CREW VERBAL REPORT OF FLAPS 2 SELECTED DURING OVERSPEED NOTED TO BE 5 KNOTS IAW VFE PLACARD. PERFORMED FLAP/SLAT EXTENSION RETRACTION CHECKOUT AND VISUAL INSP IAW AMM 05-51-13-200-001-A. NO DEFECT NOTED OK FOR SERVICE.
Part: UNKNOWN — ODOR (CABIN) · airframe 15,221 hrs · 7,230 cycles
TOXIC FUMES NOTED BY AFT FLIGHT ATTENDANTS AND COCKPIT CREW IN FLIGHT. AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED AN ENGINE SMOKE ODOR FUMES TROUBLESHOOTING IAW MCM 05-96-72, NO FUMES OR ODOR NOTED.
2018
Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 14,903 hrs · 7,077 cycles
L2 CABIN DOOR ASSIST BOTTLE WAS BELOW LIMITS. SERVICED THE L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.
Part: GENERATOR — DEFECTIVE (LAV VACUUM) · airframe 13,863 hrs · 6,622 cycles
AIRCRAFT WAS GROUNDED. INBOUND CREW REPORTS ELECTRICAL SMELL RELATED TOO RIGHT HAND AFT LAVATORY AREA. REPLACED LAVATORY GENERATOR VACUUM PER AMM 38-31-64.
Part: OUTFLOW VALVE — FAILED (CABI PRESSURE) · airframe 13,646 hrs · 6,526 cycles
DURING CRUISE, RECEIVED A VENT SKIN FAULT AND BLOWER VENT FAULT WHILE ENROUTE. AIRCRAFT DIVERTED. NO EMERGENCY WAS DECLARED. AIRCRAFT WAS GROUNDED. REPLACED THE FIN 22HQ AVIONICS VENTILATION SKIN AIR OUTLET VALVE IAW AMM 21-26-53-400-001-A01.
2017
Part: LINE — MISSING (LT OVERWING) · airframe 11,445 hrs · 5,572 cycles
ESCAPE LIFE LINE AT THE LEFT OVERWING MISSING. INSTALLED A NEW LIFE LINE IAW AMM 25-34-00.
Part: LINE — MISSING (LT OVERWING) · airframe 11,435 hrs · 5,566 cycles
LEFT OVERWING LIFELINE IS MISSING FROM THE OVERHEAD COMPARTMENT, ADJACENT TO LEFT OVERWING HATCH. REPLACED LEFT OVERWING EXIT LIFELINE IAW AMM 25-34-00.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 11,416 hrs · 5,554 cycles
EMERGENCY BACKUP BATTERY FAILED DURING CIDS TEST & PS CHECK. REPLACED EMERGENCY BACKUP BATTERY IAW AMM 33-51-38.
Part: DOOR LATCH — UNSECURE (ZONE 800) · airframe 10,797 hrs · 5,265 cycles
AIRCRAFT WAS NOT GROUNDED. LEFT AFT CABIN DOOR LATCH ON TOP LEFT EMERGENCY EXIT SLIDE CONTAINER IS LOOSE OR ABOUT TO COME OFF. MAINTENANCE RESECURED LATCH TO AFT LEFT SLIDE CONTAINER PER AMM 20-21-00.
Part: LENS — MISSING (SLIDE ARMED) · airframe 10,402 hrs · 5,079 cycles
SLIDE ARMED LIGHT LENS IS MISSING FROM THE R1 DOOR. REPLACED THE LENS IAW AMM 25-62-44.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 9,345 hrs · 4,611 cycles
EMERGENCY LIGHT POWER SUPPLY UNIT AT 12WL FAILED TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.
2016
Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 8,282 hrs · 4,131 cycles
EMERGENCY LIGHT AT ROW 27 ABC INOPERATIVE. FOUND WIRE BROKEN IN LIGHT WIRING HARNESS. REMOVED AND REPLACED WIRING HARNESS IAW ESPM 20-33-22. OPS CHECKED GOOD IAW AMM 33-51-00-710-004-A.
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 7,865 hrs · 3,933 cycles
EMERGENCY POWER SUPPLY UNIT 11WL FAILED TEST. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED UNIT IAW AMM 33-51-88. CIDS TEST NORMAL.
1997
Part: LATCH PLATE — BENT (PAX DOOR)
AIRCRAFT DIVERTED TO SYR DUE TO CABIN PRESSURE PROBLEMS. *S/D* FOUND DOOR FRAME LATCH PLATE BENT (NOT FLUSH) CAUSING SEAL NOT TO SEAT ON THE FRAME. REPAIRED COVER PLATE.
1996
Part: LIGHT STRIP — INOPERATIVE (CABIN)
EMERGENCY ESCAPE PATH LIGHTING AT ROW 12 INOPERABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS O.K.
1995
Part: FIRE CONTL UNIT — MALFUNCTIONED (NR 1 ENGINE)
LANDED UNDER AMBER ALERT, DUE TO A FIRE WARNING INDICATION ON THE NUMBER 1 ENGINE. REPLACED ENGINE FIRE CONTROL UNIT.