# Service difficulty reports: N91050, cancelled Aug 26, 2011

A list on [N91050, cancelled Aug 26, 2011](https://openairdocs.org/deregistered/N91050-2011-08-26.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 88 reports

- [SDR AALA2009051500002](https://openairdocs.org/sdr/AALA2009051500002.md): Gcu · faulty · May 15, 2009 · N91050 · Airbus A300B4605R · AC Generator-Alternator
  > MIA - AIRCRAFT REPORTED PITCH TRIM SYSTEM FAIL. EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND ALL PARAMETERS SPIKED WHEN LEFT ENGINE GENERATOR TRIPPED OFF. REPLACED NUMBER ONE GENERATOR CONTROL UNIT. SYSTEM GROUND
- [SDR AALA2009041800776](https://openairdocs.org/sdr/AALA2009041800776.md): Power Supply · inoperative · Apr 18, 2009 · N91050 · Airbus A300B4605R · Emergency Lighting
  > JFK - RIGHT NUMBER 2 DOOR EXIT SIGN INOPERATIVE. REPLACED POWER UNIT AT RIGHT NUMBER 2 DOOR PANEL.
- [SDR AALA2009040300707](https://openairdocs.org/sdr/AALA2009040300707.md): Battery Pack · discharged · Apr 3, 2009 · N91050 · Airbus A300B4605R · Emergency Lighting
  > MIA - EMERGENCY LIGHTS IN AFT CABIN AT SEAT 29C VERY DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN AT SEAT 29C.
- [SDR AALA200802685](https://openairdocs.org/sdr/AALA200802685.md): Jackscrew · malfunctioned · Oct 7, 2008 · N91050 · Airbus A300B4605R · Trailing Edge Flap Control System
  > MIA - CREW REPORTED FAULT FOR FLAP SYSTEM NUMBER ONE AND TWO. FLAPS DID NOT EXTEND. ABORTED APPROACH AND FLEW AROUND FOR SECOND APPROACH. SLATS AND FLAPS WORKED NORMAL. LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED SPECIAL ITEMS CARD 5705 FLAP JACKSCREW DRAIN
- [SDR AALA20071816](https://openairdocs.org/sdr/AALA20071816.md): Battery Pack · inoperative · Sep 27, 2007 · N91050 · Airbus A300B4605R · Emergency Lighting
  > LGA - EMERGENCY LIGHT AT STATION 243 INOPERATIVE. REPLACED BATTERY PACK AND MODULE FOR EMERGENCY LIGHT AT STATION 243. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20071657](https://openairdocs.org/sdr/AALA20071657.md): Battery Pack · inoperative · Aug 30, 2007 · N91050 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20071658](https://openairdocs.org/sdr/AALA20071658.md): Battery Pack · inoperative · Aug 30, 2007 · N91050 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT MOUNTED RIGHT MID CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050091](https://openairdocs.org/sdr/AALA20050091.md): Circuit Board · burned · Feb 7, 2005 · N91050 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY EXIT LIGHT AT LEFT 2 DOOR INOPERATIVE. FOUND BURNED CIRCUIT BOARD ON LIGHT ASSEMBLY AT LEFT NUMBER 2 DOOR FOR EMERGENCY EXIT LIGHT. REPLACED LIGHT ASSEMBLY AT 63WL FOR EMERGENCY EXIT LIGHT AT LEFT NUMBER 2 DOOR. SYSTEM GROUND CHECKED NORMAL
- [SDR AALA20040696](https://openairdocs.org/sdr/AALA20040696.md): Cylinder · failed · Jun 24, 2004 · N91050 · Airbus A300B4605R · Escape Slide
  > DURING SLIDE RAFT DEPLOYMENT TEST LEFT 4 DOOR FAILED TO FULLY OPEN. REPLACED EMERGENCY OPERATION CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20040695](https://openairdocs.org/sdr/AALA20040695.md): Flap Track · corroded · Jun 23, 2004 · N91050 · Airbus A300B4605R · Trailing Edge Flaps
  > TUL - NUMBER ONE LEFT HAND FLAP TRACK HAS LIGHT CORROSION INSIDE RADIUS AFT END OF NUMBER ONE FLAP TRACK ATTACH POINT BARREL NUT. CORRODED AREA IS ONE INCH BY ONE INCH. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004.
- [SDR AALA20040693](https://openairdocs.org/sdr/AALA20040693.md): Skin · corroded · Jun 23, 2004 · N91050 · Airbus A300B4605R · Fuselage Main, Plate/Skin
  > TUL - SKIN CORRODED BETWEEN STRINGERS 53L AND 54L AT FRAME 65 IN AFT CARGO AT STATION NUMBER 4256. AREA OF CORROSION IS 3.75 INCHES BY 4.88 INCHES. INSTALLED SKIN FILLER AND STACK DOUBLER PER ESO 30595 DATED JUNE 22, 2004.
- [SDR AALA20040694](https://openairdocs.org/sdr/AALA20040694.md): Flap Track · gouged · Jun 23, 2004 · N91050 · Airbus A300B4605R · Trailing Edge Flaps
  > TUL - FLAP TRACK NUMBER ONE LIFT GOUGED INSIDE AFT ATTACH POINT BARREL NUT HOLE. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH AND LOCATED AT STATION 3300. REPAIRED PER ESO 30595 REPAIR NUMBER 40 572000 3473 DATED JUNE 22, 2004.
- [SDR AALA20040692](https://openairdocs.org/sdr/AALA20040692.md): Skin · corroded · Jun 23, 2004 · N91050 · Airbus A300B4605R · Fuselage Main, Plate/Skin
  > CORROSION ON LOWER RIGHT WING SKIN INSIDE SLAT TRACK SEVEN TRACK WELL. AREA OF CORROSION IS SEVEN INCHES BY FIVE INCHES AND LOCATED A STATION NUMBER 1260. REPAIRED CORROSION PER ESO 30595 DATED JUNE 22, 2004.
- [SDR AALA20040691](https://openairdocs.org/sdr/AALA20040691.md): Stringer · corroded · Jun 21, 2004 · N91050 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > STRINGER 56L IS CORRODED JUST AFT OF FRAME 54. CORRODED AREA WAS 2 INCH BY 2 INCH. REPAIRED STRINGER 56L PER 51-71-10-0.
- [SDR AALA20040665](https://openairdocs.org/sdr/AALA20040665.md): Butt Joint · corroded · Jun 17, 2004 · N91050 · Airbus A300B4605R · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT SPLICE STRAP CORRODED AT FRAME 65 BETWEEN STRINGERS 54 AND 55L. AREA IS 2 INCHES BY 5 INCHES IN THE AFT CARGO AREA. INSTALLED NEW BUTTSTRAP AND BUTTSTRAP EXTERNAL DOUBLER PER ESO 30595 DATED 6/16/04.
- [SDR AALA20021385](https://openairdocs.org/sdr/AALA20021385.md): Pin · backed out · Sep 29, 2002 · N91050 · Airbus A300B4605R · Emergency Lighting
  > MIA - EMERGENCY SEAT MOUNTED LIGHT AT 32G INOPERATIVE. RESECURED PIN THAT WAS FOUND OUT OF CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20000132](https://openairdocs.org/sdr/AALA20000132.md): Switch · failed · Jan 22, 2000 · N91050 · Airbus A300B4605R · Emergency Equipment
  > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION SIGNAL CUT OFF SWITCH AT DOOR R1 DOES NOT CUT OFF. REPLACED EMERGENCY EVACUATION SIGNAL CUT OFF SWITCH AT DOOR R1. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA991971](https://openairdocs.org/sdr/AALA991971.md): Wire · chafed · Dec 26, 1999 · N91050 · Airbus A300B4605R · Communications System Wiring
  > PTY - FLT 917 - DURING FLIGHT ELECTRICAL BURING SMELL AROUND BUSINESS CLASS VIDEO RECORDER. DIVERTED AND LANDED PTY WITHOUT INCIDENT. REPAIRED CHAFED WIRING. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED VIDEO RECORDER AS PRECAUTION. (M)
- [SDR AALA991871](https://openairdocs.org/sdr/AALA991871.md): Shear Tie · corroded · Dec 3, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 59 AND BETWEEN STRINGER 46R AND 47R. INSTALLED NEW SHEAR TIE PER SRM 51-74-10. (M)
- [SDR AALA991870](https://openairdocs.org/sdr/AALA991870.md): Splice · corroded · Dec 3, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - STRINGER SPLICE CORRODED ON STRINGER 54 LEFT BETWEEN FRAMES 32 AND 34. REPLACED STRINGER SPLICE PER SRM 51-72-10. (M)
- [SDR AALA991834](https://openairdocs.org/sdr/AALA991834.md): Stringer · corroded · Dec 2, 1999 · N91050 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 52R AT FRAME 59. INSTALLED REPAIR DOUBLER PER SRM 53-10-14. (M)
- [SDR AALA991833](https://openairdocs.org/sdr/AALA991833.md): Shear Tie · corroded · Dec 2, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - SHEAR TIE HAS CORROSION AT FRAME 59 AND BETWEEN STRINGER 53R AND 54R. INSTALLED MANUFACTURED SHEAR TIE PER SRM 51-75-10. (M)
- [SDR AALA991832](https://openairdocs.org/sdr/AALA991832.md): Fitting · corroded · Nov 30, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON STRINGER 51L AND FITTING AT FRAME 80. INSTALLED NEW STRINGER END FITTING PER SRM 51-75-10. (M)
- [SDR AALA991822](https://openairdocs.org/sdr/AALA991822.md): Splice · corroded · Nov 30, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON STRINGER SPLICE 39 LEFT AT FRAME 58. INSTALLED NEW SPLICE PER SRM 51-72-10. (M)
- [SDR AALA991821](https://openairdocs.org/sdr/AALA991821.md): Splice · corroded · Nov 30, 1999 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON STRINGER SPLICE 37L AT FRAME 58. INSTALLED NEW STRINGER SPLICE PER SRM 51-72-10. (M)
- [SDR AALA991102](https://openairdocs.org/sdr/AALA991102.md): Connector · loose · Jul 28, 1999 · N91050 · Airbus A300B4605R · Emergency Lighting
  > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. RESECURED CONNECTOR TO AFT CABIN EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA971983](https://openairdocs.org/sdr/AALA971983.md): Fitting · corroded · Oct 17, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - LOWER AFT MAN HOLE ACCESS FITTING HAS SEVERAL POCKETS WITH HEAVY CORROSION AROUND FASTENERS. INSTALLED DOUBLERS PER ESO 30595 DATED 10-15-97. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971990](https://openairdocs.org/sdr/AALA971990.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - ROLLER TRAY NR 3 AT FRAME 60 HAS DEEP CORROSION CENTER OF TRAY. REPLACED CORRODED SECTION OF TRAY WITH NEW SERVICEABLE SECTION PER SRM 51-72-10. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971989](https://openairdocs.org/sdr/AALA971989.md): Roller Pan · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION UNDER POWER ROLLER PAN AND AROUND TEMPORARY REPAIR PAN BETWEEN NR 2 AND NR 3 ROLLER TRAYS AND FRAMES 61 AND 62. INSTALLED NEW POWER ROLLER PAN PER SRM 51-22-10-0. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971988](https://openairdocs.org/sdr/AALA971988.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION IN AND AROUND FASTENER HOLES, NR 3 ROLLER TRAY AT FRAME 63. REPLACED CORRODED SECTION OF TRAY WITH NEW SERVICEABLE SECTION PER SRM 51-72-10. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971987](https://openairdocs.org/sdr/AALA971987.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - NR 6 ROLLER TRAY FROM FRAMES 60 TO 61 HAS CORROSION. INSTALLED NEW DOOR SEAL ROLLER TRAY PER SRM 51-72-10-0. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971986](https://openairdocs.org/sdr/AALA971986.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION NR 3 ROLLER TRAY UNDER SIDE AT DOME NUTS BETWEEN FRAMES 61 AND 62. REPLACED CORRODED SECTION OF TRACK WITH NEW SERVICEABLE SECTION OF TRACK PER SRM 51-72-10. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971985](https://openairdocs.org/sdr/AALA971985.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON NR 6 ROLLER TRAY OUTBOARD FLANGE AT FASTENER BETWEEN FRAMES 59 AND 60. REPLACED ROLLER TRAY SECTION WITH NEW PER SRM 53-10-15. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971984](https://openairdocs.org/sdr/AALA971984.md): Roller Tray · corroded · Oct 16, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - ROLLER TRAY NR 6 BETWEEN FRAMES 57.2 AND 57.3 HAS CORROSION AT FLOOR BOARD ATTACH HOLE. REPLACED ROLLER TRAY SECTION WITH NEW ONE PER SRM 53-10-15. TST: 26,111.18 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971972](https://openairdocs.org/sdr/AALA971972.md): Beam · corroded · Oct 10, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - DOOR SEAL BEAM HAS DEEP CORROSION BETWEEN FRAME 59 AND 60. INSTALLED DOUBLER PER SRM 51-71-50-2 PAGE 205. (M)
- [SDR AALA971963](https://openairdocs.org/sdr/AALA971963.md): Support · corroded · Oct 10, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FLOOR SUPPORT HAS CORROSION DAMAGE AT RIGHT AISLE, FOURTH TRACK FROM RIGHT SIDE. INSTALLED NEW FLOOR SUPPORT BETWEEN FRAME 70 TO 72 PER 51-72-10 AND ESO 30595 DATED 10-9-97. (M)
- [SDR AALA971969](https://openairdocs.org/sdr/AALA971969.md): Splice · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON STRINGER SPLICE STRINGER 44L AT FRAME 58. REMOVED AND REPLACED STRINGER SPLICE AT FRAME 58 AT 44L PER SRM 53-10-14. (M)
- [SDR AALA971945](https://openairdocs.org/sdr/AALA971945.md): Frame · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - BELL FRAME NR 58 HAS CORROSION FROM 54L TO 54R. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 53-10-13. (M)
- [SDR AALA971942](https://openairdocs.org/sdr/AALA971942.md): Stringer · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER 44L IS CORRODED AT FRAME 69. REMOVED CORRODED AREA AND INSTALLED NEW SECTION OF STRINGER PER SRM 53-10-14-2. (M)
- [SDR AALA971937](https://openairdocs.org/sdr/AALA971937.md): Stringer · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER 46L AT FRAME 69 HAS CORROSION. REMOVED CORROSION STRINGER AND INSTALLED NEW SECTION PER SRM 53-10-17-2. (M)
- [SDR AALA971926](https://openairdocs.org/sdr/AALA971926.md): Support · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FLOOR SUPPORT, 4TH FROM LEFT SIDE, TOP SURFACE HAS CORROSION DAMAGE BETWEEN FRAMES 70 TO 74. INSTALLED FLOOR SUPPPORT AND SPLICED AT FRAME 70 PER ESO 30595 DATED 10-8-97 AND SRM 51-72-10-0. TST: 26,111 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971925](https://openairdocs.org/sdr/AALA971925.md): Seat Track · corroded · Oct 9, 1997 · N91050 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - SEAT TRACK NR 8 HAS CORROSION DAMAGE ON TOP SURFACE FROM FRAME 26 TO FRAME 33. REPLACED SEAT TRACK NR 8 AT AND BETWEEN PRODUCTION SPLICES IAW 51-72-10-00 FROM FRAMES 26 TO 33. TST: 26,111 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971956](https://openairdocs.org/sdr/AALA971956.md): Skin · corroded · Oct 8, 1997 · N91050 · Airbus A300B4605R · Wing, Plate/Skin
  > TUL - TRAILING EDGE OF WING APPROX 7 FEET FROM WINGLET HAS DEEP CORROSION. REPAIRED AREA IAW ESO30595 DATED 10-07-97. (M)
- [SDR AALA971953](https://openairdocs.org/sdr/AALA971953.md): Static Wick · corroded · Oct 8, 1997 · N91050 · Airbus A300B4605R · Static Discharge System
  > TUL - HEAVY CORROSION UNDER AND AROUND STATIC WICK INBOARD OF WINGLET AT TRAILING EDGE. REPAIRED CORROSION PER ESO 30595 DATED 10-07-97. (M)
- [SDR AALA971951](https://openairdocs.org/sdr/AALA971951.md): Seat Track · corroded · Oct 8, 1997 · N91050 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION AROUND FLOORBOARD ATTACHMENT HOLES AND SEAT LOGS, TRACK NR 10 RIGHT SIDE. REPLACED SECTION OF SEAT TRACK BETWEEN FRAMES 21 TO 26 PER AARD 51-10-00. (M)
- [SDR AALA971924](https://openairdocs.org/sdr/AALA971924.md): Sill · corroded · Oct 8, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON DOOR SILL BEAM AT STA 1678; PRIOR BLENDING OF AREA WAS DONE. BLEND WAS BEYOND LIMITS. FASTENER HOLES WERE DRILLED, BUT NEVER INSTALLED OR PLUGGED. BEAM WAS REPAIRED PER ESO 30595 DATED 10-7-97. TST: 26,111.18 HOURS. CYCLES: 10,811. (
- [SDR AALA971971](https://openairdocs.org/sdr/AALA971971.md): Support · corroded · Oct 7, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORRODED BEYOND LIMITS TOP FWD SIDE LEFT NOSE GEAR DOOR SUPPORT FOR UPLOCK. REPLACED PART AND RIGGED PER CARD NR 7209/ E58 NR 0095203. (M)
- [SDR AALA971922](https://openairdocs.org/sdr/AALA971922.md): Support · corroded · Oct 7, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - OUTER FLOOR BOARD ATTACHMENT FLANGE AREAS HAVE CORROSION DAMAGE RT SIDE AT LAVATORY. INSTALLED NEW SECTION OF FLOOR SUPPORT PER AARD 51-10-00-3, AND SPLICED IN IAW SRM 53-10-16-2, FIG 204. TST: 26,111. CYCLES: 10,811. (X)
- [SDR AALA971917](https://openairdocs.org/sdr/AALA971917.md): Support · corroded · Oct 7, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - SECOND AFT LAVATORY SUPPORT, LEFT OF CENTER, TOP SURFACE HAS CORROSION DAMAGE. REPLACED FLOOR STRUCTURE COMPONENT PER SRM 51-72-10-0. TST: 26,111 HOURS. CYCLES: 10,811. (X)
- [SDR AALA971916](https://openairdocs.org/sdr/AALA971916.md): Support · corroded · Oct 6, 1997 · N91050 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - LAVATORY SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT OR LAVATORY PER SRM 51-72-10-00. TST: 26,111 HOURS. CYCLES: 10,811. (X)

Next page: https://openairdocs.org/deregistered/N91050-2011-08-26/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N91050' AND deregistration_id = 'N91050-2011-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N91050-2011-08-26/reports

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