# Service difficulty reports: N14053, cancelled Apr 26, 2002

A list on [N14053, cancelled Apr 26, 2002](https://openairdocs.org/deregistered/N14053-2002-04-26.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 · 62 reports

- [SDR AALA20011004](https://openairdocs.org/sdr/AALA20011004.md): Stringer Clip · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND FRAME 18 STRINGER 51R STRINGER CLIP IS CORRODED, FS 1336. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 51R PER SRM 51-72-10. (M)
- [SDR AALA20011005](https://openairdocs.org/sdr/AALA20011005.md): Stringer Clip · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND FRAME 18 STRINGER 52R STRINGER CLIP IS CORRODED. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 52R PER SRM 51-72-10. (M)
- [SDR AALA20011003](https://openairdocs.org/sdr/AALA20011003.md): Stringer · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 53 RIGHT OUTBOARD OF ELECTRICAL POWER BOX, FS 1336, 3 INCHES BY 1 INCH. INSTALLED NEW STRINGER PER SRM 51-72-10. (M)
- [SDR AALA20011002](https://openairdocs.org/sdr/AALA20011002.md): Stringer · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - FOUND FRAME 18 TO FRAME 19 STRINGER 53R IS CORRODED, 2 INCHES BY 1 INCH. INSTALLED NEW STRINGER AT FRAME 18 TO FRAME 19 PER SRM 51-72-10. (M)
- [SDR AALA20011001](https://openairdocs.org/sdr/AALA20011001.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18 STRINGER 51R TO 50R, CORRODED ON SHEAR TIE, BS 1336. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
- [SDR AALA20011000](https://openairdocs.org/sdr/AALA20011000.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18 STRINGER 50R TO 49R CORROSION ON SHEAR TIE, FS 1336. INSTALLED NEW FRAME SECTION FRAME 18 STRINGER 50R TO 49R PER SRM 51-72-10. (M)
- [SDR AALA20010999](https://openairdocs.org/sdr/AALA20010999.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18 STRINGER 52R TO 51R HAS CORROSION ON SHEAR TIE, 1 INCH BY 2 INCHES, BS 1336. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
- [SDR AALA20010998](https://openairdocs.org/sdr/AALA20010998.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18 STRINGER 53R TO STRINGER 52R SHEAR TIE CORRODED, 3 INCHES BY 2 INCHES. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
- [SDR AALA20010997](https://openairdocs.org/sdr/AALA20010997.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18 STRINGER 54R TO 53R SHEAR TIE CORRODED. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
- [SDR AALA20010983](https://openairdocs.org/sdr/AALA20010983.md): Frame · corroded · May 9, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - FOUND FRAME 18, STRINGER 54R TO 54L HAS CORROSION ON SHEAR TIE. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
- [SDR AALA20011006](https://openairdocs.org/sdr/AALA20011006.md): Skin · corroded · May 8, 2001 · N14053 · Airbus A300B4605R · Fuselage Main, Plate/Skin
  > TUL - FOUND AREA OF LOWER FUSELAGE SKIN BULGED APPROX 1.5 SQUARE INCHES LOCATED BETWEEN FS 18-19 OF THE NOSE GEAR CUTOUT AFT DOUBLER, LEFT FINGER CORROSION IS AT PREVIOUS REPAIR EDGE. AREA REPAIRED PER ESO 30595 DATED 5/8/2001. (M)
- [SDR AALA20010240](https://openairdocs.org/sdr/AALA20010240.md): Light · inoperative · Feb 13, 2001 · N14053 · Airbus A300B4605R · Emergency Lighting
  > JFK - DURING OVERNIGHT MAINTENANCE, OVERHEAD R3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001552](https://openairdocs.org/sdr/AALA20001552.md): Connector · unsecure · Sep 14, 2000 · N14053 · Airbus A300B4605R · Emergency Lighting
  > JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3G INOPERATIVE. RESECURED PIN CONNECTOR FOR SEAT 3G EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001327](https://openairdocs.org/sdr/AALA20001327.md): Flashlight · inoperative · Aug 10, 2000 · N14053 · Airbus A300B4605R · Emergency Equipment
  > MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY FLASHLIGHT AT 4R DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20000742](https://openairdocs.org/sdr/AALA20000742.md): Transmitter · leaking · May 9, 2000 · N14053 · Airbus A300B4605R · Hydraulic System, Main
  > MCO - FLT 915 - DURING FLIGHT, GREEN HYDRAULIC SYSTEM LEAKING. DIVERTED AND LANDED MCO WITHOUT INCIDENT. REPLACED HYDRAULIC PRESSURE TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20000061](https://openairdocs.org/sdr/AALA20000061.md): Stringer · corroded · Jan 6, 2000 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER CORRODED. SPLICED IN NEW SECTION PER ESO 30595 DATED 1-5-00 FROM FR 34 TO FR 36. TST: 3,224.11 HOURS. CYCLES: 12,979. (X)
- [SDR AALA200064](https://openairdocs.org/sdr/AALA200064.md): Shear Tie · corroded · Jan 3, 2000 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION FROM STR 49L TO STR 50L AT FRAME 36. ALODINED, PRIMED, AND PAINTED PER SRM 51-74-10. INSTALLED NEW SHEARTIE PER SRM 51-72-10. TST: 32,241 HOURS. CYCLES: 12,979. (X)
- [SDR AALA200063](https://openairdocs.org/sdr/AALA200063.md): Shear Tie · corroded · Jan 3, 2000 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON SHEAR TIE BETWEEN 50L AND 51L AT FRAME 35. REMOVED CORROSION PER SRM 51-74-10. ALODINED, PRIMED, AND PAINTED PER SRM 51-74-10. INSTALLED NEW SHEAR TIE PER SRM 51-72-10. TST: 32,241 HOURS. CYCLES: 12,979. (X)
- [SDR AALA2000012](https://openairdocs.org/sdr/AALA2000012.md): Skin · corroded · Dec 30, 1999 · N14053 · Airbus A300B4605R · Fuselage Main, Plate/Skin
  > TUL - SKIN UNDER ANTENNA CORRODED. INSTALLED DOUBLER PER SRM 53-10-12. TST: 32,241.11 HOURS. CYCLES: 12,979. (X)
- [SDR AALA991996](https://openairdocs.org/sdr/AALA991996.md): Lavatory Track · corroded · Dec 27, 1999 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - CORROSION ON LAVATORY SUPPORT IKNBOARD FLANGE BRACKET TRACK B ANC C LEFT SIDE BETWEEN FRAMES 30 AND 31. INSTALLED NEW LAVATORY SUPPORT TRACK PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. (X)
- [SDR AALA991997](https://openairdocs.org/sdr/AALA991997.md): Floorbeam · corroded · Dec 16, 1999 · N14053 · Airbus A300B4605R · Fuselage Main, Floor Beam
  > TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 76 AND 82 ON FLOOR TRACK E LEFT. INSTALLED NEW FLOOR TRAK E LEFT, CPN 4035847 PER SRM 51-72-10-0. TST: 32,291.11 HOURS. CYCLES: 12,979. (X)
- [SDR AALA991995](https://openairdocs.org/sdr/AALA991995.md): Floorbeam · corroded · Dec 16, 1999 · N14053 · Airbus A300B4605R · Fuselage Main, Floor Beam
  > TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 75 AND 80 ON FLOOR TRACK E, RIGHT. INSTALLED NEW FLOOR TRACK E RIGHT, PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. P/N A53278453200. (X)
- [SDR AALA991935](https://openairdocs.org/sdr/AALA991935.md): Floorbeeam · corroded · Dec 15, 1999 · N14053 · Airbus A300B4605R · Fuselage Main, Floor Beam
  > TUL - CORROSION ON FLOOR SUPPORT BETWEEN SEAT TRACKS 'E' RIGHT AND 'D' RIGHT, LOCATED BETWEEN FRAMES 71 1/2 AND 74. REMOVED AND REPLACED FLOOR SUPPORT FROM FRAME 71 1/2 TO FRAME 74 BETWEEN TRACK 'E' RIGHT, AND 'D' RIGHT PER SRM 51-72-10-0. ALODINED, PRIMED,
- [SDR AALA991090](https://openairdocs.org/sdr/AALA991090.md): Acm · defective · Jul 25, 1999 · N14053 · Airbus A300B4605R · Cabin Cooling System
  > KIN - FLT 628 - AFTER TAKEOFF KIN EN ROUTE TO MIA, SMOKE AND FUMES WERE NOTED IN COCKPIT. AIRCRAFT RETURNED TO KIN AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AIR CONDITIONING PACK ACM. ALSO, REPLACED NR 1 AIR CONDITIONING PACK FLOW CONTROL VALVE AS PRECAUTI
- [SDR AALA981723](https://openairdocs.org/sdr/AALA981723.md): Skin · corroded · Sep 24, 1998 · N14053 · Airbus A300B4605R · Wing, Plate/Skin
  > TUL - FOUND RIGHT WING LOWER SURFACE AFT AND OUTBOARD OF NR 2 ENGINE PYLON HAS CORROSION TWO AREAS. REMOVED CORROSION, INSTALLED INTERAL DOUBLER REPAIR PER ESO 30595, DATED 9-24-98. (M)
- [SDR AALA972526](https://openairdocs.org/sdr/AALA972526.md): Stringer · corroded · Dec 19, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STR 52R HAS SURFACE CORROSION AT FRAME 54.1 FORWARD SIDE. REPAIRED PER ESO 30595 DATED 12-18-97. TST: 26,718.41 HOURS. CYCLES: 10,861. (X)
- [SDR AALA972458](https://openairdocs.org/sdr/AALA972458.md): Seat Track · corroded · Dec 18, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON NR 3 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
- [SDR AALA972525](https://openairdocs.org/sdr/AALA972525.md): Support · corroded · Dec 17, 1997 · N14053 · Airbus A300B4605R · Leading Edge Slat Actuator
  > TUL - CORROSION ON OUTBOARD SHELF FOR RT KRUEGER FLAP ACT. REMOVED AND REPLACED SUPPORT PER SRM 57-45-11-0 PAGE 2 ITEM 20. TST: 26,718.41 HOURS. CYLES: 10,861. (X)
- [SDR AALA972483](https://openairdocs.org/sdr/AALA972483.md): Frame · corroded · Dec 16, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - BELLFRAME AT FRAME STATION 60 HAS CORROSION ON AFT SIDE. INSTALLED DOUBLER AS PER SRM 53-10-13. (M)
- [SDR AALA972482](https://openairdocs.org/sdr/AALA972482.md): Stringer · corroded · Dec 16, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER 49R HAS CORROSION AT FRAME STATION 60 ON FORWARD SIDE. INSTALLED DOUBLER AND FILLER AS PER SRM 53-10-14 WHERE CORRODED SECTION OF LONGERON REMOVED. (M)
- [SDR AALA972481](https://openairdocs.org/sdr/AALA972481.md): Frame · corroded · Dec 16, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - BELL FRAME CORRODED AT STATION 57.2 FRONG AND BACK SIDE BETWEEN STRINGER 55R AND 55L. REPAIRED BELL FRAME PER SRM 53-10-13 ALODINED PRIMED AND PAINTED PER SRM 51-75-10. (M)
- [SDR AALA972466](https://openairdocs.org/sdr/AALA972466.md): Support · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Wing Miscellaneous Structure
  > TUL - RIGHT WING LE SUPPORT HAS CORROSION. REPAIRED PER ESO30595, DATED 12-12-97. (M)
- [SDR AALA972465](https://openairdocs.org/sdr/AALA972465.md): Beam · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Wing Miscellaneous Structure
  > TUL - RIGHT KRUGER FLAP ACT CROSSBEAM HAS CORROSION ON BEAM. REMOVED AND REPLACED CROSSBEAM PER SRM 57-45-11 PAGE 2 ITEM NR 5. (M)
- [SDR AALA972464](https://openairdocs.org/sdr/AALA972464.md): Stringer · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 48 LEFT. REPLACED SECTION OF STRINGER AT FRAMES 70 AND 71, STRINGER 48L PER SRM 51-72-10. (M)
- [SDR AALA972463](https://openairdocs.org/sdr/AALA972463.md): Stringer · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - STRINGER 49L HAS CORROSION FORWARD SIDE AT STATION FRAME 59. REPAIRED STRINGER PER SRM 53-10-14 PAGE 203-204. ALODINED, PRIMED AND PAINTED PER SRM 51-25-10. (M)
- [SDR AALA972459](https://openairdocs.org/sdr/AALA972459.md): Roller Tray · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON OUTBOARD SIDE OF ROLLER TRAY, FORWARD CARGO NR 1 TRAY LEFT SIDE OF A/C. INSTALLED NEW SECTION OF ROLLER TRAY, NR 1 LEFT SIDE OF FWD CARGO BETWEEN FRAMES 27 TO 31, PR 53-10-15. (M)
- [SDR AALA972457](https://openairdocs.org/sdr/AALA972457.md): Roller Tray · corroded · Dec 15, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON NR 3 ROLLER TRAY. REPLACED NR 3 ROLLER TRAY BETWEEN FRAMES 30 TO 32 PER SRM 53-10-15. (M)
- [SDR AALA972462](https://openairdocs.org/sdr/AALA972462.md): Support · corroded · Dec 13, 1997 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ALONG SUPPORT AT SEVERAL PLACES BETWEEN FRAME 60-63. REMOVED AND REPLACED FRAME SUPPORT FROM FRAME 59-64 PER SRM 53-10-14. (M)
- [SDR AALA972461](https://openairdocs.org/sdr/AALA972461.md): Stringer · corroded · Dec 13, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - TOP OF STRINGER HAS CORROSION ON IT STRINGER 54 FROM FRAME 19 TO 20. INSTALLED STRINGER REPAIR PER SRM 53-10-14 PAGE 203 AND 204. (M)
- [SDR AALA972460](https://openairdocs.org/sdr/AALA972460.md): Intercostal · corroded · Dec 12, 1997 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON INTERCOSTAL RT SIDE CARGO COMPT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-71-30. (M)
- [SDR AALA980329](https://openairdocs.org/sdr/AALA980329.md): Bracket · corroded · Dec 11, 1997 · N14053 · Airbus A300B4605R · Wing Miscellaneous Structure
  > TUL - SWITCH BRACKET A5351094120000 CORRODED IN KRUEGER WELL. REMOVED CORRODED BRACKET AND INSTALLED NEW SWITCH BRACKET PER A360 SRM 51-72-10. (X)
- [SDR AALA972524](https://openairdocs.org/sdr/AALA972524.md): Mount · corroded · Dec 11, 1997 · N14053 · Airbus A300B4605R · Leading Edge Devices
  > TUL - KRUEGER FLAP OUTBOARD CARRIER MOUNT CORRODED. REMOVED OUTBOARD CARRIER MOUNT. REPLACED WITH NEW MOUNT. A-300 MM 27-87-14-4. TST: 26,718.41 HOURS. CYCLES: 10,861. (X)
- [SDR AALA972402](https://openairdocs.org/sdr/AALA972402.md): Frame · corroded · Dec 11, 1997 · N14053 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - HEAVY CORROSION ON FRAME NR 25 UNDER ROLLER TRAY NR 3. INSTALLED NEW TOP CAP BEAM SECTION AS PE SRM 53-10-15. (M)
- [SDR AALA972441](https://openairdocs.org/sdr/AALA972441.md): Support · corroded · Dec 10, 1997 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON 'T' ANGLE SUPPORT UNDER NR 1 ROLLER TRAY. SPLICED IN NEW TOP CAP PER SRM 53-10-15, ALODINE, PAINT PER SRM 51-75-10. (M)
- [SDR AALA972361](https://openairdocs.org/sdr/AALA972361.md): Seat Track · corroded · Dec 9, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON NR 8 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
- [SDR AALA972360](https://openairdocs.org/sdr/AALA972360.md): Tie Down Track · corroded · Dec 9, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON TIE DOWN TRACK BETWEEN SEAT TRACKS 8 AND 9. INSTALLED NEW TRACK PER 51-72-10-0 SRM. (M)
- [SDR AALA972359](https://openairdocs.org/sdr/AALA972359.md): Seat Track · corroded · Dec 9, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON NR 8 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
- [SDR AALA972392](https://openairdocs.org/sdr/AALA972392.md): Seat Track · corroded · Dec 8, 1997 · N14053 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON NR 7 SEAT TRACK. REPAIRED PER AARD 53-20-00-2 BY INSTALLING STRAP. (M)
- [SDR AALA972358](https://openairdocs.org/sdr/AALA972358.md): Support · corroded · Dec 8, 1997 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON SUPPORT AT 'A' LAV. REPLACED SUPPORT PER SRM 51-72-10. (M)
- [SDR AALA972357](https://openairdocs.org/sdr/AALA972357.md): Beam · corroded · Dec 8, 1997 · N14053 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FOUND CORROSION ON BEAM BETWEEN SEAT TRACKS 8 AND 9. REPLACED BEAM PER SRM 51-72-10. (M)

Next page: https://openairdocs.org/deregistered/N14053-2002-04-26/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 = 'N14053' AND deregistration_id = 'N14053-2002-04-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14053-2002-04-26/reports

---
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