# Service difficulty reports: N80052, cancelled Aug 19, 2011

A list on [N80052, cancelled Aug 19, 2011](https://openairdocs.org/deregistered/N80052-2011-08-19.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 · 63 reports

- [SDR AALA200802251](https://openairdocs.org/sdr/AALA200802251.md): Cover · broken · Aug 31, 2008 · N80052 · Airbus A300B4605R · Pressure Regulator/Outflow Valve
  > NAS INFLIGHT T861/31AUG MCO TO SJU. CREW REPORTED PRESSURIZATION FAULT. LANDED NAS WITHOUT INCIDENT. REPLACED FLAPPER VALVE COVER. SYSTEM GROUND CHECKED NORMAL OPS.
- [SDR AALA200801584](https://openairdocs.org/sdr/AALA200801584.md): Link Assy · defective · Jun 11, 2008 · N80052 · Airbus A300B4605R · Landing Gear Position and Warning
  > JFK INFLIGHT T1299/11JUN. CREW REPORTED RED MAIN LANDING GEAR DOOR INDICATION AFTER TAKEOFF. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SENSOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
- [SDR AALA200801557](https://openairdocs.org/sdr/AALA200801557.md): Pitot Tube · failed · Jun 7, 2008 · N80052 · Airbus A300B4605R · Pitot/Static System
  > PTY INFLIGHT T2110/07JUN LIM TO MIA. CAPTAINS AIR SPEED INDICATION INOPERATIVE. LANDED PTY WITHOUT INCIDENT. REPLACED CAPTAINS PITOT PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
- [SDR AALA200800437](https://openairdocs.org/sdr/AALA200800437.md): Lamp · inoperative · Feb 28, 2008 · N80052 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200800439](https://openairdocs.org/sdr/AALA200800439.md): Lamp · inoperative · Feb 28, 2008 · N80052 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200800438](https://openairdocs.org/sdr/AALA200800438.md): Lamp · inoperative · Feb 28, 2008 · N80052 · Airbus A300B4605R · Emergency Lighting
  > JFK - EMERGENCY LIGHT AT LEFT NR 2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20072339](https://openairdocs.org/sdr/AALA20072339.md): Computer · inoperative · Nov 30, 2007 · N80052 · Airbus A300B4605R · Rudder Control System
  > MIA INFLIGHT T377/30NOV - BOTH NUMBER ONE AND TWO RUDDER SYSTEM FAILURE DURING CLIMB. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO FEEL LIMITATION COMPUTERS, NUMBER ONE AND TWO SLAT FLAT CONTROL COMPUTERS, AND NUMBER ONE AND TWO F
- [SDR AALA20072011](https://openairdocs.org/sdr/AALA20072011.md): Battery Pack · inoperative · Oct 22, 2007 · N80052 · Airbus A300B4605R · Emergency Lighting
  > JFK - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20071837](https://openairdocs.org/sdr/AALA20071837.md): Valve · leaking · Oct 1, 2007 · N80052 · Airbus A300B4605R · Hydraulic System, Main
  > BOG INFLIGHT T915/01OCT - BLUE HYDRAULIC SYSTEM AMBER LOW QUANTITY INDICATION AND CHIME. LANDED BOG WITHOUT INCIDENT. FOUND PRESSURE LINE IN WHEEL WELL LEAKING. TIGHTENED LINE AT C PORT OF RELIEF VALVE 2063. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20071712](https://openairdocs.org/sdr/AALA20071712.md): Connector · disconnected · Sep 9, 2007 · N80052 · Airbus A300B4605R · Light System Wiring
  > MIA - EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. SECURED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070990](https://openairdocs.org/sdr/AALA20070990.md): Connector · loose · May 30, 2007 · N80052 · Airbus A300B4605R · Light System Wiring
  > MIA - FOUND EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070992](https://openairdocs.org/sdr/AALA20070992.md): Connector · loose · May 30, 2007 · N80052 · Airbus A300B4605R · Light System Wiring
  > MIA - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070991](https://openairdocs.org/sdr/AALA20070991.md): Lens · missing · May 30, 2007 · N80052 · Airbus A300B4605R · Emergency Lighting
  > MIA - EMERGENCY LIGHT AT SEAT 24G HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070562](https://openairdocs.org/sdr/AALA20070562.md): Lens · missing · Mar 26, 2007 · N80052 · Airbus A300B4605R · Emergency Lighting
  > MIA - EMERGENCY LIGHT IN FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD MISSING COVER. REPLACED LENS FOR EMERGENCY LIGHT IN FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060978](https://openairdocs.org/sdr/AALA20060978.md): Battery Pack · discharged · Nov 4, 2006 · N80052 · Airbus A300B4605R · Emergency Lighting
  > MIA - EMERGENCY LIGHTS FROM SEATS 16G TO 22G ARE DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS SEATS 16G TO 22G. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060840](https://openairdocs.org/sdr/AALA20060840.md): Power Supply · inoperative · Sep 26, 2006 · N80052 · Airbus A300B4605R · Emergency Lighting
  > TUL - EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT NUMBER TWO DOORS INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT HAND NUMBER TWO DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20060012](https://openairdocs.org/sdr/AALA20060012.md): Connector · loose · Jan 8, 2006 · N80052 · Airbus A300B4605R · Light System Wiring
  > JFK - EMERGENCY LIGHT AT 36C INOPERATIVE. FOUND LOOSE CONNECTOR. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT 36C. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20030846](https://openairdocs.org/sdr/AALA20030846.md): O-Ring · cut · Aug 9, 2003 · N80052 · Airbus A300B4605R · Hydraulic Power System
  > AIRCRAFT LOST GREEN SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. FOUND GREEN SYSTEM PRESSURE LINE TO MANIFOLD O-RING CUT AND LEAKING. REPLACED O-RING AND BACK UP RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20012184](https://openairdocs.org/sdr/AALA20012184.md): Connector · loose · Dec 29, 2001 · N80052 · Airbus A300B4605R · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9G INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001572](https://openairdocs.org/sdr/AALA20001572.md): Bottle · discharged · Sep 18, 2000 · N80052 · Airbus A300B4605R · Passenger/Crew Doors
  > MIA - DURING OVERNIGHT CHECK, L1, L2, AND R1 DOOR ASSIST BOTTLES LOW PRESSURE. SERVICED BOTTLES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA20001189](https://openairdocs.org/sdr/AALA20001189.md): Connector · loose · Jul 19, 2000 · N80052 · Airbus A300B4605R · Emergency Lighting
  > TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT DOOR R2 INOPERATIVE. RECONNECTED CONNECTOR ON BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA20001083](https://openairdocs.org/sdr/AALA20001083.md): Bottle · discharged · Jun 29, 2000 · N80052 · Airbus A300B4605R · Emergency Equipment
  > JFK - DURING OVERNIGHT MAINTENANCE, R1 DOOR ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICED BOTTLE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991566](https://openairdocs.org/sdr/AALA991566.md): Support · corroded · Oct 18, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FLOOR SUPPORT AT FRAME 56 HAS CORROSION ON TOP SIDE. INSTALLED FLOOR SUPPORT SECTION PER SRM 53-10-15. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991565](https://openairdocs.org/sdr/AALA991565.md): Stringer · corroded · Oct 16, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 53R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991564](https://openairdocs.org/sdr/AALA991564.md): Stringer · corroded · Oct 16, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991563](https://openairdocs.org/sdr/AALA991563.md): Stringer · corroded · Oct 16, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991569](https://openairdocs.org/sdr/AALA991569.md): Stringer · corroded · Oct 13, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > TUL- STR 45R CORRODED - FRAME FITTING. REPLACED STRINGER AND FRAME FITTING PER SRM 53-17-18. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991590](https://openairdocs.org/sdr/AALA991590.md): Frame · corroded · Oct 12, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - CORROSION ON FRAME 58 BETWEEN STR 55L AND STR 55R. INSTALLED DOUBLER PER SRM 51-10-13. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991534](https://openairdocs.org/sdr/AALA991534.md): Splice · corroded · Oct 9, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON STRINGER SPLICE AT STR 57 AND AFT SIDE OF FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-14. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991533](https://openairdocs.org/sdr/AALA991533.md): Frame · corroded · Oct 7, 1999 · N80052 · Airbus A300B4605R · Fuselage Main, Frame
  > TUL - CORROSION ON FRAME BETWEEN STR 49L TO STR 49R. INSTALLED DOUBLER REPAIR PER SRM 53-10-13. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991532](https://openairdocs.org/sdr/AALA991532.md): Beam · corroded · Oct 7, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991531](https://openairdocs.org/sdr/AALA991531.md): Beam · corroded · Oct 7, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991512](https://openairdocs.org/sdr/AALA991512.md): Beam · corroded · Oct 6, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991518](https://openairdocs.org/sdr/AALA991518.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. STRAP REPAIR PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991517](https://openairdocs.org/sdr/AALA991517.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991516](https://openairdocs.org/sdr/AALA991516.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991515](https://openairdocs.org/sdr/AALA991515.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991514](https://openairdocs.org/sdr/AALA991514.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-74-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991513](https://openairdocs.org/sdr/AALA991513.md): Beam · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-29-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991511](https://openairdocs.org/sdr/AALA991511.md): Seat Track · corroded · Oct 5, 1999 · N80052 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - CORROSION BEYOND LIMITS. SECTION SPLICE PER SRM 53-10-16. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA991507](https://openairdocs.org/sdr/AALA991507.md): Beam · corroded · Oct 1, 1999 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
- [SDR AALA990932](https://openairdocs.org/sdr/AALA990932.md): Light · inoperative · Jun 23, 1999 · N80052 · Airbus A300B4605R · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ON FLOOR AT R4 AND L4 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT R4 AND L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990850](https://openairdocs.org/sdr/AALA990850.md): Wire · broken · Jun 4, 1999 · N80052 · Airbus A300B4605R · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON RIGHT SIDE OF EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA981713](https://openairdocs.org/sdr/AALA981713.md): Angle · cracked · Sep 21, 1998 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - EFO252X CALLS FOR INSPECTION OF RT FUSE WING ROOT PICKUP ANGLE FOR CRACKS. A.75 INCH CRACK RADIATING OUT OF FASTENER TO THE OUTBOARD EDGE OF THE FITTING WAS FOUND. REMOVED PICKUP ANGLE, HFEC ACCOMPLISHED. NO CRACKS FOUND, INSTALLED NEW ANGLE PER ECO
- [SDR AALA972168](https://openairdocs.org/sdr/AALA972168.md): Mount · corroded · Nov 14, 1997 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION BEYOND LIMITS UNDER L LAVATORY. REMOVED AND REPLACED TRACK SECTION PER SRM 51-72-10. (M)
- [SDR AALA971546](https://openairdocs.org/sdr/AALA971546.md): Support · corroded · Aug 15, 1997 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - SUPPORT TRAY FOR WATER TANK PERSS PUMP EXFOLIATED. MANUFACTURED NEW SUPPORT TRAY PER ESO 30595 DABED 8/6/97, TRAY INSTALLED ON E58 NR 0094616. (M)
- [SDR AALA971440](https://openairdocs.org/sdr/AALA971440.md): Sill · corroded · Aug 8, 1997 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FORWARD CARGO DOOR BEAM, TOP FLANGE HAS CORROSION TOP SURFACE PLACE AND FROM FRAME 20 TO 25A. INSTALLED DOUBLERS AND LEVEL BLEND PER ESO 30595 DATED 8/6/97. (M)
- [SDR AALA971439](https://openairdocs.org/sdr/AALA971439.md): Seat Track · corroded · Aug 7, 1997 · N80052 · Airbus A300B4605R · Fuselage, Seat/Cargo Attach Fittings
  > TUL - SEAT TRACK NR 8 HAS CORROSION AT FLOORBOARD LANDING AT FRAME 34. SPLICED IN SECTION OF SEAT TRACK FROM FRAME 33-35 PER FIG SRM 53-10-16-2 FIG 203. (M)
- [SDR AALA971429](https://openairdocs.org/sdr/AALA971429.md): Support · corroded · Aug 7, 1997 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON FLOOR SUPPORT NR 8 AT FRAME 74. REMOVED OLD FLOORBOARD SUPPORT FROM FRAME 73.5 THROUGH FRAME 75. MADE NEW PART PER AARD 51-10-3 INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-72-10-0. INSTALLED SPLICE AT FRAME 75 PER ESO3095. (M)
- [SDR AALA971428](https://openairdocs.org/sdr/AALA971428.md): Support · corroded · Aug 7, 1997 · N80052 · Airbus A300B4605R · Fuselage Miscellaneous Structure
  > TUL - FLOOR SUPPORT NR 4 IS CORRODED AT FRAME 74. REMOVED OLD SUPPORT FROM FRAME 73.5 THROUGH FRAME 75 MADE NEW PART PER AARD 51-10-3. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-72-10-0. INSTALLED SPLICE AT FRAME 75 PER E20 30595. (M)

Next page: https://openairdocs.org/deregistered/N80052-2011-08-19/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 = 'N80052' AND deregistration_id = 'N80052-2011-08-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N80052-2011-08-19/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
