# Service difficulty reports: N820AW

A list on [N820AW](https://openairdocs.org/aircraft/N820AW.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 7 · 347 reports

- [SDR 2026F00202](https://openairdocs.org/sdr/2026F00202.md): Snap Ring · corroded · Sep 11, 2026 · N820AW · Airbus A319132 · Engine (Turbine/Turboprop)
  > DURING INSPECTION, FOUND SNAP RINGS THAT RETAIN THE BEARINGS FOR THE ENGINE VSV (VARIABLE STATOR VANE) ACTUATION CRANKSHAFT TO BE CORRODED. UPON GENERATING A NON ROUTINE, & DEALING WITH PARTS SOURCING DIFFICULTY. UPON LOOKING AS THE SNAP RINGS ON DIFFERENT EN
- [SDR AALA202609021839](https://openairdocs.org/sdr/AALA202609021839.md): Light · inoperative · Aug 30, 2026 · N820AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT AT SEAT ROW 21ABC INOPERATIVE - MAINTENANCE REPLACED THE EMERGENCY LIGHT AT SEAT ROW 21ABC PER EA 378583 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED
- [SDR AALA202608172166](https://openairdocs.org/sdr/AALA202608172166.md): Life Vest · damaged · Aug 15, 2026 · N820AW · Airbus A319132 · Life Jacket
  > AIRCRAFT WAS NOT GROUNDED: FALIGHT ATTENDANT REPORTS ONE CREW LIFE VEST IS MOLDY - MAINTENANCE REPLACED THE LIFE VES PER AMM 25-66-52
- [SDR AALA202606128974](https://openairdocs.org/sdr/AALA202606128974.md): Indicator · out of position · Jun 9, 2026 · N820AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: 2R DOOR ARMED/DISARMED VIEWER WINDOW INDICATOR INOPERATIVE. DOES NOT SWITCH INDICATION WITH THE ARM/DISARMING LEVEL SELECTION. MAINTENANCE FOUND DOOR LOCK/ UNLOCKED PLACARD CROOKED AND ADJUSTED / SECURED DOOR LOCK UNLOCKED PACARD PER AMM
- [SDR AALA202605276133](https://openairdocs.org/sdr/AALA202605276133.md): Power Supply · no test · May 25, 2026 · N820AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: DURING CARD 26L00025010 FOUND AFT EPSU BATTERY FAIL TEST. MAINTENANCE REPLACED EPSU BATTERY WITH SERVICEABLE. OPERATIONAL TEST PERFORMED, NO DEFECT NOTED REF AMM 33-51-38.
- [SDR AALA202605189434](https://openairdocs.org/sdr/AALA202605189434.md): Bottle · low pressure · May 17, 2026 · N820AW · Airbus A319132 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: RH FWD DOOR DAMPER PRESSURE 1750 AT 80 DEGREES F. MAINTENANCE SERVICED DOOR DAMPER IAW WORK CARD 26L80052001.
- [SDR AALA202605188561](https://openairdocs.org/sdr/AALA202605188561.md): Bottle · reads low · May 17, 2026 · N820AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: LH AFT DOOR DAMPER PRESSURE 1550 AT 80 DEGREES F. MAINTENANCE SERVICED DOOR DAMPER IAW WORK CARD 26L80052001.
- [SDR AALA202605185195](https://openairdocs.org/sdr/AALA202605185195.md): Bottle · low pressure · May 17, 2026 · N820AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: LH FWD DOOR DAMPER PRESSURE 1750 AT 80 DEGREES F. MAINTENANCE SERVICED DOOR DAMPER IAW WORK CARD 26L80052001.
- [SDR AALA202605182482](https://openairdocs.org/sdr/AALA202605182482.md): Bottle · low pressure · May 17, 2026 · N820AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: RH AFT DOOR DAMPER PRESSURE 1750 AT 80 DEGREES F. MAINTENANCE SERVICED DOOR DAMPER IAW WORK CARD 26L80052001.
- [SDR AALA202506052457](https://openairdocs.org/sdr/AALA202506052457.md): Flashlight · inoperative · Jun 2, 2025 · N820AW · Airbus A319132 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FA FWD JUMPSEAT FLASHLIGHT NOT BLINKING AND TAMPER SEAL BROKEN. MAINTENANCE REPLACED FA FWD JUMPSEAT FLASHLIGHT AND TAMPER SEAL REF AMM 25-22-00.
- [SDR AALA202505151829](https://openairdocs.org/sdr/AALA202505151829.md): First Aid Kit · cracked · May 13, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH IAW EA 362868.
- [SDR AALA202505159297](https://openairdocs.org/sdr/AALA202505159297.md): Fitting · cracked · May 11, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE RH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE RH
- [SDR AALA202505157492](https://openairdocs.org/sdr/AALA202505157492.md): Window Frame · cracked · May 11, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.190 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT ARE
- [SDR AALA202505150471](https://openairdocs.org/sdr/AALA202505150471.md): Window Frame · cracked · May 11, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA 27 INTERNAL SIDE LH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE L
- [SDR AALA202505159917](https://openairdocs.org/sdr/AALA202505159917.md): Frame · cracked · May 7, 2025 · N820AW · Airbus A319132 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN RADIUS OF AFT UPPER CORNER BTW STR 8 AND STR 9 LH SIDE FROM FR68 WEB DOOR FRAME. CRACK LENGTH 0.563 INCH. MAINTENANCE PERFORMED INTERIM REPAIR INSTRUCTIONS ON RADIUS OF AFT UPPER CORNER BTW STR8 AND STR9
- [SDR AALA202505139917](https://openairdocs.org/sdr/AALA202505139917.md): Frame · cracked · May 7, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN RADIUS OF AFT UPPER CORNER BTW STR 8 AND STR 9 LH SIDE FROM FR68 WEB DOOR FRAME. CRACK LENGTH 0.563 INCH. MAINTENANCE PERFORMED INTERIM REPAIR INSTRUCTIONS ON RADIUS OF AFT UPPER CORNER BTW STR8 AND STR9
- [SDR AALA202505099754](https://openairdocs.org/sdr/AALA202505099754.md): Shear Plate · cracked · May 6, 2025 · N820AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA. MAINTENANCE REPLACED SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-72-11-911-001 AND DWG D53474180.
- [SDR AALA202505096191](https://openairdocs.org/sdr/AALA202505096191.md): Attach Fitting · cracked · Apr 22, 2025 · N820AW · Airbus A319132 · Fuselage, Landing Gear Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FWD ATTACHMENT HINGE FITTINGS AFT LUG POSITION ON LH MAIN LANDING GEAR, CRACK LENGTH IS: 0.200 INCH APPROX. MAINTENANCE REPLACED FWD ATTACHMENT HINGE FITTING AFT LUG POSITION ON LH MAIN LANDING GEAR DOOR AND CO
- [SDR AALA202505097557](https://openairdocs.org/sdr/AALA202505097557.md): Hinge Fitting · cracked · Apr 22, 2025 · N820AW · Airbus A319132 · Fuselage, Landing Gear Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FWD ATTACHMENT AFT LUG POSITION ON RH MAIN LANDING GEAR, CRACK LENGTH IS: 0.250 INCH APROX. MAINTENANCE REPLACED FWD ATTACH FITTING AFT LUG POSITION ON RH MAIN LANDING GEAR DOOR AND CONNECTING PLATE AND FASTENE
- [SDR AALA202504243814](https://openairdocs.org/sdr/AALA202504243814.md): Structure · cracked · Apr 17, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON THE UPPER CORNER FROM HOLE LOCATED AT FR 68 AND BELOW S-8L. MAINTNANCE REPLACED UPPER CORNER LOCATED AT FR68 LH AT LEVEL STR 8L IAW A319 SRM 51-42-11-801 AND DWG D53480505.
- [SDR AALA202504144719](https://openairdocs.org/sdr/AALA202504144719.md): Frame · cracked · Apr 13, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK UPPER CORNER FRAME 68 RH SIDE AT AFT GALLEY AREA. LENGTH 0.200 INCHES. MAINTENANCE REPLACED UPPER CONER LOCATED FRAME 68 RH SIDE AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911-011 AND DWG D53480505.
- [SDR AALA202504246500](https://openairdocs.org/sdr/AALA202504246500.md): Stringer · corroded · Apr 8, 2025 · N820AW · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION STR 31 RH SIDE AT LEVEL FR65 ON AFT BULK CARGO COMPARTMENT. MEASURES OF CORROSION IS: L= 3.591 IN, W= 0.871 IN. MAINTENANCE REPLACED SECTION STRINGER LOCATED STR 31R FR64 TO FR67 ON AFT BULK CARGO COMPARTMENT IAW A319 SR
- [SDR AALA202505151489](https://openairdocs.org/sdr/AALA202505151489.md): Support · corroded · Apr 7, 2025 · N820AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL FR 66 AT LEVEL STR 23R AT AFT GALLEY AREA. MAINTENANCE REPLACED LOWER SILL LOC BTW FR66 TO FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, DWG D53474250 AND DWG D53480019.
- [SDR AALA202504070960](https://openairdocs.org/sdr/AALA202504070960.md): Fitting · corroded · Apr 2, 2025 · N820AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. MAINTENANCE REPLACED SERVICEABLE LOWER SPIGOT FITTING RECEPTACLE ON LH PYLON IAW A319 SRM 54-51-12-300-002.
- [SDR AALA202504032699](https://openairdocs.org/sdr/AALA202504032699.md): Bottle · no test · Apr 2, 2025 · N820AW · Airbus A319132 · Service Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER P/NON: FE240-006 S/N ON: RFM29378 IN PASSENGER CREW
- [SDR AALA202504048150](https://openairdocs.org/sdr/AALA202504048150.md): Structure · cracked · Mar 31, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR 66 LEVEL STR23R AT AFT GALLEY AREA. MAINTENANCE REPLACED INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL 23R AT AFT GALLEY AREA IAW A319 SRM 51-72-11-801 AND DWG D534
- [SDR AALA202504041620](https://openairdocs.org/sdr/AALA202504041620.md): Structure · cracked · Mar 14, 2025 · N820AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED AT LEVEL STR23L FR66 AT AFT GALLEY AREA.,MEASURE OF CRACK IS: L=0.250 INCH. MAINTENANCE REPLACED INTERNAL STRUCTURE SECTION CONNECTION LOCATED AT LEVEL STR23L FR66 AT AFT GALLE
- [SDR AALA202504011011](https://openairdocs.org/sdr/AALA202504011011.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503311738](https://openairdocs.org/sdr/AALA202503311738.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 6 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503313209](https://openairdocs.org/sdr/AALA202503313209.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 4 ON RH HORIZONTALSTABILIZER (1EA). MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503310862](https://openairdocs.org/sdr/AALA202503310862.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 3 ON RH HORIZONTALSTABILIZER (1EA). MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503314761](https://openairdocs.org/sdr/AALA202503314761.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 1 ON RH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503310504](https://openairdocs.org/sdr/AALA202503310504.md): Hinge Fitting · excess play · Mar 13, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 54-16-42-400-001-A.
- [SDR AALA202503244207](https://openairdocs.org/sdr/AALA202503244207.md): Plate · cracked · Mar 12, 2025 · N820AW · Airbus A319132 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 844 HATCH CONTROL HANDLE PLATE CRACKED. REPLACED CONTROL HANDLE PLATE PER AMM 52-21-11.
- [SDR AALA202503249221](https://openairdocs.org/sdr/AALA202503249221.md): Plate · cracked · Mar 12, 2025 · N820AW · Airbus A319132 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 834 HATCH CONTROL HANDLE PLATE CRACKED. REPLACED CONTROL HANDLE PLATE PER AMM 52-21-11.
- [SDR AALA202504032923](https://openairdocs.org/sdr/AALA202504032923.md): Hinge Fitting · excess play · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 END FITTING ON LH HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 6 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504037433](https://openairdocs.org/sdr/AALA202504037433.md): Hinge Fitting · excess play · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 END FITTING ON LH HORIZONTAL STABILIZER). MAINTENANCE REPLACED ELEVATOR HINGE ARM 5 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504032512](https://openairdocs.org/sdr/AALA202504032512.md): Hinge Fitting · excess play · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 4 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504032696](https://openairdocs.org/sdr/AALA202504032696.md): Hinge Fitting · inoperative · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 3 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504035184](https://openairdocs.org/sdr/AALA202504035184.md): Hinge Fitting · excess play · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504033975](https://openairdocs.org/sdr/AALA202504033975.md): Hinge Fitting · excess play · Mar 11, 2025 · N820AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 END FITTING ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 1 END FITTING ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202409309296](https://openairdocs.org/sdr/AALA202409309296.md): Battery · inoperative · Sep 29, 2024 · N820AW · Airbus A319132 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FWD FA JUMP SEAT FLASHLIGHT'S RED LIGHT NOT BLINKING. REPLACED BATTERY FWD F/A FLASHLIGHT. SECURED AND OPS NORMAL.
- [SDR AALA202409198178](https://openairdocs.org/sdr/AALA202409198178.md): Light · inoperative · Sep 18, 2024 · N820AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: 2L DOOR EXIT SIGN PLACARD DOES NOT LIGHT UP. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY AT L2 DOOR AND WALL MOUNT ASSEMBLY AT RH SIDE OVERWING EXIT AS REQUIRED.
- [SDR AALA202408221875](https://openairdocs.org/sdr/AALA202408221875.md): Power Supply · faulted · Aug 21, 2024 · N820AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FOUND EMERERGENCY SYSTEM EMERGENCY POWER SUPPLY UNIT ON THE FORWARD LEFT WITH A FAULT 33-51-38 WHILE PREPARING FOR OVER-WING SLIDE REPLACEMENT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.
- [SDR AALA202408142686](https://openairdocs.org/sdr/AALA202408142686.md): Oven · odor · Jul 25, 2024 · N820AW · Airbus A319132 · Buffet/Galleys
  > AIRCRAFT WAS NOT GROUNDED: OVEN IN FIRST CLASS GALLEY HAS FOUL ODOR WHEN USED AS FOOD WAS LEFT IN IT WHILE AIRCRAFT WAS DOWN FOR MAINTENANCE AND HAD SPOILED. **SUPPLEMENTAL REPORT FOR AALA202407292686: MAINTENANCE CLEANED OVEN IN FIRST CLASS AND ACCOMPLISHED
- [SDR AALA202407292686](https://openairdocs.org/sdr/AALA202407292686.md): Oven · odor · Jul 25, 2024 · N820AW · Airbus A319132 · Buffet/Galleys
  > AIRCRAFT WAS NOT GROUNDED: OVEN IN FIRST CLASS GALLEY HAS FOUL ODOR WHEN USED AS FOOD WAS LEFT IN IT WHILE AIRCRAFT WAS DOWN FOR MAINTENANCE AND HAD SPOILED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
- [SDR AALA202407261665](https://openairdocs.org/sdr/AALA202407261665.md): Hydraulic Line · ruptured · Jul 13, 2024 · N820AW · Airbus A319132 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THE LOSS OF THE GREEN HYDRAUILIC SYSTEM QUANTITY SHORTLY AFTER DEPARTURE. THE AIRCRAFT LANDED SAFELY AT PHL WITHOUT FURTHER INCIDENT. **SUPPLEMEN
- [SDR AALA202407151665](https://openairdocs.org/sdr/AALA202407151665.md): Hydraulic System · failed · Jul 13, 2024 · N820AW · Airbus A319132 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHL DUE TO THE FLIGHT CREW REPORTING THE LOSS OF THE GREEN HYDRAUILIC SYSTEM QUANTITY SHORTLY AFTER DEPARTURE. THE AIRCRAFT LANDED SAFELY AT PHL WITHOUT FURTHER INCIDENT. (OPEN)
- [SDR AALA202405282711](https://openairdocs.org/sdr/AALA202405282711.md): Reservoir · overserviced · May 26, 2024 · N820AW · Airbus A319132 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE THE FLIGHT CREW REPORTING A YELLOW HYDRAULIC RESERVOIR LOW LEVEL MESSAGE. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE
- [SDR AALA202405024767](https://openairdocs.org/sdr/AALA202405024767.md): Cylinder · low pressure · May 2, 2024 · N820AW · Airbus A319132 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR EMERGENCY CYLINDER LOW PRESSURE, 950 PSI 73F. SERVICED L4 DOOR CYLINDER BOTTLE

Next page: https://openairdocs.org/aircraft/N820AW/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 = 'N820AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N820AW/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.