# Service difficulty reports: N821AW

A list on [N821AW](https://openairdocs.org/aircraft/N821AW.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 5 · 223 reports

- [SDR AALA202608040164](https://openairdocs.org/sdr/AALA202608040164.md): Strap · out of position · Aug 1, 2026 · N821AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: 1R ARMING HANDLE POPS UP CAUSING THE SLIDE TO ARM AND DISARM UNTIL PLACED JUST RIGHT. MAINTENANCE FOUND SUPPORT STRAP OUT OF PLACE AND SECURED THE STRAP. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
- [SDR AALA202601301799](https://openairdocs.org/sdr/AALA202601301799.md): Girt Bar · sticking · Jan 29, 2026 · N821AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: AFT LEFT CABIN WILL NOT SECURE AND SLIDE WILL NOT ARM. MAINTENANCE CLEANED / LUBRICATED L2 DOOR SLIDE GIRT BAR AND ATTACH POINTS AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.
- [SDR AALA202503279222](https://openairdocs.org/sdr/AALA202503279222.md): Power Supply · no test · Mar 26, 2025 · N821AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: STEP 4 D OF J/C26L00025010 FAILS EMERGENCY LIGHTING SYSTEM TEST- RT MID CABIN POWER SUPPLY SHOWS FAIL. MAINTENANCE REAPLCAED EPSU IAM AMM 33-51-38.
- [SDR AALA202503271253](https://openairdocs.org/sdr/AALA202503271253.md): Power Supply · no test · Mar 26, 2025 · N821AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: STEP 4 D OF J/C26L00025010 FAILS TEST OF EMERGENCY LIGHTING SYSTEM TEST - FWD POWER SUPPLY SHOWS FAIL. MAINTENANCE REPLACED EPSU IAM AMM 33-51-38 CHECK GOOD A/C OK FOR SERVICE.
- [SDR AALA202407291360](https://openairdocs.org/sdr/AALA202407291360.md): Slide · deformed · Jul 26, 2024 · N821AW · Airbus A319132 · Escape Slide
  > AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ESCAPE SLIDE PACK ASSEMBLY IN PASSENGER CREW DOOR 842 AT AFT GALLEY AREA (THIS NR IS FOR TRACKING PURPOSE ONLY). REPLACED ESCAPE SLIDE PACK ASSEMBLY IN PASSENGER CREW DOOR 842 AT AFT GALLEY AREA.
- [SDR AALA202407293169](https://openairdocs.org/sdr/AALA202407293169.md): Slide · deformed · Jul 26, 2024 · N821AW · Airbus A319132 · Escape Slide
  > AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ESCAPE SLIDE PACK ASSEMBLY IN PASSENGER CREW DOOR 841 AT FWD GALLEY AREA (THIS NR IS FOR TRACKING PURPOSE ONLY). REPLACED ESCAPE SLIDE PACK ASSEMBLY IN PASSENGER CREW DOOR 841 AT FWD GALLEY AREA (THIS NR IS FOR TRA
- [SDR AALA202407293445](https://openairdocs.org/sdr/AALA202407293445.md): Slide · deformed · Jul 26, 2024 · N821AW · Airbus A319132 · Escape Slide
  > AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION ESCAPE SLIDE PACK ASSEMBLY IN PASSENGER CREW DOOR 831 (THIS NR IS FOR TRACKING PURPOSE ONLY). SLIDE, ESCAPE F OFF 26-2561-9-0007 9057 ON 26-2561-9-0007 8315.
- [SDR AALA202408050652](https://openairdocs.org/sdr/AALA202408050652.md): Damper · no test · Jul 16, 2024 · N821AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS IN BASE MAINTENANCE: DID NOT PASS DAMPING TEST FUNCTION DOOR DAMPER IN PASSENGER CREW DOOR 841 IN FORWARD GALLEY AREA. REPLACED DOOR DAMPER IN PASSENGER CREW DOOR 841 PER AMM 52-11-14-000-001-B.
- [SDR AALA202407166258](https://openairdocs.org/sdr/AALA202407166258.md): Bolt · corroded · Jul 15, 2024 · N821AW · Airbus A319132 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADIING EDGE SLAT TRACK #12 LOWER AFT BOLT BETWEEN WS 13464 AND WS 14459, BETWEEN RIBS 25 AND 27. REPLACED BOLT PER AMM 27-84-67-400-002-A AND TASK CARD 26C61057005.
- [SDR AALA202407166529](https://openairdocs.org/sdr/AALA202407166529.md): Bolt · corroded · Jul 10, 2024 · N821AW · Airbus A319132 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #4 LOWER BOLT BETWEEN RIBS 5 AND 6. REPLACED BOLT PER TASK CARD 26C51057005 AND AMM 27-84-63-400-002.
- [SDR AALA202407168164](https://openairdocs.org/sdr/AALA202407168164.md): Fitting · corroded · Jun 29, 2024 · N821AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.
- [SDR AALA202407168714](https://openairdocs.org/sdr/AALA202407168714.md): Fitting · corroded · Jun 29, 2024 · N821AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.
- [SDR AALA202408166513](https://openairdocs.org/sdr/AALA202408166513.md): Fitting · none · Jun 25, 2024 · N821AW · Airbus A319132 · Standard Practices/Structures
  > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 4 AT Y0 REQUIRES REPLACEMENT DUE TO THE MAJOR REPAIIR BEING ACCOMPLISHED PER EA 355317. REPLACED CONTINUITY FITTING PER EA 355317.
- [SDR AALA202407297421](https://openairdocs.org/sdr/AALA202407297421.md): Hinge Fitting · cracked · Jun 25, 2024 · N821AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON KEEL BEAM AFT LUG CRACKED AT FR 42 AND S41R. REPLACED HINGE FITTING PER EA 355864.
- [SDR AALA202407299069](https://openairdocs.org/sdr/AALA202407299069.md): Hinge Fitting · cracked · Jun 25, 2024 · N821AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON KEEL BEAM AFT LUG CRACKED AT FR 42 AND S41L. REPLACED HINGE FITTING PER EA 355883.
- [SDR AALA202407019135](https://openairdocs.org/sdr/AALA202407019135.md): Hinge Fitting · excess play · Jun 25, 2024 · N821AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER, ELEVATOR #2 HINGE ARMBEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202407010348](https://openairdocs.org/sdr/AALA202407010348.md): Hinge Fitting · excess play · Jun 25, 2024 · N821AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER, ELEVATOR #1 HINGE ARMBEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202407018737](https://openairdocs.org/sdr/AALA202407018737.md): Hinge Fitting · excess play · Jun 25, 2024 · N821AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER, ELEVATOR #3 HINGE ARMBEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202407197545](https://openairdocs.org/sdr/AALA202407197545.md): Fitting · corroded · Jun 24, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING IN LOWER SILL AT FR 66 AND S23R. REPLACED CORNER FITTING PER SRM 51-42-11.
- [SDR AALA202408142799](https://openairdocs.org/sdr/AALA202408142799.md): Window Frame · cracked · Jun 22, 2024 · N821AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD RIGHT HAND LATERAL FRAME RIGHT AT FR 4 AND Y0. REPLACED WINDSHIELD FRAME PER EA 355670
- [SDR AALA202408144392](https://openairdocs.org/sdr/AALA202408144392.md): Window Frame · cracked · Jun 22, 2024 · N821AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD LEFT HAND LATERAL FRAME RIGHT AT FR 4 AND Y0. REPLACED WINDSHIELD FRAME PER EA 355669.
- [SDR AALA202407024325](https://openairdocs.org/sdr/AALA202407024325.md): Fitting · corroded · Jun 18, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD RIGHT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202406276511](https://openairdocs.org/sdr/AALA202406276511.md): Fitting · corroded · Jun 18, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD LEFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 16 AND FR 20 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202407167716](https://openairdocs.org/sdr/AALA202407167716.md): Floor Support · corroded · Jun 15, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FORWARD GALLEY BETWEEN FR 20 AND FR 24 AND -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.
- [SDR AALA202407124384](https://openairdocs.org/sdr/AALA202407124384.md): Seat Track · corroded · Jun 15, 2024 · N821AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA FLOOR SUPPORT/SEAT TRACK BETWEEN FR 12 AND FR 24 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.
- [SDR AALA202407017276](https://openairdocs.org/sdr/AALA202407017276.md): Seat Track · corroded · Jun 15, 2024 · N821AW · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA SEAT TRACK BETWEEN FR 20 AND FR 21 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.
- [SDR AALA202408135321](https://openairdocs.org/sdr/AALA202408135321.md): Shear Plate · cracked · Jun 14, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY AREA SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202408096089](https://openairdocs.org/sdr/AALA202408096089.md): Shear Plate · cracked · Jun 14, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY AREA FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202407190840](https://openairdocs.org/sdr/AALA202407190840.md): Support · corroded · Jun 14, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT STR 23R LOCATED BETWEEN FR 66 AND FR 68 IN AFT GALLEY AREA. REPLACED LOWER SILL PER SRM 51-42-11-801.
- [SDR AALA202406252213](https://openairdocs.org/sdr/AALA202406252213.md): Floorbeam · corroded · Jun 14, 2024 · N821AW · Airbus A319132 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM SPLICE / SECTION-CONNECTING AT FR 68 AND -Y1162. REPLACED SPLICE / SECTION-CONNECTING PER SRM 51-42-11.
- [SDR AALA202407117001](https://openairdocs.org/sdr/AALA202407117001.md): Intercostal · cracked · Jun 13, 2024 · N821AW · Airbus A319132 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING LOWER INBOARD HOLE AT FR 16 LEFT AND DOOR STOP FITTING #1. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
- [SDR AALA202408204860](https://openairdocs.org/sdr/AALA202408204860.md): Window Frame · cracked · Jun 12, 2024 · N821AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD LEFT HAND FRAMING ON UPPER RADIUS OF WINDSHIELD CENTER POST INTERNAL LOWER ATTACHMENT AREA BETWEEN FR 3 AND FR 5 AT Y0 LEFT. REPLACED FRAME PER EA 355317.
- [SDR AALA202408205859](https://openairdocs.org/sdr/AALA202408205859.md): Window Frame · cracked · Jun 12, 2024 · N821AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD RIGHT HAND FRAMING ON UPPER RADIUS OF WINDSHIELD CENTER POST INTERNAL LOWER ATTACHMENT AREA AND THE LOWER CORNER RADIUS BETWEEN FR 3 AND FR 5 AT Y0 RIGHT REPLACED FRAME PER EA 355317.
- [SDR AALA202408169937](https://openairdocs.org/sdr/AALA202408169937.md): Fitting · none · Jun 12, 2024 · N821AW · Airbus A319132 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 4 AT Y0. REPLACED CONTINUITY FITTING PER EA 355317.
- [SDR AALA202407017555](https://openairdocs.org/sdr/AALA202407017555.md): Skin · debonded · Jun 10, 2024 · N821AW · Airbus A319132 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING FLAP REPAIR DOUBLER DEBONDED BETWEEN FLAP RIBS 11 AND 13. REPAIRED FLAP PER SRM 57-53-00-300-119
- [SDR AALA202408062954](https://openairdocs.org/sdr/AALA202408062954.md): Fork · worn · May 15, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED RIGHT HAND LATERAL FORK END FITTING PER EA 355510A.
- [SDR AALA202408060157](https://openairdocs.org/sdr/AALA202408060157.md): Fork · worn · May 15, 2024 · N821AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 355510A.
- [SDR AALA202404191716](https://openairdocs.org/sdr/AALA202404191716.md): Wire · broken · Apr 17, 2024 · N821AW · Airbus A319132 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: SEAT 20 AND 21 EMERGENCY LIGHTS ARE INOP. FOUND WIRES BROKEN AT WALL CONNECTOR AT ROW 20. RE-TERMINATED IAW AWM 33-51-08. OPS CHECK GOOD IAW AMM 31-51-00-710-007
- [SDR AALA202402075771](https://openairdocs.org/sdr/AALA202402075771.md): Engine · leaking · Jan 24, 2024 · N821AW · Airbus A319132 · Turbine Engine Oil System
  > AIRCRAFT WAS GROUNDED: IN DESCENT LEVEL FL 130, FLIGHT ATTENDANT CALLED ABOUT DIRTY SOCK SMELL ENTIRE AIRCRAFT. WAS SMELL WAS ALSO IN THE FLIGHT DECK AND LASTED UNTIL DEPLANING ABOUT 30 MINUTES. **SUPPLEMENTAL REPORT FOR AALA202401265771: MAINTENANCE FOUND EVI
- [SDR AALA202401265771](https://openairdocs.org/sdr/AALA202401265771.md): Unknown · odor · Jan 24, 2024 · N821AW · Airbus A319132 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: IN DESCENT LEVEL FL 130, FLIGHT ATTENDANT CALLED ABOUT DIRTY SOCK SMELL ENTIRE AIRCRAFT. WAS SMELL WAS ALSO IN THE FLIGHT DECK AND LASTED UNTIL DEPLANING ABOUT 30 MINUTES. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
- [SDR AALA202401048243](https://openairdocs.org/sdr/AALA202401048243.md): Servo Valve · leaking · Dec 18, 2023 · N821AW · Airbus A319132 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: ON FINAL FLIGHT ATTENDANTS REPORTED BAD DIRTY SOCK SMELL THROUGHOUT CABIN. **SUPPLEMENTAL REPORT FOR AALA202312208243: MAINTENANCE FOUND THE RIGHT HAND MAIN LANDING GEAR NORMAL BRAKE SERVO VALVE LEAKING HYDRAULIC FLUID IN THE WHEEL WELL
- [SDR AALA202312208243](https://openairdocs.org/sdr/AALA202312208243.md): Unknown · unknown · Dec 18, 2023 · N821AW · Airbus A319132 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: ON FINAL FLIGHT ATTENDANTS REPORTED BAD DIRTY SOCK SMELL THROUGHOUT CABIN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
- [SDR AALA202312052371](https://openairdocs.org/sdr/AALA202312052371.md): Connector · inoperative · Dec 4, 2023 · N821AW · Airbus A319132 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: ROW 20 AND 21 WHITE EMERGENCY EXIT LIGHTS ON CENTER AISLE SEATS INOPERATIVE. MAINTENANCE RESEATED CANNON PLUG IAW AMM 20-27-00 AND 33-51-19.
- [SDR AALA202310266009](https://openairdocs.org/sdr/AALA202310266009.md): Control Lever · inoperative · Oct 24, 2023 · N821AW · Airbus A319132 · Landing Gear Selector
  > AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO PHL. ON TAKEOFF GEAR WOULD NOT RETRACT HANDLE WOULD NOT MOVE IN UP POSITION. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER PER AMM 32-31-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202308224456](https://openairdocs.org/sdr/AALA202308224456.md): Engine · stalled · Aug 16, 2023 · N821AW · Airbus A319132 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MEM. AT CRUISE FLIGHT CREW REPORTED A ENGINE #2 COMPRESSOR VANE ECAM MESSAGE. WHILE THE FLIGHT CREW WAS ACCOMPLISHING THE ECAM / QRH PROCEDURES THE #2 ENGINE STALLED AND WENT TO IDLE
- [SDR AALA202308184456](https://openairdocs.org/sdr/AALA202308184456.md): Engine · stalled · Aug 16, 2023 · N821AW · Airbus A319132 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND TEH AIRCRAFT RETURNED TO MEM. AT CRUISE FLIGHT CREW REPORTED A ENGINE #2 COMPRESSOR VANE ECAM MESSAGE. WHILE THE FLIGHT CREW WAS ACCOMPLISHING THE ECAM / QRH PROCEDURES THE #2 ENGINE STALLED AND WENT TO IDLE
- [SDR AALA202308035151](https://openairdocs.org/sdr/AALA202308035151.md): Brake · worn · Jun 16, 2023 · N821AW · Airbus A319132 · Landing Gear Brake System
  > AIRCRAFT WAS GROUNDED: THE AIRCRAFT DIVERTED TO DFW. HOT BRAKES AFTER TAKE OFF, CREW CYLCED THE GEAR PER THE QRH AND NOTED THAT THE GEAR WOULD NOT RETRACT AND HAD MULTIPLE ECAM MESSAGES FOR HOT BRAKES, LANDING GEAR DOORS NOT CLOSED, LANDING GEAR NOT UPLOCKED A
- [SDR AALA202308038893](https://openairdocs.org/sdr/AALA202308038893.md): Bolt · worn · Jun 16, 2023 · N821AW · Airbus A319132 · Landing Gear System
  > AIRCRAFT WAS GROUNDED: THE AIRCRAFT DIVERTED TO DFW. HOT BRAKES AFTER TAKE OFF, CREW CYLCED THE GEAR PER THE QRH AND NOTED THAT THE GEAR WOULD NOT RETRACT AND HAD MULTIPLE ECAM MESSAGES FOR HOT BRAKES, LANDING GEAR DOORS NOT CLOSED, LANDING GEAR NOT UPLOCKED A
- [SDR AALA202306195151](https://openairdocs.org/sdr/AALA202306195151.md): Unknown · unknown · Jun 16, 2023 · N821AW · Airbus A319132 · Landing Gear System
  > AIRCRAFT WAS GROUNDED: THE AIRCRAFT DIVERTED TO DFW. HOT BRAKES AFTER TAKE OFF, CREW CYLCED THE GEAR PER THE QRH AND NOTED THAT THE GEAR WOULD NOT RETRACT AND HAD MULTIPLE ECAM MESSAGES FOR HOT BRAKES, LANDING GEAR DOORS NOT CLOSED, LANDING GEAR NOT UPLOCKED A
- [SDR AALA202305120299](https://openairdocs.org/sdr/AALA202305120299.md): Wire · broken · May 9, 2023 · N821AW · Airbus A319132 · Door System Wiring
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR INDICATION ON ECAM SHOWS OPEN WHEN CLOSED AND LOCKED. MAINTENANCE FOUND WIRE 3154-1496 BROKEN BEHIND PROXIMITY SWITCH CONNECTOR 11WV1A AND REPAIRED IT PER ESPM 20-53-21.

Next page: https://openairdocs.org/aircraft/N821AW/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 = 'N821AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N821AW/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.