# Service difficulty reports: N580UW

A list on [N580UW](https://openairdocs.org/aircraft/N580UW.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 3 · 118 reports

- [SDR AALA202609026179](https://openairdocs.org/sdr/AALA202609026179.md): Elec Connector · disconnected · Aug 31, 2026 · N580UW · Airbus A321231 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: SEAT 21ABC WHITE SEAT MOUNTED EMERGENCY AISLE LIGHT DOES NOT TURN ON - MAINTENANCE FOUND CONNECTOR UNPLUGGED FOR SEAT 21ABC MOUNTED EMERGENCY AISLE LIGHT AND RECONNECTED IT - A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO
- [SDR AALA202609022638](https://openairdocs.org/sdr/AALA202609022638.md): Elec Connector · not seated · Aug 31, 2026 · N580UW · Airbus A321231 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: SEAT 22ABC WHITE SEAT MOUNTED EMERGENCY AISLE LIGHT DOES NOT TURN ON - MAINTENANCE FOUND CONNECTOR NOT FULLY SEATED FOR SEAT 22ABC MOUNTED EMERGENCY AISLE LIGHT AND RECONNECTED IT - A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED W
- [SDR AALA202606103920](https://openairdocs.org/sdr/AALA202606103920.md): Diaphragm · leaking · Jun 6, 2026 · N580UW · Airbus A321231 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: 4R DOOR ASSIST BOTTLE PRESSURE LOW, MAINTENANCE REPLACED THE DIAPHRAGM FOR THE PERCUSSION ASSEMBLY OF THE 4R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER CMM 52-11-03.
- [SDR AALA202606104589](https://openairdocs.org/sdr/AALA202606104589.md): Bottle · low pressure · Jun 6, 2026 · N580UW · Airbus A321231 · Service Doors
  > AIRCRAFT WAS GROUNDED: CHECK DOOR PRESSURE 4R MESSAGE ON CIDS PANEL. MAINTENANCE SERVICED 4R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM.52-10-00.
- [SDR AALA202606051678](https://openairdocs.org/sdr/AALA202606051678.md): Bottle · low pressure · Jun 4, 2026 · N580UW · Airbus A321231 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: DOOR 4R LOW PRESSURE MESSAGE AFTER ARMING SLIDE. MAINTENANCE SERVICED THE 4R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202605261519](https://openairdocs.org/sdr/AALA202605261519.md): Battery · no test · May 23, 2026 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 14WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 14WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.
- [SDR AALA202605267312](https://openairdocs.org/sdr/AALA202605267312.md): Battery · no test · May 23, 2026 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 10WL BATTERY FAULT DISPLAYED DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.
- [SDR AALA202602257222](https://openairdocs.org/sdr/AALA202602257222.md): Bottle · no test · Feb 24, 2026 · N580UW · Airbus A321231 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: R4 PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DAMPING FUNCTION TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.
- [SDR AALA202602055379](https://openairdocs.org/sdr/AALA202602055379.md): Hinge Fitting · excess play · Jan 30, 2026 · N580UW · Airbus A321231 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601280887](https://openairdocs.org/sdr/AALA202601280887.md): Hinge Fitting · excess play · Jan 27, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202602094460](https://openairdocs.org/sdr/AALA202602094460.md): Fitting · corroded · Jan 25, 2026 · N580UW · Airbus A321231 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.
- [SDR AALA202602025510](https://openairdocs.org/sdr/AALA202602025510.md): Fitting · corroded · Jan 24, 2026 · N580UW · Airbus A321231 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202601273300](https://openairdocs.org/sdr/AALA202601273300.md): Hinge Fitting · excess play · Jan 24, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601274524](https://openairdocs.org/sdr/AALA202601274524.md): Hinge Fitting · excess play · Jan 24, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601276602](https://openairdocs.org/sdr/AALA202601276602.md): Hinge Fitting · excess play · Jan 24, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202602238520](https://openairdocs.org/sdr/AALA202602238520.md): Shear Plate · cracked · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202602132889](https://openairdocs.org/sdr/AALA202602132889.md): Shear Plate · cracked · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L, REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202602096744](https://openairdocs.org/sdr/AALA202602096744.md): Door Sill · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 67 AND S23R. REPLACED LOWER SILL PER SRM 51-72-11.
- [SDR AALA202602095649](https://openairdocs.org/sdr/AALA202602095649.md): Seat Track · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN SEAT TRACK AT FR 66 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.
- [SDR AALA202602068804](https://openairdocs.org/sdr/AALA202602068804.md): Beam · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y1162. REPLACED BEAM PER SRM 51-72-11.
- [SDR AALA202602058399](https://openairdocs.org/sdr/AALA202602058399.md): Floorbeam · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND -Y765. REPLACED BEAM PER SRM 51-42-11.
- [SDR AALA202602031346](https://openairdocs.org/sdr/AALA202602031346.md): Fitting · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202602026744](https://openairdocs.org/sdr/AALA202602026744.md): Door Sill · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-72-11.
- [SDR AALA202602023929](https://openairdocs.org/sdr/AALA202602023929.md): Fitting · corroded · Jan 20, 2026 · N580UW · Airbus A321231 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202602025870](https://openairdocs.org/sdr/AALA202602025870.md): Attach Fitting · excess play · Jan 20, 2026 · N580UW · Airbus A321231 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-42-11.
- [SDR AALA202602020619](https://openairdocs.org/sdr/AALA202602020619.md): Attach Fitting · excess play · Jan 20, 2026 · N580UW · Airbus A321231 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING BEARING HAS EXCESSIVE PLAY. REPLACED ATTACH FITTING PER SRM 51-42-11.
- [SDR AALA202601283956](https://openairdocs.org/sdr/AALA202601283956.md): Hinge Fitting · excess play · Jan 19, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601289310](https://openairdocs.org/sdr/AALA202601289310.md): Hinge Fitting · excess play · Jan 19, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202602041206](https://openairdocs.org/sdr/AALA202602041206.md): Hinge Fitting · excess play · Jan 18, 2026 · N580UW · Airbus A321231 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202602043522](https://openairdocs.org/sdr/AALA202602043522.md): Hinge Fitting · excess play · Jan 18, 2026 · N580UW · Airbus A321231 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601280508](https://openairdocs.org/sdr/AALA202601280508.md): Hinge Fitting · excess play · Jan 18, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601284389](https://openairdocs.org/sdr/AALA202601284389.md): Hinge Fitting · excess play · Jan 18, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202601284015](https://openairdocs.org/sdr/AALA202601284015.md): Hinge Fitting · excess play · Jan 18, 2026 · N580UW · Airbus A321231 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202602168564](https://openairdocs.org/sdr/AALA202602168564.md): Door Frame · cracked · Jan 17, 2026 · N580UW · Airbus A321231 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON FRAME AT FR 68 LEFT-HAND SIDE DOOR STOP 1 LOWER INBOARD HOLE. REPAIRED FRAME PER SRM 53-41-12-300-011
- [SDR AALA202510134587](https://openairdocs.org/sdr/AALA202510134587.md): Battery · discharged · Oct 10, 2025 · N580UW · Airbus A321231 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: UPON PREFLIGHT FLIGHT ATTENDANT FOUND BOTH FORWARD EMERGENCY FLASHLIGHT SEALS BROKEN AND FLASHLIGHTS ARE STOWED IMPROPERLY. MAINTENANCE FOUND THE BATTERIES ON BOTH FLASHLIGHTS WERE DISCHARGED AND REPLACED BOTH FLASHLIGHTS PER AMM 25-
- [SDR AALA202509117600](https://openairdocs.org/sdr/AALA202509117600.md): Reservoir · low pressure · Aug 31, 2025 · N580UW · Airbus A321231 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: DOOR SLIDE 3L HAS LOW PRESSURE INDICATION. MAINTENANCE REPLACED THE L3 DOOR SLIDE INFLATION RESERVOIR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-49.
- [SDR AALA202509017600](https://openairdocs.org/sdr/AALA202509017600.md): Slide · low pressure · Aug 31, 2025 · N580UW · Airbus A321231 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: DOOR SLIDE 3L HAS LOW PRESSURE INDICATION. (OPEN)
- [SDR AALA202509118146](https://openairdocs.org/sdr/AALA202509118146.md): Reservoir · low pressure · Aug 28, 2025 · N580UW · Airbus A321231 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: WHEN FLIGHT ATTENDANT ARMED THE L3 DOOR CHECK SLIDE PRESSURE LIGHT CAME ON. MAINTENANCE REPLACED THE L3 DOOR SLIDE INFLATION RESERVOIR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-49.
- [SDR AALA202509018146](https://openairdocs.org/sdr/AALA202509018146.md): Warning Light · illuminated · Aug 28, 2025 · N580UW · Airbus A321231 · Door Warning System
  > AIRCRAFT WAS NOT GROUNDED: WHEN FLIGHT ATTENDANT ARMED THE L3 DOOR CHECK SLIDE PRESSURE LIGHT CAME ON. (OPEN)
- [SDR AALA202505215350](https://openairdocs.org/sdr/AALA202505215350.md): Battery · no test · May 20, 2025 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 15WL DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL (AALA202505218809) AND BATTERY (AALA202505215350) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOM
- [SDR AALA202505218809](https://openairdocs.org/sdr/AALA202505218809.md): Power Supply · no test · May 20, 2025 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 15WL DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 15WL (AALA202505218809) AND BATTERY (AALA202505215350) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOM
- [SDR AALA202505210507](https://openairdocs.org/sdr/AALA202505210507.md): Battery · no test · May 20, 2025 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FAULT MESSAGE DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 12WL DURING SYSTEM TEST. REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 12WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
- [SDR AALA202409304016](https://openairdocs.org/sdr/AALA202409304016.md): Door Latch · out of adjust · Sep 29, 2024 · N580UW · Airbus A321231 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR HANDLE DOES NOT OPEN WHEN ROTATED COUNTERCLOCKWISE. OPENS THE OTHER DIRECTION BUT STILL SEEMS LIKE IT NEEDS TOBE ADJUSTED AS IT BARELY CLEARS THE LATCH. ADJUSTED F/D DOOR CENTER LATCH MECHANISM.
- [SDR AALA202409278776](https://openairdocs.org/sdr/AALA202409278776.md): Door Latch · out of adjust · Sep 26, 2024 · N580UW · Airbus A321231 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR HANDLE WILL NOT UNLATCH WHEN TURNING HANDLE CLOCKWISE AND IS DIFFICULT TO OPEN DOOR WHEN TURNING HANDLE COUNTECLOCKWISE. FOUND LOWER LATCH WORN AND LOOSE DUE TO WORN TEFLON WASHER AND WEAR, NEEDS LATCH 26-5251-3-0059 NIS
- [SDR AALA202409238108](https://openairdocs.org/sdr/AALA202409238108.md): Door Latch · out of adjust · Sep 22, 2024 · N580UW · Airbus A321231 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR WILL NOT OPEN TURNING HANDLE COUNTER CLOCKWISE ONLY CLOCKWISE. MAINTENANCE ADJUSTED FLIGHT DECK DOOR CENTER LATCH PER AMM 52-51-21.
- [SDR AALA202405234721](https://openairdocs.org/sdr/AALA202405234721.md): Battery · no test · May 22, 2024 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY BATTERY CIDS TEST FAILED AT EPSU POS 11WL. REMOVED AND REPLACED EPSU BATTERY AT 11WL AS REQUIRED PER AMM 33-51-38. TEST OK.
- [SDR AALA202405232790](https://openairdocs.org/sdr/AALA202405232790.md): Battery · no test · May 22, 2024 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY BATTERY CIDS TEST FAILED AT EPSU POS 12WL. REMOVED AND REPLACED EPSU BATTERY AT 12WL AS REQUIRED PER AMM 33-51-38. TEST OK.
- [SDR AALA202405235106](https://openairdocs.org/sdr/AALA202405235106.md): Battery · no test · May 22, 2024 · N580UW · Airbus A321231 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY BATTERY CIDS TEST FAILED AT EPSU POS 15 WL. REMOVED AND REPLACED EPSU BATTERY AT 15WL AS REQUIRED PER AMM 33-51-38. TEST OK.
- [SDR AALA202402201944](https://openairdocs.org/sdr/AALA202402201944.md): Connector · unsecure · Feb 16, 2024 · N580UW · Airbus A321231 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH LIGHT AT SEAT 26ABC INOPERATIVE. RESECURRED CONNECTOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202402036207](https://openairdocs.org/sdr/AALA202402036207.md): Battery · inoperative · Feb 1, 2024 · N580UW · Airbus A321231 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: L3 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED L3 FLIGHT ATTENDANT FLASHLIGHT BATTERY AS REQUIRED.

Next page: https://openairdocs.org/aircraft/N580UW/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 = 'N580UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N580UW/reports

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