# Service difficulty reports: N830AW

A list on [N830AW](https://openairdocs.org/aircraft/N830AW.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 · 225 reports

- [SDR AALA202609152600](https://openairdocs.org/sdr/AALA202609152600.md): Carriage · worn · Sep 7, 2026 · N830AW · Airbus A319132 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: WHILE TROUBLESHOOTING CHRONIC FLAP VIBRATION MAINTENANCE FOUND THE RIGHT WING POSITION 1 FLAP TRACK CARRIAGE ASSEMBLY WAS WORN. MAINTENANCE REPAIRED THE CARRIAGE ASSEMBLY PER CMM 27-54-43 AND AMM 27-54-46.
- [SDR AALA202609151034](https://openairdocs.org/sdr/AALA202609151034.md): Carriage · worn · Sep 7, 2026 · N830AW · Airbus A319132 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: WHILE TROUBLESHOOTING CHRONIC FLAP VIBRATION MAINTENANCE FOUND THE RIGHT WING POSITION 2 FLAP TRACK CARRIAGE ASSEMBLY WAS WORN. MAINTENANCE REPLACED THE CARRAGE ASSEMBLY IAW JOB CARD 26L00027008 AND AMM 27-54-46.
- [SDR AALA202606303131](https://openairdocs.org/sdr/AALA202606303131.md): Life Line · misinstalled · Jun 27, 2026 · N830AW · Airbus A319132 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: WATER EVACUATION ROPES IMPROPERLY STOWED IN BIN. MAINTENANCE REINSTALLED LIFELINE IN STORAGE BAG AND PUT IN OVERHEAD STOWAGE COMPARTMENT PER AMM 25-60-00.
- [SDR AALA202604022486](https://openairdocs.org/sdr/AALA202604022486.md): Wire · broken · Apr 1, 2026 · N830AW · Airbus A319132 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT NEAR 1R DOOR HAS BROKEN TERMINAL. MAINTENANCE RETERMINATED WIRE IAW ESPM 20-48-14. PERFORMED EMERGENCY LIGHTING OPS CHECK IAW AMM 33-51-11.
- [SDR AALA202603015809](https://openairdocs.org/sdr/AALA202603015809.md): Bottle · no test · Feb 18, 2026 · N830AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS DAMPING FUNCTION OPERATIONAL TEST OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSEGER CREW DOOR 831 AT FWD GALLEY AREA. MAINTENANCE REPLACED NEW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DO
- [SDR AALA202602068964](https://openairdocs.org/sdr/AALA202602068964.md): Shear Panel · cracked · Jan 31, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEET-SHEAR BETWEEN FR 68 AND FR 69 AT S23L. REPLACED SHEET SHEAR PER SRM 51-72-11-911-001.
- [SDR AALA202601278960](https://openairdocs.org/sdr/AALA202601278960.md): Hinge Fitting · excess play · Jan 25, 2026 · N830AW · Airbus A319132 · 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 AALA202602063560](https://openairdocs.org/sdr/AALA202602063560.md): Spigot · corroded · Jan 16, 2026 · N830AW · Airbus A319132 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.
- [SDR AALA202602064323](https://openairdocs.org/sdr/AALA202602064323.md): Spigot · corroded · Jan 16, 2026 · N830AW · Airbus A319132 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.
- [SDR AALA202602015367](https://openairdocs.org/sdr/AALA202602015367.md): Fitting · corroded · Jan 15, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT GALLEY AREA CORNER FITTING AT FR 68, AT LEVEL S23L. REPLACED CORNER FITTING PER SRM 51-42-11-801.
- [SDR AALA202603197984](https://openairdocs.org/sdr/AALA202603197984.md): Shear Plate · cracked · Jan 11, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202603188465](https://openairdocs.org/sdr/AALA202603188465.md): Shear Plate · cracked · Jan 11, 2026 · N830AW · Airbus A319132 · 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 51-72-11.
- [SDR AALA202602051661](https://openairdocs.org/sdr/AALA202602051661.md): Floor Support · corroded · Jan 11, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 64 AND FR 67 AT -Y465. REPLACED FLOOR SUPPORT PER SRM 51-72-11.
- [SDR AALA202602017065](https://openairdocs.org/sdr/AALA202602017065.md): Floor Support · corroded · Jan 11, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORTBETWEEN FR 65 AND FR 67 AT -Y318. REPLACED FLOOR SUPPORT IAW SRM 51-42-11-801.
- [SDR AALA202601267234](https://openairdocs.org/sdr/AALA202601267234.md): Door Sill · corroded · Jan 10, 2026 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001, REPAIR PRINCIPLE NR 5.
- [SDR AALA202601258535](https://openairdocs.org/sdr/AALA202601258535.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 4 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 4 ON LH ELEVATOR IAW A320 AMM 55-16-42-000-001-A AND A320 AMM 55-16-42-400-001-A.
- [SDR AALA202601253583](https://openairdocs.org/sdr/AALA202601253583.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 6 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 6 ON LH ELEVATOR IAW A320 AMM 55-16-42-000-001-A AND A320 AMM 55-16-42-400-001-A.
- [SDR AALA202601259835](https://openairdocs.org/sdr/AALA202601259835.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 6 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 6 ON RH ELEVATOR IAW A320 FAM AMM55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.
- [SDR AALA202601258904](https://openairdocs.org/sdr/AALA202601258904.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 4 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 4 ON RH ELEVATOR IAW A320 FAM AMM55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.
- [SDR AALA202601255027](https://openairdocs.org/sdr/AALA202601255027.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 3 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 3 ON RH ELEVATOR IAW A320 FAM AMM55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.
- [SDR AALA202601256989](https://openairdocs.org/sdr/AALA202601256989.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 2 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 2 ON LH ELEVATOR IAW A320 AMM55-16-42-000-001-A AND A320 AMM 55-16-42-400-001-A.
- [SDR AALA202601250375](https://openairdocs.org/sdr/AALA202601250375.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 1 ON LH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 1 ON LH ELEVATOR IAW A320 AMM 55-16-42-000-001-A AND A320 AMM 55-16-42-400-001-A.
- [SDR AALA202601252175](https://openairdocs.org/sdr/AALA202601252175.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 5 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 5 ON RH ELEVATOR IAW A320 FAM AMM55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.
- [SDR AALA202601253506](https://openairdocs.org/sdr/AALA202601253506.md): Hinge Fitting · excess play · Jan 10, 2026 · N830AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING 2 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING 2 ON RH ELEVATOR IAW A320 FAM AMM55-16-42-000-001-A AND A320 FAM AMM 55-16-42-400-001-A.
- [SDR AALA202602011550](https://openairdocs.org/sdr/AALA202602011550.md): Door Sill · corroded · Jan 9, 2026 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LT PASSENGER DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED LOWER SILL IAW SRM 51-72-11.
- [SDR AALA202602052816](https://openairdocs.org/sdr/AALA202602052816.md): Threshold Web · corroded · Jan 7, 2026 · N830AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER THRESHOLD SHEET BETWEEN FR 55A AND FR 59 AT S38R. REPLACED THRESHOLD SHEET PER SRM 51-42-11.
- [SDR AALA202602091893](https://openairdocs.org/sdr/AALA202602091893.md): Stiffener · cracked · Jan 6, 2026 · N830AW · Airbus A319132 · Fuselage Main, Bulkhead
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD PRESSURE BULKHEAD STIFFENER, UPPER POSITION FORWARD FACE, AT FR 1, Z-169. REPLACED STIFFENER PER SRM 51-72-11-911-801 AND A319 SRM 51-42-11-801.
- [SDR AALA202602051624](https://openairdocs.org/sdr/AALA202602051624.md): Fitting · corroded · Jan 6, 2026 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-72-11.
- [SDR AALA202603114465](https://openairdocs.org/sdr/AALA202603114465.md): Window Frame · cracked · Dec 30, 2025 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD FRAME LH, POCKET INTERNAL AREA A T 2 O CLOCK OF UPPER BOLT, CRACK LENGTH IS 0.080 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR (MIRROR FITTING REPAIR) LOCATED ON WINDSHIELD FRAME CENTER POST L
- [SDR AALA202603111871](https://openairdocs.org/sdr/AALA202603111871.md): Fitting · cracked · Dec 30, 2025 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING RH, CRACK IS IN VERTICAL DIRECTION, CRACK LENGTH IS 0.120 IN. MAINTENANCE REPLACED CONTINUITY FITTING RH BETWEEN FR1 TO FR4 AND Y0 IAW EA # 371162, DWG # R53112919 ISSUE L AND DWG R531
- [SDR AALA202603119832](https://openairdocs.org/sdr/AALA202603119832.md): Fitting · cracked · Dec 30, 2025 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING LH, CRACK IS IN VERTICAL DIRECTION, CRACK LENGTH IS 0.135 IN. MAINTENANCE REPLACED CONTINUITY FITTING LH BETWEEN FR1 TO FR4 AND Y0 IAW EA # 371162, DWG # R53112919 ISSUE L AND DWG R531
- [SDR AALA202603058124](https://openairdocs.org/sdr/AALA202603058124.md): Window Frame · cracked · Dec 30, 2025 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD FRAME RH, POCKET INTERNAL AREA AT 10 O' CLOCK OF UPPER BOLT,CRACK LENGTH IS 0.072 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR (MIRROR FITTING REPAIR) LOCATED ON WINDSHIELD FRAME CENTER POST L
- [SDR AALA202601222566](https://openairdocs.org/sdr/AALA202601222566.md): Flashlight Assy · broken · Dec 26, 2025 · N830AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN FLIGHT ATTENDANT BASE FLASHLIGHT (SWIVEL) IN LAVATORY E. MAINTENANCE REPLACED FLIGHT ATTENDANT BASE FLASHLIGHT (SWIVEL) IN LAVATORY E. FOR INSTALLATION SEE JOB CARD 26C22025010 STEP 2.D(5)(B).
- [SDR AALA202603172307](https://openairdocs.org/sdr/AALA202603172307.md): Door Frame · cracked · Nov 28, 2025 · N830AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: INTERIM REPAIR ON ASSOCIATED HOLES N5, B AND D LOCATED ON FRAME 16 RH DOUBLE JOGGLE AREA AT DOOR STOP FITTING N7 LVL ON UPPER FUSELAGE. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON FR 16 RH DOUBLE JOGGLE AREA PARTIAL FRAME REPL
- [SDR AALA202510026523](https://openairdocs.org/sdr/AALA202510026523.md): Diaphragm · leaking · Oct 1, 2025 · N830AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: FOUND DOOR ASSIST PRESSURE AT 0 PSI.MAINTENANCE REPLACED FWD LH DOOR DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREWDOORS IAW WITH AMM 52-10-00.
- [SDR AALA202508198950](https://openairdocs.org/sdr/AALA202508198950.md): Bulb · inoperative · Aug 15, 2025 · N830AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY MARKER LIGHT ASSEMBLY HAS MULTIPLE BULBS INOP. RELAMPED EMERGENCY EXIT LIGHT AT DOOR R1, OPS GOOD.
- [SDR AALA202505164933](https://openairdocs.org/sdr/AALA202505164933.md): Shade · stuck · May 7, 2025 · N830AW · Airbus A319132 · Passenger Compartment Equipment
  > AIRCRAFT WAS NOT GROUNDED: EXIT ABC ROW 14 WINDOW SHADE WILL NOT RAISE OR LOWER. **SUPPLEMENTAL REPORT FOR SDR AALA202505094933.** (CLOSED)** MAINTENANCE REPLACED WINDOW SHADE @ ROW 14 A/C LEFT, OPS CHECK GOOD. AMM 25-20-00.
- [SDR AALA202505094933](https://openairdocs.org/sdr/AALA202505094933.md): Shade · stuck · May 7, 2025 · N830AW · Airbus A319132 · Passenger Compartment Equipment
  > AIRCRAFT WAS NOT GROUNDED: EXIT ABC ROW 14 WINDOW SHADE WILL NOT RAISE OR LOWER. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)
- [SDR AALA202503036126](https://openairdocs.org/sdr/AALA202503036126.md): Pump · leaking · Feb 27, 2025 · N830AW · Airbus A319132 · Hydraulic Pump (Electric/Engine), Main
  > AIRCRAFT WAS GROUNDED: HYD Y SAYS FAIL FLUID LOSS. PILOTS RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED DUAL VALVE ALT BRAKE DISTRIBUTION UNION & RIGID LINE REF AMM 32-43-14.
- [SDR AALA202502286126](https://openairdocs.org/sdr/AALA202502286126.md): Warning Message · illuminated · Feb 27, 2025 · N830AW · Airbus A319132 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: HYD Y SAYS FAIL FLUID LOSS. PILOTS RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. (OPEN)
- [SDR AALA202502175586](https://openairdocs.org/sdr/AALA202502175586.md): Skin · cracked · Feb 10, 2025 · N830AW · Airbus A319132 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACK AT FASTNER/ FRAME 14 RHS. MAINTENANCE ADDED DOUBLER TO SKIN AT FR12 TO FR14 IAW EA 361937.
- [SDR AALA202502172499](https://openairdocs.org/sdr/AALA202502172499.md): Skin · cracked · Feb 8, 2025 · N830AW · Airbus A319132 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACK RADIATING OUT FROM FASTENER HOLE. MAINTENANCE ADDED DOUBLE REPAIRE IAW EA 361924.
- [SDR AALA202502172235](https://openairdocs.org/sdr/AALA202502172235.md): Hinge Fitting · chafed · Feb 5, 2025 · N830AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: CHAFING DAMAGE TO THE FWD FACE OF THE AFT LUG LH MLG DOOR HING FITTING. MAINTENANCE REPLACED LH MLG DOOR HINGE FITTING IAW EA 361811.
- [SDR AALA202502174927](https://openairdocs.org/sdr/AALA202502174927.md): Hinge Fitting · chafed · Feb 5, 2025 · N830AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: CHAFING DAMAGE TO THE FWD FACE OF AFT LUG HINGE FITTING CONNECTORS. MAINTENANCE REPLACED LH MLG DOOR FUSELAGE HING FITTING IAW EA 361811.
- [SDR AALA202411052085](https://openairdocs.org/sdr/AALA202411052085.md): Slide Raft · faulted · Nov 4, 2024 · N830AW · Airbus A319132 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHMENT OF EPSU TEST FOR PS CHECK, FOUND EPSU EXT LOAD FWD L FAULT. T/S IAW TSM 33-51-00-810-808-A. REMOVED AND REINSTALLED L1 SLIDE IAW AMM 25-62-44. REMOVED R1 SLIDE IAW AMM 25-62-44. TEMPORARILY CONNECTED SERVICEABLE
- [SDR AALA202411058104](https://openairdocs.org/sdr/AALA202411058104.md): Wire · broken · Nov 4, 2024 · N830AW · Airbus A319132 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATHWAY AISLE LIGHT INOP ON SEAT 1C. MAINTENANCE REPAIRED WIRE AT SEAT 1A IAW ESPM 20-43-11.
- [SDR AALA202409165452](https://openairdocs.org/sdr/AALA202409165452.md): Guide Fitting · out of adjust · Sep 12, 2024 · N830AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: 1L DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. MAINTENANCE ADJUSTED THE UPPER AND LOWER GUIDE FITTINGS PER AMM 52-11-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
- [SDR AALA202408282973](https://openairdocs.org/sdr/AALA202408282973.md): Switch · defective · Aug 27, 2024 · N830AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION. MAINTENANCE REPLACED ARM SWITCH 4WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
- [SDR AALA202405138623](https://openairdocs.org/sdr/AALA202405138623.md): Bulb · missing · May 10, 2024 · N830AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT COVER AND LIGHT MISSING AT EXIT ROW 14. INSTALLED NEW BULB.
- [SDR AALA202402274788](https://openairdocs.org/sdr/AALA202402274788.md): Wire Harness · damaged · Feb 27, 2024 · N830AW · Airbus A319132 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: ROW 27 EMERGENCY PATHWAY LIGHT AT SEAT INOPERATIVE. REPLACED EMERGENCY LIGHT SEAT HARNESS UNDER SEAT 27ABC PER CMM 25-22-52.

Next page: https://openairdocs.org/aircraft/N830AW/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 = 'N830AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N830AW/reports

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