# Service difficulty reports: N653AW

A list on [N653AW](https://openairdocs.org/aircraft/N653AW.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 6 · 293 reports

- [SDR AALA202608265779](https://openairdocs.org/sdr/AALA202608265779.md): Wire · disconnected · Aug 22, 2026 · N653AW · Airbus A320232 · Light System Wiring
  > AIRCRAFT IN BASE MAINTENANCE: R1 DOOR LOWER EMERGENCY ESCAPE LIGHT IS INOP. FOUND WIRE FOR CONNECTOR TO R1 DOOR LOWER EMERGENCY ESCAPE LIGHT BROKEN AND OTHER CONNECTOR NOT CONNECTED. MAINTENANCE SPLICED BOTH WIRES PER ESPM 20-53-29, ESPM 20-53-21 AND AWM 33-51
- [SDR AALA202605150598](https://openairdocs.org/sdr/AALA202605150598.md): Battery · discharged · May 13, 2026 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT AT AFT FA JUMPSEAT INOPERATIVE. MAINTENANCE REPLACED BATTERY IN EMERGENCY FLASHLIGHT AT AFT F/A SEAT AMM 25-65-00.
- [SDR AALA202604280098](https://openairdocs.org/sdr/AALA202604280098.md): Fitting · cracked · Apr 19, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE, CRACK DIRECTION: 5 OCLOCK (VIEW AFT LOOKING FWD). D1-D2= 0.212 INCH; AD 2020-19-03 (L= 0.212 IN). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON RH LA
- [SDR AALA202604249791](https://openairdocs.org/sdr/AALA202604249791.md): Fitting · cracked · Apr 17, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: WINDSHIELD FRAMING CENTER POST LH HALF FOUND CRACKED IN AREA A. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE IAW EA 372184.
- [SDR AALA202604281730](https://openairdocs.org/sdr/AALA202604281730.md): Fitting · cracked · Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE IAW EA 372184. MAINTENANCE REPLACED CONTINUITY FITTING LOCATED Y0 AND FR2 LH SIDE BY EA 372184.
- [SDR AALA202604249438](https://openairdocs.org/sdr/AALA202604249438.md): Fitting · cracked · Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: MAINTENANCE: WINDSHIELD FRAMING CENTER POST FITTING LOWER FITTING FOUND CRACKED AT Y0 AND FR2. MAINTENANCE REPLACE LOWER FITTING YO AND FR2 IAW EA 372184.
- [SDR AALA202604241668](https://openairdocs.org/sdr/AALA202604241668.md): Floorbeam · cracked · Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N2 FR 36. CRACK L= 0.530 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOOR BEAM Y765 VERTICAL STRINGER #2 AT FR 36
- [SDR AALA202604226871](https://openairdocs.org/sdr/AALA202604226871.md): Floorbeam · cracked · Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N3 FR 36. CRACK L= 0.550 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM Y254 VERTICAL STRINGER #3 AT FR 36 IAW
- [SDR AALA202604225191](https://openairdocs.org/sdr/AALA202604225191.md): Floorbeam · cracked · Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N5 FR 36. CRACK L= 0.875 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y765 VERTICAL STRINGER #5 AT FR 36 I
- [SDR AALA202604220542](https://openairdocs.org/sdr/AALA202604220542.md): Floorbeam · cracked · Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N4 FR 36. CRACK L= 0.610 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y254 VERTICAL STRINGER #4 AT FR 36 IA
- [SDR AALA202604282565](https://openairdocs.org/sdr/AALA202604282565.md): Frame · cracked · Feb 9, 2026 · N653AW · Airbus A320232 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN WEB AFT FACE RADIUS WITH STGR 8 HORIZONTAL FLANGE, AT AFT GALL EY AREA CRACK LENGTH IS 0.430 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON FR68 BTW STR7 AND STR9 RH SID
- [SDR AALA202602184795](https://openairdocs.org/sdr/AALA202602184795.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602189094](https://openairdocs.org/sdr/AALA202602189094.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602188638](https://openairdocs.org/sdr/AALA202602188638.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602188350](https://openairdocs.org/sdr/AALA202602188350.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602184281](https://openairdocs.org/sdr/AALA202602184281.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602189099](https://openairdocs.org/sdr/AALA202602189099.md): Hinge Fitting · excess play · Feb 9, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202604283330](https://openairdocs.org/sdr/AALA202604283330.md): Shear Plate · cracked · Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AFT GALLEY AREA. MEASURE OF CRACK ON SHEAR PLATE IS L= 1.826 INCH.
- [SDR AALA202603098225](https://openairdocs.org/sdr/AALA202603098225.md): Floorbeam · corroded · Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 AT LEVEL FR66 AT AFT GALLEY AREA. MEASURES L = 2.732 IN, W = 1.17 IN, D = 0.0210 IN. MAINTENANCE REPLACED FLOOR BEAM +Y1292 LOC. BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 AND DWG D5
- [SDR AALA202603038853](https://openairdocs.org/sdr/AALA202603038853.md): Floorbeam · corroded · Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. IAW A320 S
- [SDR AALA202603039183](https://openairdocs.org/sdr/AALA202603039183.md): Floorbeam · corroded · Feb 8, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM Y765 BETWEEN FR64 THRU FR66 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, DWG D53142
- [SDR AALA202602253028](https://openairdocs.org/sdr/AALA202602253028.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator 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 AALA202602259815](https://openairdocs.org/sdr/AALA202602259815.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator 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 AALA202602255822](https://openairdocs.org/sdr/AALA202602255822.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator 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 AALA202602188026](https://openairdocs.org/sdr/AALA202602188026.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON HINGE ARM END FITTING N1 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602187296](https://openairdocs.org/sdr/AALA202602187296.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING N5 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202602181427](https://openairdocs.org/sdr/AALA202602181427.md): Hinge Fitting · excess play · Feb 8, 2026 · N653AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING N2 ON RH ELEVATOR. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH ELEVATOR IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202604289710](https://openairdocs.org/sdr/AALA202604289710.md): Door Frame · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL R/H SIDE IN PASSENGER CABIN. LENGTH OF CRACK IS= 0.562 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE (SEGMENT FWD) AND BEAM 1 AND ACCOMPLISHED MODIFY ON EM
- [SDR AALA202604288846](https://openairdocs.org/sdr/AALA202604288846.md): Door Frame · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. MAINTENANCE REPLACED LOAD TRANSMITTING (FWD AND AFT SEGMENT) AND UPPER BEAM 1, AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844, IAW EO# 5210
- [SDR AALA202604285695](https://openairdocs.org/sdr/AALA202604285695.md): Frame · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. MAINTENANCE REPLACED LOAD TRANSMITTING (FWD AND AFT SEGMENT) AND UPPER BEAM 1, AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT DOOR 844, IAW EO# 5210
- [SDR AALA202604286828](https://openairdocs.org/sdr/AALA202604286828.md): Frame · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 ON VERTICAL FRAME INTERNAL AREA IN PASENGER CABIN. CRACK L: 0.465 INCH.
- [SDR AALA202604240577](https://openairdocs.org/sdr/AALA202604240577.md): Profile · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL R/H SIDE I N PASSENGER CABIN. MAINTENACE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE, BEAM 1 AND ACCOMPLISHED MODIFY ON EMERGENCY EXIT DOOR 833 IAW EO 5210Y228-001 AND MAN
- [SDR AALA202604242373](https://openairdocs.org/sdr/AALA202604242373.md): Profile · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 833 ON LOAD TRANSMITTING PROFIL L/H SIDE IN PASSENGER CABIN. LENGHT OF CRACK = 0.500 INCH. REPLACED LOAD TRANSMITTING PROFILE L/H SIDE AND ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT 833, IAW EO# 5210Y228
- [SDR AALA202604207450](https://openairdocs.org/sdr/AALA202604207450.md): Profile · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFILE L/H SIDE IN PASSENGER CABIN, CRACK LENGTH 0.520 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE L/H SIDE (FWD SEGMENT) BTW BEAM 1 AND BEAM 3; ACCOMPLISHED MODIFICATIO
- [SDR AALA202604205818](https://openairdocs.org/sdr/AALA202604205818.md): Profile · cracked · Feb 7, 2026 · N653AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 843 ON LOAD TRANSMITTING PROFIL R/H SIDE IN PASSENGER CABIN, CRACK LENGTH 0.580 INCH. MAINTENANCE REPLACED LOAD TRANSMITTING PROFILE R/H SIDE (AFT SEGMENT) BTW BEAM 1 AND BEAM 3; ACCOMPLISHED MODIFICATI
- [SDR AALA202604287088](https://openairdocs.org/sdr/AALA202604287088.md): Window Frame · cracked · Feb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INST
- [SDR AALA202604284966](https://openairdocs.org/sdr/AALA202604284966.md): Window Frame · cracked · Feb 5, 2026 · N653AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LOCATED ON UPPER TENSION BOLT, WINDSHIELD CENTER POST LH SIDE. CRACK DIRECTION: 1 OCLOCK (VIEW ON LH SIDE), CRACK LEN GHT= 0.200 INCH APPROX, AD-2020-17-03. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INS
- [SDR AALA202510033494](https://openairdocs.org/sdr/AALA202510033494.md): Sign · inoperative · Oct 1, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: R2 DOOR EXIT SIGN HAS BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.
- [SDR AALA202510034506](https://openairdocs.org/sdr/AALA202510034506.md): Sign · inoperative · Oct 1, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: L2 DOOR EXIT SIGN HAS BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.
- [SDR AALA202510039345](https://openairdocs.org/sdr/AALA202510039345.md): Sign · inoperative · Oct 1, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FWD GALLEY CENTER EXIT SIGN HAS LIGHT BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.
- [SDR AALA202510031169](https://openairdocs.org/sdr/AALA202510031169.md): Sign · inoperative · Oct 1, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED, R1 DOOR EXIT SIGN HAS LIGHT BULBS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.
- [SDR AALA202510037170](https://openairdocs.org/sdr/AALA202510037170.md): Sign · inoperative · Oct 1, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: L1 DOOR EXIT SIGN HAS LIGHT BULBS INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY IAW AMM 33-51-16.
- [SDR AALA202509031926](https://openairdocs.org/sdr/AALA202509031926.md): Power Supply · no test · Sep 2, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM DURING SLIDE CHANGE FOUND RIGHT EPSU FAULT. MAINTENANCE REPLACED RIGHT CENTER EPSU IAW AMM 33-51-38.
- [SDR AALA202505293230](https://openairdocs.org/sdr/AALA202505293230.md): Bulb · inoperative · May 29, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EXIT LIGHT AT ROW 10 FWD SIDE HAS MULTIPLE LIGHTS OUT. MAINTENANCE RELAMPED EXIT SIGN AT ROW 10.
- [SDR AALA202505203025](https://openairdocs.org/sdr/AALA202505203025.md): Light · no test · May 17, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FOUND R/H EMERGENCY EXIT MARKER LIGHT INOP AT EMERGENCY EXIT HATCHES. MAINTENANCE REPLACED EMERGENCY EXIT MARKER LIGHT REF AMM 33-51-16.
- [SDR AALA202505202051](https://openairdocs.org/sdr/AALA202505202051.md): Light · no test · May 17, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FOUND L/H EMERGENCY EXIT MARKER LIGHT INOP AT EMERGENCY EXIT HATCHES. MAONTENANCE REPLACED EMERGENCY EXIT MARKER LIGHT REF AMM 33-51-16 OPS CHECK GOOD.
- [SDR AALA202505156479](https://openairdocs.org/sdr/AALA202505156479.md): Bracket · inoperative · May 13, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING J/C 26L00005005 FOUND SEAT 11DEF CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 11DEF CABIN EMERGENCY LIGHT OUTER BRACKET IAW CMM 25-40-07 AND REINSTALLED EMERGENCY LIGHT IAW AMM 33-51-18,
- [SDR AALA202505158884](https://openairdocs.org/sdr/AALA202505158884.md): Light · no test · May 12, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: SEAT 19ABC CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 19ABC EMERGENCY LIGHT ASSY IAW AMM 33-51-18.
- [SDR AALA202505138884](https://openairdocs.org/sdr/AALA202505138884.md): Light · no test · May 12, 2025 · N653AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: SEAT 19ABC CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SEAT 19ABC EMERGENCY LIGHT ASSY IAW AMM 33-51-18.
- [SDR AALA202503242062](https://openairdocs.org/sdr/AALA202503242062.md): Handle · broken · Mar 23, 2025 · N653AW · Airbus A320232 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS LAVATORY E DOOR HANDLE HAS BROKEN OFF, AND ARE UNABLE TO OPEN THE DOOR AFTER GETTING IT CLOSED. MAINTENANCE RESECURED AND TIGHTENED LAVATORY DOOR LATCH SCREWS AS REQUIRED..

Next page: https://openairdocs.org/aircraft/N653AW/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 = 'N653AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N653AW/reports

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