# Service difficulty reports: N664AW

A list on [N664AW](https://openairdocs.org/aircraft/N664AW.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 · 233 reports

- [SDR AALA202511248287](https://openairdocs.org/sdr/AALA202511248287.md): Shade · stuck · Nov 23, 2025 · N664AW · Airbus A320232 · Passenger Compartment Equipment
  > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE IN 10F (EMERGENCY EXIT) IS STUCK IN THE DOWN POSITION. MAINTENANCE REMOVED AMD REPLACED THE SHADE.
- [SDR AALA202510140384](https://openairdocs.org/sdr/AALA202510140384.md): Bulb · inoperative · Oct 11, 2025 · N664AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: ROW 11C EMERGENCY PATH LIGHT NEEDS RELAMP. MAINTENANCE INSTALLED LAMP EMERGENCY PATH LIGHT ROW 11 C IAW CMM B/E AEROSPACE 25-40-07 ASSEMBLY STEP 3.A(1) ITEM (B), (C).
- [SDR AALA202509307006](https://openairdocs.org/sdr/AALA202509307006.md): Hinge Fitting · excess play · Sep 29, 2025 · N664AW · Airbus A320232 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: OUT LIMIT RH AFT DOOR (6MM) IAW JC 26C71032007 IN NOSE WHEEL WELL. MAINTENANCE REPLACED AFT AND FWD HINGE FITTINGS ON NLG AFT DOOR RH IAW CMM 52-82-32-000-801-B01; CMM 52-82-32-000-803-C01; CMM 52-82-32-400-802-C01 AND CMM 52-82
- [SDR AALA202509300309](https://openairdocs.org/sdr/AALA202509300309.md): Hinge · excess play · Sep 29, 2025 · N664AW · Airbus A320232 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: OUT LIMIT LH AFT DOOR (6MM) IAW JC 26C71032007 IN NOSE WHEEL WELL. MAINTNENANCE REPLACED AFT AND FWD HINGE FITTINGS ON NLG AFT DOOR LH IAW CMM 52-82-32-000-801-B01; CMM 52-82-32-000-803-C01; CMM 52-82-32-400-802-C01 AND CMM 52-82-
- [SDR AALA202509290999](https://openairdocs.org/sdr/AALA202509290999.md): Bottle · low pressure · Sep 26, 2025 · N664AW · Airbus A320232 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE INFLATION RESERVOIR EMERGENCY EXIT RH DOOR 844. MAINTENANCE REPLACED INFLATION RESERVOIR EMERGENCY EXIT RH DOOR 844 IAW AMM 25-62-46-000-001-A AND AMM 25-62-46-400-001-A.
- [SDR AALA202509106666](https://openairdocs.org/sdr/AALA202509106666.md): Bottle · no test · Sep 9, 2025 · N664AW · Airbus A320232 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DO NOT PASS DAMPING TEST FUNCTION DOOR DAMPER PASSENGER CREW DOOR 832AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.
- [SDR AALA202509106633](https://openairdocs.org/sdr/AALA202509106633.md): Bolt · corroded · Aug 27, 2025 · N664AW · Airbus A320232 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT 1 LOWER BOLT TRACK #3 ATTACHMENT ON RT WING, MEASURES OF CORROSION L: 0.105 IN, W:0.079 IN, D: 0.001IN. MAINTENANCE REPLACED SLAT 1 LOWER BOLT TRACK #3 ATTACHMENT ON RH WING.
- [SDR AALA202509112079](https://openairdocs.org/sdr/AALA202509112079.md): Oxygen Mask · missing · Aug 16, 2025 · N664AW · Airbus A320232 · Passenger Oxygen System
  > AIRCRAFT IN BASE MAINTENANCE: YELLOWISH MASK IN EMERGENCY OXYGEN CONTAINER ALONG PASSENGER CABIN RH SIDE EXCEPT ROW 25. FINAL REPAIR UPDATED: REPLACED MASK IN EMERGENCY OXYGEN CONTAINER ALONG PASSENGER CABIN RH SIDE EXCEPT ROW 25. IAW AMM 35-21-43-000-001-A AN
- [SDR AALA202509106621](https://openairdocs.org/sdr/AALA202509106621.md): Fitting · worn · Aug 8, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE UPPER FITTING LOCATED AT LEVEL FR20 NOSE LANDING GEAR BAY INTERNAL STRUCTURE IN LATERAL AVIONIC COMP LH HOLE WIDTH =0.560 INCH. MAINTENANCE REPLACED UPPER FITTING AT LEVEL FR20 NOSE LANDING GEAR BAY INTERNAL STRUC
- [SDR AALA202510146811](https://openairdocs.org/sdr/AALA202510146811.md): Shear Plate · cracked · Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23R AT AFT GALLEY AREA, MEASURE OF CRACK IS L= 1.021 IN. MAINTENANCE REPLACED SHEAR SHEAR PLATE STR 23R BETWEEN FR69 AND FR70 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801, A320 SRM 51-72-11-911-001 AND DWG D5
- [SDR AALA202509294444](https://openairdocs.org/sdr/AALA202509294444.md): Stringer · corroded · Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 42L BTW FR58 AND FR 59 IN AFT CARGO COMPARTMENT MEASURE CORROSION ARE L=6.823 INCH W=0.878 INCH D=0.025 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON STRINGER 42L BTW FR58 AND FR 59 IN AFT CARGO COMPARTMENT IA
- [SDR AALA202509290845](https://openairdocs.org/sdr/AALA202509290845.md): Stringer · corroded · Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT L=5.748 INCH W=0.878 INCH D=0.023 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON STRINGER LOC ON STRG 43L BTW FR57 AND FR59 IN AFT CARGO COMPARTMENT IAW A320 S
- [SDR AALA202509028347](https://openairdocs.org/sdr/AALA202509028347.md): Floorbeam · corroded · Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 FR 66 AT AFT GALLEY AREA, MEASURE OF CORROSION ARE: L= 1.613 INCH W= 1.060 INCH D= 0.040 INCH. MAINTENANCE REPLACED FLOOR BEAM Y1292 BETWEEN FR64 TO FR66 AFT GALLEY AREA LH SIDE IAW A320 SRM 51-72-11-91
- [SDR AALA202509020656](https://openairdocs.org/sdr/AALA202509020656.md): Shear Plate · cracked · Aug 7, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. CRACK L= 1.465 IN. MAINTENANCE REPLACED SHEAR PLATE LOC. ON STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53
- [SDR AALA202508269906](https://openairdocs.org/sdr/AALA202508269906.md): Fitting · corroded · Aug 7, 2025 · N664AW · Airbus A320232 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING PASSENGER CREW DOOR BETWEEN FR16 AND FR20 AT LEVEL STR23R FWD GALLEY AREA MEASURE CORROSION ARE L=0.456 INCH W=0.388 INCH D=0.014 INCH.
- [SDR AALA202508207140](https://openairdocs.org/sdr/AALA202508207140.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508205069](https://openairdocs.org/sdr/AALA202508205069.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508205551](https://openairdocs.org/sdr/AALA202508205551.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 FITTING ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508203061](https://openairdocs.org/sdr/AALA202508203061.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508202380](https://openairdocs.org/sdr/AALA202508202380.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508206708](https://openairdocs.org/sdr/AALA202508206708.md): Hinge Fitting · excess play · Aug 6, 2025 · N664AW · Airbus A320232 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. MSINTENANCE REPLACED ELEVATOR HINGE ARM FITTING 4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202510140621](https://openairdocs.org/sdr/AALA202510140621.md): Structure · cracked · Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN HOLE LOCATED ON FUSELAGE AT FR35 AND STGR 30 LH. (CRACK: 0.125 INCH). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON HOLE 2 LOC FR 35 AT LEVEL STGR 30LH IAW EA 367091.
- [SDR AALA202510146795](https://openairdocs.org/sdr/AALA202510146795.md): Floor Support · cracked · Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 5 OPEN HOLE ZONE 1, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.094 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 5 (-Y765), CENTER BOX FRONT SPAR VERTICAL STR FR36 IAW EA 3673
- [SDR AALA202510148145](https://openairdocs.org/sdr/AALA202510148145.md): Floor Support · cracked · Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 4 OPEN HOLE ZONE 1, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH IS: 0.157 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 4 (-Y254), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EA
- [SDR AALA202510141712](https://openairdocs.org/sdr/AALA202510141712.md): Floor Support · cracked · Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 3 OPEN HOLE ZONE 2, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.155 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 3 (Y254), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EA 3673
- [SDR AALA202510147088](https://openairdocs.org/sdr/AALA202510147088.md): Floor Support · cracked · Aug 5, 2025 · N664AW · Airbus A320232 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON POSITION 2 OPEN HOLE ZONE 2, CENTER BOX FRONT SPAR VERTICAL STR FR 36. CRACK DEPTH= 0.155 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR LOC POSITION 2 (+Y765), CENTER BOX FRONT SPAR VERTICAL STR FR 36 IAW EA 367
- [SDR AALA202510082347](https://openairdocs.org/sdr/AALA202510082347.md): Door Frame · no discrepancy · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.
- [SDR AALA202510080186](https://openairdocs.org/sdr/AALA202510080186.md): Door Frame · cracked · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 843 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.
- [SDR AALA202510080481](https://openairdocs.org/sdr/AALA202510080481.md): Door Frame · no discrepancy · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 843 FRAME, BETWEEN FR 38 AND FR 39, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.
- [SDR AALA202510087242](https://openairdocs.org/sdr/AALA202510087242.md): Door Frame · cracked · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK IN OVERWING EXIT 844 RIGHT HAND LOAD TRANSMITTING PROFILE BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3. REPLACED SEGMENT PER EO 5210Y228.
- [SDR AALA202510089637](https://openairdocs.org/sdr/AALA202510089637.md): Door Frame · no discrepancy · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.
- [SDR AALA202510088979](https://openairdocs.org/sdr/AALA202510088979.md): Door Frame · no discrepancy · Aug 4, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: MODIFICATION OF OVERWING EMERGENCY EXIT 844 FRAME, BETWEEN FR 40 AND FR 41, BETWEEN BEAM 2 AND BEAM 3, REQUIRED DUE TO POTENTIAL CRACK PER EO 5210Y228. MODIFICATION OF FRAME ACCOMPLISHED PER EO 5210Y228.
- [SDR AALA202510084915](https://openairdocs.org/sdr/AALA202510084915.md): Fitting · cracked · Jul 30, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED CONTINUITY FITTING PER EA 366931.
- [SDR AALA202509265046](https://openairdocs.org/sdr/AALA202509265046.md): Window Frame · cracked · Jul 30, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE, CRACK INDICATION FOUND ON WINDSHIELD FRAME LOWER ATTACHMENT AREA INTERNAL SIDE. LOCATED ON LOWER RADIUS LH SIDE IN COCKPIT. CRACK LENGTH=0.400 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR, REPAIR ON CENTER POST LT AND RT SIDE
- [SDR AALA202509237127](https://openairdocs.org/sdr/AALA202509237127.md): Fitting · cracked · Jul 30, 2025 · N664AW · Airbus A320232 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING RADIUS AREA. LOCATED ON WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE. IN COCKPIT. CRACK LENGTH= 0.250 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR REPLACED CONTINUITY FITTING
- [SDR AALA202506169933](https://openairdocs.org/sdr/AALA202506169933.md): Elt · inoperative · Jun 15, 2025 · N664AW · Airbus A320232 · Emergency Locator Beacon
  > AIRCRAFT WAS NOT GROUNDED: FOUND FWD EMERGENCY LOCATOR TRANSMITTER WIRING UNWOUND. MAINTENANCE REPLACED FWD PORTABLE ELT IAW AMM 25-65-32. J/C 99L20025003.
- [SDR AALA202411226834](https://openairdocs.org/sdr/AALA202411226834.md): Sign · missing · Nov 21, 2024 · N664AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: DOOR 2L IS MISSING PLASTIC CAP THAT SAYS EMERGENCY EXIT. MAINTENANCE INSTALLED LENS ON LAMP ASSY AFT OF DOOR #2L AS REQUIRED.
- [SDR AALA202410020986](https://openairdocs.org/sdr/AALA202410020986.md): Pressure Switch · warning message · Oct 1, 2024 · N664AW · Airbus A320232 · Hydraulic System, Main
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO IAH DUE TO THE FLIGHT CREW REPORTING THAT WHILE CLIMBING OUT A GREEN HYDRAULIC ENGINE #1 PUMP LOW PRESSURE ECAM MESSAGE DISPLAYED. THE AIRCRAFT LANDED SAFELY AT IAH AND TAXIED TO THE
- [SDR AALA202408123095](https://openairdocs.org/sdr/AALA202408123095.md): Battery · inoperative · Aug 9, 2024 · N664AW · Airbus A320232 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT INOP AT 2L DOOR. REMOVED AND REPLACED FLASHLIGHT BATTERY, OPS CK GOOD OK SERVICE IAW GPM 02.01.2.
- [SDR AALA202405289644](https://openairdocs.org/sdr/AALA202405289644.md): Skin Panel · cracked · May 26, 2024 · N664AW · Airbus A320232 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL AT FR 14 AND S6R. MAINTENANCE REPAIRED SKIN PANEL PER SRM 53-11-11-300-054.
- [SDR AALA202402076319](https://openairdocs.org/sdr/AALA202402076319.md): Slide · unwanted deploy · Feb 6, 2024 · N664AW · Airbus A320232 · Escape Slide
  > AIRCRAFT WAS GROUNDED: FORWARD ENTRY DOOR SLIDE WAS INADVERTANTLY DEPLOYED AND MAINTENANCE REPORTED THE SLIDE DID NOT FULLY DEPLOY. MAINTENANCE REPLACED THE SLIDE PER AMM 25-62-00.
- [SDR AALA202312204897](https://openairdocs.org/sdr/AALA202312204897.md): Fitting · sticking · Dec 19, 2023 · N664AW · Airbus A320232 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: DOOR 2L SLIDE ARM LEVER HARD TO MOVE. MAINTENANCE LUBRICATED THE L2 DOOR FORWARD AND AFT GIRT BAR FITTINGS.
- [SDR AALA202310272708](https://openairdocs.org/sdr/AALA202310272708.md): Flashlight · inoperative · Oct 26, 2023 · N664AW · Airbus A320232 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT #1 JUMPSEAT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT AT FLIGHT ATTENDANT #1 JUMPSEAT PER AMM 25-65-00.
- [SDR AALA202308239080](https://openairdocs.org/sdr/AALA202308239080.md): Knob · sticks · Aug 18, 2023 · N664AW · Airbus A320232 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: AFT LEFT LAVATORY DOOR HANDLE STICKS, DIFFICULT TO OPERATE. LUBRICATED AFT LAVATORY DOOR KNOB PER AMM 52-50-00.
- [SDR AALA202306277960](https://openairdocs.org/sdr/AALA202306277960.md): Fork · worn · Jun 27, 2023 · N664AW · Airbus A320232 · Fuselage Structure (General)
  > AIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER LEFT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32L. REPLACED FORK END (AALA202306277960) AND FITING (AALA202306274651) PER EA 343852.
- [SDR AALA202306272377](https://openairdocs.org/sdr/AALA202306272377.md): Fork · worn · Jun 27, 2023 · N664AW · Airbus A320232 · Fuselage Structure (General)
  > AIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER RIGHT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32R. REPLACED FORK END (AALA202306272377) AND FITING (AALA202306275345) PER EA 343852.
- [SDR AALA202306275345](https://openairdocs.org/sdr/AALA202306275345.md): Fitting · worn · Jun 27, 2023 · N664AW · Airbus A320232 · Fuselage Structure (General)
  > AIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER RIGHT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32R. REPLACED FORK END (AALA202306272377) AND FITING (AALA202306275345) PER EA 343852.
- [SDR AALA202306274651](https://openairdocs.org/sdr/AALA202306274651.md): Fitting · worn · Jun 27, 2023 · N664AW · Airbus A320232 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: 80VU RACK LOWER LEFT LATERAL ATTACH FITTINGS HOLES WORN AT FR 24 AND S32L. REPLACED FORK END (AALA202306277960) AND FITING (AALA202306274651) PER EA 343852.
- [SDR AALA202301098856](https://openairdocs.org/sdr/AALA202301098856.md): Sign · inoperative · Jan 7, 2023 · N664AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: 1R EMERGENCY EXIT SIGN BURNT OUT. MAINTENANCE REPLACED 1R EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202301097529](https://openairdocs.org/sdr/AALA202301097529.md): Sign · inoperative · Jan 7, 2023 · N664AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FORWARD BULKHEAD CEILING EXIT SIGN BURNT OUT. MAINTENANCE REPLACED FORWARD BULKHEAD EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Next page: https://openairdocs.org/aircraft/N664AW/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 = 'N664AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N664AW/reports

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