# Service difficulty reports: N121UW

A list on [N121UW](https://openairdocs.org/aircraft/N121UW.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 · 262 reports

- [SDR AALA202605190552](https://openairdocs.org/sdr/AALA202605190552.md): Control Box · inoperative · May 18, 2026 · N121UW · Airbus A320214 · Fixed Inner Doors
  > AIRCRAFT WAS GROUNDED: ON LANDING COCKPIT DOOR POPPED OPEN. MAINTENANCE REPLACED CDLS CONTROL UNIT IAW AMM 52-51-14.
- [SDR AALA202603027499](https://openairdocs.org/sdr/AALA202603027499.md): Oil System · leaking · Feb 19, 2026 · N121UW · Airbus A320214 · Turbine Engine Oil System
  > AIRCRAFT WAS GROUNDED: AT FL340 GOT ECAM ADV, ENG 1 OIL QUANTITY. STARTED FLIGHT WITH 18 QT. TOOK SEVERAL MINUTES FOR OIL QUANTITY TO GO TO ZERO. ALL OTHER ENGINE PARAMETERS NORMAL. SEVERAL MINUTES AFTER QUANTITY AT ZERO, OIL PRESSURE DECREASED SLOWLY TO ZERO.
- [SDR AALA202602227499](https://openairdocs.org/sdr/AALA202602227499.md): Oil System · leaking · Feb 19, 2026 · N121UW · Airbus A320214 · Turbine Engine Oil System
  > AIRCRAFT WAS GROUNDED: AT FL340 GOT ECAM ADV, ENG 1 OIL QUANTITY. STARTED FLIGHT WITH 18 QT. TOOK SEVERAL MINUTES FOR OIL QUANTITY TO GO TO ZERO. ALL OTHER ENGINE PARAMETERS NORMAL. SEVERAL MINUTES AFTER QUANTITY AT ZERO, OIL PRESSURE DECREASED SLOWLY TO ZERO.
- [SDR AALA202501275856](https://openairdocs.org/sdr/AALA202501275856.md): Power Supply · inoperative · Jan 23, 2025 · N121UW · Airbus A320214 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHT AT ROW 3 AC BURNT OUT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL AT PASSENGER CABIN IAW AMM33-51-38-000-001-A AND AMM 33-51-38-400-001-A.
- [SDR AALA202501044927](https://openairdocs.org/sdr/AALA202501044927.md): Slat Track · corroded · Jan 2, 2025 · N121UW · Airbus A320214 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 2 UPPER FWD ON LH WING (L:0.2085 INCH, W:0.0215 INCH, D:0.001 INCH. MAINTENANCE REPLACED SLAT TRACK 2 IAW JOB CARD 26C51057005.
- [SDR AALA202411290198](https://openairdocs.org/sdr/AALA202411290198.md): Floor Panel · delaminated · Nov 25, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR PANEL 261BG INSERTS AT AFT GALLEY AREA. PERFORMED VISUAL AND TAP TEST INSPECTION NOT FOUND CORROSION WAS FOUND DELAMINATION. MAINTENANCE REPLACED FLOOR PANEL 261BG AT AFT GALLEY AREA WITH NEW REPLACEMENT MATERIAL I
- [SDR AALA202411291735](https://openairdocs.org/sdr/AALA202411291735.md): Floor Panel · delaminated · Nov 24, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261PF AT AFT GALLEY AREA. MAINTENANCE REPLACED FLOOR PANEL 261PF AT AFT GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV.L.
- [SDR AALA202411297716](https://openairdocs.org/sdr/AALA202411297716.md): Floor Panel · delaminated · Nov 24, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 242LF AT PASSENGER CABIN. MAINTENANCE REPLACED FLOOR PANEL 242LF AT PASSENGER CABIN A WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV. L.
- [SDR AALA202412020223](https://openairdocs.org/sdr/AALA202412020223.md): Bolt · corroded · Nov 18, 2024 · N121UW · Airbus A320214 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LEFT WING LEADING EDGE SLAT TRACK #1 UPPER AFT BOLT. REPLACED BOLT PER TASK CARD 26C51057005.
- [SDR AALA202411251149](https://openairdocs.org/sdr/AALA202411251149.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR RH HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM #1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM AMM 55-16-42-400-001-A.
- [SDR AALA202411253458](https://openairdocs.org/sdr/AALA202411253458.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZE R. REPLACED ELEVATOR HINGE ARM #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM AMM 55-16-42-400-001-A.
- [SDR AALA202411250550](https://openairdocs.org/sdr/AALA202411250550.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZE R. REPLACED ELEVATOR HINGE ARM #4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM AMM 55-16-42-400-001-A.
- [SDR AALA202411255125](https://openairdocs.org/sdr/AALA202411255125.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZE R. REPLACED ELEVATOR HINGE ARM #5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM AMM 55-16-42-400-001-A.
- [SDR AALA202411254614](https://openairdocs.org/sdr/AALA202411254614.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM #3 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A, IAW AMM 55-16-42-400-001-A AND NCN 6852346.
- [SDR AALA202411252156](https://openairdocs.org/sdr/AALA202411252156.md): Hinge Arm · excess play · Nov 14, 2024 · N121UW · Airbus A320214 · Elevator Structure
  > AIRCRAFT WAS NOT GROUNDED: EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZE R. REPLACED HINGE ARM #2 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND IAW AMM 55-16-42-400-001-A.
- [SDR AALA202411130705](https://openairdocs.org/sdr/AALA202411130705.md): Floorbeam · worn · Nov 10, 2024 · N121UW · Airbus A320214 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR BEAM SECTION CONNECTING (SPLICE) HAS ELONGATED HOLE AT FR 68 AND +Y1162. REPLACED FLOOR BEAM SECTION CONNECTING (SPLICE) PER SRM 51-42-11.
- [SDR AALA202501216219](https://openairdocs.org/sdr/AALA202501216219.md): Fitting · none · Nov 8, 2024 · N121UW · Airbus A320214 · Standard Practices/Structures
  > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 3 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 359265. REPLACED RIGHT HAND CON
- [SDR AALA202501216395](https://openairdocs.org/sdr/AALA202501216395.md): Fitting · none · Nov 8, 2024 · N121UW · Airbus A320214 · Standard Practices/Structures
  > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 3 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 359265. REPLACED LEFT HAND CONTI
- [SDR AALA202412028717](https://openairdocs.org/sdr/AALA202412028717.md): Floor Panel · corroded · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR PANEL 262BG INSERTS AT AFT GALLEY AREA. MAINTENANCE REPLACED FLOOR PANEL 262BG AT AFT GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV L.
- [SDR AALA202411253246](https://openairdocs.org/sdr/AALA202411253246.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 242BF AT PASSENGER CABIN. REPLACED FLOOR PANEL 242BF AT PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV.L
- [SDR AALA202411250062](https://openairdocs.org/sdr/AALA202411250062.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 221EF INSERT AT FWD GALLEY AREA. REPLACED FLOOR PANEL 221EF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411256425](https://openairdocs.org/sdr/AALA202411256425.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 221DF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 221DF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411258378](https://openairdocs.org/sdr/AALA202411258378.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 222EF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 222EF AT FWD GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411251402](https://openairdocs.org/sdr/AALA202411251402.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261AG AT AFT GALLEY AREA. REPLACED FLOOR PANEL 261AG AT AFT GALLEY AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV.L
- [SDR AALA202411257441](https://openairdocs.org/sdr/AALA202411257441.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 231CF AT PASSENGER CABIN. REPLACED FLOOR PANEL 231CF AT PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411254115](https://openairdocs.org/sdr/AALA202411254115.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 232EF AT PASSENGER CABIN. REPLACED FLOOR PANEL 232EF AT PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411254602](https://openairdocs.org/sdr/AALA202411254602.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 231FF AT PASSENGER CABIN. REPLACED FLOOR PANEL 231FF AT PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-12-00-300-006 AND IRM 9701 REV.L
- [SDR AALA202411229987](https://openairdocs.org/sdr/AALA202411229987.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 231KF AT PASSENGER CABIN. MAINTENANCE REPLACED FLOOR PANEL 231KF AT PASSENGER CABIN AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM53-02-00-300-011 AND IRM 9701 REV L.
- [SDR AALA202411226156](https://openairdocs.org/sdr/AALA202411226156.md): Floor Panel · delaminated · Nov 8, 2024 · N121UW · Airbus A320214 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 241LF AT PASSENGER CABIN. MAINTENANCE REPLACED FLOORPANEL 241LF AT PASSENGER CABIN AREA WITH NEW REPLACEMENT MATERIAL IAW A320 SRM 53-02-00-300-011 AND IRM 9701 REV L.
- [SDR AALA202501210842](https://openairdocs.org/sdr/AALA202501210842.md): Door Frame · cracked · Nov 6, 2024 · N121UW · Airbus A320214 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT RIGHT HAND PASSENGER / CREW DOOR 842 AFT UPPER CORNER FRAME AT FR 68 AND S8R. REPLACED FRAME PER SRM 51-42-11.
- [SDR AALA202411217662](https://openairdocs.org/sdr/AALA202411217662.md): Door Sill · corroded · Nov 6, 2024 · N121UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 66 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 6.
- [SDR AALA202501113081](https://openairdocs.org/sdr/AALA202501113081.md): Shear Plate · cracked · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STGR23L BTW FR69 TO FR70 AT AFT GALLEY AREA (L: 0.593 INCHES.). MAINTENANCE REPLACED SHEAR PLATE LOC ON STGR 23L BTW FR68 TO FR70 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 AND DWG D53474180.
- [SDR AALA202411292297](https://openairdocs.org/sdr/AALA202411292297.md): Floorbeam · corroded · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.
- [SDR AALA202411250697](https://openairdocs.org/sdr/AALA202411250697.md): Floorbeam · corroded · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA FLOOR BEAM LOCATED AT FR 20 AND -Y1292 REPLACED FLOOR BEAM PER SRM 51-42-11-801.
- [SDR AALA202411180483](https://openairdocs.org/sdr/AALA202411180483.md): Cover · corroded · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA JOINT COVER BETWEEN FR 12 AND FR 16 AT -Y81. REPLACED JOINT COVER PER SRM 51-42-11.
- [SDR AALA202411180217](https://openairdocs.org/sdr/AALA202411180217.md): Dummy Rail · corroded · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT WAS IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA RAIL DUMMY ON Y503.2 AT FR16. REPLACED DUMMY RAIL AT FORWARD GALLEY AREA IAW A320 SRM 51-42-11-801.
- [SDR AALA202411132915](https://openairdocs.org/sdr/AALA202411132915.md): Floorbeam · corroded · Nov 5, 2024 · N121UW · Airbus A320214 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND Y1162. REPLACED FLOOR BEAM PER SRM 51-42-11.
- [SDR AALA202501289663](https://openairdocs.org/sdr/AALA202501289663.md): Skin · corroded · Nov 4, 2024 · N121UW · Airbus A320214 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 17 ON RH WING L=2.334 INCH W=1.687 INCH D=0.151 INCH. MAINTENANCE PERFORMED TIME LIMIT REOAIR (BLEND OUT R7) TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 17 ON RH WI
- [SDR AALA202501280510](https://openairdocs.org/sdr/AALA202501280510.md): Skin · corroded · Nov 4, 2024 · N121UW · Airbus A320214 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 8 (WX4349) ON RH WING L=3.561 INCH W=2.397 INCH D=0.132 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR (BLEND OUT R2) TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 8 (
- [SDR AALA202501275115](https://openairdocs.org/sdr/AALA202501275115.md): Skin · corroded · Nov 4, 2024 · N121UW · Airbus A320214 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 15 RH WING. MAINTENANCE PERFORMED TIME LIMITED REPAIR (BLEND OUT R6) TRAILING EDGE TOP SKIN LOWER SURFACE AT LEVEL RIB 15 ON RH WING IAW EA 359548 AND REPAIR INSTRUCTIONS
- [SDR AALA202411257440](https://openairdocs.org/sdr/AALA202411257440.md): Stiffener · cracked · Nov 3, 2024 · N121UW · Airbus A320214 · Fuselage Main, Bulkhead
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED STIFFENER ON THE FORWARD PRESSURE BULKHEAD FORWARD FACE AT FR 1 AND Z-1329. REPLACED STIFFENER PER SRM 51-72-11.
- [SDR AALA202412209608](https://openairdocs.org/sdr/AALA202412209608.md): Support Fitting · corroded · Nov 2, 2024 · N121UW · Airbus A320214 · Wing Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRAILING EDGE SUPPORT FITTING AT LEVEL RIB 8 ON LEFT WING. REPLACED SUPPORT FITTING PER SRM 51-42-11-801.
- [SDR AALA202411188799](https://openairdocs.org/sdr/AALA202411188799.md): Skin · debonded · Nov 1, 2024 · N121UW · Airbus A320214 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: DEBONDED OUTBOARD FLAP LOWER SURFACE ON LEFT-HAND WING LOCATED BETWEEN RIB 12 AND RIB 15. PERFORMED PERMANANT REPAIR ON OUTBOARD FLAP LOWER SURFACE PER SRM 57-53-00-300-120.
- [SDR AALA202501212734](https://openairdocs.org/sdr/AALA202501212734.md): Window Frame · cracked · Oct 28, 2024 · N121UW · Airbus A320214 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE RIGHT HAND CENTER POST AREA. REPAIRED WINDSHIELD FRAMING PER EA 359265.
- [SDR AALA202501216150](https://openairdocs.org/sdr/AALA202501216150.md): Window Frame · cracked · Oct 28, 2024 · N121UW · Airbus A320214 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE LEFT HAND CENTER POST AREA. REPAIRED WINDSHIELD FRAMING PER EA 359265.
- [SDR AALA202501289406](https://openairdocs.org/sdr/AALA202501289406.md): Skin · corroded · Oct 27, 2024 · N121UW · Airbus A320214 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN UPPER SURFACE BTW RIB 8 TO RIB 9 RH WING CORRODED AREA IS L= 1.441 IN, W= 1.060 IN, D=0.002 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON TRAILING EDGE TOP SKIN UP
- [SDR AALA202501274237](https://openairdocs.org/sdr/AALA202501274237.md): Skin · corroded · Oct 27, 2024 · N121UW · Airbus A320214 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LEADING EDGE TOP SKIN UPPER SURFACE BETWEEN RIB 19 TO RIB 20 ON LH WING. MEASURE L=1.074 W=0.861 D= 0.002 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (BLEND OUT R9) LEADING EDGE TOP SKIN UPPER SURFACE BETWEEN RIB 19
- [SDR AALA202406116242](https://openairdocs.org/sdr/AALA202406116242.md): Power Supply · no test · Jun 11, 2024 · N121UW · Airbus A320214 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: AFT LEFT EMERGENCY POWER SUPPLY UNIT FAULT DISPLAYED DURING TESTING. REPLACED AFT LEFT EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.
- [SDR AALA202405305864](https://openairdocs.org/sdr/AALA202405305864.md): Hinge Fitting · lack of lube · May 29, 2024 · N121UW · Airbus A320214 · Fuselage, Door Hinge
  > AIRCRAFT WAS GROUNDED: R/H FWD DOOR HARD TO CLOSE AND MAKES A GRINDING NOISE WHEN MOVING. LUBRICATED R1 DOOR HINGE ARM SUPPORT FITTING.
- [SDR AALA202404126397](https://openairdocs.org/sdr/AALA202404126397.md): Cradle · defective · Apr 11, 2024 · N121UW · Airbus A320214 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASHLIGHT BRACKET WILL NOT HOLD THE FLASHLIGHT. MAINTENANCE REPLACED THE FLASHLIGHT BRACKET.

Next page: https://openairdocs.org/aircraft/N121UW/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 = 'N121UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N121UW/reports

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