# Service difficulty reports: N754UW

A list on [N754UW](https://openairdocs.org/aircraft/N754UW.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 4 · 168 reports

- [SDR AALA202609306610](https://openairdocs.org/sdr/AALA202609306610.md): Lamp · inoperative · Sep 27, 2026 · N754UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT (RED) ON FORWARD LEFT CLOSET INOP. MAINTENANCE REPLACED LAMP AT FORWARD LEFT CLOSET PER AMM 33-51-18. OPS CHECKED GOOD.
- [SDR AALA202608111778](https://openairdocs.org/sdr/AALA202608111778.md): Power Supply · no test · Aug 10, 2026 · N754UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED DURING SYSTEM TEST - MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11W PER AMM 33-51-38
- [SDR AALA202606305590](https://openairdocs.org/sdr/AALA202606305590.md): Battery · no test · Jun 27, 2026 · N754UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FAULT EPSU BATTERY FWD L. DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202606305101) AND BATTERY (AALA202606305590) PER AMM 33-51-38.
- [SDR AALA202606305101](https://openairdocs.org/sdr/AALA202606305101.md): Power Supply · no test · Jun 27, 2026 · N754UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: FAULT EPSU BATTERY FWD L. DISPLAYED DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202606305101) AND BATTERY (AALA202606305590) PER AMM 33-51-38.
- [SDR AALA202606031777](https://openairdocs.org/sdr/AALA202606031777.md): Manifold · defective · Jun 2, 2026 · N754UW · Airbus A319112 · Landing Gear Brake System
  > AIRCRAFT IN BASE MAINTENANCE: DURING TAXI FOR TAKEOFF, EVERY TIME THE RIGHT BRAKE IS DEPRESSED IT GRABS AND JOLTS THE AIRCRAFT. BRAKE TEMPS HIGHER ON BOTH RIGHT BRAKE TEMP INDICATORS. 60 DEGREES ON LEFT AND 220 ON RIGHT. MAINTENANCE REPLACED THE RIGHT-HAND NOR
- [SDR AALA202601273637](https://openairdocs.org/sdr/AALA202601273637.md): Battery · abnormal · Jan 26, 2026 · N754UW · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS FLASHLIGHT AT THE L2 DOOR NOT WORKING. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202511249808](https://openairdocs.org/sdr/AALA202511249808.md): Actuator · leaking · Nov 18, 2025 · N754UW · Airbus A319112 · Engine Thrust Reverser
  > AIRCRAFT WAS GROUNDED: LAV SMOKE DETECTOR WENT OFF AND CABIN FILLED WITH A LIGHT HAZE. SMOKE DISCAPATED AS WE HEADED TO THE GATE. UPON ENGINE #2 INSPECTION MAINTENANCE FOUND UPPER OUTBOARD THRUST REVERSER ACTUATOR LEAKING AND SUSPECTED IT AS SOURCE FOR ODORS.
- [SDR AALA202511199808](https://openairdocs.org/sdr/AALA202511199808.md): Actuator · leaking · Nov 18, 2025 · N754UW · Airbus A319112 · Engine Thrust Reverser
  > AIRCRAFT WAS GROUNDED: LAV SMOKE DETECTOR WENT OFF AND CABIN FILLED WITH A LIGHT HAZE. SMOKE DISCAPATED AS WE HEADED TO THE GATE. UPON ENGINE #2 INSPECTION MAINTENANCE FOUND UPPER OUTBOARD THRUST REVERSER ACTUATOR LEAKING AND SUSPECTED IT AS SOURCE FOR ODORS.
- [SDR AALA202510209177](https://openairdocs.org/sdr/AALA202510209177.md): Flap System · warning message · Oct 17, 2025 · N754UW · Airbus A319112 · Trailing Edge Flap Control System
  > AIRCRAFT WAS GROUNDED: AFTER TAKEOFF WHEN RAISING THE FLAPS TO UP POSITION, F/CTL FLAPSFAULT CAUTION MESSAGE APPEARED. ECAM ACTIONS DID NOT RECTIFY SITUATION. AFTER TROUBLESHOOTING AND QRH PROCEDURES, IT WAS DETERMINED THAT FLAPS TWO AND THREE POSITIONS CLEA
- [SDR AALA202505081394](https://openairdocs.org/sdr/AALA202505081394.md): Control Unit · inoperative · May 5, 2025 · N754UW · Airbus A319112 · Landing Gear Steering System
  > AIRCRAFT WAS GROUNDED: AFTER TAKE OFF WE RECEIVED A NOSE STEERING FAULT AND A BRAKE SYSTEM 1 FAULT ON THE ECAM. BRAKE SYSTEM 1 IN FLIGHT QRH PROCEDUREPERFORMED AND CLEARED BOTH FAULTS. DISCUSSION WITH COMPANY ANDMOC RECOMMENDED RETURN TO CLT. UPON LANDING NO
- [SDR AALA202505023921](https://openairdocs.org/sdr/AALA202505023921.md): Sensor · faulted · Apr 30, 2025 · N754UW · Airbus A319112 · Landing Gear Steering System
  > AIRCRAFT WAS GROUNDED: WHEEL N/S STEERING FAULT IN FLIGHT AFTER STARTED DESCENT FROM FL370. DIVERTED TO POP. EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE WHEEL STEERING FEED BACK SENSOR BOX 3GC IAW AMM 32-51-19-400-002.
- [SDR AALA202504140483](https://openairdocs.org/sdr/AALA202504140483.md): Shear Plate · cracked · Apr 7, 2025 · N754UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L BTW FR69 AND FR70 AT AFT GALLEY AREA, MEASURE OF CRACK IS: L:1.054 INCH. MAINTENANCE REPLACED SHEAR PLATE LOCATED STR 23 L BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53474180
- [SDR AALA202504145015](https://openairdocs.org/sdr/AALA202504145015.md): Attach Bolt · corroded · Mar 29, 2025 · N754UW · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 2 UPPER AFT BOLT ON RH WING. L=0.340 INCH, W=0.047 INCH, D=0.002 INCH. MAINTENANCE
- [SDR AALA202504242982](https://openairdocs.org/sdr/AALA202504242982.md): Door Frame · cracked · Feb 27, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON DOOR FRAME LOC. BTW FR67 TO FR68 AT LEVEL STG8 LH AFT GALLEY AREA, CRACK L=0.134 INCH.
- [SDR AALA202504089626](https://openairdocs.org/sdr/AALA202504089626.md): Lintel · cracked · Feb 27, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON LINTEL LOC. BTW FR66 AND FR68 AT LEVEL STGR 8L UPPER FUSELAGE, MEASURE OF CRACK L= 0.135 IN. MAINTENANCE REPLACED LINTEL LOC. BTW FR66 AND FR68 AT LEVEL OF STGR 8L UPPER FUSELAGE, IAW A319 SRM 51-42-11-801 AND DWG D53480
- [SDR AALA202502244923](https://openairdocs.org/sdr/AALA202502244923.md): Hinge Fitting · excess play · Feb 23, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH HORIZONTAL STABILIZER (1EA) IAW AMM 55-16 42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202502245200](https://openairdocs.org/sdr/AALA202502245200.md): Hinge Fitting · excess play · Feb 20, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BUSHING ATTACH FITTING HINGE ARM END FITTING 4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202502244268](https://openairdocs.org/sdr/AALA202502244268.md): Hinge Fitting · excess play · Feb 20, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202503207548](https://openairdocs.org/sdr/AALA202503207548.md): Splice · cracked · Feb 16, 2025 · N754UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED / BROKEN UPPER SPLICE / SECTION CONNECTING AT FR 57 AND S24R. REPLACED SPLICE PER SRM 51-42-11.
- [SDR AALA202504240476](https://openairdocs.org/sdr/AALA202504240476.md): Door Frame · cracked · Feb 11, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT THE AFT FACE OF FR68 WEB JOINT TO THE DOOR FRAME LEVEL OF STR 8L. CRACK L=0.700 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR AFT FACE OF FR68 WEB JOINT TO THE DOOR FRAME LEVEL OF STR 8L IAW EA362281.
- [SDR AALA202504017570](https://openairdocs.org/sdr/AALA202504017570.md): Hinge Fitting · cracked · Feb 11, 2025 · N754UW · Airbus A319112 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON MAIN LANDING DOOR HINGE FITTING AFT FACE AT WEB RADIUS LEFT SIDE, CRACK L=0.187. MAINTENANCE PERFORMED PERMANENT REPAIR (PART REPLACEMENT ENTIRE) ON FWD HINGE FITTING OF MAIN LANDING DOOR LOC. FR42 AT LEVEL S
- [SDR AALA202503247528](https://openairdocs.org/sdr/AALA202503247528.md): Hinge Pin · corroded · Feb 11, 2025 · N754UW · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #5 HINGE PIN BETWEEN RIBS 26 AND 27. REPLACED HINGE PIN PER AMM 27-14-41-400-001-A.
- [SDR AALA202503247811](https://openairdocs.org/sdr/AALA202503247811.md): Hinge Pin · corroded · Feb 11, 2025 · N754UW · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #4 HINGE PIN BETWEEN RIBS 26 AND 27. REPLACED HINGE PIN PER AMM 27-14-41-400-001-A.
- [SDR AALA202503245421](https://openairdocs.org/sdr/AALA202503245421.md): Frame · cracked · Feb 10, 2025 · N754UW · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED MAIN CABIN FRAME FITTING AT FR 57 AND S23R. REPLACED FRAME FITTING PER SRM 51-42-11.
- [SDR AALA202503249235](https://openairdocs.org/sdr/AALA202503249235.md): Seat Track · corroded · Feb 6, 2025 · N754UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 16 AND FR 20 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.
- [SDR AALA202502264156](https://openairdocs.org/sdr/AALA202502264156.md): Hinge Arm · excess play · Feb 6, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE END ARM #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202502219990](https://openairdocs.org/sdr/AALA202502219990.md): Hinge Fitting · excess play · Feb 6, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING 3 ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER (1EA) IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202502214011](https://openairdocs.org/sdr/AALA202502214011.md): Hinge Fitting · excess play · Feb 6, 2025 · N754UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING 2 ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER (1EA) IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202504217516](https://openairdocs.org/sdr/AALA202504217516.md): Shear Plate · cracked · Feb 5, 2025 · N754UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA, CRACK MEASURE IS L=1.029 INCH. MAINTENANCE REPLACED SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53474180.
- [SDR AALA202504211839](https://openairdocs.org/sdr/AALA202504211839.md): Skin · corroded · Feb 4, 2025 · N754UW · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION EXTERNAL SKIN UNDER ACCESS PANEL 321AL ON UPPER FUSELAGE, MEASURE CORROSION ARE L=1.264 INCH W=1.135 INCH D=0.008 INCH.
- [SDR AALA202503052019](https://openairdocs.org/sdr/AALA202503052019.md): Stop Fitting · out of adjust · Feb 4, 2025 · N754UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: OUT OF ADJUSTMENT DOOR STOP SCREWS ON PASSENGER CREW DOOR 841 ATFWD G ALLEY AREA. INSTALLED TOOL BALLAST WEIGHT 98D52103501000 WHICH IS REQUIRED PRIOR TO ADJUSTMENT PROCESS. I.A.W AMM 52-11-00-820-001-A STEP3.F. MAINTENANCE PERF
- [SDR AALA202504259587](https://openairdocs.org/sdr/AALA202504259587.md): Floorbeam · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON FRAME 36 IN FWD CARGO COMPARTMENT FLOOR BEAM 3 (+Y254) DIMENSION OF CRACK L=0.100 IN. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) ON FLOOR BEAM POSITION 3 (+Y254) ON FRAME 36 IAW EA361963.
- [SDR AALA202504246939](https://openairdocs.org/sdr/AALA202504246939.md): Frame · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FR36 IN FWD CARGO COMPARTMENT CRACK INDICATION FOUND ON OPEN HOLE ZONE 1 POSITION 2 FR36. CRACK DIRECTION IS 1 AND 5 OCLOCK, LENGTH 0.100 INCH.
- [SDR AALA202504248115](https://openairdocs.org/sdr/AALA202504248115.md): Frame · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FR36 IN FWD CARGO COMPARTMENT (CRACK INDICATION FOUND ON OPEN HOLE ZONE 2 POSITION 2 FR36. CRACK DIRECTION IS 11 OCLOCK, LENGTH 0.100 INCH). MAINTENANCE ACCOMPLISHED INTERIM REPAIR ON OPEN HOLE ZONE 2 POSITION
- [SDR AALA202504242495](https://openairdocs.org/sdr/AALA202504242495.md): Frame · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FR36 IN FWD CARGO COMPARTMENT (CRACK INDICATION FOUND ON OPEN HOLE ZONE 2 POSITION 5 FR36. CRACK DIRECTION IS 12 OCLOCK, LENGTH 0.100 INCH). MAINTENANCE ACCOMPLISHED INTERIM REPAIR ON OPEN HOLE ZONE 2 POSITION
- [SDR AALA202504228501](https://openairdocs.org/sdr/AALA202504228501.md): Floorbeam · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON FLOOR BEAM POSITION 4 (-Y254) FRAME 36 ON OPEN HOLE ZONE 1 DIMENSION OF CRACK IS L=0.100 IN. ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) ON FLOOR BEAM POSITION 4 (-Y254) ON FRAME 36 IAW EA361963.
- [SDR AALA202504229055](https://openairdocs.org/sdr/AALA202504229055.md): Beam · cracked · Feb 2, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON OPEN HOLE ZONE 1 POSITION 5 FR36. CRACK DIRECTION IS 12 AND 9 OCLOCK, LENGTH 0.100 INCH). ACCOMPLISHED INTERIM REPAIR ON OPEN HOLE ZONE 1 POSITION 5 FR36 (-Y765) IAW EA361963.
- [SDR AALA202504245454](https://openairdocs.org/sdr/AALA202504245454.md): Fork · burred · Jan 30, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACEMENT FITTING FORK END (BURRED MATERIAL) IS REQUIRED BY EA 361774. MAINTENANCE PERFORMED INTERIM REPAIR ON FITTING FORK-END RH AND LH SIDE ON RACK 80VU LOC BTW FR 23 TO FR 24 AND AT LEVEL STR 32RH /LH LOWER AREA IAW EA 36177
- [SDR AALA202504218492](https://openairdocs.org/sdr/AALA202504218492.md): Fitting · cracked · Jan 30, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHEMENT AREA INTERNAL SIDE, MEASURE OF CRACK IS: L=0.200 INCH. REPLACED CONTINUITY FITTING RH IAW MANUAL TALLY #99 EO# 5319Y017-002. EXACTLY LOCATION IS BTW F
- [SDR AALA202504218730](https://openairdocs.org/sdr/AALA202504218730.md): Fork · burred · Jan 30, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: BURRED MATERIAL LOWER LATERAL FITTING RH SIDE RAC 80VU AFT AVIONIC, MEASURE ENLOGATED HOLE IS W=0.301 INCH.
- [SDR AALA202504072703](https://openairdocs.org/sdr/AALA202504072703.md): Fitting · cracked · Jan 30, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE, MEASURE OF CRACK IS: L=0.100 INCH. MAINTENANCE REPLACED CONTINUITY FITTING LH IAW MANUAL TALLY #99 EO #5319Y017-002. EXACTLY LOCAT
- [SDR AALA202504243737](https://openairdocs.org/sdr/AALA202504243737.md): Skin Panel · none · Jan 23, 2025 · N754UW · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: PREVIOUS REPAIR FOUND 12" X 9.5" ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 39R TO STR 43R. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 39R TO STR 43R IAW EA 362801.
- [SDR AALA202504240038](https://openairdocs.org/sdr/AALA202504240038.md): Skin Panel · none · Jan 23, 2025 · N754UW · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: EXESTING REPAIR FOUND 8" X 8", FR 62 TO FR63 AND STR 41L TO 42L. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON REAR FUSELAGE SKIN BETWEEN FR 62 TO FR63 AND STR 40LH TO STR 43LH IAW EA 362800 FOR MON REFER TO NCN 5030926.
- [SDR AALA202504217430](https://openairdocs.org/sdr/AALA202504217430.md): Door Frame · cracked · Jan 21, 2025 · N754UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON PASSENGER CREW DOOR LOCATED AT FR16 LH AT LEVEL OF THE DOOR STOP 7 HOLE 7 IN PASSENGER CABIN 1 EA CRACK DIRECT ION 9 O CLOCK MEASURE CRACK IS L=6.352 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (REPLACED PA
- [SDR AALA202404081863](https://openairdocs.org/sdr/AALA202404081863.md): Battery · inoperative · Apr 5, 2024 · N754UW · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT JUMPSEAT 1L NEEDS FLASHLIGHT. INSTALLED NEW BATTERY PACK ON FORWARD FLIGHT ATTENDANT FLASHLIGHT.
- [SDR AALA202312196192](https://openairdocs.org/sdr/AALA202312196192.md): Wire · broken · Dec 18, 2023 · N754UW · Airbus A319112 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: CREW REPORTED WIRE PULLED LOOSE UNDER SEAT 15A. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT ROW 15ABC AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202311306506](https://openairdocs.org/sdr/AALA202311306506.md): Power Supply · no test · Nov 30, 2023 · N754UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: AFT CABIN EMERGENCY POWER SUPPLY UNIT 13WL WILL NOT TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
- [SDR AALA202309256144](https://openairdocs.org/sdr/AALA202309256144.md): Sensor · leaking · Sep 23, 2023 · N754UW · Airbus A319112 · APU Oil System
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND TEH AIRCRAFT DIVERTED TO PIT: ON INITIAL CLIMB OUT, ROUGHLY 5000' THERE WAS A BRIEF OIL ODOR.THE SMELL RETURNED THE FLIFGHT ATTENDANTS REPORTED ONLY FAINT ODOR UNTIL FINAL. ON-FINAL SMELL WAS STRONG IN AFT
- [SDR AALA202309253467](https://openairdocs.org/sdr/AALA202309253467.md): Plug · leaking · Sep 23, 2023 · N754UW · Airbus A319112 · APU Oil System
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND TEH AIRCRAFT DIVERTED TO PIT: ON INITIAL CLIMB OUT, ROUGHLY 5000' THERE WAS A BRIEF OIL ODOR.THE SMELL RETURNED THE FLIFGHT ATTENDANTS REPORTED ONLY FAINT ODOR UNTIL FINAL. ON-FINAL SMELL WAS STRONG IN AFT
- [SDR AALA202308259651](https://openairdocs.org/sdr/AALA202308259651.md): Actuator · warning message · Aug 24, 2023 · N754UW · Airbus A319112 · Aircraft Fuel Distribution System
  > AIRCRAFT WAS GROUNDED: LOW PRESSURE #2 FUEL SHUT OFF VALVE SHOW AMBER AND IN TRANSIT. SHOULD BETWEEN OPEN AND CLOSED. ALL ENGINE INDICATIONS NORMAL AT FL 300 CRUISE. MAINTENANCE REPLACED THE #2 FUEL VALVE ACTUATOR PER AMM 28-24-51 AND ACCOMPLISHED A SATISFACT

Next page: https://openairdocs.org/aircraft/N754UW/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 = 'N754UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N754UW/reports

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