# Service difficulty reports: N748UW

A list on [N748UW](https://openairdocs.org/aircraft/N748UW.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 · 215 reports

- [SDR AALA202609279519](https://openairdocs.org/sdr/AALA202609279519.md): Wire Harness · defective · Sep 25, 2026 · N748UW · Airbus A319112 · Light System Wiring
  > AIRCRAFT WAS GROUNDED: SEAT MOUNTED EMERGENCY LIGHTS WILL NOT ILLUMINATE ROWS 24 AND 25 ABC -MAINTENANCE REPLACED HARNESS 26-3351-3-0057 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED
- [SDR AALA202609089848](https://openairdocs.org/sdr/AALA202609089848.md): Apu · odor · Sep 7, 2026 · N748UW · Airbus A319112 · Airborne Auxiliary Power Unit (APU) System
  > AIRCRAFT WAS GROUNDED: STRONG SOCK SMELL THROUGH 6,000 FT IN DESCENT WHICH CLEARED UP AFTER MAYBE A MINUTE - THE FLIGHT CREW REPORTED THAT DURING PREFLIGHT PREP FOR NEXT FLIGHT THE SMELL RETURNED MUCH STRONGER WITH IT BEING THE STONGEST IN THE FLIGHT DECK AND
- [SDR AALA202606174586](https://openairdocs.org/sdr/AALA202606174586.md): Elec Connector · broken · Jun 15, 2026 · N748UW · Airbus A319112 · Light System Wiring
  > AIRCRAFT IN BASE MAINTENANCE: IN SEAT EMERGENCY LIGHT CONNECTOR BROKEN AT FLOOR AT ROW 23ABC. MAINTENANCE REPAIRED EMERGENCY LIGHT CONNECTOR 7260VC8 PER ESPM 20-44-10 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED.
- [SDR AALA202601124703](https://openairdocs.org/sdr/AALA202601124703.md): Bottle · low pressure · Jan 11, 2026 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L2 CABIN DOOR EMERGENCY ASSIST ACCUMULATOR REQUIRE SERVICING. MAINTENANCE SERVICED CYLINDER IAW AMM 52-10-00.
- [SDR AALA202505121776](https://openairdocs.org/sdr/AALA202505121776.md): Power Supply · inoperative · May 9, 2025 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS GROUNDED: EMERGENCY PATH LIGHTING INOP AT ROWS, 17ABC, 18ABC, 19ABC, 22ABC, 23ABC, 26ABC, 27ABC. MAINTENANCE REPLACED BATTERY EMERGENCY POWER SUPPLY UNIT (EPSU) 13WL IAW AMM 33-51-38.
- [SDR AALA202503254780](https://openairdocs.org/sdr/AALA202503254780.md): Battery · inoperative · Mar 24, 2025 · N748UW · Airbus A319112 · Emergency Equipment
  > COMPONENT IN SHOP MAINTENANCE: FLIGHT ATTENDANT FLASHLIGHT BY THE 2R DOOR BATTERY INDICATOR NOT FLASHING/LOW BATTERY. R/R BATTERY, OPS CK OF FLASHLIGHT GOOD.
- [SDR AALA202412307612](https://openairdocs.org/sdr/AALA202412307612.md): Power Supply · inoperative · Dec 29, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: OVER WING EMERGENCY LIGHTS EPSU LEFT, RIGHT AND AFT INOP. MAINTENANCE REPLACED EPSU BATTERY IAW AMM 33-51-38.
- [SDR AALA202412120943](https://openairdocs.org/sdr/AALA202412120943.md): Power Supply · inoperative · Dec 10, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP EMERGENCY POWER SUPPLY UNIT (EPSU) AT AFT CABIN UTILITY AREA. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT EPSU (13WL) AT AFT CABIN UTILITY AREA IAW AMM 33-51-38-400-001-A.
- [SDR AALA202412111741](https://openairdocs.org/sdr/AALA202412111741.md): Beam · cracked · Dec 10, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 2 ZONE 1. CRACK DEPTH IS 0.145INCH AND CRACK DIRECTION IS 7 OCLOCK. MAINTENANCE PERFORMED INTERIM REPAIR ON FASTENER HOLE OF
- [SDR AALA202412100496](https://openairdocs.org/sdr/AALA202412100496.md): Light · broken · Dec 9, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN LIGHTS EMERGENCY (ASSY) IN DOOR FRAME AT DOORS 831. MAINTENANCE REPLACED LIGHTS EMERGENCY IN DOOR FRAME AT DOORS 831 IAW AMM 33-51-13-000-001-A STEP 1. THRU 4.A.(1). AND AMM 33-51-13-400-001-A STEP 1. THRU 5.
- [SDR AALA202412103801](https://openairdocs.org/sdr/AALA202412103801.md): Light · broken · Dec 9, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN LIGHTS EMERGENCY (ASSY) IN DOOR FRAME AT DOORS 841. MAINTENANCE REPLACED LIGHTS EMERGENCY IN DOOR FRAME AT DOORS 841 IAW AMM 33-51-13-000-001-A STEP 1. THRU 4.A.(1). AND AMM 33-51-13-400-001-A STEP 1. THRU 5.
- [SDR AALA202412107795](https://openairdocs.org/sdr/AALA202412107795.md): Light · broken · Dec 9, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN LIGHTS EMERGENCY (ASSY) IN DOOR FRAME AT DOORS 832. MAINTENANCE REPLACED LIGHTS EMERGENCY IN DOOR FRAME AT DOORS 832 IAW AMM 33-51-13-000-001-A STEP 1. THRU 4.A.(1). AND AMM 33-51-13-400-001-A STEP 1. THRU 5.
- [SDR AALA202412101082](https://openairdocs.org/sdr/AALA202412101082.md): Light · broken · Dec 9, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN LIGHTS EMERGENCY (ASSY) IN DOOR FRAME AT DOORS 842. MAINTENANCE REPLACED LIGHTS EMERGENCY IN DOOR FRAME AT DOORS 842 IAW AMM 33-51-13-000-001-A STEP 1. THRU 4.A.(1). AND AMM 33-51-13-400-001-A STEP 1. THRU 5.
- [SDR AALA202412099972](https://openairdocs.org/sdr/AALA202412099972.md): Bottle · inoperative · Dec 7, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER PASSENGER DOOR 832 AT AFT GALLEY AREA IAW AMM 52-13-14-000-001-B AND AMM 5
- [SDR AALA202412098413](https://openairdocs.org/sdr/AALA202412098413.md): Bottle · no test · Dec 7, 2024 · N748UW · Airbus A319112 · Emergency Equipment
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR CYLINDER PASSENGER DOOR 832 AT AFT GALLEY AREA IAW AMM 52-13-14-000-001-B AND AMM
- [SDR AALA202412020778](https://openairdocs.org/sdr/AALA202412020778.md): Spring · broken · Dec 1, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN PERCUSSION MECHANISM SPRING ON THE EMERGENCY DOOR DAMPER AND OPERATION CYLINDER AT PASSENGER CREW DOOR 831 AT FWD GALLEY. MAINTENANCE REPLACED PERCUSSION MECHANISM SPRING ON THE EMERGENCY DOOR DAMPER AND OPERATION CYLINDER
- [SDR AALA202411187060](https://openairdocs.org/sdr/AALA202411187060.md): Stop Fitting · worn · Nov 14, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: WEAR DOOR STOP PASSENGER CREW DOOR 842 FWD POSITION 1. MAINTENANCE REPLACED DOOR STOP PASSENGER CREW DOOR 842 FWD POSITION #1 IAW AMM 52-13-31-000-002-A AND AMM 52-13-31-400-002-A.
- [SDR AALA202411187100](https://openairdocs.org/sdr/AALA202411187100.md): Stop Fitting · worn · Nov 14, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: WEAR DOOR STOP PASSENGER CREW DOOR 842 AFT POSITION 5. MAINTENANCE REPLACED DOOR STOP PASSENGER CREW DOOR 842 AFT POSITION #5 IAW AMM 52-13-31-000-002-A AND AMM 52-13-31-400-002-A.
- [SDR AALA202411144787](https://openairdocs.org/sdr/AALA202411144787.md): Stop Fitting · worn · Nov 12, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 HAS 3 WORN DOOR STOPS ON THE AFT SIDE. REPLACED DOOR STOPS PER AMM 52-13-31-000-002-A AND 52-13-31-400-002-A.
- [SDR AALA202410228762](https://openairdocs.org/sdr/AALA202410228762.md): Bolt · corroded · Oct 17, 2024 · N748UW · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SLAT TRACK #3 UPPER BOLT BETWEEN WS 1957 AND WS 2580, BETWEEN RIBS 4 AND 5. REPLACED BOLT PER TASK CARD 26C61057005 AND AMM 27-84-63.
- [SDR AALA202410168497](https://openairdocs.org/sdr/AALA202410168497.md): Hinge Arm · excess play · Oct 14, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202410160432](https://openairdocs.org/sdr/AALA202410160432.md): Hinge Arm · excess play · Oct 14, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202410167149](https://openairdocs.org/sdr/AALA202410167149.md): Hinge Arm · excess play · Oct 14, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202410166080](https://openairdocs.org/sdr/AALA202410166080.md): Hinge Arm · excess play · Oct 14, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #6 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202410164779](https://openairdocs.org/sdr/AALA202410164779.md): Hinge Arm · excess play · Oct 13, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202410165744](https://openairdocs.org/sdr/AALA202410165744.md): Hinge Arm · excess play · Oct 13, 2024 · N748UW · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.
- [SDR AALA202412113959](https://openairdocs.org/sdr/AALA202412113959.md): Fitting · cracked · Oct 12, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CONTINUITY FITTING LH MUST BE REPLACED IAW EA 358461.MAINTENANCE REPLACED CONTINUITY FITTING LH SIDE LOC ON WINDSHIELD CENTER POST AREA IAW EA 358461.
- [SDR AALA202412118920](https://openairdocs.org/sdr/AALA202412118920.md): Fitting · cracked · Oct 12, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CONTINUITY FITTING RH MUST BE REPLACED IAW EA# 358461. MAINTENANCE REPLACED CONTINUITY FITTING RH LOC ON WINDSHIELD CENTER POST AREA IAW EA #358461.
- [SDR AALA202411046282](https://openairdocs.org/sdr/AALA202411046282.md): Fitting · corroded · Oct 12, 2024 · N748UW · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING ON LH PYLON BETWEEN RIB 4 AND RIB 5 L=9.423 INCH, W=2.585 INCH, D=0.008 INCH. CORRODED AREA. MAINTENANCE REPLACED FITTING BETWEEN RIB 4 AND RIB 5 ON LH PYLON IAW A319 SRM 54-51-12-300-001.
- [SDR AALA202411042833](https://openairdocs.org/sdr/AALA202411042833.md): Spigot · corroded · Oct 12, 2024 · N748UW · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING ON RIGHT HAND PYLON. REPLACED SPIGOT FITTING BETWEEN RIB 4 TO RIB 5 PER A319 SRM 54-51-12
- [SDR AALA202412128988](https://openairdocs.org/sdr/AALA202412128988.md): Pressure Deck · cracked · Oct 11, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE LOC FR 36 RH SIDE AT 3 IN CH OF -Y1292. PRESSURE DECK AREA. CRACK AT 12 O CLOCK.HOLE DIAMETER I S 0.194 INCH. D1-D2 0.099 INCH. PERFORMED TIME LIMITED REPAIR LOC ON FR 36 RH SIDE AT
- [SDR AALA202412124272](https://openairdocs.org/sdr/AALA202412124272.md): Pressure Deck · cracked · Oct 11, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE LOC FR 36 LH SIDE AT 2 IN CH OF Y1292. PRESSURE DECK AREA. CRACK AT 12 O CLOCK.HOLE DIAMETER IS 0.194 INCH. D1-D2 0.079 INCH. PERFORMED TIME LIMITED REPAIR LOC ON FR 36 LH SIDE AT 2
- [SDR AALA202411264866](https://openairdocs.org/sdr/AALA202411264866.md): Bushing · excess play · Oct 11, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BUSHINGS ON UPPER AND LOWER CONNECTION LINK BTW SUPPORT ARM PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACE BUSHINGS ON UPPER AND LOWER CONNECTION LINK BTW SUPPORT ARM PASSENGER CREW DOOR 832 AT AFT
- [SDR AALA202412069886](https://openairdocs.org/sdr/AALA202412069886.md): Bellcrank · out of adjust · Oct 9, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: OUT OF ADJUSTMENT OF THE TORSION BAR BELLCRANK ON PASSENGER CREW DOOR 841 AT FWD GALLEY AREA. MAINTENANCE PERFORMED ADJUSTMENT OF THE TORSION BAR BELLCRANK ON PASSENGER CREW DOOR 841 AT FWD GALLEY AREA IAWAMM 52-11-21-400-001-A S
- [SDR AALA202412022031](https://openairdocs.org/sdr/AALA202412022031.md): Bushing · excess play · Oct 9, 2024 · N748UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BUSHING UPPER AND LOWER CONNECTION LINKS AND SUPPORT ARM ON PASSENGER CREW DOOR 831 AT FWD GALLEY AREA). MAINTENANCE REPLACED BUSHINGS ON UPPER AND LOWER CONNECTION LINKS AND SUPPORT ARM ON PASSENGER CREW DOOR 83
- [SDR AALA202411199502](https://openairdocs.org/sdr/AALA202411199502.md): Hinge Fitting · cracked · Oct 7, 2024 · N748UW · Airbus A319112 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON KEEL BEAM CRACKED AT FR 42 AND S41R. REPLACED HINGE FITTING PER EA 358735.
- [SDR AALA202410190466](https://openairdocs.org/sdr/AALA202410190466.md): Seat Track · corroded · Oct 5, 2024 · N748UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 20 AND FR 21 AT -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.
- [SDR AALA202410161892](https://openairdocs.org/sdr/AALA202410161892.md): Floorbeam · corroded · Oct 5, 2024 · N748UW · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 24 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.
- [SDR AALA202412099973](https://openairdocs.org/sdr/AALA202412099973.md): Pressure Deck · cracked · Oct 4, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN FASTENER HOLES AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 358669.
- [SDR AALA202412094716](https://openairdocs.org/sdr/AALA202412094716.md): Pressure Deck · cracked · Oct 4, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN FASTENER HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 358669.
- [SDR AALA202412113987](https://openairdocs.org/sdr/AALA202412113987.md): Beam · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 2 ZONE 2. CRACK DEPTH IS 0.219 INCH AND CRACK DIRECTION IS 9 OCLOCK. MAINTENANCE PERFORMED INTERIM REPAIR ON FASTENER HOLE O
- [SDR AALA202412117770](https://openairdocs.org/sdr/AALA202412117770.md): Beam · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 5 ZONE 2. (CRACK DEPTH: 0.202 INCHES). MAINTENANCE ACCOMPLISHED REPAIR LOC. HORIZONTAL FLOOR BEAM AND VERTICAL STRINGER IN CEN
- [SDR AALA202412116958](https://openairdocs.org/sdr/AALA202412116958.md): Beam · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 4 ZONE 1 (CRACK DEPTH:0.212 INCHES). MAINTENANCE ACCOMPLISHED REPAIR ON HORIZONTAL FLOOR BEAM AND VERTICAL STRINGER IN CENTER
- [SDR AALA202412111981](https://openairdocs.org/sdr/AALA202412111981.md): Stringer · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND OF FASTENER HOLE OF SPAR VERTICAL STRINGER IN CENTER FUSELAGE ON FRAME 36 NUMBER 3 ZONE 1 (CRACK DEPTH: 0.183 INCHES). MAINTENANCE ACCOMPLISHED REPAIR ON HORIZONTAL FLOOR BEAM AND VERTICAL STRINGER IN CENTER
- [SDR AALA202411278811](https://openairdocs.org/sdr/AALA202411278811.md): Shear Plate · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202411191792](https://openairdocs.org/sdr/AALA202411191792.md): Shear Plate · cracked · Oct 3, 2024 · N748UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE STR 23L BETWEEN FR 69 AND FR 70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-42-11-801.
- [SDR AALA202412110986](https://openairdocs.org/sdr/AALA202412110986.md): Window Post · cracked · Sep 28, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH WINDSHIELD VERTICAL CENTER POST UPPER SPOTFACE AREA, CRACK DIRECTION IS AT 2 O CLOCK LOOKING INB, L=0.200. MAINTENACE PERFORMED TIME LIMIT REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LH/RH S
- [SDR AALA202412115764](https://openairdocs.org/sdr/AALA202412115764.md): Window Post · cracked · Sep 28, 2024 · N748UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH WINDSHIELD VERTICAL CENTER POST UPPER SPOTFACE AREA, CRACK DIRECTION IS AT 10 O CLOCK LOOKING INB, L=0.200. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SI
- [SDR AALA202406143037](https://openairdocs.org/sdr/AALA202406143037.md): Connector · damaged · Jun 14, 2024 · N748UW · Airbus A319112 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: DURING A FUNCTIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM MAINTENANCE FOUND SEAT ROWS 18ABC AND 19ABC EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND BROKEN PINS ON CONNECTOR 7260VC6 AND REPLACED THE BROKEN PINS PER ESPM 20-4
- [SDR AALA202403118980](https://openairdocs.org/sdr/AALA202403118980.md): Battery Pack · discharged · Mar 9, 2024 · N748UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHTS BATTERIES DEPLETED. REPLACED EMERGENCY BATTERY PACK CABIN.

Next page: https://openairdocs.org/aircraft/N748UW/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 = 'N748UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N748UW/reports

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