# Service difficulty reports: N770UW

A list on [N770UW](https://openairdocs.org/aircraft/N770UW.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 · 288 reports

- [SDR AALA202609233885](https://openairdocs.org/sdr/AALA202609233885.md): Bottle · low pressure · Sep 22, 2026 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: 2L DOOR CYLINDER PRESSURE LOW. AMB TEMP 80F, 1450 PSI. MAINTENANCE ACCOMPLISHED JOBCARD 26L80052001 FOR 2L DOOR DAMPERS. OK FOR SERVICE.
- [SDR AALA202609239610](https://openairdocs.org/sdr/AALA202609239610.md): Bottle · low pressure · Sep 22, 2026 · N770UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: 1R DOOR CYLINDER PRESSURE LOW, AMB TEMP 80F,1500 PSI. MAINTENANCE ACCOMPLISHED JOBCARD 26L80052001 FOR 1R DOOR DAMPERS. OK FOR SERVICE.
- [SDR AALA202606012772](https://openairdocs.org/sdr/AALA202606012772.md): Skin · cracked · May 27, 2026 · N770UW · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT WAS GROUNDED: CRACK ON #3 SLAT INBOARD TOP EDGE. MAINTENANCE REPLACED THE SLAT PER JOB CARD 26L000027012
- [SDR AALA202602276645](https://openairdocs.org/sdr/AALA202602276645.md): Fitting · sticking · Feb 26, 2026 · N770UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS DOOR ARMING LEVER AT DOOR 1L IS DIFFICULT TO MOVE. MAINTENANCE LUBRICATED GIRT BAR FITTINGS AND 1L DOOR ARMS / DISARMS NORMALLY PER AMM 52-10-00.
- [SDR AALA202601108908](https://openairdocs.org/sdr/AALA202601108908.md): Apu · contaminated · Dec 27, 2025 · N770UW · Airbus A319112 · APU Core Engine
  > AIRCRAFT WAS GROUNDED: WHEN AIRCRAFT WENT TO IDLE ON DESCENT, FO AND MYSELF NOTICED HEAVY "DIRTY SOCK" SMELL. IT WAS ONLY IN COCKPIT. MAINTENENCE DEONTAMINATED APU AND ACCOMPLISHED J/C 26L00021002 AND 26L00021014, NO LEAKS NOTED FROM APU OR COMPONENTS. OK FOR
- [SDR AALA202512298908](https://openairdocs.org/sdr/AALA202512298908.md): Unknown · odor · Dec 27, 2025 · N770UW · Airbus A319112 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: WHEN AIRCRAFT WENT TO IDLE ON DESCENT, FO AND MYSELF NOTICED HEAVY "DIRTY SOCK" SMELL. IT WAS ONLY IN COCKPIT. (OPEN)
- [SDR AALA202511212611](https://openairdocs.org/sdr/AALA202511212611.md): Light · missing · Nov 20, 2025 · N770UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: ROW 14 DEF EMERGENCY EXIT DOOR MISSING PANEL. MAINTENANCE REPLACED ROW 14 DEF EMERGENCY EXIT FOOR LIGHT ASSEMBLY PANEL IAW AMM 52-73-21, OPS CHECKED GOOD.
- [SDR AALA202509036566](https://openairdocs.org/sdr/AALA202509036566.md): Power Supply · inoperative · Sep 2, 2025 · N770UW · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP EPSU 13WL. MAINTENANCE REPLACED EPSU (13WL) P/N: 3214-54-10, S/N: 5245 IAW AMM 33-51-38-000-001-A AMM 33-51-38-400-001-A.
- [SDR AALA202509036435](https://openairdocs.org/sdr/AALA202509036435.md): Fitting · cracked · Aug 31, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF CORNER FITTING LOCATED AT PRESSURE DECK MEMBRANE TO CENTER WING BOX AREA, ON FR36 AND -Y1292 PLUS 3 INCHES TO OUTBOARD, RH SIDE. LOWER FUSELAGE. CRACK DIRECTION IS: 9 OCLOCK. CRACK DEPTH
- [SDR AALA202509025525](https://openairdocs.org/sdr/AALA202509025525.md): Fitting · cracked · Aug 28, 2025 · N770UW · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE OF CORNER FITTING LOCATED AT PRESSURE DECK MEMBRANE TO CENTER WING BOX AREA, ON FR36 AND Y1292 LH SIDE LOWER FUSELAGE, CRACK DIRECTION IS 9 OCLOCK CRACK DEPTH IS: 0.108 INCHES. MAINTENANCE R
- [SDR AALA202509027003](https://openairdocs.org/sdr/AALA202509027003.md): Door Frame · cracked · Aug 27, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK AT EMERGENCY EXIT DOOR 844, AFT SEGMENT FR41. MEASURE OF CRACK IS 1.015 IN. MAINTENANCE REPLACED EMERGENCY EXIT DOOR 844, AFT SEGMENT FR41 IAW EO 5210Y228-001.
- [SDR AALA202507256736](https://openairdocs.org/sdr/AALA202507256736.md): Bottle · no test · Jul 23, 2025 · N770UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 831 DAMPING FUNCTION OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 831 AT FWD GALLEY AR
- [SDR AALA202507283876](https://openairdocs.org/sdr/AALA202507283876.md): Bolt · corroded · Jul 22, 2025 · N770UW · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER BOLT AT SLAT TRACK 7 RH WING MEASURE ARE L= 0.344 IN, W= 0.123 IN, D= 0.002 IN. MAINTENANCE REPLACED BOLT AT SLAT TRACK 7 RH WING IAW AMM 27-84-65-400-002-A AND JOB CARD 26C61057005 STEP 6.A(3).
- [SDR AALA202507256323](https://openairdocs.org/sdr/AALA202507256323.md): Bolt · corroded · Jul 20, 2025 · N770UW · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 4 BOLT (LOWER BOLT) SLAT 1 ON RH WING MEASURE CORROSION ARE L=0.117 INCH W=0.071 INCH D=0.001 INCH. MAINTENANCE REPLACED SLAT TRACK 4 BOLT (LOWER BOLT) SLAT 1 ON RH WING IAW A319 AMM 27-84-63-400-002-A.
- [SDR AALA202507066456](https://openairdocs.org/sdr/AALA202507066456.md): Hinge Fitting · excess play · Jul 5, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 4 ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001- A AND AMM 55-16-42-400-001-A.
- [SDR AALA202507258775](https://openairdocs.org/sdr/AALA202507258775.md): Attach Fitting · excess play · Jul 4, 2025 · N770UW · Airbus A319112 · Engine Thrust Reverser
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY THRUST REVERSE AFT ATTACH FITTING BEARING INBOARDON RH PYLON. MAINTENANCE REPLACED THRUST REVERSER AFT ATTACH FITTING INBOARD ON RH PYLON IAW AMM 54-57-17-000-003-A AND AMM 54-57-17-400-003-A AND A319 SRM 51-49-00-
- [SDR AALA202507163994](https://openairdocs.org/sdr/AALA202507163994.md): Fitting · corroded · Jul 4, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11.
- [SDR AALA202507064965](https://openairdocs.org/sdr/AALA202507064965.md): Hinge Fitting · excess play · Jul 4, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 3 ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202507064542](https://openairdocs.org/sdr/AALA202507064542.md): Hinge Arm · excess play · Jul 4, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER). MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 2 ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001- A AND AMM 55-16-42-400-001-A.
- [SDR AALA202507063006](https://openairdocs.org/sdr/AALA202507063006.md): Hinge Arm · excess play · Jul 4, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 1 ON LH HORIZONTAL STABILIZER I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202507217559](https://openairdocs.org/sdr/AALA202507217559.md): Fitting · corroded · Jul 1, 2025 · N770UW · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE (C545117-01) ON LH PYLON MEASURES OF CORROSION ARE: L=13.603 IN, W=1.300 IN, D=0.001 IN. MAINTENANCE BLEENDED SPIGOT FITTING RECEPTICLE.
- [SDR AALA202507211169](https://openairdocs.org/sdr/AALA202507211169.md): Fitting · corroded · Jul 1, 2025 · N770UW · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE (C545117-01) ON RH PYLON MEASURES OF CORROSION ARE: L=13.603 IN, W=1.300 IN, D=0.002 IN. MAINTENANCE BLEENDED SPIGOT FITTING.
- [SDR AALA202507210221](https://openairdocs.org/sdr/AALA202507210221.md): Attach Fitting · corroded · Jun 29, 2025 · N770UW · Airbus A319112 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION UPPER FWD PYLON SLEEVE I/B SIDE WING ATTACH FITTIN ON RH PYLON. MEASURES ARE D= 0.003 INCH, W= 0.479 AND L= 0.794. MAINTENANCE REPLACED ATTACHED FITTING.
- [SDR AALA202507212359](https://openairdocs.org/sdr/AALA202507212359.md): Attach Fitting · corroded · Jun 29, 2025 · N770UW · Airbus A319112 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION UPPER FWD PYLON SLEEVE O/B SIDE WING ATACH FITTING ON RH PYLON. MEASURES ARE D=0.003 INCH, W= 0.479 INCH AND L= 0.794 INCH. MAINTENANCE REPLACED ATTACHED FITTING.
- [SDR AALA202507217514](https://openairdocs.org/sdr/AALA202507217514.md): Floorbeam · elongated · Jun 26, 2025 · N770UW · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON SPLICE O/B SIDE LOWER LOC. FLOOR BEAM +Y765 AT LEVEL FR64 AFT GALLEY AREA MEASURE OF ELONGATE HOLE ON SPLICE IS 0.263 INCH. MAINTENANCE REPLACED SPLICE O/B SIDE LOWER AND FASTENERS LOC. FLOOR BEAM Y765 AT LEVEL
- [SDR AALA202506309170](https://openairdocs.org/sdr/AALA202506309170.md): Hinge Fitting · excess play · Jun 26, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 4 ON RHHORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202506303455](https://openairdocs.org/sdr/AALA202506303455.md): Hinge Fitting · excess play · Jun 26, 2025 · N770UW · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACE HINGE ARM ENDFITTING 6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202508090339](https://openairdocs.org/sdr/AALA202508090339.md): Fitting · burred · Jun 23, 2025 · N770UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: DAMAGE RACK 80VU BURRED MATERIAL ON LOWER LATERAL FITTING LH IN AFT AVIONIC COMPARTMENT MEASURE BURRED MATERIAL IS L=0.027 INCH. MAINTENANCE PERFORMED INTERIM REPAIR, REPLACEMENT LOWER LATERAL FITTING LH LOC. ON AFT LOWER AVIONIC
- [SDR AALA202508091529](https://openairdocs.org/sdr/AALA202508091529.md): Fitting · burred · Jun 23, 2025 · N770UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: DAMAGE RACK 80VU BURRED MATERIAL ON LOWER LATERAL FITTING RH AND WAS FOUND IN CONTACT WITH STRUCTURE IN AFT AVIONIC COMPARTMENT MEASURE BURRET MATERIAL 0.116 INCH. MAINTENANCE PERFORMED INTERIM REPAIR, REPLACEMENT LOWE
- [SDR AALA202507179413](https://openairdocs.org/sdr/AALA202507179413.md): Attach Fitting · excess play · Jun 22, 2025 · N770UW · Airbus A319112 · Wing, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING ATTACH FITTING INTERCONNECTING STRUT LOWER POSITION LH WING. MAINTENANCE REPLACED ATTACH FITTING INTERCONNECTING STRUT LOCATED LOWER POSITION LH WING IAW A319 SRM 51-42-11-801 AND DWG D57570280.
- [SDR AALA202508257717](https://openairdocs.org/sdr/AALA202508257717.md): Shear Plate · cracked · Jun 21, 2025 · N770UW · 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 DAMAGE IS L: 0.727 INCH. MAINTENANCE REPLACED SHEAR PLATE LOCATED ON FR69 TO FR70 ON STR 23 LH SIDE AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801, A319 SR
- [SDR AALA202508207584](https://openairdocs.org/sdr/AALA202508207584.md): Shear Plate · cracked · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE OF CRACK IS L:0.653 INCH. MAINTENANCE REPLACED SHEAR PLATE LOCATED ON FR69 TO FR70 BETWEEN STR 23R AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801,A319 SRM 51-72
- [SDR AALA202508010086](https://openairdocs.org/sdr/AALA202508010086.md): Oxygen Gen · broken · Jun 21, 2025 · N770UW · Airbus A319112 · Passenger Oxygen System
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN EMERGENCY OXYGEN CONTAINER BOX ROW POSITION 26RH IN PASSENGERS CABIN. MAINTENANCE REPLACED EMERGENCY OXYGEN CONTAINER ROW POSITION 26RH IN PASSENGERS CABIN IAW AMM 35-21-41-000-001-A AND AMM 35-21-41-400-001-A.
- [SDR AALA202507210372](https://openairdocs.org/sdr/AALA202507210372.md): Fitting · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LH SIDE AT FWD GALLEY AREA MEASURES OF CORROSION ARE L=0.560 INCHES W=0.274 INCHES D=0.002 INCHES. MAINTENANCE REPLACED CENTER FITTING AND FASTENERS LOC. AT LEVEL STRG 23L BTW FR16 TO FR20 AT FWD GALLEY
- [SDR AALA202507215800](https://openairdocs.org/sdr/AALA202507215800.md): Fitting · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FITTING (LOWER CORNER) FR 16 LH SIDE AT FWD GALLEY AREA L=1.463 INCH, W=0.486 INCH, D=0.001 INCH. MAINTENANCE REPLACED FITTING (LOWER CORNER) LOCATED FR 16 L/H SIDE AT FWD GALLEY AREA IAW A319 SRM 51-72-11-911-001 AND D
- [SDR AALA202507218542](https://openairdocs.org/sdr/AALA202507218542.md): Floor Support · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOC. BTW FR64 AND FR65 AT AFT GALLEY AREA MEASURE ARE: L=1.425 INCH, W=1.359 INCH, D=0.002. MAINTENANCE REPLACED FLOOR BEAM Y765 AND FASTENERS LOCATED BTW FR 64 AND FR 66 AT AFT GALLEY AREA AND SPLICES (
- [SDR AALA202507161867](https://openairdocs.org/sdr/AALA202507161867.md): Door Sill · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPLACED LOWER SILL PER SRM 51-72-11.
- [SDR AALA202507108219](https://openairdocs.org/sdr/AALA202507108219.md): Fitting · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION PASSENGER CREW DOOR CENTER FITTING LOC BTW FR 66 TO FR 68 LH CPCP 534136-01 IN PASSENGER CABIN MEASURE CORROSION ARE L=4.024 INCH W=0.648 INCH D=0.003 INCH. MAINTENANCE REPLACED CENTER FITTING AND FASTENERS LOC. AT LEVE
- [SDR AALA202507108574](https://openairdocs.org/sdr/AALA202507108574.md): Floor Support · corroded · Jun 21, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR SUPPORT -Y765 LOC. BTW FR64 AND FR65 AT AFT GALLEY AREA, MEASURE ON CORRODED AREA ARE: L=0.894 INCH, W=0.529 INCH, D=0.003. MAINTENANCE REPLACED FLOOR SUPPORT -Y765 AND FASTENERS LOC. AT LEVEL FR64 THRU FR65 AT A
- [SDR AALA202509099299](https://openairdocs.org/sdr/AALA202509099299.md): Beam · damaged · Jun 20, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: PREVIOUS TEMP REPAIR REQUIRES REPLACEMENT OF BEAM LOC ON FR40 BTW BEAM 2 AND BEAM 3 IAW EO 5210Y228-001. MAINTENANCE REPLACED BEAM LOC ON FR40 BTW BEAM 2 AND BEAM 3 IAW EO 5210Y228-001.
- [SDR AALA202509096280](https://openairdocs.org/sdr/AALA202509096280.md): Structure · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 834 AT SEGMENT FR41 BTW BEAM 2 AND BEAM 3 DIMENSION OF CRACK IS L= 1.010 IN. MAINTENANCE REPLACED EMERGENCY EXIT DOOR 834 SEGMENT FR41 BTW BEAM 2 AND BEAM 3 IAW EO 5210Y228-001.
- [SDR AALA202509098910](https://openairdocs.org/sdr/AALA202509098910.md): Structure · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCYEXIT DOOR 834 SEGMENT AT FR40 BTW BEAM 2 AND BEAM 3 DIMENSION OF CRACK L=0.935 IN. MAINTENANCE REPLACED EMERGENCYEXIT DOOR 834 SEGMENT AT FR40 IAW EO 5210Y228-001.
- [SDR AALA202509099100](https://openairdocs.org/sdr/AALA202509099100.md): Structure · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 FWD SEGMENT AT FR 40. MAINTENANCE REPLACED EMERGENCY EXIT DOOR 844 FWD SEGMENT AT FR 40 IAW EO 5210Y228-001.
- [SDR AALA202509094245](https://openairdocs.org/sdr/AALA202509094245.md): Structure · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: CRACK MEREGENCY EXIT DOOR 844 FWD SEGMENT AT FR 40 L=0.935 IN. MAINTENANCE REPLACED MEREGENCY EXIT DOOR 844 FWD SEGMENT AT FR40 IAW EO 5210Y228-001.
- [SDR AALA202509091102](https://openairdocs.org/sdr/AALA202509091102.md): Beam · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 FORWARD SEGMENT AT FR 40. MAINTENANCE REPLACED BEAM AT DOOR 844 IAW EO 5210Y288-001.
- [SDR AALA202509027426](https://openairdocs.org/sdr/AALA202509027426.md): Floorbeam · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME IN PASSENGER CABIN (1E/A) CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS OF THE BACKSIDE THE SPAR VERTICAL STR 3 ZONE 1 FR36 CENTER WING BOX CRACK LEGTH 0.318 INCH. MAINTENANCE PERFORMED PERMANENT
- [SDR AALA202509029715](https://openairdocs.org/sdr/AALA202509029715.md): Floorbeam · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1 STR 5 FR36 CENTER WING BOX CRACK DEPTH: 0.097 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON ZONE 1 FR36, -Y765 CENTER WING BOX IAW EA# 366035.
- [SDR AALA202509023724](https://openairdocs.org/sdr/AALA202509023724.md): Floorbeam · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME IN PASSENGER CABIN (1 EA) CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS OF THE BACKSIDE THE SPAR VERTICA L STR 2 ZONE 1 FR36 CENTER WING BOX CRACK L=0.283 INCH. MAINTENANCE PERFORMED PERMANENT R
- [SDR AALA202509029501](https://openairdocs.org/sdr/AALA202509029501.md): Floorbeam · cracked · Jun 20, 2025 · N770UW · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CARCK INDICATION ON FRAME IN PASSENGER CABIN CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS OF THE BACKSIDE THE SPAR VERTICAL STR 4 ZONE 2 FR36 CENTER WING BOX, CRACK LENGTH 0.236 INCH. MAINTENANCE PERFORMED PERMANENT REP
- [SDR AALA202507256513](https://openairdocs.org/sdr/AALA202507256513.md): Floor Support · corroded · Jun 20, 2025 · N770UW · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR SUPPORT +Y1292 LOC. AT LEVEL FR16 AT FWD GALLEY AREA. (CORRODED AREA L: 1.739 INCH, W: 1.220 INCH AND D: 0.010 INCH). MAINTENANCE REPLACED FLOOR SUPPORT +Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A319 SRM

Next page: https://openairdocs.org/aircraft/N770UW/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 = 'N770UW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N770UW/reports

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