# Service difficulty reports: N762US

A list on [N762US](https://openairdocs.org/aircraft/N762US.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 · 289 reports

- [SDR AALA202610013161](https://openairdocs.org/sdr/AALA202610013161.md): Bulb · detached · Sep 29, 2026 · N762US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY LIGHT TEST DISCOVERED AFT LAV "E" AUXILIARY LIGHT INSIDE LAV INOP. MAINTENANCE FOUND BULB POPPED OUT OF SOCKET AND RE-INSERTED BULB INTO SOCKET. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR AALA202606297300](https://openairdocs.org/sdr/AALA202606297300.md): Bottle · low pressure · Jun 26, 2026 · N762US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
- [SDR AALA202606013417](https://openairdocs.org/sdr/AALA202606013417.md): Bottle · low pressure · May 28, 2026 · N762US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202604205833](https://openairdocs.org/sdr/AALA202604205833.md): Fcu · leaking · Apr 14, 2026 · N762US · Airbus A319112 · APU Engine Fuel and Control
  > AIRCRAFT WAS GROUNDED: WITH APU BLEED ON, STRONG FOUL SMELL. AFTER ENGINE START AND APUSELECTED OFF, SMELL DISSIPATED. ON DESCENT WITH ENGINES IDLE, SMELL CAME BACK.SINGLE PACK OPERATION AS WELL. #2 PACK WAS SELECTED OFF PER MEL. MAINTENANCE REPLACED APU FCU I
- [SDR AALA202604165833](https://openairdocs.org/sdr/AALA202604165833.md): Unknown · odor · Apr 14, 2026 · N762US · Airbus A319112 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: WITH APU BLEED ON, STRONG FOUL SMELL. AFTER ENGINE START AND APUSELECTED OFF, SMELL DISSIPATED. ON DESCENT WITH ENGINES IDLE, SMELL CAME BACK.SINGLE PACK OPERATION AS WELL. #2 PACK WAS SELECTED OFF PER MEL. (OPEN)
- [SDR AALA202604135258](https://openairdocs.org/sdr/AALA202604135258.md): Air Filter · dirty · Mar 30, 2026 · N762US · Airbus A319112 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: NOTICED MUSTY ODOR AT TOP OF DESCENT WHEN POWER WAS REDUCED TO IDLE. CABIN CREW DID NOT NOTICE ANYTHING. MAINTENANCE FOUND SOURCE OF COCKPIT ODOR TO BE CLOGGED/DIRTY AVEC FILTER. RELACEMENT OF FILTER SOLVED COCKPIT ODOR.
- [SDR AALA202604025258](https://openairdocs.org/sdr/AALA202604025258.md): Unknown · odor · Mar 30, 2026 · N762US · Airbus A319112 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: NOTICED MUSTY ODOR AT TOP OF DESCENT WHEN POWER WAS REDUCED TO IDLE. CABIN CREW DID NOT NOTICE ANYTHING. (OPEN)
- [SDR AALA202511058340](https://openairdocs.org/sdr/AALA202511058340.md): Slide Raft · inoperative · Nov 4, 2025 · N762US · Airbus A319112 · Escape Slide
  > AIRCRAFT WAS NOT GROUNDED: SCHEDULED PARTS CHANGE FOR P/N 26-2562-9-0009S/N 0082 SLIDE, POSITION RIGHT 4. MAINTENANCE INSPECTION REJECTED SLIDE FOR CHANGE REF JC 26L00025010 STEP 3.B.2. REMOVED AND REPLACED R4 DOOR SLIDE IAW JOB CARD 26L00025010.
- [SDR AALA202510178908](https://openairdocs.org/sdr/AALA202510178908.md): A/C Pack · odor · Oct 12, 2025 · N762US · Airbus A319112 · Cabin Cooling System
  > AIRCRAFT WAS GROUNDED: ONCE AT FLIGHT IDLE ON THE DESCENT THROUGH 17000 ABNORMAL ODOR NOTICED IN FLIGHT DECK. NOTHING NOTED IN CABIN. COMPLIED WITH QRH15-38, AND ODOR DISSIPATED WITHIN SEVERAL MINUTES. TURNED PACK1 AND CROSS BLEED BACK TO AUTO AND ODOR CAME BA
- [SDR AALA202510148908](https://openairdocs.org/sdr/AALA202510148908.md): Unknown · odor · Oct 12, 2025 · N762US · Airbus A319112 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: ONCE AT FLIGHT IDLE ON THE DESCENT THROUGH 17000 ABNORMAL ODOR NOTICED IN FLIGHT DECK. NOTHING NOTED IN CABIN. COMPLIED WITH QRH15-38, AND ODOR DISSIPATED WITHIN SEVERAL MINUTES. TURNED PACK1 AND CROSS BLEED BACK TO AUTO AND ODOR CAME BA
- [SDR AALA202506131856](https://openairdocs.org/sdr/AALA202506131856.md): Fitting · corroded · Jun 6, 2025 · N762US · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON L=13.500 INCHES W= 1.300 INCHES D=0.003. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE BTW STA6793/RIB 4 AND STA7063/RIB 5 ON LH PYLON I.A.W A319 SRM-54-51-12-300-001.
- [SDR AALA202508011308](https://openairdocs.org/sdr/AALA202508011308.md): Intercostal · cracked · May 20, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON INTERCOSTAL FITTING LOC. AT FR20 RH AT LEVEL DOOR STOP FITTIN G 7 PAX CABIN UPPER FUSELAGE L= 0.100. MAINTENANCE REPLACED INTERCOSTAL FITTING #7 LOCATED ON FR 20 BTW STRG 10 AND STRG 11 RH SIDE AT FWD GALLEY AREA. I.A.W.
- [SDR AALA202506253416](https://openairdocs.org/sdr/AALA202506253416.md): Fitting · cracked · May 20, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON INTERCOSTAL FITTING LOC AT FR20 LH AT LEVEL DOOR STOP FITTING 7 PAX CABIN UPPER FUSELAGE L= 0.110 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING LOCATED FR20 LH AT LEVEL DOOR STOP FITTING 7 PAX CABIN UPPER FUSELAGE IAW A3
- [SDR AALA202507060193](https://openairdocs.org/sdr/AALA202507060193.md): Hinge Fitting · cracked · May 12, 2025 · N762US · Airbus A319112 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ATTACHMENT FITTING ON RH MAIN LANDING GEAR (CRACK INDICATION FOUND ON FWD MLG DOOR KEEL BEAM HINGE FITTING EXTERNAL RH) CRACK L=0.100 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (PART REPLACEMENT- ENTIRE) ON FR
- [SDR AALA202507015962](https://openairdocs.org/sdr/AALA202507015962.md): Hinge Fitting · cracked · May 12, 2025 · N762US · Airbus A319112 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FWD MLG DOOR KEEL BEAM HINGE FITTING EXTERNAL LH, CRACK L=0.110 INCH.
- [SDR AALA202506055376](https://openairdocs.org/sdr/AALA202506055376.md): Attach Bolt · corroded · May 12, 2025 · N762US · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION UPPER AFT BOLT TRACK 1 SLAT 1 ON RH WING L=0.35 INCH, W=0.05 INCH, D= 0.007 INCH. MAINTENANCE REPLACED UPPER AFT BOLT TRACK 1 SLAT 1 ON RH WING IAW AMM 27-84-63-400-002-A JOB CARD 26C61057005.
- [SDR AALA202508015847](https://openairdocs.org/sdr/AALA202508015847.md): Fitting · worn · May 8, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: WEAR ON UPPER FITTING LOCATED AT LEVEL FR20 WHEEL WELL STRUCTURE IN LATERAL AVIONIC COMP LH L= 0.576 IN. MAINTENANCE REPLACED FITTING LOCATED FR20 LH AT LEVEL OF Y520 WHEEL WELL STRUCTURE IN LATERAL AVIONIC COMPARTMENT LH IAW A319
- [SDR AALA202506251147](https://openairdocs.org/sdr/AALA202506251147.md): Skin Panel · corroded · May 8, 2025 · N762US · Airbus A319112 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION DRY BAY INBOARD BOTTOM SKIN UPPER SURFACE ON RH WING MEASURES L:2.70 INCH W:2.40 INCH D:0.003 INCH. MAINTENANCE BLENDED BOTTOM SKIN UPPER SURFACE ON RH WING PER EA 365038 AND IAW SRM 51-74-00.
- [SDR AALA202508013571](https://openairdocs.org/sdr/AALA202508013571.md): Splice Angle · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER SPLICE I/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH SIDE, MEASURES OF CORROSION ARE L=0.270INCH, W=0.235INCH, D=0.001INCH. MAINTENANCE REPLACED UPPER SPLICE I/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH AND STRG 23L
- [SDR AALA202508018757](https://openairdocs.org/sdr/AALA202508018757.md): Fitting · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING AT FRAME 66 LH SIDE, MEASURES OF CORROSION ARE L= 3.168INCH, W=1.045INCH, D=0.003INCH. MAINTENANCE REPLACED CORNER FITTING LOC ON FRAME 66 AT LEVEL OF STR23 LH IAW A319 SRM 51-42-11-801 AND SRM 51-72-1
- [SDR AALA202508013365](https://openairdocs.org/sdr/AALA202508013365.md): Splice · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER SPLICE O/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH SIDE, MEASURES OF CORROSION ARE L=0.365 INCH, W=0.344 INCH, D=0.001 INCH. MAINTENANCE REPLACED UPPER SPLICE O/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH AND STRG 2
- [SDR AALA202508012580](https://openairdocs.org/sdr/AALA202508012580.md): Splice · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SPLICE O/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH SIDE, MEASURES OF CORROSION ARE L: 0.301 INCH W:0.245 INCH D: 0.001 INCH. MAINTENANCE REPLACED LOWER SPLICE O/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH AND STRG 2
- [SDR AALA202508018694](https://openairdocs.org/sdr/AALA202508018694.md): Splice · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SPLICE I/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH SIDE, MEASURES OF CORROSION ARE L: 0.300 INCH W:0.239 INCH D: 0.001 INCH. MAINTENANCE REPLACED LOWER SPLICE I/B SIDE ON LOWER SILL AT LEVEL FRAME 66LH AND STRG 2
- [SDR AALA202506066519](https://openairdocs.org/sdr/AALA202506066519.md): Fitting · corroded · May 5, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING AT FRAME 68LH SIDE, MEASURES OF CORROSION ARE L=0.601 INCH, W=0.271 INCH, D=0.015 INCH. MAINTENANCE REPLACED CORNER FITTING LOC ON FRAME 68 AT LEVEL OF STR23 LH IAW A319 SRM 51-42-11-801 AND SRM 51-72-1
- [SDR AALA202505083222](https://openairdocs.org/sdr/AALA202505083222.md): Plate · cracked · May 5, 2025 · N762US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON BONDING PLATE LOCATED ON HINGE ARM N5 ON TRAILING EDGE LH HORZONTAL STABILIZER. MAINTENANCE REPLACED BONDING PLATE LOCATED ON HINGE ARM #5 ON TRAILING EDGE LH HORIZONTAL STABILIZER IAW A319 SRM 51-42-11-801 AND SRM 51-72
- [SDR AALA202508064054](https://openairdocs.org/sdr/AALA202508064054.md): Shear Plate · cracked · May 3, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE LOCATED BTW FR69 AND FR70 AT LEVEL OF STR 23R AFT GALLEY AREA. (L:0.930 IN). MAINTENANCE REPLACED SHEAR PLATE LOCATED BTW FR69 AND FR70 AT LEVEL OF STR 23R AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 51-72
- [SDR AALA202506309837](https://openairdocs.org/sdr/AALA202506309837.md): Shear Plate · cracked · May 3, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE LOCATED BTW FR69 AND FR70 AT LEVEL OF STR 23L AT AF T GALLEY AREA. L=1.020 INCH. MAINTENANCE REPLACE SHEAR PLATE LOCATED BTW FR69 AND FR70 AT LEVEL OF STR 23L AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801 AND
- [SDR AALA202505277869](https://openairdocs.org/sdr/AALA202505277869.md): Seat Track · corroded · May 3, 2025 · N762US · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOCATED BTW FR66 AND FR70 AT AFT GALLEY AREA L=1.100 INCH W=1.020 INCH D=0.058 INCH. MAINTENANCE REPLACED FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 AT LEVEL STRG 23L AT AFT GALLEY AREA IAW A319 SRM 51-42-11-
- [SDR AALA202505270461](https://openairdocs.org/sdr/AALA202505270461.md): Fitting · corroded · May 3, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BTW FR16 AND FR20 LH SIDE AT FWD GALLEY AREA. L=0.980 INCH, W=0.740 INCH, D=0.003 INCH. MAINTENANCE REPLACED CENTER FITTING BTW FR16 AND FR20 AT LEVEL OF STRG 23L AT FWD GALLEY AREA IAW A319 SRM 51-42-11-8
- [SDR AALA202508012034](https://openairdocs.org/sdr/AALA202508012034.md): Floor Support · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 16 TO FR 20 FWD GALLEY AREA. L= 1.985 INCH, W=1.100 INCH, D=0.058 INCH. MAINTENANCE REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR 12 TO FR 24 FWD GALLEY AREA I.A.W A319 SRM 51-42-11-801, A319
- [SDR AALA202507250185](https://openairdocs.org/sdr/AALA202507250185.md): Structure · cracked · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #2 ZONE 1. CRACK DIRECTION AT 12 AND 1 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #2 +Y765 IAW EA
- [SDR AALA202507213544](https://openairdocs.org/sdr/AALA202507213544.md): Floorbeam · cracked · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #4 ZONE 1. CRACK DIRECTION AT 12 AND 3 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #4 -Y254 IAW EA
- [SDR AALA202507216259](https://openairdocs.org/sdr/AALA202507216259.md): Floorbeam · cracked · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #3 ZONE 1. CRACK DIRECTION AT 1 AND 12 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #3 Y254 IAW EA#
- [SDR AALA202507187563](https://openairdocs.org/sdr/AALA202507187563.md): Floorbeam · cracked · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER N5 ZONE 1, CRACK DIRECTION IS 12, 1 AND 3 OCLOCK LOOCKING AFT. CRACK D=0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (SPLICE REPAIR) ON CENTER WING B
- [SDR AALA202506098898](https://openairdocs.org/sdr/AALA202506098898.md): Floorbeam · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOCATED BTW FR64 AND FR67 AT LEVEL OF STR 23L AT AFT GALLEY AREA, MEASURES OF CORROSION ARE L=1.400 INCH, W=0.800 INCH, D=0.058 INCH. MAINTENANCE REPLACED FLOOR BEAM Y765 LOC. BTW FR64 AND FR67 AT LEV
- [SDR AALA202506064545](https://openairdocs.org/sdr/AALA202506064545.md): Floor Support · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE, CORROSION FLOOR SUPPORT +Y1292 FR 16 TO FR 20 FWD GALLEY AREA, MEASURE ARE L:0.495 IN, W:0.382 IN, D:0.040 IN OF CORRODED AREA. MAINTENANCE REPLACED BEAM +Y1292 LOCATED BTW FR12 TO FR24 FWD GALLEY AREA IAW A319 SRM 51-42-11-801
- [SDR AALA202506058712](https://openairdocs.org/sdr/AALA202506058712.md): Fitting · corroded · May 1, 2025 · N762US · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1732 LOCATED BTW FR65 AND FR66 AT LEVEL OF STR 23L AT AFT GALLEY AREA L=0.531 INCH, W=0.667INCH, D=0.040 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON I.A.W A319 SRM-54-51-12-300-001.
- [SDR AALA202506033975](https://openairdocs.org/sdr/AALA202506033975.md): Floorbeam · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOCATED BTW FR64 AND FR67 AT LEVEL OF STR 23L AT AFT GALLEY AREA L: 2.505 INCH, W: 1.899 INCH, D:0.058 INCH, CORRODED AREA. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC.BTW FR64 AND FR67 AT LEVEL OF STR 23
- [SDR AALA202506030084](https://openairdocs.org/sdr/AALA202506030084.md): Support · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FR 66 TO FR 68 AT LEVEL STRG 23L AT AFT GALLEY AREA. MEASURE OF CORROSION ARE L:3.73 INCH, W=2.03 INCH, D= 0.030 INCH. MAINTENANCE REPLACED LOWER SILL LOCATED BTW FR 66 TO FR 68 AT LEVEL STRG 23L A
- [SDR AALA202505271640](https://openairdocs.org/sdr/AALA202505271640.md): Fitting · corroded · May 1, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LOCATED BTW FR 66 TO FR 68 AT LEVEL STRG 23L AT AFT GALLEY AREA L=27 INCH W=1.8 INCH D=0.015 INCH. REPLACED CENTER FITTING LOC BTW FR 66 TO FR 68 AT LEVEL STRG 23L AFT GALLEY AREA IAW A319 SRM 51-42-11-801
- [SDR AALA202505050607](https://openairdocs.org/sdr/AALA202505050607.md): Hinge Arm · excess play · May 1, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 6 ELEVATOR ON LH. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202505053661](https://openairdocs.org/sdr/AALA202505053661.md): Hinge Arm · excess play · May 1, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 5 ELEVATOR ON LH. MAINTENANCE REPLACED HINGE ARM 5 ELEVATOR ON LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202505053789](https://openairdocs.org/sdr/AALA202505053789.md): Hinge Arm · excess play · May 1, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON LH. MAINTENANCE REPLACED HINGE ARM 4 ELEVATOR ON LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202505061052](https://openairdocs.org/sdr/AALA202505061052.md): Hinge Fitting · excess play · Apr 30, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 4 ELEVATOR ON RH. MAINTENCE REPLACED HINGE ARM END FITTING 4 ELEVATOR ON RH IAW AMM 55-16-42-000-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202505058409](https://openairdocs.org/sdr/AALA202505058409.md): Hinge Fitting · excess play · Apr 30, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 6 ELEVATOR ON RH. MAINTENANCE REPLACED HINGE ARM END FITTING 6 ON ELEVATOR RH IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202507061232](https://openairdocs.org/sdr/AALA202507061232.md): Stiffener · cracked · Apr 29, 2025 · N762US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK STIFFENER ASSY Z-169 FR 1 ON FORWARD PRESSURE BULKHEAD MEASURES OF CRACK: L= 0.398 IN, W= 0.005 IN. MAINTENANCE REPLACED STIFFENER ASSY Z-169 LOCATED ON FRAME 1 FORWARD PRESSURE BULKHEAD. I.A.W. A319 SRM 51-72-11-911-001. A
- [SDR AALA202508269814](https://openairdocs.org/sdr/AALA202508269814.md): Skin Panel · corroded · Apr 28, 2025 · N762US · Airbus A319112 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TOP SKIN LOWER SURFACE LEVEL RIB 14 ON RH WING L= 4.214 INCH W= 1.954 INCH D= 0.114 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON TOP SKIN LOWER SURFACE BTW RIB 13 TO RIB 15 ON RH WING IAW EA# 364937 DWG R572-58616
- [SDR AALA202506255512](https://openairdocs.org/sdr/AALA202506255512.md): Fitting · cracked · Apr 28, 2025 · N762US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON INTERCOSTAL FITTING IN FR16 RH AT LEVEL DOOR STOP FITTING 7 PAX CABIN UPPER FUSELAGE,MEASURE IS L=0.120 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING #7 LOCATED ON FR 16 BTW STRG 10 AND STRG 11 RH SIDE AT FWD GALLEY ARE
- [SDR AALA202506164765](https://openairdocs.org/sdr/AALA202506164765.md): Hinge Arm · excess play · Apr 27, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON SUPPORT STRUT ELEVATOR HINGE ARM 4 LH. MAINTENANCE REPLACED SUPPORT STRUT ELEVATOR HINGE ARM 4 LH IAW AMM 55-16-48-400-001-A AND IAW AMM 55-16-48-000-001-A.
- [SDR AALA202505027002](https://openairdocs.org/sdr/AALA202505027002.md): Hinge Fitting · excess play · Apr 24, 2025 · N762US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM 5 ELEVATOR ON RH. MAINTENANCE REPLACED HINGE ARM END FITTING 5 ON ELEVATOR RH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Next page: https://openairdocs.org/aircraft/N762US/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 = 'N762US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N762US/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.