# Service difficulty reports: N767UW A list on [N767UW](https://openairdocs.org/aircraft/N767UW.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 · 209 reports - [SDR AALA202609276165](https://openairdocs.org/sdr/AALA202609276165.md): Battery · faulted · Sep 24, 2026 · N767UW · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: FOUND EMERGENCY POWER SUPPLY UNIT AFT LEFT FAULT ON PERIODIC SERVICE CHECK. MAINTENANCE REPLACED BATTERY AT EMERGENCY POWER SUPPLY UNIT (13WL). RESET EMPERGENCY POWER SUPPLY UNIT. ALL CHECKS NORMAL. OK FOR SERVICE. REFERENCE AMM 33-5 - [SDR AALA202609275304](https://openairdocs.org/sdr/AALA202609275304.md): Battery · faulted · Sep 24, 2026 · N767UW · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: FOUND EMERGENCY POWER SUPPLY UNIT BATTERY FORWARD LEFT FAULT ON PERIODIC SERVICE CHECK. MAINTENANCE REPLACED BATTERY AT EMERGENCY POWER SUPPLY UNIT (10WL). ALL CHECKS NORMAL. OK FOR SERVICE. REFERENCE AMM 33-51-38. - [SDR AALA202606054141](https://openairdocs.org/sdr/AALA202606054141.md): Battery Pack · unsecure · Jun 4, 2026 · N767UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: MEGAPHONE INOPERATIVE. MAINTENANCE REINSTALLED BATTERY PACK SCREW FOR MEGAPHONE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-64-51. - [SDR AALA202606029353](https://openairdocs.org/sdr/AALA202606029353.md): Reservoir · low pressure · May 31, 2026 · N767UW · Airbus A319112 · Escape Slide > AIRCRAFT WAS GROUNDED: R2 DOOR SLIDE PRESSURE OUT OF LIMITS. REPLACED SLIDE ASSEMBLY PER JOB CARD 26L0002510. - [SDR AALA202606013295](https://openairdocs.org/sdr/AALA202606013295.md): Lanyard · unsecure · May 28, 2026 · N767UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS EXTREMELY LOUD NOISE COMING FROM 1L DOOR DURING CLIMB- PRESSURIZATION AND DELTA P APPEAR TO BE NORMAL. MAINTENANCE FOUND A SEAL AND SLIDE CORD HANGING DOWN, SECURED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL - [SDR AALA202601224186](https://openairdocs.org/sdr/AALA202601224186.md): Shade · stuck · Jan 5, 2026 · N767UW · Airbus A319112 · Passenger Compartment Equipment > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE STUCK IN THE CLOSED POSITION FOR EMERGENCY ROW SEAT14 A. MAINTENANCE REPLACED WINDOW SHADE, NO HELP. MAINTENANCE REPLACED SEAT 14A WINDOW SHADE WITH FAIRING ASSY IAW AMM 25-23-47. - [SDR AALA202601084186](https://openairdocs.org/sdr/AALA202601084186.md): Shade · stuck · Jan 5, 2026 · N767UW · Airbus A319112 · Passenger Compartment Equipment > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE STUCK IN THE CLOSED POSITION FOR EMERGENCY ROW SEAT14 A. MAINTENANCE REPLACED WINDOW SHADE, NO HELP. - [SDR AALA202510217746](https://openairdocs.org/sdr/AALA202510217746.md): Doubler · cracked · Oct 12, 2025 · N767UW · Airbus A319112 · Trailing Edge Flaps > AIRCRAFT IN BASE MAINTENANCE: PREVIOUS REPAIR COMPLETED (FINGER DOUBLER AND FILLER PLATE) ON OUTBOARD FLAP ACCESS DOOR CUTOUT AT TRACK NO 4 AT LEVEL RIB 15 RH WING, L=5.745IN X W=3.800. MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION PRIOR TO FLIGHT AT O/B FLA - [SDR AALA202510124657](https://openairdocs.org/sdr/AALA202510124657.md): Power Supply · inoperative · Oct 9, 2025 · N767UW · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: INOP EPSU UNIT 13WL IN AFT GALLEY AREA. MAINTENANCE REPLACED EPSU UNIT 13WL IN AFT GALLEY AREA IAW A30FAM AMM 33-51-38-000-001-A AND A30FAM AMM 33-51-38-400-001-A. - [SDR AALA202509262860](https://openairdocs.org/sdr/AALA202509262860.md): Hinge Fitting · cracked · Aug 7, 2025 · N767UW · Airbus A319112 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH MLG DOOR HINGE FITTING. CRACK LEGHT 0.20 0 INCH. MAINTENANCE REPLACED DOOR HINGE FITTING LOCATED ON FR42 LH MLG IAW EA 367463 AND REPAIR DWG R53370500 ISSUE F, A319 SRM 51-42-11-801 AND SRM 51-72-11-9 - [SDR AALA202508071521](https://openairdocs.org/sdr/AALA202508071521.md): Hinge Fitting · excess play · Aug 4, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR #2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 2 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202509025391](https://openairdocs.org/sdr/AALA202509025391.md): Spigot · corroded · Aug 1, 2025 · N767UW · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE BORE LOCATED ON UPPER SPAR BTW RIB 4 AND RIB5 LH PYLON L=13.384 INCH, W=1.338 INCH AND D=0.004 INCH. MAINTENANCE REMOVED AND REPLACED SPIGOT FITTING RECEPTACLE OF LH PYLON IAW A319 SRM 54-51-12- - [SDR AALA202508292855](https://openairdocs.org/sdr/AALA202508292855.md): Fitting · corroded · Aug 1, 2025 · N767UW · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE BORE LOCATED ON UPPER SPAR BTW RIB 4 AND RIB5 RH PYLON, L=13.386 INCH, W=1.340 INCH, D=0.006 INCH. MAINTENANCE REMOVED AND REPLACED SPIGOT FITTING RECEPTACLE OF RH PYLON IAW A319 SRM 54-51-12-30 - [SDR AALA202512014262](https://openairdocs.org/sdr/AALA202512014262.md): Window Frame · cracked · Jul 31, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK IN FLIGHT DECK WINDSHIELD LEFT HAND LATERAL FRAME BETWEEN FR 4 AND FR 8. REPAIRED WINDSHIELD FRAME PER EA 366681. - [SDR AALA202510144463](https://openairdocs.org/sdr/AALA202510144463.md): Fitting · cracked · Jul 29, 2025 · N767UW · Airbus A319112 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CRACK ON CORNER FITTING LOCATED AT PRESSURE DECK MENBRANE ON FR36 LH SIDE, CRACK DEPTH IS 0.147 INCH. MAINTENANCE REPLACED CORNER FITTING LOC. AT PRESSURE DECK MENBRANE ON FR36 LH SIDE IAW A319 SRM 51-42-11-801 AND DWG D57130101. - [SDR AALA202509107240](https://openairdocs.org/sdr/AALA202509107240.md): Support · corroded · Jul 21, 2025 · N767UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL AT LEVEL STR23L BTW FR66 AND FR68 AT AFT GALLEY AREA MEASURES OF CORROSION ARE L=0.939 IN, W=0.589 IN,D=0.040 IN. MAINTENANCE REPLACED LOWER SILL LH SIDE BTW FR66 TO FR68 AND STR 23L AFT GALLEY AREA IAW A319 - [SDR AALA202509101294](https://openairdocs.org/sdr/AALA202509101294.md): Floor Support · corroded · Jul 21, 2025 · N767UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR SUPPORT +Y1292 BTW FR65 AND FR66 AT AFT GALLEY AREA L=0.887 INCH, W=0.380 INCH, D=0.020 INCH. MAINTENANCE REPLACE FLOOR SUPPORT Y1292 LOC. BTW FR64 AND FR66 AT AFT GALLEY IAW SRM 51-42-11-801, SRM 51-72-11-911-001 - [SDR AALA202509030592](https://openairdocs.org/sdr/AALA202509030592.md): Frame · inoperative · Jul 21, 2025 · N767UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT WAS NOT GROUNDED: CRACK FRAME 68 UPPER CORNER CUTOUT AT LEVEL STR8R AT AFT GALLEY AREA, CRACK MEASURE IS L=0.650 INCH. MAINTENANCE REPLACED FRAME UPPER CORNER CUTOUT AT FR68 LEVEL STR8R AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53480009. - [SDR AALA202509023251](https://openairdocs.org/sdr/AALA202509023251.md): Sill Drain · corroded · Jul 21, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL AT LEVEL STR 23R BTW FR 66 AND FR 68 AT AFT GALLEY AREA L=2.450 INCH W=2.037 INCH D=0.013 INCH. MAINTENANCE REPLACED LOWER SILL RH SIDE BTW FR66 TO FR68 AND STR23R AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A3 - [SDR AALA202508067442](https://openairdocs.org/sdr/AALA202508067442.md): Hinge Arm · excess play · Jul 21, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508063618](https://openairdocs.org/sdr/AALA202508063618.md): Hinge Arm · excess play · Jul 21, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508062255](https://openairdocs.org/sdr/AALA202508062255.md): Hinge Arm · excess play · Jul 21, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENCE REPLACED HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508063977](https://openairdocs.org/sdr/AALA202508063977.md): Hinge Arm · excess play · Jul 21, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508062221](https://openairdocs.org/sdr/AALA202508062221.md): Hinge Arm · excess play · Jul 21, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508061538](https://openairdocs.org/sdr/AALA202508061538.md): Hinge Arm · excess play · Jul 20, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR #3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 3 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508063525](https://openairdocs.org/sdr/AALA202508063525.md): Hinge Arm · excess play · Jul 20, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR #4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 4 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508068041](https://openairdocs.org/sdr/AALA202508068041.md): Hinge Arm · excess play · Jul 20, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR#6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 6 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508068886](https://openairdocs.org/sdr/AALA202508068886.md): Hinge Arm · excess play · Jul 20, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR #5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202508063090](https://openairdocs.org/sdr/AALA202508063090.md): Hinge Arm · excess play · Jul 20, 2025 · N767UW · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR #1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 1 ELEVATOR ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507309812](https://openairdocs.org/sdr/AALA202507309812.md): Splice · corroded · Jul 20, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPLICE UPPER POSITION INBOARD SIDE ON FLOOR BEAM -Y1162.5 AT LEVEL FR68 AT AFT GALLEY AREA L=1.684 INCH, W=0.961 INCH, D= 0.078 INCH. MAINTENANCE REPLACED SPLICE LOC. UPPER POSITION INBOARD SIDE ON FLOOR BEAM -Y1162.5 - [SDR AALA202510069966](https://openairdocs.org/sdr/AALA202510069966.md): Shear Plate · cracked · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURE IS L= 0.895. MAINTENANCE REPLACED SHEAR PLATE LOCATED BTW FR69 TO FR70 AT LEVEL STGR 23 RH SIDE AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801, A319 SRM 51-7 - [SDR AALA202509296658](https://openairdocs.org/sdr/AALA202509296658.md): Shear Plate · cracked · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURES OF CRACK, L= 1.030 INCH. MAINTENANCE REPLACED SHEAR PLATE STR 23 L LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801 AND A319 SRM 51 - [SDR AALA202509198874](https://openairdocs.org/sdr/AALA202509198874.md): Dummy Rail · corroded · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION RAIL DUMMY Y503.2 LOC. AT LEVEL FR16 AT FWD GALLEY AREA, MEASURE CORROSION ARE L=1.103 INCH W=0.973 INCH D=0.013 INCH. MAINTENANCE REPLACED RAIL DUMMY Y503.2 LOC. AT LEVEL FR16 AT FWD GALLEY AREA. IAW A319 SRM 51-42-11-8 - [SDR AALA202509020592](https://openairdocs.org/sdr/AALA202509020592.md): Floorbeam · corroded · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOC AT LEVEL FR16 AT FWD GALLEY AREA L= 1.574 IN W= 1.240 IN D= 0.077 IN. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC AT LEVEL FR12 TO FR24 FWD GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911 - [SDR AALA202509022612](https://openairdocs.org/sdr/AALA202509022612.md): Floorbeam · corroded · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK +Y765 LOC. AT LEVEL FR16 AT FWD GALLEY AREA L= 1.112 IN W= 1.002 IN D=0.009 IN. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC AT LEVEL FR12 TO FR24 FWD GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911 - [SDR AALA202508200255](https://openairdocs.org/sdr/AALA202508200255.md): Seat Track · corroded · Jul 19, 2025 · N767UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK +Y1162.5 SECTION CONNECTION I/B SIDE UPPER POSITION AT LEVEL FR68 AT AFT GALLEY AREA, MEASURES ARE: L=1.118 IN; W=0.872 IN; D=0.020 IN. MAINTENANCE REPLACED SECTION CONNECTION LOCATED SEAT TRACK BEAM +Y1162.5 - [SDR AALA202510105489](https://openairdocs.org/sdr/AALA202510105489.md): Floorbeam · cracked · Jul 18, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FASTENER HOLE ZONE 1 OF HORIZONTAL FLOOR BEAM 1 AT FR 36. CRACK DIRECTION 1 OCLOCK VIEW LOOKING AFT. CRACK D= 0.130 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX POSITION +Y1292 FR 36 ON SPAR - [SDR AALA202510103608](https://openairdocs.org/sdr/AALA202510103608.md): Floorbeam · cracked · Jul 18, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 3 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36. CRACK MEASURE L= 0.305 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX POSITION (3) Y254 FRONT SPAR VERT - [SDR AALA202510107798](https://openairdocs.org/sdr/AALA202510107798.md): Floorbeam · cracked · Jul 18, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIOUS OF HORIZONTAL FLOOR BEAM 4 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR36. CRACK L:0.395 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX POSITION (4)-Y254 ON SPAR VERTICAL STRINGER - [SDR AALA202510106968](https://openairdocs.org/sdr/AALA202510106968.md): Floorbeam · cracked · Jul 18, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 2 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36. CRACK L= 0.105 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX POSITION (2)Y765 FRONT SPAR VERTICAL STRIN - [SDR AALA202510067363](https://openairdocs.org/sdr/AALA202510067363.md): Floorbeam · cracked · Jul 18, 2025 · N767UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 5 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36. CRACK L= 0.155 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX POSITION (5) -Y765 ON SPAR VERTICAL STRING - [SDR AALA202510108547](https://openairdocs.org/sdr/AALA202510108547.md): Pressure Deck · cracked · Jul 17, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBRANE, ON FR36 AND -Y1292 PLUS 7 INCHES TO OUTBOARD, RH SIDE CRACK DEPTH IS: 0.133 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON FRAME 36 PRESSURE DECK MEM - [SDR AALA202510107846](https://openairdocs.org/sdr/AALA202510107846.md): Pressure Panel · cracked · Jul 17, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT FASTENER HOLE LOCATED AT PRESSURE DECK MEMBRANE AT FR36 AND Y1292 PLUS 5 INCHES TO OUTBOARD, LH SIDE CRACK DIRECTION IS 11 OCLOCK. CRACK DEPTH IS 0.147 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR L - [SDR AALA202508292046](https://openairdocs.org/sdr/AALA202508292046.md): Stiffener · cracked · Jul 17, 2025 · N767UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK STIFFENER LOCATED ON FR1 (Z-169) FWD FACE FWD PRESSURE BULKHEAD MEASURE OF DAMAGE L: 0.900 INCH. MAINTENANCE REPLACED STIFFENER LOCATED ON FR1 (Z-169) FWD FACE FWD PRESSURE BULKHEAD IAW A319 SRM 51-42-11-801, SRM 51-72-11-9 - [SDR AALA202508261026](https://openairdocs.org/sdr/AALA202508261026.md): Bottle · no test · Jul 17, 2025 · N767UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST OF THE DOOR DAMPING OF DOOR DAMPER ON PASS ENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW AM - [SDR AALA202510150832](https://openairdocs.org/sdr/AALA202510150832.md): Frame · cracked · Jul 15, 2025 · N767UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE (AFT LOWER POSITION) LOCATED ON FRAME 35 AT LEVEL OF STRINGER 30 LH SIDE, LOWER FUSELAGE, L= 0.260 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED ON FRAME 35 AT LEVEL OF STRINGER 30 - [SDR AALA202509116923](https://openairdocs.org/sdr/AALA202509116923.md): Fitting · cracked · Jul 15, 2025 · N767UW · Airbus A319112 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR16 RH DOOR STOP FITTING 7 UPPER I/B HOLE CRACK DEPTH IS 0.157 INCH APPROX. MAINTENANCE REPLACED INTERCOSTAL FITTING AT LEVEL DOOR STOP #7 ON FRAME 16 RH IAW A319 SRM 51-42-11 - [SDR AALA202510216734](https://openairdocs.org/sdr/AALA202510216734.md): Rib · worn · Jul 14, 2025 · N767UW · Airbus A319112 · Wing, Rib/Bulkhead > AIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING L=0.313 INCH W=0.145 INCH, D=0.034 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 368892. - [SDR AALA202510218026](https://openairdocs.org/sdr/AALA202510218026.md): Rib · worn · Jul 14, 2025 · N767UW · Airbus A319112 · Wing, Rib/Bulkhead > AIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING. L=0.727 INCH, W=0.442 INCH AND D=0.001 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 36889 - [SDR AALA202510211013](https://openairdocs.org/sdr/AALA202510211013.md): Rib · worn · Jul 14, 2025 · N767UW · Airbus A319112 · Wing, Rib/Bulkhead > AIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING L=1.514 INCH W=1.173 INCH, D=0.055 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 368892. Next page: https://openairdocs.org/aircraft/N767UW/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 = 'N767UW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N767UW/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.