# Service difficulty reports: N763US A list on [N763US](https://openairdocs.org/aircraft/N763US.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 · 243 reports - [SDR AALA202607279637](https://openairdocs.org/sdr/AALA202607279637.md): Lamp · inoperative · Jul 22, 2026 · N763US · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: FORWARD LEFT CLOSET RED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RE-LAMPED PER AMM 33-51-18 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202606220852](https://openairdocs.org/sdr/AALA202606220852.md): Flashlight · no test · Jun 19, 2026 · N763US · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00. - [SDR AALA202606153033](https://openairdocs.org/sdr/AALA202606153033.md): Door · out of rig · Jun 11, 2026 · N763US · Airbus A319112 · Standard Practices/Structures > AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTED INCREASED NOISE LEVEL NEAR AFT CABIN DOOR ON DESCENT. MAINTENANCE FOUND THE L2 DOOR OUT OF RIG AND DOOR SEAL LEAKING. MAINTENANCE REPLACED DOOR SEAL PER AMM 52-13-18 AND RIGGED THE DOOR PER AMM 52-13-00 (AALA2 - [SDR AALA202512292083](https://openairdocs.org/sdr/AALA202512292083.md): Battery · no test · Dec 26, 2025 · N763US · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: DURING THE PS-CHECK FOUND THAT EPSU AFT BATTERY FAILED. MAINTENANCE REPLACED AFT BATTERY OF THE EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38. - [SDR AALA202509125567](https://openairdocs.org/sdr/AALA202509125567.md): Power Supply · no test · Sep 12, 2025 · N763US · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING JC 26L00025010 GOT EPSU BATTERY AFT L DURING OPERATION TEST OF EMERGENCY LIGHTING SYSTEM. MAINTENANCE REPLACED AFT L EPSU IAW AMM 33-51-38. - [SDR AALA202508011995](https://openairdocs.org/sdr/AALA202508011995.md): Hinge Fitting · excess play · Jul 28, 2025 · N763US · Airbus A319112 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: OUT OF LIMITS HOLES (9.60MM) IN FORWARD-FITTINGASSEMBLY ON RH MLG DOOR. PERFORMED PERMANENT REPAIR IN HOLE COMMON TOFORWARD-FITTING ASSEMBLY AND REPLACED HINGE FITTING ON RH MLG DOOR IAWA319 SRM 52-81-14-300-140. HFEC INSPECTI - [SDR AALA202508196862](https://openairdocs.org/sdr/AALA202508196862.md): Plate · cracked · Jul 26, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON CONNECTING PLATE LOC. ON RH MAIN LANDING GEAR MEASURE OF CRACK D1-D2=0.069 INCH. MAINTENANCE REPLACED CONNECTING PLATE LOC AT FR 42 BTW STR 41RH AND 42RH MAIN LANDING GEAR IAW EA #366188 PART B STEP 2.B, DWG D53370790, A3 - [SDR AALA202508134533](https://openairdocs.org/sdr/AALA202508134533.md): Door Frame · cracked · Jul 25, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON DOOR FRAME LOC. BTW FR67 AND FR68 AT LEVEL STRG 8R, PASSENGER CABIN, AFT GALLEY AREA. CRACK L=0.538 IN. MAINTENANCE REPLACED DOOR FRAME LOC. BTW FR67 AND FR68 AT LEVEL STRG 8R, PASSENGER CABIN, AFT GALLEY AREA IAW A319 SR - [SDR AALA202508019065](https://openairdocs.org/sdr/AALA202508019065.md): Fitting · cracked · Jul 25, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON HOLE H1 INSTERCOSTAL FITTING LOC. ON FR 20 LH SIDE AT LEVEL DOOR STOP 7, FWD GALLEY AREA, MEASURE OF CRACK IS L=0.103 IN. MAINTENANCE REPLACED INSTERCOSTAL FITTING LOC. ON FR 20 LH SIDE AT LEVEL DOOR STOP 7, FWD GALLEY A - [SDR AALA202508063639](https://openairdocs.org/sdr/AALA202508063639.md): Fitting · cracked · Jul 18, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON HOLE 1 INTERCOSTAL FITTING LOC. FRAME 20 RH AT LEVEL DOOR ST OP 7, FWD GALLEY27 AREA L=0.150 INCH. MAINTENANCE REPLACED INSTERCOSTAL FITTING LOC. ON FR 20 RH SIDE AT LEVEL DOOR STOP 7, FWD GALLEY AREA I.A.W A319 SRM 53- - [SDR AALA202507236104](https://openairdocs.org/sdr/AALA202507236104.md): Fitting · cracked · Jul 17, 2025 · N763US · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: CRACK ON H1 AND H3 INTERCOSTAL FITTING LOC. FR 16 AT LEVEL DOOR STOP FITTING 7 LH SIDE FWD GALLEY AREA, CRACK LENGTH L=0.102 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING LOC. ON FR 16LH AT LEVEL DOOR STOP 7, FWD GALLEY AREA I.A - [SDR AALA202508115023](https://openairdocs.org/sdr/AALA202508115023.md): Gusset · cracked · Jun 29, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON GUSET LOC. BTW FR68 AND FR69 AT LVEL STRG 8 RH SIDE ON PASSEN GER CABIN, AFT GALLEY AREA L= 0.090 INCH. MAINTENANCE REPLACED GUSET LOC. BTW FR68 AND FR69 AT LVEL STRG 8 RH SIDE ON PASSENGER CABIN, AFT GALLEY AREA IAW A319 - [SDR AALA202508139950](https://openairdocs.org/sdr/AALA202508139950.md): Lintel · cracked · Jun 28, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON LINTEL LOC. BTW FR66 AND FR68 AT LEVEL STRG 9R, PASSENGER CABIN, AFT GALLEY AREA. CRACK L=0.140 IN. MAINTENANCE REPLACED LINTEL LOC. BTW FR66 AND FR68 AT LEVEL STRG 8R, PASSENGER CABIN, AFT GALLEY AREA IAW A319 SRM 51-72- - [SDR AALA202506169630](https://openairdocs.org/sdr/AALA202506169630.md): Hinge Fitting · excess play · Jun 13, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING # 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001- - [SDR AALA202506163392](https://openairdocs.org/sdr/AALA202506163392.md): Hinge Fitting · excess play · Jun 13, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING # 4ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001 - [SDR AALA202506162769](https://openairdocs.org/sdr/AALA202506162769.md): Hinge Fitting · excess play · Jun 10, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING N6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507060394](https://openairdocs.org/sdr/AALA202507060394.md): Fitting · corroded · Jun 9, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FITTING HOLE LOC. AT DOOR CUTOUT BTW FR55A AND FR 56 AT LEVEL STR 38R AT LOWER FUSELAGE MEASURES OF CORROSION IS L= 1.375 INCH W= 1.017 D=0.010 INCH. MAINTENANCE REPLACED FITTING AND FASTENERS LOCATED AT DOOR CUTOUT B - [SDR AALA202506165826](https://openairdocs.org/sdr/AALA202506165826.md): Hinge Fitting · excess play · Jun 9, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR 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 AALA202506168250](https://openairdocs.org/sdr/AALA202506168250.md): Hinge Fitting · excess play · Jun 9, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506160136](https://openairdocs.org/sdr/AALA202506160136.md): Hinge Fitting · excess play · Jun 9, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506303285](https://openairdocs.org/sdr/AALA202506303285.md): Bolt · corroded · Jun 8, 2025 · N763US · Airbus A319112 · Wing Main, Frame Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 LOWER BOLT ON LH WING (1 EA) MEASURE OF CORROSION ARE L= 0.306 IN W= 0.06 IN D= 0.006 IN - [SDR AALA202506309817](https://openairdocs.org/sdr/AALA202506309817.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING # 1ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506256177](https://openairdocs.org/sdr/AALA202506256177.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #4ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR 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 AALA202506103068](https://openairdocs.org/sdr/AALA202506103068.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506105225](https://openairdocs.org/sdr/AALA202506105225.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506106358](https://openairdocs.org/sdr/AALA202506106358.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING #2 ON LH HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM END FITTING #2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202506103893](https://openairdocs.org/sdr/AALA202506103893.md): Hinge Fitting · excess play · Jun 7, 2025 · N763US · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING # 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A - [SDR AALA202508257899](https://openairdocs.org/sdr/AALA202508257899.md): Bolt · worn · Jun 2, 2025 · N763US · Airbus A319112 · Main Landing Gear > AIRCRAFT IN BASE MAINTENANCE: WEAR ON FWD FITTING MAIN DOOR UNDER BOLT HEAD ON RH MAIN LANDING GEAR MEASURE WEAR ARE L=1.217 INCH W=0.165 INCH D=0.034 INCH. MAINTENANCE REPLACED FWD FITTING MLG DOOR (DOOR HINGE FITTING) LOC AT FR 42 BTW STR 41RH AND 42RH MAIN - [SDR AALA202506095042](https://openairdocs.org/sdr/AALA202506095042.md): Attach Bolt · corroded · Jun 2, 2025 · N763US · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 5 ON FWD BOLT RH WING CORRODED AREA IS L=0.350 IN W=0.067 IN D= 0.006 IN. MAINTENANCE REPLACED FWD BOLT ON SLAT TRACK 5 PER JOB CARD 26C61057005. - [SDR AALA202506096931](https://openairdocs.org/sdr/AALA202506096931.md): Attach Bolt · corroded · Jun 1, 2025 · N763US · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 ECCENTRIC LOWER BOLT ON RH WING CORRODED AREA IS L=0.256 IN W=0.116 IN D=0.006 IN. MAINTENANCE REPLACED ATTACH BOLT ON SLAT TRACK #7 RH WING IAW JOB CARD 26C61057005. - [SDR AALA202506302446](https://openairdocs.org/sdr/AALA202506302446.md): Fitting · corroded · May 30, 2025 · N763US · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTABLE BORE ON RH PYLON L=13.567 IN, W = 1.351 IN, D = 0.008 IN. MAINTENANCE REPLACED SPIGOT LOWER FITTING ON RH PYLON IAW A319 SRM 54-51-12-300-001 AND AMM 54-51-41-400-001-A. - [SDR AALA202506062134](https://openairdocs.org/sdr/AALA202506062134.md): Bolt · corroded · May 29, 2025 · N763US · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SLAT BOLT AFT POSITION (ECCENTRIC BOLT) TRACK 3 LH WING, CORROSION MEASURES ARE L=0.227 IN; W=0.105 IN; D=0.008 IN. MAINTENANCE REPLACED LOWER SLAT BOLT AFT POSITION LH WING IAW AMM 27-84-63-400-002-A STEP 4. B - [SDR AALA202508155911](https://openairdocs.org/sdr/AALA202508155911.md): Door Frame · cracked · May 25, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 834 INTERNAL STRUCTURE LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, MEASURE CRACK IS L=4.133 INCH. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGENCY EXIT DOOR (834) F - [SDR AALA202508144042](https://openairdocs.org/sdr/AALA202508144042.md): Profile · cracked · May 25, 2025 · N763US · Airbus A319112 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 834 INTERNAL STRUCTURE RH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, MEASURE CRACK IS L=2.96 INCH. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGENCY EXIT DOOR (834) (RH - [SDR AALA202508143282](https://openairdocs.org/sdr/AALA202508143282.md): Profile · cracked · May 25, 2025 · N763US · Airbus A319112 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 RH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN, MEASURE CRACK IS L=1.856 INCH. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGENCY EXIT DOOR (844) FR40 PLUS 18 INCH BTW - [SDR AALA202508145287](https://openairdocs.org/sdr/AALA202508145287.md): Profile · cracked · May 25, 2025 · N763US · Airbus A319112 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 834 LH LOAD TRASMITTING PROFILE IN PASSENGER CABIN REPLACEMENT OF SEGMENT REQUIRED FOR EO # 5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGENCY EXIT DOOR (834) - [SDR AALA202508018808](https://openairdocs.org/sdr/AALA202508018808.md): Door Frame · cracked · May 25, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844 LH LOAD TRANSMITTING PROFILE IN PASSENGER CABIN MEASURE CRACK IS L=0.588 INCH. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGENCY EXIT DOOR (844) FR40 PLUS 4 INCH BTW S - [SDR AALA202508012800](https://openairdocs.org/sdr/AALA202508012800.md): Profile · cracked · May 25, 2025 · N763US · Airbus A319112 · Emergency Exits > AIRCRAFT IN BASE MAINTENANCE: CRACK EMERGENCY EXIT DOOR 844, (LH SIDE OF DOOR) LOAD TRASMITTING PROFILE IN PASSENGER CABIN, REPLACEMENT OF SEGMENT IS REQUIRED FOR EO #5210Y228-001. MAINTENANCE ACCOMPLISHED MODIFY OVERWING EMERGENCY EXIT CRACKED FRAME ON EMERGE - [SDR AALA202508267542](https://openairdocs.org/sdr/AALA202508267542.md): Pressure Deck · cracked · May 24, 2025 · N763US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MEMBRANE TO CENTER WING BOX AREA, ON FR36 AND Y1292 PLUS 4 INCHES, LH SIDE CRACK DEPTH 0.097 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOCATED AT PRESSURE D - [SDR AALA202507068351](https://openairdocs.org/sdr/AALA202507068351.md): Profile · corroded · May 24, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION DOOR CUTOUT ON SEALING PROFILE LOC. BTW FR56 TO FR59 STR38R LOWER AREA IN AFT CARGO COMPARTMENT. MAINTENANCE MAINTENANCE REPLACED DOOR CUTOUT SHEET. - [SDR AALA202506309672](https://openairdocs.org/sdr/AALA202506309672.md): Floorbeam · corroded · May 24, 2025 · N763US · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOC. AT LEVEL FR16 AT FWD GALLEY AREA (L: 1.436 INCH W: 1.064 INCH D: 0.017 INCH). MAINTENANCE REPLACED FLOOR BEAM Y1292 AND FASTENERS LOC BTW FRAME 12 TO FRAME 24 I.A.W A319 SRM 51-42-11-801 AND SRM 5 - [SDR AALA202508199993](https://openairdocs.org/sdr/AALA202508199993.md): Stringer · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 42L LOCATED BTW FR59 TO FR60 IN AFT CARGO COMPARTM ENT L= 5.236 INCH, W= 0.837 INCH, D= 0.003 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON STRINGER 42L LOCATED BTW FR58 TO FR61 IN AFT CARGO COMPARTMENT IAW E - [SDR AALA202506302864](https://openairdocs.org/sdr/AALA202506302864.md): Floorbeam · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM -Y765 BTW FR69 TO FR70 AT AFT GALLEY AREA MEASURE OF DAMAGE ARE: L=0.316 INCHES, W=0.232 INCHES, D=0.025 INCHES. MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42- - [SDR AALA202506304589](https://openairdocs.org/sdr/AALA202506304589.md): Shear Plate · cracked · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L BTW FR 69 TO FR 70 AT AFT GALLEY AREA L=0.935. MAINTENANCE REPLACED SHEAR PLATE LOC STR 23L BTW FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, SRM 51-72-11-911-001 DWG D53474180. - [SDR AALA202506094914](https://openairdocs.org/sdr/AALA202506094914.md): Splice · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR STRUCTURE UPPER INBOARD SPLICE OF Y1292 AT FR66 AT AF T GALLEY AREA L: 2.347 IN W: 1.275 IN D: 0.036 IN. REPLACED FLOOR STRUCTURE UPPER INBD SPLICE OF Y1292 BTW FR 66 LOC AT AFT GALLEY AREA IAW A319 SRM 51-42-11-80 - [SDR AALA202506093906](https://openairdocs.org/sdr/AALA202506093906.md): Floor Support · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM -Y1162 AT STR 23R AND BTW FR 68 TO FR 69 AT AFT GALLEY AREA. L=1.884 INCH, W=1.704 INCH, D=0.006 INCH. MAINTENANCE REPLACED FLOOR BEAM -Y1162 AT STR 23R AND BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW DWG D53 - [SDR AALA202506094672](https://openairdocs.org/sdr/AALA202506094672.md): Shear Plate · cracked · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23R BTW FR 69 AND FR 70 AT AFT GALLEY AREA. L=1.195 INCH. MAINTENANCE REPLACED SHEAR PLATE LOCATED STR 23R BTW FR 69 AND FR 70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53474 - [SDR AALA202506060170](https://openairdocs.org/sdr/AALA202506060170.md): Floor Support · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR STRUCTURE UPPER INBOARD SPLICE OF Y1162 BTW FR67 AND FR68 AT AFT GALLEY AREA, DAMAGE SIZE L: 1.600 IN W: 1.125 IN D: 0.040 IN. MAINTENANCE REPLACED FLOOR STRUCTURE UPPER INBD SPLICE OF Y1162 BTW FR 67 AND FR 68 - [SDR AALA202506062655](https://openairdocs.org/sdr/AALA202506062655.md): Floor Support · corroded · May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR STRUCTURE UPPER INBD SPLICE OF -Y1162 BTW FR 67 AND F R 68 AT AFT GALLEY AREA, DAMAGE SIZE L: 1.196 INC W:0.853 INCH D: 0.036 INCH. MAINTENANCE REPLACED FLOOR STRUCTURE UPPER INBD SPLICE OF -Y1162 BTW FR 67 AND F - [SDR AALA202508195345](https://openairdocs.org/sdr/AALA202508195345.md): Stringer · cracked · May 22, 2025 · N763US · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME IN PASSENGER CABIN CRACK INDICATION FOUND ON OPEN HOLE ZONE 2 STR 4 FR36 CENTER WING BOX CRACK LENGTH 0.100 INCH AND DIRECTION 9 AND 12 OCLOCK. MAINTENANCE PERFORMED INTERIM REPAIR ON CENTER WING BOX UPPE Next page: https://openairdocs.org/aircraft/N763US/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 = 'N763US' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N763US/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.