N763US

Service difficulty reports · 243

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR AALA202607279637Lamp · inoperativeAIRCRAFT IN BASE MAINTENANCE: FORWARD LEFT CLOSET RED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RE-LAMPED PER AMM 33-51-18 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Jul 22, 2026 · N763US · Airbus A319112 · Emergency LightingSDR AALA202606220852Flashlight · no testAIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.Jun 19, 2026 · N763US · Airbus A319112 · Emergency EquipmentSDR AALA202606153033Door · out of rigAIRCRAFT 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 (AALA2Jun 11, 2026 · N763US · Airbus A319112 · Standard Practices/StructuresSDR AALA202512292083Battery · no testAIRCRAFT 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.Dec 26, 2025 · N763US · Airbus A319112 · Emergency LightingSDR AALA202509125567Power Supply · no testAIRCRAFT 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.Sep 12, 2025 · N763US · Airbus A319112 · Emergency LightingSDR AALA202508011995Hinge Fitting · excess playAIRCRAFT 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 INSPECTIJul 28, 2025 · N763US · Airbus A319112 · Fuselage, Door HingeSDR AALA202508196862Plate · crackedAIRCRAFT 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, A3Jul 26, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508134533Door Frame · crackedAIRCRAFT 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 SRJul 25, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508019065Fitting · crackedAIRCRAFT 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 AJul 25, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508063639Fitting · crackedAIRCRAFT 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-Jul 18, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202507236104Fitting · crackedAIRCRAFT 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.AJul 17, 2025 · N763US · Airbus A319112 · Passenger/Crew DoorsSDR AALA202508115023Gusset · crackedAIRCRAFT 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 A319Jun 29, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508139950Lintel · crackedAIRCRAFT 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-Jun 28, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202506169630Hinge Fitting · excess playAIRCRAFT 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-Jun 13, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506163392Hinge Fitting · excess playAIRCRAFT 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 55-16-42-400-001Jun 13, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506162769Hinge Fitting · excess playAIRCRAFT 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.Jun 10, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202507060394Fitting · corrodedAIRCRAFT 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 BJun 9, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506165826Hinge Fitting · excess playAIRCRAFT 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.Jun 9, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506168250Hinge Fitting · excess playAIRCRAFT 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.Jun 9, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506160136Hinge Fitting · excess playAIRCRAFT 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.Jun 9, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506303285Bolt · corrodedAIRCRAFT 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 INJun 8, 2025 · N763US · Airbus A319112 · Wing Main, Frame StructureSDR AALA202506309817Hinge Fitting · excess playAIRCRAFT 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.Jun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506256177Hinge Fitting · excess playAIRCRAFT 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.Jun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506103068Hinge Fitting · excess playAIRCRAFT 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.Jun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506105225Hinge Fitting · excess playAIRCRAFT 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.Jun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506106358Hinge Fitting · excess playAIRCRAFT 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.Jun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202506103893Hinge Fitting · excess playAIRCRAFT 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-AJun 7, 2025 · N763US · Airbus A319112 · Elevator StructureSDR AALA202508257899Bolt · wornAIRCRAFT 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 MAINJun 2, 2025 · N763US · Airbus A319112 · Main Landing GearSDR AALA202506095042Attach Bolt · corrodedAIRCRAFT 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.Jun 2, 2025 · N763US · Airbus A319112 · Leading Edge DevicesSDR AALA202506096931Attach Bolt · corrodedAIRCRAFT 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.Jun 1, 2025 · N763US · Airbus A319112 · Leading Edge DevicesSDR AALA202506302446Fitting · corrodedAIRCRAFT 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.May 30, 2025 · N763US · Airbus A319112 · Nacelle/Pylon, Main FrameSDR AALA202506062134Bolt · corrodedAIRCRAFT 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. BMay 29, 2025 · N763US · Airbus A319112 · Leading Edge DevicesSDR AALA202508155911Door Frame · crackedAIRCRAFT 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) FMay 25, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508144042Profile · crackedAIRCRAFT 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) (RHMay 25, 2025 · N763US · Airbus A319112 · Emergency ExitsSDR AALA202508143282Profile · crackedAIRCRAFT 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 BTWMay 25, 2025 · N763US · Airbus A319112 · Emergency ExitsSDR AALA202508145287Profile · crackedAIRCRAFT 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)May 25, 2025 · N763US · Airbus A319112 · Emergency ExitsSDR AALA202508018808Door Frame · crackedAIRCRAFT 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 SMay 25, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202508012800Profile · crackedAIRCRAFT 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 EMERGEMay 25, 2025 · N763US · Airbus A319112 · Emergency ExitsSDR AALA202508267542Pressure Deck · crackedAIRCRAFT 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 DMay 24, 2025 · N763US · Airbus A319112 · Fuselage Main, StructureSDR AALA202507068351Profile · corrodedAIRCRAFT 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.May 24, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506309672Floorbeam · corrodedAIRCRAFT 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 5May 24, 2025 · N763US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202508199993Stringer · corrodedAIRCRAFT 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 EMay 23, 2025 · N763US · Airbus A319112 · Fuselage Main, Longeron/StringerSDR AALA202506302864Floorbeam · corrodedAIRCRAFT 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-May 23, 2025 · N763US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202506304589Shear Plate · crackedAIRCRAFT 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.May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506094914Splice · corrodedAIRCRAFT 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 51-42-11-80May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506093906Floor Support · corrodedAIRCRAFT 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 D53May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506094672Shear Plate · crackedAIRCRAFT 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 D53474May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506060170Floor Support · corrodedAIRCRAFT 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 68May 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202506062655Floor Support · corrodedAIRCRAFT 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 FMay 23, 2025 · N763US · Airbus A319112 · Fuselage Miscellaneous StructureSDR AALA202508195345Stringer · crackedAIRCRAFT 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 UPPEMay 22, 2025 · N763US · Airbus A319112 · Fuselage Main, Longeron/Stringer
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