N760US

Service difficulty reports · 197

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 = 'N760US' 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 AALA202610088200Chiller · odorAIRCRAFT WAS NOT GROUNDED: AFT GALLEY CHILLER INOP. CABIN CREW NOTICED THE AFT GALLEY CHILLER WAS NOT OPERATING PROPERLY AND HAD AN ODOR BEFORE SHUTTING THE CHILLER OFF. (OPEN)Oct 4, 2026 · N760US · Airbus A319112 · Buffet/GalleysSDR AALA202609143020Elec Connector · looseAIRCRAFT WAS GROUNDED, WHITE EMERGENCY LIGHT ON SIDE OF SEAT 25C IS NOT WORKING. MAINTENANCE FOUND LOOSE CONNECTOR BY SIDEWALL AND RECONNECTED CONNECTOR. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.Sep 10, 2026 · N760US · Airbus A319112 · Emergency LightingSDR AALA202609141135Elec Connector · looseAIRCRAFT WAS GROUNDED: WHITE EMERGENCY LIGHT ON SIDE OF SEAT 24C IS NOT WORKING. MAINTENANCE FOUND LOOSE CONNECTOR BY SIDEWALL AND RECONNECTED CONNECTOR, A SATISFACTORY OPS CHECK WAS ACCOMPLISHED WITH NO ISSUES NOTED.Sep 10, 2026 · N760US · Airbus A319112 · Light System WiringSDR AALA202609063873Cids · faultedAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED THAT ION TOUCHDOWN THERE WAS A CONTINUOUS ALARM IN THE FLIGHT DECK THAT CONTINUED AFTER SHUTDOWN WITH NO ASSOCIATED INDICATIONS *RAPID BEEPING* FOR ABOUT 10 MINUTES, THEN STOPPED ON ITS OWN AND CAME BACK FOR ABOUT 30Sep 2, 2026 · N760US · Airbus A319112 · Emergency EquipmentSDR AALA202607224089Power Supply · no testAIRCRAFT WAS NOT GROUNDED: FAULT DISPLAYED FOR EMERGENCY POWER SUPPLY UNIT 12WL DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED.Jul 22, 2026 · N760US · Airbus A319112 · Emergency LightingSDR AALA202606030456Stay · wornAIRCRAFT WAS GROUNDED: WHILE TROUBLESHOOTING A NOSE LANDING GEAR SHIMMY AFTER TAKEOFF DISCREPANCY MAINTENANCE NOTED THAT THE NOSE LANDING GEAR JOINT AND LOWER FORESTAY TO NLG LEG ATTACH POINT APPEARED TO HAVE EXCESSIVE PLAY. MAINTENANCE REPORTED THAT THE NOSE May 30, 2026 · N760US · Airbus A319112 · Nose/Tail Landing GearSDR AALA202605205986Cids · faultedAIRCRAFT WAS NOT GROUNDED: UPON POWER UP EMERGENCY CALL PUSHBUTTON AND EVACUATION COMMAND BUTTON ILLUMINATED. MAINTENANCE REPLACED THE #2 CIDS DIRECTOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 23-73-34.May 19, 2026 · N760US · Airbus A319112 · Emergency EquipmentSDR AALA202605203548Battery · no testAIRCRAFT WAS NOT GROUNDED: LORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED DURING EMERGENCY LIGHTS TEST. REPLACED BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.May 19, 2026 · N760US · Airbus A319112 · Emergency LightingSDR AALA202604279795Module · leakingAIRCRAFT WAS GROUNDED: AIRCRAFT FUMES WHILE DESCENDING OUT OF FL180. ACRID SOCK SMELL. MAINTENANCE REPLACED APU OIL LUBE MODULE GTCP PER AMM 49-91-45. **SUPPLEMENTAL REPORT FOR SDR AALA202604249795 SUBMITTED BY DFW 4/24/26.Apr 22, 2026 · N760US · Airbus A319112 · APU Oil SystemSDR AALA202604249795Unknown · odorAIRCRAFT WAS GROUNDED: AIRCRAFT FUMES WHILE DESCENDING OUT OF FL180. ACRID SOCK ODOR. (OPEN)Apr 22, 2026 · N760US · Airbus A319112 · Air Distribution SystemSDR AALA202603272567Solenoid Valve · leakingAIRCRAFT WAS GROUNDED: SOF EVENT. SMELL WAS REPORTED BY CABIN CREW AS BURNT RUBBER OR VERY HOT PLASTIC. MILD ODORS WERE NOTED FOLLOWING TAKEOFF BUT WERE NOT OBTRUSIVE OR IMPAIRING AND APPEARED TO DISSIPATE. THE ODOR RETURNED ON DECENT. MAINTENANCE REPLACED AMar 23, 2026 · N760US · Airbus A319112 · APU Oil SystemSDR AALA202601150809Power Supply · faultyAIRCRAFT WAS NOT GROUNDED: DURING OPS CHECK OF EMERGENCY LIGHTING SYSTEM FOUND AFT LT UNIT FAULT. MAINTENANCE REPLACED AFT L EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38.Jan 12, 2026 · N760US · Airbus A319112 · Emergency LightingSDR AALA202601026113Accumulator · low pressureAIRCRAFT WAS NOT GROUNDED: EMERGENCY ACCUMULATOR NITROGEN PRESSURE BELOW LIMITS. MAINTENANCE SERVICED EMERGENCY ACCUMULATOR NITROGEN PRESSURE IAW AMM 32-44-11.Jan 2, 2026 · N760US · Airbus A319112 · Passenger/Crew DoorsSDR AALA202507060201Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE DOOR DAMPER CYLINDER ON PASSENGER CREW DOOR 831 ATFWD GALLEY AREA. MAINTENANCE PERFORMED CHARGING OF DOOR DAMPER CYLINDER ON PASSENGER CREW DOOR 831 AT FWD GALLEY AREA IAW AMM 52-10-00-614-001-A STEP 4.BJul 3, 2025 · N760US · Airbus A319112 · Passenger/Crew DoorsSDR AALA202506096133Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 2 MID FWD BOLT ON LH WING. L:0.048 IN, W:0.019 IN, D:0.007 IN. MAINTENANCE REPLACED ATTACH BOLT SLAT TRACK #2 ON LH WING IAW JOB CARD 26C51057005.May 25, 2025 · N760US · Airbus A319112 · Leading Edge DevicesSDR AALA202506052124Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 2 UPPER AFT BOLT ON LH WING. L:0.040 IN, W:0.018 IN, D:0.006 IN. MAINTENANCE REPLACED AFT BOLT LH WING STAT TRACK 2 IAW JOB CARD 26C51057005.May 25, 2025 · N760US · Airbus A319112 · Leading Edge DevicesSDR AALA202506302705Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER FR65 STRG 31 RH AFT CARGO COMPARTMENT L=3.889 INCH, W=0.614 INCH, D=0.172 INCH. MAINTENANCE REPLACED NEW SECTION STRINGER 31 RH LOC BETWEEN FR64 TO FR65 AFT CARGO COMPARTMENT IAW A319 SRM 51-42-11-801, A319 SRMay 2, 2025 · N760US · Airbus A319112 · Fuselage Main, Longeron/StringerSDR AALA202505086999Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505055642Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505058008Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505050507Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505052860Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 3 ON RH HORIZONTAL STABILIZER IAW AMM-55-16-42-000-001-A AND AMM-55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505055258Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505057426Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER (1 EA)IAW AMM-55-16-42-000-001-A AND AMM-55-16-42-400-001-A.May 2, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505054569Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.May 1, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505050170Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER (1 EA)IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 30, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202507064513Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE AT OPEN FASTENER HOLE 2 INCH OB FROM -Y1292. CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.090 INCH, IN FWD CARGO COMPARTMENT. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIApr 28, 2025 · N760US · Airbus A319112 · Fuselage Main, FrameSDR AALA202507046495Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 PRESSURE DECK MEMBRANE AT OPEN FASTENER HOLE 2 INCH OB FROM Y1292. CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO COMPARTMENT.Apr 28, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202506135618Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK STIFFENER ASSY -Z169 FR 1 ON FORWARD PRESSURE BULKHEAD MEASURE OF CRACK IS L=3.946 INCH. MAINTENANCE REPLACED STIFFENER LOC. ON Z-169 AT FR 1 ON FORWARD PRESSURE BULKHEAD IAW A319 SRM 51-42-11-801 AND DWGD53133319 AND D531Apr 27, 2025 · N760US · Airbus A319112 · Fuselage Main, BulkheadSDR AALA202505200281Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BETWEEN FRAME 66 TO FRAME 68 LH SIDE AFT GAL LEY AREA CORROSION AREA IS L: 2.205 INCHES, W:0.530 INCHES, D:0.009 INCHES. MAINTENANCE REPLACED CENTER FITTING LOC. AT LEVEL STR23L AND BTW FR66 TO FR68 AT AFApr 27, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202505208347Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BETWEEN FRAME 66 TO FRAME 68 RH SIDE AFT GALL EY AREA CORROSION AREA IS L:6.057 INCHES, W:4.335 INCHES, D:0.103 INCHES. MAINTENANCE REPLACED CENTER FITTING LOC. AT LEVEL STR23R AND BTW FR66 TO FR68 AT AFT Apr 27, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202506034980Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION INBOARD PIN SPOILER 3 HINGE ON LH WING, MEASURES OF CORROSION ARE L= 0.537 INCH W= 0.154 INCH D= 0.002 INCH. MAINTENANCE REPLACED HINGE PIN ON SPOILER 3 LH WING IAW AMM 27-64-43-400-001-A STEP 4A(3).Apr 26, 2025 · N760US · Airbus A319112 · SpoilersSDR AALA202603183710Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 1 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 6 AT FR 36 AND -Y1292. REPAIRED FLOOR BEAM PER EA 364302.Apr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202603183720Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 2 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 6 AT FR 36 AND -Y1292. REPAIRED FLOOR BEAM PER EA 364302.Apr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202507044428Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 5 ZONE RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.25 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC. ON CENTER WINGBOX UPPER BEAM -Y765 PApr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202507044674Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 4 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.687 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC. ON CENTER WINGBOX UPPER BEAM -Y254Apr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202507048878Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 3 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.937 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC ON CENTER WINGBOX UPPER BEAM Y254 PApr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202507046222Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 2 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.625 INCH.Apr 24, 2025 · N760US · Airbus A319112 · Fuselage Main, Floor BeamSDR AALA202506309598Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR 35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT AROUND FASTENER LOCATED 1 INCH BELOW STR 30L. CRACK L= 0.190 INCH AT 3 OCLOCK AND CRACK L= 0.260 INCH AT 9 OCLOCK. MAINTENANCE PERFORMED TIME LIMITED REPAIR Apr 23, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202505200079Shear Tie · not reportedAIRCRAFT IN BASE MAINTENANCE: LH FR43 FOOT COUPLING REPLACEMENT REPAIR IAW EO 5320Y003-002. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (REPLACED FR 43 LH COUPLING BTW STR18/24) IAW EA 364176 AND DWG R53370232 ISSUE D.Apr 22, 2025 · N760US · Airbus A319112 · Fuselage Internal Mounting StructureSDR AALA202506307645Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATOR ON LATERAL POST WINDOW FRAME UPPER ATTACHMENT LH SIDE CRACK LENGTH 11 O CLOCK (L:0.438 INCH). MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (REPLACED LH LATERAL WINDOW FRAMING) IAW EA 364034.Apr 20, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202506252572Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATOR ON LATERAL POST WINDOW FRAME UPPER ATTACHMENT RH SIDE MEASURE CRACK L=0.125 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (REPLACED RH LATERAL WINDOW FRAMING) IAW EA 364032.Apr 20, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202505084622Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505050922Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202505056077Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N760US · Airbus A319112 · Elevator StructureSDR AALA202507063406Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON VERTICAL JUNCTION FLANGE OF THE WINDSHIELD C ENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.075 INCH. MAINTENANCE REPLACED CENTER WINDSHIELD FRAME POST LH SIDE Y0, BTW FR 2 TO FR4 IAW EA 3Apr 18, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202507066879Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER RADIUS OF THE WINDSHIELD CENTER POST L OWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.390 INCH. MAINTENANCE REPLACED CENTER WINDSHIELD FRAME POST RH SIDE Y0, BTW FR 2 TO FR4 IAW EA 363997.Apr 18, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202507044415Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF THE WINDSHIELD LOWER A TTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.200 INCH. MAINTENANCE REPLACED CONTINUITY FITTING RH ON Y0 BTW FR1 TO FR2 ON WINDSHIELD CENTER POST IAW EA 363997.Apr 18, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202506301908Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF THE WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.200 INCH. MAINTENNCE REPLACED CONTINUITY FITTING LH LOC ON Y0 BTW FR1 TO FR2 ON WINDSHIELD CENTER POST IAW EA 36399Apr 18, 2025 · N760US · Airbus A319112 · Fuselage Main, StructureSDR AALA202409309373Battery · no testAIRCRAFT WAS GROUNDED: DURING PS CHECK, WHILE PERFORMING EMER LT TEST, FOUND MTX MSG EPSU BATTERY EMER L FAULT MSG. FOLLOWED TSM 33-51-00-810-802-A, REMOVED AND REPLACED ESPU BATTERY 11WL.Sep 28, 2024 · N760US · Airbus A319112 · Emergency Lighting
Back to N760US