Airbus A320-232

Service difficulty reports · 32,653

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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 aircraft_model_key = 'A320232'
  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 YENA2024030500314Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR1/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 4, 2024 · N643JB · Airbus A320232 · Vertical StabilizerSDR YENA2024030500313Hinge Arm · not reportedDURING HEAVY MAINTENANCE: STABILIZER/ VERTICAL STABILIZER/ HINGE ARM BR3/ PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 4, 2024 · N643JB · Airbus A320232 · Vertical StabilizerSDR CALA2024030500636Skin · gougedR/H WING L/E AT #1 SLAT ABOVE #3 TRACK SKIN IS GOUGED APPROX. 1. 5 INCH LONG. REMOVED AND REPLACED SKIN AT RH WING #1 SLAT ABOVE #3 TRACK A320 SRM 51-72-11.Mar 4, 2024 · N491UA · Airbus A320232 · Wing, Plate/SkinSDR AALA202404299455Bypass Valve · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE FLIGHT CREW ABORTED THE APPROACH INTO MZT DUE TO A LOSS OF THE GREEN HYDRAULIC SYSTEM. FLIGHT CREW REPORTED THAT THE GREEN HYDRAULIC QUANITY WENT TO ZERO DURING FINAL APPROACH WITH THE GEAR DOWN AND FLAPMar 3, 2024 · N604AW · Airbus A320232 · Hydraulic System, MainSDR AALA202404157786Mount · corrodedAIRCRAFT IN BASE MAINTENANCE: #2 ENGINE AFT MOUNT 2EA LONG INNER PINS HAS PITTING CORROSION. ENGINE 2 AFT MOUNT INNER PIN REPLACED.Mar 3, 2024 · N679AW · Airbus A320232 · Engine Mount SectionSDR AALA202403079455Hydraulic System · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE FLIGHT CREW ABORTED THE APPROACH INTO MZT DUE TO A LOSS OF THE GREEN HYDRAULIC SYSTEM. FLIGHT CREW REPORTED THAT THE GREEN HYDRAULIC QUANITY WENT TO ZERO DURING FINAL APPROACH WITH THE GEAR DOWN AND FLAPMar 3, 2024 · N604AW · Airbus A320232 · Hydraulic System, MainSDR AALA202403067572Oven · odorAIRCRAFT WAS NOT GROUNDED: FA'S REPORT STRONG BAD ODOR FROM OVEN NUMBER 2. REMOVED AND REPLACED THE FWD #2 OVEN.Mar 3, 2024 · N654AW · Airbus A320232 · Buffet/GalleysSDR YENA2024030600358Unknown · odorFLT#471, LGA-FLL. 'INFLIGHT REPORTED A LEVEL 3 FUME EVENT UPON ARRIVAL, STATING IT BEGAN AT TOP OF DESCENT UNTIL BLOCKIN; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-085B. A/C OK FOR SVC.Mar 3, 2024 · N517JB · Airbus A320232 · Air Distribution SystemSDR CALA2024030500643Fuel Cap · missingPDA 2 FUEL CAP WAS FOUND MISSING PRIOR TO REFUELING FUEL CAP WAS CONFIRMED LEFT ON TRUCK IN IAD PRIOR TO FLIGHT 1262-02 COMPLIED WITH GMM. REPLACED FUEL/DEFUEL COUPLING CAP IAW AMM 28-25-41-400-005-A, OK FOR SVC.Mar 2, 2024 · N428UA · Airbus A320232 · Fuel StorageSDR CALA2024030400633Stringer · corrodedAFT CARGO COMPARTMENT FR 56-57 STR 41 L/H HAS CORROSION. R & R STRINGER SEGMENT FR53 TO FR60 STR 41 L/H P/N D5347 042020800 IAW A320 SRM 51-42-11/001 RESTORED INTERIOR FINISH IAW A320 SRM 51-23-11/001.Mar 2, 2024 · N452UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2024030600357Cooling Fan · failedFLT#1289, EWR-SJU. 'FUME EVENT DURING DESCENT THROUGH 8000' ( APU SYSTEM ); REMOVED AND REPLACED APU COOLING FAN ASSY IAW AMM 49-52-00. PLACARD REMOVED. MX-4 UPDATED.'Mar 1, 2024 · N519JB · Airbus A320232 · APU Core EngineSDR YENA2024030600356Wire Harness · shortedFLT#365, BOS-RSW. (AIRCRAFT DIVERTED TO JFK). 'ENG 1 EGT INDICATION INOP. AMBER XX AFTER TAKEOFF; PER TSM 77-20-00-810-801-B. FOUND EGT HARNESS SHORTED TO GROUND REMOVED AND REPLACED ENG #1 EGT HARNESS IAW AMM 77-21-43. OPS CHECK NORMAL.'Mar 1, 2024 · N587JB · Airbus A320232 · Engine Indicating System WiringSDR YENA2024030500337Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 56 TO FR 57 AFT CARGO COMPARTMENT (C PCP RELATED, REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00028) REF AEROMAN WO 2023 365/1 NR 2023-768643 REMOVED AND REPLACED STRINGER 43LMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2024030500336Shear Tie · crackedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC FR65 BTW STR 43L TO STR 44 IN AFT CARGO COMPARTMENT (CPCP RELATED, REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00030) REF AEROMAN WO 2023 365/1 NR 2023-768737 REMOVED AND REPLACED SHEARMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2024030500335Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 6 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00031) REF AEROMAN WO 2023 365/1 NR 2023-768521 AMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500334Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 7 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 9 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00032) REF AEROMAN WO 2023 365/1 NR 2023-768522 Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500333Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE A AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, AT FWD GALLE Y AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00033) REF AEROMAN WO 2023 365/1 NR 2023Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500332Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE C AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00034) REF AEROMAN WO 2023 365/1 NR 2023-768525 AMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500331Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 68 FRAME WEB AFT FACE HORIZONTAL FLANGE L OWER RADII LEVEL OF STR 22R. CRACK L= 0.960 INCH; (RESOLVED ON W/O: 1259323 TASKCARD: NR-00036) REF AEROMAN WO 2023 365/1 NR 2023-768633 ACCOMPLISHED REPAIR PER ECMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500330Skin · debondedDURING HEAVY MAINTENANCE: DEBONDED OB FLAP SURFACE ON RH WING; REPAIRED OB FLAP LOWER SURFACE ON RH WING IAW EC# A24-129-01, EA# 57-0022-24 REVISION 0 AND EA# 57-0022-24 PART 1. TOOL USED: DIGITAL CALIPER: P/N 500-197-30, S/N A21043111, DUE DATE: JUL/20/2024. Mar 1, 2024 · N536JB · Airbus A320232 · Trailing Edge FlapsSDR YENA2024030500329Cleat · corrodedDURING HEAVY MAINTENANCE: CORROSION CLEAT LOC. BTW STR41R AND STR42R AT FR30 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED CLEAT AND FASTENERS LOC ON FRAME 30 BETWEEN STRINGER 41R TO STRINGER 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DRAWING D532Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2024030500328Cleat · corrodedDURING HEAVY MAINTENANCE: CORROSION CLEAT LOC. BTW STR 40R AND STR41R AT FR31 IN FWD CARGO COMPA RTMENT; REMOVED AND REPLACED CLEAT AND FASTENERS LOC ON BTW STRINGER 40R AND STRINGER 41R ON FRAME 31 IN FWD CARGO COMPARTMENT I.A.W. A320 SRM 51-42-11 AND DWG D53Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2024030500327Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME AT FWD GALLEY AREA (1 EA) (FRAME 16 LH IN OPEN FASTENER HOLE C AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK); RESOLVED ON W/O: 1259323 TASKCARD: NR-00040) PERFORMED PERMANENT REPAIR LOCATED OMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024030500326Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE IN OPEN FASTENER HOLE H6 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, AT FWD GALL EY AREA (2 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00041) PERFORMED PERMANENT REPAIR LOCMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500325Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE IN OPEN FASTENER HOLE A AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 9 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00042) PERFORMED PERMANENT REPAIR LOCATED ON DOORMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500324Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 35 LH SIDE FWD FACE TO THE PRESSURE BULKHEAD ATTACHMENT AROUND FASTENER LOCATED 1.5 INCH BELOW STR 30L. CRACK L= 0.120 INCH; ACCOMPLISHED REPAIR OF CRACKS FOUND ON FR35 AND STR30L PRESSURE BULKHEAD ATTAMar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024030500323Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON RH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING IAW A320 SRM 54-51-12-283-002, A320 SRM 54-51-12-300-002, AND AMM 54-51-41-400-001-A TOOL USED: CALIPER: P/N: 500-197-30 S/N: A21043111, Mar 1, 2024 · N536JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2024030500322Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON LH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING ON LH PYLON IAW A320 SRM 54-51-12-283-002 AND A320 SRM 54-51-12-300-002. TOOL USED: DIGITAL CALIPER P/N: 500-197-30, S/N: A21043111, DUE Mar 1, 2024 · N536JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2024030500321Stop Fitting · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024030500320Doubler · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / RHS FR16 DOUBLE JOGGLE AREA HOLE #6, #7, #A, AND #C / CRACKS - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024030500319Attach Fitting · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - TEMPORARY REPAIR (CONSIDERED A MAJOR REPAIR)Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2024030500318Attach Fitting · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - PERMANENT REPAIR (TBD) (CONSIDERED A MAJOR REPAIR)Mar 1, 2024 · N536JB · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2024030500642Fuel Cap · missingPDA 2 FLIGHT CREW REPORTS FUEL CAP IS MISSING PDA LOG PAGE GENERATED IAW GMM 02-30-95, VERIFIED NO FUEL LEAKING FROM COUPLING SEAL. OK TO DEFER THE CAP IS MISSING IAW CDL 28A. INSTALLED NEW FUEL COUPLING CAP. REF: AMM TASK 28-25-41-400-005 -A.Mar 1, 2024 · N456UA · Airbus A320232 · Fuel StorageSDR AALA202403049395Lamp · burned outAIRCRAFT WAS NOT GROUNDED: EXIT SIGN 2R BULBS BURNT OUT. MAINTENANCE REPLACED LAMP ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Mar 1, 2024 · N650AW · Airbus A320232 · Emergency LightingSDR GTIA2024030237959Unknown · odorPOSSIBLE FUMES EVENT THRU FINAL DECENT ABOUT 5000 SPED 180 KTS ENGINES AT IDLE THE SMELL LASTED FOR LESS THAN A MINUTE THE SMELL WAS MUSTY DRY/MOLD -PERFORMED INSPECTION PER TSM 05-50-00-810-831-A NO SIGNS OF CONTAMINATION NOTED WITH AEROTRACER ON BOARD REF 2Mar 1, 2024 · N649NK · Airbus A320232 · Air Distribution SystemSDR YENA2024030400309Tachometer · failedFLT#2613, ATL-LGA. (AIRCRAFT DIVERTED TO JFK). 'TRANSFERED ITEM, REF. LOG 3910901-1. BREAK AUTO BRAKE FAULT, AFTER TAKE OFF; REMOVED & REPLACED TECHOMETER IAW AMM 32-42-57. OPS CHECK GOOD AIRCRAFT OK FOR SERVICE.'Feb 29, 2024 · N662JB · Airbus A320232 · Landing Gear Position and WarningSDR AALA202402293216Wire Harness · damagedAIRCRAFT WAS NOT GROUNDED: EMERGENCY ISLE LIGHT AT SEAT 3C IS INOP. RELAMP DID NOT FIX. REMOVED AND REPLACED ISLE LIGHT AS REQUIRED. NO FIX. FOUND OPEN IN SEAT HARNESS. REPAIRED.Feb 29, 2024 · N651AW · Airbus A320232 · Light System WiringSDR YENA2024022900306Unknown · odorFLT#765, JFK-GCM. 'CABIN ODOR ON DESCENT INTO GCM (DIRTY SOCK); FOLLOWED INFORMATION NOTICE 2017-T015J FOR REPORTED CABIN ODOR. PERFORMED ENGINE RUNS WITH FLIGHT CREW IAW AMM 71-00-00-710-012-B. RAN BOTH ENGINES WITH BLEEDS AND PACKS ON. NO CABIN ODOR / FUME Feb 29, 2024 · N564JB · Airbus A320232 · Air Distribution SystemSDR YENA2024022900305Unknown · odorFLT#461, LGA-PBI. 'STRONG DIRTY DSOCK ODOR AND OIL IN COCKPIT AND CABIN. NOTICED AT 4000 FEET ON ARRIVAL; COMPLIED WITH INFO NOTICE 2017-T0155 B2 DECONTAM LEVEL 2 ACCOMPLISHED PER TSM 05-50-00-010-031 NO ODOR PRESENT ODOR WAS ENVIORMENTAL. A/C OK FOR SVC.'Feb 29, 2024 · N588JB · Airbus A320232 · Air Distribution SystemSDR YENA2024022900304Unknown · odorFLT#613, HPN-FLL. 'AFT FLIGHT ATT SAID HE SMELLED SMOKE OR BURNING WHEN WE LOWERED THE GEAR; PERFORMED INSPECT FOR SMOKE OR BURN SMELL PER TSM 05-50-00-810-8310A. NO HISTORY OR SIGNS OF ODOR . CLASSIFIED AS A TYPE 10 . A/C OK FOR SERVICE.'Feb 29, 2024 · N621JB · Airbus A320232 · Air Distribution SystemSDR AALA202403016988Light · inoperativeAIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT AT L1 DOOR BULKHEAD MISSING RED LIGHT/LENS. MAINTENANCE NOTED THAT THE LAMP WAS HANGING UNSECURED AND WAS INOPERATIVE IN ADDITION TO THE LENS MISSING. REPLACED EMERGENCY EXIT LIGHT PER AMM 33-51-18Feb 28, 2024 · N665AW · Airbus A320232 · Emergency LightingSDR CALA2024022900606Beam · corrodedFRAME AREA AT C69 L/H TRIPLE BEAM TO WEB EVIDENCE OF CORROSION.Feb 28, 2024 · N452UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2024022900604Stringer · corrodedAFT CARGO COMPARTMENT FR 63-64 STR 42 R/H HAS CORROSION.Feb 28, 2024 · N452UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202402285472Light · inoperativeAIRCRAFT WAS NOT GROUNDED: SEAT 26L MOUNTED EMERGENCY EXIT PATH LIGHT INOP. REPLACED ROW 26L SEAT MOUNTED EMERGENCY EXIT PATH LIGHT.Feb 28, 2024 · N662AW · Airbus A320232 · Emergency LightingSDR YENA2024022900303Gasket · leakingFLT#1680, FLL-DCA. 'DURING CRUISE FLIGHT AT FL310 THE FLIGHT ATT CALLED AND STATED THERE WAS AN EXTREMELY LOUD AIR SEAL TYPE NOISE AT ROW 3 A/C LEFT. CONFIRMED BY DH CA TO BE VERY UNUSUAL WEAR WINDOW 3A; REPLACED AOA SENSOR 3FP1 SEAL ON LH FUSALAGE AND REPLACEFeb 27, 2024 · N508JL · Airbus A320232 · Navigation SystemSDR AALA202402288019Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: L1 DOOR FLASHLIGHT FLASHING RED. REMOVED AND REPLACED L1 DOOR FLASHLIGHT.Feb 27, 2024 · N652AW · Airbus A320232 · Emergency EquipmentSDR AALA202402282017Switch · faultyAIRCRAFT WAS GROUNDED: AT APPROXIMATELY 2300Z, DURING CRUISE AT FL 350 RECEIVED ELECTRONIC CENTRALIZED AIRCRAFT MONITOR "HYD G RSVR OVHT" MESSAGE. WE DID THE ECAM ACTIONS, TURNING OFF PTU AND THE ENGINE 1 HYDRAULIC PUMP. AFTER APPROXIMATELY 25 MINUTES, WE RECEFeb 26, 2024 · N659AW · Airbus A320232 · Hydraulic Indicating SystemSDR CALA2024022700553Stringer · corrodedAFT CARGO COMPARTMENT FR 58-59 STR 42 L/H HAS CORROSION PER HAEC O LCQ NR 22824/9292824 GENERATED BY V926223 RMVD AND RPLD STRINGER SECTION P/N 5347042021000 PO 1138917.1 IA W A320 SRM 51-42-11/001 RESTORED STRUCTURE FINISH IAW A320 SRM 51-23-11/001 BY MECH V9Feb 26, 2024 · N452UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2024022800594Actuator · faultedSLAT SYS FAULT. WARNINGS & CORRELATED FAULTS F/CTL SLATS FAULT 27-00 06 19:39:00 SLT 1 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 1 06 19:39:00 SLT 2 SYSTEM JAMCHECK SLT MECH DRIVE 27-80-00 SFCC 2 06 19:40:00. IN REF TO TSM 27-81-00-810-810-A. INSECTED TOFeb 25, 2024 · N498UA · Airbus A320232 · Leading Edge Slat ActuatorSDR YENA2024022600292Warning Light · illuminatedFLT#1247, LGA-TPA. 'UPON GEAR RETRACTION, THE NOSE GEAR SHOWED UNLK AND THE ECAM SHOWED L/G DOORS AND L/G UNLK MESSAGES. GEAR RECYCLED, CLEARED FAULTS.' (SUPPLEMENTAL INFORMATION TO FOLLOW)Feb 25, 2024 · N505JB · Airbus A320232 · Landing Gear Retraction/Extension System
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