Airbus A320-232

Service difficulty reports · 32,652

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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 GTIA2025011638687Access Panel · corroded"CORROSION FOUND ON LEFT WING FUEL ACCESS PANEL BETWEEN RIBS 14 AND 15 HOLE ""AB"" AT THE 12 O'CLOCK POSITION. LENGHT .4180 WIDTH .4180-REPAIRED FASTENER HOLE FOR LEFT WING FUEL MAN HOLE 540JB IAW A320 SRM 57-21-11-300-002 RDAF 81503198 / 0372024#B SRI 2800FC Jan 21, 2025 · N619NK · Airbus A320232 · Wing, Plate/SkinSDR GTIA2025011638686Door Sill · corroded"INSEDE CABIN AFT WET AREA R-2 DOOR SILL BEAM AT FRAME 68 HAS CORROSION. LENGTH .5 WIDTH .5 DEPTH .063-REPAIRED ACP ON HAECO S.O. 122206 OPS 44330 IAW A320 SRM 53-41-14 CAT A REPAIR NO RE INSPECTION REQUIRED "Jan 21, 2025 · N619NK · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2025011638685Frame · dentedDENT ON FUSELAGE FRAME 61+18 STRINGER 36+1 LEFT, LENGTH 1.0 WIDTH 1.1 DEPTH .018, RAF-01 -REPAIRED DENT IAW A320 SRM 53-41-11-300 036 AT FR 67+18STR 36 L CAT A REPAIR.Jan 21, 2025 · N619NK · Airbus A320232 · Fuselage Main, FrameSDR GTIA2025011638684Stop Fitting · crackedFR 68 LH DOORSTOP FITTING #7 HOLE #1 HAS CRACK INDICATIONS RAF-01 3371750-02 -REPAIR ACP ON HAECO S.O 122206 OPS 44630 IAW A320 SRM 53-41-12-300-010 CAT A REPAIR NO RE INSPECT REQUIREDJan 21, 2025 · N619NK · Airbus A320232 · Fuselage Main, StructureSDR GTIA2025011638683Skin Panel · corrodedFWD CARGO COMPT PROFILE PANEL HOLE CORROEDED FRAME 28 STR 37R RAF 01 3371750-01 GENERATED SDR CREATED-REPAIRED FWD CARGO COMPT FASTENR HOLE AT FRAME 28 STR 37A IAW SRM 51-44-11 RDAF AIRBUS 81515054/003 2024#A FOUND TO BE CAT A REPAIR, NO FURTHER ACTION REQUIREJan 21, 2025 · N619NK · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2025011638682Skin · gouged"LEFT WING BOTTOM SKIN AT FUEL TANK ACCESS BETWEEN RIB 14-15 HAS GOUGE ON FWD SIDE OF ACCESS CUTOUT RAF-01 3292701-01 LENGTH 1.4 WIDTH .040 DEPTH .0655 SDR CREATED-REPAIRED LH WING SKIN AND FUEL ACCESS BETWEEN RIB 14-15 BOTTOM SKIN TOP SURFACE MAJOR REPAIR CATJan 21, 2025 · N619NK · Airbus A320232 · Wing, Plate/SkinSDR GTIA2025011638681Bushing · bent"LEFT WING SHARKLET NUMBERED FRONT TO BACK BUSHINGS ARE BENT AND PITTED AT LUG #1-6,9,11 RAF-01 3292702-02 LENGTH 1.7 WIDTH 1.175 DEPTH .014 SDR CREATED -REMOVED AND REPLACED LH WING SHARKLET BUSHINGS INSP THRESHOLD 64400 FC / 128200 FH FROM A/C FIRST FLIGHT IJan 21, 2025 · N619NK · Airbus A320232 · Wing, Attach FittingsSDR GTIA2025011638680Lug · gougedLH WINGTIP, SHARKLET LUGS FRONT TO BACK #2 & #7 LUGS HAVE GOUGE RAF-01 3292702-01 REPAIRED LH WING SHARKLET LUGS, REF AIRBUS RDAF 81512142/003/2024#A CAT B REPAIR 80,400FC / 160,900 FH FROM A/C FIRST FLIGHT INTERVAL TBD METHOD OF INSPECTION TBDJan 21, 2025 · N619NK · Airbus A320232 · Wing, Attach FittingsSDR GTIA2025011638679Stop Fitting · cracked" FR 66 DOORSTOP FITTING #7, HOLE #1, (TOP, INBD) HAS A CRACK INDICATION 10:OCLOCK POS (AFT LOOKING FWD) 100% . LENGTH .4735 WIDTH 4.735-REPAIR ACCOMPLISHED REF HAECO S.O. 122206 OPS 44631 IAW A320 SRM 53-41-12-300-011 CAT B REPAIR RE INSPECT AT 15400 FC SUBSJan 21, 2025 · N619NK · Airbus A320232 · Fuselage Main, StructureSDR GTIA2025011638678Lug · damagedRIGHT WING TIP SHARKLET STRUCTURE - LUGS NUMBERED FROM FRONT TO BACK LUGS GOUGED AT #3,8,#6 RAF -01 3292703-1 GENERATED-REPAIRED RH WING TIP SHARKLET STRUCTURE REF A320 SRM 51-73-00 AND RDAF REF 81514401 / 003 / 2024#A WITH CAT B MINOR REPAIRINSPECTION THRESHOJan 21, 2025 · N619NK · Airbus A320232 · Wing, Attach FittingsSDR GTIA2025011638677Table · damagedG 1 GALLY WORK DECK REQUIRES REPLACEMENT RAF-01 3292704-01 GENERATED-TEMPORARY LIFE LIMMITED REPAIR OF GALLEY G1 WORKDECK TOP METALIC SKIN CRAKED COMPLIED WITH IAW EA 2530-2501Jan 21, 2025 · N619NK · Airbus A320232 · Buffet/GalleysSDR GTIA2025011638676Table · damagedINSIDE CABIN G4 GALLEY WORKDECK IS DELAMINATED -REMOVED AND REPLACED G4 GALLEY WORKDECK KIT 263422-50011 IAW REF TR 2533-015 RAF -01 GENERATED 3292706-02Jan 21, 2025 · N619NK · Airbus A320232 · Buffet/GalleysSDR GTI2025F00004Lug · damaged"RIGHT WING SHARKLET ASSY. LUGS NUMBERED FROM FRONT TO BACK - GOUGED LUGS AT #2,3,4 RAF-01 3292704-02 GENERATED-EVALUATED AND REPAIRED RH WING SHARKLET ASSY LUGS #2, #3, #4 IAW A320 SRM 51-73-00 CAT C LIMMITATIONS. SOLUTIONS LIFE OR LIMMITATIONS 6 MONTHS RDAF Jan 21, 2025 · N619NK · Airbus A320232 · Wing, Attach FittingsSDR YENA2025012200099Rod End · damagedFLT#240, NAS-MCO. 'L2 DOOR ARMING/DISARMING LEVER HAS VERY LITTLE TENSION AND DROPS DOWN AUTOMATICALLY WHEN IN THE UP POSITION; REMOVED AND REPLACED L2 DOOR ARMING CABLE EYE ROD END BOTTOM DOOR IAW AMM 52-13-22. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THE Jan 20, 2025 · N709JB · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025012100162Spar · crackedR/H PYLON O/B SLIDE SPAR DOUBLER HAS CRACK. R & R R/H PYLON O/B SPAR IAW A320 SRM 51-75-12-911-001.Jan 20, 2025 · N455UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2025012200094Bleed Air Sys · odorFLT#743, JFK-AUA. 'DIRTY SOCK SMELL REPORTED BY FLIGHT ATTENDANT FROM MID TO AFT CABIN ( APU BLEED AIR SUPPLY SYSTEM ); REF LP # 4219340, ITEM 2 OR WO # 1387703 TSI . THIS CLEARS THIS MDDR. MDDR CLEARED. MX-4 UPDATED. PLACARD RMVD. MCC NOTIFIED.'Jan 20, 2025 · N613JB · Airbus A320232 · APU Bleed Air SystemSDR YENA2025012200093Actuator · faultedFLT#704, RSW-BDL. (AIRCRAFT DIVERTED TO MCO). 'NOSE GEAR DID NOT RETRACT PROPERLY AFTER TAKEOFF. NOSE GEAR UNLOCKED ECAM PERFORMED GEAR EXTENDED NORMAL LANDING; INSTALLED NLG UNLOCKING ACTUATOR PER A320 AMM 32-31-23 OPS CHECK AND FUNCTIONAL CHECK OF FREE FALL Jan 20, 2025 · N608JB · Airbus A320232 · Nose/Tail Landing GearSDR CALA2025012301984Battery · faultedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS FOUND ESPU BATTERY FORWARD LEFT (ABOVE DOOR 1L) BAD. REMOVED AND REPLACED L1 ESPU BATTERY REF AMM 33-51-38. SYSTEM TEST PASSEDJan 19, 2025 · N495UA · Airbus A320232 · Emergency LightingSDR YENA2025012200098Indication Sys · failedFLT#62, PBI-LGA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO PBI) ' AT FL 280 MAP NOT AVAILABLE AUTO THR OFF, NO FLIGHT DIRECT A/P OFF. RAN CK LIST ADV MX . RETURNED TO PBI; ACCOMPLISHED TSM 22-11-00-810 REMOVED AND REPLACED FMGC 1 SYS OPS CHECK NORM AMM 22-83-34.Jan 19, 2025 · N569JB · Airbus A320232 · Auto Flight SystemSDR AALA202501218083Megaphone · inoperativeAIRCRAFT WAS NOT GROUNDED: MEGAPHONE INOP. MAINTENANCE REPLACED FC MEGAPHONE IAW AMM 25-65-51.Jan 19, 2025 · N647AW · Airbus A320232 · Emergency EquipmentSDR CALA2025012201966Handle · detachedCOVER ON LH FWD OVERWING EXIT HANDLE FELL OFF ADJUSTED AND TIGHTENED GAP ON FASTENER ARMS ON LEFT FWD OVERWING EMERGENCY EXIT HATCH COVER FLAP. REF AMM 52-21-11-400-001-A. OPS CHECK GOODJan 18, 2025 · N495UA · Airbus A320232 · Emergency ExitsSDR YENA2025012100072Ecs · contaminatedFLT#41, FLL-MDE. 'STRONG ODOR DETECTED BY ALL CREWMEMBERS BEGINNING DURING DESCENT AND CONTINUING UNTIL ENGINES SHUT DOWN AT GATE ODOR WAS INITIALLY SWEET THEN ODOR WAS OIL LIKE AND A LITTLE BURNING SMELL ( PACKS ); COMPLIED WITH INFO NOTICE 2017-T015K, SECTIOJan 18, 2025 · N807JB · Airbus A320232 · Cabin Cooling SystemSDR CALA2025012300186Floor Support · corrodedAFT BULK CARGO FR 58-59 RSTR 38 PROFILE PANEL HAS CORROSION. GEN BY V798788 ON HAECO LCQ NR 9292817 / 36817 REMOVED AND REPLACED PROFILE PANEL AFT CARGO FROM FR 58 - FR59 I AW A320 SRM 51-42-11.Jan 17, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025012300185Web · corroded#2 MOVABLE FAIRING INTERNAL WEB CORRODED. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11-001.Jan 17, 2025 · N455UA · Airbus A320232 · Wing Miscellaneous StructureSDR CALA2025012200171Door Sill · corrodedMAIN CABIN, R-2 ENTRY SILL, AT FR 68 HAS CORROSION. REMOVED AND REPLACED R-2 DOOR SILL IAW A320 SRM 51-72-911-001-00 2.Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025012200170Stiffener · crackedRH FWD EMERGENCY EXIT HATCH AFT VERTICAL STIFFNER IS CRACKED. REMOVED AND REPLACED AFT VERTICAL STIFFENER ON RH FWD EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025012200172Stiffener · crackedRH FORWARD EMERGENCY EXIT HATCH FWD VVERTICAL STIFNER IS CRACKED . REMOVED AND REPLACED FWD VERTICAL STIFFENER ON RH FWD EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025012100161Stringer Clip · corrodedAFT CARGO COMPARTMENT AREA AROUND PRESSURIZATION OUTFLOW VALVE L OWER STRINGER AT FR65 CORRODED. REMOVED AND REPLACED DISCREPANT STRINGER CLIP AND FRAME ST RAP BTW FR 64-67 AT STGR 31 IAW A320 SRM 51-72-11 51-42-11 51-44 -11.Jan 17, 2025 · N449UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2025012100160Skin · dentedFUSELAGE SKIN UPPER R/H SIDE ABOVE HORZ BESIDE RUDDER BETWEEN FR 79-80 STR3-4 R/H HAS PUNCTURE. ACOMPLISHED CAT-A PERMANANT REPAIR ON FUSELAGE SKIN BETWEEN STR3 -4 R/H AT FR79-80 IAW A320 SRM 53-51-11-300-002Jan 17, 2025 · N449UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025012100154Seat Track · corrodedMAIN CABIN SEAT TRACK +Y765 CORROSION OUT OF LIMITS FRAME 63. REMOVED SEAT TRACK +Y765 OUT OF LIMITS FRM 61 / FRM 64 IAW A320 SRM 51-42-11/001 REV 151, REPAIRED AREA ON FRM 61 / FRM 64 IAW A 320 SRM 53-41-15-300-003 REV 151 PAR 2.Jan 17, 2025 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025012100165Stiffener · crackedLH AFT EMERGENCY EXIT HATCH FWD VERTICAL STIFFNER IS CRACKED. REMOVED AND REPLACED VERT STIFFENER ON L/H AFT EMERGENCY EXIT IA W SRM A320 51-72-911-001.Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025012100164Stiffener · crackedLH AFT OVER WING EXIT AFT VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER ON L/H OVER WING EXIT IA W A320 SRM 51-72-911-001. ACMP BY MECH V934190 INSP BY V935513Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012200097Contactor · faultedFLT#821, JFK-NAS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' ELEC BCL 2 FAULT ECAM APPEARED WHILE IN CRUISE; AS PER TSM 24-38-00-810-848-A & ASM 24-38-02, REPLACED CONTACTOR 6PB2 IAW AMM 24-38-58. OPS TEST OK. NO FAULTS NOTED. (REPLACED RELAY 16XC - NO FIJan 17, 2025 · N564JB · Airbus A320232 · Electrical Power SystemSDR YENA2025012100089Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.135 INCH APPROX; REF AEROMAN N/R 2024-755221 REMOVED AND REPLACED FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LHJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100088Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.125 INCH APPROX; REF AEROMAN N/R 2024- 755213, REMOVED AND REPLACED FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD Jan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100087Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.140 INCH APPROX; REF. AERO WO: 2024 423/1 NR 2024-755216 - R&R FR SEGMENTS 1 AT OVERWING EMERG. EXIT DOOR ( AFT LH EEH DOOJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100086Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT RH EEH DOOR 844) CRACK L=0.129 INCH APPROX; REF. AERO WO: 2024 423/1 NR 2024-755222 - R&R FR SEGMENTS 1 AT OVERWING EMERG. EXIT DOOR (AFT RH EEH DOORJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100085Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 RH SIDE, DOOR STOP FITTING 7. CRACK DIRECTION IS: 11 OCLOCK; CRACK DEPTH IS : 0 .118 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00026) REF AEROMAN N/R 2024-755200, PJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100084Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H3 ON FRAME 16 RH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 11 OCLOCK; CRACK DEPTH IS : 0 .120 INCH APPROX; REF AEROMAN N/R 2024-755201, REMOVED AND REPLACED INTERCOSTAL FITTING LOC AJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100083Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 20 LH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 8 OCLOCK; CRACK DEPTH IS : 0. 114 INCH APPROX; REF AEROMAN N/R 2024-755205, PERFORMED REPAIR AT HOLE H1 ON FRAME 20 LH SIDEJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100082Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 LH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 4 OCLOCK; CRACK DEPTH IS : 0. 114 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00027) FUR-A320-53-01952, REF AEROMAJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100081Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 20 RH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 3 OCLOCK; CRACK DEPTH IS : 0. 112 INCH APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00028) FUR-A320-53-01953, REF AEROMJan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100080Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE, AT AFT GALLEY AREA, DOOR STOP 1, INBOARD/LOWER HOLE, CRACK INDICATION LOCATED AT 4 OCLOCK VIEW LOOK ING FROM FWD, DEPTH IS 0.167 INCHES APPROX; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00032) FUR-A3Jan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025012100079Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE FRAME 16 UPPER CORNER DOU BLER JOGGLE AREA HOLE C AT 3 OCLOCK LH SIDE CRACK LENGTH APROX. 0.169 INCH; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00033) FUR-A320-53-01966, REF AEROMAN N/R 2024-Jan 17, 2025 · N729JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025012100078None · noneDURING HEAVY MAINTENANCE: EXISTING REPAIR STRINGER 2 LH FR29 TO FR30 IN PASSENGER CABIN (FOR A320 AGING AIRCRAFT PROGRAM); (RESOLVED ON W/O: 1331840 TASKCARD: NR-00045) PERFORMED REPAIR ON STR 2 LH BTW FR28 TO FR31 IN PASSENGER CABIN IAW A320 SRM 53-21-13-300-Jan 17, 2025 · N729JB · Airbus A320232 · Standard Practices/StructuresSDR YENA2025012100077Duct · damagedDURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/SB-53-1500 TAIL CONE/ SUBSTRUCTUREREMOVAL AND FIXATION OF APU AIR INTAKE DUCT TO THE STRUCTURE/DEVIATIONS/ PERMANENT REPAIR; REFERENCES /1/ AEROMAN EA 53-9072-24 (COVER + PART 1)/2/ AIRBUS TD/81437230/072/2024#Jan 17, 2025 · N729JB · Airbus A320232 · APU Core EngineSDR YENA2025012100076Attach Fitting · corrodedDURING HEAVY MAINTENANCE: VERTICAL STAB TRAILING EDGE #7 RUDDER ATTACH FITTING HAS SMALL AREA OF CORROSION AT FWD LOWER PANEL FASTENER; ACCOMPLISH REPLACEMENT OF HINGE ARM BR7 ON VERTICAL STABILIZER IN ACCORDANCE WITH REF HAECO W/O # 169003 JETBLUE W/O # 13776Jan 17, 2025 · N519JB · Airbus A320232 · Vertical StabilizerSDR YENA2025012100075Wire · pinchedDURING HEAVY MAINTENANCE: EPSU FAILED DUE TO PINCHED WIRES IN WIRE BUNDLE. LOCATION @ 12WL; REF HAECO WO 169003 NR 28519, R&R ESPU AT 12WL IAW AMM 33-51-38-000-001 & 33-51-38-400-001.OPS CHECK GOOD.Jan 17, 2025 · N519JB · Airbus A320232 · Light System WiringSDR YENA2025012100074Slide · faultedDURING HEAVY MAINTENANCE:L1 DOOR EMERGENCY ESCAPE SLIDE INTERNAL FAULT; REF HAECO W/O 169003 NR28557 R & R L1 DOOR SLIDE IAW AMM A320-25-62-44-400-801.Jan 17, 2025 · N519JB · Airbus A320232 · Escape SlideSDR YENA2025012100073Wire Harness · shortedDURING HEAVY MAINTENANCE: EPSU AT LOCATION 10WL FAILED DUE TO A SHORT IN THE L1 SLIDE HARNESS; REF HAECO W/O 169003 NR 28557 R&R EPSU AT 10WL IAW AMM 33051-38-000-001 & 33-51-38-400-001-A OPS CHECK GOOD. NOTE: L1 DOOR SLIDE R & R ON LP 4060374 ITEM 1.Jan 17, 2025 · N519JB · Airbus A320232 · Equipment/Furnishings Wiring
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