Airbus A320-232
Service difficulty reports · 32,652
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 SDR 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 "SDR 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.SDR 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 REQUIREDSDR 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 REQUIRESDR 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 CATSDR 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 ISDR 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 TBDSDR 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 SUBSSDR 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 THRESHOSDR 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 2530-2501SDR 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 3292706-02SDR 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 SDR 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 SDR 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.SDR 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.'SDR 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 SDR 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 PASSEDSDR 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.SDR AALA202501218083Megaphone · inoperativeAIRCRAFT WAS NOT GROUNDED: MEGAPHONE INOP. MAINTENANCE REPLACED FC MEGAPHONE IAW AMM 25-65-51.SDR 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 GOODSDR 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, SECTIOSDR 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.SDR CALA2025012300185Web · corroded#2 MOVABLE FAIRING INTERNAL WEB CORRODED. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11-001.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 53-51-11-300-002SDR 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.SDR 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.SDR 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 V935513SDR 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 FISDR 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 LHSDR 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 SDR 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 DOOSDR 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 DOORSDR 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, PSDR 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 ASDR 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 SIDESDR 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 AEROMASDR 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 AEROMSDR 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-A3SDR 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-SDR 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-SDR 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#SDR 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 # 13776SDR 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.SDR 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.SDR 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.
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