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 CALA2025100609633Window Frame · crackedCONTACT ENGINEERING FOR REPAIR INSTRUCTIONS. LEFT WINDSHIELD FWD NODE, MOST INBD HOLE FROM CENTER LINE HAS A CRACK INDICATION AT THE 6:O CLOCK POSITION 100% SH. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 5,600 FLIGHT CYCLES CURRENT HOURS 74772:19 FLSDR CALA2025092209112Spar · corrodedLH WING AFT MOVEABLE FAIRING IS CORRODED. REMOVED AND REPLACED NO. 1 MOVABLE FAIRING UPPER SPAR IAW A320 SRM 54-42-11-P. 5-25SDR YENA2025091700945Battery · no testFLT#591. BOS-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 10WL IAW 33-51-38. OPS CHK GOOD.SDR CALA2025091708999Wire Harness · brokenSEAT 24C SEAT TRIM BROKEN OFF. EMERGENCY LIGHT WIRING PULLED OUT. EMERGENCY LIGHT WIRING CONNECTOR PULLED OUT OF SEAT SIDE WIRING HARNESS. CAPPED AND STOWED SEAT SIDE EXPOSED WIRES. REPLACED SEAT TRIM REF AMM 25-21-41, REMOVED AND REPLACED SGL LIGHT FIXTURE SDR CALA2025091608958Slide · deployedDOOR 1L SLIDE DEPLOYED. REPLACED DOOR 1L SLIDE. REF AMM 25-62-44-400-006-A. REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM. REF AMM 52-10-00-610-001-A. CHARGED THE EMERGENCY OPERATION CYLINDER. REF AMM 52-10-00-614-001-A. ALL OPS CHECK GOOD. AMM 25-62SDR CALA2025091608955Battery · no testEPSU BATTERY FWD L FAULT DURING EMERGENCY LIGHT TEST. R & R FWD LT EPSU BATTERY REF AMM 33-51-38. OPS CHECK PASSED. PARTS USED: 18-3351-3-0001, QTY :1SDR YENA2025091700944Ecs · contaminatedFLT#172, FLL-LGA. CABIN CREW REPORTED FUMES DURING DESCENT IN ROWS 10-15. SMELL OF CHEMICALS OR DIRTY SOCKS; COMPLIED WITH INO NOTICE 2017-T015, ACCOMPLISHED ECS DECONTAMINATION AND REPLACED HEPA FILTERS AND OZONE FILTERS, REF PAGE 4527976 AND 4527977. A/C OK SDR CALA2025091708988Door · no discrepancyFA REPORTED LOUD SQUEELING SOUND FROM LEFT OVERWING EMERGENCY EX IT ROW 21. PRESSURIZED CABIN TO 4 PSI IAW AMM 05-53-00-780-001-A01. NO SQUEELING COMING FROM EXT ROW ON GROUND.SDR YENA2025091600939Unknown · odorFLT#706, FLL-EWR. "WET SOCK GYM LOCKER SMELL IN DESCENT FROM 12000FT - 8000FT; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, MOST PROBABLE CAUSE OF ODOR IS TRANSCIENT OR AMBIENT AIR PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085-SDR CALA2025091608960Spar · corrodedRH WING AFT MOVABLE FAIRING IS CORODDED. REMOVED AND REPLACED UPPER SPAR IAW A320 SRM 51-42-11 P5-25 SRM 51-44-11 P.3 SRM 54-55-12-283-007 FIG 4 SRM 51-57-12-911-001.SDR YENA2025091500934Battery · failedFLT#591, BOS-TPA. "EMERGENCY LIGHT BATTERY (12WL) FAILED TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (12WL) IAW AMM 33-51-38 OPS CHK GOOD. A/C OK CONT SVC."SDR YENA2025091500933Battery · failedFLT#591, BOS-TPA. "EMERGENCY LIGHT BATTERY (10WL) FAILED TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY (10WL) IAW AMM 33-51-38 OPS CHK GOOD. A/C OK CONT SVC."SDR GTIA2025091539076Unknown · odorSOUR SMELLL IN THE CABIN FOUND OIL ALL THE WAY TO THE APU. DESCRIPTION OF ODOR/FUMES: TEMPORARY ODOR DURING DESCENT. APPARENT CABIN SOURCE: UNKNOWN. FLIGHT DECK. NO VISIBLE SMOKE/HAZE. NO MEDICAL ATTENTION REQUIRED.-REF TSM 05-50-00. APU VERIFIED NO LEAKS. PERSDR YENA2025091500931Oil System · leakingFLT#1383, GUA-FLL. "FUMES EVENT ON DECENT THROUGHT 10,000 FEET STUNK IN BACK LESS UP FRONT DIRTY SOCKS OIL; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 TYPE 1 APU AND PERFORMED DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRCSDR CALA2025091508878Light · no testVISUAL INSP FOUND EMERGENCY ROW LIGHTING AT SEAT ROWS 26, 27 AND 28 (ABC) INOPERATIVE. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 26,27,28. IAW TASK 33-51-19-000-002-A AND TASK 33-51-19-400-002-A OPS CHECK GOOD.SDR AALA202511183478Fitting · damagedAIRCRAFT IN BASE MAINTENANCE: ELONGATE HOLE ON SPLICE FITTING L/H LOCATED ON CENTER WINDSHIE LD FRAME POS LOWER ATTACHMENT AREA, MEASURES OF DAMAGE ARE L=0.335IN,W=0.215IN. MAINTENANCE REPLACED SPLICE FITTING L/H LOCATED ON CENTER WINDSHIELD FRAME POST ON LOWSDR GTIA2025091539075Epsu · faultyDURING TASK CARD 256241-03-1 REMOVE DOOR ESCAPE SLIDE (7501MM) EPSU SYSTEM TEST FAILED (13WL)-R/R EPSU BATTERY(13WL) IAW AMM 33-51-38-000-002-A.EPSU SYSTEM TEST IS GOOD.SDR YENA2025091500932Unknown · odorFLT#1310, JAX-BOS. "ELECTRICAL BURING SMELL BETWEEN ROWS 19-24 REPORTED BY FLIGHT ATTENDANTS AND PAX. NO SMOKE VISIBLE DURING TROUBLESHOOTING FA TURNED OFF PED AND SMWLL DISSAPTED. BURNING SMELL LASTED APPROX 5 MIN DURING CRUISE. ( THALES-AVANT IFE (ENTIRE SYSDR YENA2025091500930Unknown · fumesFLT#1380, FLL-GUA. "INFLIGHT COMPLAINED ABOUT FUMES AFTER LANDING BOTH ENGINES OFF APU ON WITH APU BLEED NO NOTIFICATION DURING FLIGHT ( APU SYSTEM ).SDR CALA2025091508876Power Supply · no testEPSU UNIT RT MESSAGE AFTER EMERGENCY LIGHTS TEST NEEDS REPLACED. R & R RT ESPU. REF: AMM TASK 33-51-38-000-002-A & TASK 33-51-38-400-002-A. OP CHECK TEST OKAY, IAW AMM TASK 33-51-00-710-001-A.SDR AALA202512157352Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA ON FRAME JOINT AREA AT LEVEL OF LOWER TENSION BOLT RH SIDE LENGTH =0.197 INCH APPROX. MAINTENANCE PERFORMED TIME LIMITED REPAIR INSTRUCTIONS (REPLACED FRONT WSDR AALA202512120707Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 4 AT Y0. REPLACED CONTINUITY FITTING PER EA 368108.SDR AALA202512089920Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RADIO L/H SIDE ADJACENT AT UPPER TENSION BOLT CRACK DIRECTION 2 OCLOCK, CRACK LENGTH =0.188 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR INSTRUCTIONS SDR AALA202512044909Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 4 AT Y0. REPLACED CONTINUITY FITTING PER EA 368108.SDR AALA202512018174Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND WINDOW POST FRAME UPPER ATTACHMENT AT FR 4. REPLACED WINDSHIELD FRAME PER EA 368189.SDR AALA202511282439Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC.ON WINDSHIELD SIDE POST AT FR.4 LH INTERNAL SIDE OF THE UPPER ATTACHMENT AREA, INTERNAL FI TTING VERTICAL FLANGE MEASURE OF CRACK IS: L: 0.145 INCH. MAINTENANCE ACCOMPLISHED PERMSDR AALA202510246518Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON CONNECTING FITTING ON MLG AREA RH SIDE L=0.152 INCH. MAINTENNCE ACCOMPLISHED PERMANET REPAIR INSTRUCTION (REPLACED CONNECTING PLATE) LOC BTW FR42 TO FR43 AT LEVEL OF WEB W10 AT MLG AREA ON RH SIDE IAW EA 368105, A320 SRM SDR CALA2025091608968Bleed Valve · faultedABORTED TAKEOFF DUE TO ECAMS NOT APPROPRIATE WITH MEL. ACP'D ON L/P 6256763.ENG1 HP VALVE INDICATES OPEN ON BLEED PAGE. ALLOTHER INDICATIONS NORMAL SECURED THE ENGINE 1 HPV CLOSED AND INSTALLED DF STICKER REF MEL 3611S. DM SUGGEST TSM 36-11-00-810-835-A, R &SDR CALA2025091608963None · no discrepancyBIRDSTRIKE ON T/O LEFT WINDSCREEN HOT BRAKES FROM RTO 440 DEGREES. ACP BIRDSTRIKE PER AMM 05-51-14-200-803. ACP'D BIRDSTRIKE INSP OF AIRFRAME AND ENGS PER AMM 05-51-14. NO DAMAGE NOTED.SDR CALA2025091508904Door Frame · crackedLEFT FWD EMERGENCY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED LT FWD EMER EXTI DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D52279010010, D52279040004.SDR CALA2025091508903Door Frame · crackedAFT EMERGECY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED THE LT AFT EMER EXIT DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWINGS D52279010010, D52279040004.SDR CALA2025091508902Door Frame · crackedRIGHT FWD EMERGENCY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED RT FWD EMER EXIT DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D5227900010, D5227040004.SDR CALA2025091508901Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR FWD VERT BEAM CRACKED. REMOVED AND REPLACED RT AFT AMER EXIT DOOR FWD FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWINGS D52279010010, D52279040004.SDR CALA2025091508900Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR & AFT VERT BEAMS CRACKED A3NB-MP-2100-52 2102-01-1-AFT-R. REMOVED AND REPLACED RT AFT EMER EXIT AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D52279010010, D52279040004.SDR CALA2025091508899Unknown · odorFA HEARD BANG ON APPROACH & LOUD NOISE FROM R2 DOOR, SMELLED SMOKE IN AFT GALLEY, AFT FLT ATTENDENTS STATED THEY HEARD BANGING COMING FROM AFT RT DOOR THROUGHOUT FLT. AFT PORTION OF ACFT SMELLED LIKE SMOKE. PILOT STATED ODOR CAME AFTER LANDING, IN AFT CABINSDR CALA2025091208831Door Frame · crackedLT FWD EMER EXIT DOOR FWD AND VERT BEAMS CRACKED. REMOVED AND REPLACED LH FWD EMER EXIT DOOR FWD FRAME SEGMENT IAW A320 DRM 51-42-11/001 AND DRAWING D52279010010, D52279040004. P ERFORMED BY V061630 AND INSP BY N078625SDR CALA2025091208827Door Frame · crackedLT AFT EMER EXIT DOOR FWD AND VERT BEAMS CRACKED. REMOVED AND REPLACED LH AFT EMER EXIT DOOR FWD VERT BEAM IAW A32 0SRM 51-42-11/001 AND DRAWINGS D52279010010 AND D52279040004.SDR GTIA2025091139074Epsu · inoperativeDURING SERVICE CHECK EPSU 12WL FOUND FAILED-REMOVED + REPLACED EPSU 12 WL IAW AMM 33-51-38 OPS CHECK GOODSDR AALA202511186370Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING RH SIDE AFT LUG, WEB LOWER RADIUS. CRACK LENGTH IS 0.150 INCH APPROX, AT MAIN WHEEL WELL.SDR AALA202510282854Keelbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING LH SIDE FWD LUG, WEB LOWER RADIUS. CRACK LENGTH IS 0.130 IN, AT MAIN WHEEL WELL. ACCOMPLISHED PERMANENT REPAIR INSTRUCTION (REPLACED DOOR HINGE FITTING) LOC. BTW FR42 AND FR43,SDR CALA2025091708995Shear Tie · corrodedAFT CARGO FRAME SHEAR TIE AT FR 62 BETWEEN STRINGER 42L AND 43L HAS CORROSION. REMOVED AFT CARGO FRAME SHEAR TIE FR 62 STR 42L & 43L. FABRICATED AND INSTALLED NEW SHEAR TIE AS REQUIRED IAW SRM 51-72-11-911-00 1.SDR CALA2025091208825Door Frame · crackedRT FWD EMER EXIT DOOR FWD VERT BEAMS CRACKED. REMOVED AND REPLAED RT FWD EMER EXIT DOOR'S FWD VERT DRAIN IAW A 320 SRM 51-42-11/001 AND DRAWINGS D52279010010 AND D52279040004 ESFR #1827.SDR YENA2025091200926A/C Pack · odorFLT#1144, MCO-MHT. INFLIGHT REPORTED DIRTY SOCK SMELL IN CABIN IN FLIGHT AND ON THE GROUND (PACKS); PERFORMED LEVEL C DECONTAM. IAW AMM 21-00-00-615-804-A ECS PACK 1+2 OK FOR SVC. MX-4 UPDATED, PLACARD REMOVED.SDR CALA2025091108779Floorbeam · corrodedAFT CABIN FLOORBEAM, -Y1292 GOUGED AT FR68. REMOVED AND REPLACED BEAM -Y1292, FR 68 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, CMM 51-21-11/001, SRM 53-41-14- 283-009, SRM 53-41-14-01A, & SRM 51-11-12/001.SDR CALA2025091108777Seat Track · corrodedSEAT TRACK Y765 FR 25-35 HAS CORROSION. PERFORMED REPAIR ON SEAT TRACK Y765, FR 25-35 IAW SRM 53-21- 15-300-004.SDR CALA2025091108772Fitting · damagedUPON REINSTALLATION OF RT MLG DOOR ACTUATOR, REQURIED GAP COULD NOT BE OBTAINED AFTER WASHER NAS1149C1016R INSTALLED. REPLACED RH MLG DOOR ACTUATOR FITTING FWD AND AFT AIRBUS DWG R83 370501 ISSUE F.SDR AALA202509106666Bottle · no testAIRCRAFT IN BASE MAINTENANCE: DO NOT PASS DAMPING TEST FUNCTION DOOR DAMPER PASSENGER CREW DOOR 832AT AFT GALLEY AREA. MAINTENANCE REPLACED DOOR DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.SDR CALA2025091008740Battery · no testEMERGENCY LIGTH TEST SHOWING EPSU BATTERY EMER R, EPSU BATTERY EMER L, AND AFT L DURING SERVICE CHECK 2. RESET CB ON 49VU H5, H6 AND 122VU V7, PERFORMED CIDS EMERGENCY LIGHT TEST AND JUST HAVE EPSU BATTERY EMER R ON CIDS DISPLAY. ALL WORK PERFORMED IN REFER TSDR AALA202510301205Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 6. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR AALA202510144984Shackle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT ATTACH FITTING (SHACKLES) FWD POSITION ON LH PYLON. MEASURES ARE L=0.520 INCH, W=0.37 INCH AND D=0.012 INCH. MAINTENANCE REPLACED SHACKLE ATTACH FITTING ASSY IAW JC D5463008400000.
Back to Airbus A320-232