Airbus A320-232
Service difficulty reports · 32,653
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 YENA2021042300264Flap System · warning messageFLT 2894, MIA-EWR. F/CTL FLAPS LOCKED - WING TIP BRK ON ECAM CAME ON WHEN CONFIGURING TO LAND. IN SELECTING FLAPS 2 THE FLAP HANDLE OVERSHOT 1/1 WAY TO FLAPS 3. IN RETURNING THE HANDLE TO THE FLAPS 2 POSITION WE POTENTIALLY TRIGGERED THE ECAM ; PERFORMED BITE SDR YENA2021042700285Unknown · odorFLT 993, JFK-MIA. DIRTY SOCK SMELL IN DECENT INTO MIA. PASSING 11'000 ONCE ENTERED HUMID/HAZE LAYER DISSAPATED ONCE ON GROUND. NO CONFIGURATION /PACK /OTHER CHANGES ATTEMPED BY FLIGHT CREW TO MITIGATE/ REMOVE. NO PHYSIOGICAL ISSUES REPORTED BY INFLIGHT. CUSTOMSDR AALA202104239006Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA DUMMY RAIL LOCATED AT FR 16 AND Y503.2. REPLACED DUMMY RAIL PER SRM 51-72-11-911-001 AND DWG D53112826.SDR YENA2021042300265Smoke Detector · no testFLT 992, TPA-BOS. ECAM SMOKE DET FAULT ; R&R AFT BULK CARGO SMOKE DECTOR 6HW. FAULT REMOVED OPS CHECK GOOD REF TSM 26-17-00-810-801A AND AMM 26-16-00.SDR YENA2021042600277Lock Pin · damagedDURING HEAVY MAINTENANCE, PUSHED OFF WING ESCAPE SLIDE BALL LOCKPIN ASSY 194AT RH WING. R & R OFF WING ESCAPE SLIDE ASSY 194 AT IAW AMM 25-62-42-000-A, AND AMM 25-62-42-400-001-A. OPS TEST OK. OPENSDR YENA2021042600276Slide · out of positionDURING HEAVY MAINTENANCE, SLIDE RAFT ON DOOR 842 TOUCHES FUSELAGE REF AMM 25-62-44-400-803-A. PROCEDURE 4.B 12(B). REQUIRES REPLACMENT; (REF AEROMAN WO 2021-83/1, NR 2021-152197) R & R ESCAPE SLIDE RAFT AT PASSENGER CREW 842 IAW AMM 25-62-44-000-804-A AND 25-6SDR YENA2021042600275Slide · out of positionDURING HEAVY MAINTENANCE, SLIDE RAFT ON DOOR 831 TOUCHES FUSELAGE REF AMM 25-62-44-400-007-A, PROCEDURE 4.B, 12 (B). REQUIRES REPLACEMENT; (REF AEROMAN WO 2021-83/1, NR 2021-152199) R & R ESCAPE SLIDE RFT AT PASSENGER CREW 831 IAW AMM 25-62-44-000-012-A AND 25SDR YENA2021042600273Battery · failedDURING HEAVY MAINTENANCE, INOP EPSU 11WL BATTERY LH AT AFT GALLEY AREA (1EA); (REF AEROMAN WO 2021-83/1, NR 2021-152457) R & R BATTERY EPSU FIN (11WL) IAW AMM 33-51-38-400-002-A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK.SDR YENA2021042600272Battery · failedDURING HEAVY MAINTENANCE, INOP EPSU 10WL BATTERY AT LH FWD GALLEY AREA 1 (EA); (REF AEROMAN WO 2021-83/1, NR 2021-152456) R & R BATTERY EPSU FIN (10WL) IAW AMM 33-51-38-400-002-A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK.SDR YENA2021042600271Battery · failedDURING HEAVY MAINTENANCE, INOP EPSU BATTERY FIN 13WL AT PASSENGER CABIN; (REF AEROMAN WO 2021-83/1, NR 2021-152451) R & R BATTERY EPSU FIN (13WL) IAW AMM 33-51-38-400-002-A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK.SDR YENA2021042600270Battery · failedDURING HEAVY MAINTENANCE, INOP EPSU BATTERY FIN 12WL AT PASSENGER CABIN; R & R BATTERY EPSU FIN (12WL) IAW AMM 33-51-38-400-002-A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A. TEST IS OK.SDR YENA2021042300263Cabin Air Sys · odorFLT 928, MCO-SJU. DIRTY SOCK SMELL AFT CABIN APPROX PASSING 10000 FT ON DESCENT ; COMPLIED WITH INFO NOTICE 2017-T015F SEC. B APU PLACED ON MEL 36-12-02A, MX4 UPDATED, PLACARD INSTALLED. MCC NOTIFIED. AICRAFT OK FOR SERVICE. APU BLEED/LOAD CONTROL VALVE SECURESDR GTIA2021042235694Megaphone · destroyedFWD MEGAPHONE FELL APART-REPLACED FWD MEGAPHONE WITH SERVICABLE UNIT PER AMM 25-63-00SDR CALA2021042200519Motor · failedB ELEC PUMP LO PR DISPLAYED ON UPPER ECAM SCREEN. - HYD HYD B ELEC PUMP LO PRECAMACCOMPLISHED ECAMAND CHKLIST UPON ARIVAL NOTED BLUE SYSTEM HYD RESERVIOR QTY IS NORMAL, BLUE HELP. C.B DID NOT POP AGAIN, LIGHT ON SWITCH IS DEAD. SYSTEM HYDRAULIC PUMP C.B IS OUTSDR GTIA2021041935693Bottle · low pressureBOTH AFT L2 & R2 DOOR ASSIST BTL LOW-SERVICED BOTH L2 & R2 DOOR ASSIST BTL IAW AMM 52-10-00 TO LEAK NOTED AT THIS TIME.SDR GTIA2021041935692Bottle · low pressureFWD L1 DOOR ASSIST BTL LOW -SERVICED L1 DOOR ASSIST BTL IAW AMM 52-10-00 NO LEAK NOTED AT THIS TIME.SDR CALA2021041900502Stringer · corrodedSTRINGER 42L CORROSION BETWEEN FR63 - FR64. BLENDED OUT CORROSION FROM STRINGER 42L BETWEEN FR63 AND FR64. REMAINING THICKNESS AT GREATEST BLENDOUT MEASURES .049 THICK. REMAINING THICKNESS 049" PER NTM 51-10-04 PART 4 VERIFIED MATERIAL TO BE USED FOR REPAIR ASSDR CALA2021041900501Skin · corrodedSKIN CORROSION AT FR65-FR66 BETWEEN STR39R TO STR40R PER AVO ESC210415-4294-1 COMPLIED WITH STEP 6 DETAILED US INSPECTION AND MAPPING OR REWORKED AREA. LP OPEN MORE DETAILS AWAITED.SDR CALA2021041900500Stringer · corrodedSTRINGER 41 CORRODED FROM FR 57 TO FR 64. LOCATION IS AIRCRAFT RIGHT. REMOVED CORRODED STRINGER 41R FROM FR57 TO FR64. VERIFIED REPLACEMENT PART AS D5347047120200 PO# 7123438305 M&E 18-5300-3-0007 REF SRM 53-41-13-07B FIG007 ITEM90. LP OPEN MORE DETAILS AWAITESDR CALA2021041900499Stringer · corrodedSTRINGER 38 CORRODED FROM FR 60 TO FR 61. REMOVED INTERCOSTAL FROM FR60-61 ABOVE STR38R IN REF TO SRM 51-40-02 REMOVED TRANSITION PANEL ABOVE STR38R FR60-62 BLENDED OUT CORROSION ON STRINGER 38R FROM FR60 TO FR61. REMAINING THICKNESS AT GREATEST BLENDOUT MEASUSDR AALA202104301155Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORRODED AREA, MEASURING 1.5 BY 1.5 BY 0.065 INCH, ON FLOOR BEAM AT FR16, Z-500, AND Y1292. REMOVED AND REPLACED FLOOR BEAM REF SRM 51-72-11 AND SRM 51-42-11.SDR AALA202104308612Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: FOUND CORRODED AREA MEASURING 1.5 INCH DIAMETER BY 0.058 INCH DEEP ON FLOOR BEAM AT STR 23L, -Z500 AND Y765. REMOVED AND REPLACED FLOOR BEAM REF SRM 51-72-11 AND SRM 51-42-11.SDR AALA202104199010Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 252MF DELAMINATED. REPLACED FLOOR PANEL PER 53-02-00-300-011 AND IRM 9701.SDR AALA202104199007Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241AF DELAMINATED. REPLACED FLOOR PANEL PER 53-02-00-300-011 AND IRM 9701 REV K.SDR AALA202104269025Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN AREA SILL PLATE LOCATED AT FR68 Y1175 Z-500. REPAIRED PER SRM 53-41-14-300-001. **SUPPLEMENTAL REPORT TO CORRECT SECTION 7 CORROSION LEVEL TO REFLECT "2".SDR YENA2021042700284Ecs · contaminatedFLT 512, AUS-FLL. STRONG DIRTY SOCK ODOR FROM PACKS WHEN ON APU BLEED OR ENGINE BLEED. *REPEAT WRITE UP. (4-10-21); INSP APU COMP & FOUND MINOR OIL SATURATION AT INLET SEAL AND PLENUM SEAL. CLEANED APU COMP PER 49-00-00. INSP ENG 1 & 2 AND FOUND NO LEAKS. INSPSDR AALA202104269026Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN AREA SILL PLATE LOCATED AT FR68 Y-1295 Z-500. REPAIRED PER SRM 53-41-14-300-001.SDR GTIA2021041935689Bottle · low pressureL1 DOOR ASSIST ACCUMULATOR LOW-SERVICED L1 DOOR ASSIST ACCUMULATOR TO PROPER PRESSURE IAW AMM 52-10-00SDR CALA2021041900491Stop Fitting · crackedDOOR STOP FITTING NO1 FR16L LOWER INBOARD FASTENER HOLE EXHIBITS CRACK BETWEEN THE INTERCOSTAL AND FRAME. (REF AAR NON-ROUTINE 9479245) REF N/R AAR- 9479245 REWORKED DOOR STOP #1 AT FR16L LOWER I/B FASTENER HOLE AS PER EC/RA 5311-02546. PART-1 INTERIM REPAIR SDR GTIA2021041935688Bottle · low pressureDURING WEEKLY R1 DOOR ASSIST BOTTLE FOUND LOW.-SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.SDR CALA2021041600486Skin · corrodedBELLY SKIN AT STRINGER 40R BETWEEN FR56 AND FR64 IS BULGING/DIMPLING AT FASTENER HEADS DUE TO CORROSION FROM MATING SURFACES OF INTERNALLY CORRODED AREAS. PHOTO IS ATTACHED TO ADD VISUAL CONTEXT. NO EVIDENCE THAT THE BELLY SKIN IS CORRODED. ALL OTHER FASTENER SDR YENA2021042000250Light · unsecureFLT 129, SDQ-BOS. EMERGENCY EXIT SIGN AT READ OF CABIN OVER AISLE IS BURNED OUT; RESECURED EMERGENCY EXIT LIGHT OPS CHECK OK PER AMM 33-51-17 A/C OK FOR SERVICE MCC NOTIFIEDSDR YENA2021042000249Light · inoperativeFLT 830, SDQ-BOS. INFLIGHT REPORTED THAT AFTER SECOND L/G EXTENSION, THE ""EXIT"" SIGNS AT FWD DOORS DID NOT ILLUMINATE; PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHTING SYSTEM PER AMM 33--51-00. OPS CK NORMAL.SDR AALA202104169010Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATION FOUND ON FLOOR PANEL 231VF LOCATED AT STA FR32, BUTT LINE Y254. REPLACED FLOOR PANEL 231VF LOCATED AT STA FR32, BUTT LINE Y254.SDR AALA202104169012Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 232LF DELAMINATED. REPLACED FLOOR PANEL PER 53-02-00-300-011 AND IRM 9701 REV K.SDR YENA2021041600236Safety Valve · failedFLT# 830, SDQ-BOS. AFTER EXTENDING THE LANDING GEAR L/G GEAR NOT DOWNLOCKED ECAM OCCURRED RAN QRH AND HAD A NORMAL EXTENSION ; TROUBLSHOT IAW TSM 32-31-00-810-859A, R/R NLG OPENING SAFETY VALVE 2630GM IAW AMM 32-31-19, OPS CHECK OK, LEAK CHECK OK.SDR CALA2021041600475Waste Tank · leakingLAV WASTE WATER LEAKED AT FR46.5 TO FR65 FROM STR LH-42 TO STR RH-38 & AT FR65 TO FR67 FROM STR44 TO STR RH35. PERFORMED EC/RA# 2011-01000 LAVATORY SPILL STEPS 1. THROUGH 2.B.(13). LARGE SPILL DETECTED 4/7/21 ON BELLY SKIN FR56-64 AT STRINGER 40R. AREA BEING CSDR CALA2021041600474Door Frame · crackedL/H AFT EMERG. EXIT DOOR (Z834) Z ANGLE BETWEEN LOAD TRANSMITTER AND EDGE BEAM CRACKED. REF TO PEMCO NR 10670.0168 REMOVED AND REPLACED L/H AFT EMERG DOOR Z-ANGLE IAW A320 SRM 51- 42-11 AND A320 SRM 51-44-11. ALODINED, PRIMED AND TOPLOCATED REP AIR AREA IAW A3SDR CALA2021041600473Profile · crackedL/H AFT EMERG. EXIT DOOR (Z834) L/H LOAD TRANSMITTER CRACKED. REF TO PEMCO NR 10670.0167 REMOVED AND REPLACED L/H AFT EMER, DOOR LOAD TRANSMITTER (SEGMEN T) IAW A320 SRM 51-42-11 AND 51-44-11. ALODINED, PRIMED AND TOPL OCATED REPAIR AREA IAW A320 SRM 51-21-11 SDR YENA2021041600235Battery · failed inspFLT# 6101, FLL-MZJ.EPSU BATTERY FAILED EMERGENCY LIGHT TEST ; R/R EMERGENCY LIGHT BATTERY IAW AMM 33-51-38 OPS GOOD.SDR YENA2021041600234Battery · failed inspFLT# 6101, FLL-MZJ. EPSU BATTERIS 10WL FAILED EMERGENCY LIGHT TEST ; EPSU BATTERIS 10WL FAILED EMERGENCY LIGHT TEST.SDR CALA2021041400467Structure · crackedL/H AFT EMERG. EXIT DOOR (Z834) L/H LOAD TRANSMITTER CRACKED. REMOVED AND REPLACED L/H AFT EMER, DOOR LOAD TRANSMITTER (SEGMEN T) IAW A320 SRM 51-42-11 AND 51-44-11. ALODINED, PRIMED AND TOPL OCATED REPAIR AREA IAW A320 SRM 51-21-11 AND SRM 51-23-11 AND AI RSDR YENA2021042000248Slide · deformedDURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT ON FUSELAGE WHEN THE DOOR IS FULLY OPENED AND L OCKED DUE TO SWELLING AT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA ( 1 EA); R & R NEW ESCAPE SLIDE DOOR 841 IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803SDR GTIA2021041535685Bottle · low pressureL1 DOOR ASISST BOTTLE REQ SVC-SVCD LI DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR CALA2021041400463Angle · crackedL/H AFT EMERG. EXIT DOOR (Z834) Z ANGLE BETWEEN LOAD TRANSMITTER AND EDGE BEAM CRACKED. REF TO PEMCO NR 10670.0168 REMOVED AND REPLACED L/H AFT EMERG DOOR Z-ANGLE IAW A320 SRM 51- 42-11 AND A320 SRM 51-44-11. ALODINED, PRIMED AND TOPLOCATED REP AIR AREA IAW A3SDR YENA2021042000252Light · malfunctionedFLT 227, SJU-MCO. EMERGENCY EXIT LIGHTS STAY ON IN FLIGHT IN ARM. TRIED RESETING BUT DID NOT HELP; T/S SYST PER TSM 33-51-00-810-881 R & R (8WL) RELAY NO HELP. R & R (4WL) TOGGLE SWITCH OPS CKD NORMAL OK FOR SERVICE PER ESPM 20-45-21SDR YENA2021042000251Cabin Air Sys · odorFLT 1969, BOS-FLL. CABIN ODOR EVENT DURNING CLIMBOUT AND DESCENT, APU WAS OFF; PERFORMED LEVEL ""B"" DECONTAMINATION OF THE ECS IAW AMM 21-00-00-615-803-A. PACK BURN SUCCESFUL NO ODOR NOTED FROM ENGINES DURING RUN. ONLY WITH APU BLEED. SMELL STRONG THRU ECS. PSDR GTIA2021041535684Idg · faultedIN CLIMB HERD A CLICK SIMILAR TO AUTO PILOT DISENGAGEMENT EVEN THOUGH AP WAS ALREADY ENGAGED. IN CRUISE VARIOUS CLICKS HERD IN CB PANEL BEHIND FO SEAT. AP 2 DISENGAGED UNCOMANDED SHORTLY THERE AFTER. FOLLOWED BY ECAM GEN 2 FAULT. PERFORMED ECAM ACTIONS RESET GSDR GTIA2021041535683Apu Bay · odorFUME EVENT ON APPROACH TURNED OFF PACK 1 AND SMELL WENT AWAY ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )-PERFORMED INSPECTION OF THE APU #1 ANSDR CALA2021041400448Frame · crackedFLIGHT DECK, RH FR 4 UPPER ATTACHMENT, HOLE IN VERTICAL FRAME HAS CRACKE INDIATION AT ATTCHMENT, HOLE IN VERTICAL PRAME HAS CRAC K INDICATION AT JUNCTION OF VER. FRAME AND CORNER FITTINGS, CRAC AIMING PER LCQ 9298605/24605. REPAIRED FLT DECK RH FR4 UPPER ATT
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