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 CALA2025011300088Seat Track · corrodedMAIN CABIN SEAT TRACK Y765 FR 24-35 CORROSION OUT OF LIMITS. REMOVED AND REPLACED +Y765 FR24-35 SEAT TRACK IAW A320 SRM 57-72 -12-911-001.SDR CALA2025011001864Elec Connector · damagedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - SEAT MOUNTED EMERGENCY LIGHT AT 22C AND 28C INOP. AT SEATS 22C & 28C, REPLACED DAMAGED PINS & SOCKETS ON LIGHT ASSY CONNECTORS IAW SWPM 20-42-01. EMERGENCY SEAT TRACK LIGHTING OPS CK'D NORMAL.SDR CALA2025011001852Battery · dischargedCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - TEST FAIL SHOWED FWD LH EPSU BATTERY. REPLACED EPSU BATTERY REF AMM TASK 33-51-38-000-002-A AND TASK 33-51-38-400-002-A. ACP EPSU BITE, BITE CHECKS OKAY. ACP CIDS POWER ON TEST, TESSDR CALA2025011300097Floor Support · corrodedFWD CABIN FLOOR STRUCTURE CORROSION AND BROKEN FASTENERS AT RH P ROFILE FWD OF R-1 DOOR FR 13 TO FR 16. REMOVED AND REPLACED FWD CABIN FLOOR ANGLE ASSY AT RH PROFILE FW D OF R-1 DOOR FR13 TO FR16 IAW SRM 57-42-11/001 PARA D.SDR CALA2025011300089Floorbeam · corrodedAFT CABIN FLOOR BEAM Y512.5 HAS CORROSION. REMOVED AND REPLACED AFT CABIN FLOOR BEAM Y512.5 IAW A320 SRM 51 -72-11-911-001.SDR CALA2025011300087Web · corrodedFWD CABIN CORROSION AT R/H WEB Y-1732 AT FR20 O/B OF R/H FLOOR BEAM Y-1584 I/B OF R-1 DOOR FRAME. REMOVED AND REPLACED RH WEB Y-1732 AR FR20 IAW A320 SRM 51-42-11 PAGE 18-21.SDR CALA2025011001853Fuel Cap · brokenHANDLE TO FUEL CP FOUND MISSING UPON ARRIVAL. REPORTS FUEL CAP BROKE FOUND FUEL CAP HANDLE MISSING. CREATED PDA, REMOVED AND REPLACED FUEL CAP REF 28-25-41-02B.SDR CALA2025011700133Skin · dentedR-2 DOOR EXTERNAL MID LOWER SURFACE HAS DENT (A3NB-52-4-6024) PE R HAECO LCQ NON ROUTINE 9292021/36021 ACCOMPLISHED DOUBLER & FILLER INSP AT 60,000 FC FROM RPR EMBODIMENT IAW SRI RPR IAW SRM 52-10-00-300-005. THIS IS A CAT B RPR & REQUIRES 52-10-00-205-011.WOSDR CALA2025011300096Floor Support · crackedLH FR 4 FLOOR SUPPORT ANGLE CRACKED. REMOVED AND REPLACED DISCREPANT FR4 L/H FLOOR SUPPORT ANGLE IAW A320 SRM 51-72-11-911-001.SDR CALA2025010800059Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS AT 29 IN FROM INBOARD, 14 IN FRO M TRAILING EDGE, 1 1/2 IN DIAMITER.SDR CALA2025010800058Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS AT 141 A/2 IN FROM INBOARD, 16 I N FROM TRAILING EDGE, A 1/2 IN DIAMITER.SDR CALA2025010800057Panel · dented#2 ENG O/B T/R SLEEVE AFT OUTER SKIN DENTED PER HAECO LCQ N/R 9292111/20111 GEN BY V061642 REMOVED AND REPLACED #2 ENGINE O/B T/R SLEEVE IAW A320 AMM 78-32 -46-000-010-A/400-010-A BY MECH V077079 INSP BY V892285 ROTABLE PARTS CHANGE WAS INDICATED - TT # 179303SDR CALA2025010701836Power Supply · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - CHECK OF EMERGENCY LIGHTS FAILS. PRODUCES FAULT- "EPSU BATTERY EMER L" R/R EPSU BATTERY AT EPSU 11WL REF AMM 33-51-38, OPS CHECKS OK. PARTS USED: 18-3351-3-0001, QTY :1SDR AALA202501071931Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: 2L FA JUMPSEAT FLASHLIGHT LED DOES NOT FLASH AND TAMPER SEAL ISBROKEN. REPLACED FLASHLIGHT BATTERY AND TAMPER SEAL 2L FA JUMPSEAT.SDR AALA202501073751Ground Wire · looseAIRCRAFT WAS NOT GROUNDED: FIRST CLASS SEAT AB EMERGENCY LIGHT INOP GROUND WIRE LOOSE. RE-TERMINATED LOOSE WIRE AT ROW 1 AB. OPS CHECK NORMAL. REF AWM33-51-06.SDR CALA2025010700055Floorbeam · gougedMAIN CABIN FLOOR BEAM -Y106.5 FRAME 70 HAS GOUGE ON HARD POINT.SDR CALA2025010700054Door Sill · corrodedR-2 DOOR SHAPE SILL UPPER SURFACE HAS CORROSION (3EA) SPOTS.SDR CALA2025010700049Intercostal · crackedR/H FR16 DOOR STOP 1 HOLE NUMBER 3 HAS A CRACK INDICATION AT THE 9 O''CLOCK POSITION IN THE INTERCOSTAL . REMOVED AND REPLACED INTERCOSTAL AT FR 16 DOOR STOP #2 IAW A320 AMM 52-11-31-400-002-A.SDR CALA2025010601799Wire Harness · damagedWHILE PERFORMING THE EMERGENCY LIGHT CHECK ON THE 2 SERVICE FOUND EMERGENCY EXIT LIGHTING ON ROW 22 ABC TO BE DAMAGED REF AMM 33-51-18 REPLACED WIRE HARNESS TO EMERGENCY EXIT LIGHT OPS CHECKS GOOD.SDR YENA2025010700026O-Ring · leakingFLT#1736, STI-JFK. (AIRCRAFT DECLARED AN EMERGENCY) 'DURING CRUISE FLIGHT " HYD Y RSVR LO LVL" ECAM + QRH PROCEDURES APPLIED; REF. L.P. ' S 4156052 ITEMS 1 (REPLACED EDP IAW AMM 29-13-51 LEAK CHECK REQUIRED REF LGP 4156054 ITEM 1 (LEAK CH'D # 2 HYD EDP, REF.SDR YENA2025010700024Ecs · contaminatedFLT#939, JFK-SJD. 'HEAVY DIRTY SOCK SMELL DURING DESCENT THROUGH 5000 FT AT 1000 FT DESCENDING SMELL WAS EVEN STRONGER ,WE OPEN COCKPIT WINDOW DURING TAXI IN. ( PACKS );COMPLIED WITH INFO NOTICE 2017-T015K AND TSM 05-50-00810-831-A. PERFORMED DECONTAMINATION SDR CALA2025010700056Floorbeam · corrodedFWD CABIN FLOOR STRUCTURE CORROSION AT L/H FLOOR BEAM Y 503.2 AT FR 16 ABOVE RUDDER AND THSA CABLES. RMVD+RPLCD DISPLACED Y503.2 FLOOR SUPPORT FR12-20 IAW A320 SRM 5 1-42-11-001 + 51-72-11-911-001.SDR CALA2025010701825Bleed Valve · faultedWING ANTI ICE SYS FAULTON DEPARTURE.FALULT LIGHT ILLUMINATEW EC AMCREW BRIEF OUT OF DEN STATES ICING CONDITIONS ON GRD/AIR.FAULT OCCURED AT CLIMB AND CRUISE DURING MULTIPLE POWER SETTINGS. CREW ALSO STATED FAULT WOULD OCCASIONALLY GO AWAY WITH RESET. NO BMC 1/SDR YENA2025010700023Unknown · odorFLT#2319, EWR-AUA. 'LEVEL 1 ODOR EVENT IN DESCENT. OIL SMELL STARTED AT 10,000 AND DISSIPATED AT 3,000. FLT CREW AND FWD FA SMELLED ODOR, AFT FA SMELLED NOTHING. COMPLETED ODOR RECOGNITION GUIDANCE CHECKLIST AND ODOR REPORTING FORM. APU OFF ( PACKS ).' (SUPPLESDR YENA2025010700022Unknown · odorFLT#1015, EWR-PUJ. 'THE INFLIGHT CREW NOTICED A "DIRTY SOCK" SMELL AT TOP OF DESCENT. THEY CALLED ON THE GROUND TO TELL US IT GOT VERY STRONG. APU WAS NOT RUNNING. ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2025010700021Unknown · odorFLT#803, JFK-SJU. ' ALL 4 FAS REPORTED FUMES OR DIRTY SOCK SMELL ON SHORT FINAL INTO RWY 10 FOR SJU. OUR POSITION WAS APPROX. 5.10 DME ON THE FINAL APP. COURSE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 CABIN HEMS & AMBIESDR CALA2025010600043Door Frame · crackedL/H FWD EMERGENCY EXIT HATCH HAS CRACKS ON FRAME AS MARKED. REMOVED AND REPLACED ANGLE SEGMENT AT LH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.SDR CALA2025010600042Door Frame · crackedL/H AFT EMERGENCY EXIT HATCH HAS CRACKS ON FRAME AS MARKED. GENE RATED BY V926223 ON HAECO LCQ NR 9296437/40437. REMOVED AND REPLACED SEGMENT AT LH AFT EMERGENCY EXIT DOOR IAW A 320 SRM 51-72-11-911-001. ACMP BY MECH V947030 INSP BY V077960SDR CALA2025010600041Web · crackedRT AFT EMERGENCY EXIT DOOR WEB CRACKED. REMOVED AND REPLACED ANGLE SEGMENT AT RH AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.SDR CALA2025010600044Web · crackedRT FWD EMERGENCY EXIT DOOR WEB CRACKED. REMOVED AND REPLACED ANGLE SEGMENT AT RH FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001.SDR CALA2025010601820Battery · no testRIGHT HAND OFF-WING ESCAPE SLIDE INSTALL {A3NB-25-3-6280} - DURING OPS CHECK OF EMERGENCY LIGHT CIDS DISPLAYED EPSU INT LOAD EMER L MSG. UPDATING ROTABLE PARTS CHANGE WAS INDICATED - TT # 1559479 SN OFF 8303 .POWER SUPPLY, P OFF 31-3350-9-9001 8303 ON 31-3350SDR CALA2025010601819Battery · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY EMER L 33-51-38 12WL FAILS BATTERY TEST. LOWER FLOOR PANEL REMOVED ROW 21A REMOVED AND REPLACEDEPSU BATTERY MERL, PER 33-51-11, TEST OK. PARTS USED: 18-3351-3-0001,QTY :1SDR YENA2025010600029Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN LOC.AFT VENT OUTLET BETWEEN FR69 TO FR70 AND S TR 30R TO 33R LOWER FUSELAGE; REF AEROMAN N/R 2024-652123, PERFORMED PERMANENT REPAIR LOC. EXTERNAL SKIN AFT VENT OUTLET BETWEEN FR69 TO FR70 AND STR 30R TO 33R LOSDR YENA2025010600028Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE H3 ON DOOR STOP 1 FR68RH. CRACK DIREC TION 6 OCLOCK AND DEPTH 0.100 INCH; REF AEROMAN N/R 2024-652650, PERFORMED PERMANENT REPAIR ON FR68 RH AT LOWER INB FASTENER HOLE OF DOOR STOP FITTING #1 IAW A320 SDR YENA2025010600027Placard · missingDURING HEAVY MAINTENANCE: REF VTASK CARD A1124092-01 E/F WASTE FLAP DOOR PLACARD INSTALLATION- SPACEFLEX LAVATORIES- A320M / A321HD; AEROMAN ACCOMPLISHED TC A1124092-01 W/O 1353055. MAJOR ALTERATION.SDR YENA2025010600026Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 31R LOC, BTW FR, 65 TO FR, 66 IN BULK CARGO COMPARTMENT (CPCP RELATED), (RESOLVED ON W/O: 1342223 TASKCARD: NR-00033) REF AEROMAN N/R 2024-652843, EVALUATED CORROSION LOCATED ON STRINGER 31R AT LEVEL FR65 AND NOT FOSDR YENA2025010600025Fitting · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING LH SIDE. CRACK LENGTH: 0. 200 INCHES APPROX; ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT AT AREAS A1 (LHS) AND D1 (RHS) IN ACCORDASDR YENA2025010600024Windshield · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON THE WINDSHIELD CENTRAL LOWER NODE, AROUND UP PER TENSION BOLT LH SIDE. CRACK DIRECTION: 1 OCLOCK, CRACK LENGTH: 0.1 50 INCHES APPROX; ACCOMPLISH THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMING CESDR YENA2025010600023Panel · elongatedDURING HEAVY MAINTENANCE: ELONGATED HOLE CUT OUT AREA FUEL TANK ACCESS PANEL BTW RIB 14 AND RIB 15 RH WING; (RESOLVED ON W/O: 1342223 TASKCARD: NR-00035) REF WO 2024 292/1 NR 2024-652732 PERFORMED PERMANENT REPAIR ON BOTTOM SKIN PANEL 2 LOCATED BTW RIB 14-RIB SDR YENA2025010600022Light · inoperativeDURING HEAVY MAINTENANCE: EMERGENCY LIGHT AT EPSU 12WL FAILED TEST; REF AEROMAN WO 2024 292/1 NR 2024-652950 REMOVED AND REPLACED EPSU AT 12WL IAW AMM 33-51-38-000-001 AND AMM 33-51-38-400-001-A. EMERGENCY LIGHT TEST GOOD IAW AMM 33-51-00-710-006-A.SDR YENA2025010600021Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ WINDSHIELD FRAME / CENTER POST / LOWER NODE AREA / CRACK DAMAGE - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9061-24 (COVER + PARTS 1-5) /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03) /3/ AIRBUS RSDR CALA2025010601791Pump · faultyAT 18000FT AT IDLE IN DESCENT ENGINE FLAMMED OUTUPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PILOT REPORTS IN DESCENT AT FL180 E2 FLAMED OUT, LOSS OF POWER. HE SAID IT WAS LIKE FUEL STARVATION AND FUEL FLOW WENT SDR CALA2025010601784Light · missingLEFT LANDING LIGHT MISSING ON ARRIVAL. REF LOG# 3413284 SEE LOG #3413284 FOR CORRECTIVE ACTION. LT LDG LIGHT MISSING WIRES EXPOSED, REPLACED LH LANDING LIGHT HOUSING REF AMM 33-42-11-400-003-A. OPS CHECK GOOD AT THIS TIME.SDR CALA2025010600031Floor Support · gougedFWD CABIN FLOOR SUPPORT -Y254 HAS GOUGE. REMOVED AND REPLACED -Y254 FLOOR SUPPORT IAW A320 SRM 51-72-11-911- 001.SDR CALA2025010600027Panel · crackedAFT CARGO FR 56-58 RSTR 38 PROFILE PANEL IS CRACKED. REMOVED & REPLACED AT AFT CARGO FR56-FR58 STR 38 PROFILE PNL IAW A320 SRM 51-42-11/001 - SRM 51-72-11-911-001.SDR CALA2025010600030Floor Support · corrodedFWD CABIN FLOOR SUPPORT Y765 HAS CORRISOION.SDR AALA202501029067Power Supply · inoperativeAIRCRAFT WAS NOT GROUNDED: ON PS CHECK FOUND EMERGENCY LIGHTS INOP AT ROWS 17 & 22 AS WELL AS AFT 2 EMERGENCY CEILING LIGHTS IN SUCCESSION. MAINTENANCE PERFORMED RELAMP OF ALL WITH NO HELP. THEN REPLACED AFT LH EPSU IAW AMM 33-51-38. OPS TEST SAT.SDR YENA2025010700025Unknown · odorFLT#405, EWR-FLL. 'F1 REPORTED MOMENTARY PATRID/DIRTY SOCK SMELL ON CLIMBOUT DID NOT RECURR. CABIN ODOR REPORTING FORM COMPLETED; COMPLIED WITH INFO-NOTICE 2017-T015K INSPECTED APU AND FOUND IN CLEAN CONDITION WITH NO LEAKS. INSP AFT FUSELAGE AND FOUND NO EVIDSDR CALA2025010301771Lanyard · out of positionDOOR 1L/INDICATOR ON FLO OR POSSIBLY NOT GETTING TO FULL ARM PO SITION. FOUND LANYARD MATERIAL OBSTRUCTING GIRT BART TRAVEL. STOWED LANYARD IN PLACE. CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES. ARMED AND DISARMED DOOR SEVERAL TIMES ALSO. DOOR INDICATION NORMALSDR CALA2025010301765Anti-Ice Valve · faultyWING A.ICE SYS FAULT HAS HISTORY PLEASE TROUBLESHOOT FALLOW TSM 30-11-00-810-803-A OPERATIONAL TEST OF WAY SYSTEM AMM 30-11-00-710-001 FAIL/PASS MULTIPLE TIME (INTERMITTENT CONDITION FAULT LIGHT ON WING A ICE PUSH BOTTOM WONT EXTINGUISH). TEMP CTL TEST PER AMM
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