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 YENA2022101001008Unknown · odorFLT#349, BOS-SAV. ' STRONG OIL FUME SMELL LEVEL 3 THROUGHOUT ENTIRE A/C ON DESCENT. COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. DECON TAMAINUTION LEVEL A WAS ACCOMPLISHED PER TSM TASK 21-00-00-615-802A THIS CLEARS MDDR 487800 MX4 UPDATED PSDR GTIA2022101036716Megaphone · inoperativeMEGAPHONE INOP-R + R MEGAPHONE IAW AMM 25-63-00. OPS CHECK GOODSDR YENA2022101401020None · noneFLT#1584, MCO-JFK. 'UNCOMMANDED REDUCTION IN THURST AT 9500 IN CLIMB FROM 1.3 TO 1.2 EPR IN ENGINE #1 FOR APPROX 25SEC CAUSING SIGNIFICANT YAWING MOTION AT THE SAME TIME FUEL IN THE CENTER WENT TO 0 AND GOT A CTR TANK 1 PUMP 1 FAULT; #1 ENG REMOVED AND REPLACESDR GTIA2022101036713None · noneR1 DOOR ASSIST BOTTLE REQUIRES NITROGEN SERVICING.-SERVICED R1 DOOR DAMPER IAW AMM 52-10-00. NO LEAKS NOTED.SDR CALA2022101002752Beam · corrodedCORROSION FOUND ON RH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818030010 PERFORMED REMOVAL OF CORROSION PER SRM 51074-00 REV 142. REWORK CATEGORY "A" PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5 REV 142 DIMENSIONS: L=24.SDR CALA2022101002753Seat Track · corrodedCABIN SEAT TRACK -Y765 FR20 CORRODED.SDR CALA2022101002751Beam · corrodedCORROSION FOUND ON LH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818070010. PERFORMED REMOVAL OF CORROSION PER SRM 51-74-00 REV 142. REWORK THICKNESS (1.6MM). PERFORMED PERMANENT REPAIR CATEGORY "A" PER DIMENSIONS.REWORK ISDR CALA2022101002750Slat · puncturedLH SLAT #3 I/B SIDE TRAILING EDGE CHAFFING ON WING TOP, FURTHER EVALUATION REQUIRED, LTPR NR# 5001181948-0010. ACCOMPLISHED REPAIR ON PUNCTURED DAMAGE TO #3 SLAT IB SIDE OF RIB #7 IAW SRM 57-44-21-300-001. THIS IS A CAT "A" PERMANENT RPR. BY LHT TECH 5H0885 &SDR CALA2022101002744Frame · crackedLEFT FR 35 STR 30 HOLE 1,2,3, HAS A OUT OF ROUND INDICATION IN THE FR LAYER INTERIOR FACE AT 3-7 O''CLOCK AND AFT SKIN LAYER FWD SKIN LAYER AS VIEWED FROM EXTERIOR ADDITIONALY HOLE FOUND AT L/H FR35 STR28 FOUND CRACKED PER HAECO LCQ N/R 9290148/30148/9290149 SDR CALA2022100702742Eiu · inoperativeENG 1 FUEL VALVE FAULT ON CLIMBOUT UPDATED PICTURES UNABLE TO POWER UP FADEC 1 ON CHANNEL A OR B ALSO LOWER ECAM SWAPPED ENGINE EIU AND #1 ENGINE PARAMETERS WENT TO NORMAL AND ENGINE PAGE SHOWING BOTH A AND B IGNITION ON WITH ENGINE MASTER ABLE TO ACCESS #1 ESDR YENA2022100601005None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE UPPER CORNER WEB JOINT AFT FACE BETWEEN UPPER FASTENER AND STRINGER 8 RADIUS, CRACK LENGTH IS 0.2 50 INCH APPROX AT AFT GALLEY AREA (1 E/A); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00014 ) RESDR YENA2022100601004None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF AEROMAN WO 2022 181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITY FISDR YENA2022100601003None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2O22 181/1 NR 2022-481928, REMOVED AND REPLACE CONTINUITYSDR YENA2022100601002None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16RH SIDE IN OPEN FASTENER HOLE 2 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS AREA 6 AND 8 O CLOCK AT FWD GALLEY AREA (2EA); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00019 ) REF TO AEROMAN WO 2022 181/1 SDR YENA2022100601001None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 8 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481996, REMOVED AND REPLACED INTERCOSTSDR YENA2022100601000None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 2 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2, 5, 8, AND 11 OCLOCK AT THE FWD GALLEY AREA (4 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481998, REMOVED AND REPLACESDR YENA2022100600999None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 1 AND 4 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2020 181/1 NR 2022-481999, REMOVED AND REPLACED INTERCOSTSDR YENA2022100600998None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2022-181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITYSDR CALA2022100702736Fitting · crackedRIGHT FR35, STGR 30, HOLE #2 HAS A CRACK INDICATIONS IN THE FRAM E LAYER 7 O''CLOCK POSITION, AFT SKIN LAYER 6 O''CLOCK POSITION, A ND FWD SKIN LAYER O''CLOCK POSITION, AS VIEWED FROM EXTERIOR GENE RATED BY V061671 AT HAECO LCQ PER NR 9290145 (30145) O''CLOCK SDR CALA2022100702734Frame · corrodedAFT CARGO RH SIDE AT FR57 STGR37 HAS CORROSION PER HAECO LCQ N/R 9290712/30712 GEN BY V935513 REMOVED AND REPLACED STRINGER 37 RT FRAME 57 IAW A320 SRM 51-72- 11 AND EC/RA 5341-01340 NO REINSPECT REQUIRED BY MECH V052030 IN SP BY V935513SDR CALA2022100702733Stringer · corrodedA3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.SDR CALA2022100602729Limiter · warning messageRUD TRVL LIMITER CAUTNIFLIGHT. RAN ECAM. DIDNOT RESOLVE. RUDDER A CTED NORMAL ON LNDING FLT CREW REPORTED ''RUD TRV LIM SYS'' FAULT. CYCLED FAC1&2 TWICE, NO HELP. LOCKED FOR POSITIVE FIX. PILOT DECLARED AND EMERGENCY COMING . INTO SFO. CANNOT JUST TEST AND SSDR CALA2022100602724Spring Assy · missingPDA 3 NLG TOWING BOX LEVER HAS BOTH SPRING CLIPS MISSING -- SEE PHOTO PHOTO ADDED INSTALLED BOTH NEW SPRING CLIPS ON NLG TOWING BOX LEVER .. REF IPC 32-51-12-01ESDR CALA2022100602723Stringer · corrodedA3NB-53-4-6179 BULK CARGOSTRINGER 43L BET FR64-65 IS CORRODED() REPAIRED STRINGER 43L BETWEEN FR64 TO FR65 IAW A320 SRM 53-41-13 -300-004. EMP#V934585 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP ACE OF MOBILE AT BFM ON NR# 38656.SDR CALA2022100602709Frame · corrodedCORROSION FRAME 20 AT LEVEL STR23R IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-359976 REPLACED FR 20 LOC BTW STR 5 TO STR 31 RH SIDE IAW EA #53-0389-22 COVER REV 0 AND EC/RA #5311-02889 THIS REPAIR IS CATEGORY A, ADDITIONAL INSPECTION IS NOT REQUIRED PERFOSDR YENA2022100600990None · noneFLT#80, RNO-JFK. 'AT TOP OF DESCENT / IN DESCENT AT FL270 TO 10,000 FT HP VALVES OPEN WE HAD FUMES / DIRTY SOCK / OILY SMELL. WHEN HP CLOSED IT SEEMED TO DISSIPATE; REF TSM TASK 05-50-00-810-831-A AND 71-00-00-810-801-A, T/S CABIN ODOR TO APU AND ENG 2. ACCOMPSDR GTIA2022100636705None · noneFUME EVET AT FL 380 SUSPECTED ON PAACK 1. ISOLATED AND FUMES DISPERSED, UPON DESCENT PACK #1 WAS TESTED AGAIN AND FUMES RETURNED. ISOLATED AGAIN WITH NO FURTHER FUMES. ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCEDSDR GTIA2022100636704None · damagedRUDDER HINGE FITTING #3 REQUIRE REPLACEMENT DUE TO ELONGATED BUSHINGS IN PREVIOUS REPAIRS. RAF-01 2907255-01-ACCOMLPISHED VERTICLE STAB ATTACH FITTING HINGE ARM BR 3 REPLACEMENT IN ACCORDANCE WITH EA # 55-0488-22, REVISION # O. REPAIR CATEGORY "A", REPAIR CLASDR GTIA2022100636703None · damagedRUDDER HINGE ARM BEARING #4 HAS ELONGATED HOLE IN EXISTINE REPAIR. RAF-01 2907254-02 GENERATED-ACCOMPLISHED VERTICAL STAB ATTACHMENT FITTINGS HINGE ARM BR4 EXISTING BUSHING REPAIRS AND ENLONGATED HOLES REPAIR IN ACCORDANCE WITH EA # 55-0489-22 REVISION # 0 RESDR CALA2022100602703Skin · noneADDITIONAL DATA IS NEEDED TO EVALUATED ON EXISTING DOUBLER AS PER ECRA 5330-06364 (LP 6802117). SEE AEROMAN 2022-359933. ARE L=1.372IN W=1328IN, USED MATERIAL IN REPAIR DOUBLER IS CLAD INTERVALS TBD INSPECTION METHOD TBD ASPER SRI 53-11-11-205-051, 2024T3-0.0SDR CALA2022100602702Frame · crackedCRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPPSDR CALA2022100602700Floorbeam · corrodedCORROSION FLOOR BEAM +Y765 LOC BTW FR66 TO FR70 AT AFT GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359946. REPLACED FLOOR BEAM STRUCTURE Y+765 LOCATED FR66 TO FR70 IAW NTM 51-90-00. PERFORMED SCEPTRE AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND ENTRY ON LOGPAGE SDR CALA2022100602699Floorbeam · corrodedCORROSION FLOORBEAM Y-189 LOC.BTW F20 TO TR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359893. REPLACED FOORBEAM -Y189 LOC BTW FR20 TO FR24 AT FWD GALLEY AREA OF CORROSION ARE L=2.360 IN W=0.878 IN D=0.010 IN TOOL USED I.A.W SRM A320 51-72-11-911-001 ASDR CALA2022100602698Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359890. REMOVED AND REPLACED SEAT TRACK-Y1292 LOC. BTW FR12 TO FR24 AT DITIONAL DAMAGE I.A.W. NTM 51-90-00. PERFORMED SCEPTRE ENTRY INE 2022-359890. FWD GALLEY ASDR CALA2022100602697Stop Fitting · crackedWHILE WORKING EA 5340-01724 REV C OP002, STEP 3.1 NDT NOTED A CRACK INDICATION IN DOOR STOP FITTING 1 BOTTOM IB HOLE AT 4:00 POS ITION FACING AFT. FRAME 68 LH REPAIRED LWR I/B HOLE AT L/H FR68 DOOR STOP FITTING #1 IAW SRM 5 3-41-12-300-010. AND INSTALLED DOOR SDR CALA2022100602696Fitting · crackedLH FRAME FOOT AT FR43 CRACKED IN OUTBOARD POSITION 3:00 FACING A FT. REPAIR BEFORE NEXT FLIGHT.SDR YENA2022100600994None · noneFLT#904, SJU-JFK. (AIRCRAFT DECLARED AN EMERGENCY) 'MANUAL GEAR EXTENSION SMOOTH LANDING; MLG GEAR HANDLE RETRACTION STOWED IAW AMM 32-33-00. REQUIRES OPERATIONAL CHECK OF FREE FALL MANUAL EXTENSION REF LP 3437186-2 (PERFORMED OPS CHECK OF FREE FALL MECHANICALSDR YENA2022100600992Hinge Arm · vibrationFLT#39, FLL-SJO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'STRONG AIRCRAFT VIBRATION IN FLIGHT. OVERWEIGHT LANDING PERFORMED 1500,000 <200 FPM.' ACCOMPLISHED FLIGHT CONTROLS REPLACEMENT OF LH AND RH ELEVATOR ATTACH HARDWARE AND FITTINGS I.A.W EC NO. A5515SDR YENA2022100600989None · noneFLT#379, DCA-FLL. 'AFT FA REPORTED DIRTY SOCK SMEL DURING FINAL DESCENT. LEFT AND RIGHT FAN COWLS OPENED FOR MAINTENANCE; AIRCRAFT IS OK FOR SERVICE. ECS DECONTAMINATION LEVEL A (1) ACCOMPLISHED MITH ENGINES. NO ODOR IS PRESENT. COMPLIED WITH INFORMATION NOTICSDR CALA2022100602694Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 LOC BTW FR68 TO FR69 AT AFT GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359948. REPLACED FLOOR STRUCTURE LOCATED FR68 TO FR69 -Y1292 SCEPTRE ENTRY ON LOGPAGE NUMBER IS: 9185702. MEASURES AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DRASDR CALA2022100602693Frame · crackedCRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTE NER HOLE BTW STGR21 AND STGR22, CRACK DIRECTIONS ARE 3 AND 9 OCL OCK IN PASSENGER CABIN (1 EA). SEE AEROMAN NON-ROUTINE 2022-393 695. REPLACED FRAME FOOT COUPLING LOCATED ON FR43 LH SIDE IAW EA SDR CALA2022100602691Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4SDR CALA2022100602692Stiffener · crackedCRACK INDICATION FOUND ON VERTICAL STIFFENER OF THE LATERAL WINDOW FRAME 4 RIGHT SIDE LENGTH APPROXIMATELY =0.278 INCHES SEE AEROMAN NON ROUTINE 2022-393434. INDICATION NOT FOUND IAW NTM 51-10-08. THIS REPAIR IS CATEGORY A AND RE-INSPECTION ARE NOT REQUIRED PESDR CALA2022100602690Floor Panel · corrodedCORROSION FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-00SDR CALA2022100602689Floorbeam · corrodedCORROSION FLOOR BEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001SDR CALA2022100602688Floorbeam · elongatedELONGATED HOLE FLOOR BEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-393859 REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER IS:9289332 MEASURE OF IAW SRM A320 51-72-11-911SDR CALA2022100602687Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV ASDR CALA2022100302650Flange · crackedCRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPPSDR CALA2022100302649Doubler · damagedTHIS REPAIR IS CATERGORY B INSPECTION THRESHOLD FROM EXCEEDING 37,500FC OR 80,000FH WICHEVER OCCURS FIRST INSTALLED TIME OF ADL FC 60,000; FH 120,000 SUBSEQUENT INSPECTION AT DOT IAW GMM 06-35-05. EVALUATED EXISTING REPAIR ON EXTERNAL SKIN FUSELAGE LH SIDE LOCSDR CALA2022100302648Fastener · missingPDA 3 MISSING FWD PANEL FASTENER WAS REPLACED AS REQ REPLACED MISSING FASTENER ON PANEL 191AT , NOTE TOMC NOTIFIED
Back to Airbus A320-232