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 YENA2023120501547Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SILL DOOR IN BULK CARGO COMPARTMENT; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00005 ) REF AEROMAN WO 2023 279/1 WCC 2023-590586 PERFORMED REPAIR LOWER SILL DOOR IN BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49-300-003 ANDSDR YENA2023120501546Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.68 AND STR. 8L INTERNAL STRUCTURE CRACK L ENGTH: 0.410 INCH APPROX; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00023 ) REF AEROMAN W/O 2023 279/1 WCC 2023-590638 PERFORMED REPAIR LOCATED ON FR 68 AND STGR 8 LHSDR YENA2023120501545Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHEM ENT INTERNAL AREA FROM UPPER TENSION BOLT LH SIDE, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGTH IS 0.135 INCH, IN COCKPIT (1 EA); ALL WORK ACCMPLISHED ON AE WO 2023-2SDR YENA2023120501544Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA FROM UPPER TENSION BOLT RH SIDE, CRACK DIRECTION IS 10 OCLOCK, CRACK LENGTH IS 0.105 INCH, IN COCKPIT (1 EA); ALL WORK ACCOMPLISHED ON AE WO # 2023SDR YENA2023120501543Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON CENTER WING BOX FR41 TO FR42 ON LH SID E IN PASSENGER CABIN; (RESOLVED ON W/O: 1264003 TASKCARD: NR-00028 ) ALL WORK ACCOMPLISHED ON AE WO # 2023 279/1 NR # 2023-590664 ACCOMPLISHED THE REPAIR OF THE CORRSDR YENA2023120501542Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOC RIB 7 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590805 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TSDR YENA2023120501541Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC.RIB 11 PLUS 3 INCHES TRAILING EDGE (OVERH ANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590791 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 ATSDR YENA2023120501540Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 11 PLUS 20 INCHES TRAILING EDGE (OVER HANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590792 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 ASDR YENA2023120501539Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 14 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590793 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND SDR YENA2023120501538Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 14 PLUS 16 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590795 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TSDR YENA2023120501537Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 15 PLUS 17 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590797 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TSDR YENA2023120501536Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 16 PLUS 20 INCHES TRAILING EDGE ON RH WING; REF AEROMAN WO 2023 279/11 WCC 2023-590799 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND SDR YENA2023120501535Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE LOC RIB 17 PLUS 16 INCHES TRAILING EGDE ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590801 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TSDR YENA2023120501534Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOC RIB 7 TRAILING EDGE (OVERHANG AREA) ON RH WING; REF AEROMAN WO 2023 279/1 WCC 2023-590805 ACCOMPLISHED REPAIR OF CORROSION AT RH WING TOP SKIN PANEL 2 BETWEEN WX3494-WX-4490 AND RIBS 9-18 AT REAR SPAR AND TSDR YENA2023120501533Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ELEVATOR TIP OUTBOARD RIB ON RH HORIZONTAL STABILIZER (CPCP RELATED REFER TO THE MPD TASK: 552006-01); (RESOLVED ON W/O: 1264003 TASKCARD: NR-00021 ) REF AEROMAN W/O 2023 279/1 WCC 2023-590516 REMOVED AND REPLACED TIP ELEVATSDR YENA2023120501532Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON CENTER WING BOX FR41 TO FR42 ON LH SID E IN PASSENGER CABIN; ALL WORK ACCOMPLISHED ON AE WO # 2023 279/1 NR # 2023-590664 ACCOMPLISHED THE REPAIR OF THE CORROSION FOUND AT THE CENTER WING BOX-LH TOP SKIN BSDR YENA2023120501531Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / LH TOP SKIN BTWN FR 41-42 AT BEAM Y1292. CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023120501530Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / REAR SPAR - TE OVERHANG / WX3494-WX4490 AND RIBS 9-18 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023120501529Window Frame · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST UPPER FASTENERS LH & RH AREA / CRACKS - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)SDR CALA2023120503554Seat Track · corroded96-76-A3NB-53-3-6356 AFT CABIN FLOOR SEAT TRACK Y765 HAS CORROSION FR 66. W/C:78394 AFT CABIN FLOOR SEAT TRACK Y765 FR66 OUT OF LIMITS IAW SRM 53-41 EMP:V936636 STA:STENGBFM -14-283-009 CORROSION AT EXCLUDED AREA, REMOVED SEAT TRACK IAW S RM 51-42-11, RECEIVEDSDR YENA2023120401521Unknown · unknownFLT#128, MCO-EWR. 'EPSU (EMERGENCY POWER SUPPLY UNIT) AT 11WL INOP; REMOVED AND REPLACED LH AFT EMERGENCY LIGHT AFT LAMP IAW AMM 33-51-15. OPS CHECK GOOD.'SDR GTIA2023120137662Megaphone · inoperativeL1 DOOR MEGAPHONE IS INOP-REMOVED + REPLACED FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD, MOC # 70318/119285SDR AALA202312010658Light · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT ON ROW 15 ABC INOP. REMOVED AND REPLACED EMERGENCY LIGHT ON ROW 15 ABCSDR AALA202312017237Door · lack of lubeAIRCRAFT WAS NOT GROUNDED: FWD LAV DOOR DIFFICULT TO OPEN. LUBED DOOR.SDR CALA2023120103515Battery · no testEPSU BATTERY (13WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0040. PERFORMED EPSU BATTERY REPLACEMENT (13WL) IAW AMM: SDR CALA2023120103513Battery · no testEPSU BATTERY (12WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT AS RECORDED ON LTPR NR#5001274773-0030. PERFORMED EPSU BATTERY REPLACEMENT (12WL) IAW AMM: 33-51-38-000- 002 / 33-51-38-400-00SDR CALA2023120103511Battery · no testEPSU BATTERY (11WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0020. PERFORMED EPSU BATTERY REPLACEMENT (11WL) IAW AMM: SDR CALA2023120103509Battery · no testEPSU BATTERY (10WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0010. PERFORMED EPSU BATTERY REPLACEMENT (10WL) IAW AMM: SDR CALA2023120503564Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 33 INC HES FROM IB EDGE AND 9 INCHES FROM AFT EDGE, 4.5 INCHES DIA. PER HAECO LCQ NON ROUTINE 9294369/26369 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 33 IN FROM I/B 9 IN FROM T/E 1.5 IN DIA 2EA ARSDR CALA2023120503562Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 70.25 INCHES FROM IB EDGE AND 10 INCHES FROM AFT EDGE, 1 INCH DIA. PER HAECO LCQ NON ROUTINE 9294370/26370 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 70.25 IN FROM VB 10 IN FROM T/E 1.5 IN DIA ZONSDR CALA2023120503550Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 79.5 I NCHES FROM IB EDGE AND 9.5 INCHES FROM AFT EDGE, 1.5 INCH DIA. P ER HAECO LCQ NON ROUTINE 9294371/26371 REPAIRED RH ELEVATOR UPPER SKIN 79.5 IN FROM I/B 9.5 IN FROM T/E 1.5 IN DIA ZONE 1 IAW A32SDR CALA2023120503560Skin · contaminatedRH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 21.5 I NCHES FROM IB EDGE AND 11 INCHES FROM AFT EDGE, 2.5 INCHES DIA. PER HAECO LCQ NON ROUTINE 9294368/26368 GENERATED BY V892444 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 21.5 IN FROM I/B 11 INSDR CALA2023120103506Relay · faultySIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL RESETTING SECS AND GRD SCAN CHECKS OK. TSM CALLS OUT TO CHANGE RELAYS 47CE1 AND 47CE2. SECOND HIT AND DOES HAVE SEC HISTORY. SEE TSM 27-92-00-810-830AH FLT WAS RTO. FO FLYING AND HAD STICK NOSE DOWN ANSDR GTIA2023120137653Megaphone · no testAFT GALLEY MEGAPHONE NOT TESTING PROPERLY & NOT BLINKING DURING TEST.-R+R AFT F/A MEGAPHONE IAW A320 SPIRIT AIRLINES EMERGENCY EQUIPMENT DRAWINGSDR CALA2023120103516Fuel Cap · missingPDA 2 FUEL CAP FOUND MISSING UPON ARRIVAL TO ORD. COMPLIED W CDL REQUIREMENTS. NO DAMAGE TO COUPLER, STICKER APPLIED. CDL 28A COMPLIED WITH. OK TO APPLY CDL 28A.TOMC SMITH FUEL CAP NIS DEN CAP, COUPLING R OFF 0000 ON 31-2825-9-0001 7103 INSTALLED MISSING FUEL SDR YENA2023113001518Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H1, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631069, PERFORMED REPAIR FR16LH AT LEVEL DOOSDR YENA2023113001517Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631070, PERFORMED REPAIR FR16LH AT LEVEL DOOSDR YENA2023113001516Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 10 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); PERFORMED REPAIR FR16RH AT LEVEL DOOR STOP FITTING #7 HOLE 3. IAWSDR YENA2023113001515Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00012 ) FUR-A320-53-00976, REF ASDR YENA2023113001514Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; REF AEROMAN N/R 20232-631118, PERFORMED REPAIR ON DOOR STOP FITTING #7 FR SDR YENA2023113001513Unknown · unknownDURING HEAVY MAINTENANCE: WEAR ON BUSHING I/B ACTUATOR HING O/B LUG ON LH ELEVATOR; AFTER REMOVAL OF THE WORN BUSHING FOUND CORROSION ON THE LUG BORE FORUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ELEVATOR ACTUATOR ATTACH FITTING O/B LH THIS IS A CAT "A" REPSDR YENA2023113001512Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA LH SIDE CONTINUITY FITTING, CRACK LENGTH IS 0.180 INCH, IN COC KPIT (1 EA); ROTOTEST INSPECTION IN OPEN FASTENER 3 HOLES OF LH AND RH SIDES IAW NTM 51-10-0SDR YENA2023113001511Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK LENGTH IS 0. 100 INCH, CRACK DIRECTION IS 2 OCLOCK, IN COCKPIT (1 EA); REMOVED AND REPLACED MIRROR FITTINSDR YENA2023113001510Unknown · unknownDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 RH SIDE, FRAME 68; CRACK LOCATION: 06 OCLOCK , CRACK DEPTH: 0.145 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00024 ) PESDR YENA2023113001509Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 LH SIDE, FRAME 68; CRACK LOCATION: 06 AND 12 OCLOCK , CRACK DEPTH:0.187 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00025 ) PERFORMED REPAIR ON FSDR YENA2023113001508Unknown · unknownDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CORROSION STRINGER 43L LOCATED BTW FRAME 62 AND FRAME 63 IN AFT CARGO COMPARTMENT (CPCP-RELATED MPD TASK 534107-01); (RESOLVED ON W/O: 1269492 TASKCARD: NR-00026 ) REMOVED AND REPLACED STRINGER 43L LOCATED BTWSDR YENA2023113001507Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE AT UPPER JOGGLE AREA, HOLE A, CRA CK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1EA); REF AEROMAN NR 2023-631084 WO 2023 358/1 ACCOMPLISHED REPAIR OF THE CRACK AT FR 20 RH UPPER JOGGLE AREA HOLE A ISDR YENA2023113001506Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 AT FWD GALLEY AREA (1 EA) (CRACK INDICAT ION ON FRAME 20 LH SIDE AT UPPER JOGGLE AREA, HOLE 6, CRACK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2023-631085 WO 2023 358/1 ACCOMPLISHED RSDR YENA2023113001505Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON UPPER SURFACE OF THE UPPER SKIN OF THE C ENTER WING BOX FR41 TO FR42 ON LH SIDE IN PASSENGER CABIN (CPCP RELATE D REFER MPD TASK 571157-01); REF AEROMAN NR 2023-631067 WO 2023 358/1 PERFORMED PERMANENT REPSDR YENA2023113001504Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER ATTACHMENT AREA AND CONTINUITY FITTING / CRACKS - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
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