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 YENA2022031500224Stringer · corrodedDURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19283 - CORROSION STRINGER 43R BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19283 - PERFORMED PERMANENT REPAIR ON SECTION STRINGER LOC. ON FR32 TO FR 34 AND STR 43R IN FWD CARGO COMPARTMENT IASDR YENA2022031500223Stringer · corrodedDURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19151 - CORROSION STRINGER 44 BETWEEN FRAME 24A TO FRAME 28 IN FWD CARGO COMPA RTMENT; PER AEROMAN N/R 2022-19151 - REMOVED AND REPLACED STRINGER 44 PRODUCTION SECTION LOC BTW FR24A TO FR28 IN FWD CARGO COMPARTMESDR YENA2022031500222Stringer · corrodedDURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19280 - CORROSION STRINGER 40L BETWEEN FR31/FR32 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19280 - PERFORMED PERMANENT REPAIR ON SECTION STRINGER LOC. FR 31 TO FR 33 AND STRINGER 40L IN FWD CARGO COMPARTMENTSDR YENA2022031500221Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19125 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT FWD RH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 843). AFT FRAME SEGMENT L= 2.20 INCHES. FWD FRAME SEGMENT L= 2.00 INCHES; PER AEROMAN N/R 2022-19125 SDR YENA2022031500220Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19128 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT AFT RH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 844). AFT FRAME SEGMENT L= 1.20 INCHES. FWD FRAME SEGMENT L= 1.70 INCHES; PER AEROMAN N/R 2022-19128 SDR YENA2022031500219Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19130 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT AFT LH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 834). FWD FRAME SEGMENT L= 0.80 INCHES; PER AEROMAN N/R 2022-19130 - REMOVED AND REPLACED FRAME SEGMESDR YENA2022031500218Frame · crackedDURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19132 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT FWD LH SIDE OVERWING EMERGENCY EXIT HATCH (EEH DOOR 833). AFT FRAME SEGMENT L= 1.40 INCHES. FWD FRAME SEGMENT L= 1.20 INCHES; PER AEROMAN N/R 2022-19132 -SDR YENA2022031500217Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 41R BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 2/1 N/R 2022-19284 REPLACED SECTION STRINGER 41R AND FASTENERS LOC ON FR32 TO FR34 IAW SRM A320 51-72-11, 51-42-11 AND DRAWINGS # E533231472, D532314SDR YENA2022031500216Fitting · corrodedDURING HEAVY MAINTENANCE, CORROSION ON FITTING MLG ACTUATOR L/H SIDE; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00039 )
REF: ARM W/O 2022 2/1 N/R 2022-19333 REPAIRED IAW A320 SRM 57-26-13-300-007 TABLE 001. THIS IS CAT C WITH REPAIR LIFE LIMIT 40000FC FROM FIRSDR YENA2022031500215Fitting · corrodedDURING HEAVY MAINTENANCE, CORROSION ON FITTING MLG ACTUATOR RH SIDE; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00040 )
REF: ARM W/O 2022 2/1 N/R 2022-19333 REPAIRED FITTING IAW A320 SRM 57-26-13-300-008 TABLE 001. THIS REPAIR IS CAT C WIFE LIMIT 35000FC FROM RSDR YENA2022031500214Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION STRINGER 44 BETWEEN FR33/FR34 IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00041 ) REF: ARM W/O 2022 2/1 N/R 2022-19282 REPAIRED IAW A320 SRM 53-00-13-300-001 PROCEDURE 2. A AND DRAWING D53231375. THIS RESDR AALA202202227820Sealant · leakingAIRCRAFT WAS GROUNDED: ON TAKE OFF FROM PHX, ATC REPORTED VISUAL VERIFICATION ON SOMETHING LEAKING FROM RIGHT WING, VERIFIED BY SOUTH WEST AIRLINES CREW. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHX WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENTSDR GTIA2022022136293Not Reported · not reportedAFTER T.O. POWER REDUCTION THE OIL QUANTITY WENT DOWN TO APPROX 6.2 QT. WE GOT THE ADVISORY AND FLASHING INDICATION. IT SHOWED 8.5 DURING THE APPROACH AND LANDING-SRVCD ENG #2 IAW AMM 12-13-79 W/9QTS OF OILSDR YENA2022022100082None · noneFLT # 1021, FLL-POS. APU AUTO SHUTDOWN IN FLIGHT; PERFORMED RESET OF APUT ECB. IAW AMM 49-61-34. OPS CHECK GOOD. NO FAULTS FOUND. A/C OK FOR SVCSDR CALA2022022100463Intercostal · crackedR1 FR16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APPE ARS TO BE IN FRAME LAYER AT 5 O''CLOCK. GENERATED BY V892444 PER NR 9298275/36275 INSPECTIONS AT RH FR16 AT DOOR STOP FITTING #1 HOLE#3 AND #4 PER REACHES 38,829 TOTAL ACFT FC.PERFORM REPEAT INSPSDR CALA2022022100462Skin · crackedFR 35 STR 30 LH CRACK INDICATIONS NOTED IN FASTENER HOLE #2 FRAM E,AFT SKIN FWD SKIN LAYERS AND HOLE #3 FRAME LAYER ONLY. 5331-02848 PART 1.1. ACCOMPLISH PERMANENT REPAIR AT LH FR 35 STR BEFORE 16AUG2022. ALL WORK ACCOMPLISHED ON HAECO NR 9298178 AND 30 HOLES SDR YENA2022022400086None · failedFLT # 2092, MIA-JFK. A/C FLYING UNCOORDINATED IN CRUISE ON APPROACH RUDDER TRIM WAS TRIMMING IN THE OPPOSITE DIRECTION AND CREATED A SIGNIFICANT MISS TRIM AT A/P DISCONNECT; REF LOG PG 3322673 ITEM #2 R/R #5 LEFT WING SPOILER ACTUATOR AND PERFORMED RUDDER RIGGSDR GTIA2022022136291Megaphone · inoperativeAFT MEGA PHONE INOP-R&R AFT MEGA PHONE IAW AMM 25-60-00,OPS CHK GOODSDR CALA2022022100450Joint · corrodedA3NB-53-3-6105 FORWARD CARGO STRG 42R HAS CORROSION BETWEEN FR 3 3 AND FR 34. (DOT 38-82)() REMOVED AND INSTALLED SPLICE, STRG 42R BETWEEN FR33 AND FR34 IAW A320-200, SRM 51-42-11/001 AND APPLIED TREAT AND PRIME IAW A320 -200, SRM 51-21-11/001. ATTACHED 44-000SDR AALA202202247069Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING BORE BETWEEN PYLON RIB 4 AND RIB 5. REPAIRED SPIGOT FITTING PER SRM 54-51-12-283-002.SDR AALA202202184652Smoke Detector · false activationAIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE MESSAGE AFT LAVATORY (FALSE). PERFORMED OPERATIONS TEST OF LAVATORY SMOKE SYSTEM PER TSM 27-17-00- TEST OK-NO FAULTS.SDR AALA202202180351Damper · faultyAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 DAMPING FUNCTION FAILS OPERATIONAL TEST. REPLACED DOOR DAMPER / EMERGENCY OPERATION CYLINDER PER AMM 52-11-14-400-001-B.SDR CALA2022021800428Landing Gear · noiseNOISE AND SHAKING AFTERGEAR UP/ 250KTSNOISE WAS INTERMITTENT OCURRING AS PER L/P 8006234 , PERFORMED FUNCTIONAL TEST OF NOSE LANDING EXTENSION ANDRETRACTION PER AMM 32-31-00-720-003-A ALL CHECKS NORMAL.SUSPECT NLG SHOCK STRUT SEVICEING.PERFORMED NLG SHOCK ABSOSDR CALA2022021800427Stringer · corrodedAFT CARGO BILGE STRINGER 42 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298691 (36691) REMOVED AND REPLACED STR42 L/H AT FR57 IAW A320 SRM 51-72-11-911 -001.PERFORMED BY V061765,INSPECTED BY: V061334.SDR CALA2022021800426Stringer · corrodedAFT CARGO BILGE STRINGER 40 LEFT CORRODED AT FR57.A3NB-12-3-6020 GENERATED BY:V892285 AT HAECO LCQ PER NR:9298690 (36690) REMOVED AND REPLACED STR40 L/H FR47-57 IAW A320 SRM 51-72-11-911 -001 PERFORMED BY:V061630 INSPECTED BY:V061334SDR CALA2022021800424Intercostal · crackedL1 FR 16 DOOR STOP #1 HAS CRACK INDICATION IN LOWER IB HOLE, APP EARS TO BE IN INTERCOASTAL LAYER AT 3 O''CLOCK. SUPPORT TASK GENE RATED BY:V892444 AT HAECO LCQ PER NR:9298272 (36272) PERFORMED INTERCOASTAL REPLACEMENT AT L1 FR16, STOP FITTING #1 IAW EA5311-0SDR CALA2022021800423Intercostal · crackedL1 FR 16 DOOR STOP #7 HAS CRACK INDICATION IN UPPER IB HOLE, APP EARS TO BE INTERCOASTAL LAYER AT 4 O''CLOCK. SUPPORT TASK. GENERA TED BY V892444 AT HAECO LCQ PER NR:9298273 (36273). PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT L1 FR16, STOP FITTI NG #7. IAW ESDR CALA2022021800422Intercostal · crackedR1 FR16 DOOR STOP #7, HAS CRACK INDICATION IN UPPER IB HOLE AT 5 O''CLOCK. GENERATED BY:V892444 AY HAECO LCQ PER NR:9298276 (3627 6) SUPPORT TASK.. PERFORMED INTERCOASTAL REPLACEMENT REPAIR AT R1 FR 16, STOP FITT ING #7 IAW EA 5311-02164.002 & REPAIR DWG R5311SDR CALA2022021800421Plate · corrodedAFT CARGO PIT R/H DOOR SILL SUPPORT BOX BETWEEN FR52A-56, HAS CO RROOSION ON UPPER SURFACE.A3NB-05-3-6023. GENERATED BY V919150 A T HAECO LCQ PER NR:9298328 (36328) REMOVED 7 REPLACED AFT CARGO PIT R/H DOOR SILL SUPPORT FR52A-56 IAW A320 SRM 51-72-11 PERFORMEDSDR CALA2022021600407Light · faultyCHRONIC ISSUE EMERGENCY LIGHTS ON IN ARMED POSITION. REF TSM 33-51-00-810-881-A FOR TROUBLESHOOTING. PILOT REPORTS ONLY LEFT SIDE OF AIRCRAFT IS COMING ON. PLEASE REF TSM 33-51-00-810- 881A FOR TROUBLE SHOOTING. SUSPECT WIRING ISSUE TO LEFT SIDE OF AIRCRAFT. PSDR CALA2022021600406Reservoir · low*EMERGENCY* Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD ECAM HYD Y RSVR LO LVL CREW REPORTS NO ALTERNATE EXTEND REPLACED YELLOW SYSTEM LOW LEVEL SWITCH PER AMM 29-13-41. ECAM MESSAGE CLEARED NO FURTHER ISSUES ADD EMP:U377618 ROTABLE PARTS CHANGE WAS INSDR YENA2022021800078Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR YENA2022021800077Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR YENA2022021800076Computer · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-SDR GTIA2022021736287Unknown · odorAIR QUALITY EVENT UNDER 10,000 FT IN CABIN -PER TSM 05-50-00-810-831-A. RUN ENG #1 PACK1&2 NO SMELL. RUN ENG #2 PACK1&2 NO SMELL. PACK BURN OUT COMPLY. SYSTEMS SERVISABLESDR CALA2022021600401Intercostal · damaged(A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBISDR CALA2022021600398Fitting · cracked(AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 LH SIDE CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR BEFO RE NEXT FLIGHT.SDR CALA2022021600397Crossbeam · cracked(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IASDR CALA2022021600396Floor Support · corroded(A3NB-53-3-6038) FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/FR20 H AS CORROSION. DOT 52-67. () FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/20 REPLACED IAW A320 SR M 51-42-11 P/N: D531127820201 BATCH:0003858615. ACCOMPLISHED BY EMP#V934585 AT BFM ST AEROSPACE MOBILESDR AALA202202157361Flap · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUT BOARD TRAILING EDGE FLAP UPPER SURFACE HAS DELAMINATION / DISBOND BETWEEN RIB 4 AND RIB 5 IN TRAILING EDGE ZONE 2. REPAIRED FLAP PER SRM 57-53-00-300-100.SDR GTIA2022021436286Not Reported · not reportedL2 DOOR ASSIST BOTTLE NEEDS SERVICE-SERVICED L2 DOOR ASSIST BOTTLE I.A.W. AMM 52-22-00SDR GTIA2022021436285Not Reported · not reportedR2 DOOR ASSIST BOTTLE REQUIRES SERVIVING-SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00. OPS CHECK GOODSDR CALA2022021400384Beam · corroded(A3NB-53-3-6038) FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/FR20 H AS CORROSION. DOT 52-67. () FWD CABIN FLOOR BEAM -Y1292 BETWEEN FR16/20 REPLACED IAW A320 SR M 51-42-11 P/N: D531127820201 BATCH:0003858615. ACCOMPLISHED BY EMP#V934585 AT BFM ST AEROSPACE MOBILESDR CALA2022021400383Crossbeam · cracked(AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IASDR YENA2022021600063None · noneFLT # 2864, SRQ-JFK (DIVERTED TO ATL). AIR ENG 1 BLEED LEEK ECAM ON IN FL. APPLIED ECAM AND QR PROCEDURES. DID NOT RESET.; FOUND LPSOV (ENG #1) LOWER V-CLAMP UNLATCHED, ALLOWING HOT AIR TO ESCAPE. RE-SECURED CLAMP TO LPSOV AND PERFORMED OPS + LEAK CHECK PER ASDR GTIA2022021436279Not Reported · not reportedAIR QUALITY EVENT UNDER 10,000FT. FOLLOWED COM PROCEDURE ISOLATED PACK 1 ( 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 )--SDR GTIA2022021436278Megaphone · inoperativeREAR MEGAPHONE IS INOP-R&R AFT MEGAPHONE IAW CMM 25-60-01. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIMESDR GTIA2022021436277Hinge Arm · corrodedDENT FOUND ON FUSELAGE SKIN LOCAATED AT FR 21-23 STOR 24-25 LH RAF 2890091-1 CREATED REF LTPR NR 500436517-0010.-VERIFIED NR #5001136517-0010, DENTS IS WITHIN LIMITS AS PER SRM 53-00-11-283-005 REV. 139, WITH RE-INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMSDR GTIA2022021436276Not Reported · not reportedDURING WEEKLY CHECK FOUND L2 DOOR REQUIRES DOOR ASSIST SERVICED-SERVICED L2 DOR ASSISST IAW AMM 52-10-00SDR CALA2022021400372Stringer · corrodedA3NB-53-3-6186 AFT CARGO BILGE AREA STRINGER FR56 TO FR57 S43L H AVE CORROSION DOT 42-037 () REMOVED AND INSTALLED NEW COUPLING AND STRINGER IAW SRM 51-42-11 -00. ACCOMPLISHED BY EMP#V934344 AT BFM ST AEROSPACE MOBILE. NR #0020417.
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