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 YENA2023021400162None · noneDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC FR 66 TO FR 68 AT LEVEL STR 23L AFT GALLEY AR EA (CPCP RELATED REFER TO THE MPD TASK 534195-01); ALL WORK ACCOMPLISHED ON AEROMAN NR #2022-676475, PERFORMED REPAIR AT LOWER SILL LOC FR 66 TO FR 68 AT LEVEL STRSDR YENA2023021400161None · noneDURING HEAVY MAINTENANCE: WINGS / CENTER WING / FRONT SPAR / FR 36 / VERTICAL STIFFENER / CRACK DAMAGES - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023021400160None · noneDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / MLG ACTUATOR FITTING – STRUCTURAL REINFORCEMENT. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023021400159None · noneDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR68 & STGR 22R HORIZONTAL FLANGE RADIUS & DOOR STOP FITTING #1 HOLE 3 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023021400158None · noneDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST / CRACK DAMAGE - PERMANENT REPAIR (MIRROR FITTING SOLUTION). (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023021300154Filter · failedFLT#599, LGA-MCO. 'DIRTY SOCK SMELL ON APPROACH MX-270 COMPLETED. ( PACKS ); PERFORMED APU CLEANING & COMPRESSOR WASH, LEVEL B DECON, AND REPLACED BOTH RECIR AND OZONE FILTERS APU BORO OK. DETERMINED ENG 1 WAS NOT THE SOURCE OF SMELL COMPLIED WITH INFORMATION SDR CALA2023021000385Wheel · unknownDUE TO REPORT FROM UPLINE STATION, PLEASE CHECK MLG WHEELS AND VERIFY ALL MLG WHEEL BOLTS INTACT REF AMM 32-41-00. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CONTRACT MX V939360 SHELDAHL , BRIAN INSPECTED ALL 4 MLG WHEELS CHECK MLG WHEELS AND VERIFY ALL MLG SDR YENA2023021300153None · noneFLT#1463, LAX-SJD. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX) ' AFTER ROTATION & CALL FOR GEAR UP. THE NOSE DOOR OR GEAR DID NOT CLOSE OR RETRACT. ECAM ALERT CLIMBED TO 1000' & DOOR OR GEAR RETRACTED. NO FURTHER INDICATION. CONTACT MX TOLD T TO RETURN TO LAXSDR GTIA2023020136967Unknown · unknownFUME EVENT. DIRTY SOCKS SMELL DURING CLIMB & WORSE DURING DESCENT-FOUND NO EVIDENCE OR SMELL OF CONTAMIANTS OR DRTY SOCK SMELL IN CABIN OR COCKPIT PER TSM 05-50-00-810-831-ASDR GTIA2023020136966Unknown · unknownFUME EVEN, DIRTY SOCKS SMELL DURING CLIMB & WORSE DURING DESCENT-FOUND NO EVIDENCE OR SMELL OFCONTAMINANTS OR DIRTY SOCK SMELL IN CABIN OR COCKPIT PER TSM 05-50-00-810-831-ASDR GTIA2023020136965Epsu · no testEPSU- EMERGENCY SUPPLY UNIT 13WL FAILED TEST, SDR REQUIRED.-SDR 2907402-1 GENERATED FOR EPSU AT POSITION 13WL. NO FURTHER ACTION REQUIRED. REFERENCE AEROMAN NON ROUTINE 2022-648758 ON W/O 2022-481/1SDR GTIA2023020136964Bracket · crackedCRACK BRACKET TELESCOPIC DUCT OUTBOARD OF FIXED LEADING EDGE ON LH WING RAF-01 3102849-02 GENERATED-PERFORMED PERMANENT REPAIR ON LH WING LE UPPER SKIN TELESCOPIC DUCK BRACKET OB RIB IAW E.A.# 57-0031-23 AND EC NO. EA 5741-2311. REPAIR CATEGORY "A" INSPECTION SDR GTIA2023020136963Unknown · corrodedCORROSION FRAME 70 BTW STR 41R TO STR 44R IN AFT CARGO COMPARTMENT RAF-01 3102843-02 GENERATED-REPLACED FRAME 70 SEGMENT IAW EA # 53-0643-22 AND EC NO EO5351-2311. REPAIR CATAGORY "A" AND INSPECTION NOT REQUIRED.SDR GTIA2023020136962Unknown · corrodedCORROSION FRAME 70 FWD FACE OF THE REAR PRESSURE BULKHEAD AT LEVEL STR 43R IN AFT CARGO COMPARTMENT-REPLACED REAR PRESSURE BULKHEAD FR 70 LOWER DOME IAW EA # 53-0643-22 AND EC NO. EO 5351-2311. REPAIR CATAGORY "A" AND INSPECTION NOT REQUIRED.SDR GTIA2023020136961Rib · wornWEAR ON INTERCONNECTING STRUT FITTING ON RH WING RAF-01 3102842-02 GENERATED-RAF 3102842-02 NOT REQUIRED AS RAF 3102833-02 PREVIOUSLY GENERATED ADDRESSES THIS DISCREPANCY.SDR GTIA2023020136960Stringer · corrodedCORROSION STRINGER 42L LOCATED BTW FR 54 TO FR 55 IN AFT CARGO COMPARTMENT RAF-01 3102842-01 GENERATED-PERFORMED PERMANENT REPAIR ON STRINGER 42L LOCATED BETWEEN FRAME 54 TO FRAME 55 IN AFT CARGO COMPARTMENT IAW EA # 53-0640-22 AND EC NO. EO 5341-2301. REPAIR SDR GTIA2023020136959Unknown · dentedDENT LEG ASSY-NLG FWD POS ON NOSE LANDING GEAR RAF-01 3102841-02 GENERATED-PERFORMED PERMANENT REPAIR LOCATED ON LEG- ASSY-NLG FORWARD POSSITION ON NOSE LANDING GEAR IAW EA # 32-0656-22 AND EC NO 3221-2208. REPAIR CATEGORY "A" INSPECTION NOT REQUIRED.SDR GTIA2023020136958Unknown · damagedAFT GALLEY WORKDECK HAS NICKS AND DENTS RAF 3102841-01 GENERATED-REPLACED WORK DECK ON GALLEY #4 AT AFT GALLEY AREA IAW EA # 25-0634-22 AND EC NO.2530-2217SDR GTIA2023020136957Skin · corrodedCORROSION FOUND ON RH WING LOWER SURFACE AT RIB 14-17. RAF CREATED-PERFORMED PERMANENT REPAIR ON RH WING - TOP SKIN PANEL 2 - TRAILING EDGE OVERHANG BETWEEN RIB 14-15 , RIB 15-16, RIB 16-17 AND RIB 17-18 LOWER SURFACE IAW E.A. NO 57-0596-22 AND EC NO EO 5721-2SDR GTIA2023020136956Stringer · corrodedCORROSION FOUND ON STR 43L BETWEEN FR54 AND FR56 IN AFT CARGO COMPARTMENT. RAF CREATED-PERFORMED PERMANENT REPAIR ON STRINGER 43L LOCATED BETWEEN FRAME 54 TO FRAME 56 IN AFT CARGO COMPARTMENT IAW EA # 53-0640-22 AND EC NO. EO 5341-2301. REPAIR CATEGORY "A" SDR GTIA2023020136955Seat Track · corrodedCORROSION FOUND ON SEAT TRACK -Y1292 RH BTW FR41- FR7 IN CABIN. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y1292 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270. REPAIR CSDR GTIA2023020136954Seat Track · corrodedCORROSION FOUND ON SEAT TRACK -Y765 RH BTW FR41- FR47 IN CABIN. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270. REPAIR CASDR GTIA2023020136953Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y765 LH FR41- FR47. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270.. REPAIR CATEGORY "A" INSDR GTIA2023020136952Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y1292 LH FR41-FR47. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y1292 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270.. REPAIR CATEGORY "A" ISDR GTIA2023020136951Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y765 LH BTW FR36-41. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 36 TO FRAME 41 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IN ACORDANCE WITH EA # 53-0636-22 AND EC. NO EO 5331-2270. REPAIR SDR GTIA2023020136950Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y1292 LH FR36-41. RAF CREATED-PERFORMED PERMANENT REPAIR ON TO FRAME TRACK Y1292 LOCATED BETWEEN FRAME 36 TO FRAME 41 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IN ACCORDANCE WITH EA #53-0636-22 AND EC. NO. EO 5331-2270. REPAISDR GTIA2023020136949Spar · corrodedCORROSION FOUND ON SPAR LH WING SHROUD BOX FWD FACE BETWEEN RIBS WX866-WX1069. RAF-01 3102833-01 GENERATED.-PERFROMED PERMANENT REPAIR ON SHROUD BOX FWD FACE BETWEEN RIB 2 TO RIB 3 ON LH WING IAW EA # 57-0593-22 AND EC NO. EO 5751-2236.SDR GTIA2023020136948Skin · corrodedCORROSION ON LH WING TOP SKIN TRAILING EDGE LOWER SURFACE AT RIB 7 AND RIB 8. RAF-01 3102830-01 GENERATED-PERFORMED PERMANENT REPAIR ON LH WING - TOP SKIN PANEL 2 - TRAILING EDGE OVERHANG BETWEEN RIB 7-8 LOWER SURFACE IAW E.A. NO 57-0595-22 AND EC NO. EO 572SDR GTIA2023020136947Skin · corrodedCORROSION ON RH WING TOP SKIN TRAILING EDGE LOWER SURFACE AT RIB 7. RAF-01 3102829-02 GENERATED-PERFORMED PERMAMENT REPAIR ON RH WING TOP - SKIN PANEL 2 - TRAILING EDGE OVERHANG BETWEEN RIB 7-8 LOWER SURFACE IAW EA N0 57-0596-22 AND EC NO EO 5721-2307. REPAIRSDR CALA2023021000403Frame · corrodedR1 DOOR FR16 STGR 22R-STGR 23R CORRODED PER HAECO LCQ N/R 929651 4/40514 GEN BY V061629 "ACCOMPLISH A PERMANENT REPAIR ON THE FRAME AT RH FR16 AFT OF ECRA 5310-08111 ON OR BEFORE JANUARY 27, 2024" WEB FACE AT Z-520 FLOOR LEVEL PER PART 3 OF THE LATEST REVISIONSDR GTIA2023020936946Unknown · unknownDURING WEEKLY FOUND L1 DOOR ASSIST BOTTLE NEEDS SERVICING -SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR YENA2023020900148None · noneDURING HEAVY MAINTENANCE: FUSELAGE / TAIL CONE / FR 83-85 & STGR 3L-6L / IMPACT DAMAGE -PRELIMINARY INSPECTIONS. (SUPPLEMENTAL TO FOLLOW)SDR AALA202302090269Smoke Detector · false indicationAIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE WARNING. NO EVIDENCE OF SMOKE OR FUME OR FIRE. MAINTENANCE FOUND NO FAULT INDICATED AFTER CREW DEPARTED. PERFORMED SMOKE DETECTOR OPERATIONAL CHECK THROUGH MCDU PER AMM 26-17-00 WITH NO DEFECTS NOTED.SDR CALA2023020800369Fuel Cap · missingPDA 2 UPON ARRIVAL FUELER REPORT MISSING FUEL CAP. INSTALLED FUEL CAP.SDR YENA2023020900145None · failedFLT#954, SJU-FLL. 'SEC #3 FAULT DURING FINAL DESCENT WITH STRONG ELECTRICAL ODOR; PERFORMED TSM 24-00-00-810-823-A. IDENTIFIED SOURCE OF BURNT ELECTRICAL ODOR TO THE SEC3. REPLACED SEC 3 IAW AMM TASK 27-94-34. OPS CHECK NORMAL.'SDR YENA2023020800140None · noneFLT#595, HPN-MCO. ' FLIGHT ATTENDANT IN AFT GALLEY STATED SHE SMELLED "HYDRAULIC FLUID" DESCENDING THROUGH 10, 000 FEET; PER INFO NOTICE 2019-T015J NO HISTORY PAST 30 DAYS. SECTION A OPS BOTH PACKS ON APU BLEED NO ODOR PRESENT. INSP APU NO OIL CONTAMINATION PRSDR AALA202302082672Sign · intermittentAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 1L DOOR EMERGENCY EXIT SIGN FLASHES. MAINTENANCE REPLACED L1 DOOR EMERGENCY EXIT SIGN PER AMM 33-51-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR CALA2023020600351Battery · lowCABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - FWD L1 BATTERY LOW. REMOVED AND REPLACED FWD L1 EMERGENCY LIGHT BATTERY.SDR CALA2023020600350Epsu · not reportedMAIN CABIN FWD, EMERGENCY LIGHT DOES NOT WORKS (TROUBLESHOOT) REMOVED AND REPLACED EPSU 10WL OK IAW AMM 33-51-39-000-006-C1 AN D 33-51-39-400-006-C1. OPS CHECK PERFORMED IAW AMM 33-51-00-710- 002-C2 GOOD FOR SERVICE.SDR CALA2023020600349Panel · stuckEMERGENCY LIGHTS WILL NOT TURN OFF AFTER SELECTING ON FROM AFT ATT PANEL. FOUND EMER LIGHT SWITCH AT AFT ATTENDANT PANEL STUCK IN ON POSITION AND SWITCH WOULD NOT RELEASE. REMOVED AND REPLACED THE AFT ATTENDANT PANEL. OPS CHECK IS GOOD.SDR CALA2023020600348Battery Pack · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - MOST AFT EPSU BAT FAILED TEST REMOVED AND REPLACED EPSU BAT, OPS TST GOOD.SDR CALA2023020600347Battery Pack · not reportedCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LEFT EMERGENCY LIGHTS BATTERY FAILED THE CAPACITY TEST. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHTS BATTERY PER AMM 33-51-38. OPS CHECK GOOD.SDR CALA2023020600338Web · crackedRH FWD EMERGENCY EXIT DOOR FWD AND AFT WEB SUPPORT CRACKED PER H AECO N/R 9292715/40715 GEN BY V798788 RMVD AND RPLD 2EA WEB SUPPORTS ON R/H EMERGENCY EXIT DOOR IAW A3 20 SRM 51-72-11-911-001 BY MECH V061616 INSP BY V921658SDR GTIA2023020636937Epsu · inoperativeEPSU- EMERGENCY POWER SUPPLY UNIT 10WL AT FWD GALLEY INOP- SDR REQUIRED-SDR 3102850-02 GENERATED FOR EPSU AT POSITION 10WL. NO FURTHER ACTION REQUIRED. REFERENCE AEROMAN NON ROUTINE 00627 FOR REPLACEMENT ON WO 2022-481/1SDR YENA2023020600138Not Reported · not reportedFLT#2085, BDL-MIA. 'DURING DESCENT THROUGH 10,000 FT A MODERATE CHEMICAL ODOR WAS NOTICED ODOR WAS TRANSIENT & GONE AFTER LANDING ( APU BLEED AIR SUPPLY SYSTEM); BP PERFORMED APU COMPRESSOR WASH AS PER TC A320-49-20-00-100-004 ON WO 1234163.SDR AALA202302062081Mechanism · defectiveAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SFO DUE TO THE LANDING GEAR WOUND NOT RETRACT AND SHOCK ABSORBER FAULT. THE AIRCRAFT LANDED AT SFO SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE GEAR FLIGHT / GROUND SENSDR CALA2023020600323Flange · crackedA3NB-52-4-6031. DOT# 143-034. EMERGENCY ESCAPE HATCH R/H FLANGE THATS ATTACHED TO DOOR SKIN () FOUND CRACKS EXCEEDING DAMAGE LIMITS (LENGTH 5.4"). REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-11 AND SRM 51-72-11. P/N:D522 7902620451 BATCH NO:0003934661 ST ENSDR CALA2023020600321Director · unserviceableEVAC COMMAND ALARMSOUNDED DURING TAKEOFFROLL AT HIGH SPEED. LOCKING DUE TO MULTI CIDS 1 & 2 FAULT AFTER T/O UNLOCKING FOR UPDATE UNABLE TO PRODUCE FAULTS. FOUND FAULT HISTORY OF COMMUNICATION ERRORS IN POST FLIGHT REPORT. PRECAUTIONARILY R&R BOTH CIDS DIRECTORSDR CALA2023020300317Escape Hatch · crackedA3NB-52-4-6031. DOT# 143-034. EMERGENCY ESCAPE HATCH R/H FLANGE THATS ATTACHED TO DOOR SKIN () FOUND CRACKS EXCEEDING DAMAGE LIMITS (LENGTH 5.4"). REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-11 AND SRM 51-72-11. P/N:D522 7902620451 BATCH NO:0003934661 ST ENSDR AALA202302076080Hinge · excess playAIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR AFT HINGE HAS EXCESSIVE PLAY. MAINTENANCE REPLACED HINGE PER CMM 52-82-32.
Back to Airbus A320-232