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 CALA2022122603486Stringer · corrodedAFT CARGO COMPARTMENT, FR56-FR58, STRG43L CORRODED. REMOVED AND REPLACED STRINGER 43L FR56 TO FR58 IAW SRM 51-42-11.SDR CALA2022122603485Floor Support · corrodedFLOOR SUPPORT -Y1292 FR64-FR66 HAS CORROSIONAT FR64 AND FR66. FLOOR SUPPORT -Y1292 FR64-FR66 REMOVED IAW SRM 51-42-11, FOUND T ENGBFM WC: 41194 O BE OUT LIMITS IAW SRM TASK 53-00-14-283-002 L-1.500",W=1.0", D =0.075" T93986, RECEIVED NEW FLOOR SUPPORT P/N D534SDR CALA2022122303476Floor Support · corrodedFLOOR SUPPORT -Y1292 CORRODED AT FRAME 68. FLOOR SUPPORT REMOVED IAW SRM 51-42-11, FOUND TO BE OUT LIMITS IAW SRM 53-00-14-283-002, AND INSTALLED NEW IAW SRM 51-42-11.SDR CALA2022122303475Stringer · corrodedAFT CARGO COMPARTMENT, FR56-FR58, STRINGER 43L CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11.SDR CALA2022122303474Door Sill · corrodedMAIN CABIN FLOOR STRUCTURE. R2 DOOR SILL FR 66 CORROSION AT FAST ENER HOLE IN PLATE UNDER GIRT BAR FITTING. INBD AND AFT OF GIRT BAR FITTING. VISUAL INSPECTION, CORROSION NOTED OUT OF LIMITS IAW SRM 51-75-12. REMOVED DOOR SILL IAW SRM 51-42-11/001. LOCATEDSDR CALA2022122303473Stringer · corrodedAFT CARGO PIT BILGE STRINGER 42L FR57-FR58 HAS CORRSION. REMOVED FASTENERS ON AREA IAW SRM 53-41-13-300-010, INSTALLED REPAIR ANGLE AND APPLIED TOP COAT IAW SRM 53-41- PERFORMED 13-300-010.SDR CALA2022122303472Profile · crackedLEFT FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED THE PROFILE IAW SRM 51-42-11.SDR AALA202212278049Proximity Switch · dirtyAIRCRAFT WAS NOT GROUNDED: R1 DOOR INDICATES OPEN IN CLOSED POSITION. **SUPPLEMENTAL REPORT FOR AALA202212238049: CLEARED DEBRIS FROM R1 DOOR PROXIMITY SWITCH. ACCOMPLISHED SATISFACTORY OPERATIONAL TEST FOR DOOR WARNING SYSTEM PER AMM 52-71-00.** (CLOSED)SDR AALA202212238049Warning Message · illuminatedAIRCRAFT WAS NOT GROUNDED: R1 DOOR INDICATES OPEN IN CLOSED POSITION. (OPEN)SDR AALA202212234731Window · scratchedAIRCRAFT IN BASE MAINTENANCE: SCRATCH ON COCKPIT LEFT HAND SIDE FIXED WINDOW. REPLACED WINDOW PER AMM 56-11-12-000-001-A AND AMM 56-11-12-400-002-A.SDR YENA2022122301283Power Supply · inoperativeFLT#769, BOS-FLL. EMERGENCY LIGHTS INOPERATIVE AT 13 ABC, 17 ABC & 18 ABC, OVERHEAD. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-38. OPS CHECKED GOOD.SDR YENA2022122301287Apu · leakingFLT# 1475, BDL-SJU. STRONG ODOR OF WET DOG DESCENDING THROUGH 11,000 REPORTED MID CABIN BY FAS, COULD ALSO ODOR IN COCKPIT. THE ODOR WENT AWAY WHEN PACK NR 2 WAS SELECTED OFF. PERFORMED INSPECTION DUE TO ODOR EVENT LEVEL A IDENTIFIED APU INTAKE SWEAT WITH OSDR CALA2022122303468Profile · crackedLH AFT EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REMOVED AND REMPLACED PROFIL AT LT EMERGENCY EXIT DOOR FAN NEW PROFILE IAW SRM 51-72-11-91 1-001.SDR CALA2022122303467Stringer · corrodedAFT CARGO PIT BILGE STRINGER 42L FR57-FR58 HAS CORRSION. DOT NO. 17-154 () REMOVED FASTENERS ON AREA I.A.W SRM 53-41-13-300-010, REMOVED CO EA, INSTALLED REPAIR ANGLE AND APPLIED TOP COAT I.A.W SRM 53-41- RROSION IN AREA D= 0.0185 L= 2.2265 I.A.W 51-42-11 SRM,SDR CALA2022122303466Profile · crackedLH FWD EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. REPLACED FWD LOAD TRANMITTING PROFILE IAW SRM 51-42-11.SDR CALA2022122303465Door Sill · corrodedMAIN CABIN FLOOR STRUCTURE. R2 DOOR SILL FR 66 CORROSION AT FAST ENER HOLE IN PLATE UNDER GIRT BAR FITTING. INBD AND AFT OF GIRT BAR FITTING. () VISUAL INSPECTION AROUND DOT. CORROSION NOTED OUT OF LIMITS IAW W SRM 51-75-12. ACCOMPLISHED IAW SRM 53-41-14-283-0SDR CALA2022122303464Door Sill · corrodedL2 DOOR SILL HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED L2 DOOR SILL. IAW A320 SRM 51- 42-11. RESTORED SURFACE PROTECTION IAW SRM 51-75-12-911-001 .SDR CALA2022122303463Skin · corrodedINTERNAL FUSELAGE SKIN AFT OF AFT LAV EXHAUST VENT CORRODED. A3N B-53-3-0047. REMOVED AND REPLACED AFT LAV EXHAUST REENFORCEMENT PLATE IAW A32 0 SRM 51-42-11/001.SDR GTIA2022122236844Bottle · low pressureDURING WEEKLY CHECK FOUND R1 DOOR ASSIST REQUIRES SERVICE-SERVICED R1 DOOR ASSIST IAW AMM 52-10-00SDR GTIA2022122236843Unknown · odorSOCK ODOR AT 10K, DURING DESENT, LASTED AROUND 5 MINUTES. C/W ODOR INSPECTION IAW TSM 05-50-00. C/W ENG RUN PER AMM 71-00-00. NO DEFECTS NOTEDSDR CALA2022122103459Profile · crackedLH AFT EMERGENCY EXIT DOOR FWD LOAD TRANSMITTING PROFILE CRACKED. DOT NO. 17-30 () REMOVED AND REMPLACED PROFIL AT LH EMERGENCY EXIT DOOR FAN NEW P ROFILE P/N D5227907620551 BATCH# 0004041671 I.A.W SRM 51-72-11-91 1-001 EMP#: V940362 WORK ACCOMPLISHED AT ST ENSDR YENA2022122301286A/C Pack · malfunctionedFLT#1691, JFK-LIR. ' ( PACKS )ON DESCENT, NOTICED THE CABIN TEMP INCREASE TO 76-78DEG TURNED TEMP VALVE KNOBS TO A COOLER SETTING. BUT NO RESPONSE TURNED THE HOT AIR VALVE OFF AND TEMP COOLED SMELT HOT SMELT HOT IN IN COCKPIT BEFORE THE CABIN COOLED OFF. TURNESDR YENA2022122301284None · noneFLT# 460, FLL-BDL. FO EMERGENCY FLASHLIGHT INOPERATIVE. ACCOMPLISHED AN OPS CHECK OF THE F/O FLASHLIGHT. OPS CHECKED GOOD IAW AMM 25-60-00. NO DEFECTS NOTED.SDR AALA202212216359Control Unit · warning lightAIRCRAFT WAS GROUNDED: ECAM AUTO BRAKE FAULT AFTER TAKEOFF. EMERGENCY DECLARED. FLIGHT RETURNED TO PHX LANDING SAFELY. MAINTENANCE REPLACED BRAKE / STEERING CONTROL UNIT (BSCU) PER AMM 32-42-34 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.SDR CALA2022122103454Door Sill · corrodedL2 DOOR SILL HAVE CORROSION FWR AND AFT ENDS PER HA ECO LCQ N/R 9296328/40328. FWD SIDE WAS FOUND TO BE WITHIN LIMITS, AFT WAS OUT OF LIMITS, PERFORMED REPAIR PRINCIPLE 5 IAW SRM 53-41-14-300-001. RESTORED SURFACE PROTECTION IAW SRM 51-21-11.SDR CALA2022122103452Controller · faultedFCTL SPLR FAULT AT CRZ SPLRS APPEAR FLUSH, INOP SYS SPLR 5 INSPECTED WIRING AT NR 5 SPOILER ACTUATORS, NO DAMAGE FOUND. VERIFIED INSTALLATION OF #5 SPOILER , SAFETY AND SECURITY OF COMPONENT UP TO 4 C 9 IAW GMM 09-25-05. ACCOMPLISHED CONTINUITY CHECKS AND MEGGSDR GTIA2023011236873Computer · faultedF/CTL ELAC 1 AND 2 FAULT ALTERNATE LAW FOLLOWED BY DIRECT LAW-PERFORMED EFCS GND SCAN IAW TSM 27-40-00-810-802A AND TSM 27-40-00-804A. NO FAULTS DETECTED . PERFORMED OPS CHECK OF THS AND EFCS SYSTEM IAW AMM 27-96-00 OPS CHECK GOOD NO DEFECTS NOTED A/C GOOD FORSDR YENA2022121901265Battery Pack · no testFLT#225, JFK-TPA. 'EMERG LIGHT BATTERY 13WL FAILED BATTERY TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY FIN 13WL IAW AMM 33-51-38.SDR AALA202301041145Transfer Valve · faultedAIRCRAFT WAS NOT GROUNDED: LEFT FUEL TRANSFER VALVE DID NOT OPEN ON DESCENT INTO PHX. OPENED AFTER LANDING. **SUPPLEMENTAL REPORT FOR AALA202212201145: MAINTENANCE ACCOMPLISHED TSM 28-15-00-810-801-A AND FOUND NO FAULTS OR ISSUES NOTED. ** (CLOSED)SDR AALA202212201145Transfer Valve · faultedAIRCRAFT WAS NOT GROUNDED: LEFT FUEL TRANSFER VALVE DID NOT OPEN ON DESCENT INTO PHX. OPENED AFTER LANDING. OPENSDR YENA2022121901267Battery Pack · no testFLT#225, JFK-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FIN 10WL IAW AMM 33-51-38.SDR YENA2022121901266Battery Pack · no testFLT#225, JFK-TPA. EMERGENCY LIGHT BATTERY FIN 11WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERG LIGHT BATTERY 11WL IAW AMM 33-51-38.SDR YENA2022121901264Battery Pack · no testFLT#2752, SJU-TPA. EMERG LIGHT BATTERY 13WL FAILED TEST; REMOVED AND REPLACED PER AMM 33-51-12.SDR CALA2022121903440Pump · low pressureCTR TK PUMP 1 LO PR DISPLAYED ON UPPER ECAM SCREEN. - FUEL SHORTLY AFTER DEPARTURE CENTER TANK FUEL PUMP 1 WAS REPLACED.SDR CALA2022121903432Intercostal · corrodedSUPPORT TASK AFT WET AREA LH WEB SUPPORT BETWEEN FR69 AND FR70 HAVE CORROSION PER HAECO LCQ N/R9296334/40334 GENERATED BY V06168 2 STEP 1 REMOVED LH WEB SUPPORT @ FR 69-70 DUE TO CORROSION IAW A3 PART AT LH FRAME AREA 69-70 IAW SRM SOR A320-200-51-42-11-001 APSDR CALA2022121903431Floor Support · corrodedFLOOR SUPPORT Y1292 FR68-FR69 CORRODED AT FR68. REMOVED AND REPLACED FLOOR SUPPORT Y1292 FR68 TO 69 I.A.W SRM 51 -42-11-001 AND APPLIED TOP COAT I.A.W SRM 51-23-11. EMP: V934614 WC: 41180 STA: ST ENG BFMSDR CALA2022121903430Floor Support · corrodedFLOOR SUPPORT Y1292 FR66-FR68 HAS CORROSION AT FR66 AND FR68. REMOVED AND REPLACED FLOOR SUPPORT Y1292 FR66 TO FR68 I.A.W SRM 51-42-11 AND APPLIED TOP COAT I.A.W SRM 51-23-11. EMP: V934614 W C: 41184 STA: ST ENG BFMSDR AALA202212280953Nut · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT PYLON SPIGOT FITTING NUT. MAINTENANCE REPLACED THE NUT IAW TASK CARD 26C411554031.SDR GTIA2022121936838Flashlight · inoperativeFWD RH CABIN FLASHLIGHT INOP ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R/R FLASHLIGHT ASSY IAW AMM 25-65-00. THIS CLEARS MDDR 44395. PLACARD REMOVED. MOC NOTIFIED.SDR YENA2022121901272Bulb · burned outFLT#129, JFK-RSW. 'EMERGENCY EXIT LIGHTS BULBS ARE BURNT OUT. (SEVERAL); RELAMPED EMERGENCY EXIT LIGHT BULBS IAW AMM 33-51-13. THE OPS CHECK IS GOOD. A/C OK FOR SERVICE.'SDR CALA2022121903423Fitting · crackedF.O LOWER WINDHISELD CONTINUITY FITTING AT LOWER CENTER POST PRODUCED A CRACK INDICATION DURING THE HFEC INSPECTION. GENERATED A T HAECO LCQ PER NR 9298244 (32244) BY V061690 EA 5310-07675 AD 2 020-17-03. THE FRONT WINDSHIELD FRAME RH CONTINUITY FITTING, ACCOMSDR AALA202301234587Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING. MAINTENANCE REPLACED LOWER SPIGOT FITTING [ER AMM 54-51-41.SDR AALA202301043054Oil System · failedAIRCRAFT WAS GROUNDED, NR 1 ENGINE LOST OIL QUANTITY AND OIL PRESSURE AT FL380 IAW ECAM MESSAGES. FT CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO BNA, LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE IAW SDR GTIA2022121936837Epsu · no testEPSU BATTERY (11WL) FAILED. SDR REQD.-VERIFIED NR # 5001200054-0010, EPSU BATTERY (11WL) WAS REPLACED I.A.W AMM 33-51-B8-000/400-002-A REV. 74. TEST SATISFACTORY.SDR GTIA2022121936836A/C Pack · odorDIRTY SOCK SMELL DURING DESCENT TO MCO WE WERE ABLE TO ISOLATE PACK 1 AND CONTINUE WITH PACK 2 AND SMELL RECEDED ( 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 NSDR YENA2022121901268Apu · leakingFLT 8362, AUA-FLL. EXPERIENCED A FUME EVENT ON CLIMB OUT AND DESCENT BY ENTIRE FLIGHT CREW AT APPROX 15,000'-18,000'. APU WAS OFF, DURING T/S, FOUND A SOURCE OF OIL CONTAMINATION FROM APU, COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2. DECONTAMINATION, LESDR CALA2022121903420Web · corrodedFWD CABIN WEB AT -Y1732 CORRODED AT FR20. FWD CABIN WEB AT -Y1732 REMOVED AND REPLACED IAW SRM 51-42-11/00 1 AND APPLIED TOPCOAT IAW SRM 51-23-11. EMP: V934614 WC: 41297 S TA: ST ENG BFMSDR CALA2022121903419Floor Support · corrodedFLOOR SUPPORT Y515 FR68 TO FR70 CORRODED AT 2 LOCATIONS REMOVED/REPLACED SUPPORT Y515 FR68 TO FR70 P/N D5347209400400 BT CH 0003912854 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 41168 S TA: ST ENG BFMSDR CALA2022121903418Floor Support · corrodedFLOOR SUPPORT Y515 FR64 TO FR67 CORRODED AT 2 LOCATIONS REMOVED/REPLACED FLOOR SUPPORT Y515 FR64 TO FR67 P/N D5347209400 800 BTCH 0003809500 IAW SRM 51-72-11-911-001. EMP: V934337 WC: 4 1167 STA: ST ENG BFMSDR CALA2022121903410Fuel Cap · missingPDA 2 AIRCRAFT ARRIVED WITH FUEL CAP MISSING. REPLACED MISSING REFUEL COUPLER CAP.
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