Airbus A320-231
Service difficulty reports · 3,758
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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 = 'A320231' 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 = 'A320231' 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 AWXA0001495Floor Support · corrodedFLOOR SUPPORT AT RT FR 16 Y-1292 CORRODED. FLOOR SUPPORT FABBED AND INSTALLED IAW AIRBUS DWG 53112091200.SDR AWXA0001453Door · icedDTW - ABORTED TAKEOFF - 2/26/01 - DURING TAKEOFF ROLL THE CREW GOT AN ECAM MESSAGE FOR THE AFT CARGO DOOR. THE TAKEOFF WAS ABORTED BELOW 60 KTS. THE AFT CARGO DOOR WAS INSPECTED AND AN ICE BUILDUP AROUND THE DOOR WAS FOUND. THE ICE WAS REMOVED AND THE CARGOSDR AWXA0001452Line · cloggedLAS - AIR TURNBACK - 2/22/01 - ALL LAVS WOULD NOT FLUSH (CIDS PANEL RED LIGHT WAS ON, WASTE AT 0 PERCENT FULL, WATER AT 40 PERCENT FULL); AIRCRAFT DESTINATION WAS JFK SO THE FLIGHT RETURNED TO LAS. THE LAV SYSTEM HAD PREVIOUSLY BEEN PLACED ON MEL 38-30-01 FORSDR AWXA0001451Fire Loop · chafedPHX - AIR TURNBACK - 2/22/01 - DURING CLIMB THE CREW GOT A CLASS I ECAM MESSAGE, ENG 2 FIRE DET FAULT AND RETURNED TO PHX. IN PHX MAINTENANCE FOUND THE NR 2 ENG LOWER CORE FIRE LOOP CHAFED; THE LOWER CORE FIRE DETECTOR ASSY WAS REPLACED AND FUNCTIONALLY CHECKSDR AWXA0001420Elevator · damagedON REMOVAL OF RT ELEVATOR ABNORMAL SHEAR LOAD NOTED ON ELEVATOR ATTACH BOLTS AND ELEVATOR HINGE BEARINGS FOUND TO BE MISALIGNED. COMPLIED WITH AWA ER 26-5552-01054-DL2; ELEVATOR REPLACED IAW AMM 27-34-41-401.SDR AWXA0001394Seat Track · corrodedNR 4 SEAT TRACK AT FR 20 CORRODED, -0Y1292 -Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14.SDR AWXA0001395Seat Track · corrodedNR 3 SEAT TRACK AT FR 20 CORRODED, -Y765-Z500. FABED SEAT TRACK IAW DWG D53112092; INSTALLED IAW SRM 53-11-14.SDR AWXA0001374Actuator · contaminatedPHX - EMERGENCY LANDING - 2/12/01 - ON APPROACH, THE CREW GOT AN ECAM WARNING, F/CTL SLATS FAULT AND THE CREW DECLARED AN EMERGENCY; AN UNEVENTFUL LANDING WAS MADE IN PHX. MAINTENANCE TROUBLESHOT AND FOUND 1 LT AND 2 RT LEADING EDGE SLAT ROTARY ACTUATORS WITHSDR AWXA0001373Fmc · failedPHX - DIVERTED FLIGHT - 2/14/01 - AFTER TAKEOFF FROM LAS TO BOS THE MCDU FROZE IN THE FLIGHT PLAN MODE; RNAV UNAVAILABLE; THE FLIGHT WAS DIVERTED TO PHX. IN PHX MAINTENANCE REPLACED THE LEFT AND RIGHT FMGC; AFTER REPLACEMENT, CURRENT NAV DATA WAS UPLOADED ANDSDR AWXA0001340Hydraulic System · lowSEA - EMERGENCY LANDING - 2/10/01 - ON DESCENT INTO SEA THE GREEN HYDRAULIC SYSTEM WENT TO LOW LEVEL. IN SEA THE AIRCRAFT WAS INSPECTED AND NO LEAKS FOUND. THE GREEN SYSTEM HYDRAULIC SYSTEM WAS SERVICED TO FULL AND NO FURTHER PROBLEMS REPORTED. THIS WAS THESDR AWXA0001282Resolver · malfunctionedMAINTENANCE TROUBLESHOT IAW TSR 73-22-00-810-851 AND IAE TELEX; CELL CODE FAULT OF 59 ON FMU/HC/EEC 1 MESSAGE; (WFXCF) FUEL FLOW RESOLVER FAULT; CH B ON CONNECTOR J8 HAD HIGH RESISTANCE OF 104 OHMS BETWEEN PINS I & J (NORM: 15-78 OHMS); WIRING CHECKED GOOD; RASDR AWXA0001281Fmu · malfunctionedPHX - AIR TURNBACK - 2/3/01 - DURING INITIAL CLIMB, LEFT ENG UNCOMMANDED THRUST INCREASE ABOVE CLIMB EPR LIMIT WITH DEFINITE YAW TO THE RIGHT; EVENT WAS MOMENTARY AND LEFT EPR WAS NOTICED DECREASING THRU 1.5 BACK TO CLIMB EPR OF 1.3, OTHER PARAMETERS NORMAL. SDR AWXA0001257Actuator · leakingPHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS MADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SESDR AWXA0001248Computer · failedPHX - DIVERTED FLIGHT (1/14/01) - AFTER TAKEOFF FROM LAS, THE FLIGHT CREW EXPERIENCED A DUAL MCDU FAILURE; THEY WERE FROZEN ON RESPECTIVE PAGE AT THE TIME OF FAILURE AND WERE UNABLE TO INPUT DATA. CIRCUIT BREAKER B-1 & N20 WERE RESET WITH NO HELP. CREW SWITCSDR AWXA0001229Circuit Breaker · trippedEMERGENCY LIGHT CIRCUIT BREAKER POPPED IN FLIGHT. PHX MAINTENANCE PER FOR RESET OF CIRCUIT BREAKER; EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD; CIRCUIT BREAKER REMAINED ENGAGED AND NO FURTHER FAULTS NOTED.SDR AWXA0001224Light · damagedFWD LEFT BLKHD EMERGENCY LIGHT INOP AND COVER MISSING. REMOVED AND REPLACED EMERGENCY LIGHT AT FWD LEFT BULKHEAD; LIGHT OPS CHECKS GOOD.SDR AWXA0001202Landing Gear · malfunctionedON LANDING GEAR EXTENSION THE NOSE GEAR SHOWED NOT DOWN/LOCKED; THE PILOT JIGGLED THE HANDLE AND ABOUT 10 SEC LATER THE GEAR THEN SHOWED DOWN AND LOCKED; CREW MADE AN EMERGENCY LANDING. THE PROBLEM WAS TROUBLESHOT IAW TSM 32-31-00 PG.A212 & A213; NO FAULTS WERSDR AWXA0001170Power Supply · failedEXIT SIGNS OVER DOOR 1L & 1R AND FIRST CLASS OVERHEAD DO NOT ILLUMINATE WHEN NO SMOKING SIGN IS OFF. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-38; OPS CHECKED GOODSDR AWXA0001161Power Supply · failedSEVERAL EMERGENCY LIGHTS INOP WITH EMERGENCY LIGHTS ACTIVATED. REPLACED POWER SUPPLY; OPS CHECKED GOODSDR AWXA0001156Rod · stuckSEA - DURING TAXI FLIGHT CONTROL CHECK, RUDDER PEDALS BINDING IN CENTER GOING FROM RIGHT TO LEFT; RETURNED TO GATE. TROUBLESHOT IAW TSM 27-20-00-810-801 FOUND CENTERING ROD STICKING; REMOVED AND REPLACED CENTERING ROD IAW AMMSDR AWXA0001118Link · wornPHX - AIR TURNBACK - AFTER TAKEOFF ON LANDING GEAR RETRACTION THE NOSE GEAR DID NOT RETRACT; ECAM MESSAGE L/G DOOR NOT UPLOCKED/NOSE GEAR SHOCK ABSORBER FAULT; AFTER CYCLING GEAR DOWN CREW HAD 3 GREEN INDICATION; CREW TRIED CYCLING THE GEAR AGAIN PER MAINTENANSDR AWXA0001107Light · inoperativeRIGHT FWD OVERWING ERMERGENCY ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING ESCAPE LIGHT ASSEMBLYSDR AWXA0001019Servo · malfunctionedPHX - AIR TURNBACK - ON CLIMB OUT AND CRUISE AIRCRAFT HAD LEFT WING DOWN 5 TO 7 DEGREES AND RUDDER TRIM 2.8 DEGREES RT. MOST NOTICABLE AT 250 KTS. AND ABOVE; AT 210 KTS. CONDITION LESS NOTICABLE AND AT 170 KTS. FLAP 2 RUDDER TRIM WAS NORMAL AND AIRCRAFT WAS STSDR AWXA0001018Door · leakingCMH - UNSCHEDULED LANDING - ENROUTE FROM EWR TO LAS THERE WAS A LOUD LOW FREQ. NOISE FROM THE RIGHT AFT OVERWING EMERGENCY EXIT AND THE AIRCRAFT DIVERTED TO CMH; ON DESCENT THROUGH 4.3 PSI DIFFERENTIAL PRESSURE THE NOISE STOPPED. IN CMH, THE EMERGENCY EXIT DOOSDR AWXA0000999Computer · inoperativePHX - DURING CLIMBOUT AFTER TAKEOFF, ECAM F/CTL ELAC2 PITCH FAULT IDENTIFIED; RESET ELAC2 BUT FAILED AGAIN APPROX 1 MIN LATER; PERFORMED AIR TURNBACK TO PHX, UNEVENTFUL LANDING.R/R NO.2 ELAC COMPUTER IAW AMM 27-93-34, TEST OK; A/C RETURNED TO SERVICESDR AWXA0000995Connector · inoperativeDURING ROUTINE MAINTENANCE EMERGENCY SEAT LIGHT AT SEAT 15C WAS FOUND NOT WORKING.: MAINTENANCE FOUND WIRES PULLED OUT OF THE CONNECTOR & CONNECTOR BACKSHELL STRIPPED; THE CONNECTOR WAS REPLACED AND THE WIRE RETERMINATEDSDR AWXA0000994Wire · brokenDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT SEAT 24 LEFT WAS FOUND INOP. A NEW TERMINAL END WAS INSTALLED ON THE WIRE, OPS CHECKED GOODSDR AWXA0000908Seat Track · corrodedCABIN SEAT TRACK NR 3 Y765 FRAME 20 CORRODED. REPAIRED IAW SRM 53-00-15 FIG 201.SDR AWXA0000801Condenser · odorVERY BAD DIRTY SOCKS SMELL. BORESCOPED NR 3, 4, AND 7 HPC BLADES, FOUND NO EVIDENCE OF OIL SATURATION. REMOVED AND REPLACED NR 1 A/C PACK CONDENSOR, AIR CYCLE MACHINE, AND OZONE FILTER.SDR AWXA0000797Switch · failedEMERGENCY LANDING, ECAM MSG, BLUE HYDRAULIC RESERVOIR LOW AIR PRESS. REMOVED AND REPLACED LOW PRESS SWITCH 2387GH.SDR AWXA0000796Pump · failedEMERGENCY LANDING, BLUE SYS HYDRAULIC PRESS WENT TO ZERO PSI. REMOVED AND REPLACED BLUE SYS HYD PUMP.SDR AWXA0000746Wire · brokenA/C IN C CHECK, WIRES BROKEN ON EMERGENCY LIGHTS ON SEATS 17 LT, 22 LT, & 26 LT. REPAIRED EMERGENCY LIGHTS PER GMM. CHECKED SERVICEABLE PER MM 33-51-00-501.SDR AWXA0000745Connector · brokenA/C IN C CHECK, ROW 19, LEFT SEAT EMERGENCY LIGHT WIRE BROKEN AT LUG. REPLACED LIGHT CONNECTOR PER MM 20-48-14. CHECKED SERVICEABLE PER MM 33-51-00-501.SDR AWXA0000720Filter · contaminatedTHROUGHOUT FLIGHT STRONG ODOR IN CABIN. REMOVED AND REPLACED OZONE FILTERS. FOUND APU INLET OIL LEAK, APU MEL''D.SDR AWXA0000715Floor Support · corrodedC-CHECK CORROSION, HOLES CORRODED IN AFT CABIN FLOOR SUPPORT FRAME 66, Y919 LT. REMOVED AND REPLACED FLOORBEAM IAW A320 SRM 51-42-11.SDR AWXA0000714Floorbeam · corrodedC-CHECK CORROSION, HOLES CORRODED IN AFT CABIN FLOOR SUPPORT FRAME 66, Y165 RT. FABRICATED NEW BEAM AND INSTALLED IAW DWG D53472282.SDR AWXA0000713Floorbeam · corrodedC-CHECK CORROSION, HOLES CORRODED IN AFT CABIN FLOOR SUPPORT FRAME 66, Y512 LT. CORROSION REMOVED, FOUND BEYOND LIMITS, FABED AND INSTALLED NEW BEAM IAW DWG D53472094010.SDR AWXA0000680Skin · delaminatedC-CHECK, PREVIOUS REPAIRS TO THE LOWER SKIN SURFACE OF THE RIGHT I/B FLAP DISBONDING. REPAIRED IAW A320 SRM 51-77-11, 57-52-00 PARA 8N STEP 4, 57-52-00 PARA 8Q FIG 213 SHEET 3 AND AWA ER 26-5752-00266JSZ.SDR AWXA0000645Handle · crackedAIR TURNBACK, EMERGENCY DECLARED. ON CLIMBOUT, CLASS 1 MESSAGE DISPLAYED CARGO DOOR OPEN. CREW EXPERIENCED PRESSURE CHANGE AND VIBRATION. REMOVED AND REPLACED CARGO DOOR HANDLE ASSY, OPS CK GOOD.SDR AWXA0000644Window · delaminatedAIR TURNBACK, F/O FIXED WINDOW DELAMINATED. REMOVED AND REPLACED WINDOW.SDR AWXA0000615Computer · failedAIR TURNBACK - NORTH OF ICT, AFTER NR 1 IR FAULT, CAPTAINS PFD WENT BLANK AND NR 1 AUTO PILOT DISCONNECTED WITH A THRUST LOCK. REGAINED PFD APPROX 2 - 3 SEC LATER. REMOVED AND REPLACED FLIGHT AUGMENTATION COMPUTER.SDR AWXA0000612Floorbeam · corrodedC-CHECK CORROSION, AFT CABIN FLOOR PANEL FLOORBEAM 66 STR Y 1292 RT CORRODED. FABRICATED NEW FLOORBEAM IAW DWG D53472090 AND INSTALLED IAW A320 SRM 51-72-11 PAGE 1.SDR AWXA0000611Seat Track · corrodedC-CHECK CORROSION, CABIN FLOOR PANEL SUPPORT Y1292 RT FRAME 20 CORRODED. NEW FLOOR SUPPORT FABRICATED IAW DWG D53112815 AND INSTALLED IAW A320 SRM 51-72-11.SDR AWXA0000610Floor Support · crackedC-CHECK, LT AFT CABIN FLOOR SUPPORT FRAME 68 STR 1732 WEB CRACKED. FABRICATED NEW WEB IAW DWG D53480020436, INSTALLED IAW A-320 SRM 5.SDR AWXA0000609Seat Track · corrodedC-CHECK CORROSION, NR 4 SEAT TRACK FRAME 31.5 FRETTED. REPAIRED IAW A320 SRM 53-00-15 PG 202 FIG 201.SDR AWXA0000608Floor Support · corrodedC-CHECK CORROSION, LT AFT CABIN FLOOR SUPPORT FRAME 66 STR Y1292 LT TO FRAME 69 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW A320 SRM 53-41-14 PG 34.SDR AWXA0000607Floor Support · corrodedC-CHECK CORROSION, CABIN FLOOR PANEL SUPPORT Y254 LT FRAME 20 CORRODED. REPAIRED UPPER FLANGE OF Y254 LT FLOOR SUPPORT IAW A-320 SRM 53-00-14 PG 20.SDR AWXA0000606Web · crackedC-CHECK, RT AFT CABIN FLOOR SUPPORT FRAME 68 STR 1732 RT WEB CRACKED. FABRICATED AND INSTALLED NEW WEB AS PER DRAWING D53480020437.SDR AWXA0000605Seat Track · corrodedC-CHECK CORROSION, AFT FLOOR PANEL SUPPORT FRAME 66 STR Y925 LT, FLT ATTENDANT SEAT ATTACH POINT CORRODED. REMOVED AND REPLACED BEAM IAW A320 SRM 51-72-11.SDR AWXA0000604Seat Track · corrodedC-CHECK CORROSION, NR 3 SEAT TRACK AT FRAME 20R Y-765 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 51-42-11, FAB''D REPLACEMENT PART IAW DWG D53112782.
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