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 engine_model_key = 'CF650C2' 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 engine_model_key = 'CF650C2' 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 CA020215011Fuel Line · broken(CAN) WHILE IN CRUISE THE #1 ENGINE SHUTDOWN BY ITSELF. COULD NOT RE-START THE ENGINE. CAPTAIN DECIDED TO LAND IN HOUSTON, TEXAS. MAINTENANCE FOUND A BROKEN FUEL LINE ON THE MEC GOING TO VARIABLE STATOR ACTUATOR.SDR 02FDEA00088Engine · malfunctionedAT CLIMB NR 3 ENG COUGHED AND ROLLED BACK N1 TO 35 PERCENT AND N2 50 PERCENT. EGT BEGAN TO RISE 800 DEG. SHUTDOWN ENG.SDR WRLA200201Blade · vibrationNR 1 ENGINE VIBRATION 80-95, ALL OTHER INDICATIONS NORMAL. EVENT OCCURRED AT THE TOP OF THE CLIMB SEGMENT WHEN THE FLIGHT AS THE CREW WAS LEVELING THE AIRCRAFT. THE CAPTAIN ELECTED TO RETURN TO MIA. LUBED FAN BLADES, PERFORMED MAX POWER RUN AT 80-95 PERCENTSDR G6OA064Engine · flamed outNR 3 ENGINE FLAMED OUT AT CRUISE. AFTER TROUBLESHOOTING NR 3 ENGINE, REMOVED AND REPLACED NR 3 ENGINE FUEL FILTER ELEMENT PER MM 73-11-02. REMOVED AND REPLACED NR 3 FUEL PUMP PER MM 73-12-01. REMOVED AND REPLACED MEC UNIT ON NR 3 ENGINE PER MM 73-20-01. PESDR CA020228011Panel · separated(CAN) THIS IS BRIEF DESCRIPTION OF EVENTS LEADING UP TO INCID. OF PANEL 691AT, LOCATED ON RT UPPER WING, EXITING A/C MSN 183 AT TAKEOFF ON 8 DEC 2001.ON 11 NOV 01, PANEL REMOVED TO PERFORM INSP OF LOW SPEED AILERON HINGEBOLTS FOR CORROSION. INSPECTION COMPLETESDR CNMA200100035Duct · blownENGINE FIRE INDICATION ON TAKEOFF CLIMBOUT 2 APPROX 400 FT AGL ON NR 3 ENGINE. COMMENCE ENG FIRE SEVERE DAMAGE CHECKLIST PERFORMED. FIRE INDICATION WENT OUT. DUMPED APPROX 29,000 LBS FUEL AND RETURNED TO LICZ. FOUND 14TH STAGE BLEED DUCT BLOWN.SDR CA010829003Line · leaking(CAN) YELLOW SYSTEM HYDRAULIC FLUID LOSS, FOUND ON ARRIVAL BY MAINTENACE PERSONNEL. FLUID LOSS FROM FLEX LINE FITTING. LINE REMOVED AND SYSTEM CAPPED, LEAK CHECKED AND PLACED ON MEL FOR LINE REPLACEMENT.SDR CA010828008Sensor · failed(CAN) ON 3 OCCASIONS AUGUST 24, 2000, SEPT 13 2000, AND SEPT 20 2000 "ALPHA FLOOR" (MAX AUTO THROTTLE) WAS ENGAGED ON APPROACH AND DEPARTURE. PROBLEM WAS INTERMITTANT AND TROUBLESHOOTING LEAD TO AOA SENSOR. SENSOR REPLACED, PROBLEM CLEARED.SDR CA010823006Indicator · contaminated(CAN) AIRCRAFT ABORTED TAKEOFF FOR NO AIRSPEED INDICATION ON CAPTAIN'S SIDE. DEBRIS FOUND IN CAPTAIN'S PITOT TUBE. DEBRIS REMOVED AND PITPT CHECK AND AIR DATA COMPUTER CHECK CARRIED OUT. NO FAULTS FOUND AND AIRCRAFT RETURNED TO SERVICE.SDR CA010823008Fuel Cell · leaking(CAN) DURING THE PREFLIGHT INSPECTION, A HEAVY FUEL LEAK WAS NOTICED ON THE RT LOWER WING SURFACE OUTBOARD OF THE PYLON. THE FUEL WAS LEAKING ON TO THE TAIL CONE OF THE EXHAUST AREA OF NR 2 ENGINE. THE NR 2 FUEL TANK WAS DEFUELED AND A NEGATIVE PRESSURE CHECSDR CNMA200100028Wire · brokenNR 2 ENG OIL TEMP HIGH AFTER TAKEOFF, ENG SHUTDOWN. REPAIRED BROKEN WIRE AT ADEL CLAMP ON ENG IAW 20-30-01. ENGINE GROUND RUN, OPS CHECKED OK.SDR M8B2001F00000Bolt · shearedPRE DEPARTURE CHECKS FOUND RIGHT MAIN LANDING GEAR AFT AXLE BOLT HAD HEXAGONAL HEAD SHEARED OFF. PROBABLE CAUSE: FATIGUE, STRESS.SDR XNA01009Engine · malfunctionedLOUD BANG RIGHT ENGINE AT 16000 FT. EGT WENT TO RED LINE. SHUT ENGINE DOWN AT 06:12 Z.SDR CA010510006Sleeve · worn(CAN) SLATS WOULD NOT EXTEND DUE TO HIGH TORQUE REQUIRED TO ACTIVATE THE BALL SCREW.PROBABLY CAUSED BY POOR LUBRICATION LEADING TO WORN SLEEVE.SDR CNMA200100013Clamp · looseAFTER TAKEOFF, NR 3 ENGINE FIRE WARNING ILLUMINATED AT CRUISE POWER. REDUCED POWER AND INDICATION CEASED. ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT ENGINE DOWN. RETURNED TO ORIGINATING AIRPORT. INSPECTED ENGINE. FOUND LOOSE CLAMP ON PNEUMATIC DUCT AT TURSDR 01FDEA00301Compressor · stalledNR 1 ENG SHUTDOWN IN FLT DUE TO COMPRESSOR STALLS DURING PWR REDUCTIONS.SDR CA010510007Clamp · broken(CAN) - ON TAKEOFF REW NOTICED 3/4 KNOB THROTTLE STAGGER. - DURING CLIMB NR 2 ENGINE LOOP B LIGHT ON. - IN CRUISE NOTICED NACELLE TEMP RISING.- UPON LANDING FOUND NR 2 ENGINE T/R BLOW OUT PANEL HANGING DOWN. - NR 2 CORE COWLS OPENED, FOUND REMAINS OF CLAMP IN SDR 0101341232Transmitter · faultyDURING TAKEOFF ROLL, THE NR 1 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER AND THE OIL PRESSURE INDICATOR. AN ENGINE RUN WAS PERFORMED TO HSDR 20010427CW003Engine · contaminatedDURING A CHECK, BOROSCOPE INSPECTION, FOUND METAL AT TAILPIPE OF NR 2 ENGINE. METALLURGICAL ANALYSIS IDENTIFIED METAL TO BE INCONEL 718 AND SUGGESTED POSSIBEL SOURCE TO BE FROM LPT INTERSTAGE SEALS.AMOUNT OF METAL WAS SIGNIFICANT AND OEM RECOMMENDED ENGINSDR 20010427CW004Pulley · brokenAFTER LANDING , FLIGHT ENGINEER NOTICE RT DROOPED LEADING EDGE NOT RETRACTED AND FLUSHED WITH ADJACENT SLAT SURFACES. FOUND SUBJECT PULLEY BROKEN, CAUSING NR 2 SLAT EXTEND/TIE CABLE DISLODGED. ALL OF THE NR 2 SLAT CABLES WERE REPLACED DURING C CHECK AND PULLSDR 2001UALA00075Slide · failedDOOR 4 LEFT SLIDE PRESSURE LIGHT ON. CHECK OF SLIDE PRESSURE WITH OHM METER SHOWS 0 WHICH IS A BAD SLIDE. *S/D* THE SLIDE FROM AC 3056 WAS ROBBED AND INSTALLED ON AC 3058. WHEN 3058 LATER RETURNED TO ORD, THE SLIDE WAS REMOVED, A SERVICEABLE SLIDE WAS INSTSDR 2000UALA00796Battery Pack · inoperativeESCAPE SLIDE PRESSURE WARNING LIGHT CAME ON AT 4R. *S/D* THE ESCAPE SLIDE PRESSURE WARNING LIGHT WAS FALSELY ILLUMINATED DUE TO CORROSION ON REMOTE PRESSURE INDICATOR BATTERY PACK. A VISUAL INSPECTION OF THE BATTERY PACK CONFIRMED THE PRESENCE OF CORROSION SDR 20010112CW001Control Cable · brokenFOUND NR3 SLAT NOT FULLY RETRACTED AT LANDING, DROOPED APRX 2IN. ON INSP NR3 SLAT RETRACT CABLE SNAPPED OFF/DETACHED FROM SWG TERM.COCKPIT INDICATION LTS SHOWED NORMAL. REPLACED WITH THICKER TYPE CABLE TO IMPROVE CABLE RELIABILITY.SDR 2000UALA00725Engine · malfunctionedVIB IN FLR OF ACFT INTNSTY VARIES W/NR 1 ENG SPD. TAFI 71-00 HB VIBRATN IN FLR-INTENSTY VARIES W-SPED ENG NR 1CRZ ACP CHRNIC REVIEW. LOG: VIBRATN FELT IN FLR OF ARCFT -INTNSITY VARIES W/SPEED OF NR 1 ENG. BLEEDS OFF IDLE ENG READINGS NR 1 = 81.5% N1, 560 EGT,SDR 20001212SH002Damper · damagedLAX - FLT TA809 - DURING TAKEOFF, THE LANDING GEARS DID NOT RETRACT, EITHER SYSTEM NR 1 AND NR 2. DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO LAX AIRPORT AND OVERWEIGHT LANDING PERFORMED. MAINTENANCE TECHNICIANS PERFORMED A COMPLETE INSPECTION OF THE LANSDR CA001228028Line · ruptured(CAN) ON LANDING FLUID LOSS IN YELLOW SYSTEM. HYDRAULIC LINE FOUND RUPTURED IN RT WHEEL WHEEL. LINE REPLACED AND FLUID REPLENISHED.SDR CA001207025Warning System · failed(CAN) IMMEDIATELY FOLLOWING MAIN WHEELS LEAVING THE GROUND STICK SHAKERS AND STALL WARNING ACTIVATED. CREW CONTINUED WITH TAKEOFF, THE AIRCRAFT RETURNED TO AIRPORT. CREW REPORTED THAT DURING SLAT RETRACTION THAT THEY COULD NOT FULLY RETRACT THE SLATS (DUE TSDR CA001207022Fan · inoperative(CAN) DUE TO COOLING DIFFICULTIES A TEMPORARY LOSS OF COMMUNICATION ON COMM NR 1 AND COMM NR 2 WAS EXPERIENCED ON APPROACH INTO YVR FOR APPROXIMATELY 15 MINUTES.SDR CA001128018Relay · failed(CAN) AIRCRAFT ARRIVED ATDESTINATION WITH NO REVERSERS AND NO ANTI SKID. WEATHER AT THE TIME WAS HEAVY RAIN AND FOG. CAPTAIN CALLED FIRE DEPARTMENT FOR HOT BRAKES. WHEELS INSPECTED AFTER COOLING, FOUND #2 AND #8 FUSE BLOWN WHILE AIRCRAFT PARKED.- FOUND LANDINGSDR CALA0001692Duct · blownTHE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING TAKEOFF FROM IAH. THE NR 1 NACELLE TEMP WENT TO 300 DEGREES AND THE NR 1 THRUST REVERSER VALVE OPEN LIGHT CAME ON. POWER WAS REDUCED TO JUST ABOVE IDLE AND THE FIRE WARNING LIGHT EXTINGUISHED. FUESDR CA001019015Pitot Tube · contaminated(CAN) AIRCRAFT HAD A REJECTED TAKEOFF DUE TO NO INDICATION ON THE F/OS AIRSPEED INDICATOR. THE TROUBLESHOOTING HAD FOUND A WASP NEST INSIDE THE PITOT TUBE. THE PITOT TUBE WA DISCONNECTED AND THE NEST WAS BLOWN OUT. THE PITOT TUBE WAS RECONNECTED AND A PITOT STSDR UIEA00045Duct · leakingMIA/BOG -ATB - FLT GT063/06 - ENGINE A-LOOP FIRE WARNING FLUCTUATED, B-LOOP READ 4-5 STEADY. ENGINE SHUT DOWN AND FLIGHT RETURNED TO MIA. MIA MAINTENANCE FOUND PRESSURE REGULATOR VALVE AND DUCT LEAKING. REPLACED BOTH PRV, DUCT AND CLAMPS. OPERATIONAL CHECKSDR CA001013031Apu · failed(CAN) APU WAS BELCHING OUT SMOKE AND FLAMES. APU OIL LEVEL SHOWED NO INDICATION. APU SHUTDOWN BY FLIGHT CREW. MAINTENANCE INSPECTED TURBINE AND EXTERIOR OF APU PLUS AIRCRAFT STRUCTURE FOR ANY SIGNS OF DAMAGE. NO DEFECTS WERE FOUND. APU SERVICED WITH 8L OF OIL.SDR CA001128013Pitot Tube · clogged(CAN) - F/O AIRSPEED INDICATOR FROZEN AT 60 KNOTS. WHEN ADC TRANSFERRED FROM CAPTAINS ASI, OK. INSPECTED AND DEBRIS REMOVED FROM F/O PITOT TUBE, PITOT STATIC TEST DONE PER M/M 34-11-10, F/OS ASI FUNCTION TESTS NORMAL ON ALL PARAMETERS.SDR 2000UALA00575Clamp · failedABORTED TAKEOFF AT 90 KTS ACCOUNT NR 1 ENG PROBLEM. *S/D* ENG FAILURE LIGHT ON. FOUND NR 1 ENGINE HI-STAGE BLEED VALVE CLAMP BLOWN OFF AT DUCT TO HIGH STAGE VALVE INTERFACE. EXTENSIVE DAMAGE TO SURROUNDING AREA REVERSER BLANKETS. ATTACH CLAMP WAS INSTALLESDR DHLA200036715Engine · overheatedON T/O THE EGT ON BOTH ENGINES WENT OVER 945. THE NR 1 ENG WENT TO 952, THE NR 2 ENG WENT TO 962. THE N1 COMPUTER CALLED FOR 113-5 PERCENT. THE N1 AT 111-0 AT THESE TEMPS. THE TEMP WAS OVER 945 FOR 45 SECONDS. PERFORMED VISUAL INSPECTION ENG''S 1 & 2, NO SDR 2000UALA00492Oven · smokeNR 2 LOWER GALLEY OVEN STARTED SMOKING. *S/D* A BURNT PIECE OF PAPER IN THE NR 2 LOWER GALLEY OVEN WAS THE CAUSE OF SMOKE. THE BURNT PAPER WAS REMOVED FROM THE OVEN AND OPS CHECKED GOOD, NO SMOKE.SDR 00FDEA00522Engine · failedAFT DEPARTURE, NR 3 ENGINE ROLLED BACK TO IDLE. VIBRATION SOON AFT T/O AND CONTINUE UNTIL ENGINE FAILED. *S/D* REMOVED AND REPLACED PER MM 73-20-01-2.SDR 2000UALA00533Duct · failedFROM OBSERVER ON GROUND, DURING INITIAL CLIMBOUT, WHITE SMOKE OBSERVED COMING FROM THE NR 2 ENGINE AND METALLIC OBJECT DEPARTED AIRCRAFT FROM THE AREA OF NR 2 ENGINE. HAD NR 2 ENGINE FIRE WARNING FOR ABOUT 10 SECONDS. ENGINE SHUT DOWN. DUMPING FUEL IN PREPASDR 00FDEA00524Engine · failedAFT DEPARTURE NR 3 ENGINE FAILED, CKLIST PERFORMED, RETURN TO LAX. NOTED VIBRATION AFT T/O CONTINUE UNTIL ENGINE FAILED. *S/D* ACCOMPLISH BORESCOPE ON NR 3 ENG IAW W/C 72X3503, NO DEFECTS NOTED. ENGINE IS SERVICEABLE.SDR 2000UALA00457Bolt · failedREPORTED LOUD BANG WHEN LANDING GEAR EXTENDED. ALL INDICATIONS NORMAL. LANDING NORMAL. AFTER BLOCKING OBSERVED LANDING GEAR DOORS DAMAGED. *S/D* THE CENTER GEAR RETRACT ACTUATOR LOWER BOLT (P/N: AYG7257-1) FAILED. THE CENTER GEAR FREE-FELL AT EXTENSION, SDR UIEA0032Warning System · activatedFLT GT051 - ATB - DURING CLIMB-OUT AT APPROX 5500 FT, NR 3 ENGINE A AND B FIRE WARNING LOOPS PEGGED HIGH. LEVEL OUT AND REDUCED POWER AND FIRE WARNING INDICATION WENT OUT. ACCOMPLISHED ENGINE FIRE CHECKLIST AND SHUTDOWN ENGINE. DID NOT DISCHARGE FIRE BOTTLESSDR 20001004AP001Engine · bird strikeSJO-MIA - FLT TA820 - AFTER TAKEOFF, PILOTS NOTICED A BIRDSTRIKE ON THE ENGINE NR 1, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO SAN JOSE AIRPORT. AFTER AN UNEVENTFUL LANDING, MAINTENANCE TECHS PERFORMED VISUAL INSPECTION ON THE ENGINE NR 1 AS PER AMM 05-5SDR CA000614020Bracket · broken(CAN) AFTER LIFT OFF CREW HEARD LOUD BANG AFTER SELECTED LDG GEAR UP. BOTH MAIN GEAR WENT UP & LOCKED INTO POS. NOSE GEAR DID NOT GO UP & NOSE GEAR DOOR IND. LIGHT REMAINED ON. DURING CLIMB OUT SEVERE VIBRATION COMING FROMNOSE OF A/C. AFTER GETTING INSTRUCTIONSDR 2000UALA00299Unknown · odorCREW VERBAL REPORT OF POOR AIR QUALITY IN FIRST CLASS CABIN. AIRCRAFT DIVERTED INTO DEN WITH 3 ILL FLIGHT ATTENDANTS COMPLAINING OF BREATHING DIFF. ALL LOCATED IN FIRST GALLEY. *S/D* PER VERBAL FROM CABIN CREW, ACTUAL PROBLEM WAS IN LOWER GALLEY. SEVERASDR 2000UALA00241Light · misrepairedEMERGENCY DISARMED LIGHT INOP. *S/D* THE EMERGENCY LIGHT DISARMED LIGHT (ELDL) WAS LAMPED INCORRECTLY. RELAMPED THE ELDL AND THE ELDL OPERATED WITHOUT ANY INCIDENT.SDR CA000516025Switch · out of adj(CAN) ON DECENT, A PRESSURIZATION BUMP WAS FELT ACCOMPANIED WITH AIRFRAME VIBRATION, NOISE, MASTER WARNING DOOR WARNING, AND FWD CARGO LIGHT ON.EMERGENCY DECLARED AND SUBSEQUENTLY CANCELLED, AIRCRAFT LANDED. INVESTIGATION REVEALED A MICROSWITCH ON THE ACCESS DSDR CA000427027Heat Exchanger · ruptured(CAN) FUEL OIL HEATER FAILED INTERNALLY CAUSING FUEL TO CONTAMINATE THE OIL SYSTEM AND EXIT SPINNER AND NOSE COWL. THE OPERATOR EXPRESSED THAT THIS IS NOT A COMMON OCCURENCE AND THAT THIS WAS SUSPECTED TO BE THE RESULT OF TSN IN SERVICE OF THE APPLIANCE AND THSDR CA000427026Jackscrew · jammed(CAN) SLATS JAMMED IN RETRACTED POSITION. NR 1 SLAT ACTUATOR FOUND TO BE TRIPPING TORQUE LIMITER AT MID STROKE OF RANGE REPLACED UNIT.SDR 20000424AP002Packing · damagedMIA - FLT TA823 - DURNG TAKEOFF, THE AIRCRAFT LOST ALL OF BLUE HYDRAULIC SYSTEM FLUID. THE AIRCRAFT RETURNED TO MIA AIRPORT FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE TECHS FOUND THE BLUE SYSTEM HYDRAULIC PRESSURE SWITCH PACKING DAMAGED. THE
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