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 = 'CF7002D2' 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 = 'CF7002D2' 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 DKAA01013Engine · flamed outRIGHT ENGINE FLAME OUT DURING CLIMB IN TURBULENCE THROUGH FL390, 210 KTS IAS TEMP DROPPED TO 200 DEGREES C, ANTI-ICE, IGNITION OFF, 10 MINUTES UNTIL RELIGHT, OIL PRESSURE 20 PSI. RESTARTED ON FIRST TRY AT FL290. CHECKED RIGHT ENGINE FOR FOD AND CHECKED TURBISDR CA010530010Inverter · shorted(CAN) CABIN PRESSURIZATION IS AC POWERED FROM NR 1 INVERTER. WHEN NR 1 INVERTER FAILED, THE CREW HAD INDICATIONS IN THE COCKPIT OF LOSS OF PRESSURIZATION AND NR 1 INVERTER. THE CREW DID NOT SELECT THE STANDBY INVERTER TO THE NR 1 POSITION, WHICH RESULTED IN A SDR CA010507014Bearing · seized(CAN) UPON LANDING IN MONCTON, PILOT IN COMMAND NOTICED ABNORMAL BRAKING FROM RT SIDE . AFTER A/C SHUTDOWN FLIGHT CREW REPORTED TO MAINTENANCE NR 4 WHEEL ASSEMBLY DISLOCKED. IT WAS DETERMINED BY MAINTENANCE INSPECTION THAT A BEARING FAILURE HAD OCCURRED. THE BSDR 20010426CW014Drive Shaft · brokenAT FL310 A SUDDEN LOSS OF POWER, FLAME OUT AND OIL PRESSURE, FUEL PRESSURE, HYDRAULIC PRESSURE, WARNINGS. OPERATOR SUSPECTS FAILURE OF HORIZONTAL GEARBOX DRIVE SHAFT. EMERGENCY LANDING.SDR GXPA0102Cooler · leakingDUE TO LOW OIL PRESSURE NR 1 ENGINE SHUT DOWN IN FLIGHT AND DIVERTED. FOUND NR 1 ENGINE FUEL / OIL COOLER LEAKING. REMOVED AND REPLACED NR1 ENGINE FUEL / OIL COOLER. LEAK AND OPS CHECK . NO DEFECTS NOTED AT THIS TIME.SDR CA001027002Compressor Wheel · fod(CAN) ON APPROACH, FOUR MILES OUT, INTO REGINA, SASK, THE CREW NOTICED A SUDDEN POWER SURGE ON THE RIGHT HAND ENGINE. THE RIGHT ENGINE WAS SURGING FROM 83% TO 65% CONTINUOUSLY WITH A TEMPERATURE FLUCTUATION. THE CREW REDUCED POWER AND CONTINUED THE APPROACH, LSDR CA001123014Bracket · broken(CAN) APPROACH TO YUL A/C DEPLOYED LANDING GEAR AND HAD 3 GREEN DOWN & LOCKED INDICATION BUT ONLY TWO (2) GEAR DOOR OPEN LIGHTS EXTINGUISHED, LT GEAR DOOR LIGHT REMAINED ILLUMINATED, CREW CYCLED GEAR UP AND LT GEAR DOOR LIGHT REMAINED ILLUMINATED.CREW SELECTESDR CA001019007Pump · contaminated(CAN) ON LDG LT ENGINE OIL PRESSURE FLUCTUATED FROM 10-50 LBS & OIL LOW PRESSURE WARNING LAMP FLASHED ON ONCE, CREW SHUTDOWN ENGINE & TAXIED TO HANGAR. MAINT FOUND LARGE AMOUNT OF OIL ON INTERNAL SIDE OF COWLINGS. TROUBLESHOOTING REVEALED OIL L EVEL DOWN 3 QTSSDR CA000907026Pipe · ruptured(CAN) CREW REPORTED FLOOR HEAT AND WINDOW DEFOG SYSTEMS INEFFECTIVE/LOW FLOW. TROUBLESHOOTING REVEALED HOT AIR PIPE RUPTURED AT BEND ABOVE L/H WHEEL WELL UNDER L/H WING ROOT FAIRING. HOT AIR PIPE REPLACED AND AREA INSPECTED FOR HEAT DAMAGE NONE FOUND. AIRCRAFTSDR Y2PA00040Engine · fodMCI - FLT 91473 - AT FLIGHT LEVEL 310, NR 2 ENGINE FLAMED OUT. CREW DECLARED AN EMERGENCY, PERFORMED ENGINE FAILURE CHECK LIST AND DESCENDED TO FL 220. AFTER RE-LIGHT, CREW SECURED FROM THE EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT AT MCI. MAINT INSPECTSDR 20000712SH044Blade · fracturedTWO EACH STAGE 1 TURBINE BLADES FRACTURED AND LIBERATED THE TOP ONE-THIRD OF THE AIRFOIL CAUSING DAMAGE TO THE 2ND STAGE BLADES AND AFT FAN SECTION. SUBMITTER STATED INSUFFICIENT INSPECTION INFORMATION EXISTS I N THE ENGINE MANUAL TO DETECT THINNING/NECKING OSDR 20000712SH045Blade · fracturedTWO EACH STAGE 1 TURBINE BLADES FRACTURED AND LIBERATED THE TOP ONE-THIRD OF THE AIRFOIL CAUSING DAMAGE TO THE 2ND STAGE BLADES AND AFT FAN SECTION. SUBMITTER STATED INSUFFICIENT INSPECTION INFORMATION EXISTS I N THE ENGINE MANUAL TO DETECT THINNING/NECKING OSDR Y2PA00032Engine · malfunctionedMLU - FLT 88310 - LT, RT ENG FLAMED OUT FL 290. CREW REPORTED APPROX 20 MILES WEST MLU, TURNED LEFT TO DEVIATE FOR LOCAL LEVEL 3, 4 CELLS. ENTERED MODERATE/HVY RAIN, ENG/AIRFRAME ANTI-ICE ON. SELECTED IGNITERS ON. WHILE IN THE RAIN, LT ENG SPOOLED DOWN, THESDR 20000908SH017Engine · malfunctionedMLU - FLT 88310 - LT, RT ENG FLAMED OUT FL 290. CREW REPORTED APPROX 20 MILES WEST MLU, TURNED LEFT TO DEVIATE FOR LOCAL LEVEL 3, 4 CELLS. ENTERED MODERATE/HVY RAIN, ENG/AIRFRAME ANTI-ICE ON. SELECTED IGNITERS ON. WHILE IN THE RAIN, LT ENG SPOOLED DOWN, THESDR 20001113SH015Engine · fodTRI - NR 2 ENGINE HAD FOD. REPLACED NR 2 ENGINE. (X)SDR CA000713008Ignition Lead · separated(CAN) DURING ROUTINE MAINTENANCE, THE IGNITION LEAD WAS REMOVED FROM THE IGNITOR PLUG TO FACILITATE REPLACEMENT OF THE PLUG. IT WAS NOTED THAT THE LEAD WAS STUCK IN THE PLUG. REMOVAL OF THE LEAD CAUSED THE PIN TO BECOME DETECHED FROM THE ASSEMBLY. THE LEAD WASSDR 20000524SH011Engine · flamed outLEFT ENGINE FLAMED OUT PASSING 34,500 FEET, 250 KNOTS INDICATED AND 1,000 FTM. ENGINE RELIT IN-FLIGHT. REPLACED ENGINE.SDR 20000516SH018Fcu · malfunctionedAIRCRAFT WAS GROUNDED DUE TO PILOT REPORTED SQUAWK THAT ''HIGH ALTITUDE STARTS VERY DIFFICULT FOR BOTH ENGINES IN ADDISON, TX (ADS)''. BOTH SIDE FUEL CONTROLS AND FUEL PUMPS WERE REPLACED. (X)SDR 20000516SH020Pump · failedAIRCRAFT WAS GROUNDED DUE TO PILOT REPORTED SQUAWK THAT ''''HIGH ALTITUDE STARTS VERY DIFFICULT FOR BOTH ENGINES IN ADDISON, TX (ADS)''''. BOTH SIDE FUEL CONTROLS AND FUEL PUMPS WERE REPLACED. (X)SDR 20000516SH021Pump · failedAIRCRAFT WAS GROUNDED DUE TO PILOT REPORTED SQUAWK THAT ''HIGH ALTITUDE STARTS VERY DIFFICULT FOR BOTH ENGINES IN ADDISON, TX (ADS)''. BOTH SIDE FUEL CONTROLS AND FUEL PUMPS WERE REPLACED. (X)SDR CA000301012Rivet · popped(CAN) FOUND 3 RIVETS POPPED ON PRESSURE BULKHEAD FRAME 33 BETWEEN STRINGER 5-6 RIGHT SIDE.SDR CA000301013Rivet · damaged(CAN) FOUND 3 RIVETS POPPED ON PRESSURE BULKHEAD FRAME 33 BETWEEN STRINGER 5-6 LT SIDE.SDR AU000203018Switch · froze(AU) THE NOSE GEAR GREEN (DOWN AND LOCKED) INDICATION LIGHT DID NOT COME ON WHEN THE GEAR WAS SELECTED DOWN. THE CREW PERFORMED AN EMERGENCY EXTENSION AND THE LIGHT FAILED TO ILLUMINATE. AFTER AN UNEVENTFUL LANDING, THE MAINTENANCE CREW FOUND THE SWITCH ON TSDR CA000203018Downlock Switch · frozen(CAN) THE NOSE GEAR GREEN (DOWN AND LOCKED)INDICATION LIGHT DID NOT COME ON WHEN THE GEAR WAS SELECTED DOWN. THE CREW PERFORMED AN EMERGENCY EXTENSION AND THE LIGHT FAILED TO ILLUMINATE. AFTER AN UNEVENTFUL LANDING THE MAINTENANCE CREW FOUND THE SWITCH ON THE SDR CA000118031Carbon Seal · leaking(CAN) OIL SMOKE ENTERING VIA BLEED AIR SYSTEM.SDR CA000118032Actuator · failed(CAN) THE CONDITIONING VALVE(23D) FAILED TO OPEN AFTER TAKEOFF. THE CABIN FAILED TO PRESSURIZE AS A RESULT. MAINTENANCE FOUND THE CONDITIONING VALVE ACTUATOR MOTOR JAMMED DUE TO A FAILURE OF ONE OF THE LIMIT SWITCHES. THE MOTOR HAD BEEN REPLACED 3 DAYS PREVIOUSDR GXPA99007Fcu · out of adjustNR 1 ENGINE FLAMED OUT AT ALTITUDE. FLAMED OUT ABOVE 29,000 FEET. ADJUSTED FUEL DENSITY, GROUND RUN AND TEST FLIGHT. CHECKED GOOD. (X)SDR CA991230045Duct · cracked(CAN) DURING SCHEDULED MAINTENANCE THE HEAT EXCHANGER DUCT WAS FOUND CRACKED. IT HAD BEEN REPLACED 188 HOURS PREVIOUSLY.SDR CA990927068Wire · melted(CAN) AFTER READING A SERVICE DIFFICULTY REPORT IN 'AVIATION MAINTENANCE' MAGAZINE, AN INVESTIGATION OF THE GROUND POWER PLUG CONNECTIONS REVEALED THE POSITIVE CABLE ON THE PLUG TO BE BURNED AND MELTED. THE PLUG PINS AND CONNECTIONS SHOWED NO SIGN OF DAMAGE.SDR CA990915077Retainer · cracked(CAN) DURING MAINTENANCE GEAR SWING, IT WAS NOTED THE LEFT MLG ACTUATOR WAS LEAKING. UPON INSPECTION THE PACKING, RETAINER HAD COME OUT OF THE END OF THE ACTUATOR. PARTS SENT TO DASSAULT AND NEW ACTUATOR INSTALLED.SDR 99ZZZX1563Blucket · failedRECEIVED SLIP IN ENGINE WITH FOD IN THE FAN AND COMPRESSOR SECTION. THE FOD APPEARS TO BE CAUSED BY SEPARATION OF FAN BLADE (S/N 779CE) IN THE HOT SECTION PART OF THE BLADE. THE FAN BLADES ARE EDDY CURRENT INSPECTED AT EACH HOT SECTION (1,000 HOURS). THE LASDR CA990412020Pump · making metal(CAN) ON CLIMB-OUT, NR 1 ENGINE DID NOT RESPOND TO POWER SETTING TO CLIMB POWER. AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST-FLIGHT INVESTIGATION FOUND THE NR 1 ENGINE FUEL PUMP WAS MAKING METAL WHICH CONTAMINATED THE FCU AND THE FUEL NOZZLES PREVENTING FUSDR CA981130003Shaft · sheared(CAN) NR 2 ENGINE FAILED TO START. INVESTIGATION FOUND THE NR 2 STARTER/GENERATOR INTERNAL SHAFT SHEARED. UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THE SUBMITTER STATES THAT THIS IS THE THIRD FAILURE OF THIS NATURE IN THE LAST THREE MONTHS. ASDR 98ZZZX2556Fuel Control · misadjustedFLAME-OUT OCCURRED DUE TO A LOW FUEL DENSITY SETTING. ONCE PROPER DENSITY IS SET, NO FURTHER PROBLEMS OCCURRED.SDR CA970210003Fcu · bad valve(CAN) ENGINE FLAMED OUT DURING TAXI. FCU SENT FOR REPAIR. O/H SHOP FOUND METERING VALVE FAULTY AND UNIT NEEDED NEW SEALS. FCU CALIBRATED, NO OTHER FAULT.SDR CA971003004Duct · puncture(CAN) UNABLE TO MAINTAIN CABIN PRESSURIZATION WHEN ENGINE POWER SETTINGS REDUCED. MAINTENANCE INVESTIGATION REVEALED DUCT CONNECTING WATER SEPARATOR TO FRAME 33 WAS DAMAGED. DUCT REPLACED.SDR CA970530001Seal · damaged(CAN) ON PRIOR INCIDENT, THE AXIS C REAR SEAL ASSY WAS REPLACED. ON SECOND LEG OF NEXT FLIGHT, NR 2 ENG HAD TO BE SHUT DOWN, PREVIOUS SEAL HAD BEEN DAMAGED. NEW SEALS INSTALLED. PART TC: 2.SDR CA970408009Wheel Half · cracked(CAN) DURING A DAILY INSPECTION. AIR WAS NOTICED LEAKING FROM #3 WHEEL BRAKE KEYS. WHEEL ASSEMBLY REMOVED AND SENT FOR NDT. REPORT STATED THAT 2 CRACKS WERE FOUND ALONG BEAD. WHEEL SCRAPPED.SDR GLXPA97009Tube · deterioratedNR 1 ENGINE FLAMEOUT AT FL 330 DURING STEP CLIMB FROM 310 TO 350. AIRSPEED WAS 260 KNOTS. ENGINE RESTARTED AT FL 32.5. BLEED AIR WAS OFF BEFORE FLAMEOUT. REPLACED P2 BELLOWS. OLD ONE WAS FOUND DETERIORATED. ENGINE RUN-UP CHECK GOOD. (X)SDR 97ZZZX1015Engine · power lossPILOT NOTES: AFTER RE-FUEL, THE ACFT LOST PWR ON T/O APPROX 200 FEET AGL. NR 2 ENG EGT WENT RED LINE APPROX 780 DEGREES FAHRENHEIT AND RPM HAD ROLL BACK. A POP WAS HEARD IN THE CABIN BY PASSENGERS. (POSSIBLE COMPRESSOR STALL). PILOT WENT TO FLT IDLE WITH SDR GXPA97004Engine · flamed outNR 1 ENGINE FLAMED OUT AT 33,000 FEET. ENGINE WAS REMOVED AND SENT OUT FOR REPAIR. PROBLEM UNKNOWN AT THIS TIME.SDR HEEA978878Engine · oil leakLEAKING OIL FROM FAN SPLIT LINE.SDR Y2PA96007Engine · flamed outYIP - LT ENG FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FT. A/C DESCENDED AND THE ENG WAS AIRSTARTED PER THE CHECKLIST. A/C RETURNED, AND MADE A NORMAL TWO ENG LANDING. PRIOR TO THIS TEST FLT THE ENG UNDERWENT A HOT SECTION INSPECTION, INCLUDING REPLACESDR CA960916005Flight Computer · failed(CAN) AIRCRAFT CLIMBING THROUGH FL 180, THE AUTO-PILOT FLUTTERED AND DISCONNECTED. A NOTICEABLE BURNING ODOR WAS NOTICED IN THE CABIN. SMOKE WAS NOTED COMING FROM NR 1 FLIGHT COMPUTER. NR 1 FLIGHT COMPUTER FOUND BURNED INTERNALLY. UNIT REPLACED.SDR Y2PA96049Eng · flamed outYIP - THE RT ENG FLAMED OUT DURING PERFORMANCE OF A MAX ALT ACCELERATION TEST. TEST FLT TO PERFORM THIS CHK ON THE RT ENG WAS BEING DONE TO DETERMINE IF PREVIOUS FLAME OUT PROBLEM HAD BEEN RESOLVED, REF MRR Y2PA-96-008. NO EMERG PROCEDURES REQUIRED. A/C RETSDR Y2PA96046Engine · bird strikeYIP - FLT 17211 - BIRD INGESTED DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AT 110 KNOTS. NO EMERGENCY PROCEDURES BEYOND ABORTED TAKEOFF REQUIRED. AIRCRAFT DID NOT BECOME AIRBORNE. ENGINE FAN ROTOR ASSEMBLY BADLY DAMAGED DUE TO BIRD INGESTION. ALL FAN BLADESDR Y2PA96020Scavenge Pump · failedYIP - AFTER T/O AT 13,000, CREW OBSERVED LT OIL PRESS WARN LT FLASH. CHECKING OIL PRESS GAUGE SHOWED LESS THAN 25 PSI. A/C RETURNED TO YIP. ENG WAS SHUTDOWN AND ON CLEARING THE RUNWAY THE TWR REPORTED SMOKE AND SOME FLAMES. THE ENG WAS MOTORED, FLAMES WENTSDR 96ZZZM874Gearbox · stripped fittingWHILE PERFORMING A PREFLIGHT INSPECTION, OIL WAS NOTICED TO BE EXCESSIVELY LEAKING AT OIL SCAVENGE LINE FITTING ATTACHING SCAVENGER LINE TO ACCESSORY GEARBOX. FITTING WAS FOUND TO BE LOOSE. UPON FURTHER INVESTIGATION FITTING WAS FOUND TO BE STRIPPED. ACCESSSDR 96ZZZM308Fuel Pump Filter · crushedYIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUSSDR YIEA96007Low Press Filter · crushedYIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUS
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