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 HAEA202309120274Engine · fodAIRCRAFT DEPARTED LYH-SHV, AT CRUISE ALTITUDE OF FL280 THE LEFT ENGINE EXPERENCED A LOSS OF POWER/FLAMEOUT, THE CREW DECENDED TO FL240 AND PERFORMED A SUCCESSFUL AIR START. AFTER LANDING IN SHV THE ENGINE WAS INSPECTED BY AMERISTAR MAINT AND THEY FOUND FOD DAMSDR 2023F00260Fcu · abnormalAIRCRAFT DEPARTED CHS, SHORTLY AFTER TAKEOFF THE RH ENGINE ROLLED BACK ON POWER. CREW CONTACTED ATC AND RETURNED TO CHS.SDR Y2PA2022090622048Engine · flamed outDISCREPANCY: CREW REPORTED THAT WHILE CONDUCTING ENGINE ACCELERATION CHECKS ON THE #1 ENGINE, THE #1 ENGINE FLAMED OUT AT FL290. THE CREW DECLARED AN EMERGENCY WITH CLEVELAND CENTER TO OBTAIN LOWER ALTITUDE, THEY DESCENDED AND PERFORMED A SUCCESSFUL RELIGHT ATSDR 2020F00028Engine · fodWHILE THE AIRCRAFT WAS ENROUTE AT FLIGHT LEVEL 27000, THE PILOT IN COMMAND NOTICED LIGHT ICE ACCUMULATION. THE PILOT IN COMMAND SELECTED ENGINE AND AIRFRAME DE-ICE SYSTEM ON. A FEW MINUTES AFTER THE DE-ICE SYSTEMS WERE TURNED ON THE LEFT ENGINE BEGAN TO STALLSDR KC8A20190711003Frame · crackedDURING AN EDDY CURRENT INSPECTION REQUIRED PER FAA AD 2017-10-01, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33. BOTH CRACKS ARE LOCATED BETWEEN STRINGERS 5L AND 6L AND STRINGERS 5R AND 6R. SDR EXDA2019F00189Gasket · blew outTHE AIRCRAFT DEPARTED KLRD AND DURING CLIMB OUT THE RIGHT ENGINE FIRE WARNING ILLUMINATED. THE PILOT IN CHARGE REDUCED POWER TO THE RIGHT ENGINE AND BEGAN HIS ENGINE SHUT DOWN CHECK LIST. HE ALSO DECLARED AN EMERGENCY AND ASKED TO RETURN TO KLRD. BEFORE HE SHSDR Y2PA2018112170040Blade · failedCREW REPORTED – AT 34,000 FT LEFT ENGINE EXPERIENCED A LOUD BANG, LOST THRUST, EPR=1.2, EGT=695°, N1=70% AND DEVELOPED A LOUD WHIRRING SOUND. DECLARED EMERGENCY, SOUND AS THOUGH ENGINE WAS OVERSPEEDING. WAS ABLE TO USE ENGINE TO LANDING @ KONT, WITHOUT INCIDESDR 2017FA0000468Engine · power lossAFTER DEPARTING LIT ICING CONDITIONS DEVELOPED AT FL270 THE ENGINE ANTI-ICE WAS ACTIVATED FOLLOWED BY THE AIRFRAME ANTI ICE SYSTEM, SHORTLY AFTER THAT THE NR 1 AND NR 2 ENGINES STARTING LOSING RPM. THE CREW SWITCHED TO AIR START AND AT FL255-250 BOTH ENGINES RSDR Y2PA2017032100004Oil System · low pressureCREW REPORTED AN OIL PRESSURE LIGHT IN FLIGHT. RAN PROCEDURE. ZERO OIL PRESSURE ON TRI-PLEX GAUGE. PERFORMED PRECAUTIONARY SHUTDOWN, DECLARED AN EMERGENCY WITH ATC AND LANDED. MAINTENANCE REPLACED NR 2 ENGINE DUE TO OIL LOSS. REASON FOR LOSS OF OIL IS UNDSDR 2017FA0000074Line · chafedDURING CRUISE THE FLIGHT CREW NOTED THAT THE NR 2 ENGINE ROLLED BACK AND SHUT DOWN IN FLIGHT. DECLAIRED AN EMERGENCY AND DIVERTED. FOUND A FUEL LINE HAD CHAFED TRHOUGH. REPLACED THE LINE AND RETURNED THE AIRCRAFT TO SERVICE.SDR HAEA2016F00035Governor · brokenON DEPARTURE, DURING CLIMBOUT THE CREW NOTICED THE NR 1 EPR HAD DROPPED TO 1.4 AND 600 DEG EGT AND THEY RETURNED. MAINTENACE FOUND THE OVERSPEED GOVERNOR TEST LINKAGE HAD BROKEN, PUTTING THE OSG IN TO GROUND TEST MODE, THE OSG WAS REPLACED AND ALL OPS CHECKS SDR KC8A20151201001Engine · flamed outTHE CREW REPORTED THAT WHILE CLIMBING TO THEIR CLEARED ALTITUDE, THE RT ENGINE FLAMED OUT. THEY DECLARED AN EMERGENCY AND ATC CLEARED THEM TO DESCEND FOR RELIGHT. WITH THE ENGINE RE-STARTED, THEY DIDN’T NOTICE ANY OPERATING ISSUES WITH THE ENGINE AND CLIMBED SDR DJSR20150930001Garlock Seal · deterioratedLOSS OF OIL PRESSURE ON NR 1 ENGINE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. GARLOC SEAL FAILURE CAUSING LOSS OF OIL QUANTITY AND LOSS OF OIL PRESSURE.SDR CA151112004Hose · ruptured(CAN) PILOTS REPORTED LT ENGINE DE-ICE LIGHT ILLUMINATED WITHOUT SYS SELECTION. SCAT TYPE HOSE CONNECTING ENGINE DE-ICE LINES ON LT (OTBD) AREA OF ENGINE FOUND RUPTURED, ALLOWING COMPRESSOR DISCHARGE AIR TO FLOW INTO ENGINE AREA UNDER COWLINGS.SDR CA150223007Cap · cracked(CAN) HYDRAULIC FLUID WAS FOUND LEAKING FROM CAP ON LH HYDRAULIC RESERVOIR, CAP ASSEMBLY WAS REMOVED AND INSPECTED, CRACK FOUND ON UNDERSIDE OF SEALING BLOCK PORTION OF CAP, CAP ASSEMBLY REPLACED.SDR HAEA2014121000230Warning System · activatedWHILE EN ROUTE THE RT ENG OIL PRESS LIGHT KEPT FLICKERING ON & OFF WHILE AT THE SAME TIME THE RT OIL PRESS GAUGE KEPT INDICATING AROUND 5PSI. 40 MINUTES OUT THE OIL PRESS WARNING LIGHT ILLUMINATED STEADY & OIL PRESS REMAINED AT 5 PSI. ENG WAS SHUTDOWN. ACFTSDR Y2PA20120916042Lamp · burned outCREW REPORTED THAT THE LT MLG "GREEN SAFE" LIGHT EXTINGUISHED AT 500' AGL, SHORT FINAL. A MISSED APPROACH WAS EXECUTED. LANDING GEAR WAS CYCLED AND LOWERED WITH PROCEDURE "A". OPERATIONS WAS INFORMED AND DECISION WAS MADE. EMERGENCY DECLARED WITH APPROACH SDR HAEA201000218Audio Panel · defectiveACFT DEPARTED, AFTER TAKEOFF, CREW REPORTED SMOKE IN THE COCKPIT AND THAT THE NR2 COM CIRCUIT BREAKER HAD TRIPPED. ACFT RETURNED TO DEPARTURE. LANDING NORMAL. MX DISCOVERED THE NR2 AUDIO CONTROL PANEL DEFECTIVE. REPLACED DEFECTIVE AUDIO CONTROL. (CLOSED)SDR DJSR20101113A/C Pack · contaminatedON CLIMBOUT, THERE WAS A SMELL OF SMOKE AND THE AIR IN THE COCKPIT APPEARED HAZY. PULLED POWER BACK AND THE AIR CLEARED UP. RETURNED TO DEPARTURE FOR A NORMAL LANDING. SUSPECT OIL IN THE AIR CONDITIONING SYS.SDR HAEA201000217Motor · intermittentTOOK OFF FROM RUNWAY 30, TAKEOFF NORMAL AT 400 FT, V2 + 20 SELECTED FLAPS ZERO. FLAPS STAYED AT 15 DEGREES. CLIMBED TO 4000 FT MSL. ATTEMPTED TO IDENTIFY PROBLEM AND FOUND FLAPS WOULD NOT EXTEND PAST 15 DEGREES. CONTACT TOWER AND ASKED FOR LONGEST RUNWAY. TOWESDR Y2PA2010102600026Control Cable · brokenUPON LANDING, BRAKES WERE NORMAL UNTIL TAXI INTO THE RAMP WHEN BRAKES FAILED IN ALL MODES, PRIMARY, SECONDARY AND EMERGENCY. SHUTDOWN ENGINES AND ROLLED TO A STOP. ACFT WAS CHOCKED. MX WAS SENT AND DISCOVERED THAT THE BRAKE DISTRIBUTOR TELEFORCE CONTROL CASDR Y2PA2010082500017Pressure Sensor · inoperativeON DESCENT NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED. CREW CONDUCTED ABNORMAL OIL PRESS INFLIGHT CHECKLIST. OIL PRESSURE SECONDARY TRIPLEX GAUGE INDICATED 46 PSI AND FOLLOWED THROTTLE MOVEMENT. SHORTLY THEREAFTER OIL PRESSURE BEGAN TO FALL AD ENGINE WAS SHSDR HAEA201000216Unknown · odorCLIMBING THROUGH FL170 CREW REPORTED A FUEL LIKE ODOR. MX INVESTIGATED REPORT AND FOUND NO ABNORMALITIES. ACFT WAS TEST FLOWN AND NO FUEL LIKE ODOR EXISTED. ACFT RETURNED TO SERVICE.SDR HAEA200900212Anti-Ice Valve · vibrationON TRANSITION FROM CLIMB TO CRUISE A FAINT GROWLING NOISE WAS HEARD IN THE REAR OF THE ACFT. WHEN SPEED INCREASED FROM 230 KTS TO 275 KTS THE SOUND BECAME MORE APPARENT. CREW REQUESTED TO DIVERT. UPON DESCENDING THROUGH 7000 MSL A FAINT POPPING NOISE WAS HEARSDR CEDAN217CA121708Gyro · failedAFTER TAKEOFF, ENROUTE, DIRECTIONAL GYRO FAILED. PILOT ELECTED TO DIVERT DUE TO WEATHER CONDITIONS.SDR EXD2008F00000Pump · failedTHE FLIGHT CREW REPORTED APPROXIMATELY (1) HOUR INTO THE FLIGHT, THE LT ENGINE SHUT DOWN WITH NO WARNING OR PRIOR INDICATION OF A PROBLEM. THE TREND MONITORING WAS COMPLETED PRIOR TO THE ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW PROMPTLY NOTIFIED ATC AND SDR HAEA200800205Fire Loop · shortedAC DEPARTED AND CLIMBED TO 3000 FT MSL. NR1 ENG FIRE WARNING HORN AND LIGHT ACTIVATED. AC DECLARED EMERGENCY AND RETURNED TO DEPARTURE. MAINT FOUND NO EVIDENCE OF FIRE. DISCOVERED NR1 FIRE LOOP SHORTED OUT. REPOSITIONED AND TESTED FIRES SYS WARNING. OPS CHECK SDR 5102008N218CAConnector · burnedSMALL AMOUNT OF SMOKE NOTICED IN COCKPIT.SDR 551008N218CAConnector · burnedSMALL AMOUNT OF SMOKE NOTICED IN COCKPIT.SDR CA080304010Selector Valve · failed(CAN) DISC LANDING GEAR WOULD NOT EXTEND. PERFORMED MANUAL/EMERGENCY EXTENTION. ENG HYDR PUMP PRESSURE WAS NORMAL. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10. ADDITIONAL INFORMATION: ATTEMPTED TO EXTEND GEAR 3 TIMES BUT FAILED. DID GETSDR HAEA200700203Engine · fodDEPARTED BIS CLIMBING THROUGH 3000 FT, RT ENGINE LOST POWER. CREW REQUESTED VECTOR TO RETURN TO BLOCKS. ON DECENT RT ENGINE POWER WAS AVAILABLE. AIRCRAFT LANDED WITH OUT INCIDENT. RT ENGINE FOD'D DUE TO ICE INGESTION AND REQUIRES ENGINE CHANGE. [CLOSED]SDR 4006Outflow Valve · failedAIR CONDITIONING VALVE CIRCUIT BREAKER POPPED AFTER TAKEOFF AND WOULD NOT RESET WHICH PREVENTED THE AIRCRAFT FROM PRESSURIZING. THE PILOTS REMAINED AT LOWER ALTITUDE WHILE FOLLOWING PROPER PROCEDURES AND LANDED AT THE NEXT AIRPORT. THE PART WAS REPLACED AND THSDR HAEA200700202Control Box · shortedAFTER DEPARTURE, CLIMBING THROUGH 3000 FT, REAR COMPARTMENT FIRE WARNING ILLUMINATED. THE FO PEERED THROUGH THE INSPECTION GLASS NOTICING NO VISUAL INDICATION OF FIRE. AS A PRECAUTION, THE CAPT DISCHARGED THE FIRE BOTTLES AND DECLARED AN EMERGENCY, RETURNING TSDR HAEA200700201Frame · corrodedDURING MCI INSPECTION FRAME 7 ON THE LT SIDE, DIRECTLY BEHIND AFT EDGE OF PILOTS SIDE WINDOW WAS FOUND TO BE CORRODED IN THE UPPER TUB. ENGINEERING EVALUATED THE CORROSION AND DETERMINED THAT REPAIR WAS NEEDED AND ISSUED AN ENGINEERING INSTRUCTION FOR THE REPASDR HAEA002002007Attach Fitting · corrodedDURING TANK AND PLANK INSPECTION THE LT AND RT WING TO FUSELAGE ATTACH FITTINGS WERE DISCOVERED TO HAVE MINOR CORROSION ON THE LOWER OB SURFACE. THE WINGS WERE DEMATED TO INSURE THAT CORROSION HAD NOT MIGRATED TO BETWEEN THE WING TO FUSELAGE ATTACH FITTINGS. SDR F3LA200700072Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND FASTENER HOLES WHERE FLOORBEAM Y1292 ATTACHES TO FR68. REMOVED AND REPLACED FLOORBEAM ASSY. IAW A319 SRM 51-42-11.SDR F3LA200700064Floorbeam · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR68 AND FR69 AT -Y1162. FOUND TO BE OUT LIMITS IAW A319 SRM 53-00-14, FIG. 101. REMOVED AND INSTALLED FLOORBEAM ASSY IAW A319 SRM 51-42-11.SDR F3LA200700076Attach Fitting · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED INTERNAL CASTING AND THROUGH PIN BUSHING ON NLG UPPER TORSION LINK LUG CORRODED. REMOVED CORROSION AT UPPER TORSION LINK. TREATED, CAD PLATED AND REINSTALLED BUSHINGS IAW EA A9-32R-11842.SDR F3LA200700065Floorboard · corrodedDURING C4/S1 CHECK, INSPECTION REPORTED RUST BUILD-UP IN AFT OB MOUNTING HOLE IN FLOORBOARD, AFT LT LAVATORY. INSTALLED NEW BUSHING AND PACKING IN FLOORBOARD UNDER LAV D AFT OB MOUNT IAW A319 AMM 25-43-41-400-001.SDR 01172007N220CEngine · malfunctionedAFTER TAKEOFF AND CLIMBOUT TO FL210 FROM KDAY, THE CREW NOTICED THE OIL PRESSURE INDICATION WAS ERRATIC. CREW NOTIFIED ATC OF SHUT DOWN RIGHT HAND ENGINE AS A PRECAUTIONARY MEASURE. CREW PROCEEDED TO CHANGE DESTINATION TO KTOL. LANDED WITHOUT FURTHER INCIDESDR HAEA200600196Latch · faultyFALSE LANDING GEAR INDICATION (IN TRANSIT) IN MIDFLIGHT. MAINTENANCE REPLACED DOOR LATCH. PERFORMED GEAR RETRACTION SEVERAL TIMES, OPS CHECK GOOD. [CLOSED]SDR DAT2006F00004Engine · leakingDURING THE FLIGHT, THE FLIGHT CREW SAW A LOW OIL PRESSURE LIGHT. THE FLIGHT CREW CHECKED THE ENGINE GAUGES AND CONFIRMED IT BY THE LOW OIL PRESSURE GAUGE. THE FLIGHT CREW WENT THROUGH THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE RT ENGINE. THE FLIGHT CREWSDR HAEA200600189Engine · unknownAIRCRAFT DEPARTED MCI, CLIMBING THROUGH FL200 RT OIL PRESSURE LIGHT ILLUMINATED AND RT OIL PRESSURE READ ZERO. RT ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO COU. LANDED WITHOUT EVENT. MAINTENANCE INSPECTED ENGINE AND FOUND BEE NUT LOOSE ON OIL LINE. TIGHTENED OSDR HAEA200600188Seal · failedAPPROX 50 MINS INTO FLT (FL280) HEARD A LOW RUMBLING NOISE. INSTRUMENTS NORMAL EXCEPT NR 1 ENG OIL PRESSURE DROPPED 50 PSI TO 10 PSI. CONTINUED NORMALLY 30 SEC, THEN RPM BEGIN TO FLUCTUATE BETWEEN 80 & 90%, WITH CONTINUOUS RUMBLING NOISE. RETARDED THROTTLE SDR HAEA200500187Engine · fodCREW PERFORMED A STATIC TO. BOTH ENGINES INDICATED NORMAL. AT 1500 AGL CREW HEARD AN ABNORMAL NOISE FROM THE LT ENGINE ACCOMPANIED BY HIGH EGT INDICATION. CREW REDUCED POWER ANDNOTED THAT THE NOISE ENDED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO SDR CED2006F00022Windscreen · crackedDURING TAKEOFF ROLL, BETWEEN 60 AND 80 KNOTS THE CENTER SECTION OF THE WINDSCREEN CRACKED. THE TAKEOFF WAS ABORTED. THE WINDSCREEN HAD A VERTICAL CRACK DOWN THE CENTER. (K)SDR CED2006F00013Hose · leakingWHILE PASSING THROUGH FL320 ON CLIMB TO FL350, THE NR1 ENGINE ROLLED BACK TO 25 PERCENT. THE CREW REGAINED POWER AND CLIMBED TO FL350 AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE TO INCLUDE BORESCOPE, AND REPLACED T2 HOSE. ENGINE FLSDR CED2006F00004Uplock Switch · inoperativeON APPROACH, THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE C (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR1 LANDING GEAR UPLOCK SWITCH INOPERATIVE. REMOVED AND REPLACED UPLOCK SWITCH WITH SERVICEABLE PART. OPS CHECK OK. (SDR CED2006F00024Uplock Switch · inoperativeON APPROACH THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE A (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR2 LANDING GEAR UPLOCK SWITCH INOPERATIVE. REMOVED AND REPLACED UPLOCK SWITCH WITH SERVICEABLE PART. OPS CHECK GOOD. SDR HAEA200500181Gcu · failedENROUTE, AT FL280, BATTERY BUS ANNUNCIATOR LIGHT ILLUMINATED. RESET BUS IAW CHECKLIST AND REDUCED ELECTRICAL LOAD. PROBLEM CORRECTED FOR A FEW MINUTES FOLLOWED BY LOSS OF NR 1 GEN LIGHT. ATTEMPTED RESET OF NR 1 GEN UNSUCCESSFUL. NR 1 GEN WAS SHUT OFF AND E
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