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 = 'CF343A1' 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 = 'CF343A1' 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 CA091214006Actuator · malfunctioned(CAN) ON APPROACH TO MSP, THE FLAP FAIL CAUTION MESSAGE WAS DISPLAYED ON EICAS WHEN THE FLAPS WERE SELECTED FROM ZERO TO 8 DEGREES. THE FLAPS FAILED AT ZERO DEGREES AND AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. THE LT AND RT FLAP FLEX DRIVES WERE CLEANSDR CA091202004Detection Sys · faulted(CAN) ON APPROACH TO MKE THE FLAPS FAILED AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. FLAP FAIL CAUTION MESSAGE DISPLAYED. AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. THE FLAPS WERE MANUALLY CONFIGURED TO 8 DEGREES BY MTC AND THE A/C FERRIED TO A MTC BSDR CA091113009Actuator · failed(CAN) EICAS FLAP FAIL CAUTION MESSAGE APPEARED ON APPROACH INTO WHEN FLAPS SELECTED FROM 0 TO 8 DEGREES. AIRSPEED WAS 200 KNOTS AND OAT WAS 3 DEGREES C.MDC FAULT CODES WERE RETRIEVED AND INDICATED JAM,RIGHT BPSU, AND WIRING. JAZZ TECH OPS DEPARTMENT INITIATE SDR SWIA200923027Bearing · corrodedLEFT ENGINE FORWARD YOKE BEARINGS AND LINK CORRODED. (ENG CHANGE) REPLACED YOKE AND LINK PER AMM.SDR CA091019007Actuator · failed(CAN) FLAPS FAILED AT ZERO DEGREES (WHEN SELECTED TO 8 DEGREES) ON APPROACH. AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. ALL FLAP ACTUATORS WERE REPLACED AND THE SYS FUNCTION CHECKED. PN OF THE REMOVED ACTUATORS ARE: LT1, 852D100-23, LT 2, 852D100-25, LSDR CA091007003Pdu · failed(CAN) ON APPROACH, CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THEY ATTEMPTED TO EXTEND FLAPS. THE FLAPS FAILED AT ZERO DEGREES. CREW CARRIED OUT AN UNEVENTFUL FLAP ZERO LANDING. FAILURE CODES FROM THE FECU INDICATED A FLAP PDU AT FAULT. FLAP DRIVES WERESDR CA090924001Wheel · damaged(CAN) ON T/O ROLL. ACFT VEERS TO THE RT. DIFFICULT TO CONTROL. ABORTED T/O. RETURN TO GATE. MX FOUND 1 NR 4 MLG WHEEL HEAT SHIELD SEGMENT SEPARATED FROM WHEEL WITH MISSING SCREW AND INTERFERING WITH WHEEL SPINNING. NR 4 WHEEL WAS REPLACED.SDR SWIA200922532Engine · smokeRIGHT ENGINE PRODUCING SMOKE. (FLT 5863) INSPECTIONS AND ENGINE RUNS NORMAL.SDR CA090816001Connector · corrodedPINS IN CONNECTOR PLUGS, P53MD AND J53MD, FOUND CORRODED. THIS DEFECT WAS NOTED WHEN ATTEMPTING TO ROB THIS UNIT FOR USE ON ANOTHER ACFT WITH SIMILAR PROBLEM. CONNECTORS PN 206044-1, 206043-1, SOCKET PN 1-661105-9 AND PINS PN 1-66103-8 REPLACED.SDR CA090813017Connector · corrodedCONNECTOR PLUGS, P53MD AND J53MD, FOUND WITH HEAVY CORROSION WITH PINS BROKEN WHEN CONNECTOR WAS TAKEN APART. THIS HAD CAUSED THE IN OPERATION OF NO SMOKING LIGHTS IN THE CABIN. DUE TO INAVALABILITY OF THIS CONNECTOR, THE AME TRIED TO ROB THIS CONNECTOR OFF ASDR CA090729003Bpsu · malfunctioned(CAN) ON SHORT FINAL, FLT CREW RECEIVED A FLAP FAILURE CAUTION MESSAGE WITH THE FLAPS TRAVEL STOPPING AT30 DEGREES. ACFT HAD POST MOD ACTUATORS INSTALLED AT THE LAST FLAP FAIL EVENT, BACK AT FEB 08,2008. THE FECU (52B AND 25C)CODES WERE RETRIEVED BY MAINT. SDR CA090721001Relay · failed(CAN) WHILE INBOUND TO DESTINATION ACFT HAD A MOMENTARY AC BUS 1 ELECTRICAL PWR INTERUPTION. CREW RECEIVED LT WINDOW AND WINDSHEILD CAUTION MESSAGES. ALSO, LOST LT SIDE WALL LIGHTS AND CABIN EMERGENCY LIGHTS CAME ON. FAULTS CLEARED AFTER A FEW SECONDS WITH SDR CA090710006Fitting · plugged(CAN) COLLECTOR TANK IS HOUSED IN THE CTR FUEL TANK. WHEN DRAINING CTR FUEL TANK, IT WAS PROVEN THROUGH TROUBLESHOOTING THAT EVEN WHEN THE COLLECTOR TANK DRAIN (ITEM 235) WAS OBSTRUCTED BY FOD, YOU WILL STILL HAVE FUEL DRAINING FROM THE CTR FUEL TANK DRAIN BESDR CA090615003Mechanism · jammed(CAN) CREW REPORTED MAIN PASSENGER DOOR CAUTION DECENDING THROUGH FL11000 ON APPROACH. F/A REPORTED ON TOUCHDOWN MCD COMPLETELY UNLATCHED AND REQUIRED HIM TO HOLD TO PREVENT OPENING. ACFT FERRIED TO FOR REPAIR WITH OUTER HANDLE TAPED DOWN. ENGINEERS FOUND ISDR CA090619005Uplock · malfunctioned(CAN) WHEN SELECTING GEAR DOWN ON APPROACH GOT A DISAGREE AND CANCELLED HORN, THEN HERD A CLUNK, THEN GEAR (NOSE DOOR AND GEAR RED) UNSAFE THEN GEAR WENT FULLY DOWN WITH 3 GREEN. MAIN NORMALLY AND NOSE 1 MIN LONGER TO GO DOWN. AFTER MX INVESTIGATION, FOUND TSDR CA090513006Handle · seized(CAN) LANDING GEAR MANUAL RELEASE HANDLE ASSY STUCK IN THE "PULLED" POSITION DURING A LANDING ALTERNATE GEAR EXTENSION CHECK. THE ACFT WAS IN THE HANGAR FOR A HEAVY MX INSP. THE HANDLE ASSY (PN 2605890-001) WAS REPLACED. THE NEW HANDLE WAS ALSO FOUND STIFF BUSDR COMA2009050750131Bleed Valve · failedEN ROUTE FROM JFK TO CLE LEFT 10TH STAGE BLEED VALVE FAILED TO OPEN. EMERGENCY DECLARED, A/C LANDED SAFELY AT CLE. REMOVED AND REPLACED LEFT 10TH STAGE BLEED VALVE.SDR CA090429001Fan Blade · bent(CAN) ON THE TAKEOFF ROLL,THE ACFT SUSTAINED A BIRD STRIKE FROM A MEDIUM SIZED BIRD. THE BIRD WAS INGESTED INTO THE NR1 ENGINE. AFTER TAKEOFF THERE WAS A CONSTANT BUZZING NOISE WHICH WAS ABNORMAL. THE ENGINE PARAMETERS FOR BOTH ENGINES APPEARED TO BE NORMAL WISDR CA090423003Control Panel · contaminated(CAN) CREW DECLARED EMERGENCY DUE TO AILERON JAM - LWD CAUTION ON FLIGHT, AP LWD CAUTION MESSAGE. AFTER DISENGAGEMENT OF THE AP, ACFT NEEDED VERY STRONG FORCE TO ROLL. NEARLY IMPOSSIBLE. SUDDENLY THE AILERONS BECAME FREE AND ACFT WAS NORMAL TO CONTROL WITH NOSDR COMA2009040150108Engine · vibrationON CLIMBOUT FROM BOS RECEIVED LEFT ENGINE VIBE MSG ALONG WITH MAX ITT AND OIL PRESSURE OF 20 PSI. PERFORMED IFSD OF LEFT ENGINE. EMERGENCY DECLARED, A/C RETURNED TO BOS LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE.SDR COMA2009032450104Pump · faultyEN ROUTE FROM LGA TO SAV RECEIVED LEFT ENGINE OIL PRESSURE MSG. EMERGENCY DECLARED, A/C DIVERTED TO RDU LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE LUBE AND SCAVENGE PUMP.SDR RU3A0901Clamp · looseAT CRUISE FL350, THE BLEED AIR LEAK DETECT LIGHT (CENTER PANEL) INTERMITTENTLY BEGAN FLASHING. NOTICED THAT THE LEFT 10TH STAGE "DOLLS EYE" WAS TRIPPED. INITIALLY, DID NOT GET THE LEFT 10TH STAGE DUCT FAIL LIGHT. BEGAN A DESCENT TO A LOWER ALTITUDE (FL200 TSDR COMA2009010750059Fuel Control · failedON APPROACH, NR2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENGINE FUEL CONTROL.SDR CA090106001Position Sensor · malfunctioned(CAN) DURING DESCENT THE FLIGHT CREW RECEIVED A "FLAP FAIL" CAUTION MSG. THE MULTIFUNCTION DISPLAY (MFD) WAS INDICATING FLAP AT ZERO DEGREE, THERE WAS NO FLAP SELECTION DONE BY THE CREW. THE EMERGENCY RESPONSE SERVICES WERE REQUESTED AND THE ACFT LANDED WITHSDR CA090106003Bpsu · malfunctioned(CAN) FLAP FAIL C/M DISPLAYED ON INITIAL SELECTION. ACFT UNDER MEL FOR FLAP HALF SPEED SINCE DEC 31/08. LT BPSU DETERMINED AS FAULT OF FAILURE. PDU REPLACED TO CORRECT FLAP HALF SPEED. TEST FLIGHT SUCCESSFUL AND ACFT RETURNED TO SERVICE.SDR CA090109006Shutoff Valve · malfunctioned(CAN) RT WING NOT SHEDDING ICE, UP TO 75 PERCENT IN ON L/E, NOTED DURING WALKAROUND. NO MESSAGES. RECTIFICATION, RT MODULATING SHUTOFF VALVE REPLACED. TROUBLESHOOTING NOTES, HAD CREW RUN ENGINES, OPERATED WING A/ICE WITH NR1 ENG BLEED, LT WING GOT HOT TO TOSDR CA090105006Drive Unit · failed(CAN) THIS AIRCRAFT WAS UNDER A FERRY PERMIT TO YYC FOR A BROKEN OUTER DOOR HANDLE. THE FLAPS WHERE AT 8 DEGREES BEFORE DEPARTURE. AFTER TAKEOFF THE FLAP FAIL MESSAGE WAS POSTED WITH FLAPS STILL AT 8 DEGREES. THE PILOT RETURNED TO YZF DUE TO INSUFFICIENT FUSDR CA090105009Actuator · malfunctioned(CAN) FIRST FLIGHT OF THE DAY. PILOTS WERE TAXIING AND SELECTED FLAPS TO 20 DEGREES AND THE FLAPS STAYED AT 0. OAT -33 DEGREES C. ACFT FERRIED FOR REPAIR. ALL FLAP ACTUATORS REPLACED WITH POST SB ACTUATORS, FLAP DRIVE LUBE TASK COMPLETED, RIGGING AND FUNCTSDR CA081216005Fcu · malfunctioned(CAN) FLAPS FAILED AT 3 DEGREES ON APPROACH. NORMAL LANDING FOLLOWED. CREW ABLE TO RESET SYSTEM ON THE GROUND AND FLIGHT CONTINUED UNDER MEL. SECOND FLAP FAILURE ON AIRCRAFT 107 IN AS MANY FLIGHTS. FLAPS FAILED AT 23 DEGREES INBOUND. NORMAL LANDING OCCURRSDR CA081204007Shaft · worn(CAN) DURING MX OPERATION OF THE LANDING GEAR MANUAL RELEASE HANDLE IT STUCK IN THE RELEASE POSITION. MX TROUBLESHOOTING FOUND THE RELEASE HANDLE SHAFT BINDING DUE TO INTERNAL WEAR AND SLIGHTLY BENT. RELEASE HANDLE ASSY WAS REPLACED IAW AMM 32-34-01. ACF TTSDR CA081128005Fdas · odor(CAN) ON CRUISE THE F/A REPORTED A STRONG ODOR IN THE CABIN, PILOT CONFIRMED THE STRONG SMELL AND DIVERTED FLIGHT TO BASE AND DECLARE AN EMERGENCY LANDING. AFTER MX INVESTIGATION, FOUND THE FDAS "FLIGHT DECK ACCESS SYS" AT FAULT. ELECTRICAL ODOR COMING FROM TSDR CA081121002Control Unit · failed(CAN) DURING PUSH BACK FROM THE GATE, FLAP LEVER WAS MOVED TO 8 DEGREES BY THE FLIGHT CREW BUT THE FLAP DIDN`T EXTEND AND "FLAP FAIL" CAUTION MESSAGE APPEARED ON THE ENGINE INDICATION AND CREW ALERTING SYS (EICAS). THE ACFT WAS TOWED BACK TO THE GATE. FLAP ELESDR CA081111004Control Unit · malfunctioned(CAN) FLAPS SELECTED TO 20 DEGREES FOR TAKE-OFF. AFTER TAKE-OFF, FLAPS WERE SELECTED TO 8 DEGREES AND THE FLAPS LOCKED AT 20 DEGREES. FLAP FAIL CAUTION EICAS MSG AS WELL. FOUND SKEW DETECT FAULT LIGHTS ILLUMINATED, BOX RESET CARRIED OUT ALONG WITH BREAKER RSDR CA081111001Bypass Valve · stuck(CAN) ON TAXI IN, CREW NOTICED ONE OF THEIR AIR-CONDITIONING PACKS WAS OVER TEMPING. THEY WHERE NOT ABLE TO CONTROL IT, SOON NOTICED SMOKE ON FLIGHT DECK. F/A WAS NOTIFIED AND A RAPID DEPLANEMENT WAS CONDUCTED AT GATE. MX FOUND THE DUAL BYPASS VALVE STUCK IN TSDR CA081016005Transmitter · failed(CAN) CLIMBING THROUGH 12000 FT AT 250 KIAS ACFT NOSED OVER AS FLAPS WENT TO AT LEAST 25 DEGREES AND AUTOPILOT KICKED OFF. ACFT SLOWED TO 200 KIAS WHILE RETURNING TO DEPARTURE AIRPORT. FLAPS CONTINUOUSLY CYCLED FROM 0 TO 12 DEGREES. CIRCUIT BREAKERS 1F4 ANDSDR CA081010002Housing · leaking(CAN) MX DISCOVERED NR 1 ENGINE FUEL FILTER ASSEMBLY LEAKING FROM THE TOP OF THE FILTER HOUSING. HOUSING IS EITHER CRACKED AROUND TOP FITTING OR IS LEAKING THROUGH PRC AROUND FITTING. FUEL FILTER ASSEMBLY 4106T62P01 REF IPC 73-11-00 FIG 1 ITEM 110A INSTALLEDSDR CA090125005Rudder Pedal · brokenAIRCRAFT TOOK A CREW CANCEL BECAUSE THE FO CALL FATIGUE. THE AIRCRAFT THEN WAS RESCHEDULED TO REPOSITION AT 1000. GOT A CALL THAT THE CAPTAIN’S LEFT RUDDER PEDAL WAS BROKEN. WHEN THE MECHANICS WENT O BOARD THEY FOUND THAT THE CAPTAIN’S RUDDER PEDAL WAS BENTSDR CA080922006Acm · odor(CAN) ON FINAL APPROACH, SMOKE SMELL IN FLIGHT DECK. AT THE SAME TIME UNABLE TO CONTROL LT PACK IN AUTO OR MANUAL MODE. ALSO DISPLAY FAN OR AIR IN FAN MAKING GRINDING NOISE. BOTH FANS PLACED IN FLT ALTN MODE AND SMOKE STOPPED.SDR COMA086369Carbon Seal · wornENROUTE FROM CLE TO JFK RECEIVED RT ENGINE OIL PRESS WARNING MSG. FOLLOWED QRH, EMERGENCY DECLARED PERFORMED IFSD OF RT ENGINE. ACFT DIVERTED TO AVP AND LANDED SAFELY. CORRECTIVE ACTION: FOUND IDG CARBON SEAL (AGB AXIS BB) LEAKING. R&R CARBON SEAL.SDR CA080708002Bpsu · unserviceable(CAN) ACFT WAS SET UP IN LANDING CONFIGURATION WITH FLAPS AT 45 DEGREES. ON SHORT FINAL, CREW RECEIVED A FLAP FAILURE INDICATION. FLIGHT DID LAND NORMALLY. HOWEVER, WERE UNABLE TO RETRACT FLAPS ONCE ON THE GROUND. RT BPSU SHOWN TO BE AT FAULT. BPSU REPLACEDSDR CA080711008Line · disconnected(CAN) ACFT HAD A NORMAL LANDING ON ARRIVAL IN IND, HOWEVER WHILE ATTEMPTING TO TAXI OFF THE RUNWAY, EXCESSIVE POWER WAS REQUIRED TO TAXI. IT WAS SUSPECTED THAT NR 2 BRAKE ASSEMBLY HAD SEIZED AS SMOKE COMING FROM THE NR 2 BRAKE. CONTRACT MX INVESTIGATED THE ACSDR CA080630005Selector Valve · unserviceable(CAN) GEAR DISAGREE MSG ON GEAR DOWN SELECTION, MAINS INDICATING GREEN AND THE NOSE INDICATING WHITE. CREW CYCLED GEAR WITH SAME RESULT. THEY THEN DID AN ALTERNATE EXTENSION AND GOT THE 3 GREEN INDICATION AND LANDED WITH NO PROBLEM. (LANDING GEAR RETRACTION SYSDR CA080623005Uplock · cracked(CAN) PILOT REPORTED THAT THE SERVICE DOOR MESSAGE WAS DISPLAYED. MAINT WAS CALLED TO INVESTIGATE THE PROBLEM AND THEY WERE TOLD BY THE CREW THAT THE ENGINEER COULD NOT OPEN THE DOOR AND THEY START REMOVING THE DOOR LINER. ONCE REMOVED, THEY FOUND THAT THE SERSDR COMA0860277Check Valve · failedDURING CLIMBOUT FROM CVG RT ENG HIGH OIL TEMP. EMERGENCY DECLARED, ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND RT ENG AGB OVER SERVICED WITH OIL. REMOVED AND REPLACED RT ENG BYPASS CHECK VALVE. (S)SDR COMA0860278Warning Light · illuminatedEN ROUTE FROM LGA TO CHS RECEIVED LEFT REV UNLOCK MSG. ACFT DIVERTED TO JFK AND LANDED SAFELY. INSPECTED LT ENG T/R SYSTEM. NO DEFECTS FOUND. PERFORMED OPS CHECKS OF T/R SYSTEM. ALL CHECKS GOOD. COULD NOT DUPLICATE MSG ON GROUND. (S)SDR 2008FA0000359Control Handle · damagedAIRCRAFT HAD BEEN EXPERIENCING MULTIPLE INFLIGHT FLAP FAILURES WHICH WERE NOT DUPLICATED ON THE GROUND. DURING TROUBLESHOOTING OF THE FLAP SYSTEM, FLAPS WOULD NOT MOVE FROM 45 DEGREES TO 30 DEGREES WHEN SELECTED. NO FAILURE WAS DISPLAYED BY THE AIRCRAFT. FLAP SDR 2008FA0000361Fcu · failedAC HAS BEEN EXPERIENCING INTERMITTENT FLAP SYSTEM FAILURES IN DIFFERENT MODES OF FLIGHT, PRIMARILY DURING APPROACH. TROUBLESHOOTING IAW MM RECOMMENDED REPLACEMENT OF FLAP CONTROL UNIT DUE TO IMMEDIATE ( INTERMITTENT) FAILURES AFTER FLAP MOVEMENT SELECTION. AFTSDR 2008FA0000433Asymmetry Switch · failedFLAPS FAIL FOUR DEGREES AFTER SELECTION. USING BREAKOUT BOX, SELECTED THIS BDU AND FLAPS WOULD CONSISTENTLY FAIL. SELECTED OTHER SIDE BDU AND FLAPS WOULD OPERATE NORMALLY. UNIT ALSO RATTLES ON BENCH WHEN CHECKING DRAG TORQUE (UNLOCKED). (K)SDR CA080410005Bpsu · unserviceableON DESCENT, CREW SELECTED AND RECEIVED FLAPS 8 DEGREES, WHEN THEY ATTEMPTED TO PROCEED TO FLAPS 20 CREW RECEIVED A FLAP FAIL MESSAGE. FLIGHT LANDED WITHOUT INCIDENT. FECU MESSAGE POINTED TO THE RT BPSU AS THE FAULT. THE RT BPSU WAS REPLACED, FLAP SYSTEM RIGSDR COMA0860207Tube · crackedFLIGHT 5451 - EN ROUTE FROM YYZ TO CVG, NR 2 ENGINE LOW FUEL PRESSURE CAUTION MESSAGE. ENGINE REMAINED AT 56%, 70 DEG OIL TEMP, 50 PSI OIL PRESS, AND NO RESPONSE FROM THRUST LEVER. PERFORMED IFSD ON NR 2 ENGINE, EMERGENCY DECLARED AND A/C DIVERTED TO CMH AND
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