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 = 'CF343B1' 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 = 'CF343B1' 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 CA130214021Engine · failed(CAN) ON FEBRUARY 7, 2013, ACFT EXPERIENCED AN UNREPORTED STALL EVENT AT APPROXIMATELY FL340 FOLLOWED BY A FAILURE OF THE LT ENGINE. THE LT ENGINE INCURRED A CATASTROPHIC CONTAINED FAILURE OF THE HPT. THERE WAS NO DAMAGE FOUND IN THE COMPRESSOR SECTION. THE SDR CA130208002Smoke Detector · malfunctioned(CAN) SMOKE TOILET CAUTION MESSAGE DURING TAKEOFF ROLL. MESSAGE CLEARED AFTER ABORT, WHILE CLEARING THE RUNWAY. SQUAWK ALSO STATED TO ABORTED TAKEOFF, FOUND NO ODOR OR SMOKE DETECTED. MAINTENANCE PERFORMED AN ABORTED TAKEOFF HIGH ENERGY STOP INSPECTION IAWSDR REXA2013012700199Engine · fireON FLIGHT 3629 (CLT TO MEM) STARTED ENGINE NR 2 SECOND. DURING START WE GOT THE "HOT" ICON AND STOPPED START. AIRCRAFT BEHIND US INDICATED THAT FLAMES WERE COMING OUT OF RIGHT ENGINE. (ITT REACH AT 550 DEG). NO ITT EXCEEDANCE HISTORY RECORDED IN MDC. PERFSDR REXA2013012600201Engine · vibrationON FLIGHT 3938 (DTW TO ORF) SHORTLY AFTER DEPARTURE CREW LOST THE RIGHT ENGINE. IN FLIGHT SHUTDOWN OCCURRED ON NUMBER 2 ENGINE DUE TO SUSPECTED ENGINE DAMAGE. OCCURRED UPON PASSING 11000 MSL LOUD VIBRATION NOISE AND ITT IN THE RED. CREW DECLARED AN EMERGENCSDR CA130124007Spoiler Sys · faulted(CAN) DURING TAKEOFF, GROUND SPOILER UNSAFE INDICATION OCCUR. CAPTAIN ABORTED TAKEOFF ON 120 KNOTS SPEED. WHEELS NR 3,4 OVERHEATED AND FULLY DEFLATED. WHEELS AND 1 BREAK WERE REPLACED. FIM ACTIONS DID NOT LEAD TO REAL CAUSE OF FAULTY INDICATION. PROBABLY INDSDR CA130124024Shaft · bent(CAN) AFTER TAKEOFF THE CREW HAD A PAX DOOR LATCH C/M POSTED FOLLOWED BY A PAX DOOR WARNING.CREW ELECTED TO RETURN ONCE ON THE GND THE MSG CLEARED.INTERREGATED THE PSEU AND DOCUMENTED ALL THE FAULT CODES. FIM 52 & 8722, 70 & 8722,00 PAGE 107 - CODES S46 AND S4SDR CA130129006Connector · shorted(CAN) ACFT WITH 2 CREW ON BOARD, WAS DESCENDING THROUGH FL220 WHEN THE CABIN ALTITUDE ALARM ACTIVATED PROMPTING THE CREW TO DROP THEIR OXYGEN MASKS AND INITIATE AN EMERGENCY DESCENT. THE ACFT CONTINUED FOR A SAFE LANDING.SDR CA130122011Flap System · failed(CAN) ON APPROACH FLAPS WERE SELECTED FROM 0 TO 8. FLAP FAIL CAUTION MESSAGE CAME ON AND SYNOPTIC PAGE SHOWS LT AND RT FLAP INDICATION TO BE ZERO. ACFT WAS ABOUT 1 HR INTO FLIGHT BEFORE ON APPROACH AND FLAPS ATTEMPTED TO BE EXTENDED. OAT WAS ABOUT -29 DEGRESDR CA130118009Flap System · failed(CAN) FLAP FAIL REPORTED ACFT LANDED WITH NO ISSUES, OPERATING UNDER MEL UNTIL FLAP ACTION PLAN COMPLETED FLAP ACTION PLAN AND LUBE COMPLETED NO FAULTS FOUND AND ACFT RELEASED FOR SERVICE.SDR A6WA201301134010Fan · out of balanceRIGHT ENGINE FAN VIBRATION SHOWED 2.7 MILS IN FLIGHT AND HAD TURNED YELLOW. COULD NOT FEEL PRONOUNCED VIBRATION IN THROTTLE. CREW RAN QRH AND DETERMINED THAT ENGINE SHUTDOWN WAS NOT REQUIRED DUE TO NO OTHER ABNORMAL ENGINE INDICATIONS PRESENT. CREW DECLAREDSDR REXA2013011300152Engine · malfunctionedON FLIGHT 4134 (IAH - MEM) WHILE CLIMBING THROUGH 5,000FT HEARD A POP AND LOST THRUST (BOTH AT THE SAME TIME). NO INDICATIONS OF SPOOL, ITT WAS WITHIN LIMITS, ENGINE FAILURE. CREW SUSPECTED FLAMEOUT AND ATTEMPTED TO RESTART PER QRH. ENGINE DID NOT RELIGHT. SDR VNAA2013011000003Compressor Blade · damagedCREW REPORTED LEFT ENGINE WOULD NOT ATTAIN CLIMB POWER WITHOUT EXCEEDING ITT LIMIT. MULTIPLE AIRFRAME VIBRATION / SHUDDERS WERE ALSO REPORTED, WITH ONE SEVERE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE AND FOUND SDR A6WA201301094006Engine · malfunctionedFLIGHT DEPARTED NORMALLY FROM DCA. CLIMBING BETWEEN 2000-3000FT MSL, WHEN THRUST LEVERS WERE ADVANCED FROM 85% N1 TO CLIMB SETTING OF AROUND 90% N1 CREW EXPERIENCED A SIGNIFICANT VIBRATION. CREW OBSERVED RIGHT ENGINE ITT SPIKE TO 980 DEGREES C AND DRAMATIC ESDR ASOA2012122002686Engine · malfunctionedRT ENGINE VIBRATION, ITT SPIKE, AND LOOSE OF POWER AT ROTATION. FOLLOWED QRH AND RETURNED FOR LANDING. EMERGENCY DECLARED, ACFT RETURNED. R & R NR 2 ENGINE.SDR CA121218002Carbon Seal · leaking(CAN) DURING CRUISE FLIGHT AT FL300 THE RT ENGINE OIL PRESSURE BEGAN FLUCTUATING 35-40 PSI, ALL OTHER ENGINE PARAMETERS WERE NORMAL. DUE TO LOW OIL PRESSURE WARNING MESSAGES THE CREW SHUTDOWN THE RT ENGINE. AN EMERGENCY WAS DECLARED. THE ACFT LANDED UNEVENTSDR VNAA2012121300010Amplifier · malfunctionedCREW REPORTED LEFT N1 GAUGE BECAME ERRATIC WITH A CORRESPONDING INCREASE / DECREASE IN ENGINE PERFORMANCE DURING CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT CONTROL AMPLIFIER AND PERFORMED CHSDR CA121218001Engine · shutdown(CAN) IN FLIGHT SHUTDOWN. THE PARAMETERS OF THIS ENGINE WERE NORMAL AT THE MOMENT OF SHUTDOWN.SDR VNAA2012120800006Anti-Ice Valve · failedCREW REPORTED RIGHT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE ANTI-ICE VALVE, ANTI-ICE PRESSURE SWITCH AND PRV (PRESSURE RELIEF VALVE) AND PERFORMED CHECKS USDR CA121210007Throttle Cable · binding(CAN) IN CRUISE FLIGHT THE CREW NOTICED THAT THE LT THROTTLE WAS JAMMED. THEY WERE ABLE TO LOOSEN THE THROTTLE SOMEWHAT DURING THE DESCENT BUT IT WAS STILL VERY STIFF TO MOVE. ONCE ON THE GROUND THE THROTTLE SEEMED TO WORK NORMALLY. THE LT THROTTLE GEARBOX SDR CA121205002Carbon Seal · leaking(CAN) THE CREW REPORTED THAT THE LH ENGINE OIL PRESSURE WAS FLUCTUATING RAPIDLY AND DROPPING INTO THE CAUTION RANGE. DURING THE DESCENT THE CREW REDUCED THE LT ENGINE POWER TO IDLE AND LT IT THERE FOR THE REMAINDER OF THE FLIGHT DUE TO THE OIL PRESSURE ISSUESSDR VNAA2012120300003Carbon Seal · leakingCREW REPORTED SMOKE TOILET AMBER MESSAGE IN FLIGHT. CREW FOLLOWED QRH. MESSAGE EXTINGUISHED PRIOR TO LANDING. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE NUMBER ONE CARBON SEAL AND PERFORMED CHECKS USING AIRCRAFSDR CA121128002Tire · failed(CAN) THE FLIGHT CREW REPORTED A DOUBLE TIRE BURST ON TAKEOFF. APPROXIMATE SPEED AT THE MOMENT OF TIRE BURST WAS 120 KNOTS. THERE WAS NO ABNORMAL INDICATION OF ANY PARAMETER DURING THE TAKEOFF, CRUISE AND LANDING.SDR A6WA201211184000Engine · malfunctionedAT 12,000 FEET IN CRUISE AIRCRAFT STARTED TO VIBRATE WITH INCREASING FREQUENCY AND INTENSITY OVER A PERIOD OF APPROXIMATELY 5-10 SECONDS, FOLLOWED BY UNCOMMANDED ENGINE SHUTDOWN. NO INDICATION OF A FIRE OR OVERTEMP. DIVERTED TO CAE. SINGLE ENGINE LANDING WASDR VNAA2012111700010Carbon Seal · defectiveCREW REPORTED SMOKE IN CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASDR CA121120007Actuator · failed(CAN) FLAPS FAIL C/M POSTED ON EICAS DURING FLAP SELECTION ON APPROACH. FLAPS DID NOT MOVE FROM THE ZERO POSITION. QRH ACTIONED. GO AROUND FOR ZERO FLAP LANDING WAS C/O. FLAP FAIL FORM SENT TO TECH OPS. NO HISTORY. FLAP FAIL EVENT, OPERATING UNDER CREW SDR CA121116008Socket · burned(CAN) SMOKE FROM 9F SIDEWALL LIGHT. REPLACED LIGHT ASSY .SDR CA121114012Yaw Damper · failed(CAN) DURING APPORACH, THE CREW NOTICED A YAW MOVEMENT WITH RUDDER TRIM AT FULL TRAVEL. THE CREW ELECTED TO ABORT THE APPROACH IN ORDER TO COMPLY WITH QRH . THE RUDDER TRIM WAS REPOSITIONED TO NEUTRAL AND YAW DAMPER WAS DISENGAGED FOR LANDING .SDR CA121114003Fan · failed(CAN) WHILE ACFT WAS ON THE GROUND CREW WAS ABOUT TO START THE ENGINES AND THE APU DID AN AUTO SHUTDOWN. AFTER TROUBLESHOOTING THE APU LOST ALL OF ITS OIL BECAUSE THE OIL COOLER COOLING FAN BROKE AWAY FROM THE ACCESSORY GEAR BOX LEAVING A 4" HOLE IN THE CASE.SDR CA121206002Slider · failed(CAN) DURING SOME TROUBLESHOOTING, AN ISSUE WITH THE FLIGHT SPOILERS, THE FLIGHT SPOILER CONTROL LEVER WAS REMOVED FROM THE CONSOLE. THE TECH NOTICED THAT LOOSE OBJECTS COULD BE HEARD INSIDE THE LEVER BOX. FOR TROUBLESHOOTING A 2ND LEVER WAS REMOVED FROM ANOTSDR ASOA2012110902458Engine · malfunctionedLOST ABOUT 5 PERCENT POWER IN LT ENGINE EVERY FEW SECONDS ON CLIMBOUT. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. PERFORMED ACCELERATION CHECK ON LT ENGINE, OPS CHECKED GOOD IAW AMM 71-00-00-710-802. ACFT OK FOR SERVICE.SDR CA121107003Actuator · failed(CAN) PRELIMINARY REPORT FLAP FAIL ON APPROACH. FLAP FAIL EVENT, OPERATING UNDER CREW RESET. ACTION PLAN ASSIGNED 182-06, NOV 12-01 NO RESOLULTION YET MORE TO FOLLOW.SDR CA121101004Wire Harness · broken(CAN) DURING ROUTINE MTC THE LH JET PIPE LOOP A WAS FOUND U/S. TROUBLESHOOTING FOUND THAT THE ENGINE FIRE DETECTION WIRING HARNESS WAS BROKEN AT THE PYLON CONNECTOR. THE FIRE DETECTION (P590) AND FIRE PROTECTION (P592) WIRING HARNESSES WERE REPLACED. THIS DEFESDR CA121107002Bpsu · failed(CAN) FLAP FAIL CAUTION ON APPROACH WHEN SELECTING THE FLAPS FROM 0. FLAPS DID NOT MOVE FROM 0. FLAPS RUN UP AND DOWN 10 TIMES TO CHECK ACTUATORS FOR HIGH HEAT, NO FAULTS FOUND, ALL ACTUATORS BETWEEN 11-16 DEGREES CELCIUS. AMM TASK 27-53-00-750-802 COMPLESDR CA121024004Handle · malfunctioned(CAN) WHILE PERFORMING TASK : RJ2-32-900-703 FOR FUNCTIONAL CHECK OF THE NOSE AND MLG MANUAL RELEASE SYS ON THE ACFT WHICH WAS UNDERGOING A C-CHECK, THE AME FOUND THE LANDING GEAR ALTERNATE RELEASE PULL HANDLE WILL NOT REMAIN IN THE DEPLOYED POSITION WHEN PULLSDR CA121024006Actuator · failed(CAN) ON APPROACH, THE FLAPS REMAINED AT 0 DEG WHEN SELECTED. THE CREW DID A MISS APPROACH AND CAME AROUND AND LANDED SAFELY WITH FLAP 0. NO EMERGENCY WAS DECLARED. REF DEFECT- 1081476, RESOLVED ON WO: 358098, TASKCARD: NR-00001, REPLACED FLAP ACTUATORS- LSDR CA121018001Actuator · failed(CAN) GEAR DISAGREE, ON LDG EXTENSION. MLG`S INDICATION UNSAFE. ALTERNATE LDG EXTENSION PERFORMED. EMERGENCY DECLARED. LANDING PERFORMED. ACFT STOPPED AFTER LEAVING RUNWAY TO DEPLANE PASSENGERS. ACFT TOWED TO PARKING. MAINTENANCE VERIFIED THAT LDG WAS DOWSDR ASOA2012101102345Floor Support · crackedFS 484 FLOOR SUPPORT ANGLES CRACKED OTBD OF RBL 27. REPLACED CRACKED FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21.SDR REXA2012009281371Engine · malfunctionedON FLIGHT 4021 DURING CLIMBOUT OF CLT AT 4000FT LOUD POP WAS HEARD, NR 1 ENGINE N1 AND N2 ROWED BACK WITH ITT SPIKE TO AROUND 960. THE CREW THEN PROCEEDED TO SHUTDOWN THE ENGINE WITHIN 1.5 MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. SDR CA120928005Pcu · failed(CAN) RIGHT FLIGHT SPOILER DEPLOYING IN FLIGHT AND UNCOMMANDED.SDR VNAA2012092000017Pdu · failedCREW REPORTED LEFT REVERSER UNLOCK MESSAGE AT ALTITUDE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED LEFT THRUST REVERSER PER MEL. AIRCRAFT RELEASED FOR SERVICE. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED LEFT THRUST REVSDR VNAA2012091800015Carbon Seal · defectiveCREW REPORTED LEFT ENGINE OIL PRESSURE FLUCTUATES BETWEEN 32 - 28 PSI IN FLIGHT. LEFT OIL PRESSURE WARNING MESSAGE WOULD COME ON OCCASIONALLY. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED CARBON SEALS AND MASDR CA120919003Window · cracked(CAN) F/O SIDE WINDOW CRACKED. RT SIDE WINDOW REMOVED IAW TASK 56-12-01-000-801, RT SIDE WINDOW INSTALLED IAW AMM 56-12-01. LEAK CHECK PERFORMED WITH NO FAULTS FOUND.SDR ASOA2012091802226Handle · lack of lubePAX DOOR HANDLE HARD TO OPEN. CLEANED AND LUBED PAX DOOR HANDLE IAW AMM 52-11-02. OPS CHECKED GOOD NO DEFECTS NOTED.SDR VNAA2012091400009Hydraulic Line · shearedCREW REPORTED HYD 1 LOW PRESS AMBER CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE SHEARED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC LINE AND LEFT EDP (ENGINE DRIVEN PUMP) AND PERFORMEDSDR ASOA2012091702224Motor · malfunctionedPASSENGER DOOR DOES NOT OPEN FULLY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. PERFORMED OPS CHECKS OF THE PWR DOOR ASSIST IAW AMM 52-11-08-720-802. NO DEFECTS NOTED DEFER CLEARED PLACARD REMOVED. SDR CLOSED.SDR ASOA2012091702225Sensor · out of adjustRT GEAR DISAGREE MESSAGE AFTER TAKE OFF. RAN QRH PROCEDURE AND LANDED WITHOUT ISSUE WITH 3 GREEN INDICATED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. ADJUSTED PROXIMITY SENSOR. PS11GA (PS7GA) AND TARGET ON UPLOCK LATCH IAW AMM 32-32-05. OPS CHECKEDSDR CA120919004Oil System · low pressure(CAN) RT ENGINE IN FLIGHT, SHUTDOWN IN CRUISE DUE TO EICAS LOW OIL PRESSURE MESSAGE.SDR ASOA2012091402217Door · lack of lubeMAIN CABIN DOOR DIFFICULT TO OPEN. LUBRICATED PAX DOOR , OPS CHECKED GOOD IAW AMM 52-11-00.SDR ASOA2012091402218Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. INSTALLED NEW ANGLE AND RESTORED FINISH IAW REO 601R-52-11-513.SDR ASOA2012091202189Lamp · burned outEMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8D INOPERATIVE. R & R LAMP IAW AMM 33-51-13. OPS CHECKED GOOD.
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