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 A6WA200840010Seal · obstructedSERVICE DOOR DIFFICULT TO OPEN. CLEANED DEBRIS FROM DOOR SEAL. DOOR OPERATES OK AT THIS TIME. (K)SDR CHQA200800005Line · crackedIAH TO CMH - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE THEN CONFIRMED THAT THE SYSTEM 2 QUANTITY WAS ZERO. THE AIRCRAFT RETURNED TO FIELD AT IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND A HAIRLSDR CHQA200800006Control Unit · failedIAH TO TUL - DURING CLIMB CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE AIRCRAFT THEN RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FLAP SYSTEM AND INTERROGATED THE FECU FOR FAULT CODES AND FOUND A FECU BIT FAIL MESSAGE ON THE FESDR VNAA0801001Oil System · overservicedCREW REPORTED WHEN THE APU WAS TURNED ON FOR LANDING, IT CAUSED THE CABIN TO FILL WITH SMOKE. CREW FOLLOWED THE QRH, TURNED OFF THE APU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OIL LEVEL TO BE OVERSERVICED. MAINTENANCE PROPERLY SERVISDR A6WA200840009Switch · out of adjustANTI-SKID IB CAUTION MESSAGE AFTER TAKEOFF FOLLOWED BY PARKING BRAKE SHUTOFF VALVE CAUTION MESSAGE. LANDING GEAR HESITATED TO RETRACT THEN RETRACTED SLOWLY, CAUTION MESSAGES WENT AWAY. HYD SYS NR3 QUANTITY AND PRESS NORMAL, ON GROUND SYSTEM 3 HYD QTY 60 PERCSDR CA080110006Fcu · faulted(CAN) THE CREW RECEIVED A FLAP FAIL .5 HR INTO THE FLIGHT CLIMBING BETWEEN 25000 TO 27000 FT. THE AC RETURNED WITHOUT INCIDENT. MAINT T/S WAS CARRIED OUT AND THE LT AND RT BPSU’S WERE SWAPPED FOR T/S. SUSPECTED FAULTY FECU, FECU REPLACED, FUNCTION CHECK C/O ANSDR A6WA200840006Selector Valve · failedON DEPARTURE, SELECTED GEAR LEVER UP. RECEIVED TRIPLE CHIME AND DISAGREE AURAL MESSAGE. GOT GEAR DISAGREE NOSE GEAR DOOR WARN MESSAGES AND WOW INPUT AND NWS INOPERATIVE CAUTION MESSAGES. EXECUTED QRH IN THAT ORDER, HAD 3 GEAR DOWN LOCKED INDICATIONS. REMOVESDR A6WA200840007Trim System · malfunctionedON CLIMBOUT WITH FLAPS 8 DEGREES, STAB AND MACH TRIM WOULDN`T REMAIN ENGAGED. COMPLIED WITH QRH, RE-ENGAGED STAB AND MACH TRIM, BOTH DISENGAGED AND WOULDN`T REENGAGE. SET FLAPS TO 2- DEGREES, RETURNED TO DEPARTURE. REMOVED AND REPLACED FO`S HORIZONTAL STAB SDR A6WA200840008Anti-Ice System · malfunctionedGROUND LIFT DUMP UNSAFE CAUTION MESSAGE IN FLIGHT. QRH PROCEDURE CLEARED MESSAGE. COMPLIED WITH OPS CHECK OF SPOILER FLIGHT SYSTEM. IAW SYS IAW AMM 27-60-00 PARA 11. THIS MESSAGE IS CAUSED BY ANIT-SKID PROBLEM. REMOVED AND REPLACED IAW 32-44-06. OPS CHECK GSDR CA080106001Acm · smoke(CAN) SMOKE IN COCKPIT AND CABIN ON T/O ROLL. DURING T/O ROLL, SMOKE APPEARS IN THE COCKPIT AND CABIN FIRSTS ROWS. ABORTED T/O, RETURN TO BLOCKS. ACM NR1 DETERMINED TO BE THE SOURCE OF THE SMOKE. ACM NR1 DEFERRED IAW MMEL 21-51-1. (TC NR 20080106001)SDR CA080104001Bpsu · unserviceable(CAN) CREW FLYING AT LEVEL 340 FOR 30 TO 40 MIN AND THE FLAP FAIL CAME ON WITH NO SELECTION, FLAPS AT 0 DEG. O FLAP LANDING. TEMP AT ALTITUDE WAS -60 DEG. FERRIED BOTH BPSU`S REPLACED FLAPS FUNCTIONED CHECKED SER (804406 1/4/2008 06:57) (TC NR 20080104001)SDR CA080106003Bpsu · inoperative(CAN) FLAP FAIL MESSAGE DISPLAYED WHILE AC PARKED AT THE GATE. TROUBLESHOOTING REVEALED BRAKE AND POSITION SENSOR UNIT (BPSU) RT AND LT OUT OF LIMITS. MAINTENANCE RIGGED LT BPSU AND REPLACED RT BPSU. (TC NR 20080106003)SDR A6WA200840001Bulkhead · crackedCRACK FOUND ON AFT PRESSURE BULKHEAD FWD FACE IN LINTEL FITTING ARE FS 621.00 LT. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD FWD FACE IN LINTER FITTING AREA AT FS 621.00 LT IAW REO 601R-53-61-1230, REV C. (K)SDR CA080102006Windshield · broken(CAN) (RT WINDSHIELD SHATTERED IN FLIGHT). THE WINDSHIELD WAS REMOVED AND REPLACED. WINDSHIELD, (RT) P/N OFF: 601R33033-14 P/N ON: NP-139321-14 S/N OFF: 02277H7295 S/N ON: 07212H4821 (TC NR 20080102006)SDR A6WA200840004Flap · failedFLAPS FAILED ON RETRACTION AFTER LANDING. RT FLAP INDICATES -0- DEGREES, LT FLAP INDICATES 22 DEGREES. C/W FLAP RESET, FLAP FAIL DID NOT CLEAR. FOUND FLAPS COVERED WITH ICE AND SNOW, PUT AC IN HANGAR TO THAW. PERFORMED RESET IAW AWAC SUPPLEMENT 98-018B AND SDR A6WA200840005Selector Valve · malfunctionedNOSE GEAR DOOR FLAPPING NOISE HEARD AFTER GEAR EXTENSION, TOOK LANDING GEAR CYCLE LONGER THAN NORMAL TO EXTEND. GEAR INDICATOR SHOWED 3 GREEN SIMULTANEOUSLY. EMERGENCY LANDING DECLARED WITH UNEVENTFUL LANDING. (K) R&R NOSE LANDING GEAR SELECT VALVE PER AMM SDR CA080104004Bpsu · failed(CAN) DURING PUSH BACK CREW SELECTED FLAPS TO 20 DEGREES AND RECEIVED A FLAP FAIL CAUTION MESSAGE. MAINT TROUBLESHOOTING LED TO REPLACEMENT OF RT BRAKE POSITION SENSOR UNIT (BPSU) AND RIGGING OF LT AND RT BPSU’S. OF NOTE THE FIRST NEWLY INSTALLED RT BPSU (S/N SDR A6WA200740709Flap · malfunctionedFLAPS FAIL CAUTION MESSAGE AT ZERO ON APPROACH. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET, OK. (K)SDR CA080102007A/C Pack · smoke(CAN) (AC RETURNED TO THE FIELD DUE TO SMOKE TOILET WARNING. THERE WAS A HAZE IN THE CABIN. THEY DECLARED AN EMERGENCY) FOUND THAT THE RT PACK WAS SMOKING UP THE CABIN. DEFERRED THE RT PACK. ADDITIONAL INFORMATION REQUESTED TO THE FSR, AC STILL UNDER MMEL (SDR A6WA200740711Structure · corrodedMINOR CORROSION UNDER SERVICE DOOR LOWER SEAL RETAINER. CORROSION REMOVED IAW SRM 51-21-06 WITHIN LIMIT SRM 52-00-31, FIG 101. MATERIAL REMOVED .003 INCH ORIGINAL THICKNESS .040. (K)SDR CA071231001Bpsu · unserviceable(CAN) FLAP FAIL ON APPROACH. FLAP ZERO APPROACH AND LANDING CARRIED OUT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. RT FLAP BRAKE SENSOR UNIT, SKEW DETECTION UNIT AND RT OB FLEX DRIVE SHAFT REPLACED. FLAP SYS FUNCTION CHECKED SERVICEABLE. (TC NR 20071231001)SDR REXA200700066Engine · flamed outWHEN THE CREW REDUCED POWER TO DESCEND FROM FL300, THE RIGHT ENGINE FLAMED OUT. THE ENGINE OUT PROCEDURES OF THE QRH WERE PERFORMED AND THE ENGINE RESTARTED ON THE FIRST ATTEMPT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WERE MADE. MAINTENANCE TROUBLESHOSDR A6WA200740708Engine · leakingSMOKE TOILET CAS MESSAGE INFLIGHT, SMOKE VISIBLE COMPLIED WITH QRH. SMOKE SOURCE APPEARED TO BE FROM ACROSS LAV ROW 13, AREA LOWER AREA. (K) AIRCRAFT WAS TROUBLESHOT TO RT ENGINE INTERNAL LEAK. REMOVED AND REPLACED. (VENDOR FINDINGS: CARBON SEAL PRESSURIZATSDR A6WA200740712Structure · crackedAC CONNECTOR LANDING STRUCTURE OF ACCESS DOOR FOUND CRACKED APPROX 2.500 INCH. AC CONNECTOR ACCESS DOOR LANDING REPAIRED IAW REO 601R-53-11-569, REV A. (K)SDR A6WA200740713Intercostal · crackedA/C CONNECTOR BOX STRUCTURE AFT INTERNCOSTAL CRACKED. AC CONNECTOR BOX STRUCTURE AFT INTERCOSTAL REMOVED AND FABRICATED IAW SRM 51-24-16, ALODINE IAW 51-21-11 AND INSTALLED IAW SRM 51-42-06, 51-42-13, 51-42-20. (K)SDR A6WA200740706Unknown · smokeTOILET SMOKE CAS MESSAGE IN FLIGHT, COMPIED WITH QRH SMOKE VISIBLE IN COCKPIT, ELECTRICAL SMOKE ODOR IN LAV, SMOKE SUBSIDED WHEN QRH COMPLIED WITH. CORRECTIVE ACTION IN PROGRESS. (K)SDR A6WA200740710Bulkhead · crackedCRACK ON REAR PRESSURE BULKHEAD FWD FACE UNDER LINTER FITTING BRACKET. REPAIR TO REAR PRESSURE CUTOUT IAW REO 601R-53-61-1230 REV D. (K)SDR CA071227001Actuator · unserviceable(CAN) AFTER LANDING, CREW WERE UNABLE TO RETRACT FLAPS, STUCK AT 41 DEGREES. FLT CANCELLED AS A RESULT. EXPECT TO FERRY AC. CODES RETRIEVED: 1)FECU/BPSU 2)ETHER BPSU 3)WIRING, AC RETRIEVED CODES, FORWARDED TO TECH. CARRIED OUT ACTION PLAN 168 AND ALL WIRING RSDR CA071227002Sensing Element · chafed(CAN) RT 14TH STAGE DUCT MESSAGE DURING CLIMBOUT. FLIGHT RETURNED TO AIRFIELD. MAINTENANCE INSPECTION DISCOVERED 14TH STAGE COWL DUCT INSULATION BROKEN AND CHAFING ON SENSING LOOP. BOTH SENSING LOOP AND DUCT WERE REPLACED AND ENGINE RUN’S WERE C/O AND THE AC SDR CA071226001Anti-Ice Valve · unserviceable(CAN) WHILE ENROUTE, AC DEVELOPED A COWL ANTI ICE SNAG. THE AC RETURNED TO FOR REPAIRS. MAINTENANCE FOUND THE COWL ANTI ICE VALVE TO BE AT FAULT ONCE REPLACED OPERATIONAL CHECKS WERE C/O SERVICEABLE. A/C WAS RETURNED TO SERVICE. (TC NR 20071226001)SDR VNAA0712002Pdu · failedCREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED AMBER MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO TRI WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WASDR A6WA200740707Warning System · malfunctionedLT REVERSER UNLOCKED MESSAGE IN FLIGHT. REACTIVATED LT THRUST REVERSER PERFORMED FUNCTIONAL TEST IAW 78-30-00. CHECKS NORMAL THIS TIME PLACARD AND MEL REMOVED. (K)SDR A6WA200740683Pitch Control · inoperativeCONTROL COLUMN BINDS IN PITCH WHEN MOVED FORWARD AND AFT OF NEUTRAL AND FEELS HEAVIER THAN NORMAL THRU WHOLE RANGE OF MOVEMENT IN-FLIGHT AND ON GROUND AT ALL FLAP ANGLES. REMOVED AND REPLACED PITCH FEEL SIMULATOR. (K)SDR MASA200700902Access Panel · departedASH FLT 7307 ORD - THE NR 2 ENG LOWER COWL DEPARTED THE AIRCRAFT AFTER LANDING. MX REMOVED AND REPLACED BLOCKER DOORS AND SUPPORT HINGES, OPS CHECK GOOD.SDR A6WA200740701Plate · corrodedSERVICE DOOR PLATE FIND CORRODED, OUT OF LIMITS IAW SRM 53-00-00, FIG 101. SERVICE DOOR PLATE REPLACED IAW SRM 51-42-00, 51-41-02, 51-41-04. (K)SDR A6WA200740702Warning Light · illuminatedFLAPS FAIL MESSAGE ON APPROACH, FAILED AT 20 DEGREES WHEN SELECTING 30 DEGREES. RESET IAW SUPPLEMENT 98-018B. OPS CHECK NORMAL. (K)SDR A6WA200740704Unknown · unknownON TAKEOFF ROLL, AC VEERED RT, TOOK ALMOST FULL LT RUDDER TO STAY CENTERED ON RUNWAY. N1 SPEEDS WERE MATCHED. REDUCED POWER TO ABORT T/O AT 60 KNOTS. AIRCRAFT THEN TRAVELED STRAIGHT. BRAKE TEMPS WERE A 7 ON LT MAIN GEAR AND 3 AND 4 ON RT. WINDS 180 AT 5 KSDR CA080108001Sump · leaking(CAN) SMOKE CARGO MESSAGE SHORTLY AFTER T/O AND ODOR OF SMOKE ON FLIGHT DECK. LANDED, & TAXI TO PARKING AND DEBARKING OF PAX, CABIN INSPECTED BY FIRE BRIGADE. CABIN CREW REPORTED NO SMOKE IN CABIN AND TOILET DURING FLT AND TAXI BACK. DURING TROUBLESHOOTING, FSDR CHQA200700097Flap System · malfunctionedON APPROACH, THE FLAPS FAILED AT 30 DEGREES. THE AIRCRAFT PERFORMED A GO-AROUND, THE QRH WAS FOLLOWED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE AIRCRAFT AND THE FAIL MESSAGE CLEARED, AFTER OPERATING THE FLAP SYSTEM SEVERAL TIMSDR A6WA200740680Landing Gear · collapsedUPON LANDING, LT MLG COLLAPSED; AIRCRAFT DEPARTED RUNWAY TO THE LT SIDE, CVR AND FDR CIRCUIT BREAKERS HAVE BEEN PULLED, NO FIRE INDICATIONS RECEIVED. (K)SDR A6WA200740681Thermal Switch · inoperativeWING OVERHEAT WARNING MESSAGE ON CLIMBOUT SYNOPTIC PAGE SHOWS LT WING. COMPLIED WITH QRH, MESSAGE CLEARED. IN OFF, AND APPROXIMATELY 1 MINUTE LATER, REAPPEARED IN STANDBY. REMOVED AND REPLACED LT WING STANDBY THERMAL SWITCH IAW AMM 30, OPS CHECK GOOD. (K)SDR A6WA200740682Filter · inoperativeRT PACK HIGH PRESS CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF AT APPROXIMATELY 20 KNOTS, BTMS READINGS=2,2,1,2. REMOVED AND REPLACED RT ENGINE PRESSURE REGULATING SHUTOFF VALVE FILTER, REF AMM 21-51-43 AND AWAC SUPPLEMENT 06-039. (K)SDR A6WA200740684Cable · inoperativeLOUD WHISTLING NOISE COMING FROM MAIN CABIN DOOR, LOUDEST JUST AFTER TAKEOFF. REMOVED AND REPLACED ICE BREAK CABLE IN PRESSURE RELIEF DOOR. REF AMM 52-11-15, OPS TEST GOOD. (K)SDR A6WA200740703Idg · inoperativeON T/O ROLL RECEIVED (IDG 2) CAUTION MESSAGE FOLLOWED BY (GEN 2 OFF) CAUTION MESSAGE. ABORTED T/O AT APPROXIMATELY 70 KNOTS, MAX BTMS READINGS = 3,3,2,3. FOUND FAULT MESSAGE CHANGED AFTER IDG WAS PREVIOUSLY CHANGED FROM (NR 2 GEN OFF) MESSAGE TO (IDG 2) MESSASDR A6WA200740700Bracket · crackedCARGO DOOR CONNECTOR BRACKET CRACKED. (K) CARGO DOOR CONNECTOR BRACKET FABRICATED AND INSTALLED IAW SRM 51-24-15 AND 51-42-06.SDR VNAA0712003Ecu · malfunctionedCREW REPORTED A FLAPS FAIL IN FLIGHT ON FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND FOUND IT TO BE FLAGGING THE FLAP HANDLE MIS-POSITION. MAINTENANCE RESET THE FECU AND PERFORMED A SYSTEM OPSSDR VNAA0712001Static Wick · damagedCREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND TWO DAMAGED STATIC WICKS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICSDR CA071217009Actuator · malfunctioned(CAN) ON APPROACH THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER SELECTING THE FLAP LEVER TO 8 DEGREES. THE EICAS FLIGHT CONTROL PAGE WAS SHOWING THE FLAP POSITION AT 2 DEGREES. THE CREW REQUESTED EMERGENCY SERVICES AND LANDED WITHOUT FURTHER INCIDENT. SDR A6WA200740678Warning Message · illuminatedWING OVERHEAT WARNING MESSAGE ON CLIMBOUT, SYNOPTIC PAGE INDICATES LT WING. CORRECTIVE ACTION IN PROGRESS. (K)SDR A6WA200740692Bulkhead · crackedCRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE AT FS 202.00 LT LBL 23.00. CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE REPAIRED IAW REO 601R53-11-563. (K)
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