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 REXA2016030300399Structure · gougedRIGHT LOWER CORE COWL BOTH ALIGNMENT PIN HOLES ARE GOUGED. FABRICATED LOCATED, & INSTALLED 2 DOUBLER PLATES 2024 T3 .080 IAW CMM 71-12-01.SDR CA160222003Connector · contaminated(CAN) UPON SELECTING FLAPS 30 DEGREES DURING THE APPROACH, FLIGHT CREW RECEIVED A FLAPS FAIL AMBER CAUTION MESSAGE. THE APPROACH WAS CONTINUED AND THE AIRCRAFT LANDED WITH FLAPS AT 20 DEGREES WITHOUT FURTHER INCIDENT. TROUBLESHOOTING DETERMINED THE FLAPS FAIL SDR SWIA201641881Relay · failedRT THRUST REVERSER UNLOCK IN FLIGHT, DIVERTED. INSTALLED NEW THROTTLE LOCKOUT/STOW RELAY 2K7K3 INTO JB4. OPS CHECKED GOOD.SDR REXA2016021000193Seal · crackedLOWER EDGE OF LOWER FWD OTBD SEAL ON NR 1 ENG THRUST REVERSER TORQUE BOX IS CRACKED. R & R LOWER EDGE SEAL IAW CMM 78-30-00.SDR REXA2016020700199Stiffener · crackedNUMBER 1 ENG EXHAUST FAIRING HAS CRACKED STIFFENER. R & R NR 1 ENG EXHAUST FAIRING STIFFENER IAW MM 20-42-06.SDR REXA2016020200144Support Angle · brokenRIGHT UPPER THRUST REVERSER TRACK STAND FAIRING, SUPPORT Z ANGLE BROKEN. R & R SUPPORT Z ANGLE IAW MM 20-42-06.SDR CA160202002Paint · missing(CAN) DURING HEAVY MAINTENANCE, INTERNAL FUEL TANK INSPECTION, LT WING, LARGE SECTIONS OF PAINT WERE OBSERVED TO BE MISSING FROM INSIDE THE TANK. THE AREAS WERE REPAIRED IAW SRM 51-25-34.SDR CA160201004Lock Nut · wrong part(CAN) UPON DISASSEMBLY OF THE AFFECTED ENGINE AND MODULE ASSY IT WAS DISCOVERED THE PART NUMBER OF THE NO 7 BEARING LOCKNUT REMOVED WAS NOT FOUND IN THE OEM APPROVED IPC. THE PART NUMBER OF THE PART REMOVED WAS 4019T66P01 WHILE THE APPROVED PART NUMBER LISTED SDR SWIA201641768Thrust Reverser · failedLEFT REVERSER UNLOCKED CAUTION MESSAGE IN FLIGHT. RAN QRH, MESSAGE PERSISTED. DIVERTED. R & R LT ENGINE THRUST REVERSER PDU IAW AMM. OPS CHECK GOOD.SDR A6WA201643481Gearbox · bindingLEFT THRUST LEVER BINDS IN FLIGHT, BOTH ADDING & REDUCING THRUST. R & R LT THROTTLE CONTROL GEARBOX IAW AMM 76-11-17. OPERATIONS CHECKED GOOD AT THIS TIME, RII COMPLIED WITH.SDR REXA2016011400057Angle · crackedNUMBER 1 ENG INLET NOSE COWL, CRACKED SPRING ANGLE AT 6 O'CLOCK POSITION AFT OF PDU. R & R DAMAGED SPRING ANGLE ON NR 1 ENG INLET NOSE COWL AT 6 O'CLOCK POSITION IAW CMM 20-42-13.SDR CA160113005Wire · burned(CAN) 1B HYD ACMP WOULD NOT COME ONLINE (ELECTRIC PUMPS - ACMP 1B). WIRES DB44B12WHT, DB4512BLU AND WIRE DB46ORN WERE SHORTED TOGETHER UNDER CABLE TIE 2` AWAY FROM HYDRAULIC PUMP 1B. A SECTION OF THE WIRES WAS REPLACED. THEY WERE SPLICED IAW STANDARD PRACTICESSDR VNAA2016010500007Clamp · looseON TAKEOFF AT ABOUT 2,000 FT, CREW RECEIVED LT 14 DUCT WARNING MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CLAMP AT LT ENGINE COWLING ANTI-ICE DUCT INSIDE PYLON LOOSE AND LEAKING. MAINTENANCE REINSTALLED CLAMPSDR VNAA2016010300004Warning Message · illuminatedCREW REPORTED LT REVERSER UNLOCKED CAUTION MESSAGE APPEARED INTERMITTENTLY SEVERAL TIMES DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LT THRUST REVERSER IAW MEL. ACFT RELEASED FOR SERVICE.SDR CA160108006Cowling · departed(CAN) INVESTIGATING AN EVENT AS RESULT OF THE RT ENGINE UPPER FAN COWL DEPARTING THE ACFT. MORE DETAILS HAVE BEEN REQUESTED TO OPERATOR. IT WAS A PRE-MOD ACFT, BUT ROOT CAUSE IS HUMAN FACTOR, TURNOVER BETWEEN SHIFTS NOT PROPERLY DONE.SDR VNAA2016010100001Wire Harness · chafedCREW REPORTED N2 SPLIT AND N2 VIBRATION WARNING. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND ENGINE VIBRATION MONITORING CABLE ASSY CHAFED AND BROKEN. MAINTENANCE R & R ENGINE VIBRATION MONITORING CABLE ASSEMBLY SDR CA160113009Bpsu · failed(CAN) FLAP FAIL EVENT REPORTED, IN FLIGHT AT EXTENSION, FLAP FAILED AT 20SDR A6WA201543426Pressure Switch · defectiveCLIMBING THROUGH 17,000, RT ENG OIL PRESS WARNING MSG, CLEARED THEN RETURNED MULTIPLE TIMES, RAN QRH & RETURNED. OIL PRESS READ 65 PSI & NORMAL. R & R VIOLET HARNESS ON RT ENG IAW AMM 71-50-00. R & R LOW OIL PRESS SWITCH IAW AMM 79-31-03. OPERATIONS CHECK SDR SWIA201541707Transducer · malfunctionedACFT RETURNED TO DEPARTURE AFTER THE RT ENGINE OIL PRESSURE WENT TO ZERO ON CLIMB OUT. CREW FOLLOWED THE QRH PROCEDURE AND SHUTDOWN THE RT ENG. CREW REPORTED THAT THEY DID NOT LAND OVERWEIGHT AND THEY DID DECLARE AN EMERGENCY. R & R NR 2 ENGINE OIL PRESSURESDR CA160113010Bpsu · failed(CAN) FLAP FAIL EVENT REPORTED, IN FLIGHT AT EXTENSION, FLAP FAILED AT 20 LT BPSU 855D100-15 RT BPSU 855D100-15.SDR REXA2015122201249Support · brokenLEFT ENG NOSE COWL INLET, HAS A BROKEN SUPPORT ASSEMBLY THAT HOLDS THE BROWN WIRE ASSEMBLY. LOCATED AT THE 1 O'CLOCK POSITION. REPAIRED LT ENG NOSE COWL INLET SUPPORT BRACKET ASSEMBLY IAW REO 601R-71-613941 REV A DATED 04 27 10. SDR REXA2015121601234Torque Box · crackedNUMBER 1 ENG THRUST REVERSER TORQUE BOX TE IS CRACKED AT 6:30 POSITION. REPAIRED CRACK TO NR 1 ENG THRUST REVERSER TORQUE BOX AT THE 6:30 POSITION IAW REO 601R-78-30-2616.SDR VNAA2015121100008Idg · failedCREW REPORTED GENERATOR NR 2 FAILED AT 50 KIAS ON TAKEOFF ROLL. CREW ABORTED TAKEOFF. GENERATOR NR 2 DEFERRED IAW MEL AND CREW CONTINUED FLIGHT. MAINTENANCE SUBSEQUENTLY TROUBLESHOT, R & R RT INTEGRATED DRIVE GENERATOR AND PERFORMED CHECKS IAW AMM. DEFERRASDR A6WA201543295Skin · crackedLEFT LOWER CORE COWL OUTER SKIN AT NR 4, LATCH IS CRACKED, REPAIRED.SDR CA151123004Light · failed(CAN) IN CRUISE, FLIGHT CREW STARTED TO SMELL SMOKE AND OBSERVED ARCING NEAR THE NOSEWHEEL STEERING SWITCH. CREW DONNED THEIR OXYGEN MASKS, DECLARED AN EMERGENCY AND DIVERTED TO A NEARBY AIRPORT. SHORTLY AFTER CIRCUIT BREAKER 4-C1 INST FLOOD LTG POPPED AND SMOSDR REXA2015111101072Cowling · chafedRIGHT ENG UPPER FAN COWL HAS SEVERAL CHAFED AREAS ALONG TE. R & R RT ENG UPPER FAN COWL TE IAW CMM 71-41-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090. REQUIRES AFT ESDR REXA2015111101077Panel · chafedLEFT ENG, LOWER FAN COWL PANEL 432AB, TE IS CHAFED IN SEVERAL AREAS. R & R LT ENG LOWER FAN COWL TE IAW CMM 71-14-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090, REQUIRSDR A6WA201543195Pcu · malfunctionedUPON LANDING, EXPERIENCED ABNORMAL YAW MOTION WITH THRUST REVERSERS DEPLOYED, LT ENG SLOWER TO SPOOL THAN RT ENG. ACCOMPLISHED THRUST REVERSER OPERATIONS CHECK IAW AMM 71-00-00-710-806. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED. PERFORMED CHECK IAW FIM 73-2SDR CA151029026Pdu · failed(CAN) FLAP HALFSPEED MESSAGE ON TAXI OUT - EXTENDING FLAPS FROM ZERO OT 8. CB RESET OK. AFTER TAKEOFF ON RETRACTION FLAP HALFSPEED MESSAGE CAME BACK. DECISION TO RETURN A/C TO AIRPORT. (FLAP SKEW DET. SYSTEM. M TO DEACTIVATE) MAINTENANCE FOUND FLAP POWER DRIVESDR CA151030014Tire · separated(CAN) ON APPROACH AS THE CREW WAS CONFIGURING THE AIRCRAFT FOR LANDING THEY RECEIVED INDICATION THAT THE NR 2 HYDRAULIC SYSTEM FAILED AS THEY WERE EXTENDING THE FLAPS. THE CREW DID A GO AROUND, RAN THE CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT CAME AROSDR CA151026009Hinge Fitting · corroded(CAN) CONFIRMED SIGNS OF CORROSION IN THE BORE OF SEVERAL LUGS OF THE RUDDER MID HINGE FITTING. IN ADDITION TO THAT, THE UPPER AND LOWER RUDDER HINGE FITTING BUSHINGS HAVE ALSO BEEN REMOVED FROM THE LUGS DUE TO SUSPECTED CORROSION. IT IS CONFIRMED THAT CORROSDR CA151023003Web · cracked(CAN) CRACKS FOUND ON PRESSURE FLOOR WEB AT BS 460 LBL 9. REPAIRED IAW REO 601R-53-41-1826.SDR A6WA201543121Torque Box · crackedRIGHT ENG TORQUE BOX CRACKED AT 8 O CLOCK AM PANEL MOUNT. REPAIRED RT ENG TORQUE BOX IAW REO 601R-78-30-2553 REV A DATED 26 MAY 2004.SDR CA151009008Channel · corroded(CAN) DURING MAINTENANCE CHECK, CORROSION FOUND AT BULKHEADS BS 755.SDR CA150923013Actuator · malfunctioned(CAN) FLAP FAIL CAUTION ILLUMINATED INBOUND THEN ON APPROACH FLAPS SELECTED TO FLAP 8 AND THE FLAPS FAIL CAUTION LIGHT ILLUMINATED IMMEDIATELY. CREW REPORT THAT THEY DID NOT ENCOUNTER AND ICING OR RAIN ON ROUTE. THEY DID PASS THROUGH A CLOUD LAYER. OAT AT TIMESDR A6WA201543061Engine · malfunctionedRECEIVED VIBRATION & HEARD LOUD BANG, THEN SAW N1 & N2 ON LT ENG DECREASING & ITT RISING UNTIL IT EXCEEDED 900 DEG C. PULLED LT ENG BACK TO IDLE UNTIL SHUTDOWN, CHECKLIST COULD BE COMPLETED. N1 & N2 CONTINUED TO ROTATION, ITT WENT TO ALMOST ZERO. VIBRATION SDR CA150909002Mount Bracket · cracked(CAN) MAINTENANCE OBSERVED CRACKS ON THE LT ACM FORWARD MOUNTING BRACKET. BRACKET REPLACED AS PER APPROVED REFERENCE.SDR CA150908012Skin · cracked(CAN) CRACK ON LBL & RBL 18.00 LOWER CAP AT BS 559.SDR A6WA201543039Engine · surgesLEFT ENG ITT AT IDLE IS 590 DEGREES C & RT ENG ITT AT IDLE IS 480 DEGREES C. AT TAKEOFF POWER 91%, LT ENG WAS SLOW TO SPOOL UP, ITT IMMEDIATELY WENT TO 900 DEGREES C & AN AUDIBLE SURGE WAS HEARD FROM LT ENG. PERFORMED ENG POWER ASSURANCE CHECK IAW AMM 71-00-SDR CA150904007Sensor · failed(CAN) DURING CLIMB OUT OF DEPARTURE POINT, AFTER SELECTING FLAPS FROM 8 TO ZERO, CREW RECEIVED A FLAP FAIL MESSAGE GOING THROUGH 23000 FEET. CREW EXERCISED QRH AND LANDED FLAPLESS INTO DESTINATION. MAINTENANCE ACTION REVEALED BRAKE POSITION SENSOR UNIT AT FAUSDR A6WA201543013Carbon Seal · defectiveRECEIVED LT ENG OIL PRESS WARNING ENROUTE. WARNING WAS INTERMITTENT. ENG LEFT AT IDLE FOR DURATION OF FLIGHT. COMPLIED WITH QRH. LOWEST KNOWN OIL PRESS WAS 29 PSI. LOW OIL PRESS WARNING LASTED NO LONGER THAN 10 SECONDS. PERFORMED CONSUMPTION RUN & FOUND SDR CA150901012Control Valve · failed(CAN) BRAKE TEMP INDICATION APPEARS TO BE INDICATING CORRECTLY. ON ARRIVAL NR 1 BRAKE WAS FOUND COLD TO THE TOUCH AND NR 2 WAS SUBSTANTIALLY HOTTER. TAXI TEST REQUIRED TO VERIFY ANY CHANGE IN BRAKING AND TEMP INDICATIONS. GROUND TAXI TEST CARRIED OUT. NR 1 BRASDR A6WA201543008Attach Bracket · crackedRIGHT ENG OUTER NOSE COWL, ATTACH SUPPORT BRACKET CRACKED. R & R RT OUTER NOSE COWL ATTACH BRACKET IAW SRM 51-40-11 & SRM 51-41-02.SDR CA150908014Engine · power loss(CAN) DURING THE TAKEOFF ROLL, FLIGHT CREW IDENTIFIED THAT THE NR 1 ENGINE N1 WAS NOT ACHIEVED FOLLOWING APPLICATION OF THRUST. THE TAKE-OFF WAS ABORTED AND THE THRUST LEVERS WERE BROUGHT TO IDLE. THE FLIGHT CREW NOTED AT IDLE THRUST THAT THE NR 1 ENGINE N1 WASDR A6WA201542997Engine · bird ingestionBIRD STRIKE RT ENG AFTER TAKEOFF, ROTATION VIB FELT IN ACFT, N1 FAN BLADES. ENG VIB WENT FROM .3 TO 2.1, LANDED UNDERWEIGHT. VIBE FELT IN FEET & YOKE.SDR CA150825003Shaft · broken(CAN) FLEX FLAP DRIVE FAILED ON THE OUTBD RT OTBD FLAP ACTUATOR .SDR CA150824011Actuator · overheated(CAN) THE CREW PERFORMED A FLAP ZERO LANDING DUE TO A FLAP FAILURE. THERE WAS NO EMERGENCY DECLARED AND THE FA WAS ADVISED OF AN ABNORMAL LANDING. THE FLAPS WERE DEFERRED BY MEL 27-02 AND LATER INVESTIGATED BY MAINTENANCE. IT WAS DETERMINED THAT 2 ACTUATORS SDR VNAA2015081200019Carbon Seal · leakingCREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE ACCESSORY GEARBOX CARBON SEAL FOR INTEGRATED DRIVE GESDR VNAA2015081200020Carbon Seal · leakingCREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE ACCESSORY GEARBOX, AGB, CARBON SEAL FOR AIR TURBINE SSDR VNAA2015081200021Carbon Seal · leakingCREW REPORTED LT ENGINE OIL PRESSURE WARNING MESSAGE AND OIL PRESSURE OSCILLATION. CREW RAN QRH, INTENTIONALLY SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND DIVERTED. MAINTENANCE INSPECTED, R & R LT ENGINE AGB CARBON SEAL FOR ENGINE DRIVEN PUMP AND PERFORMED
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