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 aircraft_model_key = '407' 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 aircraft_model_key = '407' 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 HEEA0011472Exhaust Stack · crackedEXHAUST STACK CRACKED.SDR HEEA0011464Transmitter · failedFUEL PRESSURE PEGS OUT INTERMITTENTLY.SDR HEEA0011463Disk Coupling · crackedONE DISC ON COUPLING FOUND CRACKED ON DAILY INSPECTION.SDR 97ZZZX4901Coupling · crackedDAILY INSPECTION FOUND NR 7 TAIL ROTOR DRIVESHAFT COUPLING, NR 10 DISC ON PACK CRACKED.SDR 97ZZZX4932Disc Pack · crackedDAILY VISUAL INSPECTION OF TAILBOOM IAW NOTAM NR 51A-97, NR 5 TO NR 6 DISC PACK (T/R D/S) ASSEMBLY. ONLY ONE DISC FOUND CRACKED IN THE NR 10 POSITION OUT OF 10 DISCS. 57.8 HOURS TOTAL TIME ON DISC PACK FROM LAST CRACKED DISC.SDR HEEA0011418Transmitter · faultyFUEL PRESS TRANSMITTER WON'T COME ON LINE UNTIL CIRCUIT BREAKER IS PULLED AND PUSHED BACK IN.SDR HEEA0011415Indicator · failedINDICATOR NO TOTAL READING.SDR HEEA0011414Transmitter · failedFALSE INDICATION.SDR HEEA0011407Frahm Assy · defectiveVIBRATIONS, UNABLE TO BALANCE M/R SYSTEM.SDR 97ZZZX4711Frahm Assy · wornRUBBER BOOT CAME LOOSE AND SPRINGS ROTATED INSIDE FRAHM. HELICOPTER HAD A 4 PER VIBRATION AND COULD NOT BE ELIMINATED. REPLACED FRAHM ASSY AND BALANCED HELICOPTER ROTOR SYSTEM TO ACCEPTABLE LEVELS.SDR 97ZZZX4706Seal · leakFREEWHEELING UNIT FORWARD SEAL LEAKS EXCESSIVELY. REPLACED SEAL AND CORRECTED LEAK. AIRCRAFT TT: 135.5 HOURS.SDR HEEA0011260Support · mis identifiedSUPPORT IS MARKED FOR L/H SLAT SUPPORT P/N 206-023-119-109. PART IS FOR A R/H SLAT SUPPORT P/N 206-023-119-110.SDR HEEA0011227Receiver · malfunctionDOES NOT RECEIVE SATELLITES. FOUND LOOSE SCREW IN UNIT AND ALSO MISSING SCREW ON RECEIVER COVER. NEW DATE 6-30-97.SDR HEEA0011212Transponder · inoperativeINOPERATIVE. NO REPLY LIGHT. FOUND DS5 BULB BAD. REPLACED DS5 BULB AND ADJUSTED FREQUENCY TO SPECS. REPAIRED UNIT. BENCH CHECK GOOD.SDR HEEA0011211Indicator · failedOIL TEMP SECTION FAILED - DROPPED TO ZERO IN FLIGHT.SDR 97ZZZX4401Disc Pack · crackedDAILY INSPECTION IAW MAINTENANCE NOTAM 51A-97, NR 3 DRIVE SHAFT, FOUND 3RD DISC IN PACK WAS CRACKED.SDR HEEA0011180Carbon Seal · leakingPITTTED SEAL LEAKING.SDR CA971021023Disc Pack · cracked(CAN) AS PER AD CF-97-19, INSPECTION OF TAIL ROTOR DRIVE SHAFT THOMAS COUPLINGS CARRIED OUT. THE AFT OUTER DISC OF THE NR 7 DISC PACK WAS FOUND BROKEN IN TWO PLACES. DISC PACKS TAKEN FOR TESTING BY BELL. BHTC IS REDESIGNING DISCS TO OVERCOME MID-SPAN CRACKISDR 97ZZZX4421Disc Pac · crackedDURING DAILY INSPECTION, C/W MAINTENANCE NOTAM 52-97, FOUND CRACKED DISK IN DISC PACK.SDR GCHR0000020Frame · crackedFRAME IS CRACKED. DURING O/C SHAFT-ADAPTER INSPECTION, NUTPLATE WAS FOUND CRACKED. UPON FURTHER INSPECTION, 127 FRAME WAS ALSO FOUND CRACKED. REMOVED AND REPLACED FRAME. (X)SDR GCHR0000019Angle · crackedANGLE IS CRACKED. DURING O/C SHAFTING INSPECTION, THE O/C WAS REMOVED. WHEN TRYING TO SECURE THE ATTACHING HARDWARE TO PREVENT LOSS, THE MECHANIC REMOVED AND REPLACED ANGLE. (X)SDR GCHR0000017Bearing · roughPART IS ROUGH. FOUND FORWARD BEARING WORN WHEN REPLACING O/C DRIVESHAFT AND ADAPTER. REMOVED AND REPLACED BEARING. (X)SDR GCHR0000016Shaft · wornSHAFT IS DIMENSION UNDER MINIMUM. PRODUCT ENGINEERING RECOMMENDS REPLACE SHAFT WITH 407-040-316-101 ADAPTER. (X)SDR GCHA0000014Adapter · wornPART IS DIMENSION OVER MAXIMUM. SPLINES WORN. SUSPECT IMPROPER TYPE/LACK OF LUBRICATION FROM FACTORY. REMOVED AND REPLACED ADAPTER AND SHAFTING, BEARINGS AND RETAINING WASHERS REPLACED. CYCLES: 215. (X)SDR 97ZZZX4416Coupling Disk · crackedDURING DAILY INSPECTION, FOUND NR 7 TAIL ROTOR DRIVESHAFT FORWARD LAMINATE CRACKED.SDR 97ZZZX4402Disc Pack · crackedDURING DAILY INSPECTION IAW MAINTENANCE NOTAM 51A-97, FOUND NR 6 TAIL ROTOR DRIVESHAFT, NR 1 DISC IN PACK CRACKED.SDR HEEA0011126Seat · crackedLOWER CONE SEAT CRACKED.SDR HEEA0011114Transponder · malfunctionTRANSPONDER DEFECTIVE. WITH 6033 CODE IN TRANSPONDER, ATC RECEIVES 6733.SDR 97ZZZX4906Mast Nut · looseDAILY INSPECTION FOUND COMPLETE LOSS OF TORQUE ON T/R MAST NUT. THE NUT COULD BE REMOVED BY HAND. THE SAFETY WIRE BETWEEN THE NUT AND THE SUPPORT, (P/N 407-012-106-103) KEPT THE NUT FROM SPINNING OFF OF THE TAIL ROTOR GEARBOX OUTPUT SHAFT.SDR 97ZZZX4903Bearing · roughNR 2 SHAFT REMOVED FROM AIRCRAFT DUE TO ROUGH BEARING. FOUND BEARING 406-040-339-105 INSTALLED AT AIRCRAFT HOURS 808.0 HOURS ROUGH. ALSO, SHAFT 406-040-320-101, TT 1410.8 HOURS. FORWARD SPLINES WORN AND CORRODED BEYOND LIMITS.SDR 97ZZZX4902Disc Pack · crackedDAILY CHECK NOTAM 51A-97 OCCURRED DURING NORMAL FLIGHT, FOUND NR 7 COUPLING CRACKED 2 LAMINATES NR 1 AND NR 2 PACK HAS TEN DISCS.SDR 97ZZZX4900Disc · crackedDAILY INSPECTION AND C/W NOTAM NR 51A-97, FOUND DISC CRACKED. ON NR 7 DISC ASSEMBLY, NR 7 DISC OF THE PACK - 1 DISC ONLY.SDR CA971007014Skin · damaged(CAN) INSPECTION OF FINS FOUND THAT TWO GRINDING MARKS WERE MADE DURING MANUFACTURE AT AFT BOTTOM SECTION OF FORMERS FOR INSTALLATION OF FAIRINGS. AN ASB WILL BE ISSUED TO COVER.SDR 97ZZZX5133Blade · crackedPOST-FLIGHT FOUND TAILROTOR BLADE CRACKED AT INBOARD RADIUS INSIDE TOWARD LEADING EDGE. POSSIBLY STARTED AT CORROSION SPOT.SDR 97ZZZX4419Coupling Disk · crackedDURING C/W MAINTENANCE NOTAM 51A-97, FOUND 2 EACH LAMINATES CRACKED ON NR 7 TAIL ROTOR DRIVESHAFT COUPLING.SDR HEEA0011573Cone · wornREPLACED LOWER CONE AND CONE SET WITH SEAT P/N 407-010-107-103 ON 9-27-97.SDR HEEA0011572Cone · wornREPLACED LOWER CONE AND CONE SET WITH SEAT P/N 407-010-107-103 ON 9-27-97.SDR 97ZZZX4471Spring Pin · brokenPIN WAS BEING REMOVED TO INSTALL AN AN4-15A BOLT IN ITS PLACE AS A PRECAUTION AFTER THE TAIL SKID OF ANOTHER 407 AIRCRAFT FELL OFF IN-FLIGHT. WHEN THE SPRING PIN WAS REMOVED, IT CAME APART IN TWO PIECES. SUBMITTER STATED INSTALL AN4 BOLT IN PLACE OF THE SPRISDR 97ZZZX4403Disc · crackedDURING MAINTENANCE NOTAM 51A-97 INSPECTION, FOUND LAMINATE CRACKED ON NR 7 TAIL ROTOR DRIVESHAFT COUPLING DISC.SDR GCHR0000012Fadec · water contamFADEC FAILURE LIGHT ILLUMINATED IN DEPARTURE TRANSITION. PILOT SWITCHED TO MANUAL MODE AND LANDED AIRCRAFT. AIRCRAFT BEGAN ENGINE OVERSPEED, SYSTEM BACK-UPS CUT IN AND SHUT DOWN ENGINE. SYSTEM TROUBLESHOOTING FAILED TO RETRIEVE FLASH CODES. ENTRY TO ECU BSDR 97ZZZX4422Spring Pin · missingPOST-FLIGHT INSPECTION FOUND TAIL SKID ASSEMBLY HAD DEPARTED THE AIRCRAFT, SPRING PIN WAS ALSO MISSING. SPRING PIN MUST HAVE FALLEN OUT, AND THEN TAIL SKID WITHOUT SPRING PIN TO HOLD IT ON FELL OFF THE AIRCRAFT DURING FLIGHT. PILOT DID NOT NOTICE ANYTHING UNSDR 97ZZZX4979Disk · crackedSCHEDULED INSPECTION FOUND DISK PACK DISK CRACKED. REMOVED AND REPLACED. THREE REPORTS RECEIVED DATED 9-24-97 ON T/R DISK PACK DISK CRACKED.SDR 97ZZZX4978Disk · crackedSCHEDULED INSPECTION FOUND DISK PACK DISK CRACKED. THREE REPORTS RECEIVED DATED 9-24-97 ON T/R DISK PACK DISK CRACKED.SDR 97ZZZX4907Disc · crackedSCHEDULED INSPECTION FOUND DISC CRACKED.SDR 97ZZZX4418Coupling Disk · crackedDURING COMPLIANCE OF MAINTENANCE NOTAM NR 51A-97, FOUND NR 7 TAIL ROTOR DRIVESHAFT COUPLING LAMINATE CRACKED (1).SDR 97ZZZX4417Coupling Disk · crackedDURING 50-HOUR PMI, FOUND NR 3 TAIL ROTOR DRIVESHAFT COUPLING LAMINATE CRACKED (1).SDR 97ZZZX4404Coupling Disk · crackedINSPECTION FOUND NR 6 AND NR 7 EACH HAS ONE LAMINATE DISC CRACKED.SDR GCHA0000015Valve · failedPARTICLE SEPARATION. VALVE NOT WORKING - FAILS TO ACTUATE. REMOVED AND REPLACED VALVE. (X)SDR HEEA0011041Mgt Indicator · failedMGT INDICATOR LOSES DISPLAY. MUST BE RESET WITH CIRCUIT BREAKER.SDR HEEA0011039Brake · bolts wornROTOR BRAKE TWO EACH BOLT SHANKS WORN, P/N D0152-1, CAUSING ROTOR BRAKE PAD NOT T RELEASE FROM ROTOR BRAKE DISK. SUSPECT THAT HIGH HEAT FROM DISK CAUSED PAD TO FAIL. REMOVED TWO EACH BOLTS P/N D0152-1 AND 2 EACH PADS P/N D0138-1 AND REPLACED WITH SERVICEABLE
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