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 = '7ECA' 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 = '7ECA' 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 CA010522018Clevis Bolt · bent(CAN) BRAKES WERE NOT AS RESPONSIVE AS USUAL. UPON INSPECTION RT MASTER BRAKE CYLINDER CLEVIS BOLT FOUND TO BE BENT.SDR 2002FA0000253Spar · crackedWHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FOREWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG.SDR 20010419CW012Spar · crackedA LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR, APPROXIMATELY 30 INCHES LONG.SDR 20001229SH011Float · damagedCARBURETOR WAS OVERFILLING. UPON DISASSEMBLY, FOUND CARBURETOR GASKET, PN 16-B85, SAGGING AND THE METAL FLOAT, WHERE THE NEEDLE SEAT RUBS, WORN EXCESSIVELY AT THE FLOAT LEVER ADJUSTMENT TAB. (X)SDR 99ZZZX2381Spar · crackedWOOD SPAR (AFT) COMPRESSION CRACK, MID-SPAN AT COMPRESSION STRUT CRACKED FROM TOP SURFACE DOWN TO BOLT HOLE (COMPRESSION STRUT).SDR 99ZZZX1641Nut · missingDURING ANNUAL INSPECTION, COTTER PIN AND NUT WERE FOUND MISSING FROM UP ELEVATOR CABLE ATTACH AT REAR CONTROL STICK. ELEVATOR CABLE PULLEYS UNDER AND AFT OF BAGGAGE AREAS WERE FOUND VERY DRY. CABLES WERE FRAYED AT PULLEY LOCATIONS. THESE AREAS ARE NOT EASILSDR 99ZZZX193U Bolt · failedTHE LT MLG LEG DEPARTED THE AIRCRAFT DURING LANDING ROLL-OUT. SUBSEQUENT INVESTIGATION DISCLOSED A FATIGUE FAILURE AT THE FORWARD ATTACH POINT OF THE GEAR LEG U-BOLT, BELLANCA P/N 1-9805. THIS CONDITION INDUCED THE INSTANTANEOUS FAILURE OF THE REAR ATTACH POSDR 98ZZZX3062Spar · damagedWHILE INSPECTING THE WINGS FOR THE UPCOMING WOOD SPAR AD, FOUND SWIRL AREA WHERE THE SPAR HAD BEEN CHEWED BY MICE. THE AREA HAD BEEN VARNISHED OVER AT THE LAST RECEIVER AND SIGNED OFF. SUBMITTER RECOMMENDED THAT ACFT WITH WOOD SPARS BE CHECKED CLOSER FOR STOSDR 98ZZZX3061Spar · damagedWHILE INSPECTING THE WINGS FOR THE UPCOMING WOOD SPAR AD, FOUND SWIRL AREA WHERE THE SPAR HAD BEEN CHEWED BY MICE. THE AREA HAD BEEN VARNISHED OVER AT THE LAST RECEIVER AND SIGNED OFF. SUBMITTER RECOMMENDED THAT ACFT WITH WOOD SPARS BE CHECKED CLOSER FOR STOSDR 98ZZZX1119Control Cable · failedTHROTTLE CABLE BROKE APPROXIMATELY 1.5 INCHES FROM THROTTLE LEVER. OLDER AIRCRAFT USED QQ-2-470 MUSIC WIRE .090 INCH DIAMETER. INNERGRANULAR CORROSION WAS NOTED IN THE BROKEN AREA. SUBMITTER RECOMMENDED CABLE BE REPLACED WITH 20253-P2 PIN MATERIAL OR UPGRADSDR CA970923001Cylinder · failed(CAN) FACTORY NEW CYLINDER INSTALLED ON ANNUAL INSPECTION. AIRCRAFT TEST FLOWN AND PARKED. NEXT MORNING ON START UP THE ENGINE RAN ROUGH. INVESTIGATION FOUND NR4 CYLINDER INTAKE VALVE SEAT DISLODGED. NR4 CYLINDER REPLACED.SDR 97ZZZX3897Tube · brokeFOUND LEFT MAIN GEAR FOLDED ON LANDING. 7-1290-12 TUBE BROKE AT PREVIOUS WELD REPAIR WHERE LEFT MAIN GEAR ATTACHES. NO ENTRY FOR REPAIR IN LOGS. WELDS WERE NOT AIRWORTHY. NO PENETRATION, SIGNS OF PREVIOUS CRACKING AND CORROSION INSIDE WELDS.SDR 97ZZZX3890Wrist Shaft · pin worn1974 AND LATER, 73CA CITABRIA AIRCRAFT WHICH UTILIZE TOE BRAKES. AT APROXIMATELY 1,700 HOURS TT, FOUND WRIST PINS IN RUDDER/BRAKE PEDAL WORN TO ALMOST FAILURE. LOSS OF PIN WOULD INTERFERE WITH BRAKE OR RUDDER ACTION.SDR CA970407005Nipple · worn(CAN) GASCOLATOR FOUND LOOSE IN ITS MOUNTING BRACKET. NIPPLE REMOVED AND FOUND CHAFED 90 TO 95 PERCENT THROUGH THE WALL FROM THE FIREWALL AS THE NIPPLE PASSES THROUGH A HOLE IN FIREWALL. DESIGN OF GASCOLATOR DOES NOT PERMIT USE OF BULKHEAD FITTING TO SECURE USDR CA951211013Bracket Assy · broken(CAN)TAKING OFF THE WHEEL TO INSTALL THE TAIL SKI THE FORK ASSEMBLY CAME OFF COMPLETELY FROM THE BRACKET ASSEMBLY DUE TO THE INTERNAL FRACTURE OF THE BOLT HOLDING THE FORK TO THE BRACKET. SUBMITTER STATES THAT PART SHOULD BE INSPECTED EVER Y 500 HOURS AND THA
Back to Champion 7ECA