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 = '525C' 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 = '525C' 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 7GOR20151130001Module · failedLOSS OF BRAKE ACTUATION.SDR YGJA2015FA0000413Warning Message · false activationPRIOR TO LANDING, A CAS MESSAGE APPEARED, LOW BRAKE PRESSURE. ON TOUCHDOWN THE ACFT HAD NO BRAKES, EMERGENCY BRAKE SYSTEM WAS ACTIVATED TO STOP THE PLANE. MAINTENANCE LOOKED INTO THE SITUATION FOUND NO ISSUES. COULD NOT DUPLICATE DISCREPANCY. ON SUBSEQUENT FSDR AMCR2015051502Terminal · brokenCREW REPORTED LT GEAR DISAGREE LIGHT GOING ON AND OFF THROUGHOUT FLIGHT. MAINTENANCE DISCOVERED THAT THE GROUND WIRE FROM THE LT GEAR UPLOCK SWITCH HAD BROKEN FROM THE CRIMP AT ACFT ELECTRICAL GROUND GLSSS01. THIS IS LOCATED IN THE T/E OF THE LT WING ROOT. WISDR CA150224031Actuator · cracked(CAN) HYDRAULIC FLUID WAS NOTICED DRIPPING FROM THE RT MLG UPLOCK ACTUATOR RETURN LINE END CAP FITTING. FURTHER TROUBLESHOOTING REVEALED A CRACK IN THE -4 END CAP FITTING THREADS (POSSIBLY FROM AN OVER TORQUED CONDITION).SDR AMCR2014082107Actuator · failedCREW RECEIVED A "PITCH TRIM FAIL" CAS MESSAGE. TRIM FAILED IN PRIMARY MODE, BUT WORKED IN SECONDARY MODE. PERFORMED AN ARES DOWNLOAD FOR MFG AND DATA CONFIRMED THAT THE LT ELEVATOR TRIM ACTUATOR HAS FAILED.SDR AMCR2014060406Actuator · failedCREW RECEIVED A PITCH TRIM FAIL CAS MESSAGE. PERFORMED DOWNLOAD FOR MFG AND DATA REVEALED THE LT ELEVATOR TRIM ACTUATOR HAD FAILED.SDR AMCR2014040705Fitting · crackedMAINTENANCE NOTED HYDRAULIC FLUID WAS ON FLOOR UNDER RT MAIN LANDING GEAR WHEEL WELL. INSPECTION REVEALED THE SOURCE TO BE A CRACKED UPLOCK ACTUATOR FITTING, OTBD END. WHEN B-NUT WAS REMOVED, DISCOVERED A .1250" CRACK ON THREADED PORTION OF ACTUATOR. BOTH TSDR AMCR2014020602Flex Hose · kinkedDURING GEAR SWING, AFTER UPLOCK ACTUATOR REPLACEMENT, NOTED THAT THE BRAKE HYDRAULIC HOSE FROM FORWARD SPAR TO THE TRUNNION BRACKET ON TOP OF THE RT MLG WAS KINKING DURING THE UPSWING AT ABOUT 30 DEGREES UP FROM THE DOWN AND LOCKED POSITION. AS THE GEAR PROGRSDR AMCR2014020601Actuator · crackedDURING A PREFLIGHT CHECK, MAINTENANCE NOTED HYDRAULIC FLUID LEAKING FROM LT MAIN GEAR UPLOCK ACTUATOR AT OTBD END OF THE B-NUT. FOUND THAT THE END OF THE ACTUATOR HOUSING WAS CRACKED PERPENDICULAR TO THE THREADS FROM THE B-NUT END IN TOWARD THE MAIN BARREL OFSDR CA131212004Pcb · overheated(CAN) SPEED BRAKES FAIL ANNUNCIATED ON CAS AT FL 450. NO ADVERSE FLIGHT CONTROL EXPERIENCED AND CONTINUED FLIGHT TO UNEVENTFUL AND SAFE LANDING CARRIED OUT. TROUBLESHOOTING CONFIRMED PHYSICAL AND VISUAL OVERHEAT DAMAGE TO PCB NC106. REPLACEMENT OF THE PCB RECSDR AMCR2013091604Circuit Breaker · brokenDURING REINSTALLATION OF THE PS855A EMERGENCY BATTERY, WENT TO RESET THE 25A CIRCUIT BREAKER AND THE BREAKER BUTTON PUSHED INTO THE CASE. DISCOVERED THAT THE NECK ON THE BREAKER WAS BROKEN, WHICH CAUSES THE BODY OF THE BREAKER TO PUSH IN FURTHER RATHER THAN RSDR WI5R201308230002Blade · missingENGINE WAS FLAGGED FOR A POTENTIAL ISSUE. DURING BLEED SOURCE SELECTION FROM BOTH TO LT, A LOUD NOISE AND A SUDDEN RISE IN ITT ON THE LT ENGINE. TROUBLESHOOTING REVEALED A MISSING 3RD STAGE IP BLADE.SDR CNQR525C00072013Warning Light · illuminatedAFTER TAKEOFF, RECEIVED AN ENGINE CONTROL FAULT ON THE LT ENGINE.SDR AMCR2013032202Fitting · crackedWHEN TROUBLESHOOTING AN INOP CHECKLIST MGMT SYS, PULLED FLOORBOARD IN FORWARD CABIN TO ACCESS THE CHECKLIST BOX AND FOUND BOX TO BE WET, AND ABOUT 3.5 GALLONS OF WATER IN THE FORWARD SECTION OF THE FUSELAGE BELLY, WHERE NO FUSELAGE DRAINS ARE INSTALLED. ALSOSDR AMCR2013030101Connector · looseDURING REPLACEMENT OF THE RELIEF TUBE DRAIN HEATER, FOUND THE WIRES FROM THE ORIGINAL HEATER SLEEVE TO SPLICES AT027 AND AT028 WERE UNDER-CRIMPED AND EASILY PULLED THE WIRE FROM THE PIN SOCKET. ALSO, THE INSULATION WAS OVER-STRIPPED, EXPOSING TOO MUCH WIRE BESDR CNQR2012080886796Pin · backed outRIGHT MLG COLLAPSED WHILE ACFT WAS TAXING IN FROM LANDING. AFT TRUNNION PIN WAS INSTALLED INCORRECTLY, THE AN3-42 RETAINING BOLT WAS NOT THROUGH THE PIN AS NEEDED TO RETAIN THE TRUNNION PIN IN THE TRUNNION ASSY. A REVIEW OF ACFT ONSITE AT THE REPAIR STATION SDR AMCR2012051706Brake Pads · debondedBRAKE PAD ON BOTH LEFT AND RIGHT SIDE BRAKE ROTORS DEBONDING, WITH CHUNKS MISSING.SDR AMCR201201180002Coax · misinstalledCREW REPORTED THAT THE TCAS DISPLAY WAS INCORRECTLY PAINTING TARGETS AT 45 DEG TO THE LT OF WHERE IT SHOULD HAVE BEEN, BASED ON VISUAL AND ATC VERIFICATION. CREW EXPERIENCED SIMILAR PROBLEM ON AN EARLIER SN ACFT (0049, 19 HRS TT) A FEW MONTHS PRIOR. MX FOUND
Back to Textron 525C