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 = 'U206B' 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 = 'U206B' 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 CA100601001Bungee · failed(CAN) STEERING BUNGEE FOUND VERY WEAK WHEN A/C NEW TO COMPANY BEING INSPECTED FOR ACCEPTANCE ONTO MSA. STEERING BUNGEE REPLACED BECAUSE OF PROBLEMS REPORTED LAST YEAR. IT IS BELEIVED THAT THE WEAK STEERING BUNGEE LEAD TO THE RUDDER CONTACTING THE AFT BULK HESDR 2007FA0000155Cylinder · crackedCRACKED CYLINDER HEAD BETWEEN 4TH AND 5TH FIN IB OF TOP SPARK PLUG. CRACKS HEADED TOWARD VALVE SEAT. (K)SDR CA060808006Fitting · cracked(CAN) DURING A 100 HOUR INSPECTION LOOSE RIVETS WERE NOTICED AROUND THE LT MAIN GEAR. ONCE THE FLOOR WAS LIFTED TO PERFORM THE REPAIRS, THE LT MAIN GEAR OB FITTING WAS FOUND TO BE CRACKED PROPOGATING FROM THE AFT END OF THE GEAR LEG OPENING TOWARDS THE AFT ENSDR CA060710003Throttle Control · separated(CAN) DURING A SCHEDULED 50 HOUR INSPECTION THE THROTTLE CONTROL WAS FOUND TO BE SEPARATED AT THE SWAGE AREA JUST AFTER THE CLAMP AREA ON THE ROD END END ALLOWING THE CONTROL GUIDE TO MOVE ALONG WITH THE CONTROL END POSSIBLY RESULTING IN CONTROL JAMMING. (TC NSDR CA060526004Impulse Coupling · brokenDURING FLT, PILOT NOTICED A VERY SLIGHT RPM DROP AND SLIGHT ROUGHNESS. UPON LANDING A GROUND RUN WAS PERFORMED AND WHEN THE IGNITION SWITCH WAS SELECTED TO RT MAG, ENGINE DIED OFF BEFORE SELECTING BACK TO LT OR BOTH. WHEN COWLS WERE REMOVED IT WAS EVIDENT THSDR CA050712002Bearing · unserviceableWHILE FUNCTION CHECKING THE AILERON CONTROL SYSTEM PRIOR TO FLIGHT THEY BECAME HARD TO OPERATE. THE CO-PILOT'S CONTROL COLUMN BEARING ON OUTER SURFACE OF FIREWALL WAS FOUND TO BE UNSERVICEABLE. THE NEEDLE BEARINGS HAD DEPARTED THE CAGE. THE BEARING WAS REPLSDR CA050616002Oil Cooler · cracked(CAN) DURING INSPECTION OIL WAS NOTICED TO BE LEAKING, THE SOURCE OF WHICH WAS DETERMINED TO BE THE OIL COOLER AS THERE WAS A CRACK ON THE WELD ALONG THE UPPER OUTER CORNER OF THE OIL COOLER. THE OIL COOLER WAS REPLACED WITH AN OVERHAULED UNIT.SDR CA050413004Alternator · unserviceable(CAN) UPON CLIMB-OUT AFTER DEPARTURE NOTICED WHITE SMOKE COMING FROM THE LT SIDE OF THE AIRCRAFT AND THE SMELL OF BURNING IN THE COCKPIT. NOTIFIED THE TOWER OF THE EVIDENCE OF SMOKE AND RETURNED TO LAND UNEVENTFULLY. UPON INVESTIGATION IT WAS REVEALED THE ALSDR CA040823BBFitting · cracked(CAN) DURING THE 100 HOUR INSPECTION THE RH MAIN GEAR OUTBOARD FITTING WAS FOUND CRACKED AT THE UPPER AFT RADIUS OF THE FITTING OPENING.THE FITTING WAS REPLACED IN ACCORDANCE WITH CESSNA'S RECOMMENDATIONS (OBTAINED FROM CESSNA) WITH A USED SERVICEABLE CUSTOMERSDR CA031015014Doubler · cracked(CAN) HORIZONTAL ATTACHMENT POINT DOUBLER FORWARD RT CRACKED AT TOP NUTPLATE RIVET. DOUBLER REPLACED WITH NEW. AREA INSPECTED. NO OTHER FAULTS FOUND. CAUSE IMPROPER GROUND HANDLING (SPECULATION).SDR CA030731002Cable · broken(CAN) DURING TAXI OF AIRCRAFT ADVANCING THROTTLE WOULD NOT INCREASE ENGINE RPM. - INVESTIGATION SHOWED THROTTLE CABLE BROKEN IN ENGINE COMPARTMENT BETWEEN WIRE CABLE AT BASE OF SOLID PUSH ROD ON CONTROL ASSEMBLY (THROTTLE).SDR CA030528001Pump · failed(CAN) FAILURE OF VACUUM AIR PUMP ON DESCENT DURING UFR OPERATIONS. VANE FAILURE, DRIVE SHEARED.SDR 2003FA0000015Bolt · looseINSPECTION IAW AD AND FOUND LOOSE BOLT HOLES FOR VERTICAL STABILIZER ATTACH. INSTALLED OVERSIZE BOLTS AND DYE CHECK, NO CRACKS FOUND, RETORQUED BOLTS DYE PENETRANT INSPECTION ITEMS.SDR AUS20021008Fitting · cracked(AUS) FORWARD FIN ATTACHMENT FITTING CRACKED IN AREA ADJACENT TO THE LH BOLT HOLE. FOUND DURING INSPECTION IAW AD/C206/7A4.SDR CA020530010Hinge Bracket · cracked(CAN) AILERON BRACKETS WERE LOOSE ON SPAR AND IN SKIN ATTACH. UPON EXAMINATION FOUND BOTH BRACKETS CRACKED AT REAR AND BOTTOM FLANGES. IT APPEARS THAT THE BRACKETS HAD BEEN LOOSE PREVIOUSLY AND REPAIRED BY SUBSTITUING CHERRY MAX THROUGH BOTTOM SKIN WHICH DID NSDR AU000847Angle · corroded(AUS) LEFT AND RIGHT WING FORWARD ATTACHMENT FITTING ANGLES CONTAINED INTERGRANNULAR CORROSION. (X)SDR AU000815Angle · corroded(AUS) LEFT WING UPPER SPAR CAP ANGLE CONTAINED EXFOLIATION CORROSION. (X)SDR AU000814Angle · corroded(AUS) RIGHT WING LOWER SPAR CAP ANGLE CONTAINED INTERGRANNULAR CORROSION. (X)SDR AU000813Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED ON LEFT AND RIGHT SIDES. (X)SDR 20000828SH029Nut · damagedDURING LANDING TOUCHDOWN, THE AIRCRAFT''S NOSE WHEEL DEPARTED AIRCRAFT. LOCAL PEOPLE, AT THE SITE, FOUND THE NOSE WHEEL AND ATTACHMENT BOLT ALONG WITH OTHER ATTACHMENT HARDWARE. (THE AN6-58A NOSE WHEEL BOLT REVEALS NO SIGNS TO THREAD DAMAGE. ADDITIONALLY, SDR CA990715032Rib · cracked(CAN) THE CENTER RIB AT WS 190.0 OF RT WING FOUND CRACKED AT TRAILING END THAT IS RIVETED TO WING REAR SPAR. ALSO, FOUND SEVERAL LOOSE AND SMOKING RIVETS IN THIS AREA.SDR AU990086Static System · contaminated(AUS) STATIC SYSTEM CONTAMINATED WITH WATER. AIRCRAFT HAD BEEN PARKED IN THE OPEN DURING A RAIN STORM.SDR 97ZZZX4728Cylinder · crackedNR 5 CYLINDER ASSY CRACKED ONE-THIRD AROUND STEEL BARREL APPROXIMATELY 1 INCH BELOW CYLINDER HEAD.SDR 96ZZZX952Bulkhead · crackedANNUAL INSPECTION REVEALED BOTH LEFT AND RIGHT SIDES OF LOWER FORWARD DOORPOST BULKHEAD (PN 1213407-2) CRACKED AS SHOWN IN CESSNA SEB 93-5R1. ALTHOUGH ACFT IS BELOW THE 4,000-HOUR TOTAL TIME SHOWN IN SERVICE BULLETIN, EXTENSIVE FLOAT OPERATION AND PRIOR DAMAGSDR 95ZZZX813Bolt · failedON LANDING ROLL-OUT, NORMALLY FIXED NOSE LANDING GEAR DRAG BRACE AFT ATTACH BOLT FAILED ALLOWING LANDING GEAR TO PARTIALLY RETRACT IN FORWARD DIRECTION. INSPECTION OF BOLT INDICATED THAT A PREVIOUS FRACTURE IN THE THREADED AREA EXISTED. PREVIOUS NLG MAINTENA
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