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 = '76' 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 = '76' 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 96ZZZX4401Magneto · separatedMAGNETO SEPARATED FROM ENGINE ON TAKEOFF CAUSING ENGINE TO STOP. THIS IS A DUAL MAGNETO ON A SINGLE DRIVE. IT WAS DETERMINED THE NUTS HAD LOOSENED AND ALLOWED MAG TO COME OFF. THERE IS NO TORQUE LISTED FOR THIS MAGNETO EXCEPT STANDARD TORQUE. RECOMMEND THASDR AU961170Skin · cracked(AUS) REAR FUSELAGE SKIN CRACKED IN FIVE PLACES AROUND TWO RIVETS AT STN 210 BULKHEAD AND NEAR STRINGER PNO HSJ 5893 - CRACK LENGTHSAPPROXIMATELY 10MM (0.393IN) - SUSPECT CAUSED BY OIL CANNING OF THE SKIN - STRINGER IS NOT ATTACHED TO THE BULKHEAD AT THIS POISDR AU961169Skin · cracked(AUS) REAR FUSELAGE SKIN CRACKED IN SIX PLACES IN AREA AROUND TWO RIVETS AT STN 210 BULKHEAD AND NEAR STRINGER PNO 105-440000-11 - CRACK LENGTHS 6MM (0.236IN) - SUSPECT CAUSED BY OIL CANNING OF THE SKIN - STRINGER IS NOT CONNECTED TO THE BULKHEAD AT THIS POINSDR AU960847Pipe · cracked(AUS) LANDING GEAR HYDRAULIC 'UP' PIPE FLARE CRACKED AND LEAKING AT CONNECTION TO POWER PACK - INVESTIGATION FOUND POOR QUALITY FLARE- PIPE HAD BEEN REFLARED ON 20 OCTOBER 1992 - PERSONNEL/MAINTENANCE ERRORSDR AU960566A Frame · cracked(AUS) LH MAIN LANDING GEAR ASSEMBLY 'A' FRAME CRACKED IN WELDED AREA AND THE CORROSION TREATMENT HOLE - FOUND DURING INSPECTION IAW AD/B76/18 AND SB 2361SDR AU960444Connector · cracked(AUS) MAIN LANDING GEAR CONNECTOR PNO 105-810020.3 CRACKED ON THE INBOARD LUG ADJACENT TO THE CLEVIS PIN LOCATING HOLE - CAUSED BY CORROSION OF LOCATING ROLL PIN IN CONNECTORSDR AU960445Mount · incorrect fit(AUS) DURING REPLACEMENT OF THE ENGINE LORD MOUNTS THE FOLLOWING DEFECTS WERE FOUND:1. NO1 ENGINE MOUNTS WERE CORRECTLY ASSEMBLED BUT TRANSPOSED, PNO J9613-49 WAS INSTALLED IN THE PNO J9613-50 POSITION AND VICE VERSA 2. NO2 ENGINE LOWER MOUNTS DID NOT HAVE TSDR 96ZZZX1272Actuator Tube · disconnectedPILOT REPORTED FLAPS WOULD NOT EXTEND IN-FLIGHT. EXAMINED FLAP SYSTEM AND FOUND TUBE ACTUATOR DISCONNECTED FROM ACTUATOR ASSEMBLY. RECONNECTED TUBE AND FUNCTIONAL CHECK OF FLAPS SATISFACTORY. SUBMITTER SUGGESTS A METHOD BE DEVELOPED BY BEECH TO SAFETY TUBE SDR AU960225A Frame · broken(AUS) LH MAIN LANDING GEAR 'A' FRAME ASSEMBLY BROKEN AT CORROSION TREATMENT HOLE AS INDICATED IN BEECH SB 2361 (AD/BEECH76/18)SDR AU960098Fitting · cracked(AUS) LH FUSELAGE FRAME SHEAR FITTING CRACKED IN RADIUS OF CUTOUT - CRACK LENGTH 5MM (0.196IN)SDR AU960072Pin · fractured(AUS) ENGINE NO1 PISTON PIN FRACTURED IN CENTRE CAUSING PISTON PIN BOSSTO BREAK EVENLY ON BOTH SIDES OF PISTON - DURING THE 100 HOURLYINSPECTION THE OIL PRESSURE FILTER WAS FOUND TO CONTAIN LARGE AMOUNTS OF STEEL AND ALLOY AND THE ENGINE WAS STRIPPED - DAMAGESDR AU960023Terminal · broken(AUS) LANDING GEAR SELECTOR RELAY TO POWER PACK CONNECTION BROKEN AT TERMINALSDR 95ZZZX6825Regulator · mislabeledTHE WIRING TERMINALS HAVE INCORRECT DECAL LABELING. THE DECAL IS INSTALLED 180 DEGREES OFF. THIS CAUSES THE BUS, FIELD, GROUND, AND PARALLEL WIRE TERMINALS TO BE INCORRECTLY LABELED.SDR 95ZZZX6824Regulator · mislabeledTHE WIRING TERMINALS HAVE INCORRECT DECAL LABELING. THE DECAL IS INSTALLED 180 DEGREES OFF. THIS CAUSES THE BUS, FIELD, GROUND, AND PARALLEL WIRE TERMINALS TO BE INCORRECTLY LABELED.SDR 96ZZZX375O-Ring · failedUPON DISASSEMBLY OF THE LEFT LANDING GEAR RETRACT/EXTENSION CYLINDER, THE MAIN END CAP O-RING (AN 6227 B-10) WAS FOUND TO HAVE FAILED. THIS O-RING CONTAINS THE FLUID AND KEEPS IT FROM ESCAPING TO AN EXTERNAL LEAK ON THE LANDING GEAR DOWN SIDE. UPON CLOSE EXASDR 95ZZZX6533Disk · crackedFOUND TINY HAIR LINE FRACTURES ON INBOARD SIDE OF DISC ROTOR. COULD NOT IDENTIFY THE CAUSE OF THE CRACKS.SDR 95ZZZX6683Fitting · crackedUPON SERVICING THE RIGHT MAIN GEAR STRUT, A VISIBLE CRACK WAS SPOTTED IN THE WEB OF THE SUPPORT FOR THE SHOCK STRUT. UPON REMOVAL, THE CONNECTOR WAS FOUND TO BE SLIGHTLY WARPED.SDR 95ZZZX5981Actuator · rod brokeLEFT MLG ACTUATOR ROD BROKE AT THE THREADED END DURING GEAR RETRACTION. THE GEAR FREE-FELL AND LOCKED IN THE DOWN POSITION. THE GEAR WAS MOVED UP AND DOWN BY HAND AND NO BINDING OR LOOSENESS WAS FOUND. NEW ACTUATOR WAS INSTALLED AND THE LANDING GEAR WAS OPESDR 95ZZZX6169Keel · crackedDURING ANNUAL INSPECTION, KEEL WAS FOUND CRACKED AT RUDDER BAR ATTACH POINTS. KEEL WAS REPLACED AND ACFT RETURNED TO SERVICE. SUGGEST CLOSE INSPECTION OF THIS AREA AT INSPECTIONS. POSSIBLE REINFORCEMENT IS SUGGESTED.SDR 95ZZZX4354Power Pack · defectiveLANDING GEAR FAILED TO EXTEND THE FIRST TRY. RECYCLED LANDING GEAR AND IT EXTENDED OK. PUT AIRCRAFT IN SHOP, JACKED AIRCRAFT, AND DETERMINED PROBLEM TO BE POWER PACK. INSTALLED ON OVERHAULED POWER PACK AND HAD NORMAL OPERATION.SDR 95ZZZX6408Magneto · defectiveREMOVED MAGNETO DURING INSPECTION OF ROUGH ENGINE. FOUND BOTH CONTACT POINTS WORN, BOTH COILS CRACKED AT CENTER POST, LEFT DISTRIBUTOR ARCED, IMPROPER LUBRICATION OF BEARINGS CAUSING GREASE TO BE SLUNG OUT, CAM LOBES HAVE VERY ROUGH FINISH.SDR 95ZZZX3324Valve · crimp nut looseWHILE COMPLYING WITH LYCOMING SB NR 518C, FOUND VALVE RETAINING NUT LOOSE (BOTH ENGINES). RECOMMEND NUT BE WELDED AT FACTORY. NO ATTEMPTS SHOULD BE MADE TO RE-CRIMP NUTS AS THEY WILL FRACTURE AND FRACTURE MAY GO UNNOTICED. SUBMITTER SUGGESTS AD NOTE BE ISSUSDR 95ZZZX3323Valve · crimp nut looseWHILE COMPLYING WITH LYCOMING SB NR 518C, FOUND VALVE RETAINING NUT LOOSE (BOTH ENGINES). RECOMMEND NUT BE WELDED AT FACTORY. NO ATTEMPTS SHOULD BE MADE TO RE-CRIMP NUTS AS THEY WILL FRACTURE AND FRACTURE MAY GO UNNOTICED. SUBMITTER SUGGESTS AD NOTE BE ISSUSDR 95ZZZX3037Channel · crackedINSPECTION FOUND CHANNEL THAT NLG ACTUATOR ATTACHES TO, CRACKED.SDR 95ZZZX3036Channel · crackedINSPECTION FOUND CHANNEL THAT NLG ACTUATOR ATTACHES TO, CRACKED. ACFT TT 3,800 HRS.SDR 95ZZZX1452Elt · corrodedELT ACTIVATED ON GROUND. RESET BUTTON CURED ACTIVATION. CONDUCTED INSPECTION PER 91.52, FOUND CORROSION ON BATTERY CONNECTOR AND PC BOARD. CLEANED CORROSION. INSTALLED NEW BATTERY. G-SWITCH COULD NOT BE ACTIVATED BY FORCE. LAST INSPECTION, 12-94. SUGGESSDR 95ZZZX1451Battery · corrodedELT ACTIVATED ON RAMP. REMOVED UNIT, FOUND HEAVY CORROSION ON BATTERY PACK AND MOUNTING SPACES, ELT WAS MFG 2-93. BATTERY REPLACEMENT WAS DUE 3-95. UNIT WAS INSTALLED NEW 8-93. LAST ELT INSPECTION PER FAR 91.52 WAS COMPLETED 9-94.SDR 95ZZZX827Valve · loose crimp nutWHILE COMPLYING WITH LYCOMING SB 518, FOUND CRIMP NUT LOOSE DUE TO POOR DESIGN.SDR 95ZZZX806Valve · crimp nut looseWHILE COMPLYING WITH LYCOMING SB 518, FOUND CRIMP NUT LOOSE AS SHOWN IN STEP 2 OF BULLETIN. CRIMP NUT LOOSE DUE TO POOR DESIGN.SDR 95ZZZX744Switch · defectivePILOTS REPORTED LT DOWN AND LOCK LIGHT BLINKING INTERMITTENTLY. TROUBLEHSOT SYSTM FINDING DEFECTIVE GEAR DOWN SWITCH. REPLACED SWITCH IAW MM, SWUNG LANDING GEAR ON JACKS, OPS CHECKED OKAY.
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