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 = '7KCAB' 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 = '7KCAB' 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 2018FA0000438Solenoid · openBATTERY SOLENOID OPENED DURING LANDING GEAR EXTENSION.SDR 2018FA0000525Tube · damagedON BOTH THE LH AND RH SIDES OF THE FUSELAGE, THE U-BOLT ATTACHMENT TUBE, PN 2-1949, IS CRACKED AT THE AFT ATTACHMENT BOLT FOR THE MLG. THE CRACKS WERE DISCOVERED DURING AN ANNUAL INSPECTION STARTED ON 08/01/2018. THE ISSUE WAS ALSO DISCOVERED IN ANOTHER ACFTSDR 2017FA0000513Muffler · detachedAFTER TAKE OFF, A LOUD NOISE WAS HEARD IN THE COCKPIT. THE PILOT LANDED SAFELY AND ON INSPECTION, FOUND THE MUFFLER HAD BROKEN AWAY FROM THE EXHAUST MANIFOLD.SDR 2013FA0000670Spar · crackedDURING COMPLIANCE OF AD 00-25-02 R1, HAIR-LINE CRACKS WERE FOUND AT WING STRUT ATTACH POINT ON BOTH LT AND RT FWD WING SPARS. APPROXIMATELY THREE INCHES OF LONGITUDINAL CRACK WAS FOUND OTBD AND INBD OF PLYWOOD DOUBLERS. NO COMPRESSION CRACKS NOTED. THE ACFTSDR CA111003010Coil · malfunctioned(CAN) WEAK SPARK WHEN HOT. REPLACED WITH NEW COIL.SDR 2005FA0001260B-Nut · looseENGINE OIL PRESSURE LINE B-NUT AT GEAR CASE LOST TORQUE AND THE ENGINE LOST ALL OIL. LACK OF LUBRICATION CAUSED FAILURE OF THE NR2 CONNECTING ROD BEARING. (K)SDR 2005FA0000945Control Cable · slippedAILERON CABLE SLIPPED OUT OF THE INBOARD NICOPRESS SLEEVE ON THE FORWARD AILERON CABLE IN THE LEFT WING. ALL 4 (LEFT AND RIGHT WING) CABLES WERE PURCHASED NEW FROM AMERICAN CHAMPION AIRCRAFT IN AUG, 2002 AND INSTALLED DURING THE REBUILD OF THE AIRCRAFT. ALL SDR 2005FA0000038Bolt · improper partDURING ANNUAL INSPECTION, IT WAS FOUND THAT ONE OF THE NAS BOLTS HOLDING THE IB END OF THE LANDING GEAR WAS TOO SHORT AND DID NOT GO ALL THE WAY THROUGH THE NAS NUT. THESE BOLTS WERE INSTALLED AT THE FACTORY, DURING A REPAIR IN 2001. FAILURE WOULD RESULT IN SDR 2003FA0000965Seat Frame · broken2 SEAT BACK SUPPORT STRAPS BROKE ON HARD LANDING (G-METER REUD 9G) UPPER STRAP WAS A NEW BREAK AT WELD CENTER STRAP BROKE AT REPAIR WELD FROM PREVIOUS BREAK. CFI IN REAR SEAT SUSTAINED MINOR BACK INJURY, AIRCRAFT LT MAIN GEAR COLLAPSED RESULTING IN PROP STRIKSDR 2002FA0001377Spar · crackedWHILE COMPLYING WITH AD 2000-25-02 R1 (WING SPAR INSPECTION) FOUND BOTH FORWARD SPARS CRACKED AT SPAR ROOT. EACH SPAR HAD TWO CRACKS RUNNING THE LENGTH OF THE WOOD GRAIN AND ADJACENT TO UPPER AND LOWER ATTACH BOLT HOLES. PAINT FROM THE AREA HAD TO BE REMOVED PSDR 2002FA0001128Cable · brokenTHE DOWN ELEVATOR CONTROL CABLE FAILED AT THE REAR PULLEY BELOW BATTERY BOX. THE PULLEY HAD STOPPED TURNING THUS CUTTING OR WEARING CONTROL CABLE TO A CONDITION IT WHERE IT FAILED WITH HARD FORWARD STICK. METER SHOWED .5 AND GS.SDR 2002FA0000235Spar · crackedWING MAIN SPAR, TOP OF SPAR OUTBOARD OF STRUT FITTING.SDR 2001FA0000131Spar · unsecureAIRCRAFT REGISTERED AS BELLANCA. MODEL IS 7KCAB. DESIGN NOW OWNED BY AMERICAN CHAMPION. WOOD SPAR WING INSPECTED IN ACCORDANCE WITH AD 2000-25-02. SEVERAL RIB/SPAR ATTACHMENT NAILS MISSING. PER SERVICE LETTER SL-417 THE SPAR "DAMAGE" CAUSED BY THE MISSINGSDR 2002FA0000245Spar · crackedAIRFRAME TOTAL TIME 3161 DURING THE ANNUAL INSPECTION AND WHILE COMPLYING WITH AD INSTRUCTIONS. IT WAS DISCOVERED THAT THE RIGHT WING REAR SPAR HAD AN 8 INCHES LONG LONGITUDINAL CRACK AT THE REAR STRUT ATTACH POINT. ITS SUSPECTED THAT THE AIRFRAME HIGH TIME SDR 2001FA0000123Spar · crackedDURING INSPECTION OF RIGHT WING, A CRACK WAS FOUND ON THE AFT SIDE OF THE FORWARD WOOD SPAR, 79 INCHES OUTBOARD FROM THE BUTT RIB. THE 5 INCH LONG, HORIZONTAL CRACK WAS LOCATED AT THE COMPRESSION MEMBER AND RAN THROUGH THE HOLES FOR THE DRAG WIRES. UNDETERMISDR 2002FA0000250Spar · crackedWOODEN SPARS, NAILS OUT OF LEADING EDGE RIBS, WOODEN SPACERS WERE LEFT OUT OF FIRST FOUR INBOARD LEADING EDGE RIBS. LEADING EDGE LOOSE, NAILS LOOSE. HAD BEEN PATCHED BEFORE, HAD PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS. SOME RIBS CRACKED,SDR 20010417AP002Spar · damagedWOOD SPARS; NAILS OUT OF LEADING EDGE RIBS; WOODEN SPACERS WERE LEFTOUT OF FIRST FOUR IN-BOARD LEADINGEDGE RIBS; LEADING EDGE LOOSE; NAILSLOOSE; SOMEBODY HAD PATCHED UP BEFORE AND PUT SCREWS INSTEAD OF NAILS ON LEADING EDGE SPARS AND RIBS; SOME RIBS CRACKED; SDR AU980721Throttle Cable · broken(AUS) THROTTLE CONTROL CABLE BROKEN AT THROTTLE LEVER. PART TOTAL CYCLES: 1,552.SDR 97ZZZX2716Spar · crackedINSPECTED SPAR IAW SL 406. FOUND RIGHT FORWARD SPAR CRACKED OUTBOARD, AFT SIDE OF STRUT ATTACH DOUBLER. CRACK VERY DIFFICULT TO SEE WITHOUT BENDING LEADING EDGE ALUMINUM UP TO GET A CLEAR VIEW OF TOP OF SPAR. THIS CRACK COULD NOT BE SEEN FROM BOTTOM OF WING SDR 96ZZZX1784Pump · seal leakSEAL FAILED CAUSING FUEL TO VENT THROUGH ELECTRIC (DC) MOTOR, PAST ARCING BRUSHES. ASSEMBLY INSTALLED ORIGINALLY WITHOUT CASE VENT AND DRAIN TUBE. SUBMITTER RECOMMENDS OWNERS OF OLD 7KCAB CITABRIAS BE ADVISED TO CHECK INSTALLATION FOR LEAKING AND PRESENCE OFSDR 96ZZZX2559Lifter · damagedANNUAL INSPECTION - LARGE AMOUNT OF METAL FRAGMENTS IN OIL PRESSURE AND OIL SUCTION SCREENS. CYLINDERS REMOVED, 7 LIFTER BODIES NOT TURNING, ENGINE TEAR-DOWN REVEALED VERY LITTLE TAPER ON CAM LOBE TIPS EXCEPT NR 4 EXHAUST LUBE. IT HAD .001 INCH TAPER AND WASSDR 96ZZZX2558Camshaft · damagedANNUAL INSPECTION - LARGE AMOUNT OF METAL FRAGMENTS IN OIL PRESSURE AND OIL SUCTION SCREENS. CYLINDERS REMOVED, 7 LIFTER BODIES NOT TURNING, ENGINE TEAR-DOWN REVEALED VERY LITTLE TAPER ON CAM LOBE TIPS EXCEPT NR 4 EXHAUST LUBE. IT HAD .001 INCH TAPER AND WASSDR 95ZZZX5231Magneto · failedENGINE INTERMITTENTLY RUNNING ROUGH. MAGNETOS BOTH HAD 1,786 HOURS SINCE INSTALLATION. SABOTAGE PAINT APPLIED BY MANUFACTURER WAS NOT DISTURBED INDICATING NO 500-HOUR INSPECTIONS HAD BEEN PERFORMED. INSPECTION SHOWED TRACES OF 'CROSS-FIRING' IN DISTRIBUTOR SDR 95ZZZX5230Magneto · failedENGINE INTERMITTENTLY RUNNING ROUGH. MAGNETOS BOTH HAD 1,786 HOURS SINCE INSTALLATION. SABOTAGE PAINT APPLIED BY MANUFACTURER WAS NOT DISTURBED INDICATING NO 500-HOUR INSPECTIONS HAD BEEN PERFORMED. INSPECTION SHOWED TRACES OF 'CROSS-FIRING' IN DISTRIBUTOR SDR 95ZZZX2969Diversion Plate · brokenAFTER REMOVAL OF OIL PAN AND ACCESSORY SECTION TO COMPLY WITH 'AD' OF OIL PUMP ASSY, FOUND INVERTED FLIGHT OIL DIVERATING PAN (PART UNK) CRACKED AND BROKEN FROM FLEX STRESS, SEVERAL PIECES BROKEN WERE FOUND LAYING IN OIL PAN. THIS SYSTEM INSTALLED AT CHAMP FA
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