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 = '95B55' 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 = '95B55' 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 97ZZZX3404Selector Valve · leakFUEL VALVE INSTALLED TO REPLACE DEFECTIVE NEW FUEL VALVE WITH ONLY 24 HOURS TIME. THIS VALVE BEGAN TO LEAK WITH 25 HOURS TIME IN SERVICE.SDR 97ZZZX3403Selector Valve · leakTHIS VALVE INSTALLED TO REPLACE 2 OTHER PREVIOUS VALVES INSTALLED AS NEW THAT FAILED A SHORT TIME AFTER INSTALLATION.SDR 97ZZZX3402Selector Valve · leakFUEL VALVE BEGAN LEAKING 24 HOURS AFTER INSTALLATION FROM NEW.SDR AU970627Seal · failed(AUS) PROPELLER BLADE NUT TO HUB SEAL LEAKINGSDR 97ZZZX2591Air Box · mismanufacturedNEW AIR BOX ASSEMBLIES LISTED WERE RECEIVED DEFECTIVE. 'NEW PARTS FROM BEECH'. THE AIR FILTER SLOT IS NOT WIDE ENOUGH TO ACCOMODATE THE SUPPLIED AIR FILTER. SECOND, THE ALTERNATE AIR DOOR DOES NOT CLOSE COMPLETELY. SUBMITTER STATED POOR QC ON BOTH ASSEMBLISDR 97ZZZX2590Induct Air Box · mismanufacturedNEW AIR BOX ASSEMBLIES LISTED WERE RECEIVED DEFECTIVE. 'NEW PARTS FROM BEECH'. THE AIR FILTER SLOT IS NOT WIDE ENOUGH TO ACCOMODATE THE SUPPLIED AIR FILTER. SECOND, THE ALTERNATE AIR DOOR DOES NOT CLOSE COMPLETELY. SUBMITTER STATED POOR QC ON BOTH ASSEMBLISDR AU970527Brake Disc · worn(AUS) RH MAIN LANDING GEAR BRAKE WORN - BRAKE LOCKED UP CAUSING TYRE TO BLOW OUTSDR AU970417Cylinder · glazed(AUS) ENGINE CYLINDERS GLAZED - VALVE GUIDES WORN - NO2 CYLINDER ALSO CONTAINED A BROKEN OIL CONTROL RING - AIRCRAFT HAD NOT BEEN OPERATATED FOR SEVERAL YEARS AND IT IS SUSPECTED THAT THE ENGINES HAD NOT BEEN INHIBITED IN ANY WAYSDR CA970226057Low Pitch Stop · stripped threads(CAN) DURING A DAILY INSPECTION THE L/H PROPELLER SPINNER WAS FOUND LOOSE. FURTHER INSPECTION REVEALED THE LOCK WIRE SECURING THE PROP SPINNER TO THE LOW PITCH STOP ASSEMBLY WAS BROKEN AND THE THREADS ON THE LOW PITCH STOP WERE STRIPPED. THE LOW PITCH STOP WASSDR AU970093Seal · pinched(AUS) PROPELLER BLADE NUT SEALS PINCHED GIVING INEFFECTIVE SEALING -SEALING WAS ACHIEVED BY THE USE OF SILASTIC SEALANT BETWEEN THE BLADE NUT THREADS AND HUB AND LOCK RING ASSEMBLY - INCORRECT ASSEMBLY - PERSONNEL/MAINTENANCE ERROR - PROPELLER HAD BEEN MODIFIESDR AU970071Propeller · loose(AUS) LH ENGINE PROPELLER LOOSE ON CRANKSHAFT - ALL SIX RETAINING NUTS WERE LOOSE - FOLLOWING REMOVAL OF PROPELLER ONE OF TWO DOWELS WAS FOUND TO BE BROKEN - SUSPECT BOLTS WERE NOT TORQUED WHEN PROPELLER WAS REFITTED TWENTY THREE HOURS PREVIOUSLY (DEC 1996) - SDR AU970070Gear · melted(AUS) LH ENGINE RH MAGNETO DISTRIBUTOR GEAR MELTED - HT CONTACT SEPARATED FROM GEAR - BEARING FAILED - LARGE PIECE OF SLOW SPEED DISTRIBUTOR GEAR MISSINGSDR CA970109016Engine · making metal(CAN) DURING CLIMBOUT THE #2 ENGINE OIL PRESSURE BEGAN TO DROP AND THE RPM BEGAN TO DECAY. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND THE ENGINE WAS PRODUCING EXCESSIVE AMOUNTS OF NON-FERROUS METAL OBSTRUCTING THE PROSDR EY2R9600189Blade Nuts · crackedPROP ASSY BLADE NUTS CRACKEDSDR EY2R9600188Hub · crackedHUB ASSY CRACKED IN BOTH BLADE SOCKETSSDR 96ZZZX5912Mount · damagedINSP FOUND ENGINE MOUNT WITH HEAVY CHAFE DAMAGE AT LOWER RT FIREWALL ATTACH POINT.SDR 96ZZZX5897Mount · chafe damageINSPECTION FOUND ENG MOUNT WITH HEAVY CHAFE DAMAGE AT LOWER RT FIREWALL ATTACH.SDR CA961112026Shoulder Screw · backed out(CAN) ON APPROACH THE #1 PROPELLER RPM DROPPED WHEN THE POWER WAS REDUCED. THE AIRCRAFT LANDED WITHOUT INCIDENT, BUT THE PROPELLER FEATHERED ON SHUTDOWN. THE PROP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. DISASSEMBLY OF THE FAULTY PROPELLER FOUND THE SDR CA961002012Propeller · faulty(CAN) ON APPROACH THE R/H RPM DROPPED TO 1500 WHEN THE POWER WAS REDUCED, THE AIRCRAFT LANDED WITHOUT INCIDENT BUT THE PROPELLER FEATHERED ON SHUTDOWN. THE PROPELLER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA961002011Switch · broken wire(CAN) AFTER A MISSED APPROACH THE GEAR FAILED TO RETRACT. INSPECTION REVEALED THAT A WIRE HAD BROKEN IN THE LANDING GEAR SAFETY SWITCH BUNDLE AT THE LOCATION WHERE THE BUNDLE FLEXES DURING GEAR CYCLING.SDR 96ZZZX4155Battery · corrodedREPLACED BATTERY (ELT) BP-1025 PURCHASED FROM TRIM-CRAFT, JUNE, 1994. ELT TESTED OK; THEN, JUNE, 1995 WAS OK AT THAT ANNUAL TIME. AT THIS YEAR'S ANNUAL, TESTED ELT. SIGNAL OK, BUT FOUND CASE AND AREA OF ELT MOUNTING LOCATION FULL OF CORROSION. CALLED COMMUSDR 96ZZZX4425Impulse Coupler · crackedWHILE C/W AD 78-09-07R3, AN IMPULSE COUPLER WAS FOUND TO NEED REPLACEMENT. A NEW PART WAS INSTALLED ON MAG. WHILE TIGHTENING NUT ON COUPLER TO 240 INCH/POUNDS, THE COUPLER CRACKED WHERE IT SLIDES ON THE TAPERED SHAFT. SUBMITTER FOUND THAT IMPULSE COUPLERS TSDR AU960967Collar · worn(AUS) ENGINE LOW OIL PRESSURE - SUSPECT CRANKSHAFT TRANSFER COLLAR OR MAIN BEARINGS WORNSDR 96ZZZX3373Condenser · defectiveMAGNETOS OVERHAULED WITH NEW ELECTROSYSTEM CONDENSER, PN E510-349276, CODE NR 03108 AND NR 9544. MAGNETOS CHECKED ON TEST STAND, OPERATED NORMALLY. MAGS INSTALLED AND TIMED TO ENGINE. DURING GROUND RUN, 3 MAGS CHECKED NORMAL. FOURTH MAG DEVELOPED A 1,000 RSDR EY2R9601568Hub · damagedPROP HUB DOWEL PINS ENLARGEDSDR 96ZZZX3533Hub · crackedPROPELLER WAS SENT FOR INSPECTION BECAUSE RED OIL COMES OUT FROM THE HUB. THE REASON, THERE WAS A CRACK ON THE LOWER SIDE OF THE HUB IN THE AREA OF THE THREAD.SDR EY2R9600634Split Bearing · corrodedSPLIT BEARING HAS CORROSION.SDR EY2R9600633Split Bearing · corrodedSPLIT BEARING HAS CORROSION.SDR CA960517101Arm · broken(CAN) ON GEAR EXTENSION, A SNAP SOUND WAS HEARD AND NO INDICATION OF GEAR DOWN. CONTROL TOWER REPORTED NOSE GEAR AT 45 DEGREES. NOSE GEAR COLLAPSED ON LANDING. ACTUATOR ARM BROKEN AT MID-LENGTH.SDR 96ZZZX2157Blade · under sizeBOTH BLADES OF THE PROPELLER ASSEMBLY WERE FOUND TO BE UNDER MINIMUM SHANK DIAMETER. SUBMITTER STATED BLADE SHANKS WERE PROBABLY REWORKED UNDER DIMENSION AT LAST PROPELLER SERVICE.SDR 96ZZZX2156Blade · under sizeBOTH BLADES OF THE PROPELLER ASSEMBLY WERE FOUND TO BE UNDER MINIMUM SHANK DIAMETER. SUBMITTER STATED BLADE SHANKS WERE PROBABLY REWORKED UNDER DIMENSION AT LAST PROPELLER SERVICE.SDR 96ZZZX2155Hub · damagedHUB WAS FOUND TO HAVE DAMAGE TO PRELOAD RETENTION AREA. SUBMITTER STATED DAMAGE POSSIBLY OCCURRED FROM STRIKE DAMAGE TO ONE OR MORE BLADES.SDR 96ZZZX2154Blade · under sizeINSPECTION FOUND BOTH BLADES OF THE PROPELLER ASSEMBLY TO BE UNDER MINIMUM SHANK DIAMETER. SUBMITTER STATED BLADE SHANKS WERE PROBABLY REWORKED UNDER DIMENSION AT LAST PROPELLER SERVICE.SDR 96ZZZX2153Blade · under sizeINSPECTION FOUND BOTH BLADES OF THE PROPELLER ASSEMBLY TO BE UNDER MINIMUM SHANK DIAMETER. SUBMITTER STATED BLADE SHANKS WERE PROBABLY REWORKED UNDER DIMENSION AT LAST PROPELLER SERVICE.SDR EY2R9600047Hub · crackedHUB CRACKED IN NR 2 SOCKETSDR EY2R9600046Hub · crackedHUB CRACKED IN NR 2 SOCKETSDR 96ZZZX2292Coil · crackedDURING ANNUAL INSPECTION, FOUND MAGNETO COIL CRACKED IN NUMEROUS PLACES. AD 94-01-03 R2 REQUIRES REPLACEMENT OF THESE COILS, BUT THIS SERIAL NUMBER MAGENTO IS NOT COVERED BY THE AD (COIL IS AN OPAQUE AMBER COLOR AS REFERENCED IN TELEDYNE CONTINENTAL IGNITION SDR CA960409026Crankcase · cracked(CAN)AN OIL LEAK ON THE RIGHT HAND ENGINE WAS REPORTED. A SUBSEQUENT INSPECTION REVEALED A CRACK IN THE CRANKCASE APPROXIMATELY 3 1/2" LONG, FORWARD OF THE #5 CYLINDER. THE CAUSE OF THE CRACK IS NOT KNOWN.ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZX2030Downlock · low tensionLEFT MAIN TIRE WAS SKIDDED ON RUNWAY TO THE POINT OF TIRE FAILURE. LEFT MAIN GEAR THEN COLLAPSED. INVESTIGATION REVEALED LANDING GEAR DOWNLOCK TENSION WAS 15-20 POUNDS. BEECHCRAFT SM REQUIRES DOWNLOCK TENSION TO BE 45-65 POUNDS. IT IS SUPPOSED THE ADDITIONSDR AU960815Bearing · corroded(AUS) RUDDER BEARINGS (2OFF) CORRODED INTERNALLY - AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENT - SUSPECT BEARINGS ORIGINAL FITMENTSDR AU960814Hinge · worn(AUS) LH AND RH WING LOWER FORWARD SPAR TO LEADING EDGE `D' SECTION HINGE AND HINGE PINS WORN - MAXIMUM AMOUNT OF WEAR IS LOCATED BETWEEN WING ROOT TO JUST OUTBOARD OF ENGINESDR AU960813Bulkhead · cracked(AUS) LH AND RH SPINNER BULKHEADS CRACKED - SUSPECT CAUSED BY ROUGH RUNNING ENGINESSDR 96ZZZX1085Control Cable · end partedRT MIXTURE CONTROL ASSY SWAGED END PARTED FROM ROD ON ENGINE END OF CABLE.SDR CA960229007Circuit Breaker · failed(CAN)DURING CRUISE THE PILOT NOTICED THAT BOTH ALTERNATOR OUTPUTS WERE ZERO AND THE BATTERY VOLTAGE WAS DOWN TO 19 VOLTS. THE LEFT HAND, 50 AMP BRKER WAS POPPED. BOTH ALTERNATORS WERE SHUTOFF, THE LEFT HAND BUS CIRCUIT BREAKER WAS RESET AND THE ALTERNATORS TURSDR CA960222014Support Assy Lh · cracked(CAN)THE SUPPORT ASSEMBLY WAS FOUND CRACKED THROUGH 80 PERCENT OF THE STRUCTURE. THE SUPPORT ASSEMBLY WAS FOUND TO BE DISTORTED TO THE POINT WHERE THE RUDDER CONTROL WOULD BE INTERFERED WITH AND GROUND NOS E WHEEL STEERING WOULD BE DIFFICULT. THE SUBMITTER SUSSDR EY2R9600019Bulkhead · crackedBULKHEAD CRACKED IN HUB BOLT HOLESSDR CA960212014Fuel System · ice crystals(CAN) ON THE TAKEOFF ROLL, THE R/H ENGINE FAILED TO DEVELOP FULL POWER. THE TAKEOFF WAS ABORTED AND A GROUND RUN PERFORMED. A SECOND TAKEOFF WAS ATTEMPTED, THIS TIME DEVELOPING FULL POWER, BUT ONCE AGAIN WHEN AIRBORNE BEGAN TO LOSE POWER. THE AIRCRAFT LANDED WSDR 96ZZZX867Belt · brokenPILOT REPORTED LEFT ALTERNATOR OUT. INSPECTION REVEALED THAT NEW CONTINENTAL ALTERNATOR BELT HAD FAILED.SDR AU960050Cable · broken(AUS) THROTTLE INNER CABLE BROKE APPROXIMATELY 25MM (1IN) FROM SLIDING SLEEVE INSIDE FLEXIBLE PART OF CABLE ON THE ENGINE SIDE - CABLE HAD A VERY MINOR KINK NEAR THE ATTACHMENT BRACKET - SUSPECT INCORRECT INSTALLATION - PERSONNEL/MAINTENANCE ERRORSDR AU960043Aileron · out of balance(AUS) FOLLOWING REPAINTING WHEN THE CONTROLS WERE CHECKED FOR BALANCE IT WAS FOUND THAT THE RH AILERON WAS 0.5 INLBS NOSE HEAVY AND THELH AILERON WAS 8 INLBS TRAILING EDGE HEAVY - CHECKS ON AN AILERON FROM ANOTHER AIRCRAFT FOUND THAT IT WAS ALSO OUT OF BALANC
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