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 = 'F33A' 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 = 'F33A' 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 97ZZZX2082Bungee Spring · brokenPILOT REPORTED A LOUD POPPING SOUND AND A BIND IN THE RUDDER PEDALS. A MECHANIC PERFORMED ROUTINE INSPECTION AND FOUND UPPER FORWARD RUDDER AILERON BUNGEE SPRING HAD BROKEN IN HALF ON THE CLIP END SIDE. SUBMITTER SUGGESTED DURING ROUTINE 100-HOUR ANNUAL PROGSDR 97ZZZX1585Filter · meltedIN-LINE AIR FILTER FOR AUXILIARY AIR SYSTEM MOUNTED SIX INCHES FROM LEFT EXHAUST STACK. THIS ITEM WAS MOUNTED FOR 50 HOURS IN WHICH TIME PART OF THE HOUSING MELTED, AND THE REST BROKE APART FROM HEAT DAMAGE. HOUSING IS MADE OF PLASTIC. MANUFACTURER NEEDS TOSDR 97ZZZX1705Cover · crackedAT 100-HOUR INSPECTION, CRACK ABOUT 5 INCES LONG WAS FOUND IN NOSE GEAR WHEELWELL COVER JUST BEHIND NOSE GEAR STRUT. CAUSE OF CRACK IS UNKNOWN. SPLICED IN NEW SECTION OF A NEW COVER IAW 43.13. SUBITTER SUGGESTS KEEPING CLOSE INSPECTION OF THIS AREA FOR CRACSDR 97ZZZX1704Cover · crackedAT 100-HOUR INSPECTION, CRACK ABOUT 3 INCHES LONG WAS FOUND IN NOSE GEAR WHEELWELL COVER JUST BEHIND NOSE GEAR STRUT. CAUSE OF CRACK IS UNKNOWN. PATCHED CRACK WITH SECTION OF A NEW COVER IAW 43.13.SDR 98ZZZX1128Alternator · failedPILOT EXPERIENCED ELECTRICAL SYSTEM FAILURE. MADE EMERGENCY LANDING WITHOUT INCIDENT. FOUND ALTERNATOR FAILED.SDR 97ZZZX1715Air Filter · meltedDURING A ROUTINE INSP OF THE AIRCRAFT, FOUND THE IN-LINE AIR FILTER TO THE SECONDARY PRESSURE SYSTEM HAD BEEN HEATED BY THE EXHAUST SYSTEM ON THE LEFT EXHAUST. THE CLEAR PLASTIC MELTED THEN SHATTERED IN PIECES. SUBMITTER STATED THIS COULD CAUSE SMALL PIECES SDR 97ZZZX874Spar · crackedINSPECTION FOUND CRCKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. SUBMITTER STATED THIS IS THE 17TH AIRCRAFT REPORTED.SDR 97ZZZX546Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. THIS IS THE 16TH AIRCRAFT REPORTED.SDR 97ZZZX545Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. THIS IS THE 15TH AIRCRAFT REPORTED.SDR 97ZZZX544Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER. THIS IS THE 14TH AIRCRAFT REPORTED.SDR 97ZZZX6221Blade · corrodedPROPELLER INSPECTION FOUND BLADE CORROSION.SDR 97ZZZX6220Blade · corrodedPROPELLER INSPECTION FOUND BLADE CORROSION.SDR 97ZZZX6219Blade · corrodedPROPELLER INSPECTION FOUND BLADE CORROSION.SDR 96ZZZX5337Crankcase · crackedON 10-2-96 MAINTENANCE WAS NOTIFIED OF AN OIL LEAK ON THE ENGINE. UPON FURTHER INVESTIGATION, A CRACK WAS NOTED ABOVE THE TOP FORWARD CYLINDER HOLD DOWN STUD OF THE NR 5 CYLINDER. SUSPECT CAUSE OVERTORQUEING OR TORQUEING SEQUENCE. SUBMIMTTER STATED CLOSE INSDR EY2R9601077Blades · corrodedBLADES, SN'S K91889YS,K92027YS,K91828YS, FOUND CORRODED.SDR AU961132Spar · cracked(AUS) RUDDER SPAR CRACKED - FOUND DURING INSPECTION IAW AD/BEECH33/36 AMDT1SDR 96ZZZX5217Rod End · failedWHILE MAKING NORMAL LANDING, PILOT LOWERED GEAR AND HEARD A LOUD 'POP' FROM RT MAIN GEAR. WHEN GEAR WAS RETRACTED, GEAR INTRANSIT LIGHT WOULD NOT GO OFF. GEAR SELECTOR PLACED BACK IN DOWN POSITION AND AIRCRAFT WAS FLOWN TO HOME AIRFIELD WITH GEAR DOWN. AFTESDR 96ZZZX3778Carry-Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX3773Carry-Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX3761Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX3760Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 9504-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX3759Carry Through · crackedINSPECTION FOUND CRACKS IN CARRY-THROUGH STRUCTURE. AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR EY2R9600882Act Pin Assy · corrodedACT PIN ASSY FOUND CORRODED.SDR 96ZZZX3537Bulkhead · crackedSPINNER BULKHEAD IS CRACKED IN 6 PLACES, EACH AROUND THE PROPELLER ATTACH BOLT HOLES.SDR 96ZZZX3197Actuator · index wrongGEAR DOORS WILL NOT CLOSE PROPERLY. FOUND IMPROPER INDEXING ON ACTUATOR FROM BEECHCRAFT FOLLOWING OVERHAUL.SDR 96ZZZX3196Actuator · bindingFOUND ACTUATOR HAS INTERNAL BIND - 4 TO 6 TURNS BEFORE UP AND 4 TO 6 TURNS BEFORE BOTTOMING ON THE DOWN SIDE. COMPONENT OVERHAULED BY BEECHCRAFT.SDR AU960497Nut · cracked(AUS) WING ATTACHMENT BOLT NUT CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/BEECH33/41 - AIRCRAFT IS FOREIGN REGISTERED N93RSSDR 97ZZZX547Carry Thru Spar · crackedINSP FOUND CRACKS IN CARRY THRU STRUCTURE. AD 95-0-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX2743Arm Assy · mismanufacturedWHEN INSTALLING UPPER HINGE PER STC, FOUND WHEN NEW HINGE INSTALLED, RUDDER UPPER MOUNT WOULD NOT LINE UP STRAIGHT. VISUAL INSPECTION OF ARM REVEALED BEARING BOSS IN ARM DRILLED OFF CENTER CAUSING THIS PROBLEM ALONG WITH RUDDER CHAFING ON VERTICAL STABILIZER SDR 96ZZZX1125Spar · crackedCRACK IN SPAR CARRY-THROUGH STRUCTURE AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX1124Spar · crackedCRACK IN SPAR CARRY-THROUGH STRUCTURE AD 95-04-03 NOT VALID BY SERIAL NUMBER.SDR 96ZZZX940Spar · cracksFOUND CRACKS IN WING SPAR CARRY-THROUGH STRUCTURE, AD 95-04-03. NOT APPLICABLE BY SERIAL NUMBER OF AIRCRAFT.SDR 96ZZZX932Spar · crackedFOUND CRACKS IN WING SPAR CARRY-THROUGH STRUCTURE. AD 95-04-03, NOT APPLICABLE BY SERIAL NUMBER OF AIRCRAFT.SDR 96ZZZX251Bracket · elongated holeWHEN THE GEAR WAS SWUNG ON JACKS DURING ANNUAL INSPECTION, THE LT MAIN WOULD NOT EXTEND. WHEN THE GEAR WOULD NOT EXTEND, THE LT LANDING GEAR ACTUATING ROD BUCKLED IN COMPRESSION IN THE TUBULAR SECTION, BENDING AT 2 PLACES ABOUT EQUIDISTANT FROM THE CENTER. TSDR 96ZZZX62Pump · shaft shearedENGINE DRIVEN FUEL PUMP FAILED ON CLIMB AT 400 FEET AGL.SDR 96ZZZX822Vapor Separator · fod jammed pumpCUSTOMER REPORTED ENG DRIVEN FUEL PUMP FAILED AT 600 FEET AGL AFTER T/O. PILOT ACTIVATED ELEC PUMP AND SAFELY LANDED AIRPLANE. PUMP SENT TO THIS FACILITY FOR DISASSEMBLY AND INSP. WHEN PUMP DISASSEMBLED, 2 SMALL FLAKES OF ALUM FOUND JAMMED IN VANES OF PUMP.SDR 96ZZZX471Actuator · misinstalledDURING 100-HOUR ANNUAL INSPECTION, DAMAGE TO NOSE GEAR FORK ASSY AND LEFT NOSE GEAR DOOR ACTUATOR ROD DISCOVERED. FURTHER EXAMINATION REVEALED IMPROPER WASHER PLACEMENT WHERE THE UPPER BALL JOINT OF THE DOOR ACTUATOR ROD IS FASTENED TO THE NOSE GEAR DOOR ACTUSDR 95ZZZX6933Bolt · crackedWING ATTACH BOLTS REMOVED FOR 5-YEAR MAGNAFLUX INSPECTION. ONE BOLT, THE UPPER AFT SHOWED INDICATIONS OF A CRACK.SDR 95ZZZX6063Flap Rib · crackedDURING INSPECTION OF FLAP SYSTEM, NOSE RIB IN RIGHT FLAP WHERE FLAP ACTUATOR CONNECTS WAS FOUND CRACKED AND FLAP SKIN WAS DEFORMED. SUBMITTER SUGGESTS IT APPEARS TO BE CAUSED BY FLAP BEING OUT OF RIG AND BOTTOMING OUT IN FLAP TRACK.SDR 95ZZZX6062Flex Cable · failedEND OF FLAP DRIVE CABLE BROKE OFF AT WOODRUFF KEY AREA WHERE CABLE ENTERS GEARBOX. SINCE IT WAS LEFT CABLE, THE RIGHT FLAP EXTENDED UNTIL IT BOTTOMED OUT IN FLAP TRACK. DAMAGE APPEARS TO HAVE STARTED FROM PREVIOUS OVER EXTENSION DUE TO SWITCH FAILURES. SUBMSDR 95ZZZX5999Control Cable · frayedDURING ROUTINE INSPECTION, LEFT UPLOCK CABLE WAS FOUND HEAVILY FRAYED. JACKED A/C AND RETRACTED GEAR TO CHECK CABLE TENSION. RIGHT UPLOCK CABLE TENSION WAS 75 POUNDS. CORRECT CABLE TENSION IS 52 AND ONE-HALF, PLUS 10 OR MINUS ZERO, POUNDS. SUBMITTER RECOMMSDR 95ZZZX5619Switch · failedREMOTE SWITCH UNIT USED FOR GPS/NAV TRANSFER INTERNAL RELAY BANKS, FAILED. INTERNAL K2, K3, AND K4 RELAY BANKS FAILED IN THE CLOSED POSITION AND K5 BANK FAILED IN NEUTRAL POSITION. THIS FAILURE CAUSES THE NAV 1 HSI INDICATOR TO DISPLAY ERRONEOUS INFORMATION.SDR 95ZZZX4527Fitting · faultyAFTER A NORMAL RUN-UP, ACFT LOST POWER ON TAKEOFF AT APPROX 300 FEET AGL. PILOT SWITCHED FUEL TANKS AND ADJUSTED MIXTURE CONTROL WITH NO RESULTS. A SAFE EMERGENCY LANDING WAS MADE ON THE DOWN-WIND RUNWAY. ENGINE WAS SHUT OFF AND ACFT TOWED TO MAINTENANCE HASDR 95ZZZX3950Bracket · crackedINSPECTED A/C COMPRESSOR. A/C COMPRESSOR BELT FOUND SHREDDED. WHILE INSPECTING AREA, FOUND A CRACK FROM THE TENSIONER BOLT ALL THE WAY TO THE END OF THE BRACKET. IF THIS BROKE OFF, IT WOULD ALLOW THE COMPLETE TENSIONER TO COME LOOSE FROM ENGINE.SDR 95ZZZX4184Relay · failedLANDING GEARBOX BOTTOMED OUT IN THE GEAR UP POSITION DUE TO FAILURE OF RELAY. EXTREME FORCE WAS REQUIRED WITH BOOT ON THE GEAR HANDLE TO BREAK LOOSE BEFORE GEAR COULD BE CRANKED DOWN. NOTE: A SOLO PILOT WOULD HAVE TO CLIMB INTO BACK SEAT TO HAVE ENOUGH FORCSDR 95ZZZX4207Switch · seizedLANDING GEAR POSITION SWITCH FROZEN IN THE 'UP' POSITION DURING FLIGHT, MANUAL GEAR EXTENSION REQUIRED TO LOWER GEAR.SDR 95ZZZX3679Root Seal · detachedON ROUTINE DAY IFR FLIGHT IN VFR CONDITIONS, A FEW MONTHS AFTER AIRCRAFT HAD BEEN REPAINTED, A LOUD DRUMMING NOISE AND VIBRATION WAS FELT AND HEARD. IT WAS SIMILAR TO WHAT MIGHT BE EXPECTED IF A SEATBELT WAS CAUGHT OUTSIDE THE DOOR IN THE SLIPSTREAM OR WHEN ASDR 95ZZZX3194Bolt · brokenPILOT REPORTED NO THROTTLE CONTROL WHILE AT CRUISE POWER. AFTER LANDING, FOUND THROTTLE CONTROL DISCONNECTED FROM FUEL CONTROL ARM. BOLT WAS FOUND IN ENGINE COMPARTMENT BROKEN OFF AT THE COTTER PIN HOLE.SDR 95ZZZX3212Turbonormalizing · faultyDECREASED AIRCRAFT PERFORMANCE NOTED FOLLOWING INSTALLATION OF TURBO-NORMALIZING STC NR SA 5223NM. INVESTIGATION FOUND TURBO FLITE SYSTEM WEIGHT DATA TO BE INCORRECT. USING CORRECTED DATA STILL DOES NOT APPEAR CORRECT PER ACTUAL WEIGHT DATA FROM AIRCRAFT.SDR 95ZZZX2709Bulkhead · crackedFOUND DURING PROGRESSIVE INSPECTION AT ATCA. THE UPPER LEFT CORNER OF THE AFT BULKHEAD CRACKED APPROXIMATELY 1 INCH ALONG BULKHEAD BEND. ALSO, TWO CORNER CRACKS IN THE UPPER DOUBLER AT AFT BULKHEAD.
Back to Beech F33A