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 = 'TBM700' 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 = 'TBM700' 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 2002FA0000336Connector · looseOPERATOR REPORTED INTERMITTENT DME AND HEADPHONE JACK PROBLEMS. UPON TROUBLESHOOTING, TECHNICIAN DISCOVERED 21 LOOSE CONNECTORS ON THE SYMBOL GENERATOR DUE TO BAD CRIMPING TECHNIQUES. WIRING WAS REPAIRED AND OPERATIONAL CHECKED OK.SDR CA020220011Insert · loose(CAN) DURING 100 HOUR INSPECTION NOTICED THAT FLAP CARRIAGE INBOARD IS MOVING AT ATTACHMENT. REMOVED FLAP AND CARRIAGE AND FOUND POTTED INSERTS THAT SECURE THE CARRIAGE TO FLAP WERE LOOSE CAUSING DAMAGE TO COMPOSITE RIB, HONEYCOMB (INTERNALLY). ONE OF THE INSESDR 2001FA0000318Carriage · wornAFTER REMOVAL OF LEFT FLAP, DISCOVERED LEFT INBOARD CARRIAGE, PART LISTED ABOVE AND ACTUATOR NUT COVER, PN T700A2750029000, WORN FROM CONTACT WITH ACTUATOR NUT. WEAR APPEARS TO BE FROM WORN BUSHINGS IN CARRIAGE AND ACTUATOR NUT COVER AS WELL AS WEAR IN LOCATSDR CCA2001F00001Carriage · crackedUPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN T700A5755098001. NEW PART WEB THICKNESS IS 3X THICKER. POSSIBLE CAUSE; HIGH KIT FLAP OPERATING SPEED. REPLACEMENT PART APPEARS TO BE REINFORCED IN AFFSDR CCA2001F00000Carriage · crackedUPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN 7700AS755097000. NEW PART WEB THICKNESS IS APPROX 3X THICKER. POSSIBLE CAUSE; HIGH FLAP OPERATING SPEED. REPLACEMENT PART APPEAR TO BE REINFORCED IN AFSDR CA010629020Seal · misinstalled(CAN) INERTIA ACTUATOR MOTOR P/N 200N6071017220 WAS REPLD 29.9 HRS PRIOR TO FAILURE . NEW ACTUATOR WAS BEING INST WHEN NOTICES INERTIA APOATOR DEFLECTOR BEING CUT WHILE MANU MOVING. UNIT WAS REMOVED FROM HC & WHILE INVESTIGATING NOTICED SEAL THAT HAD UNEVEN MASDR 99ZZZX2363Switch · malfunctionedRED CAUTION LIGHT COMES ON FOR OXYGEN SYSTEM - INTERMITTENT. TROUBLESHOT SYSTEM TO COPILOT'S OXYGEN SYSTEM MICROSWITCH. WHEN COPILOT'S SEAT WAS RAISED , END OF A SCREW PUSHED SWITCH CAUSING SWITCH TO MAKE CONTACT. REMOVED COPILOT'S SEAT, CUT END OF SCREW OFSDR 98ZZZX2020Bracket · looseDURING ROUTINE 100-HOUR INSPECTION PER SOCATA MM, FOUND RT MLG DOOR FORWARD BRACKET PIVOT ATTACH BRACKET LOCATED ON WING RIB TO HAVE A LOOSE BEARING, AXIAL DIRECTION. PART WAS REMOVED AND VISUALLY INSPECTED. A CRACK WAS FOUND AT THE BOTTOM OF THE BRACKET UNDSDR 98ZZZX17Carrier · crackedWHILE CARRYING OUT A 100-HOUR REPETITIVE INSPECTION IAW DGAC AD 94-110, AND SB 70-048-57, IT WAS NOTED THAT ALL 4 FLAP BEARING CARRIAGES WERE CRACKED. THE CRACKS WERE NOT LOCATED IN THE INSPECTION AREAS SHOWN IN THE SB 70-048-57, BUT WERE LOCATED IN THE WEBS.SDR 98ZZZX16Carrier · crackedWHILE CARRYING OUT A 100-HOUR REPETITIVE INSPECTION IAW DGAC AD 94-110, AND SB 70-048-57, IT WAS NOTED THAT ALL 4 FLAP BEARING CARRIAGES WERE CRACKED. THE CRACKS WERE NOT LOCATED IN THE INSPECTION AREAS SHOWN IN THE SB 70-048-57, BUT WERE LOCTED IN THE WEBS. SDR 98ZZZX15Carrier · crackedWHILE CARRYING OUT A 100-HOUR REPETITIVE INSPECTION IAW DGAC AD 94-110, AND SB 70-048-57, IT WAS NOTED THAT ALL 4 FLAP BEARING CARRIAGES WERE CRACKED. THE CRACKS WERE NOT LOCATED IN THE INSPECTION AREAS SHOWN IN THE SB 70-048-57, BUT WERE LOCTED IN THE WEBS. SDR 98ZZZX14Carrier · crackedWHILE CARRYING OUT A 100-HOUR REPETITIVE INSPECTION IAW DGAC AD 94-110, AND SB 70-048-57, IT WAS NOTED THAT ALL 4 FLAP BEARING CARRIAGES WERE CRACKED. THE CRACKS WERE NOT LOCATED IN THE INSPECTION AREAS SHOWN IN THE SB 70-048-57, BUT WERE LOCATED IN THE WEBS.SDR 97ZZZX3500Connector · burnedWHILE REMOVING BATTERY FOR MAINTENANCE, FOUND NEGATIVE TERMINAL ON CONNECTOR ARCED AND BURNED. THE NEGATIVE POST IN BATTERY RECEPTACLE WAS ALSO DAMAGED AND POSSIBLY CAUSED BY WORN CONNECTOR (SOCKET ENLARGED) NOT PROVIDING GOOD CONTACT. CONNECTOR SHOULD BE CHSDR 97ZZZX3444Feedback Block · wornDURING ANNUAL INSPECTION, FOUND CARBON 'BETA' FEEDBACK BLOCK SEVERELY WORN. THIS HAD CAUSED DAMAGE TO FEEDBACK RING AS WELL. THIS OCCURRED DUE TO BLOCK NOT MOVING FREELY IN ARM. (LACK OF LUBRICATION). AIRCRAFT HAD NOT BEEN INSPECTED FOR 160 HOURS. NORMAL SDR EY2R9601684Rod · defectivePROP ASSY SN 1321 IS DEFECTIVESDR 96ZZZX2221Deice Tube · chafedDURING ANNUAL INSPECTION, RIGHT ELEVATOR HORN DEICE BOOT AIR TUBE FOUND CHAFED AT THE 90 DEGREE BEND WHERE IT ENTERS THE ELEVATOR TIP. THE CHAFED AREA HAD CREATED A SMALL HOLE IN THE TUBE. NEW TUBE INSTALLED AND ELEVATOR OPENING FOR TUBE SLIGHTLY ENLARGED TOSDR 96ZZZX1945Bracket · failedRIGHT MAIN GEAR DOOR LIGHT DID NOT EXTINGUISH AFTER TAKEOFF RETRACTION, GEAR WAS CYCLED DOWN, NO GEAR SAFE-LIGHT ON RT MAIN. FLY-BY INSPECTION VERIFIED GEAR (RT) NOT EXTENDING. GEAR-UP LANDING HAD TO BE MADE. AT RECOVERY OF AIRCRAFT FROM RUNWAY, RT FORWARD SDR 96ZZZX2107Transducer · failedFUEL PRESSURE WOULD DROP TO ZERO POUNDS IN-FLIGHT AT TIMES. NOTE: THIS IS THE THIRD TRANSDUCER TO GO BAD ON THIS AIRCRAFT. FIRST ONE LASTED 155 HRS. SECOND ONE LASTED 120 HRS, AND THE THIRD ONE LASTED 203 HRS.SDR 96ZZZX843Deice Pipe · chafe throughREMOVED ELEVATOR FOR C/W SOCATA SB 70-053. UPON REMOVAL, FOUND LT DEICE PIPE FOR ELEVATOR HORN WORN THROUGH AT ENTRANCE TO HORN. THIS INSTALLATION WAS DONE AT FACTORY. WEAR CAUSED BY LACK OF CLEARANCE AT PASS-THROUGH. SUBMITTER STATED TBM NEEDS TO ISSUE A SDR 96ZZZX42Deice Boot · manual errorDEICE BOOTS CYCLE OUTBOARD WING THEN INBOARD WING AND TAIL. THE MM AND POH SAY THE INBOARD WING AND TAIL SHOULD CYCLE FIRST, THEN OUTBOARD WING. AFTER TALKING TO TBM NORTH AMERICAN SERVICE REP, FOUND THE BOOKS WERE WRONG. REFERENCE: MM, CHAPTER 30, SUB-CHAPSDR 95ZZZX7059Cable · chafedDURING 100-HOUR INSPECTION, FOUND PROPELLER GOVERNOR CABLE CHAFES ON C-FLANGE OF POWER PLANT. SUBMITTER RECOMMENDS PUTTING BRACKET WITH CLAMP TO KEEP FROM CHAFING. RE: MANUAL, CHAPTER 76, SUB-CHAPTER 10, ITEM NR T700A7610049000.SDR 95ZZZX5976Carriage · crackedWHILE C/W SB 70-048-57, 2 CRACKS WERE FOUND. ONE IN THE LOWER WEB OF THE LT FLAP INBOARD CARRIAGE, ONE INCH FROM THE AFT ROLLER STUD, AND THE OTHER IN THE VERTICAL WEB, .3750 INCH FROM THE FORWARD ROLLER STUD. BOTH CRACKS WERE BEYOND ALLOWABLE STOP DRILL LIMSDR 95ZZZX5966Carriage · crackedWHILE COMPLYING WITH SB 70-048-57, A CRACK WAS FOUND IN THE LOWER WEB OF THE RIGHT FLAP INBOARD CARRIAGE, ONE INCH FROM THE AFT ROLLER STUD. CRACK WAS BEYOND ALLOWABLE STOP DRILL LIMITS IAW THIS SB. PART WAS CHANGED WITH NEW PART NUMBER WHICH HAS BEEN MODIFISDR 95ZZZX5862Actuator · pins corrodedAILERON TRIM INDICATOR WOULD NOT INDICATE. FURTHER TROUBLESHOOTING REVEALED CORROSION IN AILERON TRIM ACTUATOR POWER WIRE HARNESS CONNECTION. PINS IN CONNECTOR WERE CORRODED AND BRITTLE. REMOVED ACTUATOR, PN 14570001, AND INSTALLED NEW, IMPROVED ACTUATOR, PSDR 95ZZZX3820Transducer · failedPILOT REPORTED NO FUEL PRESSURE INDICATION, TURNED BOOST PUMP ON, SAME RESULT. REPLACED FUEL PRESSURE TRANSDUCER WITH NEW UNIT, FUEL PRESSURE INDICATING SYSTEM FUNCTIONED NORMALLY. A/C TT 275. OCCURRENCE 7-20-95.SDR 95ZZZX4548Actuator · leakingNOSE GEAR STRUT ACTUATOR LEAKING HYDRUALIC FLUID AT VENT SCREEN HOLES. THIS IS FROM FLUID BYPASSING O-RINGS IN ACTUATOR. NO FIELD LEVEL REPAIR AT THIS TIME. UNIT MUST BE OVERHAUL/EXHCHANGE FROM VENDOR. AUGUST 11, 1995, AIRCRAFT OWNER HAS BEEN WAITING FOR OSDR 95ZZZX3613Actuator · out of rig'LDG DOOR AMBER LITE ON IN-FLIGHT.' FOUND RT DOORS NOT COMPLETELY CLOSED WITH GEAR RETRACTED. FOUND GEAR ACTUATOR ROD END HAD TURNED OUT. (PISTON ROD TURNED OUT OF ROD END) AFFECTING DOOR RIGGING. RIGGED DOOR AND ROD END IAW 32-30-01. SECURED ROD END. OPSSDR 95ZZZX7058Cable · chafedDURING 100-HOUR INSPECTION, FOUND PROPELLER GOVERNOR CABLE CHAFING ON THE C-FLANGE OF THE POWER PLANT. SUBMITTER RECOMMENDS PUTTING BRACKET WITH CLAMP ON C-FLANGE TO LIFT PROP GOVERNOR CABLE AWAY FROM FLANGE TO PREVENT CHAFING. RE: MANUAL, CHAPTER 76, SUB-CSDR 95ZZZX1482Mount Adapter · failedPILOT REPORTED ENGINE VIBRATION WITH NR 1 GENERATOR FAILURE. INSPECTED ENGINE FOUND GENERATOR MOUNTING ADAPTER COMPLETELY FAILED. GENERATOR HANGING FROM WIRES AND RUBBING ON STANDBY GENERATOR DRIVE PULLEY AND BELT. SUBMITTER STATED EXACT CAUSE UNKNOWN AT THSDR 95ZZZX1384Carriage · crackedDURING FLAP CARRIAGE INSPECTION PER TBM SB 70-048, FOUND LT INBOARD CARRIAGE CRACKED AT LOWER WEB AREA (.5 INCH IN LENGTH). SUSPECT CAUSE IS INSUFFICIENT WEB STRENGTH AND/OR FLAP EXTENSION AT HIGH SPEEDS. REPLACEMENT WITH NEW STYLE CARRIAGE REQUIRED PER TBM SDR 95ZZZX3790Transducer · malfunctionedPILOT REPORTED NO FUEL PRESSURE INDICATION, TURNED BOOST PUMP ON, SAME RESULT. REPLACED FUEL PRESSURE TRANSDUCER WITH NEW UNIT. FUEL PRESSURE INDICATING SYSTEM FUNCTIONED NORMALLY. OCCURRENCE 1-17-95. A/C TT 155.
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