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 = '172D' 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 = '172D' 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 2026FA0000049Bracket · dentedELEVATOR STOP BOLT BRACKET COMPROMISED DUE TO EXCESSIVE FORCE / WIND DAMAGE, CAUSING THE LOWER ELEVATOR STOP BOLT TO BREAK THE NUT PLATE AND INDENT THE BRACKET REQUIRING REPLACEMENT. THIS FAILURE CAUSES THE AIRCRAFT ELEVATOR TO TRAVEL BEYOND THE ALLOWABLE LIMISDR 2024FA0000458Spar · corrodedFOUND MAJOR INTERGRANULAR CORROSION ON BOTH REAR WING ATTACH POINTS . BLOCK BEARING P/N 0512122. WINGS WERE REMOVED FOR RESTORATION. FURTHER FLIGHT WOULD HAVE LED TO TOTAL WING FAILURE AND WING SEPARATING FROM FUSELAGE. SIMILAR DAMAGE FOUND ON ANOTHER AIRCRAFSDR 2024FA0000307Fuel Tank · brokenREMOVED THE RH FUEL TANK TO FACILITATE OTHER MAINTENANCE. FOUND FUEL TANK BAFFLE SPOT WELDS BROKEN. THE BAFFLE WAS ABLE TO MOVE AROUND FREELY INSIDE THE TANK. THIS COULD CAUSE FALSE FUEL QUANTITY INDICATIONS DUE TO INTERFERENCE WITH THE TRANSMITTER FLOAT. SDR 2022FA0000535Piston Rod · brokenTHE THREADED END OF THE RIGHT BRAKE MASTER CYLINDER PISTON ROD SNAPPED OFF WHILE BLEEDING THE BRAKES. THE SEATS WERE OUT OF THE AIRCRAFT FOR ANNUAL INSPECTION SO THE RUDDER PEDAL WAS ONLY BEING PUSHED BY HAND. THE BROKEN END OF THE ROD LOOKED LIKE IT HAD BEESDR 2020FA0000498Spar · crackedCRACK & BUCKLE AT THE HORIZONTAL STABILIZER FORWARD SPAR CENTER LIGHTENING HOLE AT 1/4" TO 1/2" LONG. PROBABLY RELATED TO DAMAGE ON THE RIGHT INBOARD HORIZONTAL STABILIZER LEADING EDGE, IT LOOKS LIKE THE DAMAGE DESCRIBED IN CESSNA SEB 94-8 FIGURE 1.SDR 2014FA0000268Cylinder Head · crackedNR 2 CYLINDER EXHAUST VALVE STUCK HARD AT FULL LIFT POSITION. REMOVED CYLINDER. FOUND CYLINDER HEAD CRACKED AND WAS BEYOND REPAIR. CYLINDER ASSY HAD 286 HRS OPERATION SINCE LAST REMOVAL AND SERVICE. CYLINDER ASSY HAD 999.6 HRS TT. CYLINDER ASSY WAS REPLASDR 2008FA0000202Mount · wrong partAN UNKNOWN AMOUNT OF AC FIREWALL ATTACH ASSEMBLIES (ENGINE MOUNTS) THAT WERE NOT FAA-PMA APPROVED. THE MIDO ATTEMPTED TO CONTACT THE OWNER OF MFG CONCERNING THIS MATTER, HOWEVER, ALL PHONE CALLS WERE NOT RETURNED, AND CERTIFIED LETTERS NOT ACCEPTED. AS OF THISSDR CA080121006Cap · cracked(CAN) DURING ANNUAL INSP OF THE NOSE GEAR ASSY AND OLEO, THE OLEO CAP WAS FOUND TO BE CRACKED. THE CRACK WAS LOCATED .1875 IN FROM THE RADIUS OF THE END FLANGE. THE CAP WAS FOUND TO BE BROKEN THROUGH AND WAS REMOVED IN 2 PIECES. REVIEW OF THE TECHNICAL RECORDSSDR 2007FA0000874Rod End · brokenLT SIDE STEERING ROD WITH 215.92 HRS SINCE NEW HAD THE REAR BALL END THAT ATTACHES TO THE RT RUDDER BAR ASSY BREAK. THE BALL ROD END BROKE AND LEFT THE T/R STEERING ROD AS THE ONLY STEERING FOR THE NOSE GEAR. THE RODS ARE NOT SOLID RODS, THEY ARE DESIGNED TOSDR CA070419005Bracket · cracked(CAN) DURING THE ANNUAL INSPECTION, BOTH RUDDER HINGE BRACKETS WERE FOUND TO BE CRACKED. RUDDER WAS REMOVED AND REINSTALLED AFTER REPAIRS. PN 0531018-1 AND 0531018-2 WERE REPLACED WITH NEW IAW THE MM. (TC NR 20070419005)SDR 2007FA0000186Bushing · looseBRONZE BUSHING, VERY LOOSE IN DISTRIBUTOR BLOCK AND DISTRIBUTOR ARM WAS CONTACTING PINS IN BLOCK. MAG WOULD NOT OPERATE CORRECTLY. (K)SDR CA070110003Torque Link · cracked(CAN) PRIOR TO INSTALLATION ON AIRCRAFT, NOSE GEAR SHOCK STRUT ASSEMBLY WAS THOROUGHLY INSPECTED. SEVERAL CRACKS WERE FOUND ON UPPER TORQUE LINK. NEW MFG PART WAS INSTALLED. (TC NR 20070110003)SDR 2006FA0000499Cylinder · crackedNR 1 CYLINDER WAS REMOVED DUE TO A CRACK .75 AROUND STEEL BARREL. IT APPEARS THAT AN OIL CONTROL RING BROKE AND EVENTUALLY DESTROYED THE PISTON AND JAMMED BETWEEN THE PISTON AND CYLINDER. TT ON THE ENGINE IS 4156.9 HRS. SMOH IS 1432.9 HRS, THE CYLINDER WAS SDR 2004FA0000293Retainer · wornFOUND PN 24077, UPPER VALVE SPRING RETAINER WORN OUT ALLOWING VALVE SPRING TO BYPASS IT. CAUSED LOSS OF STATIC RPM AND SOME ROUGHNESS OCCASIONALLY.SDR 2004FA0000292Retainer · failedFOUND UPPER VALVE RETAINER ABOUT 09 PERCENT WORN THROUGH BY OUTER SPRING (PN 625958) BUT HAD NOT FAILED YET. PN 24077 UPPER VALVE SPRING RETAINER.SDR CA020916005Wire Rope · broken(CAN) ON TAKEOFF RUN, AT APPROXIMATELY 2 FT OFF THE WATER, A/C SETTLED BACK DOWN DUE TO UNSTABLE AIR. A NOISE WAS HEARD AND THE A/C BECAME VERY UNSTABLE. ABORTED TAKEOFF. AS THE A/C SLOWED DOWN & THE LIFT DISSIPATED, THE LT WING SUDDENLY DIPPED DOWN AND CSDR 2002FA0000697Selector Valve · misinstalledSPRING WAS INSTALLED BACKWARD. FUEL WOULD NOT SHUT OFF LEFT TANK. TO PREVENT RECURRENCE VALVE SHOULD BE INSPECTED AFTER OVERHAUL.SDR AUS20011228Wheel · failed(AUS) PILOTS CONTROL WHEEL BROKE INTO SEVERAL PIECES. INVESTIGATION FOUND THE COPILOTS CONTROL WHEEL CRACKED BEYOND LIMITS.SDR CA010727034Rheostat · failed(CAN) WHILE PERFORMING THE ANNUAL INSPECTION OF THE ELCTRICAL SYSTEM THE RHEOSTAT BEGAN SMOKING.SDR 2001FA0000139Piston · crackedDURING REPAIRS TO CYCL NR 4 FOR LOW COMPRESSION FOUND 1INCH CRACK IN PISTON SKIRT STARTING AT BOTTOM OF PISTON.SDR SW15200112284Bulkhead · crackedFORWARD PROPELLER BULKHEAD HAS BEEN CRACKING WITH MINIMAL HOURS. BOLTS HAVE BEEN PROPERLY TORQUED AND SAFETY WIND.SDR CA000712031Hub · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. (X)SDR AU000849Exhaust Valve · seized(AUS) NR 4 CYLINDER EXHAUST VALVE STUCK IN VALVE GUIDE. (X)SDR CA971010008Carburetor · failed(CAN) DURING CRUISE THE ENGINE BEGAN TO SUFFER POWER LOSS WITHOUT WARNING. EMERGENCY LANDING WAS CARRIED OUT. POST FLIGHT INSPECTION FOUND FUEL POURING FROM THE CARBURETOR. THE CARBURETOR WAS REPLACED WITH AN OVERHAULED UNIT AND THE ENGINE WAS GROUND RUN SERVISDR 97ZZZX4817Wheel · brokePILOT CONTROL YOKE BROKE, LEFT SIDE BOTTOM, IN LANDING FULL STALL CONDITION. PLASTIC MAY HAVE AGED. AIRCRAFT IS A 1962 MODEL AND HAS BEEN PARKED OUTSIDE MOST OF THE TIME.SDR 97ZZZX3476Support · crackedDURING REMOVAL FOR OIL PUMP AD COMPLIANCE, FOUND TWO OF THE THREE SUPPORT FINGERS CONNECTING THE PROPELLER GOVERNOR CONTROL CABLE CRACKED AT THE THREE-FINGER JUNCTION WELD, AND THE CABLE WAS SUPPORTED BY ONE FINGER. FAILURE OF THAT FINGER WOULD CAUSE LOSS OF SDR AU970350Hub · cracked(AUS) PROPELLER HUB CRACKED IN AREA OF NO1 BLADE BOLT HOLES - REWORK OF HUB REVEALED ONE MAIN CRACK APPROXIMATELY 15.875MM (0.625IN) LONG TOGETHER WITH THREE SUB-SURFACE CRACKS APPROXIMATELY 6.35MM (0.25IN) LONGSDR 97ZZZX1365Bracket · loose rivetsINSPECTION FOUND BOTTOM ATTACHMENT BRACKET FOR RUDDER BOLTS TO HAVE LOOSE RIVETS. SUBMITTER STATED THIS WAS THIRD ONE THIS YEAR.SDR AU961212Switch · faulty(AUS) ELT `G' SWITCH FAULTYSDR AU960783Block · corroded(AUS) CENTRE WING SPAR BEARING BLOCK CONTAINS SEVERE INTERGRANNULAR EXFOLIATION CORROSIONSDR 95ZZZX5998Cap · failedNLG STRUT CAP THAT HOLDS STRUT HOUSING TO ENGINE MOUNT, FAILED. FOUND BOLT MISSING. SUSPECT HARD LANDING AFTER BOLT CAME LOOSE AS CONTRIBUTING FACTOR.SDR 95ZZZX6439Spar Assy · crackedFOUND 2 CRACKS AT LIGHTENING HOLE IN CENTER SECTION OF FRONT SPAR AND REINFORCEMENT SPAR OF HORIZONTAL STABILIZER. SUSPECT CAUSE - IMPROPER GROUND HANDLING. RECOMMENDATION - USE TOW BAR.SDR 95ZZZX6438Spar Assy · crackedFOUND 2 CRACKS AT LIGHTENING HOLE IN CENTER SECTION OF FRONT SPAR AND REINFORCEMENT SPAR OF HORIZONTAL STABILIZER. SUSPECT CAUSE - IMPROPER GROUND HANDLING. RECOMMENDATION - USE TOW BAR.SDR 95ZZZX6007Aileron · rivet faultyDURING ANNUAL INSPECTION, FOUND 6 RIVET HEADS MISSING ON LOWER SKIN OF RIGHT AILERON WHERE BALANCE WEIGHTS ARE ATTACHED AND SKIN WAS LOOSE. FOUND ONE RIVET NEXT TO THESE WITH BLISTERED PAINT, THAT WHEN SCRAPED WITH FINGERNAIL, THE HEAD POPPED OFF. AILERON SKSDR 95ZZZX6006Aileron · rivet faultyDURING ANNUAL INSPECTION, FOUND 6 RIVET HEADS MISSING ON LOWER SKIN OF RIGHT AILERON WHERE BALANCE WEIGHTS ARE ATTACHED AND SKIN WAS LOOSE. FOUND ONE RIVET NEXT TO THESE WITH BLISTERED PAINT, THAT WHEN SCRAPED WITH FINGERNAIL, THE HEAD POPPED OFF. AILERON SKSDR 95ZZZX5941Engine · failedAFTER 40 MINUTES OF CRUISE FLIGHT TO 3,000 FEET MSL, THE ENGINE LOST POWER. ABOUT 80 FEET ABOVE THE GROUND, ON SHORT FINAL TO A HAY FIELD, THE CONTROL WHEEL BROKE. THE PILOT GRABBED THE CONTROL WHEEL TUBE AND STARTED TO FLARE FOR LANDING WHEN THE AIRCAFT STRSDR 95ZZZX5940Control Wheel · brokeAFTER 40 MINUTES OF CRUISE FLIGHT TO 3,000 FEET MSL, THE ENGINE LOST POWER. ABOUT 80 FEET ABOVE THE GROUND, ON SHORT FINAL TO A HAY FIELD, THE CONTROL WHEEL BROKE. THE PILOT GRABBED THE CONTROL WHEEL TUBE AND STARTED TO FLARE FOR LANDING WHEN THE AIRCAFT STR
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