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 = '172RG' 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 = '172RG' 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 2009FA0000925Actuator · brokenON RETURN TO AIRPORT THE PILOT COULD NOT GET THE LEFT MAIN GEAR TO FULLY EXTEND INTO THE DOWN AND LOCKED POSITION FOR LANING. AFTER SEVERAL ATTEMPS TO GET THE GEAR DOWN THE DECISION WAS MADE TO LAND THE ACFT WITH THE GEAR UP IN THE GRASS ALONG SIDE THE RUNWAYSDR 2009FA0000505Actuator · crackedDURING OCCURRENCE THE BODY OF THE MLG ACTUATOR HAS CRACKED AT THE UPPER PORTIONOF THE GEAR CAVITY OR THE BOLT HOLES. THE ACTUATOR BODY (-10) IS CONSTRUCTED FROM ALUMINUM WHILETHE PISTON/TRUNNION (-5) AND THE PISTON ROLLER (-11) ARE STEEL. CONSIDERING THE OPESDR 2009FA0000336Actuator · crackedTHE RADIUS ON THE GEAR ACTUATOR HOUSING THAT HOUSES THE SEGMENTED GEAR CRACKED ALONG THE FWD BOLT HOLE AND ALLOWED THE RACK TO JUMP A TOOTH WHEN RETRACTING THE GEAR. UPON BRINGING THE GEAR DOWN FOR LANDING THE RT GEAR DIDN'T COME INTO PLACE. A PASSENGER WAS SDR CA090326005Line · melted(CAN) PILOT REPORTED THAT AIRSPEED INDICATOR WAS READING 20 KNOTS LOW. WHEN PITOT HEAD WAS REMOVED IT WAS FOUND THAT THE PLASTIC PITOT LINE WAS MELTED HALF WAY THRU BY THE WIRES TO THE PITOT HEAT ELEMENT. AS THESE WIRES GET WARM WITH THE PITOT HEAT ON, IT IS ISDR 2009FA0000159Pivot · crackedLEFT MAIN LANDING PIVOT FOUND CRACKED WHEN INSPECTED IAW SEB90-1 REV 3.SDR 2009FA0000158Pivot Support · crackedRT MAIN LANDING PIVOT FOUND CRACKED WHEN INSPECTED IAW SEB90-1 REV 3 DURING 100 HOUR INSPECTION.SDR 2009FA0000157Pivot Assy · crackedLT MAIN LANDING PIVOT FOUND CRACKED WHEN INSPECTED IAW SEB90-1 REV 3 DURING 100 HOUR INSPECTION.SDR 2009FA0000207Actuator · crackedAFTER LANDING GEAR WAS RETRACTED IN, IT WAS NOTED THAT THE LT LANDING GEAR ASSY DID NOT FULLY RETRACT INTO THE WELL. THE PILOT WAS INFORMED AND IMMEDIATELY RETURNED TO THE AIRPORT. DURING THE RETRACT TEST, IT WAS FOUND THAT THE LEFT GEAR HUNG UP AT THE MIDWASDR 2009FA0000102Setscrew · out of positionON DISASSEMBLY OF ENGINE FOR OVERHAUL, A SETSCREW FROM THE PROPELLER IDLER GEAR SHAFT WAS DISCOVERED SLIGHTLY EMBEDDED INTO THE INSIDE OF THE REAR-LT SIDE OF THE CRANKCASE. SETSCREW WAS PROBABLY IMPROPERLY PEENED FOR RETENTION IAW OVERHAUL MANUAL SEC 7-74, ATSDR 2009FA0000063Pin · brokenONE OF THE NOSE GEAR DOWNLOCK PINS BROKE, AT THE GROOVE MACHINED INTO THE PIN FOR ROLLPIN RETENTION, ALLOWING THE UNSECURED PORTION OF THE PIN TO JAM THE NOSE GEAR DOWNLOCK HOOKS. THIS RESULTED IN A GEAR UNSAFE INDICATION AND SUBSEQUENT NOSE GEAR COLLAPSE ON LSDR 2009FA0000058Actuator · crackedDURING FLIGHT, THE R/H MAIN LANDING GEAR FAILED TO EXTEND; HOWEVER, THE L/H LANDING EXTENDED NORMALLY. AFTER SEVERAL ATTEMPTS TO CYCLE THE GEAR, A LANDING WAS MADE WITH THE GEAR IN THE UP POSITION. POST ACCIDENT INVESTIGATION DETERMINED THAT THE (P/N 1281001-SDR CA090115007Gear · wornDURING SCHEDULED 500 HOUR MAGNETO INSPECTION IT WAS NOTED THAT THERE WAS ALOT OF WHITE DUST INSIDE MAGNETO. THEN IT WAS NOTED THAT THE PLASTIC GEAR TEETH WERE PARTIALLY WORN AWAY DUE TO BEING IMPROPERLY MESHED WITH THE PLASTIC DISTRIBUTOR GEAR DUE TO THE GEARSDR 2008FA0000920Actuator · crackedON 7/08/2008, RT MLG NOT FULLY RETRACTED REPORTED BY ATC. THE PILOTS NOTICED THE RT MLG WAS NOT FULLY RETRACTED. THE LANDING GEAR WAS THEN EXTENDED, A DOWN AND LOCKED IND FOR GEAR WAS REPORTED. THE RT MLG ACTUATOR BODY (DATE STAMP OF AUG 21, 2001.) WAS FOUNSDR 2008FA0000731Pivot Assy · shearedTHE LEFT MAIN LANDING GEAR PIVOT ASSY SHEARED IN TWO NEAR THE ACTUATOR END. THE SPLICED SECTION WHERE THE DRIVE GEAR IS INSTALLED SEPARATED.SDR 2008FA0000762Chain · brokenDURING A NON RELATED MAINTENANCE ACTION, THE MECHANIC NOTICED THE RUDDER TRIM WHEEL WAS MOVING WITH NO RESISTANCE. THE MECHANIC INSPECTED FURTHER AND FOUND THE CHAIN HAD SEPARATED AT ONE OF THE LINKS. AFTER CLOSER EXAMINATION IT HAS BEEN FOUND THAT SEVERAL OFSDR CA080812002Clevis · broken(CAN) DAMPER SHAFT CLEVIS BROKE AT NOSE STRUT ATTACHMENT ALLOWING UNRESTRAINED MOTION OF SHIMMY DAMPER.SDR 2008FA0000528Strut · damagedPILOT REPORTED A CLUNKING NOISE COMING FROM THE NLG. UPON INSPECTION, IT WAS NOTED THAT .2500 INCH UP AND DOWN PLAY AT THE LOWER TRUNNION ASSY. THE AC`S NLG ASSY WAS REMOVED AND DURING FATHER INSPECTION THE BARREL WAS FOUND TO BE THE CULPRIT. THE BOLT THAT SDR 2008FA0000583Cylinder Head · separatedON JULY 8, 2008, MADE AN EMERGENCY LANDING IN DESSERT TERRAIN AFTER THE ENGINE BEGAN TO EXHIBIT SEVERE VIBRATIONS, LOSS OF POWER AND SMOKE. THE NR 2 CYLINDER WAS FOUND TO HAVE SEPARATED FROM THE CASE, SEVEN OF THE EIGHT HOLD STUDS WERE FOUND TO HAVE SHEARED.SDR LJER210408Housing · crackedLANDING GEAR FAILED TO RETRACT. LT MAIN ACTUATOR HOUSING CRACKED AT MOUNTING HOLE.SDR 2008FA0000249Seal · leakingAFTER REPEATED TOUCH AND GO PROCEDURES, THE AC FAILED TO RETRACT THE LANDING GEAR DUE TO A LACK OF HYDRAULIC FLUID. THIS RESULTED IN A GEAR UP LANDING. DURING THE ACCIDENT INVESTIGATION IT WAS DETERMINED THAT THE HYDRAULIC FLUID RESERVOIR WAS DEPLETED OF FLUISDR CA070821001Housing · cracked(CAN) 500 HOUR LIQUID PENETRANT INSPECTION IAW MFG SEB 01-2 REVEALED, CRACK AT INDICATED AREA (TC NR 20070821001)SDR 2007FA0000481Spar · damagedFOUND SMOKING RIVETS ON TOP OF FUSELAGE IN AREA OF THE REAR CENTER SECTION SPAR. REMOVED RIVETS (APPROX. EIGHT ON EACH END OF SPAR) AND FOUND RIVET HOLES SEVERELY ELONGATED. FACTORY ORIGINAL RIVETS WERE .1250 INCH DIA. AND SEVERAL HAD BEEN REPLACED IN THE FISDR A2Y2007F00000Actuator · crackedPILOT MADE A NORMAL TAKEOFF AND GEAR RETRACTION. THE TOWER THEN INFORMED THE PILOT THAT THE LT MAIN GEAR LEG WAS NOT FULLY RETRACTED. HE THEN TRIED TO CYCLE THE GEAR AGAIN WITH THE SAME RESULTS. AFTER CYCLING THE GEAR AGAIN THE GEAR THEN CAME DOWN AND INDICSDR CA070508001Starter · malfunctioned(CAN) PILOT DID RUN-UP, ALL ENGINE INDICATIONS WERE NORMAL SO HE COMMENCED HIS TAKE-OFF. JUST AFTER HE STARTED TO CLIMB HE NOTICED THAT THE ACFT DID NOT WANT TO CLIMB AS IT SHOULD. ALL ENGINE INSTRUMENTS WERE WHERE THEY WERE SUPPOSED TO BE. HE ABORTED HIS TAKESDR 2007FA0000639Housing · crackedON A DUAL TRAINING FLIGHT, STUDENT AND INSTRUCTOR HEARD A NOISE WHEN LANDING GEAR WAS RETRACTED. LT LANDING GEAR REMAINED IN A PARTIALLY RETRACTED/ EXTENDED POSITION, UNABLE TO ACTUATE UP OR DOWN. THE LT LANDING GEAR ACTUATOR BODY HAD FAILED (CRACKED) AT THESDR 2007FA0000505Attach Fitting · crackedL/W SEB 93-8 ON NOSE GEAR ACTUATOR ATTACH FITTING AND SOUND CRACK ON LT, LOWER, IB BOLT HOLE OF FITTING. ALSO, BOLT HOLES IN LOWER SKIN WERE IN EXCESS OF .030. REPLACED ATTACH FITTING, LOWER SKIN AND DOUBLER IAW SK 172-142 AND SK 172-159.SDR 2007FA0000362Powerpack · misrepairedINSTALLED A NEWLY OVERHAULED COMPLETE HYDRAULIC POWER PACK UNIT AS RECEIVED. AFTER INSTALLING THE UNIT IN THE AIRCRAFT AND PERFORMING A RETRACT TEST THE NEW OVERHAULED GEAR MOTOR WAS JERKY AND ACTING LIKE IT WAS SHORTING OUT. REMOVED MOTOR AND INSTALLED ANOTSDR CA070502005Bulkhead · cracked(CAN) PARTS WERE CRACKED AT ATTACH POINTS OF WHEEL WELL COVER SKIN 2412011-1 AND BULKHEADS STATION 108 AND 124 AND CRACK ON WHEEL WELL COVER AT RT FRONT CORNER WHERE IT ATTACHES TO BULKHEAD STATION 108. TIEDOWN RINGS ALSO ATTACH IN THIS AREA. (TC NR 20070502SDR 2007FA0000394Actuator · crackedPILOT REPORTED LOUD POP JUST BEFORE INTERING THE PATTERN AT M89. WHEN HE EXTENDED THE GEAR THE GREEN GEAR DOWN LIGHT WOULD NOT COME ON. FLY BY REVEALED THE LEFT GEAR WAS IN TRANSIENT. GEAR UP LANDING FOLLOWED. INSPECTION OF LT MAIN GEAR ACTUATOR REVEALED TSDR 2007FA0000238Brake Pads · fracturedDURING A 50 HR OIL CHANGE AND INSPECTION, FOUND BOTH LT AND RT BRAKE PADS FALLING APART, SEVERELY CRACKED WITH LARGE PIECES MISSING. BOTH SIDES WERE CHANGED AT THE PREVIOUS 100 HOUR INSPECTION. THIS HAS BEEN A FREQUENT PROBLEM WITH THESE BRAKE PADS ON ALL OFSDR 2006FA0000983Control Cable · failedUPON SHUTDOWN AFTER FLIGHT, PILOT PULLED ON CARBURETOR MIXTURE CABLE TO IDLE CUT-OFF. THE CABLE CAME OUT IN THE PILOTS HAND. SUSPECT CARBURETOR MIXTURE CABLE BROKE DURING FLIGHT. SUSPECT CABLE HAS A QUALITY ISSUE. NOTE: DID NOT EFFECT OPERATION OF AIRCRAFT DURSDR 2006FA0000792Bungee Cylinder · brokenTHE NOSE GEAR STEERING BUNGEE PN 2467003-6, BROKE WHILE TAXIING IN AFTER LANDING. THE AIRCRAFT STOPPED WITHOUT INCIDENT. THE BREAK OCCURRED IN THE THEADED AREA OF THE SHAFT THAT CONTAINS THE CHAIN SPROCKET. NOTE THAT THIS SHAFT HAS THREADS ON BOTH ENDS. TSDR 2006FA0000796Hydraulic Line · failedNOSE GEAR HYDRAULIC ACTUATOR HOSE BLEW OUT OF CRIMP IN FLIGHT CAUSING LOSS OF ALL HYDRAULIC FLUID AND GEAR WOULD NOT GO UP OR DOWN, EVEN WITH HAND PUMP. THE MFG HOSE WAS NOT THE AEROQUIP TYPE WITH STEEL BRADING OR THE SCREW ON ENDS. RECOMMEND THE AEROQUIP 30SDR 2006FA0000750Housing · crackedRT MAINT GEAR ACTUATOR HOUSING CRACKED THROUGH THE BOLT HOLES OF CASTING , CAUSING RACK TO DISENGAGE FROM PIVOT GEAR.SDR CA060510002Rib · crackedAT A 100 HOUR INSPECTION A CRACK WAS FOUND UNDER THE LEFT INBOARD RUDDER BAR BLOCK, AT THE MOST FORWARD BOLT HOLE. RUDDER BLOCK HAD ABNORMAL MOVEMENT. CRACK COULD ONLY BEEN SEEN AFTER BLOCK WAS REMOVED.SDR CA060330001Pin · cracked(CAN) NO GEAR DOWN INDICATION UNTILL RECYCLED SEVERAL TIMES. INSPECTION REVEALED CRACKED DOWNLOCK PIN (REF SEB 95-20)AND WORN ACTUATOR BEARING END PIN HOLE. (TC NR 20060330001)SDR 2005FA0001496Actuator · crackedCOMPLYING WITH SB, FOUND BFE BORE CRACKED IAW ILLUSTRATION OF ACCOMPLISHEMENT OF INSTRUCTION OF SEB. (K)SDR 2006FA0000578Actuator · crackedDURING FLIGHT, LT MLG FAILED TO EXTEND BUT TRAILED, DISCONNECTED FROM HYD SYS. PILOT WAS ABLE TO ROCK LT MLG INTO DOWN AND LOCKED POSITION, MADE SAFE LANDING. DETERMINED, ACTUATOR BODY HAD CRACKED THROUGH FWD ATTACH HOLE, HALF THROUGH AFT ATTACH HOLE, WHICH SDR 2005FA0001050Actuator · crackedMLG ACTUATOR CRACKED. (K)SDR 2005FA0001082Actuator · crackedPILOT REPORTED SIDE LOAD ON LANDING. ON SUBSEQUENT TAKEOFF RT MAIN LANDING GEAR WOULD NOT FULLY RETRACT. FOUND RT ACTUATOR CRACKED AT FORWARD BOLT HOLE. (K)SDR 2005FA0001083Actuator · crackedFOUND UPPER FORWARD BOLT SHEARED AND ACTUATOR CACKED AT 100 HOUR INSPECTION. (GL19200504416) (K)SDR 2005FA0000787Lock · failedPILOTS SEAT BACK LOCK MECHANISM SLIPPED AS PILOT LEANED BACK TO GET HIS BAG OUT OF THE REAR SEAT. UPON REMOVAL FRO AC MECHANICS WERE ABLE TO CAUSE SEAT BACK LOCK MECHANISM TO FAIL. THIS IS THE SECOND FAILURE TO OCCUR WITH THIS MECHANISM. PART LAST FAILURE SDR 2005FA0000771Lock · slippedWHEN COPILOT LEANED AGAINST THE SEAT BACK LOCK FAILED AND ALLOWED THE BACK TO FULLY BE IN THE AFT POSITION. (GL17200503735) (K)SDR 2005FA0000351Angle · corrodedTHIS ANGLE IS WHAT TIES TOGETHER THE WING STRUT, ATTACHES ON THE LT AND RT SIDES OF THE FUSELAGE. IF THIS CORROSION WHERE TO PROGRESS MUCH FURTHER, IT COULD CAUSE THE STRUTS TO FAIL. (K)SDR CA050222010Cylinder · cracked(CAN) AIRCRAFT WAS IN A CRUISE CONFIGURATION WHEN THE PILOT NOTICED A VIBRATION FROM THE ENGINE. REDUCED POWER AND CAME BACK TO LAND AT THE DEPARTING AIRPORT WITHOUT INCIDENT. AIRCRAFT WAS BROUGHT INTO THE HANGER AND THE COWLINGS WERE REMOVED. IT WAS DISCOVSDR 2005FA0000454Fitting · crackedDURING EMERGENCY LANDING GEAR OPERATIONAL CHECK, THE MECHANIC FOUND THE CRACK ON BOTH SIDE CORNER OF THE FITTING NOSE GEAR ACTUATOR ATTACHING PART. IT MAY BE SUSPECTED THAT MATERIAL FATIGUE OR AN UNREPORTED LANDING. (K)SDR 200501309Rack · tornFOUND TRAY HAD STRESS TEARS IN THE CORNERS OF THE THUMBSCREW CUTOUT AT THE BEND RADII FOLLOWING INSPECTION IAW SIL-012.SDR CA041220006Cylinder Head · separated(CAN) HEAD SEPARATION WHILE IN FLIGHT. DISCOVERED WHILE INVESTIGATING A ROUGH RUNNING ENGINE AS REPORTED BY PILOT.SDR 2005FA0001081Actuator · crackedPILOT REPORTED LT MAIN LANDING GEAR WOULD NOT FULLY RETRACT. FOUND LT ACTUATOR CRACKED AT FORWARD BOLT HOLE. (GL19200504417) (K)SDR CQN2004F00000Bulkhead · crackedCRACKS WERE LOCATED AT LT AND RT RELIEF CUTS OF STATION 124.00 UPPER FUSELAGE BULKHEAD. PROBABLE CAUSE FOR LT SIDE IS AUX POWER RECEPTACLE AND RT SIDE COULD BE FROM LANDING STRESSES.
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