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 = '182H' 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 = '182H' 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 3PSR201503200003Link · brokenDURING INSPECTION, IT WAS NOTED THAT THE NR 3 BLADE ROTATED WITHIN THE HUB. DISCOVERED THAT THE BLADE ACTUATING LINK, WAS BROKEN WHICH ALLOWED THE BLADE TO ROTATE. IT WAS UNDETERMINED IF THE LINK WAS BROKEN DUE TO MISHANDLING OF THE PROPELLER OR HAPPENED DURSDR KC2R2014091049320Impulse Coupling · crackedDURING A 500 HOUR INSPECTION OF MAGNETOS, IMPULSE COUPLING WAS FOUND TO HAVE CRACKS IN THE HUB BASE PLATE, LOCATED AT THE FULL ADVANCE STOP NOTCH. CRACKS RADIATE FROM THE SHARP-CORNERED FEATURE OF THE NOTCH OF THE PLATE. DEFECT DETECTED USING MAGNETIC PARTICSDR 2014FA0000334Bulkhead · crackedCRACK DISCOVERED IN AFT BULKHEAD DURING INSPECTION. 0.25 INCH CRACK LOCATED IN UPPER LEFT CORNER BETWEEN RUDDER CABLE CUTOUT AND BULKHEAD FLANGE.SDR 2008FA0000074Cylinder · damagedWHILE PERFORMING A COMPRESSION CHECK TO FIND AN OIL LEAK, FOUND NR 1 CYLINDER WITH O COMPRESSION. PULLED CYLINDER OFF AND FOUND THE PLATING ON THE CYLINDER LOOSE AND FLAKING OFF. (K)SDR 2007FA0000637Piston · fracturedAFTER INSTALLING NEW CYLINDER ASSY SA47006S-A20P WITH NEW PISTON ASSY PN SA640518, WE WERE PERFORMING BREAK IN RUN AT LOW POWER, FIRST AT 800 RPM FOR 2 MIN. SHUTDOWN ENGINE, CLEANED FOULED PLUGS DUE TO OIL IN CYLINDER FROM ASSY. RAN ENGINE AT 1000 RPM FOR 3 SDR 2006FA0000425Spring · brokenSTARTER DRIVE WAS OVERHAULED BY A CERTIFIED REPAIR STATION. (PN S539800M30) STARTER ADAPTER SPRINGS WERE INSTALLED IAW STC DURING THE OVERHAUL. THE STARTER WAS INSTALLED ON THIS ENGINE AND WAS OPERATED FOR 4.06 HOURS (5 STARTS) BEFORE IT FAILED. AN INSPECTISDR AU510002094Cylinder · faultyPISTON RINGS PREMATURELY WORN AND DETERIORATED CAUSING HIGH OIL CONSUMPTION AND POWER LOSS. CYLINDER VALVE GUIDES WORN AND EXHAUST VALVE REPLACED.SDR QTL2005F00000Distributor Gear · failedMAGNETO REMOVED FOR FAILURE, 24 TEETH MISSING ON DISTRIBUTOR GEAR. REPLACED WITH NEW GEAR NR 10-357586. (K)SDR 2004FA0000143Pin · brokenDURING ANNUAL INSPECTION. THIS LOWER RT DOOR HINGE PIN WAS FOUND BROKEN IN 3 PLACES. IT IS VERY SIMPLE TO DETECT, THIS JUST TO OPEN AND CLOSE DOOR SLOWLY AND WATCH FOR EQUAL ROTATION OF PIN. IF ONLY ONE END TURNS THEN THE PIN MUST BE BROKEN.SDR 01222004Hinge Pin · brokenDURING ANNUAL INSPECTION LOWER RT DOOR HINGE PIN WAS FOUND BROKEN IN 3 PLACES. THIS ITEM IS SIMPLE TO DETECT BY JUST OPENING AND CLOSING THE DOOR SLOWLY AND WATCH FOR EQUAL ROTATION OF PIN. IF ONLY ONE END TURNS THEN THE PIN MUST BE BROKEN. PART INFO: HINGE SDR AUS20030694Bolt · faulty(AUS) CONNECTING ROD BOLT FAULTY. LONGITUDINAL DISCONTINUITY FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/ENG/4 AMDT8.SDR 2003FA0000522Fuel Cell · leakingFLOATS AND FUEL CELLS. RECEIVED NEW MFG LEFT WING FUEL CELL, MFG DATE 3/03. INSTALLED IN AIRCRAFT, FILLED WITH 1000LL AVGAS, DISCOVERED FUEL LEAK, RETURNED FUEL CELL TO MFG, FFC DISCOVERED MFG LT REAR BOTTOM CHANNEL LEAK DEFECT. FFC REPAIRED DEFECT AND RETSDR EVC2002F00000Connecting Rod · brokenNR 1 CONNECTING ROD BOTS BROKEN.SDR AUS20010863Pipe · corroded(AUS) ENGINE OIL PRESSURE PIPE FROM FIREWALL TO GAUGE CORRODED IN AREAOF CONTACT WITH SOUNDPROOFING MATERIAL. PIPE IS MANUFACTURED FROM ALUMINIUM.SDR 20010507CW001Separator · contaminatedOIL FILTER INSPECTION REVEALED EXCESSIVE AMOUNT OF CONTAMINATION. INVESTIGATION REVEALED AIR/OIL SEPERATOR INTERNAL SCREEN COMING APART. YEARS OF VIBRATION MAY HAVE CAUSED SCREEN SEPARATION. FACTORY RECOMMENDS 100 HOURS CLEANING. THERE IS NO WAY TO INSPECTSDR CA010302006Bulkhead · cracked(CAN) CRACK ABOVE LT RUDDER STOP BOLT LOCATION ON (BULKHEAD) FLANGE BEND RADIUS DIRECTLY ABOVE BOLT. A/C HANGARED FOR LAST 15 YRS & NOT SUBJECTED TO WIND. REMOVAL & INSP SHOWS POOR STANDARD PRACTISE OF DRIVING 90 DEGS STIFFENER INTO BEND RADIUS OF FLANGE (ASSYSDR 99ZZZX2941Gasket · deterioratedREMOVED FILTER ASSY, P/N BA 8110, TO CHECK GASKET, 8 INCHES OF GASKET WAS MISSING. SCREEN MESH COMING LOOSE FROM FILTER FRAME.SDR AU990403Impulse Coupling · damaged(AUS) MAGNETO IMPULSE COUPLING DAMAGED.SDR AU990331Pump · failed(AUS) VACUUM PUMP DETERIORATED INTERNALLY. PUMP VANES WORN AND ROTOR BREAKING UP.SDR AU990388Harness · failed(AUS) ENGINE IGNITION HARNESS LEAD FAILED.SDR AU980153Control Cable · misrouted(AUS) ELEVATOR CONTROL CABLE INCORRECTLY ROUTED.SDR AU980152Windshield · deteriorated(AUS) WINDSCREEN BADLY CRAZED AND OPAQUE.SDR AU980151Angle · corroded(AUS) FUSELAGE ANGLE BADLY CORRODED IN AREA OF WING STRUT ATTACHMENT.SDR AU980150Fuel Cell · cracked(AUS) LH FUEL TANK BLADDER CRACKED AND LEAKING.SDR AU980149Spar · corroded(AUS) LH WING FORWARD SPAR RIVETS (20OFF) CORRODED AND RIVET HEADS POPPED OFF. LH WING SPAR SEVERELY CORRODED. RH WING FORWARD SPAR RIVETS HAD RIVET HEADS POPPEDSDR AU980148Doubler · corroded(AUS) INSPECTION PANEL DOUBLERS LOCATED IN FLAP BAYS CORRODED.SDR AU980147Rivet · damaged(AUS) RIVETS LOCATED IN REAR FUSELAGE HAD THE RIVET HEADS DAMAGED BY BEING SANDEDFLAT.SDR AU980146Fitting · corroded(AUS) STABILISER ATTACHMENT FITTING LOCATED IN REAR FUSELAGE CORRODED AND RIVETS MISSING.SDR AU980145Rivet · loose(AUS) ELEVATOR TORQUE TUBE RIVETS LOOSE AND WORKING.SDR AU980144Spar · cracked(AUS) ELEVATOR SPAR AND RIB CRACKED.SDR AU980143Rivet · loose(AUS) ELEVATOR BALANCE TAB RIVETS LOOSE.SDR AU980142Stabilizer · corroded(AUS) VERTICAL STABILIZER SEVERELY CORRODED. FORWARD SPAR CORRODEDTHROUGH.SDR AU980141Stabilizer · corroded(AUS) HORIZONTAL STABILISER SEVERELY CORRODED.SDR AU980140Engine · worn(AUS) ENGINE EXHAUST VALVE GUIDES BADLY WORN. PISTON AND PISTON RINGS BADLY WORN. PISTON PINS AND CONNECTING ROD BUSHES WORN. OIL FILTER ALMOST COMPLETELY BLOCKED WITH CARBON. FUEL STRAINER LEAKING.SDR 99ZZZX637Lifter · damagedTHREE INTAKE LIFTERS WENT FLAT. NR 3 WOULD NOT PUMP UP CAUSING SERIOUS VIBRATION. THE OTHER TWO DID EVENTUALLY PUMP UP. REPLACED ALL LIFTERS. TIME ON ORIGINAL PART, 10 HOURS. LIFTERS WERE FROM SUPERIOR AIRPARTS, INC.SDR AU971434Fuel System · contaminated(AUS) FUEL SYSTEM CONTAMINATED BY WATER. ENGINE FAILURE RESULTED IN FORCED LANDING.SDR 97ZZZX3746Belt · debondedAN ALTERNATOR DRIVE BELT PURCHASED FROM API PARTS INTERNATIONAL WAS RECEIVED IN A DE-BONDED CONDITION ALONG WITH A SECOND BELT WHICH WAS NORMAL. CURE DATE ON DEFECTIVE PART, 1Q96/3Q01.SDR 97ZZZX3697Cylinder · crackedCYLINDER CRACKED FROM TOP SPARK PLUG HOLE TO BOTTOM SPARK PLUG HOLE AROUND THE EXHAUST VALVE. HEAD OPENED UP BY THE EXHAUST VALVE AND BLEW OUT THE SIDE AND BURNED FINS OFF THE CYLINDER. ENGINE SKIPPED AND RAN ON THE OTHER 5 CYLINDERS. CYLINDER BURNED PRETTYSDR AU970560Valve Guide · worn(AUS) NO3 AND NO4 CYLINDER EXHAUST VALVE GUIDES WORN - AIRCRAFT IS INVOLVED IN PARACHUTING OPERATIONSSDR AU970882Seat Belt · wrong part(AUS) SEAT BELT WAS AUTOMOTIVE PRODUCT - PERSONNEL/MAINTENANCE ERROR -UNAPPROVED PARTSDR AU960488Cap · leaking(AUS) FUEL TANK CAPS LEAKING - REPLACED BY TYPE PNO SK182-8513 - FOUND DURING INSPECTION IAW AD/CESSNA180/70 AMDT 1SDR AU960512Valve Guide · worn(AUS) NO1 CYLINDER EXHAUST VALVE GUIDE AND VALVE STEM WORN AND LEAKING - VALVE GUIDE AND VALVE ARE ONLY 70 HOURS TSNSDR AU960398Buckle · unsafe(AUS) FRONT SEATS BELT BUCKLES FAULTY - BUCKLES UNDO AT THE SLIGHTEST TOUCH WITHOUT ANY SIGNIFICANT LIFTING OF LEVER - THE SEAT BELTS HAVE COME UNDONE DESPITE PROPER TENSION ADJUSTMENT OF BELTS - BUCKLES ARE MANUFACTURED BY `AMSAFE' AND WERE FITTED FOLLOWINGSDR AU960027Bulkhead · cracked(AUS) FORWARD DOOR POST BULKHEAD CRACKED AT BEND RELIEF NOTCH ON RH SIDE - CRACK DISAPPEARS BEHIND DOUBLERSDR 95ZZZX6431Bulkhead · crackedDURING AN ANNUAL INSPECTION, THE BULKHEAD WAS FOUND CRACKED. ACCORDING TO CESSNA' C.A.P. FOR 100 SERIES AIRCRAFT, THIS IS A CRUCIAL PART OF A GOOD INSPECTION. SUBMITTER STATED IT IS ALSO NOTEWORTHY THAT BECAUSE THE AD ON THE SUBJECT TALKS MORE SPECIFICALLY ASDR 95ZZZX6012Actuator · required lubePILOT REPORTED FLAPS WOULD NOT EXTEND IN-FLIGHT, BUT FUNCTION PROPERLY ON THE GROUND. FOUND JACKSCREW HAD NOT BEEN LUBED IAW CESSNA MANUALS, BULLETINS, AND AD, AND HAD WORN OUT JACKSCREW AND COLLAR. INSTALLED NEW UNIT.SDR 95ZZZX5632Flap · departedRIGHT COWL FLAP DEPARTED AIRCRAFT IN-FLIGHT. SUSPECT CORROSION BETWEEN HINGE AND STEEL PIN. SUBMITTER RECOMMENDS IF ANY EXCESSIVE PLAY IS DETECTED IN HINGE AREA, REMOVE AND REPLACE HINGE, ESPECIALLY IF HINGE STILL LOOKS SERVICEABLE. THIS CORROSION IS HIDDEN
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