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 = '182P' 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 = '182P' 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 AUS20040257Rivet · corroded(AUS) FUSELAGE SKIN RIVET HEADS CORRODED AND MISSING. RIVETS ARE LOCATED IN THE AREA UNDER THE BELLY OF THE AIRCRAFT AND ATTACH THE MAIN LANDING GEAR CASTINGS PNO 0741627-1 AND PNO 0741627-2 TO THE FUSELAGE BELLY SKIN.SDR 2004FA0000298Bulkhead · crackedDURING COMPLIANCE WITH AD72-07-09 REFERENCED BUKHEAD WAS FOUND CRACKED PART REPLACED WITH NEW. SUSPECT FAILURE OCCURRED DUE TO AGE.SDR 6604Fitting · brokenABORTED TAKEOFF AFTER LOUD NOISE HEARD ON TAKEOFF AND RUDDER KICKED FULL DEFLECTION. FOUND NOSE GEAR LOWER FITTING BROKEN IN TWO, INSPECT THIS FITTING CLOSELY AT ANNUAL.SDR AUS20031269Bolt · bent(AUS) NLG UPPER TORQUE LINK UPPER BOLT TO STEERING COLLAR SEVERELY BENT AND ALMOST SHEARED. INVESTIGATION ALSO FOUND THE STRUT UNDER EXTENDED DUE TO BEING OVERFILLED WITH OIL AND UNDER INFLATED WITH AIR.SDR 2003FA0001201Tab · brokenOUTBOARD RIB OF EACH CANARD WING CRACKED. OUTBOARD TAB LEFT SIDE CANARD BROKEN IN TWO. OUTBOARD HINGE TAB OF RT CANARD WING CRACKED.SDR 2003FA0001200Rib · crackedOUTBOARD RIB OF EACH CANARD WING, CRACKED. OUTBOARD HINGE TAB, LEFT SIDE CANARD BROKEN IN TWO. OUTBOARD HINGE TAB OF RT CANARD WING CRACKED.SDR CA030711002Bulkhead · cracked(CAN) BULKHEAD WAS CRACKED UNDER ANCHOR DOUBLER AT TOP LT HORIZONTAL STABILIZER ATTACH BOLT.SDR AUS20030366Rivet · missing(AUS) AIRCRAFT CONTAINED NUMEROUS DEFECTS. FOUND WHEN NEW OWNER TOOK DELIVERY. PERIODIC INSPECTION HAD BEEN CARRIED OUT SIX WEEKS (13HOURS) PREVIOUSLY. DEFECTS FOUND WERE: MISSING RIVETS ON THE RT WING MAIN SPAR DUE TO CORROSION. PROPELLER HAD 97 HTR NOT 597 ASDR 2003FA0000513Bulkhead · crackedWHEN PERFORMING A FULL STALL LANDING THE TAIL TIE DOWN STRUCK THE GROUND (RATHER HARD). INSPECTION FOUND NO DAMAGE OTHER THAN SCUFFING OF THE TIE DOWN RING. FOUND ALL FIVE NUTS AND BOLTS TO BE TIGHT TO BOTH FINGER PRESSURE AND WRENCH, COMPLIENCE WITH AD. WHSDR 2002FA0001256Float · separatedCARBURETOR, LEAKING ON AIRCRAFT. SUSPECT FLOAT OR FLOAT NEEDLE STUCK. REMOVED CARBURETOR, REMOVED BOWL. HALF OF FLOAT PONTOON COMPLETELY SEPARATED FROM FLOAT ASSY. SOLDER JOINT HOLDING FLOAT TO ARM SEPARATED.SDR 2002FA0001254Oil Cooler · leakingFACTORY REBUILT ENGINE, INITIAL START UP OIL COOLER LEAKS, REMOVED COOLER AND BASE PLATE AND CHECKED SURFACES, SURFACES FOUND NOT TO BE FLAT.SDR CA030106013Flap Track · cracked(CAN) A SPLIT FLAP CONDITION OCCURRED WHEN THE FLAPS WERE RAISED FROM 30 DEGREES TO ZERO DEGREE. THE UPPER FLAP SUPPORT CAUGHT THE FLAP TRACK SKIN SUPPORT BRACKET CAUSING LEFT FLAP TO JAM AND THE RIGHT FLAP TO CONTINUE TO GO UP.SDR 11509Wheel · crackedON REPLACING A WARN OUT TIRE WE FOUND THE CENTER HUB TO HAVE A CRACK AT 9 OF THE FLANGE MOUNTING BOLT HOLES, WE INSPECTED THE OTHER WHEEL/HUB FOUND IT TO HAVE 4 CRACKS. REPLACED BOTH WHEELS WITH CLEVELAND TWO PIECE WHEELS. WE HAVE FOUND 6 OF THE SAME WHEELS (HSDR AUS20020764Connector · deteriorated(AUS) FLEXIBLE FUEL LINE CONNECTORS PERISHED.SDR AUS20020698Skin · corroded(AUS) FLAP SKINS CONTAINED EXTENSIVE SURFACE CORROSION.SDR AUS20020697Structure · corroded(AUS) BOTH HORIZONTAL STABILISER AND FIN CONTAINED EXTENSIVE SURFACECORROSION.SDR AUS20020293Bulkhead · cracked(AUS) RT FORWARD DOORPOST BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/C180/75 A2.SDR 20010501CW016Air Box · failedDURING ANNUAL INSPECTION, IT WAS NOTED THAT THE RIVETS THAT SECURE THE CARB HEAT VALVE PLATE TO THE CONTROL CROSS SHAFT WER COMING LOOSE. THIS APPEARS TO HAVE BEEN CAUSE BY SEALING MATERIAL ON THE VALVE PLATE WHICH WAS NOT CORRECTLY TRIMMED. AS A RESULT, THESDR 2001FA0000103Snap Ring · failedEXTERNAL SNAP RING ON PROPELLER BLADE CAME OFF AFTER PREFLIGHT ENGINE HAD STOPPED ON INITIAL START, THEN WAS RESTARTED. SNAP RING CAME OFF BLADE SHANK BUT WAS RETAINED BY SPINNER. THEN AIRPLANE WAS FLOWN FOR 2 HOURS WITH FIVE TOUCH AND GO LANDINGS, WITHOUT FSDR 20010327CW010Engine · defectiveFACTORY NEW ENGINE GROUND TESTED ONLY. PROPELLER WILL NOT CYCLE. HAVE RECHECKED PROPELLER AND GOVERNOR. PROBLEM APPEARS TO BE ENGINE OIL PRESSURE, INSUFFICIENT TO CYCLE PROPELLER. WARRANTY RETURN.SDR 20010129CW013Door · crackedFORWARD DOOR POST, INSPECT AND MOD. FOUND CRACK ON RT SIDE. THE SEB CALLS FOR INITIAL INSPECTION AT 4000 HOURS. I HAVE FOUND THIS CONDITION ON 3 AC. 2 OF THE 3 HAD LESS THAN 2000 HRS T/S. HISTORY ON BOTH IS NORMAL SERVICE AND NO PASST DAMAGE OR ABUSIVE USESDR 20001108SH019Spring · crackedTHREE YEARS AFTER REPAIR OF CRACKS IN MAIN LANDING GEAR LEG FAIRING USING A RIVETED PATCH, FOUND THAT HEADS OF RIVETS HAD WORN 7 HOLES (DEPRESSIONS) ABOUT .010 INCH DEEP IN GEAR LEG. CONSULTED CESSNA TECH SERVICE WHO STATED LEG MUST BE REPAIRED OR REPLACED DUSDR AU001169Actuator · faulty(AUS) ELEVATOR TRIM ACTUATOR HAD EXCESSIVE PLAY IN THE SHAFT/INTERNAL SCREW COMBINATION RESULTING IN EXCESSIVE TRIM TAB FREEPLAY. THE UNIT HAD ONLY 62.2 HOURS SINCE NEW.SDR 20001012SH011Bulkhead · crackedNEW PART AS RECEIVED FROM CESSNA. RE-INSTALLATION INSPECTION FOUND THE .3750 INCH DIAMETER BOLT HOLES ELONGATED AND OVERSIZED, EXCEEDING THE ACCEPTABLE LIMITS FOR BOLT HOLES LISTED IN AD 7207-09 PARA C)2)B) AND CESSNA SL SE 72-3. DETERMINED THE FINISHING PROSDR AU000692Bulkhead · cracked(AUS) LEFT DOORPOST BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/C180/75. (X)SDR 20000724SH026Air Box · detachedDURING T/S OF ROUGH ENG OPERATION FOLLOWED BY NOTED REDUCTION IN AVAILABLE POWER, THE ALTERNATE-AIR DOOR PN 1652013-25 WAS FOUND LOOSE IN THE INDUCTION BOX. THE HINGE PIN HAD SLID OUT OF THE HINGE ALLOWING THE DOOR TO PARTIALLY OBSTRUCT THE AIR FLOW TO HE ENSDR AU000511Lifter · worn(AUS) HYDRAULIC VALVE LIFTERS (TAPPETS) WORN AND PITTED. EVIDENCE OF PITTING ON THE CAMSHAFT. (X)SDR AU000420Nut · cracked(AUS) NR 5 CYLINDER THROUGH BOLT NUT SPLIT.SDR CA000519009Stringer · misinstalled(CAN) AIRCRAFT FUEL STRAINER INSPECTED IAW AD 2000-06-01 EVEN THOUGH THE TECHNICAL RECORDS DID NOT INDICATE THE FUEL STRAINER TOP ASSY HAD BEEN CHANGED DURING THE SPECIFIED TIME PERIOD. THE FUEL STRAINER TUBE WAS FOUND TO BE LONGER THAN THE SPECIFIED LENGTH, SDR 20000515SH011Gasket · damagedDURING CRUISE, THE PILOT OBSERVED OIL COMING UP THE WINDSHIELD AND BOTH SIDE WINDOWS. HE DECLARED AN EMERGENCY AND MADE A SAFE AIRPORT LANDING. THE ENGINE HAD APPROXIMATELY 3 QUARTS OF OIL REMAINING. THE OIL LEAK WAS CAUSED BY A SPLIT IN P/N 5A625303 GASKETSDR CA000505023Windshield · failed(CAN) 2 HOURS INTO FLIGHT CAPTAINS WINDSHIELD OUTER PANE SHATTERED. WINDSHIELD REPLACED, HEAT CONTROLLER REPLACED AND SYSTEM CHECKS CARRIED OUT SERVICEABLE.SDR 20000508SH016Flap Track · crackedSHEARED RIVETS AT FORWARD LOWER END OF FLAP TRACK AND CRACKED FLAP TRACKMOUNTING ANGLE LOWER END FORWARD. WING FLAP WAS DAMAGED WHEN FLAPS WERE RETRACTED AND CONTACT WAS MADE WITH BRACKET IN FLAP WELL. POSSIBLE CAUSE, OPERATING FLAPS AT HIGHER THAN NORMAL SSDR AU000148Cylinder · broken(AUS) NR 2 CYLINDER EXHAUST VALVE ROCKER BOSS BROKEN.SDR 20000407SH002Lifter · damagedDURING THE REMOVAL OF THE NR 3 CYLINDER, THE EXHAUST VALVE LIFTER WAS INSPECTED AND FOUND TO HAVE CHIPS OF MATERIAL MISSING FROM THE CORNERS NEAR THE LOWER FACE. THE FACE OF THE LIFTER AND CAM LOBE WERE NOT FOUND TO HAVE ANY DEFECTS. (X)SDR 20000407SH001Cylinder · wornDURING A ROUTINE COMPRESSION CHECK, THE NR 3 CYLINDER WAS FOUND TO HAVE EXCESSIVE LEAKAGE 53/80 PAST THE PISTON RINGS. THE REMOVED CYLINDER WAS FOUND WORN OUT AT THE TOP OF THE CYLINDER. (X)SDR 99ZZZX4680Cylinder · wornDURING A ROUTINE COMPRESSION CHECK, THE NR 3 CYLINDER WAS FOUND LEAKING EXCESSIVELY PAST THE INTAKE VALVE. THE EXHAUST VALVE AND PISTON RINGS WERE REMOVED. CYLINDER WAS FOUND TO HAVE A DEFORMED INTAKE VALVE FACE, A WORN OUT EXHAUST VALVE, AND GUIDE AND NO CHSDR 99ZZZX4386Cylinder · wornDURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND GOING PAST THE PISTON RINGS ON THE NR 1 CYLINDER. THE REMOVED CYLINDER IS FOUND TO BE WORN OUT AND HAD A NEGATIVE CHOICE.SDR 99ZZZX3652Bulkhead · crackedSMALL CRACK ON LEFT TOP AND RIGHT TOP LIGHTNING HOLES IN BULKHEAD. CRACK ORIGINATED FROM TIGHT RADIUS IN LIGHTNING HOLES. THIS M OR D REPORT SUBMITTED PER AD 72-07-09 AND PART WAS REPLACED WITH NEW.SDR 99ZZZX3592Cylinder · wornDURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND PAST THE PISTON RINGS ON THE NR 2 CYLINDER. THE REMOVED CYLINDER WAS FOUND WORN TO A BELL MOUTH CONDITION AT THE TOP OF THE CYLINDER BORE.SDR 99ZZZX3591Cylinder · wornDURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND PAST THE PISTON RINGS ON THE NR 6 CYLINDER. THE REMOVED CYLINDER WAS FOUND WORN TO A BELL MOUTH CONDITION AT THE TOP OF THE CYLINDER BORE.SDR 99ZZZX3577Valve · wornDURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND LEAKING PAST THE PISTON RINGS ON THE NR 4 CYLINDER. THE REMOVED CYLINDER WAS FOUND TO HAVE A WORN OUT EXHAUST VALVE, A WORN OUT VALVE GUIDE, AND WORN TO A BELL MOUTH CONDITION AT THE TOP OF THESDR AU990905Cylinder · worn(AUS) CYLINDER EXHAUST VALVE AND VALVE GUIDE WORN. CYLINDER HAD TWO VALVES AND VALVE GUIDES REPLACED IN ONLY 474 HOURS OF OPERATION.SDR AU990875Cylinder · worn(AUS) CYLINDER EXHAUST VALVE AND VALVE GUIDE WORN PREMATURELY. THE CYLINDER HAD TWO VALVE AND VALVE GUIDE REPLACEMENTS FOR WORN ITEMS IN 474 HOURS OF OPERATION.SDR AU990871Cylinder · failed(AUS) NR 2 CYLINDER CONNECTING ROD BROKEN. CRANKCASE HOLED IN THE AREA BELOW THE MAGNETOS. NR 2 CYLINDER AND THE SURROUNDING AREA DAMAGED. SUBMMITTER SUSPECTED CAUSED BY INCOMPATIBILITY BETWEEN THE CYLINDER BORE SURFACE TREATMENT AND THE PISTON RING MATERIASDR 99ZZZX3486Magneto · damagedWHILE DOING AN ANNUAL INSPECTION, BOTH MAGS WERE FOUND TO HAVE LOOSE DISTRIBUTOR BLOCKS. THE SCREWS IN THE LEFT MAGNETO WERE COMPLETELY OUT AND THE BLOCK FELL OUT WHEN THE COVER WAS REMOVED. THE INSIDES OF BOTH BLOCKS WERE VERY DIRTY AND DID NOT LOOK LIKE THSDR CA990817027Fork · cracked(CAN) CRACK FOUND ON THE NOSE LANDING GEAR UPPER FORK INNER CORNER. REPLACED.SDR CA990817026Cylinder Head · cracked(CAN) NR 4 CYLINDER FOUND CRACKED AT THE CYLINDER HEAD SPARK PLUG BOSS.SDR 99ZZZX2471Counterweight · looseDURING START-UP OF THE ENGINE, THE NR 1 CYLINDER TRAILING COUNTER WEIGHT ON THE CRANKSHAFT CAME LOOSE FROM CRANKSHAFT AND MADE A HOLE IN THE TOP OF THE CASE. CSB99-3A HAD BEEN COMPLETED 1.7 HOURS PRIOR. REASON FOR FAILURE UNKNOWN AT THIS TIME.SDR AU990348Blade · damaged(AUS) PROPELLER BLADES (2OFF) DAMAGED IN THE BLADE SHANK RETENTION AREA. THE DAMAGE ON ONE BLADE HAD BEEN ANODIZED OVER.SDR 99ZZZX1604Bulkhead · crackedTHIS REPORT SUBMITTED IAW PARAGRAPH I OF AD 72-07-09. REAR FUSELAGE BULKHEAD CRACKED AT TOP OF RIGHT RUDDER CABLE CUT-OUT BY RUDDER STOP BOLT.
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