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 = '152' 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 = '152' 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 CA030526006Magneto · failed(CAN) DURING RUN UP IGNITION SYSTEM CHECK REVEALED POWER LOST ON RT MAGNETO. UNIT REPLACED WITH SERVICEABLE MAGNETO AND GROUND RUN OK. UNIT SENT BACK FOR CREDIT THUS INTERNAL PROBLEM IS UNKNOWN AT THIS TIME.SDR 2002FA0000940Piston Pin · wornFACTORY ENGINE OVERHAUL O1/01. ALUMINUM IN FILTER DUE TO NR 1 PISTON PIN WEAR.SDR 2002FA0000937Piston Pin · wornFACTORY OVERHAUL 12/96. REMOVED AND REPLACED NR 4 CYLINDER DUE TO PISTON PIN WEAR/ CYLINDER RIDGE. DATE OF OCCURANCE 01/00.SDR 2002FA0000936Piston Pin · wornFACTORY OVERHAUL 12/96. REMOVED ENGINE FOR ALUMINUM CONTAMINATION. NR 1 PISTON PIN WEAR, NR 3 PISTON PIN WEAR.SDR 2002FA0000935Cap · wornREMOVED NR 1 CYLINDER DUE TO PISTON PIN CAP WEAR, INSTALLED CHROME CYLINDER. FACTORY OVERHAUL 02/28/90SDR 2002FA0000933Cap · wornFACTORY OVERHAUL ENGINE 02/28/96. RIGHT NR 2, 3 CYLINDERS HAD SOME WEAR IN PINS, NOT BAD. HAND INSTALLED NEW CAPS AND RINGS. OCCURED 10/05/00SDR 2002FA0000932Cap · wornFACTORY OVERHAUL 02/28/96. OCCURRED 12/26/00. REMOVED NR 1 CYLINDER METAL IN FILTER, CAPS WORN. INSTALLED NEW FACTORY CYLINDER.SDR 2002FA0000931Piston Pin · wornFACTORY OVERHAUL 24-9. INSTALLED ALL NEW FACTORY NEW CYLINDERS DUE TO METAL CONTAMINATION FROM PISTON PIN CAPS. OCCURRED 05/07/2001SDR 2002FA0000930Piston Pin · wornREMOVED NR 1 CYLINDER. INSTALLED ANEW PISTON PIN CAPS/ WEAR WAS NOT NORMAL. THIS ENGINE FACTORY OVERHAUL 9/24. OCCURED 11/3/98SDR 2002FA0000929Piston Pin · wornREMOVED NR 1 CLYINDER DUE TO POSTON PIN CAP WEAR INSTALLED CHROME CYLINDER ASSEMBLY OCCURED 02/15/2002.SDR 2002FA0000927Piston Pin · wornCYLINDER 1 AND 3 DAMAGED DUE TO PISTON PIN WEAR. ALUMINUM IF FILTER TOTAL TIME ON CYLINDERS WAS 400 HR. TSMOH FOR ENGINE 1095.3, OCCURED 9/26/01 INSTALLED CHROME CYLINDERS.SDR 2002FA0000882Piston · wornTHIS ENGINE SENT BACK TO THE FACTORY FOR METAL CONTAMINATION AND REWORKED THERE. ALL NEW CYLINDERS INSTALLED.SDR AUS20020364Pushrod · cracked(AUS) DURING PERIODIC ENGINE INSPECTION, THREE PUSHRODS WERE FOUNDCRACKED AT THE BALLENDS. TWO HAD CRACKS 0.470IN (12MM) LONG AND THE THIRD HAD A CRACK JUST STARTING.SDR 2002FA0000939Cap · wornTHIS ENGINE FACTORY OVERHAUL 12/96. ALUMINUM IN FILTER, NR 1 CYLINDER WEARS A RIDGE FROM RING IN FORWARD SIDE THEN THE RIDGE WEARS PISTON PIN. DATE OF OCCURANCE 03/98SDR 2002FA0000938Cap · wornFOUND ALUMINUM IN FILTER REMOVED AND REPLACED NR 2 CYLINDER DUE TO PISTON PIN WEAR FROM RIDGE IN CYLINDER. DATE OF OCCURANCE 11/98SDR CA020503004Stiffener · cracked(CAN) PART FAILED IN THE CUT-OUT OF THE LOAD-BEARING MEMBER.SDR 2002FA0000472Torque Tube · brokenPILOT LEFT RUDDER PEDAL TORQUE TUBE BROKE AT WELD FOR PEDAL ARM. RESULTING IN PILOT HAVING REDUCED OR NO LEFT RUDDER OR NOSE STEERING. POSSIBLY CAUSED BY A DEFECTIVE WELD.SDR 2002FA0000934Cap · wornFACTORY OVERHAUL 02/28/96. RIGHT NR 2 CYLINDER DUE TO PISTON PIN WEAR. INSTALLED CHROME CYLINDER. 04/01/02SDR CA020312008Crankcase · damaged(CAN) DEFECT OBSERVED DURING ROUTINE MAINTENANCE. OIL LEAKING FROM CRANKCASE LT HALF NEAR CENTRE BOLTS THAT SECURE CASES TOGETHER. FURTHER INSPECTION REVEALED A PIN HOLE THAT APPEARS TO ORIGINATE FROM WITHIN/INTERNAL TO THE CRANKCASE. ENGINE REMOVED SENT TO APSDR 2002FA0000671Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD, WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THE SDR AUS20020142Exhaust Valve · burned(AUS) EXHAUST VALVE BURNED. VALVE NOT SEATING CORRECTLY.SDR 2002FA0000668Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD. WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THESDR CA020501011Skin · cracked(CAN) SKIN CRACKED AT UPPER LIGHTNING HOLE.SDR 2002FA0000279Contactor · stuckSTARTER ENGAGED UPON CLOSING AIRCRAFT MASTER SWITCH. FOUND S1577A1 CONTACTOR IN THE STUCK CLOSED POSITION, WITH NO ELECTRICAL POWER APPLIED. REPLACED CONTACTOR.SDR CA020208004Skin · cracked(CAN) - CRACK FOUND ON PRE-FLIGHT. - CRACK LOCATED AT OUTBOARD AFT CORNER OF ELEVATOR UNDER TRIM TAB HINGE.SDR 2002FA0000052Float · failedON LANDING THE ENGINE QUIT. FUEL WAS OBSERVED LEAKING FROM THE AIRCRAFT. DURING DISASSEMBLY OF THE CARBURETOR IT WAS NOTED BOTH FLOATS WERE FILLED WITH FUEL CAUSING FUEL TO POUR THRU THE VENT. THE MANUFACTURE DATE OF THE FLOAT WAS 4/92.SDR CA011219008Tube · jammed(CAN) A/C HAS 15120.6 T.AT. TIME ON PART UNKNOWN, MAY BE ORIG. UPON TAXI TO HOLD LINE, PILOT TURNED FULL LEFT THEN FULL RIGHT TO CHECK BRAKES & STEERING. PILOT APPLIED FULL POWER AFTER T/O CLEARENCE & HAD TO KEEP GREATER THAN NORMAL RIGHT RUDDER TO KEEP A/C STSDR 2001FA0000657Impulse Coupling · wornINSTALLED NEW M3007 IMPULSE COUPLINGS ON BOTH MAGNETOS. BOTH COUPLINGS CAME OUT OF BOXES DATED 5/25/01. INITIAL OPERATION WAS FINE. IMPULSE COUPLINGS INTERMITTENT SNAPPING. REMOVED MAGNETOS, INSPECTED COUPLINGS PAWLS SHOWED NOTICEABLE WEAR AT CONTACT POINT SDR 2001FA0000587Bearing · debondedPLATING ON BEARING UNBONDED FORM BACKING (ROD SIDE NOT THE CAP SIDE) DATE CODE ON BACK OF BEARING IS 200.SDR CA011102009Spring · broken(CAN) THIS IS SECOND OCCURANCE OF SAME DEFECT IN 1205 HRS/18 MONTHS. HAS ALSO OCCURED ON OTHER 152 IN OUR FLEET. OBSERVED DURING WALK-AROUND BY NEXT PILOT (RUDDER SWINGS FREELY WITHOUT NORMAL RESISTENCE). OUR AMO SAYS THAT BROKEN SPRING COULD INTERFERE WITH SDR 2001FA0000599Spar · crackedREMOVED ELEVATOR TO REPAIR WORN OUTBOARD HINGE BUSHINGS, AFTER ELEVATOR WAS REMOVED FOUND THE ELEVATOR SPAR CRACKED UNDER THE OUTBOARD HINGE WHERE IT ATTACHES TO THE SPAR, REPLACED SPAR WITH NEW.SDR 2001FA0000454Carburetor · defectivePILOT TOOK OFF IN AIRCRAFT, TURNED DOWNWIND AND ENGINE STARTED RUNNING ROUGH AND LOSING POWER. PILOT LANDED AC AND ENGINE QUIT AS HE PULLED OFF RUNWAY. ALL SYSTEMS CHECKED POINTED TO INSTALLED NEW REBUILT CARBURETOR AND ENGINE FUNCTIONED NORMALLY. PROBABLESDR 2001FA0000316Mount · grooved1. DURING A ROUTINE INSPECTION, TWO ENGINE MOUNT DIAGONALS WERE FOUND TO HAVE WORN AREAS ON THEM CAUSED BY THE BATTERY TRAY FLEXING DOWN AGAINST THE MOUNT AND FROM A STAINLESS STEEL TAG ON THE OIL PRESSURE LINE.2. THE CLAMP THAT SUPPORTS THE BATTERY TRAY ON THSDR CA011004017Seal · torn(CAN) - AIRCRAFT ROUGH RUNNING, NOT PRODUCING FULLPOWER. AIR BOX REMOVED AND BUTTERFLY SEAL FOUND UNSERVICEABLE. A SMALL PIECE A SEAL WAS FOUND IN CARB. VENTURI. A NEW AIR DOOR SEAL WAS INSTALLED.- AIRCRAFT GROUND RUN & CHECKED OK.SDR 2001FA0000326Windshield · crackedWINDSHIELD CRACKED DIRECTLY ABOVE COMPASS BLOCK AND SMALL SECTION 12 INCHES BY 6 INCHES WITH COMPASS ATTACHED. SUSPECT CRACK DEVELOPED ABOVE COMPASS BLOCK, PERHAPS BY FUELER LEANING ON WINDSHIELD, AND THEN CONTINUED TO DEVELOP CRACK UNTIL SECTION LOST INTERGRSDR 2001FA0000211Placard · fodDURING TOUCH AND GO LANDING AS CARB HEAT WAS APPLIED, ENGINE LOST POWER. REMOVING CARB HEAT DID NOT IMPROVE PERFORMANCE. DURING INVESTIGATION AND CARB REMOVAL, FOUND STARTER LUBRICATION DECAL LODGED IN VENTURI. AFTER REMOVAL AND REINSTALLATION OF CARB. ENSDR CA010808002Carburetor · malfunctioned(CAN) ENGINE STARTED LOSING POWER WHILE IN CRUISE AT 2500 FT & 30 SEC LATER QUIT RUNNING. PILOT INSTRUCTOR MADE A FORCED LANDING IN HAY FIELD. ENGINE WOULD NOT START AGAIN. CARBURATOR WAS REPLACED AND ENGINE STARTED TO RUN NORMALLY AND AIRCRAFT WAS FLOWN OFF FSDR AUS20011057Cable · corroded(AUS) SEVERAL FLIGHT CONTROL CABLES RUSTY. THE FOLLOWING CABLES WEREFOUND TO BE UNSERVICEABLE:- 1. PNO 0400107-41 AILERON CABLE (2OFF)2. PNO 0400107-21 BALANCE CABLE 3. PNO 0400107-45 FLAP CABLE4. PNO 0400107-46 FLAP CABLES 5. PNO 0400107-30 TRIM CABLE6. PNO 0SDR AUS20011053Exhaust Valve · failed(AUS) NO3 CYLINDER EXHAUST VALVE HEAD SEPARATED FROM VALVE STEM CAUSING MAJOR DAMAGE TO CYLINDER AND PISTON. SUSPECT CAUSED BY CORROSIONAND EROSION DAMAGE. INVESTIGATION FOUND TWO OF THE OTHER THREEEXHAUST VALVES IN SIMILAR CONDITION WITH THE LAST EXHAUST VALVSDR CA010725005Rudder Horn · cracked(CAN) UPON COMPLYING WITH AD CF-2000-20 RE. RUDDER INSPECTION, FOUND LOWER RIB P/N 0431004-24 CRACKED. LEVER RUDDER FAIRING HAD TO BE REMOVED IN ORDER TO REPAIR RIB. UPON FAIRING REMOVAL, FOUND RUDDER HORN CRACKED IN TWO PLACES AT RADIUS. I FEEL THIS DAMAGE WASDR CA010628002Release System · sheared(CAN) 3 OF 4 LATCH PINS CONTROLLING SEAT NIGHT FOUND SHEARED AT ENGAGEMENT HOLE ALLOWING SEAT TO DROP AND TILT.SDR 2001FA0000092Cylinder · crackedDURING ROUTINE INSPECTION, FOUND NR 1 CYLINDER TO BE CRACKED ABOVE THE INTAKE VALVE GUARD AREA. WHEN PRESSURIZED, THE ENTIRE LENGTH OF THE CRACK PRODUCED BUBBLES.SDR 2001FA0000091Fitting · crackedDURING ROUTINE 100 HR INSPECTION, MINOR CORROSION WS FOUND ON BOTH LEFT AND RIGHT VERTICAL STABILIZER ATTACH FITTINGS, APPROX BS 200.4. UPON REMOVAL OF CORROSION, A CRACK WS FOUND IN THE RADIUS OF THE RIGHT FITTING APPROXIMENTLY .7500 OF THE WAY ACROSS AND APPSDR 2001FA0000041Sump · failedINDUCTION TUBE ATTACHED TO OIL SUMP BECAME LOOSE CAUSING ROUGH RUNNING ENGINE. ENGINE OIL SUMP REPLACED TO CORRECT PROBLEM.SDR 2001FA0000030Tube · looseINDUCTION TUBE ATTACHED TO OIL SUMP BECAME LOOSE CAUSING ROUGH RUNNING ENGINE. ENGINE OIL SUMP REPLACED TO CORRECT PROBLEM.SDR SW15200112285Spar · crackedCRACK IN UPPER LIGHTING HOLE, UNDER THE TOP HINGE, IN THE LEADING EDGE RUDDER SKIN/SPAR. TO PREVENT RECURRANCE, REMOVE OR ELEMINATE LIGHTING HOLE IN NEW OR REPLACEMENT PARTS.SDR 2001FA0000586Mount · crackedPILOTS RIGHT HAND LOW RUDDER PEDAL ASSEMBLY MOUNT CRACKED AROUND WELD CAUSING ON GROUND LOSS OF DIRECTIONAL CONTROL AND MADE BRAKING DIFFICULT.SDR CA010508009Bracket · loose(CAN) MOUNTING BRACKET FOR PORTABLE ANTENNA HAS LOOSE FIT AND ALLOWS ANTENNA TO FALL OUT. MS 28775-009 O-RING USED TO RETAIN ANTENNA.SDR CA010510010Torque Tube · cracked(CAN) CRACK FOUND IN WELD FROM TORQUE TUBE TO CABLE ARM. CRACK WAS APPROXIMATELY 0.125 INCH LONG AT THE END OF WELD.SDR CA010510008Spar · cracked(CAN) 4 CRACKS WERE FOUND ORIGINATING FROM A 1.0 INCH DIA. LIGHTENING HOLE, 1.50 INCH BELOW UPPER RUDDER HINGE BRACKET. NOTE: REPLACEMENT SPAR WITH THE SAME P/N FROM CESSNA DOES NOT HAVE THIS LIGHTENING HOLE.
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