Continental C90 series
Service difficulty reports · 18
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'C90' 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 engine_model_key = 'C90' 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 2011FA0000338Fuel Sys · unbalancedOWNER NOTES THAT UNEVEN FUEL DRAW FROM FUEL TANKS, HAS SUPPLIED VENTED CAPS. RT TANK DOES NOT DRAW EVEN WITH LT TANK. RT TANK STAYS FULL AS LT TANK LOWERS. THIS HAPPENS ABOVE 95 MPH IAS. FUEL SYS HAS BEEN CHECKED FOR BLOCKAGE, NONE FOUND. PRESSURE IN TANKSDR 2008FA0000258Tape · looseDURING FLIGHT, THE FABRIC PATCH CAME OFF. THE AC WAS LANDED WITH SOME DIFFICULTY BUT WITHOUT INCIDENT. IT IS SPECULATED THE AIR STREAM GOT UNDER A LOOSE TAPE AND LIFTED THE ENTIRE PATCH FROM THE WING INCLUDING RIPPING THE FABRIC CLIPS OUT OF THE RIBS. IT ISSDR 2007FA0000714Spar · crackedAIRCRAFT WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSP HOLE KITS AS SUPPLIED IAW STC NR SA00527SE. A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUSDR 2007FA0000859Spar · crackedAC WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSPECTION HOLE KIT IAW STC NR SA005278E. A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUPPLIED WITH TSDR 2006FA0000980Rotor · inoperativePILOT NOTICED LACK OF POWER AND ROUGHNESS AFTER TAKEOFF. RETURNED TO FIELD, DISCOVERED INOPERATIVE RT MAGNETO. DISASSEMBLY OF RT MAGNETO REVEALED ROTOR SHAFT HAD SHEARED FLUSH WITH BOTTOM OF CAM CUTOUT. THE REMAINING ROTOR AND DISTRIBUTOR BOTH ROTATED FREELSDR 2006FA0000577Gauge · stuckAIRCRAFT LOST POWER AND LANDED IN A HAYFIELD UP ON ITS NOSE. PILOT STATED HE CHECKED THE FUEL GAUGE PRIOR TO THE FLIGHT AND IT READ (HALF FULL). HE DID NOT VISUALLY CHECK THE QUANTITY. INVESTIGATION REVEALED FUEL TANK TO BE EMPTY AND GAUGE STUCK IN THE (HALSDR 2006FA0000349Spar Cap · crackedDURING ACCOMPLISHMENT OF SB NR 32, A 0.625 INCH LONG, SPANWISE CRACK WAS NOTED ON THE RT UPPER SPAR CAP IN THE MAIN SPAR CENTER SECTION APPROX 0.250 INCH IB OF THE CENTER SECTION OB END. PROBABLE CAUSE IS UNKNOWN. (K)SDR 2006FA0000135Bolt · brokenBOLT LOCATED TOP OF SPRING OF LANDING GEAR, 3 OF THESE BOLTS HOLD THE SPRING GEAR ON. ALL 3 BOLTS FAILED, RECOMMEND ALL 3 BOLTS IN BOTH MAIN GEAR REPLACED EACH, 1000 HRS TIME IN SERVICE. (EA13200602813) (K)SDR 2003FA0000297Rib · corrodedLIGHT SURFACE CORROSION FOUND IN BOTH STUB WINGS IN CENTER SECTION. BOTTOM SKINS, UNDER SKIN STIFFNERS, A COUPLE SPOTS ON RIBS, AND BETWEEN REAR SPAR AND REAR RIB P/N 415-1307RINSPECTION WAS IN COMPLIANCE WITH AD 2002-26-02.SDR 2002FA0000637Spar · crackedIN COMPLYING WITH AD, FOUND CRACK AT BUTT OF MAIN SPAR JUST UNDER ATTACH FITTING TO FUSELAGE ON RIGHT WING TRAVELING SEVERAL INCHES LONGITUDINALLY. SEVERAL RIB NAILS LOOSE ON BOTH WINGS. AIRCRAFT HANGARED-CAUSE UNKNOWN, (HOURS ON WINGS 5000 TO 6000), REPAIR SDR 2002FA0000254Spar · crackedDURING THIS ANNUAL INSPECTION FOUND COMPRESSION CRACKS ON THE RIGHT WING REAR SPAR AT TOP LOCATION ON TOP SIDE OF SPAR. THIS COMPRESSION CRACK WAS HIDDEN UNDER OLD SPAR VARNISH AND WOULD HAVE BEEN MISSED IF TOP INSPECTION HOLES WERE NOT INSTALLED ALSO MANY OTSDR 2002FA0000260Strut · damagedWING STRUTS HAD FILLED WITH WATER FROM SITTING OUTSIDE. RUST STAINS VISIBLE FROM OUTSIDE OF STRUT. WHEN POKED WITH AN AWL IT PUSHED A HOLE INTO STRUT AND DRAINED WATER. DRILLED A .0312 HOLE IN BOTTOM OF OTHER 3 STRUTS AND WATER CAME OUT IN EXCESS OF 1 CUP ESDR 2002FA0000261Spar · crackedCRACK ON BOTTOM SURFACE OF SPAR LEFT SIDE REAR. FOUND PRIOR TO CRACK INSPECTION AS PER AD, OWNER DISCONTINUED ANNUAL INSPECTION PRIOR TO FULL INSPECTION.SDR 2002FA0000246Spar · defectiveCRACK VISIBLE MIDWAY FROM TOP TO BOTTOM OF RIGHT WING FRONT SPAR FROM 44 INCHES INBOARD ALONG SPAR TO APPROXIMATELY 130 INCHES FROM INBOARD. WOOD APPEARS TO BE IN GOOD CONDITION OTHER WISE. DEFECT DISCOVERED DURING SPAR INSPECTION IN COMPLIANCE WITH AD. AIRSDR 2001FA0000339Lead · severedNEGATIVE LEAD FROM LOWER BATTERY COMPARTMENT TO TRANSMITTER WAS SEVERED DUE TO CORROSION. LOWER AND UPPER BATTERY. CONTACTS WERE CORRODED AND PLATING HAD FLAKED OFF. ONE OF THE EIGHT DURACELL BATTERIES WAS DEAD BUT NO CORROSION ON IT AND HAD NO BATTERY LEAKSDR 2001FA0000387Spar · crackedDURING INSPECTION TO COMPLY WITH AD, CRACKS WERE FOUND INBOARD AND LEFT FRONT SPAR, INBOARD END RIGHT REAR SPAR. .001 FEELER GAGE COULD BE INSERTED .1250 OR MORE INTO CRACKS.SDR 20010326CW005Spar · crackedDURING ANNUAL INSPECTION, FOUND COMPRESSION CRACKS ON THE RIGHT WING REAR SPAR AT TOP LOCATION ON TOP SIDE OF SPAR. THIS COMPRESSION CRACK WAS HIDDEN UNDER OLD SPAR VARNISH AND WOULD HAVE BEEN MISSED IF TOP INSPECTION HOLES WERE NOT INSTALLED.SDR AU960834Needle · deteriorated(AUS) CARBURETTOR FLOAT NEEDLE RUBBER TIP HARDENED AND DEFORMED - OBSOLETE PART
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