Continental GTSIO-520-C
Service difficulty reports · 44
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 = 'GTSIO520C' 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 = 'GTSIO520C' 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 17GR159B092401Governor · failedAFTER ROTATION PROPELLER WENT INTO FEATHER AND ENGINE SHUT DOWN WITHOUT ACTION ON THE PART OF THE PILOT. GOVERNOR WAS FOUND TO BE BEYOND ECONOMICAL REPAIR. PROPELLER AND GOVERNOR O/H 1006.8 PRIOR TO THIS EVENT. PILOT WAS BALE TO CONTINUE CLIMB ON 1 ENGINE AND SDR HYIA20150729003Control Cable · disconnectedPILOT REPORTED NO PROPELLER RPM CONTROL THROUGH LEFT PROPELLER LEVER. FOUND LEFT PROPELLER CONTROL CABLE DISCONNECTED AT GOVERNOR. CONNECTED WITH PROPER HARDWARE IAW MM 61-20-00. OPS CHECKED GOOD.SDR 2014FA0000721Screw · shearedRPM AND MANIFOLD PRESSURE STARTED FLUCTUATING FOR THE RT ENGINE. WHITE SMOKE FROM TURBO CHARGER VENTS WAS NOTED AS WELL AS OIL STREAKS NOTED. OIL PRESSURE DROPPED TO BOTTOM OF GREEN ARC ON THE OIL PRESSURE GAGE. EMERGENCY PROCEDURE CHECKLIST CALLED FOR ENGISDR BGJA2014042300002Alternator · failedTHE ACFT HAD TOTAL ELECTRICAL FAILURE DURING FLIGHT, DUE TO BOTH CHARGING SYSTEMS FAILING TOGETHER. RT ALTERNATOR FAILED DURING CRUISE, SHORTLY AFTER LT ALTERNATOR FAILED DUE TO A FAILED DRIVE CLUTCH. THE RT ALTERNATOR APPEARED TO HAVE AN INTERNAL SHORT THATSDR 2012FA0000596Clamp · crackedTURBOCHARGER TURBINE TO TAILPIPE V BAND CLAMP, FOUND TO HAVE A 3" LONG CRACK ALONG THE OUTER PERIMETER OF THE V BAND. CRACK SEPARATION WAS LESS THAN .0625" AT THE WIDEST POINT. THIS IS NOT A MULTI-SEGMENT V BAND. NO EXHAUST LEAK EVIDENT. DISCOVERED DURING SDR 2010FA0000522Blade · looseON CLIMB OUT, ACFT BEGAN TO SHAKE, IT BEGAN TO SHAKE WORSE AS THE FLIGHT PROGRESSED. FLIGHT LANDED SAFELY AT THE INTENDED AIRPORT. AFTER INSPECTION IT WAS REVEALED ONE OF THE PROPELLER BLADES WAS LOOSE. REMOVED PROPELLER AND SENT TO PROP SHOP FOR OVERHAUL.SDR T9ZR725Y4370/40Blade · leakingPROP WAS OBSERVED TO BE LEAKING GREASE FROM TWO BLADE SHANK AREAS. SPINNER WAS REMOVED FOR INSP AND ALL 3 BLADES APPEAR TO BE LEAKING GREASE. ONE BLADE WAS OBSERVED TO HAVE EXCESSIVE BLADE SHANK MOVEMENT BEYOND ALLOWABLE LIMITS. WHEN BLADES WERE CHECK FOR BLADSDR T9ZR725Y4370/41Blade · damagedPROP WAS OBSERVED TO BE LEAKING GREASE FROM 2 BLADE SHANK AREAS. SPINNER WAS REMOVED FOR INSP AND ALL 3 BLADES APPEAR TO BE LEAKING GREASE. 1 BLADE WAS OBSERVED TO HAVE EXCESSIVE BLADE SHANK MOVEMENT BEYOND ALLOWABLE LIMITS. WHEN BLADES WERE CHECK FOR BLADE TWSDR 2009FA0000845Cylinder · crackedREPAIRED CYLINDER FOUND TO BE CRACKED SPARK PLUG TO INJECTOR.SDR 2009FA0000844Cylinder · crackedREPAIRED CYLINDER FOUND TO BE CRACKED SAME PLACE AS OTHERS, SPARK PLUG TO INJECTOR.SDR 2009FA0000843Cylinder · crackedREPAIRED CYLINDER FOUND TO BE CRACKEDSDR 2009FA0000841Cylinder · cracked12/25/08 6 CRACKED TCM CYLINDERS WERE REPLACED.SDR D382008F00000Thru Bolt · broken22.2 HOURS AFTER INSTALLING AN OVERHAULED (ALV9510) ALTERNATOR, THE PILOT CAME TO ME ABOUT A THRU BOLT THAT WAS COMING OUT OF THE ALTERNATOR CASE. THERE WAS ONE THRU BOLT STICKING OUT OF THE CASE AND ANOTHER HAD COME OUT AND WAS GONE. THE ALTERNATOR WAS CHARGISDR TVD2006F00000Cylinder · crackedNR 3 CYLINDER ON THE LT ENGINE CRACKED COMPLETELY AROUND THE HEAD, APPROX 1.25 INCHES ABOVE THE BASE OF THE HEAD. THE CRACK WAS COMPLETELY AROUND THE CIRCUMFERANCE OF THE HEAD AND ALLOWED THE HEAD TO SLIP OFF OF THE BARREL, HALF AN INCH. THE PROP WAS FEATHERSDR 2006FA0000002Circuit Breaker · corrodedAVIONICS MASTER CIRCUIT BREAKER SWITCH FOUND INTERMITTENT DURING COMPLIANCE WITH AD 2005-20-05, MEB05-1. PN 593-240-101 NOT FOUND IN MFG PARTS MANUAL BUT THIS WAS CLEARLY THE ORIGINAL FACTORY INSTALLED CB. PROBLEM NR1, INTERNAL COMPONENTS OF CB HAD SEVERE CSDR TZR2005F00022Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS. RT NR 4. (SW05200509363). (K)SDR TZR2005F00023Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 3. (K)SDR TZR2005F00024Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS. RT ENGINE, NR 3. (SW05200509364) (K)SDR TZR2005F00025Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS. RT ENGINE, NR 3 CYL. (SW05200509364) (K)SDR TZR2005F00026Cylinder · crackedCRACK IS TYPICAL FOR THESE CYLINDERS, RT ENGINE NR 6 CYLINDER. (SW05200509365) (K)SDR 2005FA0001054Antenna · inoperativeFOUND UPPER UAT ANTENNA UNSERVICEABLE. (K)SDR TZR2005F00017Cylinder · crackedCRACKED FROM EXHAUST VALVE TO TOP SPARK PLUG. ECI CYLINDER. (SW05200507950) (K)SDR 2005FA0000517Hinge · misinstalledAIRCRAFT WAS HERE FOR COMPLETE EXTERIOR REPAINT. AFTER REMOVING RUDDER, COMPLIED WITH MFG MEB004. IT IS JUST A VISUAL INSPECTION, BUT IT DOES REQUIRE REMOVING THE RUDDER. FOUND THAT RUDDER HINGE ASSY WAS INSTALLED UPSIDE DOWN. FOUND THAT ABOUT 75 PERCENT OSDR 2005FA0000396Rib · crackedDURING AN ANNUAL INSP, NOTED CRACKS IN LT AND RT WING T/E RIBS AT FORWARD END AFT SPAR ATTACHMENT POINT AREAS. AFFECTED RIBS ARE FIRST RIBS IB OF SPOILER SYSTEM ACTUATOR ATTACH POINTS. ALSO FOUND CRACKED AREA IN WING OB T/E SKIN PANEL AT ATTACHMENT POINT TO SDR 2005FA0000397Bulkhead · crackedDURING AN ANNUAL INSPECTION, FOUND AFT BULKHEAD OF THE LT WING TIP TANK ASSY. CRACKED THROUGH FROM APPROXIMATE CENTER OF THE IB LIGHTENING HOLE HORIZONTALLY TO THE BULKHEAD IB EDGE. CRACKED AREA IS ADJACENT TO AFT ATTACH POINT FOR THE TIP TANK ASSY. AIRCRAFSDR 2004FA0000927Bracket · misinstalledCOMPLIED WITH MFG MEB 00-4 RUDDER BEARING INSPECTION/REPLACEMENT. FOUND RUDDER LOWER HINGE BEARING BRACKET INSTALLED UPSIDE DOWN FROM FACTORY. REPLACEMENT PROCEDURE DESCRIBED IN MEB FOUND ERRONEOUS AND INADEQUATE TO COMPLETE SATISFACTORY REPLACEMENT OF BRACKSDR 2005FA0000125Crankshaft · brokenCRANKSHAFT BROKE AT NR 2 MAIN. NO SIGNS OF OIL STARVATION. NO SIGNS OF CASE FRETTING. CASE WAS DAMAGED BEYOND REPAIR. (K)SDR 2004FA0000355Cylinder Head · crackedAIRCRAFT NDT SERVICE WAS CONTRACTED TO VERIFY CRACKS IN THE ENGINE CYLINDER HEADS BETWEEN THE SPARK PLUG AND FUEL INJECTOR MOUNTING BOSS. AN EDDY CURRENT EXAMINATION DETERMINED THAT ALL TWELVE CYLINDER HEADS WERE CRACKED. THE OPERATOR REPLACED ALL TWELVE CYLISDR 2003FA0001035Bearing · destroyedAIRCRAFT LANDED EXITED ONTO TAXIWAY, FELT VIBRATION IN NOSE OF AIRCRAFT, FELL NOSE FIRST ONTO TAXIWAY. THE BEARINGS IN NOSE WHEEL FROZE AND SHEARED AXIAL. LANDING GEAR STRUT STRUCK GROUND AND COLLAPSED. THE BEARING AND ROLLER RETAINER ON ONE SIDE HAD DISINTSDR 2003F00283Gear · brokenREMOVED RIGHT INOPERATIVE ALTERNATOR FOR REPAIR AND NOTED. CRANKCASE DAMAGED, ALTERNATOR FACE GEAR, BROKEN AND LOOSE. FACE GEAR ATTACH BOLTS, DAMAGED AND LOOSE. (M)SDR 2002FA0001271Windshield · failedWHILE AT CRUISE ALT FL240, PILOTS FRONT WINDSHIELD DEPARTED THE AIRCRAFT ALONG WITH PART OF THE INSTRUMENT GLARE SHIELD AND PILOTS SUN VISOR. LAB EXAM OF WINDSHIELD DID NOT REVEAL POINT OF FAILURE BUT DID STATE NUMEROUS INSTALLATION DISCREPANCIES. MAINTENANCSDR TXH2002F00000Downlock Switch · failedPILOT REPORTED LT MAIN GEAR DOWN AND LOCKED BUT NO GEAR DOWN INDICATION. FOUND DOWN LOCK SWITCH FAULTY. REPLACED SWITCH AND COPLETED RETRACTION TEST SATISFACTORY.SDR 2002FA0000656Insulator · burnedON REPLACING LEFT WING LOCKER FUEL CELL, DISCOVERED (PN 5656006-2), FIREWALL FIRE SCREEN COATING BURNED THROUGH BEHIND TURBOCHARGER. REMOVED RIGHT NACELLE TOP SKIN AND DISCOVERED OTHER (PN 5656006-2) FIREWALL FIRE SCREEN IN SIMILAR CONDITION. INSTALLED NEWSDR MHJ2002F00000Transfer Pump · inoperativeTRANSFER PUMP, INOPERATIVE.SDR 2002FA0000665Structure · corrodedDURING INSPECTION OF THE WING NACELLE BAGGAGE COMPARTMENT STRUCTURE CORROSION WAS DISCOVERED UNDER THE TRIM AND CARPETS. UPON REMOVAL OF THE NACELLE BAGGAGE COMPARTMENT TRIM AND CARPETS SEVER SURFACE CORROSION WAS DISCOVERED. MAJOR SECTION OF THE NACELLE STRSDR IBU2001F00000Bolt · shearedALTERNATOR CASE THIN BOLTS ARE SHEARING. BOLTS THAT RECOVERED FROM ENGINE COWLING, SHOWS SIGNS OF STRETCHING. BOLTS POSSIBLE OVER TORQUED FROM FACTORY.SDR 2001FA0000462Cylinder · malfunctionedLEFT ENGINE EXPERIENCED A VIBRATION. PILOT ELECTED TO LAND . REPLACED NR 2 CYLINDER. CLEANED VALVE GUIDES ON REMAINING CYLINDERS. REPLACED SPARK PLUG ON NR 1 CYLINDER. FLIGHT CHECK GOOD.SDR VDQ2001F00000Cylinder · crackedALL 6 CYLINDER CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217SDR VDQ2001F00001Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR VDQ2001F00003Cylinder · crackedALL 6 CYLINDERS CRACKED AT 781.6 HOURS SINCE NEW. SERIAL NUMBERS: 52A0016149, 52A0016150, 52A0016201, 52A0016202, 52A0016215, 52A0016217.SDR 20010511CW010Spar Cap · crackedDURING AN ANNUAL INSPECTION, A CRACK APPROX 3 INCHES LONG WAS FOUND ON LEFT WING AFT SPAR, UPPER AFT CAP. BELOW BAGGAGE RACELLE.SDR AU990862Switch · faulty(AUS) COMBUSTION HEATER FAULTY. AIR VALVE SWITCH JAMMED IN THE ON POSITION. VENT MOTOR MAIN POSITIVE LEAD NOT LOCKED TO THE POWER SOURCE CAUSING ARCING ON THE POST. MAIN HEAD GASKET CRACKED AND PERISHED. FUEL NOZZLE CONTAMINATED WITH RUST AND SCUM. OVERSDR AU970724Fitting · corroded(AUS) UPPER RH FUSELAGE WING ATTACHMENT FITTING CONTAINED EXFOLIATION CORROSION ON LOWER SURFACESDR 95ZZZX1456Starter Adapter · failedAIRCRAFT LANDED AFTER DARK 2-9-95, WITH THE LEFT ENGINE SHUT DOWN. FOUND STARTER ADAPTER HAD TWO BROKEN TEETH AND METAL THROUGHOUT THE ENGINE. VERY ROUGH AIRCRAFT.
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