Continental GO-300 series
Service difficulty reports · 16
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 = 'GO300' 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 = 'GO300' 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 2013FA0000396Contact · corrodedDURING INSPECTION OF ELT, FOUND TWO OF THE FOUR BATTERY CONTACTS CORRODED, THERE WAS NO EVIDENCE OF A LEAKING BATTERY. ELT WAS STILL FUNCTIONAL.SDR 2008FA0000281Mount · crackedINSP FOUND UPPER LT BRACKET (0513132-11) WITH A SMALL CRACK ORIGINATING FROM THE LOWER EDGE OF THE ENGINE MOUNT BOLT WASHER. ONLY A SMALL BEND LINE WAS VISIBLE FROM THE COCKPIT SIDE OF THE BRACKET VIA BOROSCOPE. AFTER REMOVAL OF THIS BRACKET A CRACK WAS CLEASDR RDA092407Transmitter · crackedWHILE CALIBRATING THE FUEL QUANTITY SYSTEM THE LT FUEL GAUGE WOULD SHOW AN INCREASE IN QUANTITY THEN START DECREASING. WHILE TROUBLESHOOTING THE LT TANK FUEL QUANTITY SENDER, FOUND 2 CRACKS APPROXIMATELY 1 INCH LONG IN THE BRASS FLOAT.SDR 2006FA0000902Cylinder · separatedNR (5) CYLINDER SEPARATED FROM THE CRANK-CASE IN FLIGHT RESULTING IN ENGINE FAILURE AND AN UN-PLANNED, SAFE LANDING OF THE AIRCRAFT.SDR 2006FA0000597Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACELETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)SDR 2006FA0000598Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)SDR 2006FA0000599Gusset · crackedFOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED. BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKEING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)SDR 2006FA0000250Bracket · crackedINSP 0513132-11, MOUNT BRACKET WAS FOUND TO BE CRACKED. CRACK RAN VERT THROUGH BRACKET AROUND OUTER RADIUS OF AN960-616 WASHER ON UPPER ENG MOUNT BOLT. INSP WAS DONE DUE TO 2 OTHER KNOWN REPORTS OF CRACKS IN THIS BRACKET ON SAME MODEL OF AC, ONE RESULTED IN A SDR 2006FA0000156Attach Bracket · crackedFOUND THE LT UPPER ENGINE MOUNT ATTACHMENT BRACKET CRACKED THROUGH ON THE IB SIDE. CRACK APPEARS TO HAVE ORIGINATED AT OUTER RADIUS OF WASHER THEN PROGRESSED UP AND DOWN THROUGH BRACKET. THIS INSPECTION WAS PROMPTED AFTER REPORTED FAILURE OF SAME BRACKET, SAMESDR 2005FA0001237Connecting Rod · brokenNR 3 CONNECTING ROD PENETRATED CASE. ENGINE TSO 848 HRS. LAST ENGINE O/H 06/10/1964 OR 41 YEARS AGO. MANUFACTURER RECOMMENDS 12 YEARS IAW SIL 98-9.SDR 2001FA0000257Block · corrodedDISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCK ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY PN 05121246 WITH (4) AW320A BOLTS. REMOVE FOR INSPECTION.SDR 2001FA0000258Block · corrodedDISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCKS ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY. PN 0511162-S WITH (4) AN3-21A BOLTS. REMOVE FOR INSPECTION.SDR 2001FA0000121Wire · defectiveAIRCRAFT BROUGHT TO BE CLEAN-UP WIRING BEHIND INSTRUMENT PANEL. UPON FURTHER INSPECTION I IMMEDIATELY DISCONNECTED THE SHIPS BATTERY DUE TO THE FACT THE WIRING WAS IN SUCH A DISARRAY I COULD NOT BELIEVE IT WORKED AND IF SO WHY IT HAD NOT CAUSED A FIRE. IE: ESDR 98ZZZX1859Piston · crackedAIRCRAFT WAS IN SHOP FOR ANNUAL INSPECTION, CHECKING COMPRESSIONS. FOUND 3 CYLINDERS WITH BELOW ACCEPTABLE COMPRESSION READINGS. PULLED CYLINDERS TO EXAMINE. FOUND BROKEN RINGS IN 2 CYLINDERS AND CRACKED PISTONS. DECISION WAS MADE TO REMOVE THE 3 OTHER ACCSDR 95ZZZX4597Cylinder · guide wornVALVE GUIDE WORN EXCESSIVELY. WOULD NOT PASS COMPRESSION CHECK. OWNER STATED HE WAS NOT USING AUTO FUEL. VALVE GUIDE WAS REPLACED.SDR 96ZZZX717Cylinder · guide wornVALVE GUIDE WORN EXCESSIVELY AND WOULD NOT PASS COMPRESSION CHECK. OPERATOR STATED ENGINE NEVER WAS OVERTEMPED AND WAS NOT USING AUTO FUEL. VALVE GUIDE WAS REPLACED.
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