JASC 8500
Service difficulty reports · 745
Reports filed under 8500 · Engine (Reciprocating), newest first.
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 jasc_code = '8500' 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 jasc_code = '8500' 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 20010212CW004Engine · failedUNEXPECTED ENGINE FAILURE DURING LANDING FLAIR. ON DUAL TRAINING FLIGHT, IP DEMONSTRATING A SHORT-FIELD LANDING , OVER AN OBSTACLE, IN THE LANDING FLAIR, THROTTLE IDLE, ENGINE QUIT, PROP STOPPED TURNING. IP LANDED UNEVENTFULLY AND PULLED OFF RUNWAY. CREW PESDR 20001103SH010Engine · making metalABOUT 5 MINUTES AFTER TAKEOFF FROM HSV, THE NR 4 ENGINE OIL PRESSURE WENT TO 50 PSI. THE FLIGHT CREW ELECTED TO RETURN TO HSV. THE OIL PRESSURE NEVER WENT BELOW 50 PSI AND THERE WAS NO OVERTEMP CONDITION. THE PROPELLER WAS NOT FEATHERED. ON INSPECTION OF TSDR 20001012SH005Bearing · making metalFOUND METAL IN FILTER. SENT SAMPLE OF FILTER TO LYCOMING. THEY SAID IT WAS BEARING MATERIAL AND RECOMMENDED TAKING OUT OF SERVICE. (X)SDR 20000831SH015Engine · failedAIRCRAFT WAS IN-FLIGHT WHEN ENGINE LOST ALL OIL PRESSURE, AND HAD A CATASTROPHIC FAILURE. AIRCRAFT WAS ABLE TO MAKE A SAFE OFF-FIELD LANDING WITH NO STRUCTURAL DAMAGE. ENGINE WAS OVERHAULED ENGINE FROM LYCOMING. ENGINE SHOPPED TO LYC FOR INSPECTION. (X)SDR 20000911SH012Flyweight · crackedRELEVANT MAG PARTICLE INDICATION ON FLYWEIGHT TOE. (X)SDR 20000911SH011Gear · crackedRELEVANT MAG PARTICLE INDICATION ON IDLER GEAR TEETH. (X)SDR 20000911SH010Gear · crackedRELEVANT MAG PARTICLE INDICATION ON GEAR TEETH. (X)SDR 20000911SH019Engine · making metalDURING OIL CHANGE AND OIL FILTER INSPECTION, FOUND METAL IN THE OIL FILTER AND METAL WAS FOUND IN THE SUCTION SCREEN. 50 TO 60 PIECES WERE FOUND IN OIL FILTER AND TWO FLAKES WERE FOUND IN THE SUCTION SCREEN. (X)SDR AU000568Engine · failed(AUS) ENGINE FAILED ON TAKEOFF RESULTING IN A FORCED LANDING. AIRCRAFT DAMAGED. GROUND RUNS ON ENGINE COULD NOT REPLICATE FAULT AND ENGINE RAN OK.SDR CA000718018Engine · making metal(CAN) DURING FIREFIGHTING OPERATIONS THE PILOT NOTICED AN INCREASE IN OIL TEMPERATURE AND A DECREASE IN OIL PRESSURE. POWER WAS REDUCED AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT RETURNED TO YKA. THE MAIN OIL SCREEN AND THE HIGH CAPACITY OIL SCREENS WERE RESDR 20001011SH001Camshaft · making metalDURING 50-HOUR INSPECTION, FOUND A FEW CHIPS IN OIL FILTER. 10 HOURS LATER, NO CHIPS FOUND. DURING 100-HOUR INSPECTION, AGAIN, SOME CHIPS. ENGINE CONTROLLED WITH A MORE DETAILED INSPECTION. FOUND CAMSHAFT CYLINDERS 3 AND 4 WORN OUT EXTREMELY. AIRPLANE WAS SDR NACA200000014Cylinder · damagedZONE 1 FIRE INDICATION ON NR 1 ENGINE ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED NR 9 CYLINDER ON NR 1 ENGINE DUE HOLE IN PISTON AND PULLED STUDS AT CASE.SDR CA000714029Gasket · blown(CAN) AIRCRAFT CENTER FUEL TANK INADVERTENTLY FUELED WITH JET B IN KANGIRSUK, QUE ALTHOUGH SEALED DRUM CLEARLY MARKED JET B IT ALSO LABELLED GASOLINE 100 LL NR 19 OF 30 ON M. AIRCRAFT THEN FLEW FROM YAS TO MNR CAMP AT KANGISAVIP LAKE USING ONLY FIRST TANK, USDR AU000588Engine · making metal(AUS) DURING CRUISE, A DROP IN INDICATED OIL PRESSURE AND A RISE IN OIL TEMPERATURE WAS OBSERVED. A POST INSPECTION FOUND THE OIL FILTER CLOGGED WITH ALUMINIUM AND WHITE BEARING METAL CONTAMINATION.SDR 20000720SH019Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS DUPLICATED THE PROBLEM, BUSDR AU000512Engine · deteriorated(AUS) ENGINE IN A DETERIORATED AND POOR CONDITION. SOME UNAPPROVED PARTS FITTED. (X)SDR 20000720SH018Engine · failedPILOT REPORTED ENGINE SURGING ON TAKEOFF WITH SIGNIFICANT FUEL FLOW FLUCTUATION WHICH WAS CORRECTED WITH A DECREASE IN ENGINE POWER BY ADJUSTMENT OF THE PROP CONTROL AND ACTIVATION OF THE STANDBY ELECTRIC FUEL PUMP. POST-GROUND RUNS COULD NOT DUPLICATE THE PRSDR 20000328SH001Engine · malfunctionedENGINE RAN ROUGH AND ALMOST SHUT DOWN DURING DESCENT. (X)SDR CA000328004Engine · making metal(CAN) ENGINE MAKING METAL. TEAR DOWN REPORT REQUIRED.SDR AU000030Hose · collapsed(AUS) LT CARBURETOR SKEET HOSE INTERNAL LINER COLLAPSED BLOCKING AIR INTAKE. ENGINE FAILURE CAUSED AIRCRAFT TO CRASH.SDR 20000331SH021Engine · roughTHE ENGINE WAS REPORTED ROUGH IN CRUISE. CORRECTIVE ACTION WAS TAKEN AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X)SDR 20000407SH030Engine · malfunctionedWHILE IN THE PATTERN ON A DUAL FLIGHT, THE ENGINE BEGAN TO RUN ROUGH ON THE CROSS-WIND LEG. IT CONTINUED DOING SO ON DOWN-WIND. AN EMERGENCY WAS DECLARED AND A SUCCESSFUL LANDING WAS MADE. (X)SDR 20000407SH029Engine · malfunctionedDURING FINAL APPROACH, THE ENGINE STUMBLED AND RAN ROUGH. (X)SDR 20000330SH002Case · crackedPILOT NOTED OIL LEAK. DURING INSPECTION FOR OIL LEAK, ENGINE CASE WAS FOUND CRACKED BELOW NR 1 CYLINDER BASE PAD. CRACK IS APPROXIMATELY 4.5 INCHES PARALLEL TO CYLINDER PAD. ALSO FOUND NR 1 INTAKE TUBE LOOSE.SDR 20000403SH006Engine · making metalATL - RIGHT ENGINE PROPELLER WENT INTO FEATHER ON TAKEOFF. FOUND ALUMINUM PLUGGING PROPELLER SCREEN. REMOVED AND REPLACED ENGINE. SUBMITTER STATED CAUSE UNKNOWN AT THIS TIME. (X)SDR 20000413SH064Bearing · making metalDURING AN ANNUAL INSPECTION, FOUND METAL IN OIL SCREEN. REMOVED ENGINE AND SENT TO LYCOMING FOR REPAIRS. (X)SDR PNSA000204Engine · malfunctionedDURING TAKEOFF, ENGINE STARTED TO CUT OUT. RETURNED TO BASE. ENGINE, FUEL SYSTEM AND IGNITION SYSTEM WERE INSPECTED AND FOUND SERVICEABLE NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. NO FURTHER PROBLEMS HAVE BEEN NOTED.SDR CA000218003Gear · sheared(CAN) DURING FLIGHT, ENGINE STOPPED. IT WAS FOUND THAT THE CRANKSHAFT GEAR HAD FAILED. THE GEAR WAS STILL SECURELY FASTENED TO THE CRANK. AD 91-14-22.SDR AU000070Engine · making metal(AUS) LEFT ENGINE OIL FILTER NON-FERROUS METAL CONTAMINATION.SDR 2000ZZZX579Engine · making metalELM - LEFT ENGINE SHUT DOWN BY ITSELF IN-FLIGHT. ENGINE HAD PLENTY OF OIL, NO EXTERNAL LEAKS OR CRACKS, OIL FILTER FULL OF METAL. SUBMITTER STATED CAUSE UNKNOWN AT THIS TIME.SDR CA000218006Clamp · dislodged(CAN) DURING TAKEOFF, AN INDUCTION PIPE SEAL CLAMP SLIPPED OFF, CAUSING AN INDUCTION AIR LEAK AND SUBSEQUENT LOSS OF POWER.SDR AU000128025Engine · making metal(AU) ENGINE MAKING METAL.SDR PNSA000106Engine · malfunctionedON SHORT FINAL, ENGINE APPEARED TO SURGE. LANDING WAS UNEVENTFUL. NO FAULT FOUND. PURGED FUEL FLOW SENSE LINE.SDR CA000128053Engine · seized(CAN) ENGINE LOST ITS OIL AND SEIZED. OPERATOR SPECIFIED FROZEN BREATHER AS THE CAUSE.SDR AU000128053Engine · seized(AU) ENGINE LOST ITS OIL AND SEIZED. OPERATOR SPECIFIED FROZEN BREATHER AS THE CAUSE.SDR 99ZZZX4637Engine · malfunctionedTHE PILOT REPORTED A BRIEF POWER LOSS. THOROUGHLY INSPECTED ENGINE AND COMPONENTS. CLEANED AND INSPECTED SPARK PLUGS, FLOW DIVIDER, INSPECTED FUEL STRAINER AND SERVO SCREEN, CLEANED AND INSPECTED FUEL NOZZLES. A POST-MAINTENANCE GROUND RUN INDICATED NORMAL SDR 99ZZZX4636Engine · malfunctionedTHE PILOT REPORTED A BRIEF POWER LOSS. THE ENGINE AND RELATED SYSTEMS WERE INSPECTED. THE FLOW DIVIDER WAS DISASSEMBLED, CLEANED, AND RE-ASSEMBLED. A POST-MAINTENANCE GROUND RUN INDICATED NORMAL OPERATION.SDR 99ZZZX4634Engine · malfunctionedWHILE IN CLOSED TRAFFIC 7R AFTER COMPLETING TURN TO CROSSWIND, APPROXIMATELY 600 FEET AGL, THE ENGINE SPUTTERED AND PARTIALLY LOST POWER. THERE WAS A 300 RPM DROP FOR ABOUT 3 SECONDS. AFTER 3 SECONDS, POWER RETURNED TO NORMAL. NO EMERGENCY WAS DECLARED, ANDSDR 20000413SH047Engine · failedON CRUISE FLIGHT, RIGHT ENGINE STARTED TO VIBRATE AND LEAK OIL. PILOT DECLARED EMERGENCY AND LANDED AT TORTOLA AIRPORT (BEEF ISLAND). PRELIMINARY INSPECTION REVEALED RIGHT ENGINE CRANKCASE CRACKED. ENGINE CHANGE. (X)SDR CA991231003Engine · making metal(CAN) NON METALIC CHIPS FOUND IN SCREEN BUT NOT IN DISPOSABLE FILTER. ENG REMOVED.SDR 99ZZZX4640Engine · malfunctionedTHE PILOT REPORTED A MOMENTARY POWER LOSS. A COMPLETE INSPECTION OF THE ENGINE AND ENGINE SYSTEMS FOUND NO ABNORMALTIES.SDR 99ZZZX4407Engine · malfunctionedTHE PILOT REPORTED A MOMENTARY POWER LOSS. THERE WERE TWO SUCCESSIVE PERIODS OF POWER LOSS EACH TIME THE ENGINE RESTARTED. A COMPLETE INSPECTION OF THE ENGINE AND ENGINE SYSTEMS FOUND NO ABNORMALITIES.SDR CA991210019Engine · failed(CAN) ENGINE STOPPED AT ALT, ENG WOULD NOT RESTART. NO FAULTS WERE FOUND WITH ENG AT BENCH TEST AFTER INCIDENT.SDR 99ZZZX4423Engine · making metalAFTER DEPARTURE FROM MWO, RIGHT ENGINE OIL TEMPERATURE INCREASED AND OIL PRESSURE DROPPED TO REDLINE. AIRCRAFT RETURNED TO MWO. METAL FOUND IN OIL SCREEN. SUBMITTER SUSPECTED A FAILED MASTER ROD BEARING.SDR 99ZZZX4311Engine · malfunctionWHILE IN CRUISE AT 1,000 FEET, THE CREW EXPERIENCED A 1 TO 2 SECOND HESITATION. A COMPLETE INSPECTION OF THE ENGINE, RELATED COMPONENTS AND SYSTEMS DID NOT DISCLOSE ANY ABNORMALITIES.SDR P77A9902726Engine · making metalRIGHT ENGINE SHUT DOWN AFTER TURNING ONTO TAXIWAY AFTER LANDING. PILOT COULD NOT RESTART ENGINE. AFTER PARKING, PILOT NOTICED OIL ON COWLING AND WING. INSPECTION FOUND OIL LEAK IN VICINITY OF CYLINDERS 2 AND 4. ALSO, FOUND HEAVY METAL CONTAMINATION IN OIL.SDR 99ZZZX4262Engine · malfunctionedDURING NORMAL CLIMB, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS (2 SECONDS). THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPECT ITEMS WERE FOUND.SDR 99ZZZX4261Engine · malfunctionedDURING NORMAL CRUISE, CREW EXPERIENCED MOMENTARY ENGINE ROUGHNESS. THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPECT ITEMS WERE FOUND.SDR 99ZZZX4260Engine · malfunctionedWHILE DOING GROUND REFERENCE MANEUVERS, THE ENGINE RAN ROUGH FOR SEVERAL SECONDS. A THOROUGH INSPECTION WAS PERFORMED ON ALL ENGINE SYSTEMS AND NO SUSPECT ITEMS WERE FOUND.SDR 99ZZZX4258Engine · malfunctionedDURING NORMAL CRUIISE AT 3,500 FEET, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS. THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPECT ITEMS WERE FOUND.
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