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 CA041222004Crankcase · cracked(CAN) THE NR 4 CYLINDER HAD LOW COMPRESSION AND WAS REMOVED FOR REPAIR. WHILE THE CYLINDER WAS REMOVED, A CRACK WAS FOUND AROUND THE 4 O'CLOCK POSITION CYLINDER ATTACH STUD. THE CRACK WAS ABOUT 1.5 INCHES LONG RADIATING INWARD. THE ENGINE WAS REMOVED FORREPAIRSDR CA041216009Engine · malfunctioned(CAN) ON DEPARTURE, THE CREW HAD A POWER LOSS ON THE RT ENGINE, FEATHERED ENGINE AND RETURNED FOR A LANDING. THE ENGINE WAS REPLACED WITH A SERVICEABLE ONE AND THE AIRCRAFT RETURNED TO SERVICE. THE ENGINE SHALL BE OPENED IN OUR ENGINE SHOP IN THE NEAR FUTURE TSDR 2004F00431Ring Gear · crackedOPERATOR REPORTED THAT THE LEFT ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED DUE TO ROUGH RUNNING ENGINE SHORTLY AFTER TAKEOFF. MECHANIC INSPECTED ENGINE AFTER LANDING AND DISCOVERED CRACKED RING GEAR IN GEAR REDUCTION UNIT.SDR CA041122002Engine · failed(CAN) SMOKE ENTERED COCKPIT. PILOT RETURNED TO BASE. ENGINE LOST POWER AND BEGAN TO MISSON FINAL AND WAS SHUT DOWN.SDR CA041120001Engine · making metal(CAN) DURING 200 HR. INSP. THE OIL FILTER WAS CUT OPEN TO LOOK FOR METAL. FILTER ELEMENT WAS WASHED IN VAROSOL AND DRAINED THROUGH A FILTER TO REVEAL METAL PARTICLES. THE ENGINE SHOP WAS CALLED TO IDENTIFY THE METAL. WE PULLED NR 2 & 4 CYLINDERS TO OBSERVE TSDR 2005FA0000225Rod · nickedENGINE WAS RECEIVED FOR PHASE III MODEL CONVERSION. DURING TEARDOWN SEVERAL TIE RODS WERE FOUND WITH NICKED DOWN AREA IN THREADS. PARTS WERE SENT TO T.C. HOLDER FOR INVESTIGATION. REF RMR NR 31481.SDR NACA20040043Engine · overspeedNR 3 ENGINE SHUT DOWN DUE TO OVERSPEED AND LOSS OF OIL. FOUND NR 3 ENGINE SEIZED AND OIL OVERBOARD. REPLACED NR 3 ENGINE. CHECKED GOOD.SDR CA041017001Crankcase · cracked(CAN) THE CESSNA 185 WAS RETURNING TO HOME BASE FROM THE HUNTING CAMP, WHEN IN CRUISE,WITH ALL ENGINE PARAMETERS INDICATING NORMAL,THE ENGINE STOPPED IN FLIGHT AND T HE SEASONED PILOT WAS ABLE TO LAND WITHOUT INCIDENT. THE ENGINE SUFFERD TWO CRACKS TO THE CRANSDR 2005FA0001118Engine · making metalDURING OIL CHANGE (ROUTINE) FOUND BEARING MATERIAL COMING OUT OF SUMP PLUG. PIECES APPROX. .1250-.2500 INCH WIDE, .5 INCH LONG AND VARIOUS SMALLER PIECES. ENGINE WAS OVERHAULED 12/01/03: OWNER COMPLAINED OF VIBRATION FROM START. O/H SAID NORMAL. AFTER ENGSDR NACA20040034Engine · malfunctionedABORTED TAKE OFF DUE TO NR 2 ENGINE LOW FUEL FLOW AND LOW BMEP. PERFORMED 30 IN FIELD BARO ENGINE OP CHECK IAW OPS MANUAL SECT. 9.20. ALL PARAMETERS NORMAL, NO DEFECTS NOTED.SDR CA040910003Engine · making metal(CAN) DURING AN SCHEDULED INSPECTION, THE OIL FILTER WAS LITTERED WITH METAL CONTAMINATION. THERE WAS EVIDENCE OF BRASS, ALUMINUM AND FERRIOUS METAL. THE ENGINE WAS REMOVED AND WILL BE SENT TO THE OVERHAUL SHOP FOR FURTHER INVESTIGATION. THE PISTON PIN PLUGS ASDR CA040916006Engine · failed(CAN) FOLLOWING INSPECTION AND REPAIRS AS A RESULT OF EXHAUST VALVE FAILURE AIRCRAFT TAXIED ON WATER FOR TAKEOFF AND OIL PRESSURE DROPPED BELOW LIMITS. TAKEOFF ABORTED AND ENGINE REMOVED.SDR CA040831020Engine · making metalMAINTENANCE WAS CONDUCTING A 50 HR INSPECTION AND EXCESSIVE METAL IN FILTER. THE ENGINE WAS REMOVED FROM THE AIRCRAFT AND SENT TO AN OVERHAUL FACILITY. THE ENGINE WAS TORN DOWN AND INTERNAL COMPONENTS REVEALED THAT THE MAIN BEARING HAD FAILED DUE A OVERSPEEDSDR CA040825008Engine · failed(CAN) ON TAKEOFF ROLL THE RT ENGINE STARTED TO BACKFIRE AND LOOSE POWER, AT 90 KTS THE TAKEOFF WAS ABORTED MIXTURES TO IDLE CUT OFF,THE LOAD WAS DUMPED. THE A/C WENT OFF THE END OF THE RUNWAY, AT 1000 FEET BEYOND THE RUNWAY THE A/C IMPACTED A DITCH. THE PILOT SDR 2004FA0000636Engine · making metalFACTORY OVERHAUL FOUND FERROUS METAL FLAKES (SEVERAL HUNDRED) IN OIL FILTER. ENGINE REMOVED AND RETURNED TO MFG.SDR 2004F00351Camshaft · wornENGINE OIL FILTER CONTAINED MANY FINE FLAKES OF FERROUS MATERIAL. PREVIOUS SOAP SAMPLE SHOWED ELEVATED IRON CONTENT. VALVE LIFT OF THE NR 3 AND NR 4 INTAKE VALVES WAS APPROXIMATELY .15 INCH LESS THAN THAT OF VALVES IN THE OTHER CYLINDERS. REMOVING THE NR 3 SDR CA040716009Case · failed(CAN) DURING CLIMB THE NR 4 ENGINE WOULD NOT GOVERN, THE ENGINE WAS SHUTDOWN AND THE PROPELLER FEATHERED. THE AIRCRAFT RETURNED TO BASE WITHOUT FURTHER INCIDENT.SDR CA040716008Engine · malfunctioned(CAN) DURING CLIMB THE NR 4 ENGINE STARTED TO BACKFIRE AND SHAKE. THE ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED. THE FLIGHT RESUMED WITHOUT INCIDENT.SDR CA040716007Diaphragm · damaged(CAN) DURING CRUISE THE NR 4 ENGINE STARTED TO BACKFIRE AND SHAKE. THE ENGINE WAS SHUTDOWN AND THE PROPELLER FEATHERED. THE FLIGHT RESUMED WITHOUT INCIDENT.SDR K4S2004F00000Engine · failedON 6/18/04, RT ENGINE FAILED AT CRUISE AT 15,500 FT. ENGINE WAS SECURED AND EMERGENCY LANDING MADE. FLIGHT WAS PART 91 REPOSITIONING WITH NO PASSENGERS OR CARGO. (WP23200408767)SDR CA040628001Engine · failed(CAN) ENGINE SEIZED IN CRUISE FLIGHT. CASE BROKEN.SDR WVB2004F00001Unknown · unknownON 5/25/04, WHILE RETURNING, THE PILOT NOTICED AN INTERMITTENT LOSS IN MANIFOLD PRESSURE ON THE RT ENGINE. A GRADUAL LOSS OF OIL PRESSURE BEGAN TO DEVELOP SO THE PILOT SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE AND CONTINUED ON COURSE TO FAI. AIRPLANE LSDR 2004FA0000377Bearing · seizedTHIS WAS SECOND FLIGHT ON THE AIRCRAFT, AIRCRAFT DEPARTED, AND UPON CLIMB OUT ENGINE EXPERIENCED HIGH OIL TEMPERATURE AND REDUCED RPM, PILOT RETURNED TO RUNWAY AND LANDED SHORT OF RUNWAY THRESHOLD. EXAMINATION OF ENGINE BY THE PILOT REVEALED THAT MAIN BEARINGSSDR CA040421001Engine · vibration(CAN) DURING TAKEOFF, THE CREW NOTICED THE NR 1 ENGINE HAD A NOTICEABLE VIBRATION, THE TAKEOFF WAS ABORTED. THE ENGINE WILL BE REMOVED AND SENT FOR EVALUATION UNDER WARRANTY.SDR CA040405008Engine · malfunctioned(CAN) DURING CRUISE, THE CREW NOTICED THAT THE NR 3 ENGING WAS STARTING TO OVERSPEED. THE ENGINE WAS SHUTDOWN, PROPELLER FEATHERED, AND THE FLT RESUMED WITHOUTANY FURTHER ACTION.SDR X6PA000042004Engine · leakingSHORTLY AFTER TAKE OFF FROM RDU MARCH 31,2004, AT 1:45PM N130BW LOST OIL PRESSURE. THE PILOT TURNED BACK TOWARD THE FIELD; HOWEVER, BEING SHORT OF THE RUNWAY HE EMERGENCY LANDED ON A ROAD NEXT TO RDU. NO DAMAGE TO THE AIRCRAFT OR PILOT. UPON INSPECTION THE ENGSDR 2004FA0000383Engine · making metalDURING A PHASE INSPECTION, SOME METAL WAS FOUND IN THE FILTER, TOOK OIL SAMPLE FROM OIL COOLER, REMOVED SUCTION SCREEN, MORE METAL WAS FOUND, SENT FILTER AND OIL TO LAB FOR ANALYSIS, SENT METAL FROM SCREEN, WAS ADVISED THAT THE SCREEN MATERIAL WAS FROM BEARINSDR LAB2004F00000Engine · shutdownHAD INVOLUNTARY ENGINE SHUTDOWN DURING FLARE PORTION OF TOUCHDOWN ON RUNWAY. AFTER COASTING CLEAR OF ACTIVE RUNWAY, PILOT WAS ABLE TO RESTART ENGINE WITH EASE. AFTER DETERMINING ENGINE WAS OPERATING WITHIN NORMAL PARAMETERS, PILOT DELIVERED AC TO MAINT FOR FSDR 2004F00107Stud · looseDURING CLIMB OUT, THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE GAGE INDICATING A SIGNIFICANT INCREASE IN PRESSURE. WHEN THE RIGHT ENGINE STARTED TO RUN ROUGH THE ENGINE WAS SECURED AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURNED TO SDR 421C032204DGEngine · malfunctionedDURING A ROUTINE PREFLIGHT INSPECTION, PILOT NOTICED PULL THROUGH OF NR 1 ENGINE WAS MORE DIFFICULT THAN NORMAL FOR THAT ENGINE MAKE AND MODEL. A ENGINE START AND RUN-UP WAS PERFORMED TO NORMAL OPERATING TEMPERATURES; WITH NO ABNORMAL CONDITIONS NOTED OTHER TSDR NACA20040014Engine · leakingNR 2 ENGINE SHUT DOWN DUE TO RUNNING ROUGH AND DOUBLE SHORTED SECONDARIES ON MOST CYLINDERS. REPLACED NR 2 ENGINE DUE TO BLOWER SEAL LEAKING.SDR BHA03RSEngine · damagedDURING FLIGHT, RT ENGINE OIL PRESSURE GAGE INDICATED A SIGNIFICANT INCREASE IN PRESSURE. RT ENGINE DAMAGE OCCURRED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.SDR ENHA2004C2070Engine · shutdownON TAKE OFF AT 300 FT AGL PILOT EXPERIENCED ENGINE LOSS OF POWER, ENGINE QUIT. PILOT EMERGENCY ACTION IN ACCORDANCE WITH AFM RESTORED ENGINE OPERATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. L FUEL TANK HAD APPROX 25 GALS FUEL, R FUEL TANK HAD APPROX 25 GASDR 020204Engine · failedIN CLIMB POWER IN ROUTE RT ENGINE BEGAN TO MISFIRE AND RUN ROUGH. OIL TEMP ALSO INCREASED. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED. ENGINE WAS FOUND VERY HARD TO PULL THROUGH AND METAL FOUND IN SCREEN. SUSPECT CAM RING FAILURE.SDR CA040112004Engine · failed(CAN) DURING CLIMB THE PILOT NOTICED THE RT ENGINE OIL TEMPERATURE WAS INCREASING SIGNIFICANTLY. THE ENGINE WAS SHUT DOWN AND FLIGHT CARRIED OUT WITHOUT INCIDENT.SDR GZQ2004F00002Case Half · crackedA CRACK WAS FOUND ON THE LT CASE HALF TOP FORWARD SECTION.SDR GZQ2004F00001Case Half · crackedA CRACK WAS FOUND ON THE LT CASE HALF FORWARD OF TOP THROUGH BOLT.SDR 2003FA0001253Engine · failedAT CRUISE THE AIRCRAFT EXPERIENCED TOTAL POWER LOSS. REMOVING THE ENGINE, THE TECH NOTED GEAR TEETH IN THE OIL SUMP. ENGINE WAS SHIPPED TO MFG FOR ANALYSIS. NO DATA YET.SDR NAFA20030003Engine · overspeedNR 2 ENGINE RUNNING ROUGH AND LOOSING OIL. ENGINE/PROP OVERSPEED 3500 RPM. REPLACED NR 2 ENGINE.SDR 2003FA0001271Crankcase · failedDURING ROUTINE FLIGHT, LOUD NOISE WAS HEARD. RT ENGINE WAS SHUT DOWN AND SECURED. AFTER AN UNEVENTFUL LANDING, AN INSPECTION REVEALED A CATASTROPHIC CRANKCASE FAILURE AT THE NR 3 CYLINDER LOCATION HAD OCCURRED. CYLINDER WAS COMPLETELY SEPARATE FROM CASE. CSDR NACA20030124Engine · making metalNR 1 ENGINE PRECAUTIONARY SHUT DOWN DUE TO DOUBLE SHORTED SECONDARY AND LOSS OF OIL. REPLACED NR 1 ENGINE DUE TO MAKING METAL.SDR 2003FA0001211Crankcase · crackedLT SIDE (2.4.6) CRACKED IN CENTER MAIN BEARING BOSSES IN LOWER OIL ANNALYSIS.SDR J0F2003F00000Case · crackedOWNER/OPERATOR REPORTED OIL LEAKING FROM REAR OF ENGINE. AFTER THOROUGH CLEANING OF SUSPECTED OIL LEAK AREA, AC ENGINE WAS RUN-UP AND OIL WAS FOUND TO BE LEAKING FROM LT MAGNETO MOUNTING PAD AREA AND DRIPPING OFF OF AFT MAGNETO MOUNTING BOLTS. UPON REMOVAL OSDR NACA20030116Engine · making metalNR 3 ENGINE SHUT DOWN DUE TO LOSS OF BMEP. ENGINE MAKING METAL, REPLACED ENGINE.SDR 2003FA0001169Stud · brokenSTUD BROKEN AT CENTER, CAUSE UNKNOWN. NO RECOMMENDATIONS.SDR CA031021004Engine · failed(CAN) IN CRUISE THE LT ENGINE LOST POWER FOR APPROXIMATELY 5 MINUTES, THEN RESTARTED. THE ONLY INDICATION WAS A LOSS OF M.P. TO 20' AND A YAW TO THE LEFT. THE LT PROP WAS FEATHERED BUT CONTINUED TO ROTATE SO THE PILOT FELT THE ENGINE WAS STILL RUNNING AND UNFESDR DYV2003F00002Engine · failedSHORTLY AFTER TAKEOFF, THE PILOT EXPERIENCED AN UNEXPLAINED GRADUAL LOSS OF POWER ON THE LT ENGINE. AFTER FEATHERING THE LT PROP, THE PILOT MADE A SAFE, ON AIRPORT LANDING. UPON INITIAL INSPECTION AFTER LANDING, THE ENGINE WAS FOUND SEIZED AND UNABLE TO ROTASDR 092703Engine · failedAT CRUISE POWER FOR 3 HOURS ENROUTE FROM LRD-GMU, RT ENGINE STARTED RUNNING ROUGH AND BLOWING OIL OUT OF THE CRANKCASE BREATHER. AIRCRAFT DIVERTED TO LFT. SUSPECT CYLINDER AND SCAVENGE PUMP FAILURE.SDR 2003FA0001220Crankcase · crackedPHASE 3 CASE, 7TH STUD. CRACKED IN MAIN BEARING SADDLE AREA BOTH CENTER SADDLES. I OIL ANNULUS AREA.SDR 2003FA0001219Crankcase · crackedTHIS ENGINE WAS RECEIVED AS CORE ENGINE. THIS IS WHAT WE FOUND WHEN WE LIQUID PENETRANT INSPECTED IT: CRACKED IN BEARING SADDLES, LT SIDE BEARING BOSSES CENTERED.
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