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 CA091005006Engine · cracked(CAN) UPON INSP, MECHANIC DISCOVERED OIL LEAKING FROM BACK OF ENG. NEW BASE ASSY INSTALLED ACFT GROUND RUN AND LEAK CHECK OK.SDR CA090730007Engine · failedON CLIMB OIL PRESSURE WAS FALLING AND OIL TEMP CLIMBED TO 125 DEGREES CELSIUS. ENG SEIZED, OIL SCREENS AND MAG PLUGS FULL OF METAL.SDR CA090706004Engine · failed(CAN) ENGINE FAILED IN FLIGHT, WEATHER WAS GOOD, RESTART FAILED, ACFT MADE FORCED LANDING MINOR INJURIES. ACFT TO BE RECOVERED AND INVESTIGATED BY SAFETY BOARD.SDR CA090708005Engine · unknown(CAN) DURING TAKEOFF, PILOT REPORTED, LOST 60 PERCENT OF PWR, LANDING CARRIED OUT PERPINDICULAR TO RUNWAY IN GRASS. ONCE CLEARED BY NTSB ACFT INSPECTED IN FIELD AND NO DAMAGE FOUND. ACFT TOWED BACK TO BLOCKS WHERE VISUAL INSP REVEALED NO ABNORMALITIES. ACFTSDR HYIAN2611XEngine · failedON FINAL APPROACH, PILOT REPORTED LEFT ENGINE STARTED TO SPUTTER, AND RUN ROUGH, FOLLOWED BY SEVERE VIBRATION AND ENGINE STOPPAGE. MAINTENANCE FOUND CATASTROPHIC FAILURE OF THE LEFT ENGINE WITH A LARGE HOLE IN THE TOP ENGINE CASE FROM CONNECTING ROD PENETRATISDR CA090603004Engine · making metal(CAN) NR1 ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH OIL TEMP, SCREENS PULLED METAL AND ALUMINUM IN BOTH HIGH CAPACITY AND MAIN OIL SCREEN.SDR 2009FA0000696Engine · power lossEXPERIENCED LOSS OF ENG POWER. ATTEMPTED TO RESOLVE ENG PROBLEM, CHECKED CARB HEAT, FUEL VALVE, LT AND RT MAGS, THROTTLE, NO SUCCESS. ENG WOULD ATTEMPT TO RUN OCCASIONALLY FIRING ON CYLINDERS. FULL FUEL ON BOARD. (K)SDR CA090425001Engine · making metal(CAN) INITIALLY FAXED IN SDR APRIL 22, 2009. LOSS OF OIL PRESSURE INDICATION APPROX 5 MILES AFTER TAKE OFF, PILOT RETURNED TO AIRPORT. WHEN MX GOT THERE AND GROUND RUN ACFT OIL PRESSURE INDICATION NORMAL BUT OIL TEMP NOTICED HIGH. REMOVED AND INSPECTED OIL FSDR CA090417004Engine · failed(CAN) FORCED LANDING AFTER ENGINE FAILURES. MAJOR DAMAGE TO AIRCRAFT RIGHT WING, PROPELLER, RIGHT SIDE FUSELAGE, NOSE LANDING GEAR. LIMITED DAMAGE LEFT WING. ACFT REMAINED UPRIGHT, STRUCK TREES. WHEN REMOVING BATTERY TO SECURE ACFT IT WAS OBSERVED THAT THESDR 2009FA0000293Engine · burnedTHE ACFT EXPERIENCED A COMPLETE LOSS OF ENGINE POWER AFTER LANDING. THE PILOT TRIED TO RESTART THE ACFT ENGINE TWICE, WHILE ON RUNWAY 27R. AFTER ALLOWING APPROX 20 SECONDS FOR THE STARTER TO COOL THE PILOT NOTICED SMOKE FOLLOWED BY FLAMES. THE PILOT EXITED SDR HYIA763EABolt · unserviceableCREW REPORTED RIGHT ALTERNATOR INOPERATIVE. MAINTENANCE REMOVED ALTERNATOR AND FOUND ALTERNATOR DRIVE GEAR ATTACH BOLTS SHEARED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE.SDR BHKA52FN2202009Engine · failedTHE LT ENGINE ROLLED BACK TO SUB-IDLE DURING A SIMULATED ENGINE FAILURE DURING TAKEOFF. THE ENGINE PERFORMED NORMALLY DURING START, TAXI, AND THE INITIAL PORTION OF TAKEOFF. THE LT ENGINE ACCELERATED NORMALLY, AND THE THRUST LEVER POSITION AND ALL INDICATIONS SDR 2009FA0000069Gasket · leakingTRANSPORTING A PATIENT AND DIVERTED TO AIRPORT BECAUSE CREW DETECTED A BURNING EXHAUST ODOR IN THE CABIN. PILOT DID NOT SMELL IT, BUT DIVERTED FOR SAFETY. MECHANIC WAS ABLE TO DE-COWL NR 1 ENG. FOUND A CONSIDERABLE AMOUNT OF RESIDUAL OIL/FUEL. CLEANED AREASDR 2009FA0000047Engine · making metalDURING CERTIFICATION TEST FLIGHT, ENGINE OIL PRESSURE BEGAN TO DROP WITH AN INCREASE IN TEMPERATURE. AN UNEVENTFUL PRECAUTIONARY LANDING AT A LOCAL AGRICULTURAL AIRSTRIP WAS MADE. POST FLIGHT REMOVAL OF THE ENGINE OIL SCREEN REVEALED THE PRESENCE OF WHAT APPEASDR BSYA2009008Engine · damagedEN ROUTE FROM MKE TO STP, PILOT NOTICED LEFT ENGINE SLOWING DOWN AND OIL PRESSURE DROPPING. SHUT THE ENGINE DOWN AND DIVERTED TO MCN. MAINTENANCE FOUND NR 6 CYLINDER CONNECTING ROD BUSTED THROUGH THE CASE. REMOVED AND REPLACED ENGINE.SDR CA090129005Engine · malfunctionedPILOT REPORT, ENGINE FAILED ON RUNWAY FOLLOWING FULL POWER APPLICATION AFTER DOING TOUCH AND GO. ENGINE WAS RESTARTED AFTER SEVERAL ATTEMPTS AND TAXIED OFF. MAINTENANCE RESPONSE, FUEL SET UP PROCEDURE WAS PERFORMED IN ACCORDANCE WITH TCM SID97-3E AND GROUND SDR 2009F00005Engine · power lossAFTER APPROX 30 MINUTES OF IFR FLIGHT AT 8000 FT WITH NO OUTSIDE EVIDENCE OF AIRFRAME ICING THE PILOT NOTICED LT ENG LOOSING FUEL PRESSURE AND MANIFOLD PRESSURE, PILOT FOLLOWED ENG FAILURE CHECKLIST AND ALTERNATE AIR, BOOST PUMPS AND FULL MIXTURE WERE APPLIED SDR CA090319012Engine · making metalFERRIOUS METAL WAS FOUND IN FILTER, THE TEARDOWN FOUND.SDR CA081125004Engine · making metal(CAN) LOSS OF OIL PRESSURE DURING FLIGHT. PRECAUTIONARY LANDING ON NEARBY LAKE. INSP REVEALED HEAVY METAL CONTAMINATION IN OIL SCREEN, POSSIBLY CRANKSHAFT BEARING.SDR 2008FA0000738Engine · making metalAFTER TAKEOFF, OVERSPEED WARNING LIGHT ILLUMINATED. RPM REDUCTION USING PROP GOVERNOR CONTROL NOT SUCCESSFUL & USED THROTTLE CONTROL TO REDUCE ENGINE RPM. LANDED WITHOUT INCIDENT. REPAIR STATION INSPECTED & DUPLICATED PROBLEM ON GROUND RUN. NO DISCREPANCIES EXSDR 2008FA0000635Engine · power lossAC WAS NOT OPERATING UNDER PART 135, IT WAS UNDER PART 91 FLIGHT WHEN INCIDENT OCCURRED. PILOT STATEMENT "ENROUTE, AS WE CRESTED THE
MOUNTAINS, THE ENGINE STARTED SPUTTERING, AND RPMS WERE DROPPING. APPLIED CARB HEAT, TRIED SWITCHING BETWEEN FUEL TANKS, MAGNETSDR 2008FA0000652Engine · stoppedENGINE QUIT IN MID-AIR. ENGINE HAD 1195.0 HOURS SINCE MAJOR OVERHAUL. (K)SDR I5H2008F00001Engine · making metalJUST AFTER TAKEOFF, AT APPROXIMATELY 1700, THE CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENGINE. THE CAPTAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED ASDR I5HA0824006Engine · damagedJUST AFTER TAKEOFF AT APPROXIMATELY 1700 (L) CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENG. THE CAPTAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED AN EMSDR 2008FA0000371Engine · vapor lockAC WAS BEING FLOWN ON RT FUEL TANK. AFTER RUNNING TANK DRY, PILOT SELECTED RT FUEL TANK AND MOMENTS LATER THE ENG STOPPED PRODUCING POWER AND MADE AN EMERGENCY LANDING. AC FUEL SYS WAS INSPECTED FOR CONTAMINATES AND FAILURES, NONE WERE FOUND. POSSIBLE CAUSE ISDR 2008F00016Engine · failedAIRCRAFT EXPERIENCED AN ENGINE FAILURE. ATTEMPTS TO RESTART ENGINE FAILED AND A SAFE LANDING WAS ACCOMPLISHED. CAUSE OF FAILURE REMAINS UNKNOWN AT THIS TIME. (K)SDR 2008FA0000241Engine · power lossAFTER TAKEOFF AND PULLING LANDING GEAR UP, LT ENGINE POWER REDUCTION TO 75 PERCENT FOR ABOUT ONE MINUTE AND POWER WAS RESTORED. THIS SAME ISSUE HAS BEEN INDUCTED TWICE IN LESS THAN 24 HRS. THERE IS NO FEDAC WARNINGS SHOWN ON SYS. A REPORT HAS BEEN SENT TO MFG.SDR 2008FA0000199Case · crackedREMOVED THIS ENGINE FROM THE RT POSITION FOR SHIPMENT BACK TO RAM AC DUE TO A DAMAGED CASE. DAMAGE APPEARS TO BE CAUSED BY A FAILED CONNECTING ROD THAT BROKE APART AND PUNCTURED (2) LARGE HOLES IN THE CRANKCASE. BRIEF ENGINE HISTORY: 347 HOURS PRIOR TO THE FSDR 2008FA0000211Duct · crackedRT TURBO TRANSITION DUCT CRACKED. (NOTE: THIS IS THE SECOND TIME WE HAVE SEEN THIS)SDR CA080314013Engine · making metal(CAN) ON FINAL APPROACH INTO AIRPORT THE RT ENGINE MANIFOLD PRESSURE STARTED CHANGING. THE PILOT THEN NOTICED THAT THE RT OIL PRESSURE HAD DROPPED TO THE RED LINE. THE RT PROP WAS FEATHERED AND THE ENGINE WAS SHUTDOWN. SMALL BITS OF METAL WERE FOUND UNDER THE SDR CA080304007Engine · making metal(CAN) DURING A SCHEDULED INSP, LARGE QUANTITIES OF FERROUS PARTICLES WERE DISCOVERED IN THE PAPER ELEMENT OF THE ENGINE OIL FILTER. LARGER PIECES WERE ALSO DISCOVERED IN THE OIL SUCTION SCREEN FINGER. THE AC IS GROUNDED PENDING REPLACEMENT OF THE AFFECTED ENGISDR FFKA020108125Drive Shaft · shearedPILOT REPORTED A LOSS OF ENGINE RPM CONTROL (RUNAWAY PROP). AFTER REPLACING THE PROPELLER GOVERNOR AND THE PROPELLER THERE WAS STILL NO PROP CONTROL. MAINTENANCE FURTHER INVESTIGATED THE PROBLEM AND FOUND THE PROPELLER GOVERNOR DRIVE SHAFT GEAR SHEARED. AFTSDR 2008FA0000417Engine · seizedAIRCRAFT LANDED WITH LT ENGINE SHUTDOWN (IN-FLIGHT SHUTDOWN). INITIAL INVESTIGATION REVEALED THAT THE ENGINE WAS SEIZED. OIL SCREEN WAS REMOVED AND FOUND HEAVILY CONTAMINATED WITH METAL PARTICLES. ENGINE OIL SUMP DRAIN PLUG WAS REMOVED. LARGE METAL PARTICLESSDR CA071207004Engine · power loss(CAN) AFTER 45 MINUTE FLIGHT BOTH ENGINES BEGAN LOSING PWR WITH NO FUEL FLOW INDICATIONS OR FUEL PRESSURE INDICATIONS. ENGINES WOULD ONLY DEVELOP IDLE PWR. PILOT MADE A FORCED LANDING WITH MINOR INJURIES. FOLLOW UP INVESTIGATION TO FOLLOW. FOLLOW UP REPORT ON SDR 135632112407Engine · failedON TAKEOFF FROM MAZ, AT 2400 FEET AND CLIMBING TO 3500 FEET, PILOT HEARD LOUD BOOM WITH RIGHT ENGINE SHUT DOWN AND PROPELLER FEATHERING. THE PILOT PERFORMED ENGINE FAILURE FLOW CHECK LIST AND RETURNED TO MAZ. PRELIMINARY INSPECTION SHOWS CATASTROPHIC FAILURESDR CA071018001Engine · stalled(CAN) DURING POWER ON STALL THE PROPELLER CAME TO A FULL STOP, THROTTLE WAS AT 1700 RPM AND THE NOSE POINTED UP FOR A STALL CONFIGURATION AND ON POWER APPLICATION THE ENGINE CAME TO A FULL STOP. THE AIRCRAFT WAS THEN POINTED NOSE DOWN, THE PROPELLER STARTED WISDR 2007FA0000886Engine · making metalDURING ROUTINE OIL CHANGE, METAL SHAVINGS WERE FOUND IN OIL FILTER AND SCREEN. SHAVINGS WERE MAGNETIC. THESE ENGINES DO HAVE WEAR ISSUES ON CAM AND LIFTERS. AFTER REMOVING OIL PAN, FOUND CAM BAD AND LIFTER WEAR. OIL ANALYSIS DIDN`T PICK UP LARGER MICRON INSDR 2007FA0000496Stud · chafedDURING BUILD UP OF A NEW ENGINE FOR INSTALLATION, IT IS ROUTINE FOR US TO R&R THE OIL COOLER TO INSTALL THE GASKET WITH SEALANT AND TO INSPECT THE ADAPTER PLATE MOUNTING STUD HEIGHT. ON THIS PARTICULAR ENGINE, ALL OF THE STUDS WERE INSTALLED TOO HIGH, SO THATSDR CA070529003Engine · making metal(CAN) ENGINE REMOVED DUE TO METAL IN OIL SCREEN, TBO 750 HOURS. ENGINE BEING SENT OUT FOR OVERHAUL. (TC NR 20070529003)SDR 2007FA0000524Engine · failedON MAY 11, 2007 AT APPROXIMATELY 1815 EST, 2205Z, A BEECH BE-36-A36 BONANZA, N814JG, S/N E-2622, AT CRUISE HAD A DECREASE IN ENGINE CYLINDER TEMPERATURE, FOLLOWED BY A LOSS OF OIL PRESSURE AND ENGINE POWER WITH SUBSEQUENT ENGINE FAILURE. THE AIRCRAFT MADE AN ESDR EAVA200701117Engine · vibrationAT CRUISE ENGINE DEVELOPED VIBRATION. REQUESTED DESCENT AND TURN TO NEAREST SUITABLE FIELD. REDUCED ENGINE POWER TO IDLE ON DOWNWIND, FELT A JOLT AND SAW RIGHT ENGINE ACCESS PANEL PUSH OUT. FEATHERED AND SECURED RIGHT ENGINE AND LANDED.SDR 2007FA0000444Engine · malfunctionedAIRCRAFT ECU WARNING LIGHT COME ON FREQUENTLY. WE SPOKE WITH THIELERT ABOUT THE PROBLEM AND THEY SAY THAT DURING STEEP BANKS OR YAW THE FUEL PRESSURE CAN BE DIFFERENT BETWEEN THE RAILS ON EACH ENGINE. THE ECU CAN INTERPRET THIS AS A PROBLEM AND TURN ON THE ASDR CA070502009Engine · failed(CAN) NR 2 ENGINE FAILED SEVEN MINUTES PRIOR TO LANDING AT AIRPORT. NR 2 CYLINDER DROPPED DOWN INSIDE THE COWLING AND APPROXIMATELY 2 QUARTS OF OIL WAS LOST. THE ENGINE WAS SECURED WITHIN A FEW SECONDS AND A LANDING WAS SAFELY EXECUTED AT AIRPORT. THE ENGINESSDR 2007FA0000332Snap Ring · mismanufacturedSNAP RING USED TO RETAIN PLATE PN 643629 AND COUNTERWEIGHT PIN 643626-101 WAS BEING INSTALLED IN COUNTERWEIGHT. UPON INSTALLING, THE LAST SNAP RING, IT WAS NOTICED THAT THE SNAP RING DID NOT HAVE ANY RETAINING PROPERTIES. IT LACKED TEMPER TO SPRING BACK AND SDR CA070327008Engine · failed(CAN) ENGINE FAILURE, PROP STOPPED IN FLIGHT. NO EXTERNAL DAMAGE TO ENGINE. SUSPECT CRANKSHAFT FAILURE. (TC NR 20070327008)SDR 2007FA0000226Engine · failedTHIS ENGINE FAILED TO THE TERMINOLOGY OF CATASTROPHIC AT THE NR 1 AND NR 2 CYLINDER CONNECTING ROD LOCATIONS DURING A MAINTENANCE TEST FLIGHT WITHIN TEN MINUTES INTO THAT FLIGHT WITH A MECHANIC ON BOARD MONITORING THE ENGINE INSTRUMENTS. THE OIL PRESSURE SUDDSDR N3B2007F00000Engine · shutdownDURING LANDING (AT DESCISION HEIGHT) LT ENGINE SHUTDOWN CAUSING AIRCRAFT TO LAND WITH A YAW TO THE LT, PUTTING EXCESSIVE LOAD ON RT LANDING GEAR. AFTER LANDING, LT ENGINE WAS RESTARTED AND AIRCRAFT CONTINUED ITS TAXI, WHEN AC TURNED OFF RUNWAY. RT LANDING GESDR 2007FA0000164Engine · making metalUNDER NORMAL CONDITIONS AND UNDER OIL SAMPLE PROGRAM, ENGINE HAS HAD (6) HIGH BAD SAMPLES, HIGH IRON, COPPER AND ALUMINUM. AC IS A PUBLIC USE AIRCRAFT WITH CUSTOMS AND BORDER PROTECTION, BUT AM REPLACING ENGINE WITH NEW/ OVERHAUL. CONTACTED MFG ABOUT PROBLEMSDR PNSA070107Engine · making metalDURING ROUTINE INSPECTION FOUND METAL IN FILTER. SUSPECT METAL FROM CAM AND LIFTERS. LYCOMING RECOMMENDED ENGINE BE REMOVED AND SENT TO FACTORY FOR WARRANTY. ENGINE OVERHAULED BY LYCOMING 3/10/06. TSO 384.3SDR PNSA070106Engine · making metalDURING ROUTINE INSPECTION FOUND METAL IN FILTER. SUSPECT METAL FROM CAM AND LIFTERS. LYCOMING RECOMMENDED ENGINE BE REMOVED AND SENT TO FACTORY FOR WARRANTY. ENGINE OVERHAULED BY LYCOMING 1/27/06. TSO 813.1
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