JASC 8100

Service difficulty reports · 20

Reports filed under 8100 · Exhaust Turbine System (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 = '8100'
  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.

SDR N3XR2018121700305Valve · failedDURING CLIMB TO 8,000 FEET POWER DECREASED , UN-COMMANDED, FROM 92% TO 70%. TROUBLESHOOTING REVEALED THE ELECTRIC CHANGE OVER VALVE, P/N-E4A-41-300-801 WAS DEFECTIVE. THAT PART WAS REPLACED AND ALL OPERATIONAL CHECKS SHOWED PROPER OPERATION.Dec 14, 2018 · N305ER · Diamon DA42NGSDR N3XR2018121700309Valve · failedON TAKEOFF ROLL, THE POWER WAS LOW. THE TAKE OFF WAS ABORTED. THE ELECTRIC CHANGE OVER VALVE, P/N-E4A-41-300-801, WAS REPLACED AND ALL GROUND PERFORMANCE TESTS INDICATED NORMALLY.Dec 12, 2018 · N309ER · Diamon DA42NGSDR CA180907011Clamp · cracked(CAN) DURING ANNUAL INSPECTION AS WELL AS IN CONJUNCTION WITH AD 2000-01-16, THE V-BAND CLAMP THAT ATTACHES THE WASTEGATE EXHAUST ELBOW TO THE EXHAUST HEADER ASSY WAS FOUND CRACKED. (TC# 20180907011)Sep 7, 2018 · Cessna 340ASDR 7UVR201710130001Shaft · shearedDURING A POWER ON STALL, THE PILOTS HAD A PARTIAL POWER LOSS. ENGINE WAS AT 65 - 70 PERCENT AND WHEN THE POWER WAS INTRODUCED, THE LEFT ENGINE WENT TO 45 PERCENT WHILE THE RIGHT ENGINE WAS AT 100 PERCENT. BROUGHT THE POWER BACK AND ADVANCED THE POWER AGAIN Oct 13, 2017 · N131TS · Diamon DA42NGSDR CA090506006Clamp · failed(CAN) TURBO TURBINE FLANGE EXHAUST V-BAND CLAMP FAILED AT T-BOLT CLAMPING SUPPORT. (CLAMP FAILED) FOUND ON WALKAROUND - PREFLIGHT INSPECTION A/C TTSN 2537.2 CLAMP SUSPECTED TTSN 2537.2Apr 24, 2009 · Cessna T206HSDR 2006FA0000469Turbocharger · leakingOIL LEAKING OUT FROM JOINT IN CENTER OF TURBO. FIRST RUN ON OVERHAULED UNIT JUST INSTALLED ON AIRCRAFT. (K)Apr 26, 2006 · N4773P · Cessna P210NSDR 2006FA0000354Turbocharger · weakTURBO CHARGER WOULD NOT MAKE ENOUGH BOOST. (K)Feb 28, 2006SDR CA040416002Support · cracked(CAN) TURBOCHARGER SUPPORT MOUNT FOUND CRACKED ON LOWER LT TUBE.Apr 16, 2004 · Piper PA31350SDR 20000908SH004Clamp · strippedCLAMP AND NUT THREADS SEPARATED CAUSING CLAMP TO SPRING OPEN. THUS, HIGH PRESSURE TURBO AIR LEAKED OVERBOARD CAUSING MANIFOLD PRESSURE TO DROP TO 25 POUNDS (NATURALLY ASPIRATED). (X)Sep 8, 2000 · N84859 · Piper PA31350SDR 20001013SH026Lanyard · missingLANYARD AND ALL ATTACHING HARDWARE FOUND MISSING AND NO SIGN OF EVER BEING INSTALLED DURING FIRST ANNUAL INSPECTION. SUBMITTER STATED THIS DEFECT COULD CAUSE AN IN-FLIGHT FIRE. (X)Aug 9, 2000 · N206VW · Cessna T206HSDR 20000817SH015Link · brokenDURING 25-HOUR INSPECTION, FOUND BROKEN LINK. (X)Aug 8, 2000 · N678TB · Socata TB21SDR 20000817SH014Link · brokenLINK FOUND BROKEN; ANOTHER LINK FOUND BROKEN ON ANOTHER AIRCRAFT. (X)Aug 8, 2000 · N678TB · Socata TB21SDR 20000811SH014Tank · crackedFOUND WELD AT TURBO BEND OF OIL DRAIN TANK CRACKED. UPON REMOVAL, TUBE CAME OUT OF TANK. LOOKING AT WELD, IT APPEARED TO BE A BAD WELD. SUBMITTER STATED THAT HAD THIS GONE UNDETECTED, IT COULD HAVE BEEN A DISASTER. (X)Jul 31, 2000 · N159DM · Socata TB21SDR CA000824025Mount Bracket · broken(CAN) PILOT NOTED SLIGHT ENGINE VIBRATION, ENGINE PARAMETERS NORMAL .INVESTIGATION REVEALED EXHAUST SUPPORT MOUNT P/N 1250255-7 BROKEN, ALSO DISCOVERED MUFFLER (P/N 1250251-13) HEAT SHIELD MOUNT CRACKED AT WELD. EXHAUST SUPPORT MOUNT AND MUFFLER REPLACED, VIJul 25, 2000 · Cessna U206GSDR 20000829SH011Duct · crackedPILOT REPORTED THOTTLE SPLIT AND UNABLE TO OBTAIN RATED POWER ON LEFT ENGINE. INSPECTION OF LEFT ENGINE REVEALED EXHAUST V-DUCT ASSY AT TURBOCHARGER CRACKED. THIS PART WAS INSTALLED NEW AS A COMPONENT OF A FACTORY RE-MANUFACTURED ENGINE. TOTAL TIME SINCE INJul 14, 2000 · N8063L · Piper PA34220TSDR 20000622SH040Rotor · brokenENGINE TURBO SCAVENGING PUMP FAILED. THIS ALLOWED THE ENGINE TO PUMP ALL THE ENGINE OIL OVERBOARD THROUGH THE TURBO. EMERGENCY OFF AIRPORT LANDING CAUSED SUBSTANTIAL DAMAGE TO AIRCRAFT. (X)May 31, 2000 · N738FN · Cessna TR182SDR 20000609SH027Controller · defectiveON POST-FLIGHT INSPECTION, PILOT NOTICED OIL ON UNDER SIDE OF ENGINE COWLING AND NOTIFIED MAINTENANCE PERSONNEL. FURTHER INVESTIGATION REVEALED OIL DRIPPING FROM INDUCTION HOUSING DRAIN AND WAS DETERMINED TO BE COMING FROM THE SENSE LINE OUT OF THE DIFFERENTIMay 24, 2000 · N3582P · Piper PA31350SDR 20000531SH014Clamp · brokenTURBO CLAMP THAT ATTACHES EXHAUST PIPE TO TURBO BROKE. CLAMP WAS SAFTIED AROUND BOLT. BREAK OCCURRED SOMEWHERE ON CLAMP. POSSIBLE SEPARATION WHERE SPOT-WELD HOLDS BOLT IN PLACE. (X)May 2, 2000 · N231BT · Mooney M20KSDR CA990907018Mount · broken(CAN) TURBO MOUNT BROKEN.Aug 19, 1999 · Piper PA31SDR 95ZZZX3212Turbonormalizing · faultyDECREASED AIRCRAFT PERFORMANCE NOTED FOLLOWING INSTALLATION OF TURBO-NORMALIZING STC NR SA 5223NM. INVESTIGATION FOUND TURBO FLITE SYSTEM WEIGHT DATA TO BE INCORRECT. USING CORRECTED DATA STILL DOES NOT APPEAR CORRECT PER ACTUAL WEIGHT DATA FROM AIRCRAFT.May 15, 1995 · N16PA · Beech F33A
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