# Service difficulty reports: Continental TSIO-360-KB A list on [Continental TSIO-360-KB](https://openairdocs.org/engine/continental-tsio-360-kb.md). Newest first. General aviation reporting is voluntary. Page 1 of 2 · 54 reports - [SDR 2024FA0000239](https://openairdocs.org/sdr/2024FA0000239.md): Tire · failed · Mar 15, 2024 · N8048Q · Piper PA34220T · Tire > PILOT REPORTED ON LANDING THAT HE FELT THE AIRCRAFT YAWING TO THE RIGHT AND REALIZED HE HAD A FLAT TIRE. AIRPORT USED A SET OF DOLLIES TO MOVE THE AIRCRAFT BACK TO WINGS OF HOPE RAMP AREA. BOTH MAIN TIRES AND TUBES WERE REPLACED WITH NEW. WHEEL WAS DISASSEMBLE - [SDR 2021FA0000101](https://openairdocs.org/sdr/2021FA0000101.md): Rod End · sheared · Apr 12, 2021 · N8350Z · Piper PA34220T · Landing Gear Door Retract Section > FAILURE OF THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY, CAUSING A NOSE LANDING GEAR COLLAPSE, AND A DUAL ENGINE PROPELLER STRIKE. THE NOSE GEAR DOWN-LOCK LINK ASSEMBLY BENT, AND THEN SHEARED AT THE ADJUSTABLE ROD END. - [SDR YBBA201908280001](https://openairdocs.org/sdr/YBBA201908280001.md): Warning Light · inoperative · Aug 27, 2019 · N25460 · Piper PA34220T · Landing Gear Position and Warning > PIC REPORTS NOSE GEAR INDICATION INOP DURING GEAR DOWN CYCLE, CYCLED GEAR 3 TIMES AND CONFIRMED GEAR DOWN WITH ATC ACKNOWLEDGEMENT DURING FLY BY, AFTER CYCLING GEAR ALL THREE INDICATIONS WERE PRESENT. - [SDR 2013FA0000094](https://openairdocs.org/sdr/2013FA0000094.md): Cap · departed · Feb 2, 2013 · N8455Z · Piper PA34220T · Wing Main, Frame Structure > FUEL CAP ON THE WING INCORRECTLY INSTALLED AFTER REFUELING, FUEL CAP EVENTUALLY DEPARTED THE ACFT INFLIGHT. CAP WAS CHECKED DURING THE PREFLIGHT, AFTER REFUELING, AND THE CAP PLACEMENT WAS CLEARLY FLUSH WITH THE WING, AND THE "HANDLE" WAS FOLDED DOWN AND FLUS - [SDR 2007FA0000942](https://openairdocs.org/sdr/2007FA0000942.md): Landing Gear · collapsed · Sep 21, 2007 · N84643 · Piper PA34220T · Nose/Tail Landing Gear > AIRCRAFT TAXIED TO RUNWAY AFTER LOADING CARGO. AFTER NORMAL RUNUP, THE PILOT TAXIED ONTO THE RUNWAY AND STOPPED. THE PILOT ADVANCED THROTTLES AND RELEASED BRAKES, AFTER RELEASING BRAKE, THE NOSE GEAR COLLAPSED. AIRCRAFT WAS RECOVERED AND TOWED OFF RUNWAY TO - [SDR 2007FA0000076](https://openairdocs.org/sdr/2007FA0000076.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED - [SDR 2007FA0000077](https://openairdocs.org/sdr/2007FA0000077.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATORS, IN IMC SIMULTANEOUSLY. 1 PIECE COUPLING WITH A RUBBER LORD BUSHING BONDED/INTERFERENCE FIT SLIPPED, CAUSING THE ALTERNATORS FAILURES. PILOTS LOST ELECTRICAL AND DESCENDED THROUGH ICE, UNABLE TO SHED - [SDR 2007FA0000085](https://openairdocs.org/sdr/2007FA0000085.md): Coupling · failed · Jan 17, 2007 · N321AK · Piper PA34220T · DC Generator-Alternator > ALTERNATOR DRIVE COUPLING FAILED ON LT AND RT ALTERNATOR, IN IMC SIMULTANEOUSLY. COUPLING FAILURE RESULTED IN TOTAL ELECTRICAL FAILURE, RT ENGINE. - [SDR 2006FA0000571](https://openairdocs.org/sdr/2006FA0000571.md): Points · failed · May 31, 2006 · N8456H · Piper PA34220T · Ignition System > THE POINTS WHICH ONLY HAD A TOTAL OF 9.3 HR, HAD THE PLASTIC PORTION WHICH RIDES THE CAM, MELT ON THE METAL OF THE POINTS WHICH REDUCED THE GAP TO CAUSE MISFIREING. CAPACITOR CHECKED GOOD AND WAS NOT REPLACED ON THE 500 HR INSP. AFTER A NEW POINT SET WERE IN - [SDR CA070207006](https://openairdocs.org/sdr/CA070207006.md): Trunnion · failed · Jan 20, 2006 · Piper PA34220T · Fuselage, Landing Gear Attach Fittings > (CAN) NOSE GEAR TRUNNION DAMAGED AND REPAIRED. (TC NR 20070207006) - [SDR AU510001779](https://openairdocs.org/sdr/AU510001779.md): Alternator · faulty · Dec 12, 2005 · Piper PA34220T · DC Generator-Alternator > LT AND RT ALTERNATORS REMOVED FROM AIRCRAFT FOR INTERNAL INSPECTION FOLLOWING PURCHASE OF AIRCRAFT. BOTH ALTERNATORS WERE FOUND TO CONTAIN NUMEROUS DEFECTS. ALTERNATORS HAD ONLY 12 HOURS TSO. ALTERNATORS WERE `KELLY AEROSPACE` ITEMS. - [SDR 2005FA0001192](https://openairdocs.org/sdr/2005FA0001192.md): Adapter · cracked · Aug 19, 2005 · N321AK · Piper PA34220T · Turbine Engine Accessory Drive > STARTER ASSEMBLY BOLT HOLE FLANGE CRACKED AT THE 10 O'CLOCK BOLT POSITION. MANUFACTURER DESIGN FLAW. ONGOING NUMEROUS REOCCURENCES WITH THESE ADAPTER ASSEMBLY ACCESSORY DRIVE HOUSINGS, LEFT SIDE ONLY, IN FLEET AIRCRAFT. - [SDR 2005FA0001193](https://openairdocs.org/sdr/2005FA0001193.md): Adapter · cracked · Aug 19, 2005 · N321AK · Piper PA34220T · Turbine Engine Accessory Drive > STARTER ASSEMBLY BOLT HOLE FLANGE CRACKED AT THE 10 O'CLOCK BOLT POSITION. MANUFACTURER DESIGN FLAW. ONGOING NUMEROUS REOCCURENCES WITH THESE ADAPTER ASSEMBLY ACCESSORY DRIVE HOUSINGS, LEFT SIDE ONLY, IN FLEET AIRCRAFT. - [SDR 2005FA0000670](https://openairdocs.org/sdr/2005FA0000670.md): Gear · broken · Apr 26, 2005 · N92732 · Piper PA12 · Turbine Engine Oil System > ENGINE LOST POWER FOR UNKNOWN REASONS. ENGINE WAS DISASSEMBLED AND INSPECTED. INVESTIGATION FOUND BROKEN DRIVE DOGS ON THE OIL PUMP GEAR, AS WELL AS GEAR TEETH ON THE CRANKSHAFT GEAR AND OUTSIDE DIAMETER OF THE CAM GEAR. THE REASON FOR THE FAILURE OF THE OI - [SDR AUS20030654](https://openairdocs.org/sdr/AUS20030654.md): Washer · wrong part · Jun 30, 2003 · Piper PA34220T · Main Landing Gear Attach Section > (AUS) LT AND RT MAIN LANDING GEAR FORWARD TRUNNION WASHERS INCORRECT PARTS. CORRECT WASHERS HAVE A CHAMFER ON THE INTERNAL BORE WHICH ALLOWS CLEARANCE FOR THE TRUNNION SHOULDER RADIUS. THE WASHERS FITTED DID NOT HAVE THE CHAMFER. IN THIS CASE THE DAMAGE WAS M - [SDR NCL2003F00000](https://openairdocs.org/sdr/NCL2003F00000.md): Rib · cracked · Jan 10, 2003 · N2900S · Piper PA34200T · Wing, Rib/Bulkhead > THE LT AND RT FORWARD TRUNNION FITTING ASSEMBLIES WERE REMOVED TO REPLACE THE BEARINGS. WHILE THE FITTINGS WERE REMOVED THE TECH NOTICED THAT BOTH LT AND RT RIBS WERE CRACKED AT THE FORWARD OUTBOARD FLANGES OF THE RIBS. THIS FLANGE IS UNDER THE TRUNNION FITT - [SDR AUS20021279](https://openairdocs.org/sdr/AUS20021279.md): Lever · binding · Oct 15, 2002 · Piper PA34220T · Trailing Edge Flap Control System > (AUS) FLAP LEVER FOULING ON ENGINE CONTROL FRICTION LEVER. - [SDR AUS20021102](https://openairdocs.org/sdr/AUS20021102.md): Tube · corroded · Sep 27, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR UP' HYDRAULIC PIPE CORRODED. - [SDR AUS20021103](https://openairdocs.org/sdr/AUS20021103.md): Tube · corroded · Sep 27, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR DOWN' PIPE CORRODED. - [SDR AUS20021104](https://openairdocs.org/sdr/AUS20021104.md): Tube · corroded · Sep 9, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR DOWN' HYDRAULIC PIPE CORRODED. - [SDR AUS20021105](https://openairdocs.org/sdr/AUS20021105.md): Tube · corroded · Sep 9, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR UP' HYDRAULIC PIPE CORRODED. - [SDR AUS20020950](https://openairdocs.org/sdr/AUS20020950.md): Plate · cracked · Aug 24, 2002 · Piper PA34220T · Propeller Feathering/Reversing > (AUS) PROPELLER PITCH LEVER FEATHER STOP PLATE CRACKED PREVENTING OPERATION OF PITCH LEVER. - [SDR AUS20020951](https://openairdocs.org/sdr/AUS20020951.md): Plate · cracked · Aug 24, 2002 · Piper PA34220T · Propeller Feathering/Reversing > (AUS) PROPELLER PITCH CONTROL LEVER FEATHER STOP GATE PLATE CRACKED. - [SDR AUS20020823](https://openairdocs.org/sdr/AUS20020823.md): Shaft · scored · Aug 7, 2002 · Piper PA34220T · Reciprocating Engine Cylinder Section > (AUS) ROCKER SHAFT AND BUSH SCORED. SUSPECT CAUSED BY LACK OF LUBRICATION. - [SDR AUS20020855](https://openairdocs.org/sdr/AUS20020855.md): Exhaust Valve · worn · Aug 7, 2002 · Piper PA34220T · Reciprocating Engine Cylinder Section > (AUS) NO3 CYLINDER EXHAUST VALVE TIP WORN EXCESSIVELY. CORRESPONDINGROCKER DAMAGED ON CONTACT AREA. EXHAUST VALVES PNO 646460 AND INLET VALVES PNO 646459 IN OTHER CYLINDERS ALSO SHOWING SIGNS OFPITTING ON THE TIPS. - [SDR AUS20020948](https://openairdocs.org/sdr/AUS20020948.md): Tube · corroded · Aug 7, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR UP' HYDRAULIC TUBE CORRODED AND LEAKING THROUGH CORROSION HOLE LOCATED UNDER P' CLAMP. - [SDR AUS20020949](https://openairdocs.org/sdr/AUS20020949.md): Tube · corroded · Aug 7, 2002 · Piper PA34220T · Landing Gear Retraction/Extension System > (AUS) LANDING GEAR HYDRAULIC PIPE CORRODED IN AREA UNDER P' CLAMP. - [SDR AUS20020822](https://openairdocs.org/sdr/AUS20020822.md): Piston Pin · damaged · Aug 2, 2002 · Piper PA34220T · Reciprocating Engine Cylinder Section > (AUS) NO1 ENGINE PISTON PINS (6OFF) HAD SEVERE DAMAGE TO THE ALUMINIUMEND CAPS. THE END CAPS HAD MIGRATED OUTWARDS AND WERE RUBBING ONTHE CYLINDER WALLS. METAL CONTAMINATION OF ENGINE OIL SYSTEM. - [SDR CA020403004](https://openairdocs.org/sdr/CA020403004.md): Pump · leaking · Mar 20, 2002 · Piper PA34220T · Heating System > (CAN) WHILE CARRYING AT AD 2001-17-13 (JANAERO SOLENOID/SHUTOFF VALVE LEAK CHECK) THE HEATER FUEL PUMP WAS FOUND TO BE LEAKING OUT OF THE POWER WIRE GROMMET. THIS PUMP IS UNDER THE CENTRE FLOOR BOARD IN THE CABIN AND ALTHOUGH THERE IS A DRAIN UNDER THE PUMP FU - [SDR CA041213001](https://openairdocs.org/sdr/CA041213001.md): Skin · mismarked · Jan 11, 2002 · Piper PA34200T · Fuselage Main, Plate/Skin > (CAN) SKIN ASSY P/N 7861901 MATERIAL AND SKIN THICKNESS IDENTIFIED IN PIPER SENECA SERVICE MANUAL STRUCTURES SECTION FIG.4-9 NR 5 AS 2024-T3 0.032 - [SDR 2001FA0000583](https://openairdocs.org/sdr/2001FA0000583.md): Wire · missing · Oct 5, 2001 · N2022 · Ryan ST3KR · DC Generator-Alternator > NEW EXCHANGE ALTERNATOR SUPPLIED. ALTERNATOR OUTPUT OK. PANEL INOPERATIVE LIGHT STAYS ILLUMINATED. INSPECTION OF ALTERNATOR REVEALED MISSING LEAD WIRE FROM STATOR TO STATOR. ALT LIGHT TERMINAL ON ALTERNATOR. ALTERNATOR REQUIRES ADDITIONAL LEAD WIRE FOR A - [SDR CA010831004](https://openairdocs.org/sdr/CA010831004.md): Fastener · missing · Aug 21, 2001 · Piper PA34220T · Engine Mount Section > (CAN) 1. FITTING, ASSY OUTBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON OUTBOARD LOWER SIDE FITTING (P/N: 37437-01).2. FITTING, ASSY INBOARD LOWER ENGINE MOUNT. ONE MISSING FASTENER ON INBOARD LOWER SIDE OF FITTING (P/N: 37442-01) - [SDR 20001017SH008](https://openairdocs.org/sdr/20001017SH008.md): Controller · loose · Sep 20, 2000 · N4128X · Piper PA34220T · Fuel Control/Reciprocating Engines > EXCESS PLAY IN ARM TO LINKAGE. (X) - [SDR CA000824030](https://openairdocs.org/sdr/CA000824030.md): Ground Wire · broken · Jul 28, 2000 · Piper PA34220T · Landing Gear Actuator > (CAN) THIS AIRCRAFT SUFFERED A PARTIAL GEAR UP LANDING ON JUNE 19, 2000. TEMPORARY REPAIRS WERE MADE AND THE AIRCRAFT WAS FERRIED TO CYEG FOR FURTHER INSPECTION AND REPAIR. NECESSARY REPAIRS WERE MADE. INSPECTION BEFORE FURTHER FLIGHT REVEALED THAT THE STAKO - [SDR 20000829SH011](https://openairdocs.org/sdr/20000829SH011.md): Duct · cracked · Jul 14, 2000 · N8063L · Piper PA34220T · Exhaust Turbine System (Reciprocating) > PILOT 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 IN - [SDR 20000626SH017](https://openairdocs.org/sdr/20000626SH017.md): Fuel Control · failed · May 25, 2000 · N9299E · Piper PA34220T · Fuel Control/Reciprocating Engines > ENGINE DIED ON LANDING ROLL-OUT. AIRCRAFT WAS TAKEN TO MAINTENANCE AND A GROUND RUN PERFORMED. THE FUEL SERVO ON THIS ENGINE WAS RICH AT IDLE AND UNABLE TO ADJUST MIXTURE. SERVO WAS REMOVED FROM ENGINE AND SENT FOR REPLACEMENT. TOTAL TIME ON UNIT WAS 54 HO - [SDR 2000ZZZX603](https://openairdocs.org/sdr/2000ZZZX603.md): Magneto · failed · Feb 17, 2000 · N198PS · Piper PA34220T · Magneto/Distributor > MAGNETO FAILED IN-FLIGHT. FOUND SEVERE DAMAGE TO DISTRIBUTOR FROM ARCING. ARCING APPEARED TO HAVE STARTED BEWEEN COIL AND REAR BEARING HOUSING. SUBMITTER STATED CAUSE UNKNOWN. (X) - [SDR 99ZZZX4653](https://openairdocs.org/sdr/99ZZZX4653.md): Crankshaft · cracked · Nov 24, 1999 · N8375N · Piper PA34220T · Reciprocating Engine Power Section > TRANSIT ACFT LANDED EN ROUTE WITH LT ENGINE SHUT DOWN DUE IN-FLIGHT OIL LEAK. CLEANED ENG AND DID A SHORT RUN AND FOUND OIL COMING FROM PROP SHAFT AREA. REMOVED PROP AND CHECKED O-RING AND IT CHECKED OK. UPON FURTHER INVEST, APPEARED TO BE A CRACK BEHIND PR - [SDR 99ZZZX3583](https://openairdocs.org/sdr/99ZZZX3583.md): Mixture Plate · scored · Aug 18, 1999 · N4167B · Piper PA34220T · Fuel Controlling System > ENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES. THE ENGINE PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED. THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLED. FOUND THE BRASS - [SDR 99ZZZX3584](https://openairdocs.org/sdr/99ZZZX3584.md): Mixture Plate · scored · Aug 18, 1999 · N4178R · Piper PA34220T · Fuel Controlling System > ENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES. THE ENGINE PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED. THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLED. FOUND THE BRASS - [SDR 99ZZZX984](https://openairdocs.org/sdr/99ZZZX984.md): Fuel Servo · mismanufactured · Jan 19, 1999 · N4123C · Piper PA34220T · Fuel Control/Reciprocating Engines > NEW FUEL SERVO INSTALLED ON AIRCRAFT. FUEL LEAK AT FUEL INLET. REMOVED ADAPTER FROM UNIT, O-RING PACKING, PN 951789, WAS MISSING. SUBMITTER STATED THIS WAS A NEW SERVO AND ALL FITTINGS INSTALLED WERE TORQUED. - [SDR 99ZZZX191](https://openairdocs.org/sdr/99ZZZX191.md): Cylinder Head · broken · Nov 9, 1998 · N8170G · Piper PA34220T · Reciprocating Engine Cylinder Section > CONDITION OCCURRED DURING CRUISE CONFIGURATION. PILOT REPORTED LOSS OF MANIFOLD PRESSURE AND DIMINISHED PERFORMANCE ON RT ENGINE. PILOT NOTED OIL COMING FROM ENGINE COWLING AND SHUT ENGINE DOWN. AN INSPECTION REVEALED CYL NR 4 HAD A BROKEN HEAD. THE BREAK - [SDR CA981109012](https://openairdocs.org/sdr/CA981109012.md): Wire · broken · Aug 25, 1998 · Piper PA34220T · Landing Gear System Wiring > (CAN) WHEN GEAR SELECTED DOWN, NO GREEN LIGHT FOR LEFT GEAR AND GEAR UNSAFE LIGHT ON. FLY-BY OK. AIRCRAFT LANDED SAFELY. INSPECTION FOUND A BROKEN WIRE AT THE CONNECTOR FOR THE GEAR SWITCH. - [SDR AU980897](https://openairdocs.org/sdr/AU980897.md): Fuel System · malfunctioned · Jul 23, 1998 · Piper PA34220T · Aircraft Fuel Distribution System > (AUS) LEFT AND RIGHT ENGINES CUT OUT. SUSPECT LEAN CUT-OUT DUE TO FUEL STARVATION. - [SDR 97ZZZX4670](https://openairdocs.org/sdr/97ZZZX4670.md): Through Bolt · broken · Oct 15, 1997 · N3580H · Mooney M20K · Reciprocating Engine Power Section > DURING AN ANNUAL INSPECTION, THE BOTTOM CRANKCASE THROUGH-BOLT LOCATED BETWEEN NR 1 AND NR 3 CYLINDER POSITION WAS FOUND BACKED OUT FROM THE CASE ALMOST TO THE POINT OF FALLING OUT OF ITS MOUNTING HOLE BY APPROXIMATELY 1.1250 INCHES. WHEN BOLT WAS REMOVED, FO - [SDR AU970648](https://openairdocs.org/sdr/AU970648.md): Combustor · cracked · May 26, 1997 · Piper PA34220T · Heating System > (AUS) CABIN HEATER COMBUSTION CAN SPLIT AROUND CIRCUMFERENCE FORAPPROXIMATELY 60MM (2.36IN) - HEATER WAS BEING OVERHAULED TO COMPLY WITH REQUIREMENTS OF AD/AIRCON/9 AMDT5 PARA3 - [SDR CA970407008](https://openairdocs.org/sdr/CA970407008.md): Hub · threads flatened · Mar 27, 1997 · Piper PA34220T · Propeller Hub Section > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION AND HUB THREADS WERE FOUND FLATTENED, DUE TO REMOVING AND INSTALLING THE PROPELLER. - [SDR CA970407009](https://openairdocs.org/sdr/CA970407009.md): Blade · eroded · Mar 27, 1997 · Piper PA34220T · Propeller Blade Section > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION AND THE BLADES WERE FOUND ERODED AND REQUIRED FILING. THE TIP ANGLES WERE OUT OF SPECIFICATIONS AND REQUIRED TWISTING. - [SDR CA970407013](https://openairdocs.org/sdr/CA970407013.md): Blade · eroded · Mar 27, 1997 · Piper PA34220T · Propeller Blade Section > (CAN) INSPECTION FOUND PROPELLER LEADING EDGE ERODED/CORRODED, WHICH REQUIRED FILING. THE BLADE TIP ANGLES WERE OUT OF SPECIFICATIONS AND REQUIRED TWISTING. - [SDR 96ZZZX6146](https://openairdocs.org/sdr/96ZZZX6146.md): Engine · making metal · Dec 4, 1996 · N84643 · Piper PA34220T · Engine (Reciprocating) > DURING 100 HR INSPECTION, THE LEFT ENGINE OIL FILTER WAS FOUND TO BE CONTAMINATED WITH METAL. REMOVAL OF PROPELLER REVEALED METAL CONTAMINATION IN CRANKSHAFT. ENGINE WAS REMOVED FOR OVERHAUL. FURTHER DETAILS WILL BE PROVIDED UPON RECEIPT OF TEAR DOWN REPOR Next page: https://openairdocs.org/engine/continental-tsio-360-kb/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'TSIO360KB' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/continental-tsio-360-kb/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.