NTSB investigations · 2
Matched to this aircraft by N200AK and the event date: up to this one’s cancellation.
NTSB ANC07LA048Accident · No injuriesLimited investigationFinal reportTuluksak, AKThe loss of engine power during cruise due to the pilot's failure to refuel the airplane prior to fuel exhaustion. Factors contributing to the accident were the delayed extension of the gear, and the gear being unlocked at touchdown.NTSB ANC92IA001Incident · No injuriesIncident investigationFinal reportFairbanks, AKIncorrect installation of crankshaft counterwweight rollers by the manufacturer during remanufacture of the engine. Factor was the inadequate surveillance of the engine assembly process by the manufacturer.
FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N200AK and the event date: up to this one’s cancellation.
Accident 20070613012519AFcd/Prec Ldg From Cruise · Tuluksak, AK(-23) Enroute from kalskag to bethel aircraft reported a left engine low fuel pressure light. Pilot turned on emergency fuel pump, switched to outboard tank, light extinguished. Pilot diverted to Tuluksak. Two to three minutes later right low fuel pressure…Incident 19911002055499IForced/Precautionary Landing · Fairbanks, AKLeft engine losing power after departure. Smoke and flames. Secured and flames quit. Evacuated on taxiway.Incident 19850626031969ITo Init Climb(1st Pwr Reduct) · Fairbanks, AKRight main would not retract after takeoff. Returned for landing. Found sheared rivet in hook assembly.Incident 19840612032099ITo Aborted (Fixed Wing) · Fairbanks, AKLarge quantity smoke and oil from right engine exhaust on takeoff roll. Apparent failure turbocharger oil seal.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FFS2002F00004Support Bracket · crackedSUPPORT BRACKET FOR NOSE GEAR ACTUATOR CRACKED AT RADIUS OF CUT OUT THAT PROVIDES CLEARANCE FOR POWER PACK ACTUATING ARM. PART REPLACED WITH NEW PART. SUSPECT THIS FAILURE OCCURRED AS A RESULT OF CYCLIC STRESSED IMPOSED.SDR 20001108SH021Camshaft · failedSTEEL WAS FOUND IN BOTH SPIN-ON FILTER AND OIL SUCTION SCREENS. CAMSHAFT SUSPECTED FAILING, AND PROVEN WITH VISUAL INSPECTION AND CHECKING THE LIFT OF ALL OF THE LOBES. NR 1 AND NR 2 LOBES WERE ONLY GIVING HALF THE LIFT FROM THE OTHER LOBES. (X)SDR 20000802SH027Plate · distortedOIL FILTER CONVERER PLATE REMOVED FOR SEAL INSPECTION. SEAL FOUND SOFT AND EXTRUDED. THIS IS THE SECOND SEAL FOUND TO EXHIBIT THIS CONDITION. ENGINE WAS A FACTORY OVERHAUL WITH OVERHAUL DATE OF 3-27-00. (X)SDR 20000731SH004Gasket · failedOIL FILTER CONVERTER PLATE REMOVED FOR SEAL INSPECTION. SEAL FOUND TO BE SOFT AND EXTRUDED. THIS IS THE SECOND SEAL FOUND TO EXHIBIT THIS CONDITION. ENGINE WAS A FACTORY OVERHAUL WITH OVERHAUL DATE OF 3-27-00. (X)SDR 99ZZZX4150Circuit Breaker · failedWHILE ADJUSTING PANEL AND INSTRUMENT LIGHTS BRIGHTER, A LARGE STREAM OF SMOKE CAME FROM THE AVIONICS CIRCUIT BREAKER PANEL AREA. SHUT OFF MASTER AND SMOKE STOPPED. FOUND 'PANEL LIGHT' CIRCUIT BREAKER TRIPPED, WAS THEN DETERMINED THAT IT WAS OKAY TO TURN MAST