Beech B36TC — registry & accident history
Compiled from FAA & NTSB records · as of Jul 23, 2026
There are 309 Beech B36TC airframes on record (built 1981–2001), 225 currently registered. 15 have one or more NTSB accident records (15 records total, 8 with a fatal highest-injury classification). Data as of Jul 23, 2026.
Recent Beech B36TC accidents
The pilot’s continued flight into moderate to severe icing conditions, including supercooled large droplets, over mountainous terrain, which resulted in a loss of control and impact with terrain. Contributing to the accident was the National Weather Service forecast that underestimated the area and intensity of the icing conditions and the lack of Alaska-specific icing graphics readily accessible to the pilot for preflight planning.
The total loss of engine power due to the improper installation of the No. 4 connecting rod bolt nut during a recent overhaul.
The pilot’s likely activation of the auxiliary fuel pump to “high” for undetermined reasons during takeoff, which resulted in total loss of engine power due to an excessively rich fuel-to-air mixture. Also causal was the pilot’s exceedance of the airplane’s critical angle of attack while returning to the airport following the loss of engine power.
The pilots’ failure to abort the takeoff, which resulted in a collision with a fence at the end of the runway. Contributing to the accident was the airplane being at or over the maximum gross takeoff weight and the inappropriate elevator trim tab setting.
A lack of climb performance after takeoff for reasons that could not be determined based on the available information.
The loss of engine power due to a torn intercooler hose that resulted in an overly rich fuel mixture, which, when combined with the pilot's activation of the auxiliary fuel pump, flooded the engine.
A total loss of engine power during initial climbout for reasons that could not be determined because postaccident examination and testing of the engine did not reveal any mechanical anomalies that would have precluded normal operation.
The pilot’s continued flight into known light-to-moderate icing conditions over mountainous terrain. Contributing to the accident was the loss of engine power due to induction icing.
