Incident Overview

Description
A high-stop (cruise pitch) hang-up of both propellers at low airspeed (while the aircraft was entering a stall maneuvered) caused excessive temperatures in the turbine sections of both engines. When the training crew tried to recover from the simulated landing stall, the engines didn’t respond. The aircraft crash-landed in the desert. Excessive wear of the propeller hub contact switches was due to maintenance instruction deficiencies. Contributing was the crew non-adherence to prescribed procedures. PROBABLE CAUSE: personnel – maintenance,servicing,inspection: inadequate maintenance and inspection powerplant – propeller system: other dual student – improper operation of powerplant & powerplant controls pilot in command – inadequate supervision of flight FACTORS: miscellaneous acts,conditions – failure of two or more engines miscellaneous acts,conditions – excessive temperature miscellaneous acts,conditions – fire in engine miscellaneous acts,conditions – intentional wheels-up partial power loss – partial loss of power – 1 engine complete power loss – complete engine failure/flameout-1 engine
Primary Cause
Inadequate maintenance and inspection of the propeller system, specifically the propeller hub contact switches, combined with improper operation of the powerplant and controls, leading to a cascade of failures.Inadequate maintenance and inspection of the propeller system, specifically the propeller hub contact switches, combined with improper operation of the powerplant and controls, leading to a cascade of failures.Share on: