Summary
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all Lockheed Model 382 series airplanes. This proposal would require revising the Airplane Flight Manual (AFM) to prohibit positioning the power levers below the flight idle stop, and to provide a statement of the consequences of positioning the power levers below the flight idle stop. The proposed AD is prompted by incidents and accidents involving airplanes equipped with turboprop engines in which the propeller beta was used improperly during flight. The actions specified by the proposed AD are intended to prevent loss of airplane controllability, or engine overspeed and consequent loss of engine power caused by the power levers being positioned below the flight idle stop while the airplane is in flight.