Regulacje i polityka gospodarcza · 8.09.1995

Airworthiness Directives; Beech Model 400 and 400A Airplanes

This amendment adopts a new airworthiness directive (AD), applicable to certain Beech Model 400 and 400A airplanes, that requires modification of the autopilot and rudder boost interlock. This amendment is prompted by a report indicating that the rudder boost system installed on these airplanes does not operate correctly during deployment of a thrust reverser. The actions specified by this AD are intended to prevent incorrect operation of the rudder boost system during deployment of a thrust reverser and to prevent the autopilot from exceeding certain bank angle limits; these conditions could result in reduced controllability of the airplane.