Airworthiness Directives; Beech Model 400, 400A, and MU-300-10 Airplanes
airworthiness · Rule · Final rule. · Published 1996-02-12 · Effective 1996-03-13 · 61 FR 5275
Document
Document number
96-1521
Federal Register citation
61 FR 5275
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1996-02-12
Effective date
1996-03-13
FAA docket
Docket No. 94-NM-162-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Beech Model 400, 400A, and MU-300-10 airplanes, that requires installation of an improved adjustment mechanism on the flightcrew seats and replacement of the existing aluminum seat reinforcement assemblies with steel assemblies. This amendment is prompted by reports of incomplete latching of the existing adjustment mechanism and cracked reinforcement assemblies, which could result in sudden shifting of a flightcrew seat. The actions specified by this AD are intended to prevent such shifting of a flightcrew seat, which could impair the flightcrew's ability to control the airplane.