Airworthiness Directives; Beech Aircraft Corporation Model 1900D Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1995-03-30 · Effective 1995-04-17 · 60 FR 16366
Document
Document number
95-7784
Federal Register citation
60 FR 16366
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Beech
Publication date
1995-03-30
Effective date
1995-04-17
FAA docket
Docket No. 95-CE-15-AD
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-02-17, which was sent previously to known U.S. owners and operators of certain Beech Aircraft Corporation Model 1900D airplanes. This AD requires inspecting (one- time) the elevator trim tab control cables at the top of the vertical stabilizer to ensure that cables (at the left, right, and crossover pulleys) are correctly routed around the pulleys, within the cable guide pins, and are not contacting any structure; and replacing any cable that is incorrectly routed or chafed. The actions specified by this AD are intended to prevent in-flight separation of the elevator trim tab control cable caused by misrouting, which could result in loss of control of the airplane.