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Airworthiness Directives; Raytheon (Beech) Model 400A, 400T (Military T-1A), and 400T (Military TX) Series Airplanes

airworthiness · Rule · Final rule. · Published 1996-12-20 · Effective 1997-01-24 · 61 FR 67195

Document

Document number
96-31114
Federal Register citation
61 FR 67195
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1996-12-20
Effective date
1997-01-24
FAA docket
Docket No. 96-NM-158-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Raytheon (Beech) Model 400A and 400T series airplanes, that currently requires an inspection of certain flap roller retention components to detect discrepant or missing parts; replacement of those parts; and installation of new washers on the roller attach bolts. This amendment requires the replacement of certain previously- installed washers with new and stronger washers. This amendment also expands the applicability of the rule to include additional airplanes. This amendment is prompted by reports indicating that some locking tab washers on the roller attach bolt could fail, due to the absence of an inner tang. The actions specified by this AD are intended to prevent the loss of roller attach nuts and the flap roller, which could result in the loss of a flap when the airplane is subject to load limit conditions, and consequently lead to reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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