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Airworthiness Directives; Bell Helicopter Textron, Inc. Model 412, 412EP, and 412CF Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2000-09-13 · Effective 2000-09-28 · 65 FR 55175

Document

Document number
00-23208
Federal Register citation
65 FR 55175
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2000-09-13
Effective date
2000-09-28
FAA docket
Docket No. 2000-SW-29-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron, Inc. (BHTI) Model 412, 412EP, and 412CF helicopters. This AD requires inspecting the upper left-hand cap angle (cap angle) and adjacent structure for a crack and, before further flight, replacing any cracked cap angle and repairing any crack in the adjacent structure. This AD is prompted by a report of a fatigue crack in a tailboom attachment cap angle. The actions specified in this AD are intended to prevent failure of a cap angle, loss of the tailboom, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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