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Airworthiness Directives; Siam Hiller Holdings, Inc. Model UH-12, UH-12A, UH-12B, UH-12C, UH-12D, UH-12E, UH-12E-L, UH-12L, and UH-12L4 Helicopters

airworthiness · Rule · Final rule. · Published 2000-12-06 · Effective 2001-01-10 · 65 FR 76149

Document

Document number
00-30652
Federal Register citation
65 FR 76149
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2000-12-06
Effective date
2001-01-10
FAA docket
Docket No. 2000-SW-27-AD

Abstract

This amendment adopts a new airworthiness directive (AD), for Siam Hiller Holdings, Inc. (Hiller), formerly Rogerson Hiller Corporation, Model UH-12, UH-12A, UH-12B, UH-12C, UH-12D, UH-12E, UH- 12E-L, UH-12L, and UH-12L4 helicopters, that requires replacing all undrilled-shank bolts at pivoting joints in the control system linkage with drilled-shank bolts and installing castellated nuts and cotter pins. This amendment is prompted by an accident caused by separation of the control system linkage of a Model UH-12E helicopter. The actions specified by this AD are intended to prevent separation of the control system attachments at pivoting points and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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