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Airworthiness Directives; Sikorsky Aircraft Corporation Model S-76A, S-76B and S-76C Helicopters

airworthiness · Rule · Final rule. · Published 2002-10-21 · Effective 2002-11-25 · 67 FR 64519

Document

Document number
02-26590
Federal Register citation
67 FR 64519
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Sikorsky
Publication date
2002-10-21
Effective date
2002-11-25
FAA docket
Docket No. 2001-SW-59-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for the specified Sikorsky Aircraft Corporation (Sikorsky) model helicopters that requires removing and inspecting each main rotor spindle attachment bolt (bolt) to ensure that the correct bolts are installed. This amendment is prompted by the discovery of improper bolts installed on a helicopter during its production. The actions specified by this AD are intended to detect installation of incorrect bolts, which could result in reduced hub or bolt fatigue life, separation of the main rotor blade at the spindle attachment, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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