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Airworthiness Directives; Sikorsky Aircraft Corporation Model S-92A Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2005-06-23 · Effective 2005-07-08 · 70 FR 36333

Document

Document number
05-12417
Federal Register citation
70 FR 36333
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Sikorsky
Publication date
2005-06-23
Effective date
2005-07-08
FAA docket
Docket No. FAA-2005-21588

Abstract

This amendment adopts a new airworthiness directive (AD) for the Sikorsky Aircraft Corporation (Sikorsky) Model S-92A helicopters. This action requires replacing a certain part-numbered tail gear box output housing that has 600 or more hours time-in-service (TIS) with an airworthy part. Also, this AD revises the Airworthiness Limitations section of the maintenance manual by reducing the life limit of the tail gear box output housing. This amendment is prompted by the premature failure of the tail gear box output housing during fatigue testing by the manufacturer. The actions specified in this AD are intended to prevent fatigue failure of the tail gear box output housing, loss of tail rotor drive, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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