Airworthiness Directives; Sikorsky Aircraft Corporation Model S-76B and S-76C Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2001-03-06 · Effective 2001-03-21 · 66 FR 13422
Document
Document number
01-5165
Federal Register citation
66 FR 13422
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Sikorsky
Publication date
2001-03-06
Effective date
2001-03-21
FAA docket
Docket No. 2001-SW-01-AD
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2001-03-51, which was sent previously to all known U.S. owners and operators of Sikorsky Aircraft Corporation (Sikorsky) Model S-76B and S-76C helicopters by individual letters. This AD requires, for certain main rotor shafts, initial and recurring fluorescent penetrant inspections. Replacing each affected main rotor shaft (shaft) on or before reaching 1,000 hours time-in- service (TIS) is also required. This amendment is prompted by four reports of shaft cracks. The actions specified by this AD are intended to prevent failure of the shaft and subsequent loss of control of the helicopter.