← FAA Federal Register actions

Airworthiness Directives; Sikorsky Aircraft Corp. Model S76A, B, and C Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1999-09-17 · Effective 1999-10-04 · 64 FR 50442

Document

Document number
99-23959
Federal Register citation
64 FR 50442
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Sikorsky
Publication date
1999-09-17
Effective date
1999-10-04
FAA docket
Docket No. 99-SW-44-AD

Abstract

This amendment adopts a new airworthiness directive (AD) applicable to Sikorsky Aircraft Corporation (Sikorsky) Model S-76A, B, and C helicopters. This action requires conducting a visual inspection to detect disbonding of the attachment angle between the tail gearbox forward fairing (fairing) and the pylon and replacing or repairing the attachment angles as necessary. This amendment is prompted by incidents, two in flight and eight on the ground, of fairing bonding failures. The actions specified in this AD are intended to prevent separation of the fairing, damage to the tail rotor blades, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown