← FAA Federal Register actions

Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters

airworthiness · Rule · Final rule. · Published 2000-12-29 · Effective 2001-02-02 · 65 FR 82896

Document

Document number
00-32551
Federal Register citation
65 FR 82896
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Agusta S.p.A. Model A109E
Publication date
2000-12-29
Effective date
2001-02-02
FAA docket
Docket No. 2000-SW-07-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters that currently requires inspecting the exhaust ejector locking system, clamp, and dampers for each engine. The existing AD also requires verifying the torque of the metallic clamps and installing safety wire on the metallic clamps; inspecting and modifying the ejector saddles and the locking metallic clamps; and inspecting the metallic clamps, locking mechanisms, and dampers. This amendment requires modifying the engine exhaust ejectors. This amendment is prompted by the development of a kit to modify the engine exhaust ejectors to provide terminating action from the requirements of the current AD. The actions specified by this AD are intended to prevent loss of the metallic clamp or the engine exhaust ejector, damage to the main or tail rotor system and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown