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Airworthiness Directives; Eurocopter France Model EC 155 B and B1 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2004-06-14 · Effective 2004-06-29 · 69 FR 32857

Document

Document number
04-12905
Federal Register citation
69 FR 32857
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter France Model EC 155 B and B1
Publication date
2004-06-14
Effective date
2004-06-29
FAA docket
Docket No. 2004-SW-05-AD

Abstract

This amendment adopts a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model EC 155 B and B1 helicopters. This action requires inspecting each main rotor blade (blade) for a crack in the blade tip cap mounting bracket (tenon), measuring the vertical clearance between each blade assembly and a straight edge at the blade-to-tip cap junction, and replacing the blade if a crack is found or if the measured distance is not within certain specifications. This amendment is prompted by the discovery of a crack in a tenon. This condition, if not detected, could result in loss of the tip cap, which could lead to severe vibration and loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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