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.