Airworthiness Directives; Eurocopter France (Eurocopter) Model SE 3130, SE 313B, SA 3180, SA 318B, and SA 318C Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 1997-11-21 · Effective 1997-12-08 · 62 FR 62239
Document
Document number
97-30603
Federal Register citation
62 FR 62239
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1997-11-21
Effective date
1997-12-08
FAA docket
Docket No. 97-SW-22-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter Model SE 3130, SE 313B, SA 3180, SA 318B, and SA 318C helicopters. This action requires a visual inspection of the main rotor blade reinforcement strips for debonding between the reinforcement strips of the blade; and a visual inspection of the main rotor blade (blade) skin for cracks or corrosion, and replacement of the blade with an airworthy blade if certain debonding or a crack or corrosion is found. This amendment is prompted by an accident in which a blade separated in flight. The actions specified in this AD are intended to detect debonding, cracks, or corrosion in the affected blades and to prevent failure of a blade and subsequent loss of control of the helicopter.