Airworthiness Directives; Eurocopter France Model AS355N Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2000-03-16 · Effective 2000-03-31 · 65 FR 14209
Document
Document number
00-6035
Federal Register citation
65 FR 14209
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Eurocopter France Model AS355N
Publication date
2000-03-16
Effective date
2000-03-31
FAA docket
Docket No. 99-SW-87-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Eurocopter France Model AS355N helicopters. This action requires inspecting the: 4 engine exhaust pipe ejector attachment lugs (lugs) for cracks; starter-generator (S-G) shaft for radial play; S-G attachment flange for cracks; and S-G attachment half- clamps for cracks. This amendment is prompted by 9 reports of S-G damage; 3 reports of the discovery of cracks in the lugs; and 1 report of an in-flight loss of the exhaust pipe ejector. The actions specified in this AD are intended to prevent separation of an engine exhaust pipe ejector from the helicopter, which could result in a tail rotor strike and subsequent loss of control of the helicopter.