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Airworthiness Directives; Eurocopter France Model SA-365N, SA- 365N1, and SA-366G1 Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 1998-02-06 · Effective 1998-02-23 · 63 FR 6069

Document

Document number
98-2969
Federal Register citation
63 FR 6069
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-02-06
Effective date
1998-02-23
FAA docket
Docket No. 97-SW-23-AD

Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 97-15-15, which was sent previously to all known U.S. owners and operators of Eurocopter France Model SA-365N, SA-365N1, and SA-366G1 helicopters by individual letters. This AD requires an inspection of the main gearbox magnetic plug (magnetic plug) and the main gearbox oil filter (oil filter) for ferrous chips; vibration measurements, if necessary; and replacement of the main gearbox if a specified quantity of ferrous chips are discovered, or if abnormal vibrations are identified at a certain frequency. This amendment is prompted by two recent reports of cracks found in planetary gear shafts (gear shafts) in main gearboxes that have not been modified in accordance with MOD 077244. The actions specified by this AD are intended to detect cracks in the gear shaft which could lead to failure of the gear shaft, failure of the transmission, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
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