← FAA Federal Register actions

Airworthiness Directives; Bell Helicopter Textron Canada Model 407 Helicopters

airworthiness · Rule · Final rule. · Published 1998-06-10 · Effective 1998-07-15 · 63 FR 31609

Document

Document number
98-15264
Federal Register citation
63 FR 31609
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada Model 407
Publication date
1998-06-10
Effective date
1998-07-15
FAA docket
Docket No. 98-SW-10-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to Bell Helicopter Textron Canada (BHTC) Model 407 helicopters that requires shimming the tail rotor drive system bearing supports (bearing supports). This amendment is prompted by reports of cracked bearing hangar support arms in the area of the fillet radius. The actions specified by this AD are intended to prevent failure of the bearing supports, which could result in excessive tail rotor drive system vibration, loss of tail rotor drive, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown