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Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) Helicopters

airworthiness · Rule · Final rule. · Published 2013-10-31 · Effective 2013-12-05 · 78 FR 65200

Document

Document number
2013-24030
Federal Register citation
78 FR 65200
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada Limited (Bell)
Publication date
2013-10-31
Effective date
2013-12-05
FAA docket
Docket No. FAA-2013-0490

Abstract

We are adopting a new airworthiness directive (AD) for certain Bell Model 407 helicopters. This AD requires installing a placard beneath the NR/NP dual tachometer and revising the limitations section of the rotorcraft flight manual (RFM). This AD was prompted by several incidents of third stage engine turbine wheel failures, which were caused by excessive vibrations at certain engine speeds during steady- state operations. These actions are intended to alert pilots to avoid certain engine speeds during steady-state operations, prevent failure of the third stage engine turbine, engine power loss, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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