Summary
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2009-07-52 and supersedes Emergency AD 2009-07-51, issued March 17, 2009, which was sent previously to all known U.S. owners and operators of Bell Helicopter Textron Canada Limited (Bell) Model 206A series, 206B series, 206L series, 407, and 427 helicopters by individual letters. This AD requires, before further flight, inspecting each cyclic control lever assembly (lever assembly) that has less than 50 hours time-in-service (TIS) to determine if it is correctly installed and properly staked in the lever assembly. This amendment is prompted by a Transport Canada AD report of a bearing incorrectly installed in the copilot lever assembly. The actions specified by this AD are intended to prevent failure of a bearing, failure of the lever assembly, and subsequent loss of control of the helicopter.
Directive Details
AD Number
FAA-2009-0350
Document Number
E9-8573
Type
Rule
Publication Date
April 16, 2009
Effective Date
May 1, 2009
Affected Manufacturer
Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407, and 427
Criticality
critical
Emergency
Yes
Docket ID
Docket No. FAA-2009-0350
Topics
Official Documents
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