Airworthiness Directive

AD 2009-07-52 74 FR 17593 Active

Federal Aviation Administration · 14 CFR part 39

Corrects: This amendment is prompted by a Transport Canada AD report of a bearing incorrectly installed in the copilot lever assembly.

FR document
E9-8573
Amendment
39-15885
Published
2009-04-16
Effective
2009-05-01
Models covered
3

Last live check: 2026-10-04

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AD

2009-07-52

FR doc E9-8573 · 74 FR 17593

AD 2009-07-52Published 2009-04-16Effective 2009-05-01

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Corrects: This amendment is prompted by a Transport Canada AD report of a bearing incorrectly installed in the copilot lever assembly.

Supersedes an earlier directive that is not in our index. See the official text.

Full official abstract

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.

More directives for Bell 206 JetRanger / LongRanger

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All Bell 206 JetRanger / LongRanger directives

Applies to 3 models in our index