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Airworthiness Directives; Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes

airworthiness · Rule · Final rule. · Published 2010-07-27 · Effective 2010-08-31 · 75 FR 43809

Document

Document number
2010-18012
Federal Register citation
75 FR 43809
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Piper
Publication date
2010-07-27
Effective date
2010-08-31
FAA docket
Docket No. FAA-2009-1015

Abstract

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) PA-28, PA-32, PA-34, and PA-44 series airplanes. This AD requires you to inspect the control wheel shaft on both the pilot and copilot sides and, if necessary, replace the control wheel shaft. This AD results from two field reports of incorrectly assembled control wheel shafts. We are issuing this AD to detect and correct any incorrectly assembled control wheel shafts. This condition, if left uncorrected, could lead to separation of the control wheel shaft, resulting in loss of pitch and roll control.

Source

Authoritative
Federal Register document
Machine
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