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AD FAA-2009-1015

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

Summary

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.

Directive Details

AD Number

FAA-2009-1015

Document Number

2010-18012

Type

Rule

Publication Date

July 27, 2010

Effective Date

August 31, 2010

Affected Manufacturer

Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2009-1015

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series →

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