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
Official Documents
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