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Airworthiness Directives; Taylorcraft A, B, and F Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2007-08-13 · Effective 2007-08-20 · 72 FR 45153

Document

Document number
E7-15581
Federal Register citation
72 FR 45153
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2007-08-13
Effective date
2007-08-20
FAA docket
Docket No. FAA-2007-28478

Abstract

The FAA is adopting a new airworthiness directive (AD) for all Taylorcraft A, B, and F series airplanes. This AD requires you to initially inspect the left and right wing front and aft lift struts for corrosion and cracks, replace any cracked strut or strut with corrosion that exceeds certain limits with either sealed or non-sealed struts, and repetitively inspect any non-sealed struts. This AD results from inspections where several different struts were found with moderate to severe corrosion and required strut replacement. We are issuing this AD to detect and correct corrosion or cracks in the right and left wing front and aft lift struts. This condition, if not corrected, could result in failure of the lift strut and lead to in-flight separation of the wing with consequent loss of control.

Source

Authoritative
Federal Register document
Machine
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