Airworthiness Directives; Cessna Aircraft Company Model 525A Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2009-11-30 · Effective 2009-12-15 · 74 FR 62479
Document
Document number
E9-28234
Federal Register citation
74 FR 62479
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Cessna
Publication date
2009-11-30
Effective date
2009-12-15
FAA docket
Docket No. FAA-2009-1096
Abstract
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Model 525A airplanes. This AD requires you to repetitively inspect the thrust attenuator paddle assemblies for loose and damaged fasteners and for cracks. This AD also requires you to replace loose or damaged fasteners and replace cracked thrust attenuator paddles found during any inspection. This AD results from reports of fatigue cracks found in thrust attenuator paddles. We are issuing this AD to detect and correct loose and damaged fasteners and cracks in the thrust attenuator paddles, which could result in in- flight departure of the thrust attenuator paddles. This failure could lead to rudder and elevator damage and result in loss of control.