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Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes

airworthiness · Rule · Final rule. · Published 2008-07-10 · Effective 2008-08-14 · 73 FR 39583

Document

Document number
E8-15474
Federal Register citation
73 FR 39583
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cirrus Design Corporation Model SR20 and SR22
Publication date
2008-07-10
Effective date
2008-08-14
FAA docket
Docket No. FAA-2007-28245

Abstract

We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to replace the cabin door rod ends with new parts including a redesigned non-binding hinge pin that replaces the existing pin at the upper door hinge. This AD results from two known occurrences of in-flight cabin door separation (one total separation and one retained by the door strut). The rod ends, a component of the door hinges, may fail and result in a door separation from the airplane while in flight. We are issuing this AD to prevent in-flight failure of the cabin door, which could result in door separation from the airplane.

Source

Authoritative
Federal Register document
Machine
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