Airworthiness Directive

AD 2008-14-13 73 FR 39583

Federal Aviation Administration · 14 CFR part 39

FR document
E8-15474
Amendment
39-15608
Published
2008-07-10
Models covered
2
Last live check
2026-08-17
AD

2008-14-13

FR doc E8-15474 · 73 FR 39583

AD 2008-14-13Published 2008-07-10Effective 2008-08-14

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.

Full official 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.

Applies to 2 models in our index