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importantRule

AD FAA-2007-28245

Airworthiness Directives; Cirrus Design Corporation Model SR20 and SR22 Airplanes

Summary

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.

Directive Details

AD Number

FAA-2007-28245

Document Number

E8-15474

Type

Rule

Publication Date

July 10, 2008

Effective Date

August 14, 2008

Affected Manufacturer

Cirrus Design Corporation Model SR20 and SR22

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2007-28245

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Cirrus Design Corporation Model SR20 and SR22 →

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