Airworthiness Directive

AD 2008-14-13 73 FR 39583 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E8-15474
Amendment
39-15608
Published
2008-07-10
Effective
2008-08-14
Models covered
2
Last live check
2026-10-03
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AD

2008-14-13

FR doc E8-15474 · 73 FR 39583

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

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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.

More directives for Cirrus SR20

  1. AD 2024-24-11 Airworthiness Directives; Cirrus Design Corporation Airplanes 2024-12-06
  2. AD 2008-11-18 Airworthiness Directives; Cirrus Design Corporation Model SR20 Airplanes 2008-06-02
  3. AD 2008-03-16 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2008-02-05
  4. AD 2007-14-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2007-07-12
  5. AD 2006-21-03 Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22... 2006-10-13

All Cirrus SR20 directives

Applies to 2 models in our index