Airworthiness Directive

AD 95-26-16 R1 61 FR 17562 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitively inspecting the alternate air door assembly to ensure a cotter pin exists and is secure, and replacing the cotter pin if it does not exist or is not secure.

FR document
96-9357
Amendment
39-9575
Published
1996-04-22
Effective
1996-05-16
Models covered
1

Last live check: 2026-08-19

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AD

95-26-16 R1

FR doc 96-9357 · 61 FR 17562

AD 95-26-16 R1Published 1996-04-22Effective 1996-05-16

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 repetitively inspecting the alternate air door assembly to ensure a cotter pin exists and is secure, and replacing the cotter pin if it does not exist or is not secure.

Full official abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-26-16 R1, which was sent previously to all known U.S. owners and operators of certain Mooney Aircraft Corporation (Mooney) Model M20J airplanes. This AD requires repetitively inspecting the alternate air door assembly to ensure a cotter pin exists and is secure, and replacing the cotter pin if it does not exist or is not secure. It also provides the option of incorporating an alternate air door plate assembly of improved design as terminating action for the repetitive inspections. Priority letter AD 95-26-16 R1 was prompted by a fatal accident involving one of the affected airplanes where the alternate air door became lodged in the air intake of the fuel injector causing engine failure. The actions specified by this AD are intended to prevent the alternate air door from separating from the airplane and restricting air flow to the engine.

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All Mooney M20 directives

Applies to 1 model in our index