Airworthiness Directive

AD 2012-05-09 77 FR 16135 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-6521
Amendment
39-16981
Published
2012-03-20
Effective
2012-03-20
Models covered
1
Last live check
2026-10-02
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AD

2012-05-09

FR doc 2012-6521 · 77 FR 16135

AD 2012-05-09Published 2012-03-20Effective 2012-03-20

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 inspecting the tail pitch trim assembly for correct positioning and proper attachment and inspecting the Huck Bolt fasteners for proper security with repair as necessary for certain Models M20R and M20TN.

Full official abstract

We are issuing an airworthiness directive (AD) for all Mooney Aviation Company, Inc. (Mooney) Models M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, and M20TN airplanes that supersedes an existing AD that is applicable to certain Model M20R and M20TN airplanes. The existing AD currently requires inspecting the tail pitch trim assembly for correct positioning and proper attachment and inspecting the Huck Bolt fasteners for proper security with repair as necessary for certain Models M20R and M20TN. That AD also requires sending the inspection results to the FAA and Mooney. This AD retains all of the actions, except the reporting requirement from the previous AD and adds airplane models to the applicability. This AD was prompted by a report of an incident on a Mooney Model M20TN airplane regarding failure of the tail pitch trim assembly, which could result in loss of control. We are issuing this AD to correct the unsafe condition on these products.

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All Mooney M20 directives

Applies to 1 model in our index