Airworthiness Directive

AD 2001-06-06 66 FR 16846 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-6786
Amendment
39-12153
Published
2001-03-28
Effective
2001-05-14
Models covered
1
Last live check
2026-10-02
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AD

2001-06-06

FR doc 01-6786 · 66 FR 16846

AD 2001-06-06Published 2001-03-28Effective 2001-05-14

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 inspect the main landing gear pivot assemblies for cracks, replace any cracked main landing gear pivot assemblies, and install new bushings on the pivot assembly shaft.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Cessna Aircraft Company (Cessna) Model 172 airplanes. This AD requires you to inspect the main landing gear pivot assemblies for cracks, replace any cracked main landing gear pivot assemblies, and install new bushings on the pivot assembly shaft. This AD is the result of many service difficulty reports of cracked main landing gear pivot assemblies on the affected airplanes. The actions specified by this AD are intended to detect, correct, and prevent future cracks on the original design landing gear pivots. Cracked main landing gear pivots could fail resulting in gear-up landings or loss of braking.

More directives for Cessna 172

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All Cessna 172 directives

Applies to 1 model in our index