Airworthiness Directives; Cessna Aircraft Company Model 172RG Airplanes
airworthiness · Rule · Final rule. · Published 2001-03-28 · Effective 2001-05-14 · 66 FR 16846
Document
Document number
01-6786
Federal Register citation
66 FR 16846
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cessna
Publication date
2001-03-28
Effective date
2001-05-14
FAA docket
Docket No. 2000-CE-24-AD
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.