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AD FAA-2012-0534

Airworthiness Directives; Cessna Aircraft Company Airplanes

Summary

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, P210N, 210R, T210R, and P210R airplanes. This AD requires an inspection(s) of the left and right wing lower main spar caps for cracks and either replacing cracked wing lower main spar caps, wing spars, or wings (as applicable) with serviceable spar caps, spars, or wings that are found free of cracks or incorporating an FAA-approved modification. This AD also requires reporting the results of the inspections to the FAA. This AD was prompted by reports of cracks found in the wing lower main spar caps on the above-referenced airplanes with cantilever metal wings. We are issuing this AD to correct the unsafe condition on these products.

Directive Details

AD Number

FAA-2012-0534

Document Number

2012-11944

Type

Rule

Publication Date

May 21, 2012

Effective Date

June 5, 2012

Affected Manufacturer

Cessna Aircraft Company

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2012-0534

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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