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
Official Documents
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