Airworthiness Directive

AD 2012-10-04 77 FR 29863 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-11944
Amendment
39-17053
Published
2012-05-21
Effective
2012-06-05
Models covered
1
Last live check
2026-10-03
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AD

2012-10-04

FR doc 2012-11944 · 77 FR 29863

AD 2012-10-04Published 2012-05-21Effective 2012-06-05

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 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…

Full official abstract

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.

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All Cessna 210 Centurion directives

Applies to 1 model in our index