AD 2020-03-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | Models 210G | Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) |
| aircraft | Cessna | Various | Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) |
| aircraft | Textron | Aviation Inc | Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) |
| aircraft | Aviat | Various | Airworthiness Directives; Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) |
Unsafe Condition
Corrosion of the carry-thru spar lower cap can lead to fatigue cracking or reduced structural strength of the carry-thru spar, which could result in separation of the wing and loss of airplane control.
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Required Actions
Perform a visual inspection of the carry-thru spar for corrosion, damage, and cracks, and complete an eddy current inspection. Apply protective coating and corrosion inhibiting compound (CIC). Remove the carry-thru spar from service or repair it (if possible) in accordance with the AMOC procedures identified in paragraph (o) of this AD.
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Compliance Time
Within 60 days after the effective date of this AD.
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Affected Aircraft
Textron Aviation Inc. Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, and T210M airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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