AD 2012-10-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | Aircraft Company | Airworthiness Directives; Cessna Aircraft Company Airplanes |
Unsafe Condition
Cracks found in the wing lower main spar caps, which could result in structural failure of the wing with consequent loss of control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left and right wing lower main spar caps for cracks. Replace cracked spar caps, wing spars, or wings with serviceable parts or incorporate an FAA-approved modification. Report inspection results to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight if cracks are found; otherwise, within a specified timeframe (not explicitly stated in the provided text).
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Affected Aircraft
Cessna Aircraft Company Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, P210N, 210R, T210R, and P210R airplanes with cantilever metal wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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