AD 98-12-28
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | EADS CASA | C-212-CB | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-CC | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-CD | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-CE | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-CF | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-DE | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
| aircraft | EADS CASA | C-212-DF | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 Series Airplanes |
Unsafe Condition
Cracking in the false spar of the wing could result in reduced structural integrity of the wing.
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Required Actions
Perform a detailed visual inspection for cracking in the false spar of the wing on left and right sides in accordance with CASA Product Support Document COM 212-224. Repeat inspections at intervals not exceeding 1,200 flight hours. If cracking is found, repair prior to further flight using an approved method.
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Compliance Time
Within 1,200 flight hours after the effective date of this AD
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Affected Aircraft
CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212 series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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