AD 87-04-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | EADS CASA | C-212-CB | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-CC | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-CD | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-CE | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-CF | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-DE | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
| aircraft | EADS CASA | C-212-DF | Airworthiness Directives; CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212 Airplanes |
Unsafe Condition
Loss of aircraft control on the runway caused by fractured nose landing gear components.
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Required Actions
Modify the nose landing gear in accordance with CASA Service Bulletin 212-32-21, Revision 1, dated June 4, 1986. An alternate means of compliance or adjustment of the compliance time may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199 to operate the airplane to a base for modification.
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Compliance Time
within 45 days after the effective date of this AD
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Affected Aircraft
CONSTRUCCIONES AERONAUTICAS S.A. (CASA) Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, C-212-DE, C-212-DF airplanes identified in CASA Service Bulletin 212-32-21, Revision 1, dated June 4, 1986.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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