Number |
US-60-10-02 |
Issued by |
United States of America |
Issue date |
1960-05-12 |
Effective date |
1960-05-12 |
EASA approval number |
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ATA Chapter |
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Approval Holder / Type Designation |
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Revision |
Revised March 10, 1961. The AD published in the Federal Register as Amendment 143 was superseded by the following: Applies to All B-2 Helicopters With 248-40 and 248-46 Main Rotor Blades Installed.
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Correction |
Not applicable
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Supersedure |
None
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Publication(s) and related information |
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Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail:
ADs [at] easa.europa [dot] eu
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