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 The AD published in the Federal Register as Amendment 143 was superseded by the following: Applies to All B-2 Helicopters With 248-40 and 248-46 Main Rotor Blades Installed.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