| AD Number | 66-03-02 | Status | Active |
| Effective Date | January 14, 1966 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-181 |
| Product Type | ["Aircraft"] | Product Subtype | ["Rotorcraft"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Schweizer Aircraft Corporation |
| Model(s) | 269A 269A-1 269B |
66-03-02 HUGHES: Amdt. 39-181, Part 39, Federal Register January 14, 1966. Applies to Models 269A, 269A-1, and 269B Helicopters.
Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.
To eliminate a possible navigational hazard, accomplish the following:
(a) On helicopters with the 12-volt electrical system, remove the existing tail position light bulb and replace it with General Electric No. 1777 bulb or FAA-approved equivalent.
(b) On helicopters with the 24-volt electrical system, remove the existing bulb and replace it with a Grimes No. 1683 bulb or FAA-approved equivalent.
(Hughes Service Notices Nos. 2A-54 (269A), 2A-1-21 (269A-1 and (2B-22), (269B) dated October 28, 1965, pertain to this same modification.)
This directive effective January 14, 1966.