AD 66-03-02

Active

Electrical System

Key Information
66-03-02
Active
January 14, 1966
Not specified
Unknown
39-181
Applicability
["Aircraft"]
["Rotorcraft"]
Schweizer Aircraft Corporation
269A 269A-1 269B
Regulatory Text

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.

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References
This information is not available.
--- - Part 39
FAA Documents