AD 69-04-03

Active

Rotor Blade

Key Information
69-04-03
Active
March 22, 1969
Not specified
Unknown
39-724
Applicability
["Aircraft"]
["Rotorcraft"]
Schweizer Aircraft Corporation
269A 269A-1 269B
Regulatory Text

69-04-03 HUGHES: Amdt. 39-724. Applies to Model 269A, 269A-1, 269A-2, and 269B helicopters with P/N 269A6035 low tip speed tail rotor blade installed.

To insure continued airworthiness of the low tip speed tail rotor blade, prior to accumulation of 5000 hours' time in service, remove tail rotor blade, P/N 269A6035, marking it permanently and conspicuously to avoid its inadvertent return to service, and replace with a new or serviceable tail rotor blade, P/N 269A6035, having less than 5000 hours' time in service.

This amendment becomes effective March 22, 1969.

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