AD 62-11-04

Active

Operating Limitations

Key Information
62-11-04
Active
May 15, 1962
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Rotorcraft"]
Schweizer Aircraft Corporation
269A
Regulatory Text

62-11-04 HUGHES: Amdt. 438 Part 507 Federal Register May 15, 1962. Applies to Model 269A Helicopters Equipped With Lycoming Model 0-360-C2D Engines of Serial Numbers L-3816-36 Through L-4599-36 and L-4601-36 Through L-4640-36.

Compliance required within 50 hours' time in service after the effective date of this directive.

Because of revisions to the operating limitations necessitated by changes in engine camshafts which resulted in a reduction in maximum horsepower, the FAA approved Flight Manual shall be revised to incorporate the new operating limitations as set forth in Hughes Model 269A Flight Manual revised page 24A.

When engines modified to incorporate a new camshaft in accordance with Lycoming Service Instructions are installed, the aircraft may be operated in accordance with original operating limitations.

This directive effective May 15, 1962.

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