AD 78-05-07

Active

Main Landing Gear

Key Information
78-05-07
Active
April 13, 1978
Not specified
Unknown
39-3147
Applicability
["Aircraft"]
["Rotorcraft"]
Sikorsky Aircraft Corporation
S-61N
Regulatory Text

78-05-07 SIKORSKY: Amendment 39-3147. Applies to Model S-61N rotorcraft prior to and including Sikorsky Serial No. 61805.

Compliance required within the next 300 hours time in service after the effective date of this AD, unless already accomplished.

To prevent inadvertent landing gear retraction, modify the main landing gear electrical system in accordance with Sikorsky Service Bulletin 61B55-40 or later FAA approved revision.

The manufacturer's service bulletin identified and described in this directive is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Sikorsky Aircraft, Commercial Customer Service, Stratford, Connecticut 06602. These documents may also be examined at the Office of the Regional Counsel, New England Region, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803.

This amendment becomes effective April 13, 1978.

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