AD 80-17-07

Active

Horizontal Hinge Pins

Key Information
80-17-07
Active
August 15, 1980
Not specified
Unknown
39-3877
Applicability
["Aircraft"]
["Rotorcraft"]
Sikorsky Aircraft Corporation
S-61A S-61D S-61E S-61L S-61N S-61NM S-61R S-61V
Regulatory Text

80-17-07 SIKORSKY AIRCRAFT: Amendment 39-3877. Applies to S-61 series helicopters certificated in all categories, including military counterparts. Compliance required as indicated.

To prevent fatigue failures of the horizontal hinge pins: Replace the Rotary Wing Horizontal Hinge Pin P/N S6110-23020 and S6110-23320 prior to 4000 and 5300 hours time in service, respectively, or within 25 hours time in service after the effective date of this AD, whichever occurs later.

This amendment is effective August 15, 1980.

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