AD 60-23-05

Active

Bellcrank Assembly Retirement

Key Information
60-23-05
Active
November 08, 1960
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Rotorcraft"]
Boeing Defense & Space Group
42A 42B 44A 44B
Regulatory Text

60-23-05 VERTOL: Amdt. 218 Part 507 Federal Register November 8, 1960. Applies to All 42 and 44 Series Helicopters.

Compliance required as indicated.

As a result of a recent fatigue failure of the lower directional bellcrank assembly, P/N 22C1611-13, all Vertol parts P/N 22C1611-13 must be retired upon the accumulation of 2,500 hours of time in service.

This directive effective November 8, 1960.

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