AD 46-17-01

Active

Flap Control Universal Joint Pins

Key Information
46-17-01
Active
Not specified
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Small Airplane"]
The Boeing Company
AT-6 (SNJ-2) AT-6A (SNJ-3) AT-6B AT-6C (SNJ-4) BC-1A
Regulatory Text

46-17-01\tNORTH AMERICAN: (Was Mandatory Note 5 of AD-2-575-3.) Applies to Army BC-1A, AT-6, -6A, -6B, -6C; Navy SNJ-2, -3, -4 Aircraft. \n\n\tTo be accomplished prior to original certification or at first periodic inspection thereafter. \n\n\tInspect the universal joint pins in the flap control push-pull tubes, P/N 19-152642, connecting the outer and inner flap for broken pins. Replace all broken pins with new pins and install a close fitting rubber hose over each universal joint to hold in place any pins which may break in the future. \n\n\t(North American Service Bulletin dated March 6, 1947, covers this subject also.)

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