AD 46-46-02

Active

Elevator Stop

Key Information
46-46-02
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

46-46-02\tNORTH AMERICAN: Was Mandatory Note 6 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 January 1, 1947. \n\n\tInspect all airplanes having Vest Two-Place Chum Seats installed prior to October 9, 1946, to determine that an elevator rear stop is installed on the horizontal stabilizer rear spar directly in front of the elevator horn and that the modification incorporates revised self-aligning rudder balance brackets, rudder balance cable, rudder pedal adjustment bar and reinforcement plates on forward side of firewall at the balance pulley bracket attachment points in accordance with Vest Installation Instructions dated October 9, 1946.

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