AD 73-13-06

Active

Aileron and Rudder Trim

Key Information
73-13-06
Active
June 23, 1973
Not specified
Unknown
39-1671
Applicability
["Aircraft"]
["Small/Large Airplane"]
de Havilland Aircraft Co., Ltd., The
D.H.114 Heron Series 2A D.H.114 Heron Series 2DA D.H.114 Heron Series 2X
Regulatory Text

73-13-06 HAWKER SIDDELEY: Amdt. 39-1671. Applies to Hawker Siddeley deHavilland Model DH-114 "Heron" Airplanes, having Modifications 496 installed.

Compliance is required as indicated.

To prevent possible inadvertent actuation of aileron and rudder trim in a direction other than that desired and to prevent possible interference by the aileron trim jack with the aileron when in its full down position, accomplish the following:

Prior to September 21, 1973, unless already accomplished, incorporate Hawker Siddeley Modifications Nos. 1006 and 1053, or FAA-approved equivalents.

This amendment becomes effective June 23, 1973.

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