66-05-02 HAWKER SIDDELEY: Amdt. 39-185, Part 39, Federal Register January 28, 1968. Applies to de Havilland Model 104 Dove Series Airplanes.
Compliance required within 150 hours' time in service after the effective date of this AD.
As a result of cracking of eye ends used in the rudder and elevator trim tab connecting rod assemblies, accomplish the following unless already accomplished.
(a) Remove eye ends, P/N's CM.2A and CM.2B, and inspect for cracks visually or by use of other FAA-approved methods.
(b) Replace cracked parts with uncracked parts of the same part number before further flight.
(Hawker Siddeley Aviation, de Havilland Division T.N.S. Dove (104) Series CT (104) No. 187 or later ARB-approved issues cover this same subject).
This directive effective February 27, 1966.