80-02-08 VARGA AIRCRAFT CORPORATION (Morrisey): Amendment 39-3664. Applies to Varga Model 2150 and 2150A series airplanes certificated in all categories. Compliance required within the next ten (10) hours' time in service from the effective date of this AD, unless already accomplished. To prevent jamming of the rudder cables on the rudder balance weight attach bolts, accomplish the following: \n\n\t(a)\tRemove the two bolts attaching the rudder balance weight to the static balance arm and reinstall these bolts head downward, as shown in Figure 1 of this AD. \n\n\n\n\n\t(b)\tAlternative inspections, modifications or other actions which provide an equivalent level of safety may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\tThis amendment becomes effective January 21, 1980.