Hi, I'm building my first R/C airplane, a DAW TG-3. I'm pretty far along,
the wing is assembled and covered and the fuselage is covered also. The
next step is attaching the horizontal and vertical stablizers to the
fuselage. Through sheer luck I was surfing the Temple Hill Slope Squadron
web site and noticed that there was a review of a TG-3 by one of the
members. The review indicated that one of the areas of deficiency with the
building instructions was what the angle of incidence of the horizontal
stabilizer should be and how to set it. The reviewer is right, there
doesn't seem to be any specification of what the angle of incidence should
be in the instructions. Can someone shed some light on what the angle of
incidence of the horizontal stabilizer should be for a TG-3? How is the
angle of incidence measured?
Thanks...
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