Here is a dumb question I got asked on my NATOPS check that I didn't know-
Why does the E-2 tail have Dihedral and the C-2 has a straight tail?
Pretty dick of that IP not to tell you the real answer, or at least the answer he was looking for.
Here come the enginerd glasses:
Flash's link claims it's interference from the radome. The aerodynamicist in me says: maybe, but I don't really see it. Pilots I've talked to who have flown both the C-2 and E-2

eek

said they fly very differently, at least in the landing pattern. The E-2 is (purportedly) very pitch sensitive, which makes sense given the looong slender, cylinder of a fuselage. This indicates that maybe the E-2 would be more prone to have undesirable phugoid and/or dutch roll characteristics. You can either dampen that out with a bigger empennage (at great expense in weight, RCS, drag and re-tooling the line) or cant the tailplane to give a bit of longitudinal dihedral. Most of the big passenger tubes at your local civvie airport use the dihedral tail strategy for the same reason.
The C-2 is noticeably fatter and more oblate in cross section, which I'm told gives it some perceivable fuselage lift, which would also mean more fuselage drag about the pitch axis. Thus, more damping of those nuisance oscillatory modes and no need to fold the tailplane and decrease it's effective area.