RG or not... I'm curious:
1) What is your useful load?
2) What cruise speeds and fuel burns do you see? ROP or LOP?
3) What year/model do you have, and what engine HP?
Thanks!
1968, 150HP with a powerflow exhaust and the maple leaf fixed cowl flap and exhaust fairing
837 pounds useful
(Lots of stuff in this plane. Full panel, brittian 2 axis autopilot that tracks navs and heading bug very well, the powerflow, fiberglass fairings, BRS shoulder harness, 4 cyl EGT/CHT etc.) so it's on the heavy side IMHO
average 8 gph 120 MPH (slow but we have a climb prop due to the 150 & fixed pitch being anemic to begin with)
There's a big difference between the RG and FG, not just in the gear, but also the weight and complexity of fuel injection.
The FG 180 horse have a good power/weight ratio at gross.
150 horse, 2350 = 15.67 #/HP @ gross
180 horse (1969 which has fixed pitch prop 1970< is CS) 2500 = 13.89 #/HP
200 horse RG, 2800 = 14 #/ HP
That all being said, I really would like the RG. No stupid wheel pants to mess with when airing up the tires, goes faster etc. The baggage compartment is small tho due to the wheel well bumps.
It's said the 1968 with a 180 conversion is faster than all the later year FG due to the wing design. The 68 wing is thinner than all the other years which I like to compare to a mooney wing. The 68 (150) climbs pretty flat with typical being 400-600 FPM @ 95 MPH 110 # under gross on 90 degree day at 1,200 MSL.
I did a test the other day and about 300# under gross I climbed from 5500 to 12500 in 12 minutes, surface OAT temp was over 90 degrees.