NWade wrote:A few notes that I haven't seen anyone comment on:
[*] On O-200's I'm not surprised this still isn't supported. Sonex has made it clear that they don't feel the O-200 adds any performance over an AeroVee or a Jab/Camit. Adding weight for no additional performance is pretty antithetical to most aircraft designers, Sonex included. I mean, do you see the RV-12 supporting an O-200 option? [Hint: No.]
--Noel
Sonex #1339
TD, Center-Stick, Acro-ailerons, Flush Pulled Rivets, AeroVee Turbo
Wings & Empennage finished, Aft Fuselage nearly complete
fastj22 wrote:The wing didn't change. Bumping up the gross above 1150 will increase the stall speed above LSA requirements.
IIRC, the change in stall speed with an increase in weight is:
new stall speed =(previous stall speed) x (sqrt (new weight/old weight))
From the factory numbers, an 1150 lb Sonex has a clean stall speed of 46 MPH, so, stall speed (clean) for a SONEX at the 1320 lb LSA limit (and I'm NOT saying it's a good idea to fly that way, given ROC and G-limits): 46 x sqrt (1320/1150) = 49.3 MPH = 43 KCAS.
I'm sure there are lots of good reasons not to fly a Sonex at 1320 lbs, but the airplane should still stall slower than the 45 KCAS LSA requirement.
(If my math is right!)
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