Wing span |
21.5 ft. |
Wing area |
85 sqft |
Length |
19 ft. (varies with engine) |
Empty weight |
800-875 lbs. |
Gross weight (as LSA)* |
1210 lbs.* |
Useful load |
335-410 lbs. |
Wing loading |
14.2 psf. |
Design load factor |
+6 / - 3 "G" |
Design seat load |
250 lbs. |
Design baggage load** |
30 lbs.** |
Power*** |
100-160 hp (design)*** |
Fuel capacity (total) |
27.5 gallons |
* Note: Any Weight above 1050 lbs. must be due to fuel in wings
**Note: No acro/+4.4/-2.2 G limit with any baggage. Assumes 15 lbs evenly spread across floor either side of “tunnel”)
***Note: Possible engines, Corvair, TCM 0-200/0-240, Franklin 4B-235, Lycoming (and clone) 0-233/0-235/0-320, Titan IO-340, various UL Power, Jabiru 3300. Engine choices will affect the useful load, or possibly limit it due to available CG range.
