Wing Span |
23.5 ft. |
Wing Area |
93 sq. ft. |
Length |
19 ft. (varies with engine) |
Empty Weight |
700-775 lbs. |
Gross Weight (as LSA)* |
1,115 lbs. (Note: Any weight above 1015 lbs. must be due to fuel in wings) |
Useful Load (as LSA) |
340-415 lbs. |
Wing Loading |
11.99 per sq. ft |
Design Load Factor |
+6/-3 “G” |
Design Seat Load |
250 lbs. |
Design Baggage Load** |
30 lbs. (no acro/+4.4/-2.2 G limit with any baggage)** |
Power (see below)*** |
100-130 hp (design)*** |
Fuel Capacity (total) |
27.5 gallons |
* Any weight above 1015 lbs. must be due to fuel in wings.
** No acro/+4.4/-2.2 G limit with any baggage. Assumes 15 lbs evenly spread across floor either side of “tunnel”
***Possible engines, Corvair, TCM 0-200/0-240, Franklin 4B-235, Lycoming 0-233/0-235, various UL Power, Jabiru 3300. Engine choices will affect the useful load, or possibly limit it due to available CG range
