Construction
Materials
All composite materials made from molds of the original aircraft. Wet wing holding 40 gallons of fuel.
Engines from 100 to 230 horesepower.
| Wingspan |
28 ft |
Fuselage
Length |
21 ft |
| Wing Area |
92 ft2 |
Fuselage
Height |
7.5 ft |
| Aspect Ratio |
8.51 |
Fuselage
Width |
54.5 in |
| Wing Loading |
14.3 lbs/ft2 |
Empty Weight |
800 lbs |
| Fuel Capacity |
40 Gallons
US |
Gross Weight |
1320 lbs |
Calculated
Performance Specifications
Calculations are based
on a 100 hp engine. Aircraft can use engines up to 230 hp.
| Max
Speed @ 5500 ft msl |
156
mph |
Cruise
Speed @ 5500 ft msl |
145
mph |
| Stall w/Flaps |
56 mph |
Rate of Climb
Sea Level |
1,2000 fpm |
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information, images, photos, etc. unless otherwise noted are ©
by Jay S. McMullan. DO NOT copy in any form without the written, expressed
permission of Jay S. McMullan and/or his designees. All information contained
on this website or in any publication written by Jay S. McMullan is strictly
for entertainment purposes only! Use at your own risks! |
