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| Glenn Bishell's R-120, Powered By O-200 |
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| R-120; Nose Wheel Option |
The Specifications in the table below are published
by BushCaddy and are the result of test flights with a Rotax 912 S, 100HP engine. When I complete the airplane I will
update this chart with my results using the Lycoming O-235.
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SPECIFICATIONS |
| wing span |
32 feet |
| wing chord |
63 inches |
| wing area |
168 sq. ft |
| wing loading |
8.9 lb. per sq. ft |
| length |
22 ft. 1 in. |
| cabin width |
44 in. |
| cabin height |
44 in. |
| fuel capacity |
20 or 34 imp. gallons |
| empty weight |
823 lb. |
| maximum gross take off weight |
1500 lb. - (1700 lbs on approval from
CLASS) |
| useful load |
677 lb. |
| fuel consumption |
4 imp. gal per hour |
| G Loading |
+5.7 / -3.8 |
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PERFORMANCE |
| Maximum speed (v.n.e.) |
130 m.p.h. |
| cruising speed at 75% power |
110 m.p.h. |
| cruising speed 60% power |
90 m.p.h. |
| power off stall |
34 m.p.h. |
| flap extended stall speed |
32 m.p.h. |
| rate of climb 1500 lbs |
800 f.p.m. |
| service ceiling |
16,000 feet |
| take off 1500 lbs |
200 feet |
| take off (floats) |
15 to 30 sec. (1500 lb.) |
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All Metal, Wheels, Floats Or Skis, Robust
Bushplane
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