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| Beaver
SS - General Specs
*figures are
based on the prototype aircraft
production kit may vary based on installed options and
construction technique
| Type |
Tri-Gear Swept
Mono High Wing (Detachable) |
| Fuselage
Structure |
6061-T6 Aluminum |
| Length |
17'8" |
| Wing
Span |
31' |
| Wing
Area |
138 sq/ft |
| Seats |
single |
| Empty
Weight |
340 lbs* |
| Gross
Weight |
650 lbs |
| Fuel
Capacity |
5 U.S. Gallons
seat tank |
| Build
Time |
150-200 hours*
typical |
| Design
Load Factors |
Design Load limit
(50% margin) +4 / -2 G's |
Beaver
SS - Performance
*figures are
based on the prototype aircraft
production kit will vary based on installed options,
construction and flying technique
| Take
Off Distance |
less than 90'* |
| Glide
Ratio |
better than 7:1
at 45 mph* |
| Landing
Roll |
less than 65'* |
| Roll
Rate |
Better than 36
deg. / sec* |
| Max.
Operating Altitude |
12,000' ASL* |
| Rate
of Climb |
better than 800
ft/min* |
| Max
Level Speed |
85 mph |
| Max
Cruise Speed |
67 mph* |
| Stall,
Power Off (Vso) |
30 mph* |
| Never
Exceed (Vne) |
90 mph |
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from us within that time frame, send the e-mail again or call
us at 250-549-1102. |
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