-
4-place (the "Light
Sport Aircraft" model --hereafter "LSA"-- is
2-place)
-
1650# gross weight
[LSA 1430#]
-
Wingspan 39', area
110 ft^2
-
Fuselage frontal area
<9 ft^2; total ~20 ft^2
-
Wing loading: 12
lbm/ft^2
-
Cruise 175 kt, 9gph; Vh=215kt [LSA
cruise 105kt, 5gph; 120kt Vh, 7gph]; Vne=250kt.
-
Power Loading: ~4
lbm/HP ( Climb
3000fpm to 7000!,
2000fpm to 14000! [non-LSA
tune, pilot only] )
-
Stall 51mph clean;
Best Glide 90kt@450fpm ( Glide
ratio 17+:1 at 5000,
e.g. 110ktGS/-600fpm [ LSA, pilot only])
-
Range 1000nm [LSA
400nm]
-
Max altitude 12500 unpressurized [Pressurized 38000, LSA
7500]
-
Boxer-4 280hp@6500rpm
/ 275ftlbs@4500, turbocharged, watercooled, 340# wet [ LSA
4 cyl engine@180hp ]
-
No reduction gear or
transmission.
-
No floats, pontoons,
sponsons, pylons, or other traditional amphibian "drag devices'"
-
Repositionable gear
-
Exhaust-blown hull
hydro-steps
-
Optional ballistic parachute, air-bags
|
|
