We use cookies in this website. Read about them in our privacy policy. To disable them, configure your browser properly. If you keep using this website, you are accepting those.
OK

V300 light aircraft

a great aircraft for great people

Specification

V300-UL (80hp)

DIMENSIONS [m] [ft]
Length 6.44 21.13
High 2.4 7.87
Wing span 9.15 30.02
Cabin width 1.2 3.94
WEIGHTS & QUANTITIES [kg] [lb]
Empty weight 283 623
Maximum take-off weight 473 1042
Maximum baggage 15 33
Operation load factors 4 -2
[L] [gal.]
Wing fuel tank capacity 70 18.5
PERFORMANCE* [kW] [hp]
Rotax 912 UL 60 80
[km/h] [kn]
Never exceed speed 270 146
Maximum level speed 205 111
Cruising speed 152 82
Stalling speed, Vs1 78 42
Stalling speed, Vs0 65 35
[m/s] [fpm]
Rate of climb 5.7 1114
[m] [ft]
Service ceiling 5144 16875
Take-off run (concrate) 138 453
Take-off field length (50ft obstacle) 240 786
Landing run 125 409
Landing filed length (50ft obstacle) 254 834
[km] [nm]
Range 806 435
[L/h] [gal./h]
Average fuel consumption 14 3.6

V300-UL (100hp)

DIMENSIONS [m] [ft]
Length 6.44 21.13
High 2.4 7.87
Wing span 9.15 30.02
Cabin width 1.2 3.94
WEIGHTS & QUANTITIES [kg] [lb]
Empty weight 283 623
Maximum take-off weight 473 1042
Maximum baggage 15 33
Operation load factors 4 -2
[L] [gal.]
Wing fuel tank capacity 70 18.5
PERFORMANCE* [kW] [hp]
Rotax 912 ULS 75 100
[km/h] [kn]
Never exceed speed 270 146
Maximum level speed 218 118
Cruising speed 154 83
Stalling speed, Vs1 78 42
Stalling speed, Vs0 65 35
[m/s] [fpm]
Rate of climb 7.1 1398
[m] [ft]
Service ceiling 5858 19219
Take-off run (concrate) 114 374
Take-off field length (50ft obstacle) 206 676
Landing run 173 567
Landing filed length (50ft obstacle) 304 997
[km] [nm]
Range 848 458
[L/h] [gal./h]
Average fuel consumption 15 3.8

V300-LSA (100hp)

DIMENSIONS [m] [ft]
Length 6.44 21.13
High 2.4 7.87
Wing span 9.15 30.02
Cabin width 1.2 3.94
WEIGHTS & QUANTITIES [kg] [lb]
Empty weight 336 741
Maximum take-off weight 600 1323
Maximum baggage 25 55
Operation load factors 4 -2
[L] [gal.]
Wing fuel tank capacity 120 31.7
PERFORMANCE* [kW] [hp]
Rotax 912 ULS 75 100
[km/h] [kn]
Never exceed speed 270 146
Maximum level speed 219 118
Cruising speed 169 91
Stalling speed, Vs1 87 47
Stalling speed, Vs0 73 39
[m/s] [fpm]
Rate of climb 5.1 1013
[m] [ft]
Service ceiling 4575 15010
Take-off run (concrate) 211 691
Take-off field length (50ft obstacle) 329 1080
Landing run 129 424
Landing filed length (50ft obstacle) 262 859
[km] [nm]
Range 1373 742
[L/h] [gal./h]
Average fuel consumption 16 4.2

* All performance data is evaluated for maximum take-off weight and ISA standard sea level conditions. All airspeeds are equivelent airspeeds. Venus Aircraft reserves the right to revise the above data whenever accasioned by product improvement, goverment/authority regulations or other good causes.

Image Gallery

Contact Form

Tell us something!