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Airplane  VL-3C – 1

The plane has been derived from basic VL-3 plane respecting American LSA rules. It has a larger, newly shaped wing and is produced with fixed landing gear and on land adjustable propeller. Strength test were carried out for MTOW 600 kg (1320 lbs).

    

Weights and Capacities

Wingspan 31'6''
Height 6'11''
Fuselage Length 20'4''
Cabin Width 42"
Prop Diameter 5'8''
Empty Weight 760 lbs
Maximum Gross Weight 1,320 lbs
Useable Fuel (US) 29 gal
Useful Load 560 lbs
Full Fuel Payload 390 lbs

Aircraft performance, capabilities and speeds

Take-off Distance [ground roll] 520 ft
Landing Distance [ground roll] 550 ft
Take-off Distance [to clear a 50’ obstacle] 1,050 ft
Landing Distance [to clear a 50’ obstacle] 1,100 ft
Sea Level Climb Rate 850 fpm
Service Ceiling 13,200msl
Maximum Range 730 nm
Fuel Flow 3.8 gph
Maximum Cruise Speed 119 ktas
Stall Speed [Vs0—Landing Configuration] 35 kts
Stall Speed [Vs1—Clean] 45 kts
Best Rate of Climb [Vy] 65 kts
Maneuvering Speed [Va] 88 kts
Normal Operating Speed [Vno] 110 kts
Never Exceed Speed [Vne] 145 kts

News

7 Jan 2010

Winter weather in Central Europe

is not favourable to flying and so more

17 Jul 2009

Aveko expresses its gratitude to all participants of 1. Rally of VL-3 Sprint airplanes ....

at Vysoke Myto who helped in this way to succes of this meeting. Altogether 17 planes VL-3 came flying , from which number five crews were from Belgium, single crews came from France, Luxembourg and Poland and nine from the... more

News archive

 
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