VXL5-300-01.html - 2009-
Modified: 2010, 7th of March
Seats: 2 + 3
Construction : aluminium + composite
Standard Engine: Lycoming - 300 HP
Max. Admitted power: 310 HP
Fuel : unleaded gasoline
New Hartzell - 3 blades - constant speed propeller
Airframe is suitable for installation of other engine models
PERFORMANCE with Lycoming Engine - 300 HP
Performance numbers will vary depending on workmanship, propeller and fairing
installations
Top Speed ( sea level ): 200 kias ( 370 Km/h )
Cruise speed ( true airspeed, 75% power@8000ft) : 190 kias ( 350 Km/h )
Range@65%power ( 70 US Gal.- 265 l - version): 950 miles ( 1760 Km )
Max range @ 65% power - 2300 Km with 350 l tank
Rate of Climb: 1350 fpm ( 411 M/min )
Service ceiling: 20,000 ft ( 6.000 m )
Landing speed: 75 kts( 130 Km/h )
Minimum speed : 65 kts ( 120 Km/h )
Take off distance: 1400 ft ( 426 m )
Landing distance: 1500 ft ( 457 )
WEIGHTS
Empty Weight : from 1800 lbs ( 816 Kg )
Empty weight is dependent upon engine, propeller, avionics, etc.
Recommended gross weight: 2900 lbs ( utility category )( 1315 Kg )
Useful Load: 1100 lbs ( 499 Kg )
Wing Loading: 20.0 lb/ft²
Design Load Factors: +9/-7 G-Load
Fuel Tank capacity : from 70 to 93 US Gal ( 265 l - 352 l )
DIMENSION
Wing Span: 31' ( 9,45 m )
Canard span: 188" ( 4,78 m )
Length Overall: 20' ( 6,10 m )
Wing area: 122.5 SqFt
Canard wing area: 22.8 ft²
Wheel Base: 110" ( 2.79 m )
Track Width: 80" ( 2.03 m )
CERTIFICATIONS
USA: FAA LSA
AUSTRALIA : CASA ASTM Standard F2245
WORLDWIDE : Experimental
PRICE - YEAR 2010 -
- VXL5-300 : retractile gear - from 100.000 Euro ready to flight -