VXL4-180-01.html - 2009-
Modified: 2010, 7th of March
Seats: 4
Construction : aluminium + composite
Standard Engine: Lycoming O-360- 180 HP
Max. Admitted power: 240 BHP
Fuel : unleaded gasoline
New Hartzell - 3 blades - constant speed propeller
Airframe is suitable for installation of other engine models
PERFORMANCE with Lycoming Engine - 180 HP Typical Load : 500 Lbs - Groos Weight: 1,650 Lbs
Performance numbers will vary depending on workmanship, propeller
and fairing installations
Max Level Speed : 110 mph ( 178 Km/h)
Cruise speed 75% power@7000ft) : 105 mph ( 169 - 190 Km/h)
Range@75%power at 7,000 ft: 315 miles ( 507 Km - 112 lt )
Range@75%power - Extended : 630 miles ( 1015 Km - 224 lt )
Rate of Climb: 720 fpm ( 3.7 m/min )
Stall speed ( clean): 48 MPH ( 77 Km/h )
Stall speed ( full flap ) : 39 mph ( 64 Km/h )
Take off distance: 390 ft ( 119 m )
Endurance - Standard - 3.0 Hrs
Endurance - Extended Range Options ) 6.0 Hrs
WEIGHTS
Empty Weight : 1,150 lbs ( 522 Kg )
Empty weight is dependent upon engine, propeller, avionics, etc.
Design gross weight: 2,200 lbs ( 1,000 Kg ) ( utility category )
Useful Load: 1,050 Lbs ( 478 Kg )
Wing Loading: 16.5 lb/ft²
Power Loading: 10.0 lb/hp ( 4.54 Kg/hp ) ( 160 HP )
Power Loading: 8.0 lb/hp ( 3.63 Kg/hp )( 200 HP )
Fuel Tank capacity - Standard - 30 US Gal ( 2 x 15 ) = 176 LBS ( 112 l ( 2 x 56 l ) = 80 Kg
Fuel Tank Capacity Extended Range Option: 60 Gl ( 4 x 15 ) = 353 LBS ( 224 L ( 4 x 56 l ) = 160 Kg
DESIGN PAYLOAD ( Occupants + Baggage/cargo ) :800 lbs ( 360 Kg )
DIMENSION
Cabin width : 44 in ( 112 cm )
Cabin Length: 78 in ( 198 cm )
Wing Span: 24ft 4in ( 7.42 m )
Length: 24 ft 6 in ( 7.5 m )
Height: 10ft ( 3 m )
Wing Span: 31 ft 4 in ( 9.55 m )
Wing area: 167 ft²( 15.5 m²)
Wing Chord: 5 ft 3 in ( ( 1.6 m )
Horizontal Tail Span: 10 ft 1 in ( 3.1 m )
Horizontal Tail Area: 30 sq t ( 2.8 m² )
Wing Loading: 12.9 LBS/ft² ( 62.9 Kg/m²)
Power Loading: 11.95 LBS/ft² ( 5.44 Kg/BHP )
font color="red">DESIGN LIMITATIONS
Power: 150 - 240 BHP
MAX. Installed powerplant weight : 440 Lbs ( 200 Kg )
MTOW - MAX Take Off Weight: 2,200 Lbs - 998 Kg
DESIGN load factor ( ultimate ) @ 2,200 lbs : + 5.7 , - 2.8
MAX. Wing Loading @ 2,200 Lbs: 13.2 PSF - ( 64.4 Kg/m²)
MAX. Flap Extended Speed : 80 MPH ( 129 Km/h)
MAX. Cruise Speed - Vc - 120 MPH ( 193 Km/h )
Never Exceed Speed - VNE - : 150 MPH ( 240 Km/h)
CERTIFICATIONS
USA: FAA LSA
AUSTRALIA : CASA ASTM Standard F2245
WORLDWIDE : Experimental
PRICE - YEAR 2010 -
- VXL4-180 - STOL from 80.000 Euro ready to flight -