Acrolite® 1A

 

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Acrolite 1A Light Aircraft

Name :             Acrolite

Model:             1A

Type:                Single place ultralight biplane.

Construction:   Welded steel tube fuselage, riveted aluminum tube tail group, aluminum leading edge D cell  wing, fabric covering.

Aircraft Physical Specifications 

Engine 40 hp Rotax 447 45 hp Rotax 503
Reduction 2.58 to 1 2.58 to 1
Propeller 62 x 32 63 x 36
Airfoil     NACA 4412  
Wingspan 22 ft.  
Wing area 140 sq. ft.  
Wing Chord 3.5 ft.  
Aspect ratio 6.3 to 1  
Length 16 ft.  
Height 5.75 ft.  
Fuel capacity 5 gal U.S.  
Wheel & tire size 500 X 5  
Empty weight 280 lbs  
Gross weight 500 lbs  
Span loading 11.4 lb./ft  
Wing loading 3.6 lb./sq. ft.  
Power loading 12.5 lb/bhp 11.1 lb/bhp

Aircraft Performance Specifications

Power off stall speed 32 mph.  
Power on stall speed 30 mph.  
Landing speed 37 mph.  
Maneuvering speed 65  mph.  
Maximum level speed 70 mph. 72 mph.
Never exceed speed 80 mph.  
Cruise speed 65 mph. @ 5000 rpm. 66 mph.
Best glide speed 50  mph.  
Best rate of climb 800 fpm. 1000 fpm.
Best climb rate speed 50 mph. 55 mph.
Best climb angle speed 48 mph..  
Range 100 sm..  
Take off distance 300 ft. 250 ft.
Landing distance 200 ft.