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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. |
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