Stolp Starlet SA500L - Specifications

(When acquired by EAA in 1981)

Engine:	Lycoming O-235-C-1, rated at 108 hp
Length Overall:	17 ft.
Height Overall:	5 ft. 10 in.
Wingspan:	25 ft.
Wing Chord:
Wing Area:	83 sq. ft.
Gross Weight:	1,000 lbs.
Empty Weight:	650 lbs.
Airfoil:	Clark Y, High-Lift
With McCauley metal propeller:
Maximum Speed (vne):	180 mph
Cruise Speed:	100 mph
Approach Speed:	80 mph
Stall Speed:	60 mph
Takeoff Distance:	300 ft.
Landing Distance:	400 ft.
Service Ceiling:	15,000 ft.
Fuel Capacity:	22 gal. - 13 in wing, 9 in fuselage
Fuel Consumption:	6.8 gph @2400 rpm
Cruising Range:	300 miles with reserve
Wheels:	500 x 5 with Cleveland brakes
Gear Tread:	59 in.