Acro Sport Ace Junior Ace

$1,800 (in 1971) sports aircraft available as plan or kit since the early 1930s

Overview

Acro Sport United States ICAO: JACE 1930–Onward Active $1,800 (1971)

The Ace Junior Ace was designed by Orland Corben as a two-seat sports aircraft and was marketed by the Ace Aircraft Manufacturing Company during the early 1930s for home building.

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Specifications

Units
Engine
1 × Continental C85
Engine type
Piston
Power
85 hp · 63 kW
Avionics
—
Wing tips
No winglets
Seats
2
Crew
—
Cabin width
—
Cabin height
—
Cabin length
—
Exterior length
21 ft 4 in  ·  6.50 m
Tail height
7 ft 3 in  ·  2.20 m
Fuselage diameter
2 ft 7 in  ·  0.80 m
Wing span
26 ft 0 in  ·  7.92 m
Baggage volume
—
Gross weight
—
Empty weight
—
Max takeoff weight
1,350 lb  ·  600 kg
Max landing weight
—
Max payload
350 lb  ·  150 kg
Fuel capacity
20 gal · 100 L · 100 kg (AvGas)
Max cruise speed
113 kt  ·  130 mph  ·  209 km/h
Maximum speed
—
Cruise speed
—
Approach speed
49 kt  ·  56 mph  ·  91 km/h
Range
217 nm  ·  250 mi  ·  400 km
Fuel burn
—
Ceiling
10,500 ft  ·  3,200 m
Rate of climb
600 ft/min  ·  3 m/s
Takeoff distance
350 ft  ·  110 m
Landing distance
450 ft  ·  140 m
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Corben Junior Ace

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Operational Context

The Junior Ace was designed by Paul Poberezny, the founding president of the EAA (Experimental Aircraft Association) organization of aviation enthusiasts based in the United States. It is a lightweight aircraft, designed to be flown simply and needs very little maintenance.

The Junior Ace was piloted by Captain Bud Judy during its maiden flight where it was successful and showcased its shot field capabilities together with low stall speed which is suitable for small landing strips. The aircraft was adapted from the initial Corben Baby Ace so it could make effective use of aircraft engines.

The Junior Ace is of monoplane configuration with a parasol wing supported by cabane struts or a pylon. The wooden wing has a wingspan of 7.92 meters, and spars and ribs are manufactured from spruce. It is also fitted with conventional landing gear of chromoly tube with coil spring shocks which show better responsiveness to trail surfaces.

It is designed with modern wheels and has a wheelbase of 5 meters. The fabric-covered tubular fuselage of chromoly steel tube has been widened with a width of 0.8 meters, an external length of 6.5 meters, and an external height of 2 meters. The aircraft has a tandem cockpit for the pilot and passenger and may be closed off or left open. The tail assembly is of chromoly steel tube. It has a tail height of 2.2 meters.

The two-seat sports aircraft can be powered by a variety of Continental piston engines ranging from 85 hp to 120 hp. The Junior Ace has a maximum speed of 113 knots, a cruise speed of 91 knots, and a travel range of 217 nautical miles. It can fly up to 10,500 feet and can climb at a rate of 600 feet per minute. The takeoff and landing distances are 107 meters and 137 meters, respectively. The aircraft has a maximum takeoff weight of 606 kg, an empty weight of 367 kg, and a maximum payload of 170 kg. The fuel tank capacity is 24 US gal.