Overview
The Junior Ace first appeared in the 1950s as part of the broader homebuilt movement in the United States. It uses a welded steel tube fuselage and fabric covering. The biplane layout provides responsive handling suited to recreational flying.Engines vary by builder, but many installations produce between 65 and 100 horsepower. Cruise speeds typically range near 90 to 100 knots (167 to 185 km/h). Maximum takeoff weight generally falls below 1,000 pounds (454 kg), depending on configuration.The Junior Ace remains a symbol of grassroots aviation. Its straightforward construction makes it accessible to amateur builders. Many examples continue flying in the experimental category today.
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Specifications
- 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
Gallery