Acro Sport Nesmith Cougar

The Nesmith Cougar is a single-seat homebuilt aircraft developed in the United States during the 1970s. Intended for amateur construction, it blends straightforward fabrication with sport performance. The design reflects the experimental aviation movement’s focus on accessibility and hands-on building.

Nesmith Cougar 1C ‘N9092R’ © RuthAS

Overview

Acro Sport United States ICAO: COUG 1957–Onward Active $3,000 (1971)

Acro Sport Nesmith Cougar — single-seat homebuilt sport aircraftThe Cougar emerged in the early 1970s as a compact low-wing design built around welded steel tubing and fabric covering. Its configuration emphasizes structural simplicity and light weight. Builders were drawn to the design because it required conventional materials and did not depend on complex manufacturing processes.Engine installations vary, but most Cougars use piston engines producing between 100 and 125 horsepower. Cruise speeds typically approach 120 knots (222 km/h), depending on configuration. Maximum takeoff weight generally remains below 1,200 pounds (544 kg), consistent with its lightweight construction and single-seat layout.The Nesmith Cougar remains active in the experimental category, with many examples still flying. Its straightforward design and responsive handling make it suitable for sport and limited aerobatic flying. The aircraft stands as a representative example of grassroots American homebuilt aviation.

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Specifications

Units
Engine
1 × Lycoming O-235
Engine type
Piston
Power
115 hp · 86 kW
Avionics
Wing tips
No winglets
Seats
2
Crew
Cabin width
Cabin height
Cabin length
Exterior length
18 ft 11 in  ·  5.77 m
Tail height
5 ft 6 in  ·  1.68 m
Fuselage diameter
2 ft 0 in  ·  0.60 m
Wing span
20 ft 6 in  ·  6.25 m
Baggage volume
Gross weight
Empty weight
Max takeoff weight
1,250 lb  ·  550 kg
Max landing weight
Max payload
450 lb  ·  200 kg
Fuel capacity
30 gal · 100 L · 100 kg (AvGas)
Max cruise speed
170 kt  ·  196 mph  ·  315 km/h
Maximum speed
Cruise speed
Approach speed
46 kt  ·  53 mph  ·  85 km/h
Range
650 nm  ·  750 mi  ·  1,200 km
Fuel burn
Ceiling
13,000 ft  ·  4,000 m
Rate of climb
1,300 ft/min  ·  7 m/s
Takeoff distance
1,120 ft  ·  340 m
Landing distance
980 ft  ·  300 m
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Nesmith Cougar 1C ‘N9092R’

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Operational Context

The Nesmith Cougar was developed by Robert Nesmith in the mid-1950s. During that time, he considered to enhance the Wittmand Tailwind by Steve Wittland, but it turned out that the two aircraft have the same design and are very difficult to distinguish from each other.

The first Cougar was initially marketed by Nesmith as low-cost aircraft intended for homebuilders. In 1963, the Cougar was modified by Leonard Eaves and won a competition in the Experimental Aircraft ASSOCIATION (EAA). The organization then purchased rights on the aircraft, and in due course was acquired by Acro Sport.

The Cougar featured a conventional wooden high wing with struts and has a wingspan of 6.25 meters and a wing area of 7.66 square meters. The fixed tailwheel type undercarriage has a wheelbase of 4.6 meters. The aircraft has an external length of 5.77 meters, an eternal height of 1.47 meters, a tail height of 1.68 meters, and a fuselage diameter of 0.6 meters. The tail assembly as well as the fuselage is built of steel-tube construction. The entire aircraft was covered with fabric and was equipped with a tandem configuration for a pilot and a passenger.

The Nesmith M1 Cougar is the initial design powered by 108 horsepower Lycoming engine intended for home building. The Cougar Comet is a modified version with a single Lycoming O-290D engine rated at 125 horsepower. The Chigger and Landoll’s Skydoll had was built with two designs. The first was fitted with folding wings and Culver Cadet undercarriage, known as the Chigger while the second was fitted with folding wings that featured automatic control latching.

The typical Cougar has a maximum speed of 169 knots, an economic cruise speed of 135 knots, and a stall speed of 46 knots. The travel range is 650 nautical miles. It could fly up to 13,000 feet and could climb at a rate of 1,300 feet per minute. The takeoff distance is 340 meters and the landing distance is 300 meters.