The Curtiss P-36 Hawk was developed and built by the Curtiss-Wright Corporation as an American-built fighter aircraft during the 1930s and 1940s. It first flew in May 1935, was introduced in 1938, and was retired in 1954. A total of 215 P-36s were built plus 900 export Hawk 75 versions. The aircraft was primarily used by the United States Army Air Corps, Finnish Air Force, French Air Force, and the Royal Air Force.

United States
1938 to: 1944
US$0.023 million (1944)
1x Pratt & Whitney R-1830-17 Twin Wasp
1,050 horsepower
Max Cruise Speed:
272 knots
504 Km/h
Approach Speed (Vref):
65 knots
Travel range:
750 Nautical Miles
1,389 Kilometers
Fuel Economy:
Service Ceiling:
33,000 feet
Rate of Climb:
3400 feet / minute
17.27metre / second
Take Off Distance:
Landing Distance:
Max Take Off Weight:
2,726 Kg
6,010 lbs
Max Landing Weight:
2,563 Kg
5,650 lbs
Max Payload:
550 Kg
1,213 lbs
Fuel Tank Capacity:
135 gallon
511 litre
Baggage Volume:
Seats - Economy / General:
1 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
Cabin Width:
Cabin Length:
Exterior Length:
8.7 metre - 28.54 feet
Tail height:
2.84 metre - 9.32 feet
Fuselage Diameter:
1.2 metre - 3.94 feet
Wing Span / Rotor Diameter:
11.38 metre - 37.34 feet
Wing Tips:
No Winglets

On May 6, 1935, the aircraft prototype took to the sky for the first time. On May 27, it was brought to Wright Field in Ohio to participate in the United States Army Air Corps fly-off, however, the contest was moved to April 1936. The P-36 was produced in various versions and was used by different air forces.

The P-36 is a single-seat fighter aircraft with an external length of 8.69 meters, an external height of 2.2 meters, and a fuselage width of 1.2 meters. The tail height is 2.84 meters and the wheelbase is 5.5 meters. It has a wingspan of 11.38 meters and a wing area of 21.92 square meters. The aircraft has an empty weight of 2,072 kg, a gross weight of 2,563 kg, and a maximum takeoff weight of 2,726 kg. The maximum payload is 550 kg and the fuel tank capacity is 135 US gal.

The P-36 Hawk is fitted with a single Pratt and Whitney R-1830-17 engine. It is a fourteen-cylinder two-row supercharged air-cooled radial piston engine with two overhead valves per cylinder, a single-speed General Electric centrifugal-type supercharger, a two-barrel Stromberg carburetor fuel system, an air-cooling system, and an epicyclic reduction gear. The engine produces a maximum takeoff thrust of 1,050 horsepower and drives a three-bladed constant-speed propeller. The aircraft has a maximum speed of 272 knots and a cruise speed of 230 knots. It has a range of 543 nautical miles at 230 knots and 750 nautical miles at 170 knots. It can fly up to 32,700 feet and can climb at a rate of 3,400 feet per minute.

The aircraft is loaded with a single 7.62 mm M1919 Browning machine gun and a 12.7 mm M2 Browning machine gun. Some were also equipped with a single hardpoint located under each wing that could carry up to 45 kg of bombs or a light bomb rack for three 23 kg, five 9 kg, or 14 kg bombs.

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