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Curtiss P-6 Hawk

The Curtiss P-6 Hawk is an American single-engine biplane fighter introduced into service in the late 1920s with the United States Army Air Corps and operated until the late 1930s prior to the outbreak of World War II.

The Curtiss Aeroplane and Motor Company (which became the Curtis-Wright Corporation (15 July 1929) supplied the USAAC with P-6s beginning in 1929.

A fast and highly manoeuvrable aircraft for its time, the XP-6 prototype took 2nd place in the 1927 U.S. National Air Races, and the XP-6A with wing surface radiators took first place, at 201 mph (323 km/h).

The P-6 was flown in a variety of paint schemes depending on the squadron, the most famous being the “Snow Owl” markings of the 17th Pursuit Squadron based at Selfridge Field near Detroit, Michigan.

The P-6Es served between 1932 and 1937 with the 1st Pursuit Group (17th and 94th PS) at Selfridge, and with the 8th Pursuit Group (33rd PS) at Langley Field, Virginia.

Numerous accidents claimed at least 27 of the 46 aircraft delivered.

As the P-6Es became obsolete, instead of receiving depot overhauls, they were allowed to wear out in service and were scrapped or sold.

At least one survived into 1942 in United States Army Air Forces service.

In 1932, Capt. Ruben C Moffat flew a P-6 converted with a supercharged Conqueror engine on a record-breaking flight.

He flew from Dayton, Ohio to Washington, D.C. at a speed of approximately 266 mph, at an altitude of 25,000 ft.

Variants

XP-6

Model 34P, modified from a P-1 with a Curtiss V-1570-17 Conqueror engine

XP-6A

Model 34K, same as XP-6 but with untapered wings and wing radiators to reduce drag

P-6A

18 ordered by the U.S. Army, nine were fitted with Prestone- rather than water-cooled V-1570 engines.

XP-6B

P-1 converted to take the V-1670 engine.

P-6C

Cancelled

XP-6D

XP-6B converted to take a turbocharged V-1570-C

P-6D

P-6As, (six of the seven surviving), re-engined in 1932 with turbocharged V-1570-C installed in 1932.

XP-6E

Model 35, also designated Y1P-22, ordered in July 1931 as P-6E prototype.

P-6E

46 delivered in 1931–1932, equipped the 17th and 33rd Pursuit Squadrons

XP-6F

Modified XP-6E with a supercharger and an enclosed cockpit

XP-6G

P-6E with a V-1570F

XP-6H

P-6E with 4 × .30 in (7.62 mm) machine guns mounted in the wings.

P-6S

Hawk I, three sold to Cuba with the 450 hp (336 kW) Pratt & Whitney R-1340 Wasp radial, and one sold to Japan as the Japan Hawk with the V-1570 inverted V piston engine.

P-11

Three ordered with the Curtiss H-1640 Chieftain engine of 600 hp (447 kW), two were completed with the V-1570 and redesignated P-6D.

XP-17

P-1 used as a testbed for the experimental Wright V-1470 air-cooled inverted V.

YP-20

P-11 converted with a Wright Cyclone radial.

XP-21

Two conversions of the XP-3A used to test the 300 hp (224 kW) Pratt & Whitney R-985 Wasp Junior radial, one became the XP-21A when modified with the R-975, and the other was converted to the P-1F standard.

XP-22

Temporary designation for a P-6A used to test new radiator installations for the V-1570-23 and converted back to a P-6A.

XP-23

Model 63, unfinished P-6E with light alloy monocoque fuselage, improved tail, and a turbocharged G1V-1570C with a geared propeller and the turbocharger removed.

Later redesignated YP-23.

Specifications

P-6E

Crew

1

Length

22 ft 7 in (6.88 m)

Wingspan

31 ft 6 in (9.60 m)

Height

8 ft 11 in (2.72 m)

Wing area

252 sq ft (23.4 m2)

Airfoil

Clark Y

Empty weight

2,715 lb (1,232 kg)

Gross weight

3,436 lb (1,559 kg)

Powerplant

1 × Curtiss V-1750C Conqueror V-12 liquid-cooled piston engine,

700 hp (520 kW)

Propellers

3-bladed propeller

Performance

Maximum speed

193 mph (311 km/h, 168 kn)

Cruise speed

165 mph (266 km/h, 143 kn)

Range

244 mi (393 km, 212 nmi)

Service ceiling

23,900 ft (7,300 m)

Rate of climb

2,480 ft/min (12.6 m/s)

Armament

Guns

2 × 0.30 in (7.6 mm) machine-guns.

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