6 May 1935: At Buffalo, New York, the prototype Curtiss-Wright Model 75, X17Y, serial number 11923, made its first flight.
Designed by Donovan Reese Berlin, the airplane was a modern design of all metal construction, with fabric covered control surfaces. The Model 75 was a single-seat, single-engine low-wing monoplane with retractable landing gear.
In its original configuration, the Model 75 was powered by an air-cooled, supercharged 1,666.860 cubic inch displacement (27.315 liter) Wright Aeronautical Division GR1670A1 two-row 14-cylinder radial engine. The GR1670A1 was a developmental engine with a compression ratio of 6.75:1. It was rated at 775 horsepower at 2,400 r.p.m. at Sea Level, and 830 horsepower at 2,600 horsepower for takeoff, burning 87-octane gasoline. The engine was 3 feet, 9 inches (1.143 meters) in diameter, 4 feet, 4–25/32 inches (1.341 meters) long, and weighed 1,160 pounds (526 kilograms). The GR1670A1 drove a three-bladed Curtiss Electric constant-speed propeller through a 16:11 gear reduction.
The GR1670A1 was also used in the Seversky SEV-S1, NR18Y, a record-setting experimental variant of the rival Seversky P-35.
Registration issued 1 June 1936, cancelled 26 April 1937.
The Curtiss-Wright Model 75 would be developed into the P-36 Hawk fighter for the U.S. Army Air Corps. France ordered it as the H75A-1, and in British service, it was known as the Mohawk Mk.I.
The tenth production P-36 was modified with a liquid-cooled Allison V-1710 V-12 engine to become the prototype XP-40.
26 April 1939: The United States Army Air Corps placed an order for 524 Curtiss-Wright P-40 Warhawks. This was the largest production order for any U.S.-built fighter since World War I. The total cost was $12,872,398.¹
The order was authorized by the Air Corps Expansion Act, approved by Congress 3 April, and signed by President Roosevelt on 26 April 1939.
The Curtiss-Wright Corporation Hawk 81 (P-40 Warhawk) was a single-seat, single-engine pursuit, designed by Chief Engineer Donovan Reese Berlin. It was developed from Berlin’s radial-engine P-36 Hawk. The P-40 was a low-wing monoplane of all-metal construction and used flush riveting to reduce aerodynamic drag. It had an enclosed cockpit and retractable landing gear (including the tail wheel). Extensive wind tunnel testing at the NACA Langley laboratories refined the airplane’s design, significantly increasing the top speed.
The new fighter was 31 feet, 8-9/16 inches (9.666 meters) long with a wingspan of 37 feet, 3½ inches (11.366 meters) and overall height of 9 feet, 7 inches (2.921 meters). The P-40’s empty weight was 5,376 pounds (2,438.5 kilograms) and gross weight was 6,787 pounds (3,078.5 kilograms).
The P-40 was powered by a liquid-cooled, supercharged, 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Co. V-1710-C15 (V-1710-33). This was a single overhead cam (SOHC) 60° V-12 engine designed by Harold Caminez, Allison’s chief engineer. The V-1710-33 had a compression ratio of 6.65:1. It was rated at 930 horsepower at 2,600 r.p.m. at 12,800 feet (3,901 meters), and 1,040 horsepower at 2,800 r.p.m. for takeoff, burning 100-octane gasoline. The engine turned a three-bladed Curtiss Electric constant-speed propeller through a 2:1 gear reduction. The V-1710-33 was 8 feet, 2.54 inches (2.503 meters) long, 3 feet, 5.88 inches (1.064 meters) high, and 2 feet, 5.29 inches (0.744 meters) wide. It weighed 1,340 pounds (607.8 kilograms).
The cruising speed of the P-40 was 272 miles per hour (438 kilometers per hour) and the maximum speed was 357 miles per hour (575 kilometers per hour) at 15,000 feet (4,572 meters). The Warhawk had a service ceiling of 30,600 feet (9,327 meters) and the absolute ceiling was 31,600 feet (9,632 meters). The range was 950 miles (1,529 kilometers) at 250 miles per hour (402 kilometers per hour).
The fighter (at the time, the Air Corps designated this type as a “pursuit”) was armed with two air-cooled Browning AN-M2 .50-caliber machine guns on the engine cowl, synchronized to fire through the propeller, with 380 rounds of ammunition per gun. Provisions were included for one Browning M2 .30-caliber aircraft machine gun, with 500 rounds of ammunition, in each wing.
The first production P-40 Warhawk, 39-156, made its first flight 4 April 1940. The 8th Pursuit Group at Langley Field, Virginia, was the first Army Air Corps unit to be equipped with the P-40.
After 200 P-40s were produced for the Air Corps, production was interrupted to allow Curtiss-Wright to build 100 Hawk 85A-1 export variants for the French Armée de l’air, then engaged with the invading forces of Nazi Germany. When France surrendered 22 June 1940, none of these airplanes had been delivered. The order was then assumed by the British Royal Air Force as the Tomahawk I.
U.S. Warhawk production resumed as the improved P-40B, and the remainder of the P-40 order was cancelled.
26 March 1940: At Lambert–St. Louis Municipal Airport, just to the west of the Mississippi River in the state of Missouri, test pilots Edmund Turney Allen and Dean Cullen Smith took the prototype Curtiss-Wright CW-20T, NX19436, for its first flight.
BIMOTORED GIANT READY FOR TESTS
Curtiss-Wright Substratosphere Plane Works Smoothly in Takeoff
By DEVON FRANCIS
Associated Press Aviation Editor.
ST. LOUIS, March 27.—The world’s first bi-motored transport plane designed and powered to eliminate the hazard attending the failure of one engine on takeoff was made ready for two months or more of flight-testing today before being offered to commercial airlines.
The 19-ton, 36-passenger Curtiss-Wright substratosphere transport was engineered to permit one engine to go dead at any point on the take-off as a pilot climbs for altitude and still maintain safe flight.
Each of its engines produces 1700 horsepower. The largest engines ever to be fitted to a transport plane heretofore have been of 1500 horsepower. Either one of the new transport’s engines will carry it to an altitude of 13,000 feet.
Fastened to the 108-foot wing with rubber cushions to produce what Curtiss-Wright engineers described as “dynamic balance,” the engines transmit only about 50 per cent of the normal vibration to the cabin of the plane.
C, s/n 101. W. France, vice president and general manager of the St. Louis airplane division of the company, yesterday witnessed the maiden take-off of the transport from the ground. Then he climbed to the control tower of the St. Louis municipal airport for an innovation in airplane testing.
France called the test pilot, Eddie Allen of Seattle, on the tower radiophone.
Dean Smith, co-pilot, answered.
“Dean,” he said, “that looked grand. Congratulations.”
“O. K.,” replied Smith, “I’ll tell Eddie.”
A little later Allen brought the huge plane into a smooth landing. He remarked that the plane had flown 190 miles an hour on only 30 per cent of its power. Transports usually cruise at 50 to 55 per cent.
The additional testing will be for an approved type certificate from the government.
The Curtiss-Wright CW-20T, NX19436, (manufacturer’s serial number 101) was a prototype twin-engine commercial airliner designed by George Augustus Page, Jr. Originally built with a twin-tail configuration, flight testing resulted in a change to a single, large vertical fin and rudder. Designed to be pressurized, the fuselage had a Figure 8 cross section, with the cabin floor at the narrowest point for increased strength. In this prototype, the fuselage was faired over to provide a smooth, more cylindrical shape. Considerable wind tunnel testing had been performed by CalTech in Pasadena, California, resulting in a very sleek nose section.
On 20 June 1941, the United States Army Air Forces ¹ purchased the CW-20T and designated it as the Curtiss C-55, serial number 41-21041. It would become the prototype of the C-46 Commando military transport. The Army Air Forces returned the C-55 to Curtiss-Wright for modifications.
The CW-20T was 76 feet, 4 inches (23.266 meters) long with a wingspan of 108 feet, 0 inches (32.918 meters). It was powered by two air-cooled, supercharged, 2,603.7-cubic-inch-displacement (42.688 liters) Wright Aeronautical Corporation Cyclone 14 GR2600A5B-5 (R-2600-17A) two-row, 14-cylinder radial engines, driving three-bladed Curtiss Electric C-533-D controllable-pitch propellers through a 16:9 gear reduction. This engine had a compression ration of 6.9:1 and required 100/130 aviation gasoline. It was rated at 1,500 horsepower at 2,400 r.p.m., and 1,700 horsepower at 2,500 r.p.m. It was 5 feet, 3.1 inches (1.603 meters) long, 4 feet, 6.26 inches (1.378 meters) in diameter and weighed 1,980 pounds (898 kilograms). Only four of these engines were built.
NX14936 was sold to the British Overseas Airways Corporation (BOAC) in September 1941 and registered in the United Kingdom as G-AGDI. The airline named it St. Louis. It was converted to a 24-passenger configuration with long-range fuel tanks. It frequently flew between Lisbon, Gibraltar and Malta. The airplane was scrapped 29 October 1943.
After the necessary redesign, which included a large cargo door and strengthened floor, and the substitution of 2,000 horsepower Pratt & Whitney R-2800-51 engines for the Wright Cyclone 14s of the C-55, the Army Air Forces ordered the airplane into production as the C-46A-CU Commando. An order was placed for 200 aircraft. The U.S. Navy placed 160 in service as the R5C-1. Curtiss-Wright built the C-46 at St. Louis and Buffalo, New York. The first, 41-5159, was delivered 13 July 1942. More than 3,000 C-46s were built in nearly 30 variants. Two C-46A-1-HI Commandos were built by Higgins Aircraft at Michoud, Louisiana.
Like the CW-20T, the C-46A/R5C-1 was also 76 feet, 4 inches (23.266 meters) long with a wingspan of 108 feet, 0 inches (32.918 meters) and overall height of 21 feet, 8 inches (6.604 meters). The wing area was 1,360 square feet (126.35 square meters). It had an empty weight of 30,241 pounds (13,717 kilograms) and maximum take off weight of 52,000 pounds (23,586 kilograms). The maximum payload was 10,000 pounds (4,536 kilograms). The maximum package size was 7 feet, 6 inches × 5 feet × 6 feet, 8 inches (2.286 × 1.524 × 2.032 meters).
The C-46A was powered by two air-cooled, supercharged, 2,804.4-cubic-inch-displacement (45.956 liter), Pratt & Whitney R-2800-51 two-row, 18-cylinder radial engines with a compression ratio of 6.65:1. They drove three-bladed propellers through a 2:1 gear reduction. These engines had a Normal Power rating of 1,600 horsepower at 2,400 r.p.m. at 5,700 feet (1,737 meters), or 1,400 horsepower at 13,000 feet (3,962 meters). The Military Power rating was 2,000 horsepower at 2,700 r.p.m. at 1,500 feet (457 meters), or 1,600 horsepower at 13,500 feet (4,115 meters). Takeoff power was 2,000 horsepower at 2,700 r.p.m. The R-2600-51 was 6 feet, 3.72 inches (1.923 meters) long, 4 feet, 4.50 inches (1.335 meters) in diameter, and weighed 2,300 pounds (1,043 kilograms). All R-2600-51s were built by the Ford Motor Company.
The C-46A had a maximum speed of 233 knots (268 miles per hour/432 kilometers per hour) at 16,100 feet (4,907 meters). Its service ceiling was 20,600 feet (6,279 meters). With a fuel capacity of 3,000 gallons (11,356 liters), the maximum range was 1,960 nautical miles (2,256 statute miles/3,630 kilometers) at 121 knots (139 miles per hour/224 kilometers per hour).
During World War II, the C-46 famously flew “The Hump,” from bases in Burma, over the Himalaya Mountains, and into China.
¹ The United States Army Air Corps (USAAC) became the United Army Air Forces (USAAF) on 20 June 1941.
Buffalo, N.Y., January 24—(AP)—A Curtiss Hawk 75A pursuit plane, one of 100 being constructed for the French Government, has “substantially exceeded all known speed records” with a free dive of more than 575 miles an hour, it was announced today.
The speed mark was established yesterday while the ship was undergoing acceptance tests, officials of the Curtiss Aeroplane Division of the Curtiss Wright Corporation said.
The tests were made by H. Lloyd Child, chief test pilot of the Buffalo Curtiss plant, who said he “felt no ill effects and did not realize” that the speed was presumably the fastest man has ever traveled.”
National Aeronautic Association officials said that no Federation Aeronautique Internationale records “even approached this speed.”
The speed of the dive was so great that the marker on the recording airspeed indicator exceeded the instrument’s range and moved off the paper on which the graph of the dive was recorded.
Aviation experts, who declined to be quoted directly, estimated that the speed might have exceeded 600 miles per hour, compared with the normal falling rate for a 170-pound man of 150 miles an hour.
The dive was begun at an altitude of 22,000 feet, and the record speed was attained during a 9,000 foot dive.
At no time during the dive, Child said, did the engine exceed 2,550 revolutions a minute, its normal rated speed in level flight. Hence, he explained, the strain on the motor during the dive was not increased, but was held to the speed of normal operation by the Curtiss electric propeller, with its unlimited blade pitch range.
Since the motor’s speed was kept at normal during the dive, it was a “free,” rather than a “power” dive as when the motor throttle is opened wide, aviation experts explained.
Previously, company officials explained, a limiting factor in the speed at which an airplane could dive was the engine’s revolutions each minute, since overspeeding would result to serious damage to the motor.
The Curtis Hawk 75A pursuit plane is similar to the Curtiss P-36A, the standard pursuit airplane of the United States Army Air Corps.
It carried two machine guns and is equipped to carry bombs under each wing when on a fighting mission.
The greatest previously registered speed was 440.681 miles an hour, made by Francesco Agello of Italy over a three-kilometer course in level flight October 23, 1934.
The world’s land speed record is held by George E. T. Eyston of England at 357.5 miles an hour, established September 16, 1938.
—The Cincinnati Enquirer, Vol. XCVIII, No. 291, Wednesday, January 25, 1939, at Page 1, Columns 1 and 2
The Oakland Tribune reported:
‘Faster Than Any Man Alive,’ Flier Says After Diving 575 M.P.H.
BUFFALO, N.Y., Jan. 25.—(AP)—A test pilot who free-power dived a heavily armed pursuit airplane at more than 575 miles per hour claimed today the distinction of having traveled “faster than any other human being.”
Chief test pilot H. Lloyd Child dropped a Curtiss Hawk 75A through the clouds above Buffalo Airport yesterday at almost 1000 feet a second to exceed “all known speed records,” the Curtiss aeroplane division of the Curtiss-Wright Corporation announced.
Child was testing the plane for the French Army, which has purchased 100 of the ships. The terrific speed was recorded on instruments installed by the French Government’s representatives, who witnessed the flight.
The velocity was so great the marker on the indicator exceeded the instrument’s range and moved off the paper roll. Aviation experts said Child probably exceeded 600 miles per hour.
“I didn’t feel anything,” the test pilot commented, “it was all over too quickly.”
Child said the dive was part of a day’s work.
“No danger at all, I would say,” he commented.
His spare time hobby, skiing, however, “is awful dangerous,” Child asserted.
“I wouldn’t be surprised if someone would exceed my speed soon. A diving speed of 700 miles per hour is within the realm of possibility,” he added.
—Oakland Tribune, VOL. CXXX—NO. 25, Wednesday, January 25, 1939, Page 3, Columns 2 and 3
The Curtiss-Wright Model 75 was a single-seat, single-engine, low wing monoplane with retractable landing gear. The airplane was designed by Donovan Reese Berlin. Curtiss-Wright intended to offer it as a pursuit for the U.S. Army Air Corps. H. Lloyd Child took the prototype, X17Y,¹ for its first flight 6 May 1935.
After evaluation by the Air Corps at Wright Field, the rival Seversky Aircraft Corporation SEV-1XP was selected by the Air Corps and 77 P-35s were ordered. Don Berlin worked on improving the Model 75, and in 1937, the Air Corps ordered 210 Curtiss P-36As.
Curtiss-Wright also offered versions of the Hawk 75 to foreign governments. Variants were available with fixed or retractable gear, a choice of Pratt & Whitney Twin Wasp or Wright Cyclone engines, and various combinations of machine gun and cannon armament.
The Curtiss Hawk 75 A was 28.8 feet (8.78 meters) long with wingspan of 37.3 feet (11.37 meters) and height of 9.25 feet (2.82 meters). The total wing area was 236.0 square feet (21.93 square meters). With a Pratt & Whitney engine, the airplane had an empty weight of 4,713 pounds (2,127.3 kilograms), and gross weight of 5,922 pounds (2,675.7 kilograms).
The Armée de l’air initially ordered 100 Hawk 75A-1s, designated H75-C1 in French service. Pratt & Whitney Twin Wasp engines (including spares) were ordered separately. They were delivered to France for final assembly, and were unpainted. These airplanes had minor differences from U.S. Army Air Corps P-36As. For example, the instrument markings were metric. It was French custom to have the throttle off when pushed full forward, and wide open when pulled rearward. The pilot’s seat was different in order to fit the standard French parachute.
The French H75-A1 was powered by an air-cooled, supercharged, 1,829.39-cubic-inch-displacement (29.97 liter) Pratt & Whitney Twin Wasp SC-G [Specification Number PW-5028-C]. This was a two-row 14-cylinder radial engine with a compression ratio of 6.7:1. The SC-G was rated at 900 horsepower at 2,550 r.p.m. at 11,000 feet (3,353 meters), and 1,050 horsepower at 2,700 r.p.m., for take off. The engine drove a three-bladed, 10 foot, 1½ inch (3.086 meters) diameter Curtiss Electric constant-speed propeller through a 16:9 gear reduction. The SC-G was 48.00 inches (1.219 meters) in diameter, 59.90 inches (1.521 meters) long, and weighed 1,423 pounds (645 kilograms).
The Hawk 75A-1 had a maximum cruise speed of 260 miles per hour (418 kilometers per hour) at 19,000 feet (5,790 meters). Its maximum speed was 258 miles per hour (413 kilometers per hour) at Sea Level, 290 miles per hour at 8,200 feet (2,500 meters), and 303 miles per hour (488 kilometers per hour) at 19,000 feet (5,790 meters). Although Child demonstrated a dive at over 575 miles per hour, in service, the Hawk was restricted to a maximum dive speed of 455 miles per hour (732 kilometers per hour). The airplane had a service ceiling of 32,800 feet (9,997 meters), and absolute ceiling of 33,700 feet (10,272 meters).
The Armée de l’air H75A-1 was armed with four FN-Browning de Belgique mle 1938 7.5 mm. × 54 mm MAS machine guns, with two mounted on the engine cowl, synchronized to fire through the propeller arc, and one in each wing. 2,200 rounds of ammunition were carried. The 7.5 mm (the bullet diameter was actually 7.78 mm, or .306-caliber) was a shorter, less powerful cartridge than the .303 British (7.7 × 56 mm) or U.S. standard .30-06 Springfield (7.62 × 63 mm) cartridges.
France followed with orders for Hawk 75A-2, 75A-3 and 75A-4 fighters. These had different combinations of guns and engine variants.
After the surrender of France to invaders from Nazi Germany, many Curtiss Hawks made their way to England. In service with the Royal Air Force, these airplanes were called the Mohawk.
Henry Lloyd Child was born at Philadelphia, Pennsylvania, 25 May 1904, the second of two children of Edward Taggart Child, a consulting engineer in shipbuilding, and Lillian Rushmore Cornell Child. He was baptized at the Church of the Good Shepherd, Rosemont, Pennsylvania, 22 December 1913. Child graduated from Flushing High School in Flushing, New York, then attended the Haverford School in Philadelphia.
“Skipper” Child majored in mechanical engineering at the University of Pennsylvania where he was a member of the Hexagon Senior Engineering Society and the Phi Sigma Kappa (ΦΣΚ) and Sigma Tau (ΣΤ) fraternities. He was a member of the varsity and all-state soccer team, and also played football and tennis. Child graduated with a bachelor of science degree, 15 June 1926.
After graduation from college, Child went to work for the Curtiss-Wright Corporation as an engineer.
Child joined the United States Navy, 23 November 1927. He was trained as a pilot at Naval Air Station Hampton Roads, Norfolk, Virginia, and was commissioned as an Ensign. He was promoted to lieutenant (junior grade), 7 November 1932, and to lieutenant, 11 November 1935.
While maintaining his commission in the Navy, Child returned to Curtiss-Wright as a test pilot.
Henry Lloyd Child married Miss Allene Ann Gausby of Hamilton, Ontario, Canada, 28 October 1939. They had met in July 1938, while playing in a tennis tournament at Muskoka, Northern Ontario. They would have a daughter, Beverley L. Child.
H. Lloyd Child worked for Lockheed from 1958 to 1968, when he retired. He died at Palmdale, California 5 August 1970 at the age of 66 years.
¹ At this time, American experimental aircraft were prohibited from carrying the national identifier, “N-,” to lead their registration mark.
27 July 1934: While Ellen Evalyn Church is recorded as the first airline flight attendant, or “stewardess,” Fräulein Nelly Hedwig Diener was Europe’s first airline hostess. At the age of 22 years, she began flying for Swissair Schweizerische Luftverkehr-AG on 1 May 1934. She was known as the Engel der Lüfte (“Angel of the Skies”).
Her 79th flight departed Zürich-Dübendorf Airport enroute Stuttgart-Echterdingen Airport and then on to Berlin. The pilot was Armin Mühlematter and radio operator/navigator was Hans Daschinger. There were nine passengers on board.
The airliner was a Curtiss-Wright Airplane Division AT-32C Condor II, a one-of-a-kind variant of the AT-32 which was built specifically for Swissair. It carried identification number CH-170 on its wings and fuselage. The airliner was registered HB-LAP.
The Condor was flying in a thunderstorm at approximately 3,000 meters (9,843 feet) when the right wing structure failed and separated from the airplane. CH-170 crashed into a forest between Wurmlingen and Tuttlingen, Germany, and caught fire. All twelve persons aboard were killed.
Investigators found that a fracture had developed in the welded structure of the engine mount and wing. It was believed that it was caused by defective construction and welding techniques combined with vibration of the engine. A second fracture was caused by the violent weather.
This accident was the first for Swissair, the national airline of Switzerland.
CH-170 was one of 45 T-32 Condor II airplanes built by Curtiss-Wright for use as both a civil transport and a military transport or bomber. It was a twin-engine, two-bay biplane with retractable landing gear. CH-170 was purchased by Swissair 11 April 1934, and entered service 28 March 1934. The airliner was configured with 15 passenger seats.
The AT-32C was 49 feet, 1-1/8 inch (14.049 meters) long with an upper wingspan of 85 feet, 0 inches (25.908 meters) and lower wing span of 74 feet, 0 inches (22.555 meters), and height of 16 feet, 4 inches (4.953 meters). Both wings had a chord of 8 feet, 10.5 inches (2.705 meters). The total wing area was 1,331 square feet (123.65 square meters). The vertical gap between the upper and lower wings was 9 feet, 11 inches (3.023 meters). There was no stagger. Upper and lower wings had an angle of incidence of 1°. The center sections were straight, but outboard of the engines, they had 2¼° dihedral. ¹
CH-170 had an empty weight of 11,446 pounds (5,192 kilograms) and gross weight of 16,800 pounds (7,620 kilograms).
The AT-32C was powered by two air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.875 liter) Wright Cyclone SR-1820-F3 ² single-row nine-cylinder radial engines with a compression ratio of 6.4:1. They were rated at 675 horsepower at 1950 r.p.m., each, and required 87-octane aviation gasoline. These were direct-drive engines, turning three-bladed variable-pitch propellers. The SR-1820-F3 was 3 feet, 7.375 inches (1.102 meters) long, 4 feet, 5.75 inches (1.365 meters) in diameter and weighed 937 pounds (425 kilograms). The engines were enclosed in NACA cowlings, rather than the Townend rings of earlier T-32-series airplanes.
The AT-32C had a cruising speed of 235 kilometers per hour (146 miles per hour) and maximum speed of 274 kilometers per hour (170 miles per hour). The service ceiling was 4,000 meters (13,123 feet) and its range was 800 kilometers (497 miles).
¹ Data from three-view drawings of Richard E. Byrd’s Curtiss-Wright T-32 Condor, c/n 41, drawn by Paul R. Matt, 1965.