31 December 1908: At Camp d’Auvours, 11 kilometers (6.8 miles) east of Le Mans, France, Wilbur Wright flew a 1907 Wright Flyer a distance of 124.7 kilometers (77.48 miles) over a triangular course in 2 hours, 20 minutes, 23 seconds, setting a record for duration and distance. He won the first Michelin Trophy and a ₣20,000 prize.
The International Michelin Trophy was a prize given over eight years by Michelin et Cie, the French tire company, to the Aéro-Club de France, to award on behalf of the Fédération Aéronautique Internationale. The winner would be the pilot who by sunset, 31 December of each year, held the record which had been established by the Aéro-Club. The actual trophy would be given the aeronautical club whose members had won the most times during the eight year period. ₣160,000 was to be divided and presented to each winning pilot.
The Wright Model A, produced from 1907 to 1909, was the world’s first series production airplane. It was slightly larger and heavier than the Wright Flyer III which had preceded it. It was a two-place, single-engine canard biplane built of a wooden framework braced with wires and covered with muslin fabric. A new system of flight controls allowed the pilot to sit upright rather than lying prone on the lower wing.
The dual horizontal elevators were placed forward and the dual vertical rudders aft. The biplane was 31 feet (9.449 meters) long with a wingspan of 41 feet (12.497 meters). The wings had a chord of 6.6 feet, and vertical separation of 6 feet. The airplane had an empty weight of approximately 800 pounds (363 kilograms).
The Model A was powered by a single water-cooled, fuel-injected, 240.528 cubic-inch-displacement (3.942 liter) Wright vertical overhead-valve inline four-cylinder gasoline engine with 2 valves per cylinder and a compression ratio of 4.165:1. It produced 32 horsepower at 1,310 r.p.m. During three years of production (1908–1911) Wright “4-40” engines were built that operated from 1,325 to 1,500 r.p.m. Power output ranged from 28 to 40 horsepower. These engines weighed from 160 to 180 pounds (72.6–81.6 kilograms).
Two 8½ foot (2.591 meters) diameter, two-bladed, counter-rotating propellers, driven by a chain drive, are mounted behind the wings in pusher configuration. They turned 445 r.p.m.
The Wright Model A could fly 37 miles per hour (60 kilometers per hour).
11 December 1917: Katherine Stinson flew her custom-built Curtiss-Stinson Special from Rockwell Field, North Island, San Diego to the Presidio of San Francisco, a distance of 606 miles (975 kilometers)¹ in 9 hours, 10 minutes. This was a new American duration distance record.
Of her flight, she later said “It was easy to tell where I was all the time . . . towns, cities, farms, hills and mountains passed rapidly. . . . I never had any fear. The main thing was speed.”
A contemporary magazine article described her flight:
MISS STINSON FLIES OVER TEHACHAPI MOUNTAINS
Under the auspices of the Pacific Aero Club, Katherine Stinson, on December 11, flew from North Island, San Diego, to the Presidio at San Francisco via inland route, crossing the Tehachapi mountains at 8,000 feet [2,438 meters]. The official distance covered is 460.18 miles [740.59 kilometers]. Time, nine hours, ten minutes; non-stop flight. Left North Island at 7.31 a.m., flew over Tehachapi mountains at 8,000 feet, arrived at San Francisco at 4:41 p.m.
The flight was observed and timed at San Diego by Captain Henry Abbey and Captain Dean Smith, United States Army aviators, and was accompanied as far as Ocean Side by Theodore McCauley, Army Instructor, who piloted a Curtiss reconnaissance machine; the finish was observed and timed by Rear Admiral Chas. F. Pond, U.S.N., President of the Pacific Aero Club; Lowell E. Hardy, Secretary; J.C. Irvine, official observer, Aero Club of America; Robert G. Fowler, Chas F. Craig, and F.C. Porter of the Contest Committee Pacific Aero Club. She was given a very a very hearty reception by thousands of soldiers at the Presidio upon her arrival.
The aeroplane used was built by Curtiss from two lower wings of Curtiss J.N. 4 with triplane fuselage, Curtiss OX2 90–100 H.P. engine.
Miss Stinson is now the only living aviator to fly over the Tehachapi mountains. Silas Christofferson, deceased, was the only other aviator to perform the feat. The performance does not break the American record for distance held by Miss Ruth Law, but establishes a new record for duration cross country flight and is a most remarkable performance.
Katherine Stinson was born 14 February 1891 at Fort Payne, Alabama. She was the first of four children of Edward Anderson Stinson, an electrical engineer, and Emma Beavers Stinson. Deciding to learn to fly, she sold the family’s piano to pay for flying lessons. In 1912 she became the fourth woman in the United States to become a licensed pilot. Later, her younger sister, Marjorie, also learned to fly. In 1913, Katherine and her mother formed the Stinson Aviation Company at Hot Springs, Arkansas.
After the family moved to San Antonio, Texas, the sisters taught at the Stinson School of Flying at Stinson Field (now, Stinson Municipal Airport, FAA location identifier SSF).
During World War I, Katherine Stinson flew exhibitions on the behalf of the American Red Cross, raising more than $2,000,000. She attempted to join the Army as a pilot, but instead was sent to Europe as an ambulance driver.
While “over there,” she contracted influenza, and later, tuberculosis. Although she survived and lived a long life, her illness prevented her from continuing to fly. She moved to Santa Fe, new mexico, for its high, dry climate. Although she lacked a professional education, she he became a successful architect in Santa Fe, New Mexico, designing residences in the Spanish Pueblo Style.
in 1928, Stinson married Judge Miguel Antonio Otero, Jr., son of the former governor of New Mexico. They would adopt her deceased brother Edward’s four children.
Katherine Stinson Otero died at her home in Santa Fe, 8 July 1977, at the age of 86 years. She is buried at the Santa Fe National Cemetery.
“Fear, as I understand it, is simply due to lack of confidence or lack of knowledge—which is the same thing. You are afraid of what you don’t understand, of things you cannot account for.”
The Curtiss-Stinson Special was built by the Curtiss Aeroplane and Motor Company, specially for Katherine Stinson. It was a single-place, single-engine, two-bay biplane intended for exhibition flights. The Special used the fuselage of a Model 10 Speed Scout fighter, new wings, and the tail surfaces of the JN-4 “Jenny.” It was powered by a water-cooled, normally-aspirated, 567.45-cubic-inch-displacement (9.299 liters) Curtiss OXX-6 single-overhead-camshaft (SOHC) 90° V-8 engine, rated at 100 horsepower at 1,400 r.p.m. A replica of this one-of-a-kind airplane is in the Alberta Aviation Museum, Edmonton, Alberta, Canada.
¹ Some sources cite a distance for Stinson’s flight of 610 miles or 981.5 kilometers. The Google Maps Distance Calculator puts the straight line distance between North Island and the Presidio at 461.606 miles (742.883 kilometers).
19 April 1919: Captain Earl French White, Air Service, United States Army, and H.M. Schaffer, “his mechanician,” took off from Ashburn Aviation Field, Chicago, Illinois, at 9:50 a.m, Central Standard Time, in the Dayton-Wright DH-4, Air Service serial number A.S. 30130. At 5:40 p.m., Eastern Standard Time, the airplane and its two-man crew landed at Hazelhurst Field, Mineola, Long Island, New York. They flew 738.6 miles (1,188.7 kilometers) in 6 hours, 50 minutes at an average speed of approximately 106 miles per hour (170.6 kilometers per hour).
The New York Times reported the event on its front page on the following day:
. . . Captain White had great difficulty in taking to the air in the soft ground of Ashburn Field, the take-off grounds approved by the Aero Club of Illinois. The ground there was soft and the heavy army plane, with her load of more than 190 gallons[719.2 liters] of gasoline, cut into it deeply, but after the aviator had had his plane dragged to a drier and harder spot in the field he managed to take to the air.
Circling over Chicago, Captain White ascended to a height of more than 10,000 feet [3,048 meters] and throughout his flight he did not go below this level until he was ready to land, and at intervals he flew as high as 12,000 feet[3,658 meters]He followed the route of the New York Central Railroad for the greater part of the distance, and cities along the route reported seeing him flying at great height and at high speed.
About 5 o’clock yesterday persons visiting on the ships of the Atlantic Fleet in the Hudson River and pedestrians on Riverside Drive saw a dark blue airplane come down from the north at high speed, turn sharply to the east when it was about opposite Fiftieth Street and then gradually came to a lower level as it circled about over the city.
All thought it was only one of the many airplanes and seaplanes that take their daily practice flights over the Hudson River and Manhattan Island, but it was Captain White and the first Chicago-New York non-stop airplane, bearing the army number 30,130.
Plane a Standard Army Machine.
After sailing over the city for about ten minutes, Captain White turned his machine toward the army aviation field at Mineola, where he landed at about 5:40 o’clock. Colonel Archibald Miller, Director of Aviation in the Department of the East and one of the commanders of the Hazelhurst Field, was waiting there to meet captain White and his mechanician, H.M. Schaefer, and they were taken to the field headquarters where an informal reception was held.
Officers at the Hazelhurst Field said that the biplane used by Captain White in his flight was one of the standard De Havilland Four machines constructed for the use of the army in France, and that it was equipped with a twelve-cylinder Liberty motor of about 400 horsepower.
— The New York Times, 20 April 1919, Page 1, Column 4, and continued on Page 9.
Captain White’s flight was observed by members of the Aero Club of America. The time of White’s departure from Chicago was telegraphed to New York. The flight was certified by the Aero Club, which represented the Fédération Aéronautique Internationale (FAI) within the United States. This was the first non-stop flight between Chicago and New York, and was the longest non-stop flight that had been made anywhere in the world up to that time.
The Dayton-Wright Airplane Company DH-4 was a variant of the British Airco DH.4, designed by Geoffrey de Havilland (and commonly known as the de Havilland DH.4). It was a two-place, single-engine biplane intended as a bomber, but served in virtually every capacity during World War I and the years following.
American-built DH.4 airplanes were produced by the Boeing Airplane Company, Dayton-Wright Airplane Company, Fisher Body Corporation, and Standard Aircraft Corporation. Most were powered by the Liberty L12 engine. Following World War I, many DH-4s were rebuilt by Boeing and Atlantic Aircraft. An improved version, the DH-4M, used a tubular steel framework instead of the usual wood construction. DH-4s remained in service with the United States Army as late as 1932. At McCook Field, Dayton, Ohio, the U.S. Army’s aviation engineering center, DH-4s were commonly used as test beds for engines and other aeronautical equipment.
The Airco DH.4 had a crew of two. It was 30 feet, 8 inches (9.347 meters) long with a wingspan of 43 feet, 4 inches (13.208 meters) and height of 11 feet (3.353 meters). Empty weight was 2,387 pounds (1,085 kilograms) and loaded weight was 3,472 pounds (1,578 kilograms). British-built DH.4s were powered by a 1,239-cubic-inch-displacement (20.32 liter) liquid-cooled Rolls-Royce Eagle overhead cam 60° V-12 engine which produced 375 horsepower. A gear-reduction system kept propeller r.p.m. below engine speed for greater efficiency.
The Liberty L12 aircraft engine was designed by Jesse G. Vincent of the Packard Motor Car Company and Elbert J. Hall of the Hall-Scott Motor Company. It was a water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Liberty L-12 single overhead cam (SOHC) 45° V-12 engine with a compression ratio of 5.4:1. The Liberty produced 408 horsepower at 1,800 r.p.m. The L-12 as a right-hand tractor, direct-drive engine and it turned turned a two-bladed fixed-pitch wooden propeller. The Liberty 12 was 5 feet, 7.375 inches (1.711 meters) long, 2 feet, 3.0 inches (0.686 meters) wide, and 3 feet, 5.5 inches (1.054 meters) high. It weighed 844 pounds (383 kilograms). This engine was produced by Ford Motor Company, as well as the Buick and Cadillac Divisions of General Motors, The Lincoln Motor Company (which was formed by Henry Leland, the former manager of Cadillac, specifically to manufacture these aircraft engines), Marmon Motor Car Company and Packard. Hall-Scott was too small to produce engines in the numbers required.
Dayton-Wright DH-4, U.S. Army Air Service serial number A.S. 30130, was built at the Dayton-Wright Airplane Company factory in 1918. It was used for engineering tests at McCook Field, and carried project number P78 painted on its rudder. What became of the airplane after Captain White left it at Hazelhurst Field is not known.
Hazelhurst Field was renamed Roosevelt Field in 1920, in honor of Lieutenant Quentin Roosevelt, 95th Aero Squadron, son of former President Theodore Roosevelt, who was killed in aerial combat during World War I.
Earl French White was born at Minneapolis, Minnesota, 12 July 1888. He was the son of Clarence Otis White, a manufacturing engineer, and Harriet (“Hattie”) Isabel French White. He enlisted in the United States Army, 8 October 1910, and was assigned to the 11th Cavalry Regiment at Fort Myer, Virginia. In 1915 he transferred to the Aviation Section, Signal Corps. He completed flight training 27 March 1917.
Earl French White was commissioned as a Captain, Aviation Section, Signal Corps, United States Army, on 8 November 1917, and qualified as a Reserve Military Aviator in January 1918. In August 1918, Captain White was assigned to Wilbur Wright Field, Dayton, Ohio, and later, the Technical Flying Field in Dayton.
On 1 July 1919, Captain White was one of three pilots who flew the inaugural U.S Air Mail Service route from New York City, New York, to Chicago, Illinois. Captain White flew a DH-4 on the route segment from Bellefonte, Pennsylvania, to Cleveland, Ohio. He carried 6 pouches containing 330 pounds (150 kilograms) of mail, and arrived at Cleveland at 9:30 a.m.
Earl French White married Miss Mary Esther Edmondson at Sarasota, Florida, 26 February 1923. Miss Edmondson had served in France during World War I as a civilian aide with the American Red Cross. They would have a daughter, Patricia.
From 14 April 1923 to 30 June 1925, White flew for the U.S. Air Mail Service at Bellefonte, Pennsylvania, North Platte and Omaha, Nebraska, and Cheyenne, Wyoming. He flew scheduled night air mail from July 1924 to July 1925.
From 1928 to 1931, Earl White was a pilot for Pan American Airways in the Caribbean area.
In 1935, White was employed by William Kissam Vanderbilt II to fly his Sikorsky S-43 amphibian, NC-16825. Vanderbilt described White as “one of the most reliable and resourceful aviators in the game.”
As of 11 February 1937, White had logged a total of 5,370 hours, 50 minutes, of flight time.
During World War II, White was employed as a delivery pilot for the Consolidated Aircraft Corporation.
12 April 1918: Allan and Malcolm Loughead, owners of the Loughead Aircraft Manufacturing Company of Santa Barbara, California, set speed and distance records as they flew their twin-engine, ten-place F-1 flying boat from Santa Barbara to San Diego. The F-1 traveled 211 miles in 3 hours, 1 minute.
Designed by friend and employee John Knudson (“Jack”) Northrop, and built in a garage on State Street, the F-1 was launched on a wooden ramp at West Beach.
The airplane was intended for the U.S. Navy, but the end of World War I ended the requirement for new airplanes.
The Loughead F-1 was a twin-engine, three-bay biplane flying boat operated by a crew of 2. It could carry 8–10 passengers. The airplane was 35 feet (10.668 meters) long. The span of the upper wing was 74 feet (22.555 meters) and the lower wing was 47 feet (14.326 meters). The height was 12 feet (3.658 meters). The F-1 had an empty weight of 4,200 pounds (1,905 kilograms) and gross weight of 7,300 pounds (3,311 kilograms).
The F-1 was powered by two right-hand tractor, water-cooled, normally-aspirated 909.22-cubic-inch-displacement (14.899 liters) Hall-Scott A-5-engines. These were inline six-cylinder single-overhead-camshaft (SOHC) engines with a compression ratio of 4.6:1. It was rated at 150 horsepower and produced 165 horsepower at 1,475 r.p.m. The engines were mounted on steel struts between the upper and lower wings. The engines were direct-drive and turned two-bladed, fixed pitch propellers with a diameter of 8 feet, 8 inches (2.642 meters). The Hall-Scott A-5-a was 5 feet, 2.5 inches (1.588 meters) long, 2 feet, 0 inches (0.610 meters) wide and 3 feet, 7.875 inches (1.114 meters) high. It weighed 595 pounds (270 kilograms).
The F-1 had a cruise speed of 70 miles per hour (113 kilometers per hour) and maximum speed of 84 miles per hour (135 kilometers per hour).
The F-1 was converted to a land plane with tricycle undercarriage and redesignated F-1A. During an attempted transcontinental flight, it twice suffered engine failure and was damaged. Reconfigured as a flying boat, the airplane was used for sight-seeing before being sold. It was abandoned on a beach at Santa Catalina Island, off the coast of Southern California, and was eventually destroyed.
The Loughead Aircraft Manufacturing Company would go on to become one of the world’s leading aerospace corporations.