Tag Archives: Fédération Aéronautique Internationale

12 June 1922

Albert William Stevens (Belfast Historical Society and Museum)

12 June 1922: Captain Albert William Stevens, Air Service, United States Army, made a high altitude parachute jump from a twin-engine Martin GMB bomber flying at 24,206 feet (7,378 meters) over McCook Field, Ohio.

A contemporary magazine article described the jump:

The greatest recorded parachute jump made from an airplane was accomplished by Capt. Albert W. Stevens a year or more ago. He fell 24,200 feet—almost five miles—landing 25 miles away from the point above which he jumped and suffering no injury in his descent, beyond a couple of dislocated toes.

Popular Science Monthly, November 1924, Vol. 105, No. 5, at Page 152, Column 2.

The Army and Navy Register published this very informative report:

PARACHUTING FROM 24,206 FEET

     Hurtling four and one-half miles through space was the recent experience of Capt. A. W. Stevens, Air Service, stationed at McCook Field, Dayton Ohio, in a parachute jump on June 12 last from the high altitude of 24,206 feet from a supercharged Martin bomber, piloted by Lieut. Leigh Wade, with Sergeant Roy Lanham as the other passenger. Capt. Stevens’ fall lasted approximately 20 minutes, and the oscillations of the chute, due to the prevailing winds, made him thoroughly seasick by the time half of the descent was over. In his official report to the chief of the Air Service, Capt. Stevens says:

    “The pack-cord was ripped about ten feet below the fuselage of the bomber. The parachute opened instantly and was fully open in less than 100 feet below the plane (estimated). The writer has made several jumps before, viz., from 1,500 feet, at 85 miles per hour; 1,500 feet at 65 miles per hour, and 5,600 feet at 65 miles per hour. Although the plane speed is estimated by the pilot at 110 miles per hour, the shock of opening was less, if anything, than on the previous jumps by the writer at lower altitudes and speed—due very likely to the lower density of the atmosphere.

     “The writer had complete confidence that the parachute would open fully—sooner or later. The only question with him was whether the passage of the silk fabric through the cold, rarefied upper air might generate enough static electricity to hold the folds of the ‘chute tight together for a time, until when it did open the shock might result in a rupture, either of the operator’s body, or of the shroud lines. This fear was groundless as the ‘chute opened instantly—or practically so. The ‘chute used had the vents sewed right; it had been tested with both 100 and 200-pound weights in the usual manner over McCook Field from about 600 feet altitude.

     “The time of descent was not over 20 minutes, from the writer’s estimate. It may have been less than 20 minutes, but was over 15 minutes. The writer would like to make another jump from still higher altitude, 40,000 feet or more, when he recovers from a few broken foot bones, and if this is done, a recording barograph will be carried as part of the jumper’s equipment. Needless to say, a comparatively windless day is best to choose for a thing of this kind, as the ‘chute may get caught in a down current on a windy day and land twice as hard as usual. Also, the jumper from high altitudes is burdened with heavy flying clothing, which increases his weight considerably.

     “Attention is called to the fact that the parachute averaged a ground speed of one and one-half miles a minute, based on a travel of 30 miles and a time of descent of less than 20 minutes. The ordinary time of descent is about 1,000 feet per minute at ordinary altitudes; for instance, in the 5,600-foot jump previously referred to, the time was six minutes. In the thin upper air the ‘chute undoubtedly falls faster, especially when it is oscillating and spilling air, as was the case all the way down on the recent jump.

     “Ten minutes of such oscillation will upset anything but a cast-iron stomach. In the writer’s case, he was thoroughly seasick by the time half of the descent was over. He could get little relief by closing his eyes, and if his eyes were open the landscape below heaved and tipped in all directions. It is of interest to note that temporary relief was experienced by fixing the eyes for a few seconds on the center of the parachute, this being the only point in space reasonably at rest with respect to the body of the jumper.

     “It is inadvisable to open the second ‘chute for the purpose of checking oscillation, as one then loses control of movement. With a single ‘chute it is possible to change the direction of one’s flight very considerably, even on a windy day. On a calm day one can do much better, even to the extent of picking out a particular field in which to land. On a windy day the air currents carry you irresistibly ahead, and the best that can be done is to side-slip to the right or to the left of the line of flight.

     “About the land: if one imagines that he has just jumped from a twelve-foot wall and crouches in a jumping position, he will be in the best position for landing. Too great a tension of the leg muscles may result in ruptured tendons or broken foot bones. You are sure to collapse in a pile on the ground; it is better to relax with that in view, and thereby get a more even distribution of bruises. The jumper should face the way he is traveling; to accomplish this it is possible to make the ‘chute revolve, earlier in the drop, by taking a few of the shroud lines and pulling diagonally, with the idea of working a “propeller” surface into one point of the ‘chute circumference. The second ‘chute may be pulled about 50 to 75 feet before landing, chiefly to get rid of the extra weight. If pulled earlier, the two ‘chutes will soon stand well apart, at 60 degrees or more, and will spill air between them, so that the jumper will fall nearly as fast as ever, and with practically no control.

     “The bomber carried four recording barographs, as well as indicating altimeters. The result of McCook Field laboratory measurements showed that the elevation was 24,206 feet.

     “It was the intention of Lieut. Wade to take the plane, relieved of 250 pounds of weight, still higher, but one of the superchargers developed trouble and it was necessary to cut the flight short.”

ARMY AND NAVY REGISTER, The U.S. Military Gazette, Vol. LXIII, No. 2195, 12 August 1922 at Page 162

1st Lieutenant Albert William Stevens, Air Service, United States Army, circa 1921. Lieutenant Williams is wearing the badge of an aerial observer. The decoration beneath is the Victory Medal with four campaign stars. (Albert W. Stevens Collection)

Albert William Stevens (née Whitten) was born at Belfast, Maine, 13 March 1886, the third child of Nathan Whitten, a blacksmith and wagon builder, and Alice C. Anderson Whitten. His mother died of “consumption” (tuberculosis) when Albert was five months old. He was adopted by Albert J. Stevens and Nancy M. Trimble Stevens, and his name became Albert William Stevens.

Stevens attended the University of Maine at Orono, Maine. He graduated in 1907 with a Bachelor of Science (B.S.) degree. He earned a Masters degree in electrical engineering  from the university in 1909. He then worked as a mining engineer in Alaska, California, Idaho and Montana.

Stevens enlisted in the U.S. Air Service in Idaho, January 1918. Because of his experience in photography, which began while he was in college, Stevens was assigned to the Aerial Photography School at Cornell University, Ithaca, New York. He was commissioned as a First Lieutenant, Aviation Section, Signal Officers Reserve Corps, 18 February 1918. Sent to Europe as part of the American Expeditionary Forces, Stevens commanded the 6th Photo Section, 88th Aero Squadron. He flew in the major campaigns of the final months of the War.

In this photograph of officers of the 88th Aero Squadron in France, 1918, Lieutenant Stevens is in the front row, fifth from right. The airplane is an Avion Salmson Type 2 A.2. (United States Air Force)

He was an acknowledged expert in the field of aerial photography. Lieutenant Stevens was wounded and awarded the Purple Heart. Following the War, he was promoted to Captain, Air Service, 21 February 1919. His commission was vacated 18 September 1920, and he was appointed a Captain, Air Service, United States Army, effective 1 July 1920. On 18 November 1922, Stevens was discharged as a Captain, then re-appointed a First Lieutenant. He returned to the rank of Captain, Air Service, 10 February 1925. On 16 June 1936, he was promoted to the temporary rank of Major, United States Army Air Corps. This rank became permanent 12 June 1939. In 1940, Major Stevens took command of the Photographer’s School, Air Corps Technical School, Lowry Field, Denver, Colorado. He advanced to the temporary rank of Lieutenant Colonel, 30 December 1940. This rank became permanent 15 October 1941. He was retired from the Air Corps for medical reasons, 30 April 1942.

Stevens married Ruth E. Fischer at Rockville, Maryland, 8 August 1938.

Captain Stevens was a pioneering aviator, balloonist and aerial photographer. Using infrared film, he made the first photograph that showed the curvature of the Earth. He also took the first photograph of the Moon’s shadow on the surface of the Earth during an eclipse.

Stevens made a series of high-altitude balloon flights, and on 11 November 1935 he and Captain Orvil A. Anderson ascended to 22,066 meters (72,395 feet) aboard Explorer II, establishing a Fédération Aéronautique Internationale (FAI) world record. ¹

Lieutenant Colonel Andrew William Stevens, United States Army Air Forces (Retired), died at Redwood City, California, 26 March 1949, at the age of 63 years. He is buried at the Golden Gate National Cemetery, San Bruno, California.

Major Albert W. Stevens, U.S. Army Air Corps, circa 1936. Major Stevens is wearing the wings of an aerial observer. The ribbons beneath represent the Purple Heart, the World War I Victory Medal with four campaign stars, and the Distinguished Flying Cross with one oak leaf cluster (a second award).
1st Lieutenant Leigh Wade, Air Service, U.S. Army

1st Lieutenant Leigh Wade, Captain Stevens’ pilot, flew the Douglas World Cruiser Boston in the U.S. Army’s around the world flight, April–September 1924, for which he was awarded the Distinguished Service Medal. He reached the rank of Major General and remained in the United States Air Force until retiring, 1 November 1955.

The Martin GMB (also referred to as the Martin MB-1) was a twin-engine biplane designed as a reconnaissance airplane with a secondary role as a bomber. It had a crew of three. The bomber entered service in 1918 and was the first U.S.-built bomber to enter production.

The GMB was 44 feet, 10 inches (13.665 meters) long with a wingspan of 71 feet, 5 inches (21.768 meters) and height of 14 feet, 7 inches (4.445 meters). The airplane had an empty weight of 6,702 pounds (3,040 kilograms) and a gross weight of 10,225 pounds (4,638 kilograms).

A Martin MB-1 bomber, A.S. 39059, (P-104) at Wright Field. (U.S. Air Force)
A Martin GMB bomber, A.S. 39059 (P-104). (U.S. Air Force)

The bomber was powered by two 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. 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). The engines on Stevens’ airplane were supercharged to increase its altitude capability.

The GMB had a cruise speed of 92 miles per hour (148 kilometers per hour) and maximum speed of 105 miles per hour (169 kilometers per hour) at Sea Level. Its service ceiling was 10,300 feet (3,140 meters). Range for the standard airplane was 390 miles (628 kilometers).

Twenty-two GMBs were built by the Glenn L. Martin Company.

Martin MB-1 A.S. , P=106. (U.S. Air Force)
Martin GMB bomber A.S. 62950 (P-106). (U.S. Air Force)

¹ FAI Record File Number 10654

© 2017, Bryan R. Swopes

12 June 1918

Aviator’s Certificate No. 1702, Aero Club of America. (NASM)

12 June 1918: 2nd Lieutenant James Harold Doolittle, Aviation Section, Signal Officers’ Reserve Corps, was granted Aero Club of America pilot certificate No. 1702 on behalf of the Fédération Aéronautique Internationale.

The license was signed by Alan Ramsay Hawley, President, and William Hawley, Secretary.

Blue, leather-bound book containing James H. Doolittle’s Aero Club of America Aviator’s Certificate. (NASM)

© 2017, Bryan R. Swopes

11 June–4 August 1971

Sheila Scott on the wing of her Piper PA-23-250 Aztec D, Mythre, G-AYTO, 1971. (NASA)
Sheila Scott on the wing of her Piper PA-23-250 Aztec D, Mythre, G-AYTO, 1971. (NASA)

11 June 1971: Sheila Scott O.B.E. (née Sheila Christine Hopkins) departed Nairobi, Kenya, on her third solo around-the-world flight. On this flight she used a new airplane, a twin-engine Piper PA-23-250 Aztec D which she named Mythre. It carried United Kingdom registration G-AYTO. Scott used a NASA navigation and locator communication system to constantly relay her position to a Nimbus weather satellite, and from there to a ground station.

Sheila Scott's Piper PA-23-250 Aztec D, G-ATYO. Mythre.
Sheila Scott’s Piper PA-23-250 Aztec D, G-ATYO, Mythre, at Kidlington Airport, Oxfordshire, England, 1971. (Tim R. Badham)

Sheila Scott planned to not only fly around the world, but to fly from the Equator, over the North Pole, and back to the Equator again. She flew her Aztec from London, England, to Nairobi, Kenya, where she began the Equator–North Pole–Equator portion of the flight.

Scott took off from Nairobi on 11 June 1971 and headed northward to Khartoum, Sudan; Bengazi, Libya; Malta; arriving back at London on 21 June. From there she continued to Bodø, Norway; Andøya, Norway; Station Nord, Greenland; across the North Pole on 28 June; then southward to Barrow, Alaska; arriving at Anchorage, Alaska, on 3 July; San Francisco, California, to Honolulu, Hawaii, on 11 July. She recrossed the Equator heading south to Canton Island. On 23 July, Mythre arrived at Nadi, Viti Levu, Fiji, and then flew on to Noumea, New Caledonia. After a stop at Townsville, Queensland, Scott arrived at Darwin, Northern Teritory, Australia, 1 August. From there she continued to Singapore; Madras, India; Karachi, Pakistan; Bahrain; Athens, Greece; and finally completed her journey at London on 4 August. The trip took 55 days.

During the circumnavigation, Sheila Scott set seven Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Recognized Course: Andøya, Norway, to Station Nord, Greenland, 213.61 kilometers per hour (132.73 miles per hour) ¹; Nord to Barrow, Alaska, 183.73 km/h (114.16 mph) ²; San Francisco, California, to Honolulu, Hawaii, 236.56 km/h (146.99 mph) ³; Darwin, Northern Territory, Australia, to London, England, 160.19 km/h (99.54mph). ⁴ Three of these records remain current. ⁵

Ms. Scott’s airplane was a 1971 Piper 23-250 Aztec (“Aztec D”), serial number 27-4568. The airplane was assigned the United Kingdom registration G-AYTO on 3 March 1971. The Aztec D was a six-place twin-engine light airplane based on the earlier PA-23-235 Apache, with a larger cabin and more powerful engines. It was of all-metal construction and had retractable tricycle landing gear. The Aztec D is 31 feet, 2.625 inches (9.516 meters) long with a wingspan of 37 feet, 1.750 inches (11.322 meters) and overall height of 10 feet, 3.875 inches (3.146 meters). The wing has 5° dihedral. The Aztec D has an empty weight of 3,042 pounds (1,380 kilograms) and a gross weight of 5,200 pounds (2,359 kilograms).

The Aztec D is powered by two air-cooled, fuel-injected, 541.511-cubic-inch-displacement (8.874 liter) AVCO Lycoming IO-540-C4B5 6-cylinder, horizontally-opposed, direct-drive engines. The -C4B5 has a compression ratio of 8.5:1 and a Maximum Continuous Power/Takeoff rating of 250 horsepower at 2,575 r.p.m. It weighs 374 pounds (170 kilograms). The engines drive two-bladed Hartzell constant-speed propellers with a diameter of 6 feet, 2 inches (1.880 meters).

The PA-23-250 Aztec D has a maximum structural cruising speed (VNO) of 172 knots (198 miles per hour/319 kilometers per hour) at 7,500 feet (2,286 meters) and maximum speed (VNE) of 216 knots 249 miles per hour (400 kilometers per hour). The service ceiling is 19,800 feet (6,035 meters). With standard fuel capacity of 144 gallons (545 liters) the airplane’s range is 1,055 miles (1,698 kilometers). Mythre carried an auxiliary fuel tank in the passenger cabin.

After the around-the-world flight, Scott returned Mythre to the Piper Aircraft Company at Lock Haven, Pennsylvania, for overhaul. Following Tropical Storm Agnes in June 1972, the Piper factory was flooded to a depth of 16 feet (4.9 meters) and Scott’s airplane, along with many others and much of the tooling for aircraft manufacture, was destroyed.

Sheila Scott's Piper Aztec, Mythre, over the North Pole, by Paul Couper, 2008
“Sheila Scott over the Top—Piper Aztec,” by Paul Couper, Guild of Aviation Artists, 2008. 62 × 52 centimeters, oil/acrylic.

This painting is available from the Guild of Aviation Artists at:

http://www.gava.org.uk/index.php?option=com_phocagallery&searchterm=Paul%20Couper&view=category&id=12&Itemid=534&picsearch=simple

Sheila Christine Hopkins was born 27 April 1922 at 12 Park Avenue, Worcester, Worcestershire, England. She was the daughter of Harold Reginald Hopkins and Edyth Mary Kenward Hopkins.

Miss Hopkins married Rupert Leamon Bellamy at Kensington, in late 1945. The marriage was dissolved in 1950.

Sheila Scott had been a nurse at Haslar Naval Hospital during World War II. She was an actress on the stage, in films and on television. In 1959 she followed a lifetime ambition and learned to fly. She owned or leased several airplanes which she entered in races or used to establish flight records.

Scott was a commercial pilot, rated in single and multi-engine airplanes, seaplanes and helicopters. She was a member of The Ninety-Nines, founding and serving as governor of the British branch. She was also a member of the Whirly-Girls and the International Association of Licensed Women Pilots.

Sheila Scott was the author of I Must Fly and On Top of the World (Barefoot With Wings in the United States).

Sheila Scott, O.B.E., died of cancer at Royal Marsden Hospital, Chelsea, London, 20 October 1988, at the age of 66 years. ¹

Sheila Scott, Officer of the Most Excellent Order of the British Empire, 12 March 1968. (AP/Worth)

¹ FAI Record File Numbers 4622, 4623

² FAI Record File Number 14203

³ FAI Record File Numbers 4626, 4627

⁴ FAI Record File Numbers 4624, 4625

⁵ FAI Record File Numbers 4622, 4626, 14203

© 2020, Bryan R. Swopes

8 June 1911

Glenn Hammond Curtiss’ Federation Aeronautique Internationale/Aero Club of America Licence, No. 1, issued June 8, 1911. (NASM-CW8G-0258)

8 June 1911: The Aero Club of America, as representative of the Fédération Aéronautique Internationale, issued Aviator Certificate Number 1 to Glenn Hammond Curtiss. The document was signed by Allan A. Ryan, president of the club, and G. F. Campbell-Wood, secretary.

© 2021, Bryan R. Swopes

7 June 1919

“Portrait of famous French aviatrix Baroness de la Roche on July 1, 1919, taken after she broke the world’s record for altitude reached by a woman. (Photo: Bettmann/Corbis)” —YAHOO!

7 June 1919: Numerous sources report that the Baroness de la Roche (née Élisa Léontine Deroche) set a “world record” for women with a Caudron G.3 biplane, sometime during June 1919.

There is considerable variation among these sources, though, with dates variously given as 7 June, 12 June, 17 June, or most often, simply June. And the altitude which she is credited is also confused, varying from 3,900 meters, 4,260 meters, 4,500 meters, 4,785 meters, 4,800 meters, and even 5,150 meters.

The actual facts are uncertain. Mme. Deroche’s flight was not certified by the Fédération Aéronautique Internationale (FAI).

Mme. Deroche with a Deutsche Schaferhund.

A contemporary source of aviation news reported:

A Women’s Height Record

     Flying a small Caudron G.3 biplane, Baroness de la Roche, during a flight which lasted  1 hr. 49 mins., went up to an altitude of 3,900 metres (12,870 ft.), which is claimed, in Paris, as a woman’s record.

     Miss Ruth Law has cabled from New York claiming that in September 1917, she went up to 4,240 metres.

FLIGHT & The AIRCRAFT ENGINEER, No. 546, Vol. XI, No. 24, 12 June 1919, Page 780, Column 2

Women’s Height Record

     In view of the fact that Miss Ruth Law had claimed to have bettered the performance of Baroness de la Roche the other day, when she flew to a height of 3,900 metres (12,870 ft.), a new attempt was made on June 12. Starting from Issy on a Caudron biplane, Baroness de la Roche climbed steadily until she reached a height of 4,800 metres (15,840 ft.) Coming down she lost her way in a mist, but eventually landed safely at Gastins, 8 kiloms. from Nangis, after a flight of 2 hrs. 7 mins.

FLIGHT & The AIRCRAFT ENGINEER, No. 547, Vol. XI, No. 25, 12 June 1919, Page 799, Columns 1 and 2

For comparison,

Pushing up World’s Height Record

     Not satisfied with his height record of last week Lieut. Casole [sic] on June 14 took his Nieuport up to 10,100 metres (33,330 feet) during a flight from Villacoublay which lasted 1 hr. 55 mins. As in his previous flights, he used a Nieuport, fitted with a 300 h.p. Hispano-Suiza motor. His previous highest was 9,500 metres (31,350 ft.) and not 51,350 ft., as a printer’s error made it appear in our last issue.

FLIGHT & The AIRCRAFT ENGINEER, No. 547, Vol. XI, No. 25, 12 June 1919, Page 799, Columns 1

While Jean Casale’s ¹ record of 9,520 meters (31,234 feet), set 14 June 1919, ² is recognized by the Fédération Aéronautique Internationale, the FAI did not recognize records set by women until 28 June 1929. Neither Mme. Deroche or Miss Law have any records listed in the FAI’s online data base.

Société des Avions Caudron G.3. (Musée de l’Air et de l’Espace)

The Caudron G.3 is the same type airplane flown by Adrienne Bolland when she crossed the Andes Mountains of South America nearly two years later.

The Caudron G.3 was a World War I reconnaissance airplane and flight trainer manufactured by Société des Avions Caudron. It is called a sesquiplane because the lower wing is significantly shorter than the upper. The G.3 was a single-engine aircraft that was built in single- and two-place variants. The engine and cockpit are contained in a very short fuselage, supporting the wings and landing gear. Tail control surfaces are mounted on an open framework tail boom.

Caudron G.3 sesquiplane. (Musée de l’Air et de l’Espace)

The Caudron G.3 was 6.90 meters (22 feet, 7 inches) long with an upper wingspan of 13.26 meters (43 feet, 6 inches). The height of the aircraft was 2.60 meters (8 feet, 5 inches). The airplane had an empty weight of 420 kilograms (926 pounds) and maximum weight of 736 kilograms (1,623 pounds).

The G.3 was powered by an air-cooled, normally-aspirated 10.910 liter (665.791 cubic inches) Société des Moteurs Le Rhône 9C nine cylinder rotary engine with a compression ratio of 5:1. It was rated at 70 cheval vapeur (1 ch = 0.99 horsepower) at 1,100 r.p.m., and 80 cheval vapeur  at 1,200 r.p.m., but able to produce a maximum 92 cheval vapeur (90.77 horsepower) at 1,300 r.p.m. It drove a two-bladed, fixed-pitch wooden propeller. The 9C was 0.810 meters (2 feet, 7.9 inches) long, 0.930 meters (3 feet, 6.1 inches) in diameter and weighed 119 kilograms (262 pounds).

The Caudron G.3 had a maximum speed of 110 kilometers per hour (68 miles per hour) and service ceiling of 5,000 meters (16,404 feet). Its range was 330 kilometers (205 miles).

By the end of World War I, Caudron had built 2,402 G.3s.

Élisa Léontine Deroche

Élisa Léontine Deroche was born 22 August 1882 at nº 61, Rue de la Verrerie, in the 4e arrondissement, Paris, France. She was the daughter of Charles François Deroche, a plumber, and Christine Calydon Gaillard Deroche. In her early life she had hoped to be a singer, dancer and actress. Mlle. Deroche used the stage name, “Raymonde de Laroche.”

Mlle. Deroche married M. Louis Léopold Thadome in Paris, 4 August 1900. They divorced 28 June 1909.

She had a romantic relationship with sculptor Ferdinand Léon Delagrange, who was also one of the earliest aviators, and it was he who inspired her to become a pilot herself. They had a son, André, born in 1909. Delagrange was killed in an airplane accident in 1910. They never married.

After four months of training under M. Chateu, an instructor for Voison, at Chalons, she made her first solo flight on Friday, 22 October 1909. On 8 March 1910, Élisa Léontine Deroche was the first woman to become a licensed pilot when she was issued Pilot License #36 by the Aéro-Club de France.

Pilot Certificate number 36 of the Aéro-Club de France was issued to Mme de Laroche. (Musée de l’Air et de l’Espace)

In a 30 October 1909 article about her solo flight, Flight & The Aircraft Engineer referred to Mme. Deroche as “Baroness de la Roche.” This erroneous title of nobility stayed with her in the public consciousness. Deroche participated in various air meets, and on 25 November 1913, made a non-stop, long-distance flight of four hours duration, for which she was awarded the Coupe Femina by the French magazine, Femina.

On 20 February 1915, Mme. Deroche married Jacques Vial at Meudon, Hauts de Seine, Île-de-France, France.

During World War I she was not allowed to fly so she served as a military driver.

Mme. Deroche was at Le Crotoy in northern France, co-piloting an experimental airplane, a civil variant of the Caudron G.3. The aircraft suddenly  pitched down and crashed, killing Deroche and the pilot, M. Barrault. Mme. Deroche was 36 years old. Élisa Léontine Deroche was buried at the Cimetière du Père-Lachaise, Paris, France.

¹ Sous Lieutenant Jean Pie Hyacinthe Paul Jerome Casale, Marquis de Montferato

² FAI Record File Number 15455

© 2019, Bryan R. Swopes