11 November 1935: During a record-setting flight from England to Brazil, Jean Gardner Batten ¹ became the first woman to fly solo across the South Atlantic Ocean, flying her Percival D.3 Gull Six, G-ADPR, from Dakar, Afrique occidentale française (French West Africa, now, Senegal) to Natal, Brazil. Her elapsed time of 13¼ hours was the fastest for the Atlantic crossing up to that time.
On 7 May 1935, Jean Batten was honored with the distinction of Chevalier de la légion d’honneur at Paris, France. At Rio de Janeiro, Brazil, 21 November 1935, Getúlio Dornelles Varga, the President of the Republic of Brazil, conferred upon her its Ordem Nacional do Cruzeiro do Sul (Order of the Southern Cross). The following year, Jean Gardner Batten of the Dominion of New Zealand was appointed Commander of the Most Excellent Order of the British Empire (C.B.E.) in the King’s Birthday Honours List, 19 June 1936, for general services to aviation. Twice Batten was awarded the Britannia Trophy of the Royal Aero Club, and three times she won the Harmon Trophy of the International League of Aviators. The Fédération Aéronautique Internationale (FAI) awarded her its Gold Medal.
“This young woman, gifted with the finest of qualities, has made a great contribution, both through her daring and her patience, to the progress of aviation in the world. This year, she is worthy of receiving the Gold Medal, very few holders of which are still alive,” said George Valentin, Prince Bibescu, the president and one of the founders of the FAI, when awarding Jean Batten the medal.
A biographical article about Jean Batten can be seen at:
Batten’s Percival D.3 Gull Six, c/n D55, was a single-engine, low-wing monoplane, with fixed landing gear. It was flown by a single pilot and could carry two passengers. On 29 August 1935, the airplane was assigned Great Britain civil registration G-ADPR (Certificate of Registration 6242).
The airplane was 25 feet, 0 inches (7.62 meters) long with a wingspan of 36 feet, 0 inches (10.973 meters) and height of 7 feet, 3 inches (2.210 meters). The D.3 had an empty weight of 1,632 pounds (740.26 kilograms) and gross weight of 2,450 pounds (1,111.30 kilograms).
The Gull’s fuselage was constructed of spruce stringers and struts, covered with a three-ply skin. The wings were designed to be able to fold back alongside the fuselage. The resulting width of 12 feet, 10 inches (3.912 meters) required considerably less storage space.
The Gull Six was powered by an air-cooled, normally-aspirated 9.186 liter (560.573-cubic-inch-displacement) de Havilland Gypsy Six I, an inverted inline six-cylinder engine which produced 184 horsepower at 2,100 r.p.m., and 205 horsepower at 2,350 r.p.m. for takeoff. The engine turned a two-bladed fixed-pitch metal propeller via direct drive. The engine weighed 432 pounds (196 kilograms).
The Gull Six was capable of reaching 178 miles per hour (286.5 kilometers per hour). Its service ceiling was 16,000 feet (4,876.8 meters) and range was 700 miles (1,126.5 kilometers).
On 17 July 1940, Batten’s Percival Gull was impressed into military service and assigned a military identification of AX866. The airplane was returned to the civil register in 1946. It is now on display at the Jean Batten International Terminal, Auckland Airport, New Zealand.
During a competition for the Coupe Deutsch de la Meurthe, Lieutenant Le Marquis Bernard Henri Marie Léonard Barny de Romanet of France’s Aéronautique Militaire flew a Nieuport-Delâge Ni-D 29V to set two Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Closed Circuit of 268.63 kilometers per hour (166.92 miles per hour).¹
De Romanet’s Ni-D 29V was one of three racing variants of the highly successful single-engine, single-seat Ni-D 29C.1 biplane fighter, which was the fastest in the world at the time. The Ni-D 29V was 21 feet, 3.5 inches (6.489 meters) long, with a wing span of just 6.00 meters (19 feet, 8¼ inches), shortened from the 31 feet, 10 inch (9.703 meters) wingspan of the standard production chasseur.
The airplane was powered by a water-cooled, normally aspirated, 18.473 liter (1,127.29-cubic-inch displacement) right-hand tractor Hispano-Suiza 8Fb single overhead cam (SOHC) 90° V-8 engine, modified to increase its output to 320 horsepower. This was a direct-drive engine, and turned a two-bladed-fixed pitch propeller. The engine was 1.32 meters (4 feet, 4 inches) long, 0.89 meters (2 feet, 11 inches) wide, and 0.88 meters (2 feet, 10½ inches) high. It weighed 256 kilograms (564 pounds).
The standard airplane had a top speed of 235 kilometers per hour (146 miles per hour), a range of 580 kilometers (360 miles) and a service ceiling of 8,500 meters (27,887 feet).
Le Marquis Bernard Henri Marie Léonard Barny de Romanet was born at Saint-Maurice-de-Sathonay, Saône-et-Loire, Bourgogne, France, 28 January 1894. He was the son of Léonard Jean Michel Barny de Romanet and Marie Noémie Isabelle de Veyssière. He descended from a very old French family.
Bernard de Romanet joined the Cavalry at the age of 18 years. During World War I, he served with both cavalry and infantry regiments as a Maréchel de Logis (master sergeant) before transferring to the Aéronautique Militaire in July 1915, as a photographer and observer.
After completing flight training in 1916, de Romanet was assigned as a pilot. In early 1918, de Romanet trained as a fighter pilot. He shot down his first enemy airplane 23 May 1918, for which he was awarded the Médaille Militaire, and was promoted to Adjutant (warrant officer). De Romanet was commissioned as a Sous-Lieutenant (equivalent to a second lieutenant in the United States military) several months later. After a fourth confirmed victory he was promoted to the rank of Lieutenant (first lieutenant).
By August 1918, he was in command of Escadrille 167. He was officially credited with having shot down 18 enemy aircraft, sharing credit for 12 with other pilots. He claimed an additional 6 airplanes destroyed.
Lieutenant de Romanet was appointed Chevalier de la légion d’honneur, and was awarded the Croix de Guerre with three étoiles en vermeil (silver gilt) stars and 10 palmes.
Bernard Henri Marie Léonard Barny de Romanet was killed 23 September 1921, when the fabric covering of his Lumière-De Monge 5.1 airplane’s wings was torn away and the airplane crashed.
19 October 1908: From the grounds of the Château de Bagatelle, Paris, France, Eugène Welferinger (1872–1936) made the first flight of the Société d’aviation Antoinette monoplane, the Antoinette IV.
A single-place, single-engine airplane, the Antoinette IV was one the first successful monoplanes. American Machinist described it as a “purely racing machine.”
The airplane and its V-8 engine were designed by Léon Levavasseur. It was modified a number of times, as was its sister ship, the Antoinette V.
Augustus Post, Secretary of the Aero Club of America, wrote in the weekly technical publication, American Machinist:
M. Lavavasseur considered that the monoplane offered the advantages of simplicity of form, natural stability, and was easier to construct; that is to say, that the thrust of the motor required for flight was less under the same conditions of speed and weight.
The “Antoinette” is particularly interesting on account of the manner in which the problems have been studied and the great amount of thought that has been given to them. The machine is perhaps without question the most finely finished of those in its class, shows the most careful workmanship in its most minute detail, and presents more new and original features than any of the other machines which may be compared with it. It also provides a comfortable cockpit for the aviator, a distinct advantage in long and trying flights.
—American Machinist, Hill Publishing Company, New York, 7 October 1909, Page 608 at Column 2
The Antoinette IV was approximately 11,50 mètres (37.72966 feet) long with a wingspan of 14,80 mètres (48.55643 feet). The leading edge was swept aft 3°. They had a chord of 3 meters (9.8 feet) at the root, tapering to 2 meters (6.6 feet) at the tip. The wing had an angle of incidence of 4° with 6° dihedral. The total surface area was 34 square meters (366 square feet). The weight of the Antoinette IV was 460 kilograms (1,014 pounds) with one hour of fuel. It was capable of reaching 120 kilometers per hour (75 miles per hour).
The airplane was described in contemporary reports as “beautiful” and often mentioned was the very narrow triangular cross section of its fuselage. Different configurations of landing gear were tried, with combinations of skids and wheels, wheels in tandem, and side-by-side. Directional control was created through “wing-warping” as had been used by the Wright Brothers. This was later modified to an aileron system. The tail surfaces were cruciform, with two triangular rudders located above and below the triangular elevator. Flight controls were four hand wheels and two pedals which connected to the control surfaces by cables.
As originally built, the Antoinette IV was powered by a steam-cooled, normally-aspirated, 7.274 liter (443.861 cubic inch displacement) Antoinette 8V 90° overhead valve V-8 engine which produced approximately 45–50 chaval-vapeur (44.4–49.3 horsepower) at 1,400 r.p.m. This engine was considerably smaller and lighter than Levavasseur’s previous V-8s. Because the compression ratio was increased, the aluminum cylinder heads were replaced with forged steel heads. Carburetors were used instead of direct injection, which was prone to clogging. The 8V was a direct-drive engine which turned a propeller with two aluminum blades which were riveted to a steel tube that attached to the engine’s output shaft. The propeller had a diameter of 2.20 meters (7 feet, 2.6 inches). The V-8 engine was 0.750 meters (2 feet, 5.5 inches inches) long, 0.600 meters (1 foot, 11.6 inches) wide and (0.600 meters (1 foot, 11.6 inches) high. It weighed 60 kilograms (132 pounds), dry, and 85 kilograms (187 pounds) in running order.
The engine sold for ₣12,500 (approximately $2,451 U.S. dollars) with delivery expected in 10 months. Antoinette airplanes could be purchased for ₣25,000, or about $4,902 U.S. dollars.
On 19 July 1909, Arthur Louis Hubert Latham, who had been taught to fly by Welféringer, attempted to fly the Antoinette IV across the English Channel, but an engine failure forced it down about 8 miles (13 kilometers) off the French coast.
The airplane remained afloat and Latham was rescued by the French torpedo boat destroyer FS Harpon, but the airplane was severely damaged during the recovery.
Léon Levavasseur was a French engineer, born 8 January 1863 near Cherbourg, France. He invented the 90° V-8 engine, which he patented in 1902. He specialized in lightweight engines, using components designed to be only as strong as was required by their specific use. He developed direct fuel injection and evaporative cooling for internal combustion engines.
His company, Société d’aviation Antoinette, and its products, were named for the daughter of his business partner, Jules Gastambide. The company initially produced lightweight engines for other airplane builders, but began to construct complete airplanes in 1906. Both Levavasseur and Gastambide left Antoinette in 1909 following a disagreement with the board of directors, but they returned five months later. The company failed in 1911.
Levavasseur was appointed Chevalier de la légion d’honneur in 1909.
Léon Levavasseur died in Paris, France, 26 February 1922, at the age of 59 years.
Recommended: An excellent article about Léon Levavasseur’s Antoinette engines can be found at Old Machine Press:
18 October 1909: Charles Alexandre Maurice Joseph Marie Jules Stanislas Jacques Count de Lambert, the first student to successfully complete Wilbur Wright’s aviation school at Pau, Pyrénées-Atlantiques, flew his Wright Model A Flyer from Port Aviation (Juvisy-sur-Orge), Viry-Châtillon (in the outskirts of Paris), the World’s first airport, to the Eiffel Tower.
The Comte de Lambert departed Port Aviation at 4:36 p.m. He circled the Tower at an altitude of 400 meters (about 1,300 feet) and then returned to Pau, located on the northern edge of the Pyrenees.
The flight covered approximately 48 kilometers (30 miles) with an elapsed time of 49 minutes, 39 seconds.
Comte de Lambert’s flight coincided with an evening banquet celebrating a two-week “Grande Quinzaine de l’Aviation de Paris“. L’Aéroclub de France awarded him a Gold Medal for his achievement, and France appointed him Chevalier de la Légion d’Honneur.
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).
A water-cooled 240.5 cubic-inch-displacement (3.940 liter) Wright inline four-cylinder gasoline engine produced 32 horsepower at 1,310 r.p.m. 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 (kilometers per hour).
Lieutenant Commander William Merrill Corry, Jr., United States Navy, was assigned as aviation aide to Admiral William Braid Wilson, Jr., Commander-in-Chief, Atlantic Fleet, aboard the battleship USS Pennsylvania (BB-38). On Saturday, 2 October 1920, Lieutenant Commander Corry, in company with Lieutenant (Junior Grade) Arthur C. Wagner, Reserve Force, United States Navy, flew from Mitchel Field, Mineola, Long Island, New York, to Hartford, Connecticut. Their airplane was a two-place, single-engine Curtiss JN-4 biplane. The flight was intended as a cross-country flight for the two pilots to maintain proficiency.
On arrival at Hartford, because there was no airfield in the vicinity, the pair landed on the grounds of the Hartford Golf Club. They stayed over the weekend as guests of Colonel Hamilton R. Horsey, formerly chief-of-staff of the 26th Division, U.S. Army, during the St. Mihiel and Meuse-Argonne offensives of World War I, and Lieutenant Colonel James S. Howard.
At about 3:00 p.m., on Sunday, 3 October, Corry and Wagner were ready to return to Mineola. Lieutenant (j.g.) Wagner was flying from the forward cockpit, while Lieutenant Commander Corry was in the rear cockpit.
The Curtiss took off toward the north and at about 50 feet (15 meters) altitude, turned toward the southwest. As the airplane passed over the golf course club house, Corry waved to Colonel Horsey. The airplane approached a large grove of trees, then turned right, back to the north. The engine stopped and the airplane nose-dived into the ground from about 75 feet (23 meters).
The Hartford Courant reported:
The machine hit the ground at a sharp angle and immediately turned over endwise, the propeller catching in the ground. Commander Corry was catapulted from his seat, but Wagner, who had strapped himself into his seat, was less fortunate. As the machine turned over it burst into flames, enveloping him in a wash of blazing gasoline from the broken tank.
Commander Corry, picking himself up from the ground, was the first to rush to the aid of his comrade. It was in this way that his coat caught fire with the resulting burns to his hands and face. He was unable to pull Wagner free and it was not until Walter E. Patterson of the Travelers Insurance Company, and Martin Keane, an attache of the club, added their efforts this was successfully accomplished. Club members rushed from the clubhouse with several gallons of olive and sweet oil and were on hand almost as soon as the stricken man was freed from his seat. While the burning clothing was being removed from Wagner’s body, Benjamin Allen, a porter in the club, quickly wrapped his coat around Corry’s head and thus cut off any chance of the flames reaching the officer’s nose or eyes.
Allen then, with Corry helping, removed the coat and smothered the other smouldering pieces of clothing. Corry’s hands and face were so badly burned that not a trace of skin was left untouched. Several ribs were also broken.
Wagner was rolled over on the ground by willing hands to extinguish the flames and with the help of the two men who had dragged him from his place beneath the plane, such of his clothing as still remained unburned was stripped from his body to make way for dressings in olive and sweet oil, which by this time were available. He was wrapped in swaths of oil soaked linen and cotton sheeting to allay the agony of his burns. Every scrap of clothing was almost entirely consumed and his shoes were burned to a crisp. Throughout the process, Wagner, fully conscious, was directing the efforts of the willing helpers, despite the fact that his face was beyond recognition, with nose and ears burned from his head.
He remained game even to the time when he was being tenderly lifted to the ambulance, when he thanked those who had helped telling them that he was sure they had done all they could. . .
. . . In spite of a heroic fight for life, covering nearly eight hours from the time he received his burns, Wagner died soon after 10 o’clock. The tremendous display of pluck and vitality shown by the man through all of his agony was the marvel of all the physicians and nurses in the hospital. . . .
—The Hartford Courant, Monday Morning, 4 October 1920, Page 1, Column 8, and Page 2, Column 1.
Four days later, 7 October 1920,¹ Lieutenant Commander Corry also died of his injuries. He was just 31 years old.
For his bravery in attempting to rescue Lieutenant (j.g.) Wagner, Lieutenant Commander William Merrill Corry, Jr., United States Navy, was awarded the Medal of Honor. His citation reads:
“For heroic service in attempting to rescue a brother officer from a flame -enveloped airplane. On 2 October 1920,² an airplane in which Lt. Comdr. Corry was a passenger crashed and burst into flames. He was thrown 30 feet clear of the plane and, though injured, rushed back to the burning machine and endeavored to release the pilot. In so doing he sustained serious burns, from which he died 4 days later.”
William Merrill Corry, Jr., was born 5 October 1889 at Quincy, Florida. He was the second of six children of William Merrill Corry, a tobacco dealer, and Sarah Emily Wiggins Corry.
“Bill” Corry was admitted to the United States Naval Academy, Annapolis, Maryland, as a midshipman, 20 June 1906. He was a classmate of future Admiral Marc A. Mitscher. On 7 July 1910, Midshipman Corry was assigned to the 16,000 ton Connecticut-class battleship USS Kansas (BB-21). He was commissioned an Ensign, United States Navy, 7 March 1912.
Ensign Corry was promoted to Lieutenant (junior grade), 7 March 1915. He was assigned to the naval aeronautic station (Y-13) at Pensacola, Florida, 7 July 1915. On completion of flight training, Lieutenant (j.g.) Corry was designated Naval Aviator No. 23, 16 March 1916.
26 November 1916, Lieutenant (j.g.) Correy was assigned to the Tennessee-class armored cruiser USS Seattle (ACR-11). In 1917 he was assigned to USS North Carolina (ACR-12).
The United States entered World War I on 6 April 1917. On 22 August 1917, Lieutenant (j.g.) Corry was sent to France for for duty with the U.S. Naval Aviation Forces in Europe. Corry was promoted to the rank of Lieutenant, 7 March 1918. He was placed in command of the aviation school at Le Croisic, on the western coast of France, 7 November 1917. While there he was awarded the Navy Cross, “for distinguished and heroic service as an Airplane Pilot making many daring flights over the enemy’s lines, also for untiring and efficient efforts toward the organization of U.S. Naval Aviation, Foreign Service, and the building up of the Northern Bombing project.” (The Northern Bombing Group targeted bases supporting German submarine operations.) France appointed him a Chevalier de la légion d’honneur.
Lieutenant Corry took command of the Naval Air Station at Brest, France, 7 June 1918. He was promoted to the temporary rank of Lieutenant Commander, 1 July 1918. He remained at Brest until the Armistice, 11 November 1918. He was involved in the demobilization of U.S. forces in France and Belgium. He also served in various staff assignments.
Lieutenant Commander Corry was ordered to return to the United States as aide for aviation to the Chief-of-Staff Atlantic Fleet. He sailed from Antwerp, Belgium on 2 June 1920, aboard SS Finland, bound for New York.
Lieutenant Commander William Merrill Corry, Jr., Medal of Honor, Navy Cross, Chevalier de la légion d’honneur, is buried at the Eastern Cemetery, Quincy, Florida.
Following his death, the United States Navy named an auxiliary landing field at Pensacola. Florida, Corry Field, in his honor. A nearby airfield assumed the name in 1928, and is presently called NAS Pensacola Corry Station.
Three United States Navy warships have also been named USS Corry. On 25 May 1921, a Clemson-class “flush-deck” or “four-stack” destroyer, USS Corry (DD-334), was commissioned. It was decommissioned in 1930.
The Gleaves-class destroyer USS Corry (DD-463) was launched 28 July 1941, christened by Miss Jean Constance Corry, with Miss Sara Corry as Maid of Honor. The new destroyer was commissioned 18 December 1941. Corry is notable for its participation in anti-submarine operations in the Atlantic, sinking U-801 on 17 March 1944. Corry rescued 47 sailors from that submarine, and another 8 from U-1059, which was sunk two days later.
Corry was herself sunk by during an artillery duel with a German coastal battery off Utah Beach, Normandy, 6 June 1944. Of the destroyer’s crew of 276 men, 24 were killed and 60 were wounded. Broken in half, the ship sank in shallow water. The American Flag at her masthead remained visible above the water as the ship settled on the sea bed.
The Gearing-class destroyer USS Corry (DD-817) was commissioned 27 February 1946 at Orange, Texas. The ship’s sponsor was Miss Gertrude Corry, niece of Lieutenant Commander Corry. Corry served the U.S. Navy until decommissioned 27 February 1981 after 35 years of service. It was turned over to Greece and renamed HS Kriezis (D-217). The ship was finally retired in 1994, and scrapped in 2002.
Lieutenant (junior grade) Arthur C. Wagner, Reserve Force, United States Navy, was born 18 August 1988. He was the son of William Wagner and Elizabeth Genting (?) Wagner.
At the time of his death, Lieutenant Wagner was assigned to the Atlantic Fleet Ship Plane Division, Mitchel Field, Mineola, Long Island, New York. He had previously served aboard USS Nevada (BB-36). In 1919 he trained as a pilot at Naval Air Station Pensacola, and was then assigned to USS Shawmut (CM-4), a minelayer which had been reclassified as an airplane tender.
Lieutenant (j.g.) Arthur C. Wagner was buried at the Old Cathedral Cemetery, Philadelphia, Pennsylvania, 8 October 1920.
¹ While many sources give the date of Corry’s death as 6 October 1920, probate documents filed with the County of Gadsen court on 5 November 1920, and signed by Corry’s mother, Sarah E. Corry, give the date as 7 October 1920. Further, The Hartford Courant, in its Thursday, 7 October 1920 edition, at Page 1, Column 2 and 3, reported: “Lieutenant Commander William M. Corry, in charge of the Curtiss naval airplane which crashed to earth at Hartford Golf Club last Sunday afternoon, died at the Hartford Hospital at 2:30 o’clock this morning of burns. . . .”
² Most sources place the date of the crash as 2 October 1920. Contemporary newspapers, though, e.g., The Hartford Courant, The Philadelphia Inquirer and The Chicago Tribune, reported the date as 3 October 1920.