2–6 July 1919: Two weeks after Alcock and Brown made the first non-stop transatlantic airplane flight, the Royal Air Force rigid airship R 34 landed at Mineola, Long Island, New York, completing the first east-to-west Atlantic crossing by air. The airship was under the command of Major George Herbert Scott, A.F.C., R.A.F. The total complement, including passengers, was 30 persons.
The 108 hour, 12 minute flight started from East Fortune Airship Station near Edinburgh, Scotland at 2:38 a.m., British Summer Time (1:38 a.m., Greenwich mean time) on Wednesday, 2 July. R 34 arrived at Mineola at 9:54 a.m. Eastern Daylight Savings Time (1:54 p.m. G.M.T.) on Sunday, 6 July. According to records of the Fédération Aéronautique Internationale, the distance flown by R 34 was 5,797 kilometers (3,602 miles). On arrival, the airship had only 40 minutes of fuel remaining.
R 34 was based on extensive study of the captured German Zeppelin, L-33. It was built for the Royal Naval Air Service ¹ by William Beardmore and Company, Inchinnan, Renfrewshire, Scotland. 643 feet long (196 meters), with a maximum diameter of 78 feet, 9 inches (24 meters), the dirigible had a total volume of 1,950,000 cubic feet (55,218 cubic meters). The airship had a light weight metal structure covered with doped fabric. Buoyancy was provided by 55,185 cubic meters (1,948,840 cubic feet) of gaseous hydrogen contained in 19 gas bags inside the airship’s envelope. R 34 had a gross lift capacity of 59 tons. Useful lift was 58,240 pounds (26,417 kilograms).
The airship was powered by five water-cooled, normally-aspirated, 15.395-liter (989.483-cubic-inch-displacement) Sunbeam Maori Mk.IV dual overhead cam (DOHC) 60° V-12 engines with four valves per cylinder. The Mk.IV’s cylinder bore had been increased from 100 millimeters to 110 millimeters (3.94 to 4.33 inches), resulting in a larger displacement than previous Maori variants. The Maori Mk.IV was a direct-drive engine which produced 275 horsepower at 2,000 r.p.m. Each engine turned a two-bladed, 17 foot diameter (5.182 meter) propeller through a remote gearbox with a 0.257:1 reduction. The two wing engines were equipped with reversible gearboxes. With the engines turning 1,800 r.p.m., the R 34 had a cruising speed of 47 knots (54 miles per hour/87 kilometers per hour) and consumed 65 gallons (246 liters) of fuel per hour.
R 34 made the return flight to England, 10–13 July 1919, in 75 hours, 3 minutes.
Major Scott was appointed Commander of the Most Excellent Order of the British Empire.
CENTRAL CHANCERY OF THE ORDERS OF KNIGHTHOOD.
St. James’s Palace, S.W. 1,
23rd August 1919.
The KING has been graciously pleased to give orders for the following appointment to the Most Excellent Order of the British Empire, in recognition of distinguished services to Aviation. :—
To be a Commander of the Military Division of the Said Most Excellent Order :—
Major George Herbert Scott, A.F.C., Royal Air Force, Commander of H.M. Airship R/34 on the outward voyage to the United States of America and and also on the homeward journey.
Colonel (A./Brig.-Genl.) Edwards Maitland Maitland, C.M.G., D.S.O., Capt. (A./Major) Gilbert George Herbert Cooke, D.S.C., Lieutenant Guy Harris and 2nd Lieutenant John Durham Shotter were each awarded the Air Force Cross.
The Air Force Medal was awarded to Flight-Sergeant William Rose Gent, Sergt.-Maj. II. Walter Robert Mayes, D.S.M., Flight-Sergeant Walter James Robinson, Flight-Sergeant Reginald William Ripley, Flight-Sergeant Norman Albert Scull, and Sergeant Herbert Murray Watson, D.S.M.
¹ On 1 April 1918, the Royal Naval Air Service and the Royal Flying Corps were combined to form the Royal Air Force.
22 June 1931: In the late 1920s through mid-1930s, Miss Ruth Rowland Nichols was one of the best-known American women in aviation. She was the only person to have simultaneously held world records for speed, distance and altitude.
Miss Nichols planned to become the first woman to fly solo across the Atlantic Ocean. On the afternoon of 22 June 1931, she took off from Mitchel Field, Long Island, New York, to stage for the transatlantic flight at Harbor Grace, Dominion of Newfoundland, making an intermediate stop at Saint John, New Brunswick, Dominion of Canada.
Nichols was flying a Lockheed Model 5 Vega, owned by Powell Crosley, Jr., founder of the Crosley Radio Corporation, a manufacturer of radio equipment and owner of a broadcast network based in Cincinnati, Ohio. He had named the airplane The New Cincinnati. Miss Nichols called it Akita.
While landing at the Saint John airport in Millidgeville, her plans went awry. . .
Miss Nichols wrote about it in Wings For Life:
As I peered down at a tiny airport set like a bowl in the midst of surrounding wooded hills and cliffs, I thought at first I must be off course—this couldn’t be the St. Johns field. . .
Twice I circled, studying the small, rock-enclosed field from every angle. How on earth could the heavy, fast Lockheed land there? Those crossed runways would be safe only for small or lightly-loaded planes. . .
Because of the wind direction, I would have to use the shorter of the two runways—and even the longer one was inadequate. I flew back over the town, then headed back toward the airport while cutting the throttle to minimum flying speed.
I slid in over the trees and edged through a narrow ravine. So far, so good. Maybe my luck was holding. Dead ahead was the runway. I made an S turn for the proper approach and headed straight into the blinding rays of the sun. I couldn’t look ahead to gauge the length of the runway, because ahead was a fiery glare. Only by staring down through the cockpit window could I see even the edge of the runway. . .
Suddenly the dazzling blaze of the sun was doused by the shadow of a cliff and I saw to my horror that I had passed the intersection and still had flying speed. . .
. . . then came a splintering crack as the tail broke through the treetops. More rocks ahead—a deafening shuddering C-R-A-S-H—then paralyzing silence. From seventy miles an hour minimum climbing speed with a load the motor impacted to a dead stop. The whole back end of the ship must be coming over on top of me, relentlessly bearing down, pushing my head and shoulders down between my knees.
Splintering pain, and the silence of catastrophe.
—Wings for Life, by Ruth Nichols, J.B. Lippincott, Philadephia, 1957
Ruth Nichols suffered five fractured vertebrae and would spend months recovering. The airplane would be repaired. This was not the first time the Vega had been damaged, nor would it be the last.
A contemporary newspaper reported the accident:
. . . She had left New York at 3:22 P.M. and it was just 3 hours and 48 minutes later that she cracked up, at 7:10 P.M., New York time.
A great crowd had gathered at the St. John airport to see her land. She had announced her intention of spending the night there and proceeding to Harbor Grace, N. F., tomorrow.
Blinded by Sun.
Her plane hove into sight and took a long graceful slant downward to alight. Then, as she straightened out to land, the sun shone full into her eyes. For just one second she was blinded and in that second overshot the runway and nosed over.
Mechanics at the field awaited the arrival of Col. Clarence Chamberlin, Miss Nichols’ technical adviser, to decide what could be done for the plane.
—Daily News, Vol. 12, No. 310, Tuesday, 23 June 1931, at Page 13, Column 1
Miss Nichols did not make the solo transatlantic flight. That would take place the following Spring. The pilot would be Miss Amelia Mary Earhart.
Nichols’ airplane was a 1928 Lockheed Model 5 Vega Special, serial number 619, registered NR496M, and owned by Powell Crosley, Jr.
Built by the Lockheed Aircraft Company, Burbank, California, the Vega was a single-engine high-wing monoplane with fixed landing gear. It was flown by a single pilot in an open cockpit and could be configured to carry four to six passengers.
The Lockheed Vega was a very state-of-the-art aircraft for its time. The prototype flew for the first time 4 July 1927 at Mines Field, Los Angeles, California. It used a streamlined monocoque fuselage made of molded plywood. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them.
The Model 5 Vega is 27 feet, 6 inches (8.382 meters) long with a wingspan of 41 feet (12.497 meters) and overall height of 8 feet, 2 inches (2.489 meters). Its empty weight is 2,595 pounds (1,177 kilograms) and gross weight is 4,500 pounds (2,041 kilograms).
Nichols’ airplane was powered by an air-cooled, supercharged 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp C nine-cylinder radial engine with a compression ratio of 5.25:1. It was rated at 420 horsepower at 2,000 r.p.m. at Sea Level, burning 58-octane gasoline. The engine drove a two-bladed controllable-pitch Hamilton Standard propeller through direct drive. The Wasp C was 3 feet, 6.63 inches (1.083 meters) long, 4 feet, 3.44 inches (1.3-7 meters) in diameter and weighed 745 pounds (338 kilograms).
The standard Vega 5 had a cruising speed of 165 miles per hour (266 kilometers per hour) and maximum speed of 185 miles per hour (298 kilometers per hour). The service ceiling was 15,000 feet (4,572 meters). Range with standard fuel tanks was 725 miles (1,167 kilometers).
17–18 June 1928: Amelia Mary Earhart became the first woman to cross the Atlantic Ocean by air when she accompanied pilot Wilmer Lower Stultz and mechanic Louis Edward Gordon as a passenger aboard the Fokker F.VIIb/3m, NX4204, Friendship. The orange and gold, float-equipped, three-engine monoplane had departed from Trepassey Harbor, Newfoundland and Labrador, Canada, and arrived at Burry Port, on the southwest coast of Wales, 20 hours, 40 minutes later.
Amelia Earhart wrote 20 hrs. 40 min.—Our Flight in the Friendship (G.P. Putnam’s Sons, New York, 1928), describing her adventure.
Friendship had been originally ordered by Richard E. Byrd for his Antarctic expedition, but because Ford Motor Company was a major sponsor, he made the decision to switch to a Ford Tri-Motor airplane. Byrd sold the new Fokker to Donald Woodward, heir to the Jell-O Corporation, for $62,000, and it was registered to his Mechanical Science Corp., of Le Roy, New York. Woodward then leased the airplane to Mrs. Frederick Edward Guest (née Anne T. Phipps, also known as Amy Phipps) for her to cross the Atlantic Ocean by air. She chose the name Friendship for the airplane.
Mrs. Guest was a daughter of Henry Phipps, Jr., an American industrialist. She was married to Captain the Right Honourable Frederick Edward Guest P.C., C.B.E., D.S.O., M.P., a prominent British politician, former Secretary of State for Air, and a member of His Majesty’s Most Honourable Privy Council. Amy Phipps Guest, however, was a multi-billionaire in her own right.
Mrs. Guest was not a pilot, so Stultz and Gordon had been hired to fly the airplane. When her family ruled out her transoceanic journey, “an American girl of the right type” was selected to make the flight in her place. Miss Amelia Mary Earhart, a social worker living in Boston, was interviewed and was the candidate selected.
Although Earhart was a pilot with approximately 500 hours of flight experience, she did not act as a pilot on this flight. She was, however, the aircraft commander. Instructions from Mrs. Guest’s attorney, David T. Layman, to Stultz and Gordon, dated 18 May 1928, were very specific on this matter:
“This is to say that on arrival at Trepassey of the tri-motor Fokker plane “FRIENDSHIP” if any questions of policy, procedure, personnel or any other question arises the decision of Miss Amelia M. Earhart is to be final. That she is to have control of the plane and of the disposal of the services of all employees as fully as if she were the owner. And further, that on arrival of the plane in London full control of the disposition of the plane and of the time and services of employees shall be hers to the same extent until and unless the owner directs otherwise.”
— The Sound of Wings by Mary S. Lovell, St. Martin’s Press, New York, 1989, Chapter 11 at Page 104.
It was during the planning for this flight that Earhart first met her future husband, George Palmer Putnam.
Though Friendship was equipped with aluminum pontoons for water takeoffs and landings, it was otherwise the same type as Southern Cross, the airplane that Sir Charles E. Kingsford Smith flew from the United States to Australia earlier in the month. It was built by Anton H.G. Fokker’s N. V.Nederlandsche Vliegtuigenfabriek at Veere, Netherlands, in early 1928. Friendship , serial number 5028, was the fourth aircraft in the series. Flown by Bernt Balchen, it made its first flight 16 February 1928.
The Fokker F.VIIb/3m is a three-engine high-wing passenger transport with fixed landing gear. It could carry up to 8 passengers. The airplane was was 14.6 meters (47.9 feet) long, with a wingspan of 21.7 meters (71.2 feet) and 3.9 meters (12.8 feet) high. The wing had an area of 67 square meters (721 square feet). Its empty weight was 3,050 kilograms (6,724 pounds) and the gross weight, 5,200 kilograms (11,464 pounds).
The F.VIIb/3m was powered by three 787.26-cubic-inch-displacement (12.90 liter) air-cooled Wright Aeronautical Corporation Model J-5C Whirlwind nine-cylinder radial engines. The left engine was serial number 8229, the center, 8280, and the right engine, 8321. These were direct-drive engine with a compression ratio of 5.1:1. The J-5C was rated at 200 horsepower at 1,800 r.p.m., and 220 horsepower at 2,000 r.p.m. They drove two-bladed Standard adjustable-pitch propellers. The Wright J-5C was 2 feet, 10 inches (0.864 meters) long and 3 feet, 9 inches (1.143 meters) in diameter. It weighed 508 pounds (230.4 kilograms).
The standard F.VIIb/3m had a cruise speed of cruise 170 kilometers per hour (106 miles per hour), and maximum speed of 190 kilometers per hour (118 miles per hour). Its service ceiling was 4,750 meters (15,584 feet). It had a normal range of 1,240 kilometers (771 miles). NX4204 was modified at Fokker’s American subsidiary, Atlantic Aircraft Corporation in Teterboro, New Jersey, increasing the total fuel capacity to 870 gallons (3,293 liters).
Friendship was sold to José Roger Balet of Argentina in May 1929, and renamed 12 de Octubre, the date of an important national holiday. On 21 June 1931, the airplane was on a commercial flight from Santiago de Chile to Mendoza when it made an emergency landing in Alto Sierra. It was acquired by General Enrique Bravo for the Fuerza Aérea Nacional, November 1931.
The ultimate fate of the airplane is uncertain. Sources indicate that it was removed from service and salvaged for parts after June 1932. Other sources indicate that it was destroyed by accident or fire in September 1934.
14–15 June 1919: Captain John William Alcock, D.S.C., and Lieutenant Arthur Whitten Brown, both of the Royal Air Force, crossed the Atlantic Ocean, non-stop, aboard their twin-engine Vickers Vimy F.B.27A Mk.IV biplane bomber. This was the very first successful non-stop trans-Atlantic crossing by air.
Alcock and Brown took off from Lester’s Field, St. John’s, Newfoundland, at 16:13 GMT (2:43 p.m., NDT), 14 June 1919. They flew 1,890 miles (3,042 kilometers) to Clifden, County Galway, Ireland.
During their flight, they encountered heavy fog, icing, snow and severe turbulence. Four times Brown had to go out on the wings to clear snow and ice from the engine intakes.
The Vimy crossed the coast of Ireland at 9:25 a.m., British Summer Time (08:40 GMT), and touched down on the soft ground of Derrygimla Bog, just south of Clifden, at 9:40 a.m., BST. The airplane pitched over on its nose and was damaged, but Alcock and Brown were not hurt.
The total duration of their flight was 16 hours, 27 minutes.
The following report was published in The New York Times:
Captain Alcock’s Own Narrative of His Flight From Newfoundland to Ireland
LONDON, June 16. (By telegraph from Clifden, Ireland.) We have had a terrible journey. The wonder is that we are here at all. We scarcely saw the sun or the moon or the stars. For hours we saw none of them.
The fog was very dense, and at times we had to descend to within 300 feet of the sea. For four hours the machine was covered in a sheet of ice caused by frozen sleet; at another time the sleet was so dense that my speed indicator did not work, and for a few seconds it was very alarming.
We looped the loop, I do believe, and did a very steep spiral. We did some very comic “stunts,” for I have had no sense of the horizon.
The winds were favorable all the way: northwest and at times southwest. We said in Newfoundland we could do the trip in 16 hours, but we never thought we should. An hour and a half before we saw land we had no certain idea where we were, but we believed we were at Galway or thereabouts. Our delight in seeing Eashal Island and Turbot Island (5 miles west of Clifden) was great. People did not know who we were when we landed, and thought we were scouts on the lookout for the “Vimy.”
We encountered no unforeseen conditions. We did not suffer from cold or exhaustion except when looking over the side; then the sleet chewed bits out of our faces. We drank coffee and ale and ate sandwiches and chocolate.
The flight has shown that the Atlantic flight is practicable, but I think it should be done not with an aeroplane or seaplane, but with a flying boat. We had plenty of reserve fuel left, using only two-thirds of our supply.
The only thing that upset me was to see the machine at the end get damaged. From above, the bog looked like a lovely field, but the machine sank into it up to the axle and fell over on to her nose.
—The New York Times, 16 June 1919, Page 1, Columns 7 and 8
The construction of the Trans-Atlantic “Vickers-Vimy-Rolls” was completed at the Weybridge Aeroplane Works of Messrs. Vickers, Limited.
This aeroplane is practically similar in every respect to the Standard “Vimy” as supplied to His Majesty’s Government.
Two standard 350 hp. Rolls-Royce engines are installed. The capacity of the petrol tanks has been increased to 865 gallons, and the lubricating oil tanks to 50 gallons, and with this quantity of fuel this aeroplane has a range of 2440 miles. The maximum speed is over 100 miles per hour. The span of the “Vickers-Vimy-Rolls” is 67 feet, and overall length is 42 feet 8 inches. The width of the planes is 10 feet 6 inches. A wireless telegraphy set capable of sending and receiving messages over long distances was carried, and the pilot and navigator wore electrically heated clothing.
—AIRCRAFT JOURNAL, Vol. IV., No. 25, Saturday, 21 June 1919, at Page 9, Column 3
After their historic flight, Captain Alcock and Lieutenant Brown were invested Knight Commanders of the Order of the British Empire by King George V in a ceremony at Windsor Castle, 21 June 1919. They also had won a prize of £10,000 offered by Alfred Harmsworth, 1st Viscount Northcliffe, owner of the Daily Mail, and which was presented to them at the Savoy Hotel, 20 June, by Winston Churchill, Secretary of State for War, and the future prime minister. The pilots insisted that £2,000 go to the Vickers and Rolls-Royce mechanics who had prepared their airplane. They also received 2,000 guineas from the Ardath Tobacco Co., and £1,000 from Mr. Lawrence R. Phillips.
Alcock and Brown’s airplane was a Vickers F.B.27 Mk.IV Vimy, serial number C105. The Royal Air Force registration was B9952. The owner of the aircraft was the manufacturer, Vickers Limited. On 1 May 1919, it was assigned Certificate of Registration No. 18, with the civil registration G-EAAR. Contemporary photographs of the Vimy do not show any registration markings, however.
The Vickers Vimy F.B.27 (named after the World War I Battle of Vimy Ridge) was designed and built by Vickers Ltd. (Aviation Department) at Weybridge, Surrey, England. It was a twin-engine, three-bay biplane night bomber built for the Royal Air Force. The Vimy’s construction was typical of the time: a wooden framework covered with doped fabric. The engines were placed in individual nacelles, midway between the upper and lower wings. Each nacelle was supported by four vertical struts. The horizontal stabilizer/elevator were also biplane, and it had two vertical fins/rudders.
The Vimy was 43 feet, 6½ inches (13.272 meters) long with a wingspan of 67 feet, 2 inches (20.472 meters) and height of 15 feet, 8 inches (4.775 meters). The upper and lower wings had a chord of 10 feet, 6 inches (3.200 meters). The total wing area was 1,330 square feet (123.6 square meters). The vertical gap between the wings was 10 feet, 0 inches (3.048 meters) and there was no stagger. Both wings had and angle of incidence of 3½° and 3° dihedral.
The bomber weighed 6,700 pounds (3,039 kilograms) empty, and had a gross weight of 12,500 pounds (5,670 kilograms).
The Vimy was powered by two water-cooled, normally-aspirated, 1,240.5-cubic-inch-displacement (20.3 liter) Rolls-Royce Eagle VIII single overhead cam 60° V-12 engines with two valves per cylinder and a compression ratio of 4.9:1. These engines were rated at 350 horsepower at 1,800 r.p.m., and 360 horsepower at 2,035 r.p.m. (five minute limit). They turned four-bladed, fixed-pitch, wooden propellers through a 1.60:1 gear reduction. The Eagle VIII used four Rolls-Royce/Claudel Hobson carburetors and four Watford magnetos with two spark plugs per cylinder. Fuel consumption at normal power at Sea Level was 23 gallons (87 liters) per hour. The engine weighed 847 pounds (384 kilograms).
The Vimy had a maximum speed of 98 miles per hour (158 kilometers per hour) at 5,000 feet (1,524 meters). In standard configuration, the bomber had a range of 835 miles (1,344 kilometers). Its service ceiling was 10,500 feet (3,200 meters). Vimy C105 was modified by Vickers to carry 1,050 gallons (3,975 liters) of gasoline for the transoceanic flight.
The Vimy was repaired by Vickers and Rolls-Royce, then donated to the London Science Museum where it is displayed near Amy Johnson’s DH.60G Gipsy Moth, Jason. Its civil registration was cancelled in May 1920.
John William Alcock was born 6 November 1892, at Seymour Grove, Old Trafford, Stretford, a town near Manchester, England. He was the son of John Alcock, a coachman, and Mary Alice Whitelegg Alcock, a domestic servant.
He took an early interest in flying. Work as a mechanic at the Ducrocq School, Brooklands Aerodrome, Surrey, led to flight training. He was awarded pilot’s certificate No. 368 by the Royal Aero Club, 26 November 1912.
Alcock competed in various air races, winning the Easter Aeroplane Handicap at Brooklands with a Farman B, 24 March 1913. The prize for first place was 50 guineas.
With the onset of World War I, Alcock entered the Royal Naval Air Service, 12 November 1914. as a Warrant Officer, Second Grade (temporary). Alcock was assigned as a flight instructor at the Naval Flying School, Eastchurch, on the Isle of Sheppey, Kent, England. He was commissioned a Flight Sub-Lieutenant (tempy) 29 December 1915 and was sent to a squadron based on an island in the Aegean Sea. Alcock was flying a Sopwith Camel when he shot down an enemy airplane and forced two others into the sea. For this action he was awarded the Distinguished Service Cross:
13318 SUPPLEMENT to the LONDON GAZETTE, 19 DECEMBER, 1917.
Flt. Lieut. John William Acock, R.N.A.S. (now prisoner).
For the great skill, judgement and dash displayed by him off Mudros on the 30th September, 1917, in a successful attack on three enemy seaplanes, two of which were brought down in the sea.
After Alcock returned to base, he took a Handley Page O/100 bomber on a mission against Constantinople. When one engine failed, he turned back, but then the second failed and the airplane went down in the Gulf of Xeros. He and his two crewmen then swam to the enemy-held Gallipoli shoreline. They were captured and held as prisoners of war.
While held as a prisoner, Alcock was promoted to Flight Lieutenant (tempy), R.N.A.S., 31 December 1917.
On 1 April 1918, the Royal Flying Corps and Royal Naval Air Service were combined to establish the Royal Air Force. Flight Lieutenant Alcock, R.N.A.S., became Captain Alcock, R.A.F.
When The War to End All Wars came to an end in November 1918, Captain Alcock was repatriated to the United Kingdom, arriving at Dover 16 December 1918. He left military service in March 1919 and joined Vickers Ltd. (Aviation Department) as a test pilot.
While flying the prototype Vickers Viking to the Paris Air Show, Captain Sir John William Alcock, K.B.E., D.S.C., was killed in an accident at Cottévard, France, 18 December 1919. His remains were interred at the Southern Cemetery, Chorlton-cum-Hardy, Greater Manchester, England.
Arthur Whitten Brown was born at Crosshills, Glasgow, Scotland, 23 July 1886. He was an American citizen by birth. His parents were Arthur George Brown, a mechanical engineer for Westinghouse, and Emma Whitten Brown.
(Mr. Brown had been sent by Westinghouse to find a location for an electrical equipment factory, which was eventually built in Old Trafford, John Alcock’s birthplace.)
In 1914, Brown enlisted in the British Army.
In September 1919, Sir Arthur Whitten Brown married Miss Marguerite Kathleen Kennedy, at St. Martin’s, London. They would have a son, Arthur, who would become a pilot in the Royal Air Force. He was killed in action on D-Day, 6 June 1944, in Holland.
During World War II, Sir Arthur returned to active duty in the Royal Air Force. He instructed in navigation.
Lieutenant-Colonel Sir Arthur Whitten Brown, K.B.E., died at his home in Swansea, Wales, 4 October 1948, at the age of 62 years. His ashes interred at St. Margaret Churchyard, Tylers Green, Wycombe District Buckinghamshire.
27 May 1919: NC-4, designating number A2294, one of three United States Navy Curtiss NC flying boats, arrived at the harbor of Lisbon, Portugal, becoming the first airplane to cross the Atlantic Ocean.
NC-4 was under the command of Lieutenant Commander Albert Cushing Read, United States Navy, who also served as navigator. The pilots were First Lieutenant Elmer Fowler Stone, United States Coast Guard, and Lieutenant (j.g.) Walter T. Hinton, U.S. Navy. Lieutenant James L. Breese, USN and Chief Machinist Mate Eugene S. Rhoads, USN, were the engineers. Ensign Herbert C. Rodd, USN, was the radio operator.
Aboard the other aircraft were several officers who would rise to high rank in the Navy: Commander John Henry Towers would later command the Pacific Fleet; Lieutenant Marc A. Mitscher commanded the Fast Carrier Task Force during World War II, and later commanded the Atlantic Fleet. Lieutenant Patrick N.L. Bellinger commanded Patrol Wing 2 at Pearl Harbor on 7 December 1941, and would go on to command Naval Air Forces, Atlantic Fleet.
Three Curtiss flying boats, NC-1 (A2291), NC-3 (A2293) and NC-4 (A2294), under the command of Commander Towers in NC-3, departed Naval Air Station Rockaway, New York City, New York, United States of America, at 10:00 a.m., 8 May 1919, and flew to NAS Chatham, Massachusetts.
During the flight, NC-4 developed an oil leak from the center pusher engine, so it was shut down. This slowed the airplane but it was still able to continue. In mid-afternoon, however, the center tractor engine suffered a failed connecting rod. With only two engines operating, NC-4 was forced down at sea, approximately 80 miles (129 kilometers) from Chatham. The sea was calm and the flying boat taxied the remaining distance on the water. It arrived there at 7:00 a.m., 9 May.
At the air station, the failed engine was replaced with a 300 horsepower Liberty L12, the only spare engine available. The leaking engine was repaired.
Delayed several days by weather, NC-4 departed NAS Chatham at 9:15 a.m., 14 May, and flew to Halifax, Nova Scotia, in the Canadian Maritimes, landing there at 1:07 p.m. Continuing on to Newfoundland that day would have had them arriving after dark.
NC-4 took off from the waters of Halifax the following morning at 11:47 a.m., and arrived at Trepassey Bay, Newfoundland, at 5:41 p.m., rendezvousing with the aircraft tender USS Aroostook (CM-3). NC-1 and NC-3 had arrived two days earlier.
All three airplanes were serviced from the tender. The temporary 300 horsepower Liberty engine which had been installed on NC-4 was replaced with a correct 400 horsepower engine.
The three Curtiss flying boats took off from Trepassey Bay at 6:00 p.m. on the evening of 16 May and headed across the Atlantic Ocean to the Azores.
NC-1 and NC-3 were both forced down by rain, heavy clouds and thick fog about 200 miles short of their destination. NC-1 was damaged and unable to continue. The crew was rescued by a Greek freighter and the airplane taken in tow, but it sank several days later. NC-3 drifted for two days on surface of the Atlantic, and coming within sight of land, two engines were started and the airplane taxied into the harbor at Ponta Delgada, Ilha de São Miguel.
NC-4 deviated from its planned course and landed at Horta, on Faial Island, at 1:23 p.m., 17 May. Weather kept NC-4 at Horta for the next few days, until at 8:45 a.m. on the 20th, it took off and flew to Ponta Delgado, landing there just two hours later.
Again, NC-4 was forced to remain in harbor waiting for favorable weather. On 27 May, it was good enough to resume the journey, and the crew once again took off, this time enroute to Lisbon, Portugal.
At 8:01 p.m., 27 May 1919, NC-4 touched down on the Tagus Estuary, Lisbon, Portugal, and became the very first airplane to complete a flight across the Atlantic Ocean.
NC-4 was the fourth of ten NC flying boats designed and built by the Curtiss Aeroplane and Motor Company, Garden City, New York. It was a 3-bay biplane with a boat hull, powered by four engines installed in three nacelles between the upper and lower wings.
There were variations between the individual aircraft. NC-4’s hull was built by Herreschoff Manufacturing Company, at Bristol, Rhode Island. The hull was constructed of two layers of spruce planking with a layer of muslin and marine glue between. It was 45 feet (13.7 meters) long with a beam of 10 feet (3.0 meters and depth of 9 feet (2.7 meters).
The Curtiss NC-4 was 68 feet, 3 inches (20.803 meters) long with an upper wingspan of 126 feet, 0 inches (38.405 meters) and lower span of 96 feet, 0 inches (29.261 meters). The upper wing and the center section of the lower had no dihedral, while the lower wings’ outer panels had 3° dihedral. Their vertical gap varied from 13 feet, 6½ inches (4.128 meters), inboard, to 12 feet, 0 inches (3.658 meters). The chord was 12 feet, 0 inches (3.658 meters), and the lower wing was very slightly staggered behind the upper. The total wing area was 2,380 square feet (221.1 square meters). The biplane-configured horizontal stabilizers had an upper span of 37 feet, 11 inches (11.252 meters), no dihedral, and the vertical gap was 9 feet, 3 inches (2.819 meters). Their total surface area was 330 square feet (30.7 square meters). The overall height of the flying boat was 24 feet, 5 inches (7.442 meters).
The empty weight of NC-4 is 15,874 pounds (7,200 kilograms) and it has a gross weight of 26,386 pounds (11,968 kilograms).
Originally built with three engines, flight testing led to the addition of a fourth. These were water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Liberty L-12 single overhead cam (SOHC) 45° V-12 engines 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 (left-hand pusher), direct-drive engine. 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). Two were mounted in a center nacelle with one in tractor and one in pusher configuration. Two more were in individual nacelles in tractor configuration. The engines drove four-bladed fixed-pitch wooden propellers.
NC-4 had a maximum speed of 85 miles per hour (137 kilometers per hour), a service ceiling of 4,500 feet (1,372 meters) and range of 1,470 miles (2,366 kilometers).
NC-4 was restored by the Smithsonian Institution during the early 1960s and remains a part of its collection, though it is on long term loan to the National Museum of Naval Aviation, Pensacola, Florida.