20 September 1918

Lieutenant (j.g.) David S. Ingalls, USN, France, 1918. (U.S. Navy)
Lieutenant (j.g.) David S. Ingalls, USN, France, 1918. (U.S. Navy)

20 September 1918: While assigned to No. 213 Squadron, Royal Air Force, Lieutenant (junior grade) David Sinton Ingalls, United States Navy, shot down a Fokker D.VII reconnaissance airplane near Vlissegham, Belgium, while flying a Sopwith Camel, serial number D8177. This was Ingalls’ fifth confirmed aerial victory, making him the U.S. Navy’s only fighter ace of World War I.

Lieutenant Ingalls was awarded the Navy Cross for his actions of 15 September 1918, when “he led a flight of five machines on a low bombing raid of an enemy aerodrome. On the homeward journey he shot down a two-seater enemy aeroplane in flames. He further participated in two other low bombing raids and upon still another occasion shot down an enemy kite balloon in flames near Ostend.”  He was also awarded the Distinguished Service Medal for exceptionally meritorious service. The Royal Air Force awarded him its Distinguished Flying Cross for the 15 September mission against Uytkerke Aerodrome, and he was Mentioned in Dispatches. France appointed him Chevalier de la légion d’honneur.

Sopwith Camel F.1. (Royal Air Force)

The Sopwith Camel F.1 was a British single-place, single-engine biplane fighter, produced by the Sopwith Aviation Co., Ltd., Canbury Park Road, Kingston-on-Thames. The airplane was constructed of a wooden framework, with the forward fuselage being covered with aluminum panels and plywood, while the aft fuselage, wings and tail surfaces were covered with fabric.

The length of the Camel F.I varied from 18 feet, 6 inches (5.639 meters) to 19 feet, 0 inches (5.791 meters), depending on which engine was installed. Both upper and lower wings had a span of 28 feet, 0 inches (8.534 meters) and chord of 4 feet, 6 inches (1.372 meters). They were separated vertically by 5 feet (1.524 meters) at the fuselage. The upper wing had 0° dihedral, while the lower wing had 5° dihedral and was staggered 1 foot, 6 inches (0.457 meters) behind the upper wing. The single-bay wings were braced with airfoil-shaped streamline wires. The overall height of the Camel also varied with the engine, from 8 feet, 6 inches (2.591 meters) to 8 feet, 9 inches (2.667 meters).

The heaviest Camel F.I variant used the Le Rhône 180 h.p. engine. It had an empty weight of 1,048 pounds (475 kilograms). Its gross weight of 1,567 pounds (711 kilograms). The lightest was equipped with the Gnôme Monosoupape 100 horsepower engine, with weights of 882 pounds (400 kilograms) and 1,387 pounds (629 kilograms), respectively.

Front view of a Sopwith Camel F.I
Front view of a Sopwith Camel F.I

The first Camel was powered by an air-cooled 15.268 liter (931.72 cubic inches) Société Clerget-Blin et Cie Clerget Type 9 nine-cylinder rotary engine which produced 110 horsepower at 1,200 r.p.m. and drove a wooden two-bladed propeller. Eight different rotary engines ¹ from four manufacturers, ranging from 100 to 180 horsepower, were used in the type.

The best performance came with the Bentley B.R.1 engine (5.7:1 compression ratio). This variant had a maximum speed of 121 miles per hour (195 kilometers per hour) at 10,000 feet (3,048 meters), and 114.5 miles per hour (184 kilometers per hour) at 15,000 feet (4,572 meters). It could climb to 6,500 feet (1,981 meters) in 4 minutes, 35 seconds; to 10,000 feet (3,048 meters) in 8 minutes, 10 seconds; and 15,000 feet (4,572 meters) in 15 minutes, 55 seconds. It had a service ceiling of 22,000 feet (6,706 meters). Two other Camel variants could reach 24,000 feet (7,315 meters).

Sopwith Camel F.1 N6254, right profile. (NASA)
Lt. W.O. Bentley R.N.A.S.
Lieutenant Walter Owen Bentley, R.N.A.S.

The Bentley B.R.1 rotary engine was designed by Lieutenant Walter Owen Bentley, Royal Naval Air Service (later, Captain, Royal Air Force), based on the Clerget Type 9, but with major improvements. It used aluminum cylinders shrunk on to steel liners, with aluminum pistons. The Bentley B.R.1 (originally named the Admiralty Rotary, A.R.1, as it was intended for use by the Royal Navy) was an air-cooled, normally-aspirated 17.304 liter (1,055.9 cubic inches) nine-cylinder rotary engine with a compression ratio of 5.7:1. It was rated at 150 horsepower at 1,250 r.p.m. The B.R.1 was 1.110 meters (3 feet, 7.7 inches) long, 1.070 meters (feet, 6.125 inches) in diameter and weighted 184 kilograms (406 pounds.) The engine was manufactured by Humber, Ltd., Coventry, England.

For his work developing this engine, Captain Bentley was appointed a Member of the Military Division of the Most Excellent Order of the British Empire (M.B.E.) in the New Years Honours List, 1 January 1919. He would later found Bentley Motors, Ltd.

Sopwith Camel F.1 FG394, left rear quarter. © IWM (Q 63822)
Sopwith Camel F.1 F6394, left rear quarter. © IWM (Q 63822)

The Camel was armed with two fixed, forward-firing .303 Vickers machine guns, synchronized to fire forward through the propeller. These guns were modified for air cooling. Some night fighter variants substituted Lewis machine guns mounted above the upper wing for the Vickers guns. Four 25 pound (11.3 kilogram) bombs could be carried on racks under the fuselage.

The instruments and armament of a Sopwith Camel from No. 4 Squadron, AFC. (Australian War Memorial)
The instruments and armament of a Sopwith Camel from No. 4 Squadron, AFC. (Australian War Memorial)

The Sopwith Camel was a difficult airplane to fly. Most of its weight was concentrated far forward, making it unstable, but, at the same time making the fighter highly maneuverable. The rotary engine, with so much of its mass in rotation, caused a torque effect that rolled the airplane to the right to a much greater degree than in airplanes equipped with radial or V-type engines. A skilled pilot could use this to his advantage, but many Camels ended upside down while taking off.

Twelve manufacturers ² produced 5,490 Sopwith Camels between 1916 and 1920. By the end of World War I, it was becoming outclassed by newer aircraft, however it was the single most successful fighter of the war, shooting down 1,294 enemy aircraft. One single fighter, flown by Major William Barker, shot down 46 enemy aircraft, more than any other fighter in history.

It is believed that only seven Sopwith Camels still exist.

Lieutenant David Sinton Ingalls, Naval Reserve Flying Corps, circa 1919. (U.S. Naval Institute)

David Sinton Ingalls was born 28 January 1899 at Cleveland, Ohio. He was the son of Albert Stimson Ingalls, a vice president of the New York Central Railroad, and Jane Ellison Taft Ingalls, niece of President William Howard Taft. He  was educated at the University School, a private school for boys in Cleveland. He entered Yale University at New Haven, Connecticut, in 1916. Ingalls was a member of The First Yale Unit, which would become the U.S. Navy’s first aviation unit.

Shortly after the United States entered World War I, David Sinton Ingalls enlisted as a Machinist’s Mate 1st Class, United States Naval Reserve Force, at New London, Connecticut, 26 March 1917. He was sent to the Naval Aviation Detachment at West Palm Beach, Florida, for initial flight training, and then to the Naval Aviation Detachment, Huntington, New York. MM1c Ingalls was discharged 1 September 1917 and appointed an Ensign, 4 September 1917. He was Naval Aviator Number 85.

Ensign Ingalls was sent to France for duty, 12 September 1917. In December 1917, he was detached and sent to the Royal Flying Corps air station at Turnberry, South Ayrshire, Scotland, for training in aerial gunnery. He then underwent squadron formation training at nearby Ayr, Scotland. Following training, Ensign Ingalls was assigned to the Naval Air Detachment at Paris, France, 12 March 1918. On 23 March 1918, Ingalls was promoted to the rank of Lieutenant (junior grade).

On 21 May 1918, Lieutenant (j.g.) Ingalls was assigned to the U.S. Army Bombing School at Clermont-Ferrand, France. On 27 June 1918, Lieutenant (j.g.) Ingalls was assigned to the Naval Air Station Dunkerque. He flew combat missions with No. 213 Squadron, and No. 218 Squadron, both of the Royal Air Force. (While flying with the 218th, he was reported to have shot down an observation balloon and a biplane. The records were lost and these claims are considered unconfirmed.)

While flying with No. 213 Squadron, on 11 August 1918, Lieutenant (j.g.) Ingalls shot down an Albatros C northeast of Diksmuide, West Flanders—his first confirmed victory. His second confirmed victory was a two-place Luftverkehrsgesellschaft m.b.H. (L.V.G.) biplane south of Zevecote, Belgium, on 21 August. He shot down a Rumpler C over Ostend, 15 September. His fourth confirmed victory took place on 18 September when he destroyed an observation balloon at La Barrière. The Fokker D.VII that he shot down on 20 September was his fifth. He shot down his sixth,a Rumpler, on 24 September 1918, over Saint-Pierre-Cappelle, Belgium. Other than the Fokker D.VII, Ingalls shared credit with other pilots for the shoot-downs.

Lieutenant (j.g.) Ingalls flew his final combat mission, his sixty-third, on 3 October 1918.

On 24 September 1919, he was given the provisional rank of Lieutenant, Naval Reserve Flying Corps, with date of rank, 1 April 1919. He was released from active duty 23 December 1919.

Returning to Yale University, he graduated in 1920 with a Bachelor of Arts degree, and in 1923, received a Doctor of Laws (LL.D.) degree from Harvard University, Cambridge, Massachusetts. He practiced law for several years before being elected to the state legislature of Ohio in 1926. Later, he ran for governor and United States senator.

David Sinton Ingalls married Miss Louise Hale Harkness at Locust Valley, New York, 27 June 1922. They would have five children: Edith, Jane, Anne, Louise, and David.

Flag of the Assistant Secretary of the Navy for Aeronautics

Ingalls was appointed Assistant Secretary of the Navy for Aeronautics by President Herbert Hoover, serving from 16 March 1929 until 1 June 1932, reporting to Secretary of the Navy Charles Francis Adams III.

Secretary Ingalls’ photograph was featured on the cover of TIME Magazine, 2 March 1931.

Assistant Secretary of the Navy for Aeronautics David Sinton Ingalls was featured on the cover of TIME Magazine, 2 March 1931. Photograph by Underwood & Underwood. (TIME Magazine)

On 24 December 1931, Ingalls was appointed a Lieutenant Commander, United States Naval Reserve.

Going to work in the business sector, Ingalls became vice president and general manager of Pan American Air Ferries, a commercial transport service from the United States to Egypt, and which also transported newly-built military aircraft from the United States via South America, across the South Atlantic Ocean to Africa, and then on to the Middle East.

Lieutenant Commander Ingalls was promoted to Commander, U.S.N.R., 1 July 1941, and following the United States entry into World War II, he was recalled to active duty, 23 November 1942. Commander Ingalls served as Assistant Operations Officer on the staff of the Commander, Naval Air Forces, Pacific, (COMNAVAIRPAC), for which he was awarded the Legion of Merit. He was promoted to Captain, 10 June 1943. He then served as chief of staff to the Commander Aircraft South Pacific Force, Admiral Aubrey W. Fitch, USN.

Captain Ingalls took command of U.S. Naval Air Station 29 (now, Daniel K. Inouye International Airport—HNL—Honolulu, Hawaii) on 1 April 1944.

Captain Ingalls was released from active duty 8 November 1945, but he remained an officer in the Naval Reserve. Ingalls returned to Pan American World Airways as vice president, and remained in that position until 1949. Later, he was president and publisher of the Cincinnati Times-Star newspaper, and a vice president of Taft Broadcasting Company.

David Sinton Ingalls, April 1952. (Nina Leen/LIFE Magazine)

By 1951, Ingalls held the rank of Commodore. On 1 July 1955, Commodore Ingalls was promoted to the rank of Rear Admiral. From 1945 until 1959, Ingalls was Commander, Navy Reserve Forces Command (COMNAVRESFORCOM). He retired from the Naval Reserve in February 1959.

During his Naval career, Rear Admiral Ingalls had been awarded the Navy Cross, the Distinguished Service Medal, the Legion of Merit, the Bronze Star, World War I Victory Medal, American Defense Service Medal, American Campaign Medal, Asiatic-Pacific Campaign Medal with four service stars, the World War II Victory Medal, the National Defense Service Medal, the Naval Reserve Medal, and the Armed Forces Reserve Medal with hourglass device.

Miss Louise Hale Harkness Ingalls with her father, David S. Ingalls, 1980. (Historic Images)

Louise Harkness Ingalls died in 1978. David Ingalls married his second wife, Frances W. Wragg, 16 February 1979.

Ingalls is the author of Hero of the Angry Sky: The World War I Diary and Letters of David S. Ingalls, America’s First Naval Ace, Ohio University Press, 2013 (Edited by Geoffrey L.  Rossano).

Rear Admiral David Sinton Ingalls died 26 April 1985 at the age of 86 years. He is buried at the Warm Springs Cemetery, Warm Springs, Virginia.

¹ Humber, Ltd., Bentley B.R.1 150 h.p., B.R.1 (5.7:1 c.r.); Clerget 9B, 130 h.p., Clerget 9Bf, 130 h.p. (long stroke): Gnôme Monosoupape,  100 h.p., Gnôme Monosoupape, 150 h.p.; Le Rhône, 110 h.p., and Le Rhône 180 h.p.

² Sopwith Aviation Co., Ltd., Kingston-on-Thames; Boulton and Paul, Ltd., Norwich; British Caudron Co., London; Clayton and Shuttleworth, Ltd., Lincoln; Hooper and Co., Ltd., London; March, Jones and Cribb, Ltd., Leeds; Nieuport and General Aircraft Co., Ltd., London; Ruston, Proctor and Co., Ltd., Lincoln; Fairey Aviation Co., Ltd.; Portholme Aerodrome Ltd., Huntingdon; Wm. Beardmore & Co., Ltd., Glasgow; Pegler & Co., Ltd., Doncaster.

© 2017, Bryan R. Swopes

20 September 1904

Wilbur Wright, 1867–1912. (Library of Congress)

20 September 1904: In an effort to improve their airplane, the Wright Brothers moved their test flights from the windy Kill Devil Hills of North Carolina to Huffman Prairie, near Dayton, Ohio. Without the winds, however, they needed to achieve greater speed for the airplane to take off, so they devised a catapult which used a 1,200 pound (544 kilogram) weight dropped from a 20 foot (6.1 meter) wooden derrick to pull the Wright Flyer II down a wooden track.

The Wright Flyer II was very similar to the original Flyer. Some parts of the airframe were strengthened, which slightly increased the new airplane’s weight.

Wilbur Wright was at the controls of the Flyer II on 20 September 1904, when it made the first-ever complete circular turn by an airplane. This was witnessed by Ames I. Root, who wrote about it in his magazine, Gleanings in Bee Culture:

“When it turned that circle, and came near the starting-point, I was right in front of it, and I said then and I believe still, it was. . . the grandest sight of my life. Imagine a locomotive that has left its track, and is climbing right toward you – a locomotive without any wheels. . . but with white wings instead. . . Well, now, imagine that locomotive with wings that spread 20 feet each way, coming right toward you with the tremendous flap of its propellers, and you have something like what I saw.”

The 30th flight of Flyer II at Huffman Prairie, August 1904. (Wright State University)

The Wright Brothers flew the Flyer II 105 times that summer. Next would come the Flyer III.

Wilbur Wright and the Flyer II on Flight 85 at Huffman Prairie. (Wright State University)

© 2015, Bryan R. Swopes

19 September 1969

The first prototype V-24 which first flew September 19, 1969.. (From "Russian Gunship Helicopters" by Yefim Gordon, Page 6)
The first prototype V-24. The stub wings are nearly horizontal. (Image from “Russian Gunship Helicopters,” by Yefim Gordon, Pen and Sword Aviation 2013, at Page 6)
Алфёров Герман Витальевич
Алфёров Герман Витальевич

19 September 1969: After four days of testing in a tethered hover, OKB Mil Design Bureau test pilot Herman V. Alferov made the first free flight of the prototype Mil Mi-24 attack helicopter, V-24.

Designed by a team led by Chief Project Engineer V. A. Kuznetsov, the Mi-24 used the drive train of the Mil Mi-8 Hip-B/C transport and Mi-14 Haze-A anti-submarine helicopters. It had a five-blade main rotor. a three-blade tail rotor and was equipped with retractable tricycle landing gear.

The Mi-24 (named “Hind” by NATO forces) was operated by a pilot and a weapons system operator seated in tandem configuration, with the pilot slightly offset to the left. The gunner is in the forward position. It differed from the American Bell AH-1G Cobra attack helicopter in that it could carry 8 troops or 1,500 pounds (680 kilograms) of cargo in a center fuselage compartment.

Prototype V-24 during test flight. (Unattributed)
Prototype V-24 during test flight. (Unattributed)

The Mi-24 is 17.5 meters (57 feet, 5 inches) long, 6.5 meters (21 feet 4 inches) high, with a main rotor diameter of 17.3 meters (56 feet, 9 inches). As is standard practice with Soviet helicopters, the five-blade main rotor turns clockwise as seen from above. (The advancing blade is on the left.) The tail rotor diameter is 3.9 meters (12 feet, 9½ inches).

The entire fuselage is tilted 2° 30′ (and thus, the transmission, mast and main rotor) to the right to counteract the rotor system’s translating tendency, and helps with high-speed stability.

In early versions, the tail rotor was mounted on the right side in pusher configuration and rotated counter-clockwise as seen from the left. (The advancing blade is above the axis of rotation.) Because of poor handling conditions, the tail rotor was changed to the left side in tractor configuration, with the advancing blade below the hub.

The helicopter’s empty weight is 8,500 kilograms (18,739 pounds) and loaded weight is 12,000 kilograms (26,455 pounds).

Power is supplied by two Isotov TV3-117 turboshaft engines rated at 1,700 shaft horsepower, or 2,200 horsepower for takeoff or one engine inoperative emergency operation.

The Mi-24 has a maximum speed of 335 kilometers per hour (208 miles per hour) and range of 450 kilometers (280 miles). The service ceiling is 4,500 meters (14,764 feet).

Armament consists of a turret-mounted Gryazev-Shipunov GSh-23 23mm cannon with 450 rounds of ammunition. Air-to-air and air-to-ground missiles are carried on pylons mounted under the helicopter’s stub wings.

More than 5,200 Mi-24 attack helicopters have been built, many of them exported. It is estimated that the cost of an individual helicopter is $32,500,000.

Prototype Mil Mi-24 helicopter, which first flew September 19, 1974. (Russian Helicopters photo)
“Red 77,” the prototype Mil Mi-24A helicopter. Note the anhedral of the wings. (Russian Helicopters photo)

Herman V. Alferov (Алфёров Герман Витальевич)—also known as G.V. Alferov or German V. Alferov—was born at Moscow, Russia, U.S.S.R., 11 April 1934. He graduated from the 3rd Moscow Flying Club in 1950, and from 1952 to 1954 was a flight instructor at the Central Aeroclub Chkalov. In 1954,  He graduated from the Voluntary Society of Assistance to the Air Force (DOSAAF) central flight technical school at Saransk in the Mordovian Autonomous Oblast.

Alferov was employed as a test pilot at OKB Mil in Moscow from 1954 until 1982, and remained with the flight test center until 1992. He participated in setting 11 Fédération Aéronautique Internationale (FAI) world helicopter records, and was named an Honored Test Pilot of the Soviet Union, 16 November 1973. In 1977, he was awarded the Order of the October Revolution, twice received the Order of the Red Banner of Labor, and twice the Order of the Red Star.

Herman V. Alferov died 19 January 2012.

Herman V. Alferov with a Mil Mi-4 helicopters.
Herman V. Alferov with a Mil Mi-4 helicopter, circa 1960. (Unattributed)

© 2016, Bryan R. Swopes

19 September 1944

19 September 1944:

Air Ministry, 13th November, 1945.

     The KING has been graciously pleased to confer the VICTORIA CROSS on the undermentioned officer in recognition of most conspicuous bravery:—

Flight Lieutenant David Samuel Anthony LORD, D.F.C. (49149), R.A.F., 271 Sqn. (deceased).

Flight Lieutenant Lord was pilot and captain of a Dakota aircraft detailed to drop supplies at Arnhem on the afternoon of the 19th September, 1944. Our airborne troops had been surrounded and were being pressed into a small area defended by a large number of anti-aircraft guns. Air crews were warned that intense opposition would be met over the dropping zone. To ensure accuracy they were ordered to fly at 900 feet when dropping their containers.

While flying at 1,500 feet near Arnhem the starboard wing of Flight Lieutenant Lord’s aircraft was twice hit by anti-aircraft fire. The starboard engine was set on fire. He would have been justified in leaving the main stream of supply aircraft and continuing at the same height or even abandoning his aircraft. But on learning that his crew were uninjured and that the dropping zone would be reached in three minutes he said he would complete his mission, as the troops were in dire need of supplies.

By now the starboard engine was burning furiously. Flight Lieutenant Lord came down to 900 feet, where he was singled out for the concentrated fire of all the anti-aircraft guns. On reaching the dropping zone he kept the aircraft on a straight, and level course while supplies were dropped. At the end of the run, he was told that two containers remained.

Although he must have known that the collapse of the starboard wing could not be long delayed, Flight Lieutenant Lord circled, rejoined the stream of aircraft and made a second run to drop the remaining supplies. These manoeuvres took eight minutes in all, the aircraft being continuously under heavy anti-aircraft fire.

His task completed, Flight Lieutenant Lord ordered his crew to abandon the Dakota, making no attempt himself to leave the aircraft, which was down to 500 feet. A few seconds later, the starboard wing collapsed and the aircraft fell in flames. There was only one survivor, who was flung out while assisting other members of the crew to put on their parachutes.

By continuing his mission in a damaged and burning aircraft, descending to drop the supplies accurately, returning to the dropping zone a second time and, finally, remaining at the controls to give his crew a chance of escape, Flight Lieutenant Lord displayed supreme valour and self-sacrifice.

Fourth Supplement to The London Gazette, 13 November 1945, No. 37347 at Page 5533.

The Victoria Cross: “For Valour”
Flight Lieutenant David Samuel Anthony Lord, D.F.C., Royal Air Force.

David Samuel Anthony Lord was born in the city of Cork, Ireland, 18 October 1913, the son of Warrant Officer Samuel Beswick Lord, Royal Welsh Fusiliers, and Mary Ellen Miller Lord. He was raised in Ireland, British India and Wales. Lord was educated at St. Mary’s College, a seminary in Aberystwyth, Ceredigion, Wales, and the University of Wales in Cardiff.

David and his brother Frank enlisted in the Royal Air Force 6 August 1936. In 1938 he was promoted to corporal and requested an assignment to flight training. He trained as a pilot at RAF Uxbridge, and on completion, 5 April 1939, was promoted to sergeant.

Sergeant Lord was assigned to No. 31 Squadron, a bomber/transport unit then based at Lahore, Punjab, in what is now Pakistan. The squadron was equipped with Vickers Type 264 Valentia biplane transports, but early in World War II these were replaced by more modern Douglas DC-2s. The squadron flew in Iraq, Syria, Iran and Eqypt. Lord was promoted to Flight Sergeant, 1 April 1941. In June 1941, Lord’s Dakota was severely damaged by attacking German fighters and he was forced to crash land. Along with his passengers and crew, Lord safely returned to friendly lines.

Flight Sergeant Lord was appointed a warrant officer, 1 October 1941. In 1942, Temporary Warrant Officer Lord returned to operations in India, where he flew “the Hump,” the aerial supply line to China over the Himalaya Mountains. He was appointed to the commissioned rank of Pilot Officer on probation (emergency), 12 May 1942, and then promoted to Flying Officer.

Douglas Dakota Mk.III, FL512, of No. 31 Squadron in Burma, circa 1944.

In The London Gazette, 16 July 1943, it was announced that Flying Officer Lord had awarded the Distinguished Flying Cross for his actions in Burma.

Flying Officer Lord was reassigned to No. 271 Squadron, based at RAF Down Ampney, Wiltshire, England, flying the Dakota Mk.III. He was promoted to Flight Lieutenant, 2 June 1944, and flew in the airborne assault of Normandy, on the night of 5–6 June 1944. On 1 September 1944, Flight Lieutenant Lord was commended by George VI for valuable service in the air.

19 September 1944. Burnt-out Douglas Dakota Mark III, KG401, of No. 48 Squadron RAF. The same type aircraft as Flight Lieutenant Lord’s KG374, this is one of many Dakota’s lost while attempting to resupply Allied soldiers during the Battle of Arnhem. © IWM (CE 165)

Only one member of Lord’s crew, the navigator, Flight Lieutenant Harold King, survived. The others were buried next to the wreck of their Dakota, at Wolfheze, just northeast of Arnhem, The Netherlands. Following the war, their remains were moved to the Arnhem Oosterbeek War Cemetery.

Flight Lieutenant King was captured and spent the remainder of the war at Stalag Luft I, a prisoner of war camp at Barth, Western Pomerania. When he was repatriated, he reported what had happened on the 19 September 1944 mission.

After investigation, the Victoria Cross was posthumously awarded to Flight Lieutenant David Samuel Anthony Lord, D.F.C.  His parents received his Victoria Cross at an investiture at Buckingham Palace on 18 December 1945.

Flight Lieutenant David Samuel Anthony Lord, V.C., D.F.C., was the only member of the Royal Air Force Transport Command to be awarded the Victoria Cross during World War II.

Flight Lieutenant David S.A. Lord’s medals in the Lord Ashcroft Gallery, Imperial War Museum. (Left to right, Victoria Cross; Distinguished Flying Cross; India General Service Medal 1936 with Northwest Frontier Clasp; 1939–1945 Star; Africa Star; Burma Star; France and Germany Star; Defence Medal; War Medal 1939–1945 with Bronze Oak Leaf.)

Flight Lieutenant Lord’s airplane was a Douglas Dakota Mk.III, the Royal Air Force designation for the U.S. Army Air Forces’ Douglas C-47A Skytrain. It was built in January 1944 at the Midwest City Douglas Aircraft Plant, adjacent to the Oklahoma City Air Depot (now, Tinker Air Force Base) at Oklahoma City, OK. Douglas gave it the company serial number 12383. It was a C-47A-5-DK Skytrain with the serial number 42-92568. The airplane was one of the 5,354 built by Midwest City. The plant turned out 13 C-47s each day and produced more than half of the Skytrains built during World War II.

42-92568 was delivered to the U.S.A.A.F. on 24 January 1944. The Skytrain was turned over to Royal Air Force at Dorval Airport, Montreal, Quebec, Canada, 4 February 1944, and assigned the RAF identification KG 374. It was then flown across the North Atlantic to the United Kingdom, 17 May 1944. KG 374 was assigned to No. 271 Squadron, 10 June 1944, and the squadron identification YS L.

A Battle of Britain Memorial Flight Douglas Dakota painted in the markings of Flight Lieutenant Davis Samuel Anthony Lord’s KG 374.

The Douglas C-47 Skytrain is an all-metal, twin-engine, low-wing monoplane transport with retractable landing gear. It was operated by a minimum flight crew of two pilots, a navigator and a radio operator. The airplane’s control surfaces are covered with doped-fabric. The primary differences between the civil DC-3 and military C-47 airframes was the addition of a cargo door on the left side of the fuselage and a strengthened floor in the cabin.

The C-47 is 64 feet, 5½ inches (19.647 meters) long with a wingspan of 95 feet (28.956 meters) and height of 17 feet (5.182 meters). Empty weight of the C-47A is 17,257 pounds (7,828 kilograms) and the maximum takeoff weight is 29,300 pounds (13,290 kilograms).

The C-47A was powered by two 1,829.39-cubic-inch-displacement (29.978 liter) air-cooled, supercharged R-1830-92 (Pratt & Whitney Twin Wasp S1C3-G) two-row 14-cylinder radial engines with a compression ratio of 6.7:1. These were rated at 1,060 horsepower at 2,550 r.pm., up to 7,500 feet (2,286 meters), maximum continuous power, and 1,200 horsepower at 2,700 r.p.m. at Sea Level for takeoff. Each engine drives a three-bladed Hamilton Standard Hydromatic constant-speed full-feathering propeller with a diameter of 11 feet, 6 inches (3.505 meters) through a 16:9 gear reduction. The R-1830-92 is 48.19 inches (1.224 meters) long, 61.67 inches (1.566 meters) in diameter, and weighs 1,465 pounds (665 kilograms).

The C-47 has a cruising speed of 185 miles per hour (298 kilometers per hour) at 10,000 feet (3,048 meters) and service ceiling of 24,100 feet (7,346 meters).

The C-47 could carry 6,000 pounds (2,722 kilograms) of cargo, or 28 fully-equipped paratroopers. Alternatively, 14 patients on stretchers could be carried, along with three attendants.

KG 374 crashed at Wolfheze, The Netherlands, about 6 miles (10 kilometers) northwest of Arnhem. Fragments of the wreckage are in the collection of the Imperial War Museum.

Douglas C-47 Skytrains at the Midwest City Douglas Aircraft Plant. Douglas produced 13 C-47s a day at this facility. (U.S. Air Force)

© 2018, Bryan R. Swopes

19 September 1902

Stanley Spencer’s airship over London.

19 September 1902:

The New York Times reported:

AN AIRSHIP TRAVELS NEARLY THIRTY MILES

Stanley Spencer, the Aeronaut, Astonishes Londoners.

He Starts from the Crystal Palace and Descends Near Harrow—Makes Various Detours.

     LONDON, Sept. 20.—Stanley Spencer, the well-known English aeronaut, yesterday successfully accomplished a remarkable flight over London in an airship of his own invention. It is estimated that his ship traveled nearly thirty miles.

     From the observations of those on the ground, Stanley seemed to have complete control of the vessel. He started from the Crystal Palace at 4:15 o’clock in the afternoon, and descended three hours later near Harrow. The route taken by the aeronaut was over Streatham, Clapham Common and the smoky south side of the metropolis, across the Thames, over the populous Chelsea district, and across Kensington and Earl’s Court out to Harrow. Spencer executed an easy descent at the little village of Eastcote.

     Spencer has recently been experimenting with his vessel at the Crystal Palace. Finding the conditions suitable, he suddenly decided to start on his dangerous voyage yesterday afternoon, and the usual crown of palace spectators gave him a hearty send-off. The airship at once rose to a height of about 300 feet. After traveling for about a mile with practically no deviation in course, Spencer made various detours, and seemed able to steer his ship as easily as a torpedo boat. Near Clapham Common he came fairly close to the ground for the purpose of manoeuvring. The appearance of the air craft created intense astonishment among the thousands of persons in the streets over whose heads the aeronaut passed.

      Pericval Spencer, referring to his brother’s trip, said it exceeded the longest trip of Santos-Dumont by nearly twenty miles.

     Spencer’s airship has a blunt nose and tail, and does not taper to a cigar-like point, like the airships of Santos-Dumont. In general outline it has the appearance of a whale. The bag, which is seventy-five feet long, contains 20,000 cubic feet of hydrogen. The frame is built of bamboo, and the propeller is in front, instead of behind, as is the case with Santos-Dumont’s vessels.

     The motive power of Spencer’s machine is a petroleum motor of about 30 horse power, and the machinery is controlled by electric buttons. The extreme speed of the new airship in calm weather is about fifteen miles an hour.

     The machine accommodates only one person, and its entire weight is about 600 pounds. Special features of the airship are devices to avoid pitching and dipping.

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     Stanley Spencer is the aeronaut who, on Sept. 15, 1898, made an ascension from the Crystal Palace, and afterward claimed that he had reached the highest elevation that had yest been attained.

     Scientists denied his assertion, pointing out that Coxwell and Glaisher, in September, 1862, reached an altitude of 37,000 feet, while Mr. Spencer only claimed that he had reached an altitude of 27,500 feet.

The New York Times, 20 September 1902

Mr. Stanley Spencer, with his family.

Stanley Edward Spencer was born in April 1868 at Islington, Middlesex, England. He was the son of Charles Green Spencer, the owner of the C.G. Spencer & Sons balloon factory (14 Ringcroft Street, Holloway, London), and Louise Emma Woodward Spencer. He was the third of eight children.

Stanley Edward Spencer, “bachelor,” married Miss Rose Isabel Hawkins, a 23 year-old “spinster,” at the parish church in Hornsey, Middlesex, England. The ceremony was officiated by Charles A. Sinclair. They would have four children.

Stanley Spencer died of typhoid fever at Floriana, Malta, 27 January 1906.

© 2024, Bryan R. Swopes