Yearly Archives: 2025

Benjamin Scovill Kelsey (9 March 1906 – 3 March 1981)

March 9, 2025AviationAllison Engineering Co. V-1710, Bell XFM-1 Airacuda, Bell XP-39 Airacobra, Benjamin Scovill Kelsey, Consolidated NY-2, Curtiss JN "Jenny", Curtiss-Wright XP-40, Daniel Guggenheim Fund for the Promotion of Aeronautics, Full Flight Laboratory, Lockheed P-38G Lightning, Lockheed XP-38 Lightning, Martin B-10B, Test Pilot, Wright FieldBryan Swopes

First Lieutenant Benjamin Scovill Kelsey, Air Corps, United States Army, circa 1937. Lieutenant Kelsey is wearing the badge of a Senior Pilot. The ribbon below his “wings” represents the Distinguished Flying Cross. (Kelsey Family Collection)

Benjamin Scovill Kelsey, an aeronautical engineer and test pilot, despite his youth and junior rank, was one of the most influential Air Corps officers in the shaping of United States military air power during the years leading up to World War II.

Ben Kelsey was born in the Kelsey family home at 22 Johnson Street, Waterbury, Connecticut, on 9 March 1906. He was the son of Benjamin Richard Kelsey, an agent for the Waterbury Blank Book Co., and Elizabeth Anna Scovill Kelsey. His mother’s family, the Scovills, were a prominent manufacturing family in Connecticut. Kelsey’s father died 2 Dec 1909.

Kelsey attended Crosby High School in Waterbury. He had an early interest in aviation, and he began flight lessons at the age of 14. He enrolled with the Curtiss Flying School, located at Roosevelt Field, Long Island, New York. The school offered 500 minutes (8 hours, 20 minutes) of flight instruction for $500. Kelsey soloed 13 August 1921.

Ban Keley’s diploma and first solo certificate from the Curtiss School of Aviation. (Kelsey Family Collection)

Kelsey was able to buy a Curtiss “Jenny” airframe from the school, and accumulated parts and an OX-5 engine to put it into flying condition.

Ben Kelsey (center) and his Curtiss Jenny. (Kelsey Family Collection)

Kelsey was granted an aviator’s certificate, No. 6843, by the National Aeronautic Association of U.S.A. (N.A.A.), on behalf of the Fédération Aéronautique Internationale, about 1926. When the United States Department of Commerce began issuing pilot licenses after 1928, Kelsey qualified for Transport License No. 3200. He also held Department of Commerce Mechanic’s License No. 1368. (These, as well as a number of other licenses and identification cards belonging to Kelsey are held in the collection of the Smithsonian Institution National Air and Space Museum.)

Ben Kelsey entered the Massachusetts Institute of Technology (M.I.T.) at Cambridge, Massachusetts, in 1924, with a major in mechanical engineering. He was a member of the Reserve Officers Training Corps (R.O.T.C.), the Tau Beta Pi (ΤΒΠ) fraternity, and The Scabbard and Blade, a national military fraternity. He was president of the Aeronautical Engineering Society, a member of the Mechanical Engineering Society and the Society of Automotive Engineers (S.A.E.). Outside of academics, Kelsey participated in the varsity team sports of swimming and crew, and was a member of the Varsity Club and the Tech Boat Club. He also joined the M.I.T. Flying Club.

Kelsey graduated from M.I.T. in 1928 with a scientiae baccalaureus (S.B.) degree in Mechanical Engineering. He stayed on at the university as a Research Assistant to William G. Brown, Assistant Professor of Aeronautics, in the Department of Aeronautical Engineering.

Benjamin Scovill Kelsey was commissioned as a second lieutenant, Air Corps, United States Army, on 2 May 1929 (accepted 16 June 1929). Because of his experience as a pilot and his training in aeronautical engineering, Lieutenant Kelsey was assigned to work with First Lieutenant James Harold (“Jimmy”) Doolittle at the Guggenheim Full Flight Laboratory at Mitchel Field, Long Island, New York. Financed by the Daniel Guggenheim Fund for the Promotion of Aeronautics, Lieutenants Doolittle and Kelsey worked with Elmer Sperry, Jr., and Paul Kollsman to develop instruments and techniques to take off, fly, and land airplanes in clouds and fog.

On 24 September 1929, Lieutenant Kelsey, in the forward cockpit of a civil-registered, two-place, Consolidated NY-2 Husky biplane, NX7918, acted as a safety pilot while Doolittle flew the airplane from the rear cockpit. Doolittle had his visual reference to earth and sky completely cut off by a hood enclosure over his cockpit. He made the first completely blind airplane takeoff flight and landing, solely by reference to instruments on board his aircraft.

Jimmy Doolittle’s Consolidated NY-2 in flight. A hood covers the rear cockpit, preventing the pilot from seeing outside. Kelsey rode in the forward cockpit as a safety pilot. (San Diego Air and Space Museum)

Lieutenant Kelsey was then assigned to the Air Corps Primary Flying School at Brooks Field, and the Advanced Flying School at Kelly Field, both located in San Antonio, Texas. He completed the Air Corps Pursuit Course in 1930.

On completion of his military flight training, Lieutenant Kelsey was assigned to the 77th Pursuit Squadron, 20th Pursuit Group, based at Mather Field, Sacramento, California, and then Barksdale Field in Louisiana. The squadron flew the Boeing P-12 biplane pursuit.

Kelsey was still a very junior officer in the Air Corps. In July 1931, he was number 231 on the list of second lieutenants.

Second Lieutenant Benjamin Scovill Kelsey, 77th Pursuit Squadron, 20th Pursuit Group, at March Field, Riverside, California, 1931. The airplane is a Boeing P-12E. (Kelsey Family Collection)

Lieutenant Kelsey returned to M.I.T. to complete a master’s degree in aeronautical engineering. He was awarded a scientiae magister (S.M.) degree in Aeronautics in 1932.

The United States government had contracted with commercial aviation businesses to deliver the U.S. Mail by air. A corrupt contracting process was used by the Postal Service, however, and President Franklin D. Roosevelt cancelled those contracts and ordered the Air Corps to start delivering the mail, effective 19 February 1934.

The Air Corps organized the Army Air Corps Mail Operation. The Western Region, based at Salt Lake City, Utah, was under the command of Lieutenant Colonel Henry H. (“Hap”) Arnold (later, General of the Air Force). 2nd Lieutenant Kelsey was transferred from the navigator’s school at Rockwell Field, San Diego, California, to the A.A.C.M.O. Western Region. He and other Air Corps pilots flew at night, in winter weather, on a triangular route from Salt Lake City to Reno and Elko, Nevada. Initially, the airplanes used were the Boeing P-12 pursuits, but they were able to carry only a small amount of mail. The Curtiss A-12 Shrike was then used for the mail delivery.

During this time, Lieutenant Kelsey also worked with Captain Albert F. Hegenberger on an instrument flight research program that allowed Air Corps pilots to conduct a flight from start up to shut down, including takeoffs and landings in “zero-zero” conditions, solely by reference to instruments.

Kelsey was promoted to the rank of first lieutenant, 1 October 1934. He was next assigned as the Pursuit Projects Officer, Material Division, at Wright Field, Dayton, Ohio.

Wright Field, Dayton, Ohio, 17 May 1931. (U.S. Air Force)

Rathje, Caryl, circa 1933. (Kelsey Family Collection) — Caryl Rathje, 1933. (Kelsey Family Collection)

1st Lieutenant Benjamin S. Kelsey married Miss Caryl Rathje, 16 August 1935. Miss Rathje was the fourth of seven children of William John Rathje, president of the Mid-City Trust & Savings Bank in Chicago. Her mother was Mary Eliza Philpot Rathje.

Caryl had graduated from Morgan Park High School in 1929 and then attended Northwestern University at Evanston, Illinois. She was a member of the Beta Chapter Alpha Phi (ΑΦ) sorority. While at Northwestern, Miss Rathje sang 1st soprano in the Glee Club and was secretary of the Daughters of Neptune swimming team.

The wedding, performed by Rev. Clyde Melsee, took place in the bride’s home in Chicago, Illinois.

The Kelseys would have three children, Benjamin Scovill Kelsey, Jr., Peter Rathje Kelsey, and David W. Kelsey.

1st Lieutenant Benjamin Scovill Kelsey, Air Corps, United States Army, with a Curtiss-Wright P-36A Hawk, Air Corps serial number 38-2, at Wright Field, Ohio, circa 1938. (NASM)

Kelsey continued his assignment at Wright Field: “Engineer, Procurement Branch. Project Officer, Pursuit, Engineering Procurement Branch, Material Division.” It was his task to evaluate all pursuit aircraft in current service with the Air Corps, and to assess its future needs. He was in contact aircraft and engine manufacturers, and evaluated similar aircraft types in foreign military service. He performed as an aeronautical engineer, a test pilot and a forecaster of aviation technology.

Martin B-10 over Oahu, Territory of Hawaii, 1941. (Harold Wahlberg/Wikipedia)

On Christmas Eve, 1936, Lieutenant Kelsey was flying a twin-engine Martin B-10 bomber from Mitchel Field, New York, to Wright Field. The flight was not uneventful.

Lieut. Ben Kelsey, returning to Wright Field one night in a Martin B-10B, had reached the vicinity of Columbus, Ohio, when the left engine quit “as though the switches were cut.” After some gas valve and ignition switch manipulating, the engine started up with the gas valve in the “off” position, gasoline flowing freely from the exhaust pipe. On starting, the flames ignited the gasoline on the wing, which also ignited the fabric rear portion of the wing. The engine then began to operate normally and, after deciding against taking a chance on the Columbia Airport fire fighting facilities, Lieut. Kelsey raced the fire to Wright Field. A few inches from the aileron the fire lost, and Lieut. Kelsey, after a few practice cloud landings, shot a “hot” flapless landing successfully at Wright Field with only a little more than half the left wing surface remaining. When asked why he didn’t jump, he answered: “I had an electric train in the back for the boy.”

—Air Corps NEWS LETTER, Vol. XX, No. 3, 1 February 1937, at Page 3, Column 1

For his actions that night, Lieutenant Kelsey was awarded the Distinguished Flying Cross.

The President of the United States of America, authorized by Act of Congress, July 2, 1926, takes pleasure in presenting the Distinguished Flying Cross to First Lieutenant (Air Corps) Benjamin S. Kelsey, U.S. Army Air Corps, for heroism and extraordinary achievement while participating in an aerial flight. On 24 December 1936, at about 7:30 p.m., Lieutenant Kelsey was piloting an airplane from Mitchel Field, Long Island, New York, to Wright Field, Dayton, Ohio, flying at an altitude of approximately 1,800 feet when he left motor instantaneously failed and the left wing burst into flames. By his outstanding courage, sound judgment, and at the risk of his life Lieutenant Kelsey maintained control of the airplane and, with great difficulty due to the darkness of the night and the glare from the burning airplane, effected a safe landing at Wright Field, thereby preventing the destruction to valuable Government property.

General Orders: War Department: American Decorations, 1937 – 1938 (Supplement II-1939)

Action Date: December 24, 1936

Bell XFM-1 36-351, prototype heavy fighter. (Charles Daniels Photo Collection, SDASM, 15_002692)

On 1 September 1937, Lieutenant Kelsey made the first flight of the Bell Aircraft Corporation XFM-1 Airacuda at Buffalo, New York. This was a prototype twin-engine heavy fighter. The Airacuda was Bell’s first military aircraft and was technologically advanced, but also had many flaws. Kelsey found that the airplane would immediately enter a spin when flown with one engine. It was also unstable in pitch, as the “pusher” arrangement would cause pitch angle to climb as engine power was increased. This was the same problem that had caused the Air Service to ground all pusher-type aircraft in February 1914, and to prohibit their future use.

This Allison Engineering Co. V-1710-C4 V-12 engine, s/n 9 (V-1710-7, A.C. No. 43-7) was the first V-1710 to be flown. It had Maximum Continuous power rating of 1,000 h.p. at 2,600 r.p.m., at Sea Level. (NASM)

The XFM-1 was powered by two Harold Caminez-designed, liquid-cooled, supercharged, 1,710.60-cubic-inch-displacement (28.032 liter) Allison Engineering Company V-1710-9 single overhead cam 60° V-12 engines. These were very early models of the type, but the Allison V-12 would be a significant feature in several future aircraft which were proposed by Kelsey.

In February 1937, the Air Corps issued a proposal to aircraft manufacturers, written by Lieutenant Kelsey and Lieutenant Gordon P. Saville, for a twin-engine, high-altitude interceptor. This would be developed into the Lockheed Aircraft Company’s legendary P-38 Lightning. Ben Kelsey made the first flight of the XP-38 at March Field, Riverside, California, 27 January 1939. The Lightning was the first production airplane to use the Allison V-1710 engine.

Lockheed XP-38 Lightning 37-457. (San Diego Air & Space Museum)

Attempting a transcontinental speed record to draw public attention to the Air Corps’ need for technologically advanced aircraft, Kelsey flew the prototype XP-38 from March Field to Mitchel Field. On approach to Mitchel, the XP-38 was behind several slower training planes, so Lieutenant Kelsey throttled back the engines. When he tried to throttle up, the carburetor venturis iced and the engines would not accelerate, remaining at idle. With insufficient power to maintain altitude, the airplane crashed on a golf course short of the airport.

Wreck of the Lockheed XP-38 at Cold Stream, New York. (Associated Press)

The XP-38 was damaged beyond repair, but its performance on the transcontinental flight was so impressive that 13 YP-38A pre-production aircraft were ordered from Lockheed by the Air Corps. Testing continued with the YP-38A and was the new fighter was quickly placed in full production. The P-38 Lightning was one of the most successful combat aircraft of World War II. By the end of the war, Lockheed had built 10,037 Lightnings.

The Bell XP-39 prototype, 38-326, in the original turbosupercharged configuration. The intercooler and waste gates created significant aerodynamic drag. (Bell Aircraft Corporation)

Another Air Corps proposal written by Lieutenants Kelsey and Saville resulted in the Bell XP-39 Airacobra. This aircraft was also powered by an Allison V-1710, placed in a position behind the cockpit. The XP-39 made its first flight 6 April 1938. 9,584 Bell P-39 Airacobras were built during World War II.

The Curtiss-Wright XP-40 prototype at Langley Field in the original configuration. (NASA)

Curtiss-Wright’s Chief Engineer, Donovan Reese Berlin, had taken the tenth production P-36A Hawk, Air Corps serial number 38-10, and had its air-cooled radial engine replaced with a liquid-cooled Allison V-1710-C13 V-12 engine. Although the P-36A’s original Pratt & Whitney R-1830-17 14-cylinder radial engine had greater displacement and produced 80 horsepower more for takeoff than the Allison V-12, the long, narrow V-12 allowed for a much more streamlined engine cowling for higher speed and greater efficiency.

The XP-40 was disappointingly slow when compared to the P-36A, however. Kelsey had the prototype sent to the National Advisory Committee for Aeronautics (NACA) Research Center at Langley Field, Hampton, Virginia, where the full-size airplane was placed inside a wind tunnel.

Curtiss-Wright XP-40 prototype in the NACA wind tunnel at Langley Field, Hampton, Virginia, 24 April 1939. The technician at the lower left of the photograph provides scale. (NASA)

Over a two-month period, NACA engineers made a number of improvements. The radiator was moved forward under the engine and the oil coolers utilized the same air scoop. The exhaust manifolds were improved as were the landing gear doors.

When they had finished, Lieutenant Kelsey flew the modified XP-40 back to Curtiss. Its speed had been increased to 354 miles per hour (570 kilometers per hour), a 12% improvement.

Between 1939 and 1945, Curtiss built 13,738 P-40s in many configurations. They flew in combat in every theater of operations during World War II.

1st Lieutenant Kelsey was promoted to the rank of captain in May 1939. In July 1940, Captain Kelsey was sent to England as a military attaché. He observed combat operations during the Battle of Britain, and was able to fly the Hawker Hurricane and Supermarine Spitfire fighters. Kelsey arranged to have two Spitfire Mk.Va fighters, R7347 and W3119, shipped to the United States for evaluation at Wright Field and NACA Langley.

Supermarine Spitfire Mk.Va, R7347, at NACA Langley, circa 1941. (NASA)

Captain Kelsey returned to the United States, departing Galway, Ireland, 5 July 1940, aboard the United States Lines passenger liner S.S. Washington. The ship was under the command of Captain Harry Manning, who had been one of two navigators intended to fly with Amelia Earhardt around the world in 1937. Kelsey arrived at the Port of New York on 13 July. [Interestingly, on 11 June 1940, S.S. Washington had been stopped off the coast of Portugal by a Kriegsmarine U-boat, U-101, and the passengers and crew were given ten minutes to abandon ship before it was to be sunk. The submarine’s captain, Kapitänleutnant Fritz Frauenheim, realized that he had mistaken the ship for another, and signaled to Captain Manning, “Thought you were another ship. Please go on, go on.”]

United States Lines passenger liner S.S. Washington, San Francisco, California, 10 August 1940. (Cropped image from original photograph. Unattributed, via OpenSFHistory)

With World War II underway, Britain could not produce enough combat aircraft to meet its immediate needs. The British Purchasing Commission had asked North American Aviation to produce Curtiss-Wright Tomahawks (P-40s) under license. N.A.A. responded with a proposal for an all-new fighter, the NA-73X, which would be powered by the Allison V-1710, could be designed and built in the same time it would take to establish a P-40 assembly plant in California. On 10 April 1940, the Commission authorized North American to proceed. The prototype made its first flight on 26 October 1940, and it was placed in production as the Mustang Mk.I.

The fourth and tenth production Mustang Mk.Is, AG348 and AG354, were diverted to the Army Air Corps, designated XP-51 and assigned serial numbers 41-038 and 41-039. Both aircraft were extensively flight tested at Wright Field and by NACA at the Langley Memorial Aeronautical Laboratory. The airplane was ordered into production as the P-51A Mustang.

North American Aviation XP-51 41-039 during flight testing at Wright Field. (U.S. Air Force)

Lee Atwood, North American’s chief engineer and later president, wrote:

Ben Kelsey, in my opinion, was among the most effective Air Corps officers of World War II. His active liaison between combat and aircraft engineering was extremely productive and resulted in aircraft and weapons improvements in a timely manner and when most critically needed. I first met Ben when he was the project officer on the P-38 and he became interested in the P-51 at an early stage. Undoubtedly, he did all he could to bring it along. He had a low key, but very convincing approach.

—Warbird Factory: North American Aviation in World War II, by John Fredrickson, Voyageur Press, 2015, Chapter 8 at Page 147

Captain Kelsey was promoted to the rank of major (temporary) 15 March 1941. On 10 October 1941, he was appointed a major in the wartime Army of the United States (A.U.S.).

As the United States prepared for an unavoidable involvement in World War II, its military forces underwent a massive expansion. Promotions for serving officers came much more rapidly than had been the case during the pre-war years. Normally, they would retain their permanent rank in the United States Army while rising to higher rank and responsibility in the Army of the United States.

Major Kelsey was promoted to lieutenant colonel (temporary) on 5 January 1942, and to lieutenant colonel, A.U.S., on 1 February 1942. Four weeks later, 1 March 1942, he was advanced to colonel, A.U.S.

Lockheed P-38F Lightnings at Iceland during the summer of 1942. (U.S. Air Force)

Colonel Kelsey was involved in the planning and operation of the North Atlantic Ferry Route (Operation Bolero), by which aircraft were moved from the United States to Europe, by way of Newfoundland, Labrador, Greenland, Iceland and Ireland. He flew a Lockheed P-38F Lighting of the 14th Fighter Group on the first crossing by this route in June 1942.

(Left to right) Colonel Benjamin Scovill Kelsey, Colonel John Koehler Gerhart, Major John O. Zahn, Major Cass Sheffield Hough, Colonel John Nicholas Stone, 1st Fighter Group, 30 June 1942 (American Air Museum in Britain FRE 10064)

Colonel Kelsey resumed his assignment as chief of the Pursuit Branch at Wright Field. On 9 April 1943, Kelsey was at Lockheed in southern California, testing a P-38G-10-LO Lightning, 42-12937. He had entered a high-speed dive at 35,000 feet (10,668 meters). When he attempted to engage the new “dive flap,” intended to control some of the compressibility effects that pilots had encountered, the control lever broke away. Kelsey applied full rudder and aileron. The P-38’s left wing and tail broke away, and the remaining part of the airplane entered an inverted spin. Kelsey bailed out, suffering a broken ankle. The airplane crashed near Calabasas, California (13.5 miles, or 21.8 kilometers, from where I am now writing).

Wreckage of Lockheed P-38G-10-LO Lightning 42-12937, after Colonel Kelsey was forced to bail out, 9 April 1943. Los Angeles County sheriff’s deputies guard the scene at the southwest edge of the San Fernando Valley. This is the present location of the Los Angeles Pet Memorial Park, just north of the Ventura Freeway (U.S. 101) and Parkway Calabasas, Calabasas, California. (P-38 National Association and Museum)

Colonel Kelsey was named chief of the Flight Research Branch, Flight Test Division, at Wright Field, in July 1943.

In November 1943, Colonel Kelsey was assigned as deputy chief of staff, Headquarters, IX Fighter Command, based at Army Air Forces Station 449 (RAF Middle Wallop) in Hampshire, England. Shortly after, he was reassigned as chief of operations, Eighth Air Force. While in England, Colonel Kelsey flew 21 combat missions. During 1944, he flew combat missions is the P-51 Mustang with the 363d Fighter Squadron, 364th Fighter Group, which was based at RAF Honington (AAF Station 375) in Suffolk, England. On 30 November, Kelsey flew as Red Leader with the 77th Fighter Squadron on a mission to Leipzig.

This photograph was taken at RAF Kings Cliffe (AAF Station 367) following the Mission of 30 November 1944. Colonel Kelsey had been assigned to the 77th Squadron in 1931. Left to right, Colonel Harold J. Rau, former commanding officer, 20th Fighter Group, with Honey, his adopted yellow Labrador Retriever; Colonel Benjamin S. Kelsey; LCOL Robert Pearson (“Monty”) Montgomery, commanding officer, 20th Fighter Group; Lieutenant Colonel Russell Frederick (“Gus”) Gustke (later, Major General), executive officer, 20th Gighter Group. Rau, Montgomery and Gustke had each previously commanded the 77th Fighter Squadron. (Photograph courtesy of MSgt Arthur Sevigny USAF (Ret.), Historian, 20th Fighter Wing Association.)

Mrs. Kelsey with Colonel Kelsey, circa 1946. The medal below the ribbon bars is the Croix de Guerre avec palme, awarded by the government of France. (Kelsey Family Collection)

Following the end of the war, Colonel Kelsey returned to Wright Field. He reverted to his permanent rank of major, Army Air Forces, 2 May 1946. He then had a series of staff assignments. After the United States Air Force was established as a separate military service on 18 September 1947, Major Kelsey was appointed a major, U.S. Air Force, with a date of rank 2 May 1946. Major Kelsey was promoted to the rank of colonel U.S. Air Force, 2 April 1948.

Colonel Kelsey attended the National War College at Fort Lesley J. McNair, Washington, D.C., from August 1948 to June 1949. He then became an instructor at the College. Kelsey next served as Deputy Director for Research and Development at Air Force headquarters. He was promoted to the rank of brigadier general (temporary) on 5 September 1952.

In 1954, General Kelsey was the Air Force representative to the Research Airplane Committee which proposed the hypersonic X-15 rocketplane, which would be built by North American Aviation.

North American Aviation, Inc., X-15A 56-6670 on Rogers Dry Lake, Edwards Air Force Base, California. (NASA)

On 30 December 1955, Brigadier General Kelsey reverted to his permanent rank of colonel. He retired from the Air Force 31 December 1955, after 26 years, 7 months, 30 days of military service.

During his military career, Colonel Kelsey had been awarded the Distinguished Service Cross, the Legion of Merit, the Distinguished Flying Cross, and the Air Medal with two oak leaf clusters (three awards). France and Belgium each decorated him with their Croix de Guerre.

In 1944, Colonel Kelsey had been honored with the Octave Chanute Award of the Institute of Aeronautical Sciences “for an outstanding contribution made by a pilot or test personnel to the advancement of the art, science, and technology of aeronautics.”

In 1959, the Massachusetts Institute of Technology bestowed on Kelsey its Jerome C. Hunsaker Visiting Professor of Aerospace Systems. Professor Kelsey delivered the annual Minta Martin Lecture, “Size Considerations in Optimum Aircraft.”

The National Air and Space Museum selected Colonel Kelsey as the Charles A. Lindbergh Chair in Aerospace History for 1979. With this fellowship, he wrote The Dragon’s Teeth?: The Creation of United States Air Power in World War II (Smithsonian Institution Press, 1982).

Colonel Benjamin Scovill Kelsey, United States Air Force (Retired), died at Sherwood Farm, Stevensburg, Virginia, 3 March 1981, at the age of 74 years. His remains were cremated.

This Day in Aviation is indebted to Ms. Tiffany Kelsey, Ben Kelsey’s granddaughter, for her invaluable assistance.

8 March 1954

March 8, 2025AviationFédération Aéronautique Internationale, Sikorsky Aircraft Corporation, Sikorsky H-34 Choctaw, Sikorsky HUS-1 Seahorse, Sikorsky S-58, Sikorsky XHSS-1 Seabat, Wright R-1820-84Bryan Swopes

U.S. Navy Sikorsky XHSS-1 Seabat, Bu. No. 134668. (Sikorsky Historical Archives)

8 March 1954: A prototype for a new anti-submarine helicopter for the United States Navy, the Sikorsky XSSH-1, made its first flight at the Sikorsky factory in Bridgeport, Connecticut. The helicopter, the Model S-58, had been developed as an internal project by Sikorsky, using the company’s own money. It was a major improvement of the earlier Model S-55 (H-19 Chickasaw/HO4S).

The S-58 followed the single main rotor/tail (anti-torque) rotor configuration pioneered by Sikorsky with the Vought-Sikorsky VS-300 in 1939. The helicopter was designed to be flown by two pilots in a cockpit above the main cabin. Like the S-55, the engine was placed in the nose, installed at a 35° angle, and driving the transmission located behind the cockpit. For maintenance the engine could be accessed through two large clam shell doors in the nose. The wheeled landing gear was conventional, with two main wheels forward, and a tail wheel.

The S-58 fuselage had been designed using wind tunnel testing. The helicopter was built primarily of aluminum but the fuselage incorporated magnesium skin panels. The helicopter would be equipped with Automatic Stabilization Equipment (ASE), an autopilot system specifically for helicopters.

The S-58 has and overall length of 65.7 feet (20.03 meters) with rotors turning. The fully articulated four-blade main rotor diameter is 56.0 feet (17.07 meters), and the tail rotor, also with four blades, is 9.5 feet (2.90 meters) in diameter. The fuselage is 46.6 feet (14.20 meters) long. The helicopter has an overall height of 15.9 feet (4.85 meters). To minimize storage space on ships, the main rotor blades and the tail rotor pylon can be folded.

The four-blade main rotor allows the helicopter to reach higher speeds before encountering retreating-blade stall than the three-blade system used on previous Sikorsky models.

Sikorsky S-58 three-view illustration with dimensions. (Sikorsky)

The production HSS-1 was powered by an air-cooled, supercharged, Wright R-1820-84 nine-cylinder radial engine with a compression ratio of 6.80:1. It was rated at 1,525 horsepower at 2,800 r.p.m. for takeoff; 1,425 horsepower at 2,700 r.p.m., 30-minute limit; and 1,275 horsepower at 2,500 r.p.m., continuous. The R-1820-84 was 4 feet, 4.00 inches (1.321 meters) long, 4 feet, 7.74 inches (1.416 meters) in diameter and weighed 1,405 pounds (627 kilograms). The engine required 115/145 octane aviation gasoline.

The R-1820-84 drove the transmission through a 0.5625:1 gear reduction. The transmission had a gear reduction ratio of 11.293:1. Maximum main rotor speed was 258 r.p.m. (2,914 engine r.p.m.)

Engine bay of the XHSS-1. (Sikorsky Archives)

The HSS-1 had an empty weight of 8,400 pounds (3,810 kilograms), and maximum takeoff weight of 13,300 pounds (6,032 kilograms). Its fuel capacity was 307 U.S. gallons (1,162 liters).

The helicopter had a cruise speed of 84 knots (97 miles per hour/156 kilometers per hour), and a maximum speed of 126 knots (145 miles per hour/233 kilometers per hour) at Sea Level. Its service ceiling was 17,600 feet (5,364 meters), and the hovering ceiling, out of ground effect, was 9,900 feet (3,018 meters) at takeoff power. The range was 227 nautical miles (261 statute miles/420 kilometers).

In an anti-submarine warfare configuration, the helicopter was equipped with a dipping sonar system and armed with two Mark 43 torpedoes. The Mark 43 was an electrically driven homing torpedo, 91.5 inches (2.324 meters) long, 10 inches in diameter (0.254 meters), weighing 265 pounds (120 kilograms). It had a 54 pound (25 kilogram) explosive warhead. In transport configuration (HUS-1 Seahorse and UH-34 Choctaw) the S-58 could carry 16 troops or 6 litters and medical attendant.

U.S. Army Sikorsky H-34A Chocktaw, 56-4303. (Sikorsky Historical Archives)

Starting at 5:29 a.m., 12 July 1956, a Sikorsky H-34 Chocktaw, the U.S. Army variant of the S-58, flown by Captains Claude E. Hargett and Ellis D. Hill, near Milford, Connecticut, set three Fédération Aéronautique Internationale (FAI) world records for speed: over a 1,000 kilometer (621.4 statute miles) circuit without payload, 213,45 kilometers per hour (132.63 miles per hour/115.3 knots);¹ 500 kilometers (310.7 statute miles) without payload, 218,89 kilometers per hour (136.01 miles per hour/118.19 knots);² and 100 kilometers (62.1 statute miles) without payload, 228,39 kilometers per hour (141.92 miles per hour/123.32 knots).³ Captain Hargett was awarded a bronze oak leak cluster in lieu of a second award of the Distinguished Flying Cross. Captain Hill was awarded the Legion of Merit.

Captains Claude E. Hargett and Ellis D. Hill, U.S. Army. (FAI)

The S-58 was built in a number of military and civil variants. Sikorsky built more than 1,800 S-58 series helicopters. Another 600 were produced by licensed manufacturers.

¹ FAI Record File Number 2154

² FAI Record File Number 2155

³ FAI Record File Number 13068

6–8 March 1949

March 8, 2025AviationBeech Aircraft Corporation, Beechcraft Model 35 Bonanza, Bill Odom, Continental E185-1, Fédération Aéronautique Internationale, N80040, s/n 4, Waikiki Beech, William Paul Odom, World Record for Distance in a Straight LineBryan Swopes

Beechcraft 35 Bonanza N80040, Waikiki Beech, at NASM.

6–8 March 1949: William Paul Odom, a former captain in the U.S. Army Air Corps who had flown “The Hump” during World War II, departed Honolulu Airport on the island of Oahu, Territory of Hawaii, flying the fourth prototype Beechcraft Model 35 Bonanza, N80040, which he had named Waikiki Beech, enroute to Teterboro, New Jersey, non-stop. He arrived there after 36 hours, 1 minute, setting a Fédération Aéronautique Internationale (FAI) World Record for Distance in a Straight Line of 7,977.92 kilometers (4,957.24 miles),¹ averaging 137.64 miles per hour (221.5 kilometers per hour). The Bonanza had 12 gallons (45.4 liters) of gasoline remaining, having consumed 272.25 gallons (1,030.6 liters).

The Hawaii Aeronautics Commission Annual Report mentioned the flight:

March 1949

4—Bill Odom returns for second attempt of Honolulu-New York non-stop flight.

6—Bill Odom leaves on second Honolulu-New Jersey non-stop flight and lands at Teterboro, New Jersey on March 8, exactly 36 hours and 1 minute after leaving Honolulu Airport, setting a new distance record of 4,957.24 miles for light airplane and longest non-stop solo flight in his converted Beech Bonanza plane which was appropriately christened “Waikiki Beech.” Flight was made with only $75 worth of gasoline.

Bill Odom flew Waikiki Beech on a national publicity tour for the Beech Aircraft Corporation. — Bill Odom flew “Waikiki Beech” on a national publicity tour for the Beech Aircraft Corporation.

N80040 was the fourth prototype Beechcraft Model 35 Bonanza. (The first two were static test articles.)

The Beechcraft Model 35 Bonanza is an all-metal, single-engine, four-place light civil airplane with retractable landing gear. The Bonanza has the distinctive V-tail with a 30° dihedral which combined the functions of a conventional vertical fin and rudder, and horizontal tail plane and elevators.

The Model 35 was 25 feet, 2 inches (7.671 meters) long with a wingspan of 32 feet, 10 inches (10.008 meters) and height of 6 feet, 6½ inches (1.994 meters). It had an empty weight of 1,458 pounds (661 kilograms) and gross weight of 2,550 pounds (1,157 kilograms.)

Beechcraft Model 35 Bonanza NX80040. This is the fourth prototype. It is in the collection of the Smithsonian Institution National Air and Space Museum. (Beech Aircraft Corporation)

NX80040, s/n 4, and the following production models were powered by an air-cooled, 471.24-cubic-inch-displacement (7.72 liter) Continental Motors, Inc., E185 horizontally-opposed 6-cylinder engine. This engine was rated at 165 horsepower at 2,050 r.p.m. (NX80150, s/n 3, had been equipped with a 125-horsepower Lycoming O-290-A.) The Bonanza had a two-bladed electrically-controlled variable pitch Beechcraft R-100 propeller with a diameter of 7 feet, 4 inches (2.235 meters) made of laminated wood.

The “V-tail Bonanza” had a maximum speed of 184 miles per hour (296 kilometers per hour) at Sea Level, and a cruise speed of 175 miles per hour (282 kilometers per hour) at 10,000 feet (3,048 meters). Its service ceiling was 18,000 feet (5,486 meters). With full fuel, 40 gallons (151.4 liters), the airplane had a range of 750 miles (1,207 kilometers).

The Beechcraft 35 was in production from 1947 to 1982. More than 17,000 Model 35s and the similar Model 36 were built.

Beechcraft Model 35 Bonanza NX80040. (Hans Groenhoff Photographic Collection, Smithsonian Institution National Air and Space Museum NASM-HGC-201)

William Paul Odom was born at Raymore, Missouri, 21 October 1919, He was the first of three children of Dennis Paul Odom, a farmer, and Ethel E. Powers Odom.

Odom, then an airport radio operator, married Miss Dorothy Mae Wroe at Brentwood, Pennsylvania, 3 December 1939.

Odom flew for the Chinese National Aviation Corporation (CNAC) from 1944 to 1945, flying “The Hump,” the air route over the Himalayas from India to China.

William P. Odom had flown a Douglas A-26B Invader, NX67834, named Reynolds Bombshell, around the world in 3 days, 6 hours 55 minutes, 56 seconds, 12–16 April 1947. He made a second around the world flight, 7–11 August 1947, again flying the A-26. The duration of this second trip was 3 days, 1 hour, 5 minutes, 11 seconds. (Neither flight was recognized as a record by the FAI.)

In April 1948, Odom flew a Consolidated C-87A-CF Liberator Express transport, NL5151N, for the Reynolds Boston Museum China Expedition.

The communist Chinese government suspected that the expedition was actually a U.S. government espionage mission. The Liberator Express was impounded and the crew held for interrogation. Slipping away from their captors, they escaped and flew the transport to Japan. An “international incident” was the result.

Consolidated-Vultee Model 32 Liberator Express NL5151N. This airplane, serial number 50, was built as a C-87A-CF Liberator Express transport, 43-30570, for the U.S. Army Air Forces. It was transferred to the U.S. Navy, designated RY-1 Liberator, Bu. No. 67798. In 1948 it was sold and assigned CAA registration NL5151N. (Bill Larkins Collection)

Odom had made another FAI World Record flight with Waikiki Beech, from from Honolulu, to Oakland, California, an official distance of 3,873.48 kilometers (2,406.87 miles).²

With these records and record attempts, Bill Odom persuaded Jackie Cochran to buy a radically-modified P-51C Mustang named Beguine (NX4845N) for him to fly at the 1949 National Air Races at Cleveland Municipal Airport, Ohio.

Beguine, a radically-modified North American Aviation P-51C Mustang, NX4845N. (Torino Dave)

Though he had never flown in a pylon race, Odom had qualified the P-51 Beguine for the 105 mile Sohio Trophy Race, held 3 September 1949. He won the race, averaging 388.393 miles per hour (625.058 kilometers per hour. He had also entered the Thompson Trophy Race, qualifying with a speed of 405.565 miles per hour (652.694 kilometers per hour.)

The Thompson Trophy Race was held on 5 September. On the second lap, Odom’s P-51 went out of control and crashed into a house near the airport. Bill Odom, along with a woman and child on the ground, were killed.

William Paul Odom’s remains were buried at the Friendship Cemetery, Columbus, Mississippi.

William Paul Odom in the cockpit of the radically-modified P-51C air racer Beguine at the Cleveland National Air Races, 3 September 1949. (NASM)

¹ FAI Record File Number 9112

² FAI Record File Number 14512

8 March 1936

March 8, 2025Aviation[152 meters], 32-414, Aircraft Accident, Boeing Airplane Company, Boeing Model 248, Boeing P-26, Boeing XP-936, c/n 1680, Cheney Award, Leslie R. Tower, Logan Field, National Advisory Committee for Aeronautics, Pratt & Whitney R-1340-21, Pratt & Whitney Wasp SE, Robert Kinnaird Giovannoli, Soldier's MedalBryan Swopes

Boeing P-26 32-414 at Barksdale Field, 23 January 1934. (U.S. Air Force)

8 March 1936: First Lieutenant Robert Kinnaird Giovannoli, United States Army Air Corps, a test pilot assigned to the Material Division at Wright Field, Ohio, was killed when the right wing of his Boeing P-26 pursuit, serial number 32-414, came off in flight over Logan Field, near Baltimore, Maryland.

The Cincinnati Enquirer reported:

DAYTON HERO

Air Crash Victim.

Robert Giovannoli Dies At Baltimore Field

When Wing Of Plane Falls Off—Lexington, Ky., Man An Army Lieutenant.

Baltimore, March 8—(AP)—Lieutenant Robert K. Giovannoli, 31 years old of Lexington, Ky., hero of the spectacular bombing plane crash during army tests at Dayton, Ohio, last October, was killed today in the crack-up of his army plane at Logan Field, here.

Giovannoli’s single-seated pursuit plane lost its right wing coming out of a glide and hurtled down in a crazy spin from an altitude of less than 500 feet [152 meters]. It rolled over after hitting the landing field and was demolished.

Lieutenant Giovannoli received a medal for his heroism in rescuing two men from the flaming wreckage of the Boeing “flying fortress” after it crashed in the army bomber tests at Wright Field, Dayton.

The Wright Field hero was taking off for the Middletown, Penn., air station when his plane plunged him to death at Logan Field.

QUIZ TO BE BEGUN.

The flier had arrived here yesterday.

Lieutenant Colonel H.C.K. Nuhlenberg, air officer of the Third Corps Area and in command of Logan Field, said an Army Board of Inquiry would be summoned promptly to investigate the fatal crash.

Nuhlenberg, who had just landed at the field himself, said Giovannoli had gotten his craft under way and turned back to fly over the field at a low altitude.

The wing of Giovannoli’s plane wrenched off, Nuhlenberg said, just as the craft was coming out of the glide and starting a zoom to regain altitude.

—The Cincinnati Enquirer, Vol. XCV, No. 334, Monday, 9 March 1936, at Page 7, Column 1

Lieutenant Giovannoli had been awarded the Soldier’s Medal and the Cheney Award for his heroic rescue of two men from the burning wreck of the Boeing Model 299, which had crashed on takeoff at Wright Field, 30 October 1935. His citation reads:

The President of the United States of America, authorized by Act of Congress, July 2, 1926, takes pleasure in presenting the Soldier’s Medal to First Lieutenant Robert K. Giovannoli, United States Army Air Corps, for heroism, not involving actual conflict with an enemy, displayed at Wright Field, Dayton, Ohio, 30 October 1935. When a Boeing experimental bomber crashed and burst into flames, Lieutenant Giovannoli, who was an onlooker, forced his way upon the fuselage and into the front cockpit of the burning plane and extricated one of the passengers. Then upon learning that the pilot was still in the cockpit, Lieutenant Giovannoli, realizing that his own life was in constant peril from fire, smoke, and fuel explosions, rushed back into the flames and after repeated and determined efforts, being badly burned in the attempt, succeeded in extricating the pilot from an entrapped position and assisted him to a place of safety.

General Orders: War Department, General Orders No. 4 (1936)

The wreck of the Boeing Model 299, X13372, burns after the fatal crash at Wright Field, 30 October 1935. (U.S. Air Force)

Robert Kinnaird Giovannoli was born at Washington, D.C., 13 March 1904, the second of two sons of Harry Giovannoli, a newspaper editor, and Carrie Kinnaird Giovanolli. His mother died when he was six years old.

Robert Giovannoli, 1925. (The Kentuckian)

Giovannoli graduated from Lexington High School at Lexington, Kentucky, in 1920 and then attended the University of Kentucky, where, in 1925, he earned a Bachelor of Science degree in Mechanical Engineering (B.S.M.E.). He was a member of the Phi Delta Theta (ΦΔΘ) and Tau Beta Phi (ΤΒΦ) fraternities, treasurer of the sophomore class, and president of the American Institute of Electrical Engineers. He was employed by the General Electric Company at Schenectady, New York.

Giovannoli enlisted in the United States Army in 1927. After completing the Air Corps Primary Flying School at Brooks Field, and the Advanced Flying School at Kelly Field, both in San Antonio, Texas, he was commissioned as a second lieutenant in the Air Corps Reserve, 20 October 1928. Lieutenant Giovannoli was called to active duty 8 May 1930. In 1933, he was assigned to a one year Engineering School at Wright Field. He then was sent to observe naval aircraft operations aboard USS Ranger (CV-4) in the Pacific Ocean. He had returned just a few days prior to the accident.

At the time of his death, Lieutenant Giovannoli had not yet been presented his medals.

First Lieutenant Robert Kinnaird Giovannoli was buried at the Bellevue Cemetery, Danville, Kentucky. In 1985, the Robert Kinnaird Giovannoli Scholarship was established to provide scholarships for students in mechanical engineering at the University of Kentucky College of Engineering.

Boeing XP-936 No. 3 in flight. This airplane would be designated P-26, serial number 32-414. It is the airplane flown by Lieutenant Robert Kinnaird Giovannoli, 8 March 1936. (Boeing)

The P-26, Air Corps serial number 32-414, was the last of three prototype XP-936 pursuits built by Boeing in 1932. Boeing’s chief test pilot, Leslie R. Tower, conducted the first flight of the type on 20 March 1932. Leslie Tower was one of the two men that Lieutenant Giovannoli had pulled from the burning Boeing 299.

The Boeing P-26 was a single-seat, single-engine monoplane. It was the first all-metal U.S. Army pursuit, but retained an open cockpit, fixed landing gear and its wings were braced with wire. The airplane was 23 feet, 7 inches (7.188 meters) long with a wingspan of 28 feet (8.534 meters). The empty weight of the prototype was 2,119 pounds (961.2 kilograms) and gross weight was 2,789 pounds (1,265.1 kilograms).

The first of three Boeing Model 248 prototypes, XP-26 32-412. (Boeing)

The Y1P-26 was powered by an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney R-1340-21 (Wasp S2E), a single-row, nine-cylinder radial engine. The P-26A and P-26C were powered the Pratt & Whitney R-1340-27 (Wasp SE), while the P-26B used a more powerful, fuel-injected R-1340-33 (Wasp D2). Each of these engines were direct drive and had a compression ratio of 6:1. The engine was surrounded by a Townend Ring which reduced aerodynamic drag and improved engine cooling.

The R-1340-21 had a Normal Power rating of 600 horsepower at 2,200 r.p.m. at 6,000 feet (1,829 meters); 500 horsepower at 2,200 r.p.m. at 11,000 feet (3,353 meters); and 500 horsepower at 2,000 r.p.m. for takeoff. It required 87-octane gasoline. The –21 had a diameter of 3 feet, 3.44 inches (1.307 meters) and weighed 715 pounds (324 kilograms).

The R-1340-27 had a Normal Power and Takeoff power rating of 570 horsepower at 2,200 r.p.m., to 7,500 feet (1,524 meters), using 92-octane gasoline. The –27 was 3 feet, 7.25 inches (1.099 meters) long, 4 feet, 3.50 inches (1.308 meters) in diameter and also weighed 715 pounds (324 kilograms).

The R-1340-33 was rated at 575 horsepower at 2,200 r.p.m. to 10,000 feet (3,048 meters), and 600 horsepower at 2,120 r.p.m. for Takeoff, with 87-octane gasoline. It was 3 feet, 10.75 inches (1.187 meters) long, with the same diameter as the –27. It weighed 792 pounds (359 kilograms).

The engines drove a two-bladed, Hamilton Standard adjustable-pitch propeller.

19th Pursuit Squadron commanding officer’s Boeing P-26 in flight over Oahu, Territory of Hawaii, 6 March 1939. (NASM)

The pursuit had a maximum speed of 227 miles per hour (365 kilometers per hour) at 10,000 feet (3,048 meters), and a service ceiling of 28,900 feet (8,809 meters).

As a pursuit, the P-26 was armed with two air-cooled Browning M1919 .30-caliber machine guns, synchronized to fire forward through the propeller arc.

Boeing built 136 production P-26s for the Air Corp and another 12 for export. Nine P-26s remained in service with the Air Corps at the beginning of World War II.

A Boeing P-26, A.C. 33-56, in the Full-Scale Wind Tunnel at the National Advisory Committee for Aeronautics Langley Memorial Aeronautical Laboratory, 1934. This “Peashooter,” while assigned to the 6th pursuit Squadron, ditched north of Kaluku, Oahu, Hawaii, 14 December 1938. (NASA)

8 March 1910

March 8, 2025AviationFédération Aéronautique Internationale, J.T.C. Moore-Brabazon, John Theodore Cuthbert Moore-Brabazon 1st Baron Brabazon of Tara GBE MC PC, Pilot, Pilot Certificate, Pilot License, Royal Aero ClubBryan Swopes

8 March 1910: John Theodore Cuthbert Moore-Brabazon (later, the 1st Baron Brabazon of Tara, G.B.E., M.C., P.C.) was the first airplane pilot to be issued an aviator’s certificate by the Royal Aero Club of the United Kingdom. He had previously been assigned certificate number 40 of the Fédération Aéronautique Internationale. He was issued Certificate Number 1 in England.