Tag Archives: World Record for Speed Over a 3km Straight Course

13 September 1935

Howard Hughes in the cockpit of the H-1 Special, NR258Y, 1935. (FAI)
Howard Hughes in the cockpit of the Hughes H-1 Special, NR258Y, 1935. (FAI)

13 September 1935: Flying his Hughes H-1 Special, NR258Y,  Howard Robard Hughes, Jr. set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course near Santa Ana, California. Making four passes over the measured course, two in each direction, his average speed was 567.12 kilometers per hour (352.39 miles per hour).¹ This was 61.27 kilometers per hour (38.07 miles per hour) faster than the previous record which had been set by Raymond Delmotte, 24 December 1934.

Hughes H-1 Special NR258Y. (FAI)
Hughes H-1 Special NR258Y. (FAI)

Just after completing the final pass over the course, the airplane’s engine stopped due to fuel starvation. Hughes made a belly landing in a farm field. He was uninjured and the airplane received only minor damage.

Howard Hughes with his H-1, NR258Y, in a been field near Santa Ana, California, 13 September 1935.
Howard Hughes with his H-1, NR258Y, in a farmer’s field near Santa Ana, California, 13 September 1935. (Unattributed)

The Hughes H-1 (Fedral Aviation Administration records identify the airplane as the Hughes Model 1B, serial number 1) was a single-seat, single-engine low-wing monoplane with retractable landing gear. Emphasis had been placed on an aerodynamically clean design and featured flush riveting on the aluminum skin of the fuselage. The airplane was 27 feet, 0 inches long (8.230 meters) with a wingspan of 25 feet (7.6 meters) and height of 8 feet (2.438 meters). (A second set of wings with a span of 31 feet, 9 inches (9.677 meters) was used on Hughes’ transcontinental flight, 19 January 1937). The H-1 has an empty weight of 3,565 pounds (1,617 kilograms) and gross weight of 5,492 pounds (2,491 kilograms).

The H-1 was powered by a air-cooled, supercharged 1,534.943-cubic-inch-displacement (25.153 liter) Pratt & Whitney Twin Wasp Jr. two-row, fourteen-cylinder radial engine. Pratt & Whitney produced 18 civil and 22 military (R-1535) versions of the Twin Wasp Jr., in both direct-drive and geared configurations, rated from 650 to 950 horsepower. It is not known which version powered the H-1, but various sources report that it was rated from 700 to 1,000 horsepower. The engine drove a two-bladed Hamilton Standard controllable pitch propeller.

The Hughes H-1 Racer, NR258Y, at the National Air and Space Museum. (NASM)
The Hughes H-1 Racer, NR258Y, at the National Air and Space Museum. (Eric Long/NASM)

¹ FAI Record File Number 8748

© 2017, Bryan R. Swopes

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1 September 1953

Captain Harold E. "Tom" Collins, U.S. Air Force, in the cockpit of the FAI World Speed Record setting North American Aviation F-86D-35-NA Sabre 51-6145. (Photograph courtesy of Neil Corbett, Test and Research Pilots and Flight Test Engineers)
Captain Harold E. “Tom” Collins, U.S. Air Force, in the cockpit of the FAI World Speed Record setting North American Aviation F-86D-35-NA Sabre 51-6145. (Photograph courtesy of Neil Corbett, Test and Research Pilots and Flight Test Engineers)

1 September 1953: Captain Harold Edward Collins, United States Air Force, flying North American Aviation F-86D-35-NA Sabre, 51-6145, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course of 1,139.219 kilometers per hour (707.878 miles per hour) at Vandalia, Ohio.¹

North American Aviation F-86D-35-NA Sabre 51-6145, FAI World Speed Record holder.
North American Aviation F-86D-35-NA Sabre 51-6145, FAI World Speed Record holder.

This same F-86D (North American Aviation serial number 173-289) flown by Lieutenant Colonel William F. Barnes, set an FAI World Record for Speed Over a 3 Kilometer Straight Course of 715.697 miles per hour (1,151.803 kilometers per hour), 16 July 1953 at the Salton Sea, California. (FAI Record File Number 9868)

The F-86D was an all-weather interceptor developed from North American Aviation F-86 Sabre day fighter. It was the first single-seat interceptor, and it used a very sophisticated—for its time—electronic fire control system. It was equipped with search radar and armed with twenty-four unguided 2.75-inch (70 millimeter) Mk 4 Folding-Fin Aerial Rockets (FFAR) rockets carried in a retractable tray in its belly. The rockets could be fired in salvos of 6, 12 or 24. They had a 6 pound (2.7 kilogram) high explosive warhead and used a proximity fuse.

North American Aviation F-86D-1-NA Sabre
North American Aviation F-86D-1-NA Sabre 50-463, the eighth production aircraft. (North American Aviation, Inc.)

The F-86D was larger than the F-86A, E and F fighters, with a longer and  wider fuselage. It was also considerably heavier. The day fighter’s sliding canopy was replaced with a hinged “clamshell” canopy. A large, streamlined radome was above the reshaped engine intake.

The F-86D Sabre was 40 feet, 3¼ inches (12.275 meters) long with a wingspan of 37 feet, 1½ inches (11.316 meters), and overal height of 15 feet, 0 inches (4.572 meters). The first production variant, F-86D-1-NA, had an empty weight of 13,677 pounds (6,204 kilograms) and gross weight of 16,292 pounds (7,390 kilograms).

The F-86D was equipped with a General Electric J47-GE-17 turbojet engine, rated at 5,425 pounds of thrust, or 7,500 pounds with afterburner. (Aircraft completed after 1954 were equipped with a J47-GE-33.) It had a top speed of 692 miles per hour (1,114 kilometers per hour) at Sea Level (0.909 Mach).

The F-86D had a range of 330 miles (531 kilometers) and a service ceiling of 49,750 feet (15,164 meters). Its rate of climb was 12,150 feet per minute (61.7 meters per second).

A production North American Aviation F-86D-15-NA Sabre, 50-574, launches 2.75-inch rockets. (U.S. Air Force)
A production North American Aviation F-86D-15-NA Sabre, 50-574, launches 2.75-inch rockets. (U.S. Air Force)

Between December 1949 and September 1954, 2,505 F-86D Sabres (sometimes called the “Sabre Dog”) were built by North American Aviation. There were many variants (“block numbers”) and by 1955, almost all the D-models had been returned to maintenance depots or the manufacturer for standardization. 981 of these aircraft were modified to a new F-86L standard. The last F-86D was removed from U.S. Air Force service in 1961.

After its service with the United States Air Force, the record-setting Sabre 51-6145 was transferred to a NATO ally, the Ellinikí Vasilikí Aeroporía (Royal Hellenic Air Force).

North American Aviation F-86D-20-NA Sabre (U.S. Air Force)
North American Aviation F-86D-20-NA Sabre 51-3045. (U.S. Air Force)

¹ FAI Record File Number 8869

© 2017, Bryan R. Swopes

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25 August 1947

Major Marion E. Carl, USN, with a Douglas D-558-I Skystreak at Muroc Dry Lake, 1947. (U.S. Navy)
Major Marion E. Carl, USMC, with a Douglas D-558-I Skystreak at Muroc Dry Lake, 1947. (U.S. Navy)

25 August 1947: Major Marion Eugene Carl, United States Marine Corps, flying the Douglas D-558-I Skystreak, Bu. No. 37970, set a new Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Straight Course, averaging 1,047.356 kilometers per hour (650.797 miles per hour).¹ The Skystreak was flown over a course laid out on Muroc Dry Lake, site of Muroc Army Air Field (now Edwards Air Force Base) in the high desert of Southern California.

Douglas D-558-I Skystreak Bu. No. 37970 makes a pass over the 3 kilometer course on Muroc Dry Lake. (U.S. Navy)
Douglas D-558-I Skystreak Bu. No. 37970 makes a pass over the 3 kilometer course on Muroc Dry Lake. (U.S. Navy)

Four passes were made over the course at an altitude of 200 feet (61 meters) or lower. Two runs were made in each direction to compensate for any head or tail winds. The official speed for a record attempt was the average of the two best consecutive passes out of the four.

Major Carl’s record exceeded one set by Commander Turner F. Caldwell, Jr., U.S. Navy, just five days earlier by 10.053 miles per hour (16.178 kilometers per hour).

Major Marion E. Carl, USMC, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy)
Major Marion E. Carl, USMC, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy) 

The D-558 Program was intended as a three phase test program for the U.S. Navy and the National Advisory Committee on Aeronautics (NACA) to investigate transonic and supersonic flight using straight and swept wing aircraft powered by turbojet and/or rocket engines. The Douglas Aircraft Company designed and built three D-558-I Skystreaks and three D-558-II Skyrockets. The Phase I aircraft were flown by Douglas test pilot Eugene Francis (“Gene”) May, Navy Project Officer Commander Turner F. Caldwell, Jr., and Major Marion Carl.

Major Marion E. Carl, USMC; Gene May, Douglas Aircraft Company; Commander Turner F. Caldwell, USN.
Major Marion E. Carl, USMC; Gene May, Douglas Aircraft Company; Commander Turner F. Caldwell, USN.

The D-558-I Skystreak (also referred to as the D-558-1) was a single-engine, straight winged, turbojet-powered airplane. It was built of magnesium and aluminum for light weight, but was designed to withstand very high acceleration loads. It was 35 feet, 8 inches (10.871 meters) long with a wingspan of 25 feet, 0 inches (7.62 meters) and overall height of 12 feet, 1¾ inches (3.702 meters). The airplane had retractable tricycle landing gear. Its empty weight was approximately 7,500 pounds (3,400 kilograms), landing weight at the conclusion of a flight test was 7,711 pounds (3,498 kilograms). The maximum takeoff weight was 10,105 pounds (4,583.6 kilograms). The aircraft fuel load was 230 gallons (870.7 liters) of kerosene.

The D-558-I was powered by a single Allison J35-A-11 turbojet engine. The J35 was a single-spool, axial-flow turbojet with an 11-stage compressor section, 8 combustion chambers and single-stage turbine. The J35-A-11 was rated at 5,000 pounds of thrust (22.24 kilonewtons). The engine was 12 feet, 1.0 inches (3.683 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,455 pounds (1,114 kilograms). The J35-A-11 was a production version of the General Electric TG-180, initially produced by Chevrolet as the J35-C-3. It was the first widely-used American jet engine.

The D-558-I had a designed service ceiling of 45,700 feet (13,930 meters). Intended for experimental flights of short duration, it had a very short range and took off and landed from the dry lake at Muroc. (After 1949, this would be known as Edwards Air Force Base.) The experimental airplane was not as fast as the more widely known Bell X-1 rocketplane, but rendered valuable research time in the high transonic range.

Gene May did reach Mach 1.0 in 37970, 29 September 1948, though he was in a 35° dive. This was the highest speed that had been reached up to that time by an airplane capable of taking off and landing under its own power.

The three D-558-I Skystreaks made a total of 229 flights and Bu. No. 37970 made 101 of them. After the Douglas test program was completed, -970 was turned over to NACA as NACA 140, but it was quickly grounded after the crash of the number two aircraft, and was used for spare parts for number three.

Today, 37970 is in the collection of the National Naval Aviation Museum at Naval Air Station Pensacola, Florida. The other surviving Skystreak, Bu. No. 37972, is at the Carolinas Aviation Museum, Charlotte-Douglas International Airport, Charlotte, North Carolina.

This painting depicts Major Marion E. Carl's speed record attempt over the 3 kilometer course at Muroc Dry Lake. (Steve Cox, 24" x 30", acrylic on board)
This painting depicts Major Marion E. Carl’s speed record attempt over the 3 kilometer course at Muroc Dry Lake. (Steve Cox, 24″ × 30″, acrylic on board)

¹ FAI Record File Number 9865

© 2017, Bryan R. Swopes

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21 August 1989

Lyle Shelton in the cockpit of Rare Bear. (Lubbock Avalanche-Journal)

21 August 1989: Twenty-five years to the day after the first flight of the prototype Grumman XF8F-1 Bearcat, Lyle Shelton flew his highly-modified Unlimited Class racing plane, the F8F-2 Rare Bear, N777L, over a 3 kilometer course at Las Vegas, New Mexico, setting a Fédération Aéronautique Internationale (FAI) World Speed Record of  850.24 kilometers per hour (528.315 miles per hour),¹ and becoming the world’s fastest piston engine airplane.

Rare Bear had been built for the U.S. Navy at Grumman’s Bethpage, New York plant, and assigned Bureau of Aeronautics serial number (Bu. No.) 122629. It was a light-weight, high performance interceptor designed to operate from the Navy’s smaller aircraft carriers.

Among other things, the original 2,250 horsepower Pratt & Whitney Double Wasp E12 (R-2800-30W) engine was replaced with a 3,347.66-cubic-inch-displacement (54.858 liter) hybridized Wright R-3350 Duplex-Cyclone 18-cylinder radial engine and a 13 foot, 6 inch (4.115 meters) diameter Aeroproducts four-bladed propeller from a Douglas AD-Skyraider, with the cowling from a Douglas DC-7. This customized engine reportedly produced 4,500 horsepower at 3,200 r.p.m, with 80 inches of manifold pressure.

Rare Bear won the National Air Races six times and set several speed and time to altitude records.

Grumman F8F-2 Bearcat, Bu. No. 122629, Unlimited Class racer Rare Bear, N777L. (Kogo via Wikipedia)
Grumman F8F-2 Bearcat, Bu. No. 122629, Unlimited Class racer Rare Bear, N777L. (Kogo via Wikipedia)

The production F8F-2 Bearcat was 27 feet, 8 inches (8.432 meters) long with a wingspan of 35 feet, 6 inches (10.820 meters) and overall height of 13 feet, 5 inches (4.089 meters). Its empty weight was 7,070 pounds (3,206.9 kilograms) and maximum takeoff weight was 12,947 pounds (5,872.7 kilograms).

The production F8F-2 used an air-cooled, supercharged, 2,804.4-cubic-inch-displacement (45.956 liter) Pratt & Whitney Double Wasp VSE11-G (R-2800-30W) 18-cylinder, twin-row, radial engine. It was rated at 1,720 horsepower at 2,600 r.p.m. at Sea Level, and 2,250 horsepower at 2,800 r.p.m., takeoff and military power, with water/alcohol injection and 115/145 aviation gasoline. The engine drove an Aeroproducts Inc. four-bladed propeller with a diameter of 12 feet, 7 inches (3.835 meters) through a 0.450:1 gear reduction. The R-2800-30W was 7 feet, 10.75 inches (2.356 meters) long, 4 feet, 5.00 inches (1.346 meters) in diameter and weighed 2,560 pounds (1,161 kilograms).

The Bearcat had a top speed of 421 miles per hour (677.5 kilometers per hour). It could climb at 4,570 feet per minute (23.2 meters per second) and had a service ceiling of 38,700 feet (11,796 meters). Its range was 1,105 miles (1,778 kilometers).

Unlimited class air racer Rare Bear as it appeared in 2014. (Unattributed)
Unlimited Class air racer Rare Bear as it appeared in 2014. (Unattributed)

¹ FAI Record File Number 8437

© 2017, Bryan R. Swopes

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20 August 1947

Douglas D-558-I Skystreak Bu. No. 37970 makes a pass over the 3 kilometer course on Muroc Dry Lake. (U.S. Navy)
Douglas D-558-I Skystreak, Bu. No. 37970, makes a pass over the 3-kilometer course at Muroc Dry Lake. (U.S. Navy)

20 August 1947: At Muroc Dry Lake in the high desert of southern California, Commander Turner Foster Caldwell, Jr., United States Navy, flew the first of three Douglas D-558-I Skystreaks, Bu. No. 37970, to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Straight Course.¹

Four passes were made over the course at an altitude of 200 feet (61 meters) or lower. Two runs were made in each direction to compensate for any head or tail winds. The official speed for a record attempt was the average of the two best consecutive passes out of the four.

Commander Caldwell’s average speed was 1,031.178 kilometers per hour (640.744 miles per hour). He was awarded his second Distinguished Flying Cross for this flight.

Commander Turner F. Caldwell, jr., United States Navy with the number one Douglas D-558-I Skystreak, Bu. No. 37970, at Muroc dry Lake, 1947. (U.S. Naval Institute)
Commander Turner F. Caldwell, Jr., United States Navy, with the number one Douglas D-558-I Skystreak, Bu. No. 37970, at Muroc Dry Lake, 1947. (U.S. Naval Institute)

The D-558 Program was intended as a three-phase test program for the U.S. Navy and the National Advisory Committee on Aeronautics (NACA) to investigate transonic and supersonic flight using straight and swept wing aircraft powered by turbojet and/or rocket engines. The Douglas Aircraft Company designed and built three D-558-I Skystreaks and three D-558-II Skyrockets. The Phase I aircraft were flown by Douglas test pilot Gene May and Navy project officer, Commander Turner Caldwell.

Major Marion E. Carl, USMC, left, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy)
Major Marion E. Carl, USMC, left, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy)

The D-558-I Skystreak was a single-engine, turbojet-powered airplane. It was built of magnesium and aluminum for light weight, but was designed to withstand very high acceleration loads. It was 35 feet, 8 inches (10.871 meters) long with a wingspan of 25 feet (7.62 meters) and overall height of 12 feet, 1¾ inches (3.702 meters). The airplane had retractable tricycle landing gear. Its empty weight was approximately 7,500 pounds (3,400 kilograms), landing weight at the conclusion of a flight test was 7,711 pounds (3,498 kilograms). The maximum takeoff weight was 10,105 pounds (4,583.6 kilograms). The aircraft fuel load was 230 gallons (870.7 liters) of kerosene.

This photograph shows two of the three D-558-I Skystreaks being inspected by U.S. navy officials at the Douglas Aircraft Company plant. In the foreground is the number two aircraft, Bu. No. 37971, with the sections o fte hfuselage separted for better viewing. The entire nose section, including teh cockpit, coul dbe jettisoned in an emergency. The second aircraft is Bu. No. 37970, th eSkystrak flown by CDR Caldwell for his speed record. In the background is another Douglas airplane, the famous AD Skyraider. (Douglas Aircraft Company)
This photograph shows two of the three D-558-I Skystreaks being inspected by U.S. Navy officers at the Douglas Aircraft Company plant. In the foreground is the number two aircraft, Bu. No. 37971, with the sections of the fuselage separated. The entire nose section, including the cockpit, could be jettisoned in an emergency. Just beyond that, two wing tip fuel tanks are displayed on a cart. The second aircraft is Bu. No. 37970. An Allison J35-A-11 jet engine is shown between that and the last airplane, another Douglas product, the famous AD Skyraider. (Douglas Aircraft Company)

The D-558-I was powered by a single Allison J35-A-11 turbojet engine. The J35 was a single-spool, axial-flow turbojet with an 11-stage compressor section, 8 combustion chambers and single-stage turbine. The J35-A-11 was rated at 5,000 pounds of thrust (22.24 kilonewtons). The engine was 12 feet, 1.0 inches (3.683 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,455 pounds (1,114 kilograms). The J35-A-11 was a production version of the General Electric TG-180, initially produced by Chevrolet as the J35-C-3. It was the first widely-used American jet engine.

The D-558-I had a designed service ceiling of 45,700 feet (13,930 meters). Intended for experimental flights of short duration, it had a very short range and took off and landed from the dry lake at Muroc. (After 1949, this would be known as Edwards Air Force Base.) The experimental airplane was not as fast as the more widely known Bell X-1 rocketplane, but rendered valuable research time in the high transonic range.

Gene May did reach Mach 1.0 in 37970, 29 September 1948, though he was in a 35° dive. This was the highest speed that had been reached up to that time by an airplane capable of taking off and landing under its own power.

The three D-558-I Skystreaks made a total of 229 flights and Bu. No. 37970 made 101 of them. After the Douglas test program was completed, -970 was turned over to NACA as NACA 140, but it was quickly grounded after the crash of the number two aircraft, and was used for spare parts for number three.

Today, 37970 is in the collection of the National Naval Aviation Museum at Naval Air Station Pensacola, Florida. The other surviving Skystreak, Bu. No. 37972, is at the Carolinas Aviation Museum, Charlotte-Douglas International Airport, Charlotte, North Carolina.

Rear Admiral Turner F. Caldwell, Jr., USN, circa 1960. (U.S. Navy)
Rear Admiral Turner F. Caldwell, Jr., United States Navy, circa 1960. (U.S. Navy)
Midshipman Turner F. Caldwell, jr., 1935. (U.S. Navy)

Turner Foster Caldwell, Jr., was born 17 November 1913 at Narbeth, Pennsylvania. He was the first of four children of Lieutenant Turner Foster Caldwell and Eleanor Polk Owings Caldwell. The senior Caldwell was a graduate of Yale University, New Haven, Connecticut, and was commissioned as an ensign, United States Navy, through the Reserve Officers Training Corps (R.O.T.C). Commander Caldwell was assigned to the U.S. Naval Academy, Annapolis, Maryland, 1 September 1930, and was promoted to the rank of captain, 1 October 1930. He retired from the Navy 1 August 1940.

Turner Foster Caldwell, Jr., entered the United States Naval Academy as a midshipman, 12 June 1931. He graduated and was commissioned an Ensign, United States Navy, 6 June 1935.

Ensign Caldwell was promoted to the rank of Lieutenant (Junior Grade), with date of rank 6 June 1938. He was assigned as a flight instructor at NAS Pensacola, Florida. On that same day, Lieutenant (j.g.) Caldwell married Miss Helen Adele Glidden of Coronado, California, at Yuma, Arizona. They would have four children.

By 1940, Lieutenant (j.g.) Caldwell was assigned to Scouting Squadron Five (VS-5). On 7 December 1941, VS-5 was aboard USS Yorktown (CV-5) at Norfolk Virginia.

Caldwell was promoted to Lieutenant, 1 January 1942. He was a Douglas SBD-3 Dauntless scout bomber bomber pilot with Scouting Squadron Five (VS-5) aboard U.S.S. Yorktown (CV-5) and commanded the squadron with its 18 SBD-3s aboard U.S.S. Enterprise (CV-6) during the occupation of Guadalcanal and the Battle of the Eastern Solomons.

Two Douglas SBD-3 Dauntless dive bombers from VB-5, USS Yorktown, 1942. (U.S. Navy)

Between March and September 1942 he was three times awarded the Navy Cross, the U.S. Navy’s second-highest award for valor after the Medal of Honor. He was promoted to lieutenant commander (temporary) 1 May 1943, and to commander, 1 March 1944. (He retained the permanent rank of lieutenant until after the war.)

Later he commanded a night fighter group of F6F Hellcats and TBM Avengers, CVLG(N)-41, assigned to USS Enterprise (CV(N)-6). For his actions during that period he was awarded his first Distinguished Flying Cross and the Legion of Merit.

After the war, Caldwell commanded Carrier Air Group 4 (CVG-4) aboard USS Franklin D. Roosevelt (CVB-42). He was promoted to the rank of captain, 1 July 1954. Captain Caldwell commanded the “long-hull” Essex-class aircraft carrier USS Ticonderoga (CVA-14), from 5 September 1959 to 24 August 1960.

USS Ticonderoga (CVA-14) underway off the Philippines, 24 May 1960. (San Diego Air and Space Museum Archives)

Captain Caldwell was promoted to the rank of rear admiral, 1 April 1963. He rose to the rank of Vice Admiral, 1 November 1967, and served as Director of Anti-Submarine Warfare Plans. Admiral Caldwell retired from the Navy in May 1971. He died at Kilmarnock Hospital, Rappahannock, Virginia, 12 October 1991.

Douglas D-558-I Skystreak, Bu. No. 37970, at the National Naval Aviation Museum, Naval Air Station Pensacola, Florida. (U.S. Navy)
Douglas D-558-I Skystreak, Bu. No. 37970, at the National Naval Aviation Museum, Naval Air Station Pensacola, Florida. (U.S. Navy)

¹ FAI Record File Number 9864

© 2017, Bryan R. Swopes

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