Yearly Archives: 2024

Brigadier General Robin Olds (14 July 1922–14 June 2007)

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Major Robin Olds, United States Army Air Forces. 1946. (LIFE Magazine)
Brigadier General Robert Olds, U.S. Army Air Corps, circa 1942.

14 July 1922: Brigadier General Robin Olds, United States Air Force, was a fighter pilot and triple ace with 16 official aerial victories in two wars. Robin Olds was born Robert Oldys, Jr., at Luke Field Hospital, Honolulu, Territory of Hawaii. He was the first son of Captain Robert Oldys, Air Service, United States Army, and Eloise Wichman Nott Oldys. In 1931, the family name was legally changed from Oldys to Olds. As a child, Robert, Jr., was known as “Robin,” a dimunuitive of Robert.

Robin Olds entered the United States Military Academy at West Point, New York, on 1 July 1940. During the summer months, he received primary, basic and advanced pilot training. With training at West Point accelerated because of wartime needs, Cadet Olds and his class graduated one year early, 1 June 1943. Olds was commissioned a Second Lieutenant, Air Corps, United States Army, (number 589 of 620 on the Air Corps list of second lieutenants), and was assigned to fighter training in the Lockheed P-38 Lightning at Williams Field, Arizona. On 1 December 1943, Second Lieutenant Olds was appointed to the rank of First Lieutenant, Army of the United States (A.U.S.). (His permanent rank remained Second Lieutenant, Air Corps, until after the War.)

On completion of all phases of training, Lieutenant Olds was assigned to the 434th Fighter Squadron, 479th Fighter Group, and deployed to England aboard the former Moore-McCormack Lines passenger liner S.S. Argentina, which had been converted to a troop transport.

Lieutenant Robin Olds with "SCAT II," A lockheed P-38 Lightning.
Lieutenant Robin Olds with “SCAT II,” a Lockheed P-38J-15-LO Lightning, 43-28707. (Imperial War Museum)

The 434th Fighter Squadron was based at RAF Wattisham in East Anglia. First Lieutenant Olds was promoted to Captain (A.U.S.) on 24 July 1944. He became an ace during his first two combat missions, shooting down 2 Focke-Wulf Fw 190 fighters on 14 August 1944 and 3 Messerschmitt Bf 109s on August 23.

The squadron re-equipped with North American P-51 Mustangs and Captain Olds continued to destroy enemy fighters. On 9 February 1945, just 22 years old, he was promoted to Major. On 25 March 1945, Major Olds was placed in command of the 434th Fighter Squadron. Major Olds completed the war with a record of 12 aerial victories,¹ and another 11.5 enemy aircraft destroyed on the ground. He had flown 107 combat missions.

Major Robin Olds with “SCAT VI,” a North American Aviation P-51K-5-NT Mustang, 44-11746, in England during World War II. (U.S. Air Force via Crazy Horse Aviation)
Robin Olds’ Mustang, “SCAT VII” (P-51D-25-NA 44-44729), escorts a B-17 Flying Fortress heavy bomber during World War II. This airplane still exists. (U.S. Air Force)

When the United States Air Force was established as a separate military service on 18 September 1947, Major Olds (along with hundreds, if not thousands of other officers) reverted to their permanent rank of First Lieutenant, with his date of rank retroactive to 1 June 1946. Olds retained the temporary rank of Major.

After World War II, Major Olds transitioned to jet fighters with the Lockheed P-80A Shooting Star at March Field, near Riverside, California. He flew in an aerobatic demonstration team, and on 1 September 1946, flew a Lockheed P-80A to second place in the Thompson Trophy Race, Jet Division, at Cleveland, Ohio. Olds averaged 514.715 miles per hour (828.354 kilometers per hour) over ten laps around the 30-mile (48.3 kilometers), four pylon course.

Major Robin Olds was scheduled to fly this Lockheed P-80A-1-LO Shooting Star, “SCAT X,” serial number 44-85027, in the 1946 Thompson Trophy Race. It had to be replaced shortly before the race. This fighter was damaged beyond repair and written off at Long Beach Army Airfield, California, 14 September 1946. (Kevin Grantham Collection via airrace.com)
Ella Raines (Universal Pictures)

While stationed at March Field, Olds met his future wife, actress Ella Wallace Raines (formerly, Mrs. Kenneth William Trout). They married on 6 February 1947 at the West Hollywood Community Church, just south of the Sunset Strip in the West Hollywood area of Los Angeles County, California. Rev. Gordon C. Chapman performed the ceremony. They would have two daughters, Christina and Susan. They divorced 15 November 1976.

In October 1948, Major Olds returned to England as an exchange officer in command of No. 1 Squadron, Royal Air Force, at RAF Tangmere. He was the first non-Commonwealth officer to command a Royal Air Force squadron. The squadron flew the Gloster Meteor F. Mk.IV jet fighter.

Following the tour with the R.A.F., Olds returned to March Air Force Base as operations officer of the 94th Fighter Squadron, Jet, 1st Fighter-Interceptor Group, which had been equipped with the North American Aviation F-86A-1-NA Sabre. Soon after, he was placed in command of the 71st Fighter-Interceptor Squadron, another squadron within the 1st Fighter-Interceptor Group.

North American Aviation F-86A Sabres of the 71st Fighter-Interceptor squadron at George AFB, California, 1950. The Sabre closest to the camera is F-86A-5-NA 48-214. (U.S. Air Force)

Olds was promoted to the rank of lieutenant colonel, 20 February 1951, and to colonel 15 April 1953. From 8 October 1955 to 10 August 1956 he commanded the 86th Fighter-Interceptor Group based at Landstuhl Air Base, Germany. The group flew the rocket-armed North American Aviation F-86D Sabre. The 86th was inactivated 10 August 1956. Colonel Olds then was assigned as chief of the Weapons Proficiency Center for the United States Air Forces in Europe (USAFE) at Wheelus Air Base, near Tripoli, Libya.

After assignment as Deputy Chief, Air Defense Division, Headquarters USAF, from 1958 to 1962, Colonel Olds attended the National War College, graduating in 1963. From 8 September 1963 to 26 July 1965, Colonel Olds commanded the 81st Tactical Fighter Wing, at RAF Bentwaters, England.

Colonel Olds with a McDonnell F-101C Voodoo at RAF Bentwaters. (U.S. Air Force)
Colonel Olds with a McDonnell F-101C Voodoo at RAF Bentwaters. (U.S. Air Force)

Robin Olds returned to combat as commander of the 8th Tactical Fighter Wing at Ubon Royal Thai Air Force Base, Thailand, in September 1966. Flying the McDonnell F-4C Phantom II, Colonel Olds scored victories over two Vietnam Peoples Air Force Mikoyan-Gurevich MiG-17s and two MiG-21s, bringing his official score to 16 ² aerial victories. ³ He was the only Air Force fighter ace with victories in both World War II and the Vietnam War. (There have been rumors that he actually shot down seven MiGs, but credited those to other pilots to avoid being pulled out of combat and sent back to the United States.)

For his actions during the attack against the Paul Doumer Bridge, 11 August 1967, Colonel Olds was awarded the Air Force Cross. He flew 152 combat missions during the Vietnam War. His final combat mission was on 23 September 1967.

Coloenl Robin Olds, 8th Tactical Fighter Wing, with SCAT XXVII, his McDonnell F-4C-24-MC Phantom II, 64-0829, at Ubon Rachitani RTAFB, 1967. U.S. Air Force)
Colonel Robin Olds, 8th Tactical Fighter Wing, with SCAT XXVII, his McDonnell F-4C-24-MC Phantom II, 64-0829, at Ubon RTAFB, May 1967. U.S. Air Force)

On 1 June 1968, Robin Olds was promoted to the rank of brigadier general and assigned as Commandant of Cadets at the United States Air Force Academy. In February 1971, he was appointed Director of Aerospace Safety in the Office of the Inspector General at Norton Air Force Base, near San Bernardino, California. He retired from the Air Force 31 May 1973.

During his military career, Brigadier General Robin Olds had been awarded the Air Force Cross, Distinguished Service Medal, Silver Star with three oak leaf clusters (four awards), Legion of Merit, Distinguished Flying Cross with five oak leaf clusters (six awards), Air Medal with 39 oak leaf clusters (40 awards), Air Force Commendation Medal, as well as the Distinguished Flying Cross of the United Kingdom, the Croix de Guerre (France), and the Republic of Vietnam’s Distinguished Service Medal, Air Gallantry Medal with Gold Wings, Air Service Medal and Vietnam Campaign Medal.

Colonel Robin Olds, United States Air Force
Colonel Robin Olds, 8th Tactical Fighter Wing, United States Air Force

In 1978, Robin Olds married his second wife, Abigail Morgan Sellers Barnett. They were divorced in 1993.

Brigadier General Robin Olds passed away 14 June 2007 at the age of 84 years. He is buried at the United States Air Force Academy Cemetery, Colorado Springs, Colorado.

Brigadier General Robin Olds next assignment was as Commandant of Cadets at the United States Air Force Academy, Colorado Springs, Colorado, where I had the pleasure of serving under his command. (U.S. Air Force)
Brigadier General Robin Olds’ next assignment was as Commandant of Cadets at the United States Air Force Academy, Colorado Springs, Colorado, where I had the pleasure of serving under his command. (Bryan R. Swopes) (U.S. Air Force photograph)

Note: Thanks to Ms. Christina Olds and Lieutenant Colonel R. Medley Gatewood, U.S. Air Force (Retired), for their input to this article.

¹ Source: USAF CREDITS FOR THE DESTRUCTION OF ENEMY AIRCRAFT, WORLD WAR II, Albert F. Simpson Historical Research Center, Air University. Office of Air Force History, Headquarters, USAF, 1978. Pages 143–144:

² Source: ACES and AERIAL VICTORIES, The United States Air Force in Southeast Asia 1965–1973, Albert F. Simpson Historical Research Center, Air University. Office of Air Force History, Headquarters, USAF, 1976. Page 135:

³ Under the rules in effect at the time, a pilot and WSO shared credit for an enemy aircraft destroyed, with each being credited 0.5 kills. Colonel Olds was officially credited with 2.0 kills. The rules were changed in 1971, retroactive to 1965. This gave Olds an official score of 4.0. —Source: To Hanoi and Back: The United States Air Force and North Vietnam 1966–1973, by Wayne Thompson. Air Force History Office, 2000. Chapter 4 at Page 11.

© 2019, Bryan R. Swopes

14 July 1911

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Harry Nelson Atwood, 1914. (Bain News Service, Library of Congress)
Harry Nelson Atwood, 1914. (Bain News Service, Library of Congress)

14 July 1911: Three months after learning to fly at the Wright Flying School, Huffman Prairie, Ohio, Harry Nelson Atwood flew from Boston to Washington, D.C., a distance of 576 miles (927 kilometers) over 14 days, and completed the final leg from College Park, Maryland, by landing his Wright Model B airplane on the South Lawn of the White House. President William Howard Taft and his secretary, Charles Dewey Hilles (former Assistant Secretary of the Treasury), were watching from the south portico.

President Taft presented Atwood with a gold medal from the Aero Club of Washington. Atwood’s mother was also present at the ceremony.

Harry Atwood and his Wright Model B over the White House lawn, 14 July 1911. (Smithsonian Institution)
Harry Atwood and his Wright Model B over the White House south lawn, 14 July 1911. (Smithsonian Institution)

Atwood’s airplane was a Wright Model B, which he had named Moth. The Wright Model B was a two-place, single-engine biplane. The elevator was at the rear, rather than in canard position as had been the earlier Wright airplanes. (This configuration was known as “headless.”) Roll control was through the Wright Brother’s patented wing-warping system. It was 26 feet (7.925 meters) long with a wingspan of 39 feet (11.887 meters). It weighed 800 pounds (363 kilograms) empty and had a gross weight of 1,250 pounds (567 kilograms).

The Model B was powered by a single water-cooled, fuel-injected, 240.528 cubic-inch-displacement (3.942 liter) Wright vertical overhead-valve inline four-cylinder gasoline engine with 2 valves per cylinder and a compression ratio of 4.165:1. It produced 32 horsepower at 1,310 r.p.m. During three years of production (1908–1911) Wright “4-40” engines were built that operated from 1,325 to 1,500 r.p.m. Power output ranged from 28 to 40 horsepower. These engines weighed from 160 to 180 pounds (72.6–81.6 kilograms).

Two 8½ foot (2.591 meters) diameter, two-bladed, counter-rotating propellers, driven by a chain drive, are mounted behind the wings in pusher configuration. They turned 445 r.p.m.

The Wright Model B had a maximum speed of approximately 40 miles per hour (64 kilometers per hour) and its range was 110 miles (177 kilometers).

Approximately 100 Model B aeroplanes were built by the Wrights and under license by Burgess from 1910 to 1914. Three are known to exist.

A reproduction of a Wright Model B
A reproduction of a Wright Model B

Harry Nelson Atwood was born in the family home at Roxbury, a suburb of Boston, Massachusetts, 15 November 1883. He was the first of two children of Samuel Shurtleff Atwood, a coal dealer, and Florence Nelson Atwood, of Nantucket.

Harry Atwood attended the Massachussetts Instititute of Technology at Cambridge, Massachussetts, from 1903 to 1908, where he studied electrical engineering and was a member of the Phi Beta Epsilon (ΦΒΕ) fraternity.

He married his first wife, Sarah Matilda Jenkins at Lynn, Mass, 7 February 1906. They would have two children, but divorced after several years. On 2 March 1914, Atwood married Ruth Satherwaite at Reading, Pennsylvania. After Ruth Atwood died in 1920, he married her sister-in-law, Helen Louise Kestner Sattherwaite, widow of Ruth’s brother, 16 June 1922. They were soon divorced, and in May 1923, Helen Kestner Atwood traveled to Europe as a Red Cross social worker. Atwood next married Mary E. Dalton, who died soon after their son was born. Atwood’s fifth wife was Nellie Dow. They had a daughter, and remained together until Atwood’s death.

Atwood remained in the aviation industry as an inventor and research scientist. He died at District Memorial Hospital, Valleytown Township, Andrews, North Carolina, 14 July 1967, 56 years to the day after his landing on the White House lawn. Harry Nelson Atwood was buried at the Hanging Dog Baptist Church Cemetery, Murphy, North Carolina.

© 2017, Bryan R. Swopes

14 July 1897

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The hydrogen balloon Örnen (Eagle) on the polar ice cap, 14 July 1897. (Nils Strindberg)

14 July 1897: At 8:11 p.m., G.M.T., the Andrée Arctic Expedition’s hydrogen gas balloon, Örnen (Eagle), came to rest on an ice floe in the Arctic Ocean, at N. 82° 52′, E. 29° 32′. ¹ This was the end of a planned transpolar flight and the beginning of a three-month struggle for survival.

Balloon Örnen (Eagle) in its protective enclosure, Danes Island, Spitzbergen, Norway. (Andréemuseet, Griänna, Sweden)

At 1:50 p.m., 11 July 1897, Örnen rose from its protective enclosure on Danskøya (Danes Island) in the Svalbard Archipelago of Norway. Carried aloft in the balloon’s gondola were the expedition’s leader, Salomon August Andrée, and his fellow explorers, Knut Hjakmar Ferdinand Frænkel and Nils Strindberg.

Intrepid aeronauts: Left to right, Gustav Vilhem Emanuel Swedenborg (alternate); Nils Strindberg; Knut Hjakmar Ferdinand Frænkel; Salomon August Andrée (seated). (Andréemuseet, Griänna, Sweden)

The goal of the expedition was to fly across the North Pole and onward to Alaska on the North American Continent. Andrée considered that the balloon would need to retain enough gas during the voyage to remain airborne for 30 days. Supplies for the three men for that period were carried. 36 homing pigeons would allow the explorers to report their progress to the outside world.

This would be the expedition’s second attempt. The previous year, adverse winds forced the aeronauts to abandon the flight.

Balloon Örnen in its protective enclosure, Danes Island, Spitzbergen, Norway. (Andréemuseet, Griänna, Sweden)
Henri Lachambre

Örnen had been designed and manufactured by Henri Lachambre at his balloon factory at Vaugirard, a suburb on the Left Bank of the Seine, Paris, France. The envelope was assembled from approximately 3,360 pieces of a thin woven Chinese silk fabric called pongee, stitched by hand. The seams were covered by glued strips of pongee. The upper two-thirds of the gas bag had three layers of fabric, while the lower one-third had two plies. It is estimated that 8 million stitches were required. Once completed, the envelope was covered with varnish.

The gondola was constructed of wood and wicker. It had an upper, observation, deck, and an enclosed lower sleeping quarters/darkroom.

A net made of more than 300 hemp ropes covered the balloon, and were braided into twelve ropes which were attached to a lifting ring. The gondola was suspended below this. At Sea Level, the inflated balloon with its gondola were approximately 97 feet (29.6 meters) high, and 68 feet (20.7 meters) in diameter. Its total volume is estimated at 4,800 cubic meters (approximately 170,000 cubic feet).

Buoyancy was provided by hydrogen gas which was produced on site at Danskøya. Hydrogen is the lightest element, and gaseous hydrogen has just 7% of the density of air. This provides greater buoyancy for lighter-than-air vehicles than other gases, but hydrogen gas molecules are also the smallest and they diffuse through fabric barriers more easily than any other gas. (Tests before Örnen was launched found that the balloon was losing about 35 cubic meters/1,236 cubic feet of hydrogen each day.)

Balloons have a disadvantage in that they go where the wind takes them. They are not steerable like dirigibles. So, steady southerly winds would be needed to carry Örnen to the North Pole, and northerly winds to travel from there to Alaska. Andrée had a theory that he believed would allow him to steer his balloon as much as 30° to either side of the prevailing wind.

Andrée’s idea was that if several long, heavy ropes were dragged behind the balloon, their weight and friction would cause the balloon to travel slower than the wind was blowing. He could then use two small sails to steer.

Örnen with guide ropes dragging in the water.

Also, these ropes could be used to control the balloon’s altitude. By pulling the ropes in, the weight supported by the balloon would increase, and it would descend. Letting more rope out would mean that the extra weight would be transferred to the surface, and the balloon would rise.

Altitude was critical. Andrée planned to maintain about 150 meters (approximately 500 feet). As the balloon ascended, atmospheric pressure on the envelope decreased. The pressure differential between the atmosphere and the hydrogen would increase, forcing the hydrogen to pass through the envelope more quickly. Any hydrogen loss was permanent, and the balloon’s buoyancy would decrease.

Balloon Örnen airborne, around 2:00 p.m., 11 July 1897. The wake of the steering ropes can be seen on the surface of the sea. (Andréemuseet, Griänna, Sweden)

Problems began immediately. As the guide ropes dragged through the water, they became heavier. They pulled the balloon down to the surface and the gondola actually touched the water. The aeronauts frantically began dumping ballast. Three of the four ropes became entangled and were pulled loose. Örnen began to rise again, but having lost ballast and the weight of the three guide ropes, it climbed to about 1,600 feet (490 meters). The loss of hydrogen accelerated.

The Eagle floated northward above a fog bank. It sank into the fog and sunlight shining on the envelope decreased. The balloon cooled and the gas inside began to contract. Buoancy decreased and the balloon sank further into the fog.

An alternating pattern of rising and falling developed. After the explorers passed into the Arctic ice pack, the gondola would alternately bounce across the broken ice, then rise again into the sky. At about 10:00 p.m., July 12, the gondola settled on to the ice and remained there for the next thirteen hours.

At 10:55 a.m., 13 July, once again airborne, the balloon continued on its flight. Drizzle and fog caused ice to form on the envelope. The gondola dragged behind. After jettisoning hundreds of pounds of ballast and equipment, Örnen rose higher, but again settled toward the ice. The remaining guide rope was lost. Realizing that the end of the flight was inevitable, the crew opened to valves to release the hydrogen. The balloon settled to the ice, and at 8:11 p.m., 14 July 1897, the crew climbed down from the gondola onto the ice floe.

Örnen on the arctic ice, 14 July 1897 (Nils Strindberg)

The total elapsed time of the journey was 65 hours, 35 minutes. In that time, Andrée, Frænkel and Strindberg had traveled 295 miles (475 kilometers) from their starting point on Danskøya.

The next three months were a courageous battle for survival as the three explorers tried to make their way back to civilization. They reached Kvitøya (White Island), an ice-covered island at the northeast of the Svalbard Archipelago. Andrée’s final journal entry was made on 17 October.

The bodies of the three men were discovered in 1930. Their remains were taken to Sweden.

There is much speculation as to the cause of their deaths, ranging from exposure, exhaustion, illness, suicide, or bear attack.

Track of the 1897 Andrée Arctic Expedition.

The expedition left behind journals with detailed meteorological data and other observations. More than 200 photographic images were left on film negatives protected in metal canisters.

The 1897 Andrée Arctic Expedition is the subject of books, newspaper and magazine articles, at least one motion picture, as well as many Internet articles of varying detail. The images taken by Nils Strindberg are available on the Internet and tell of their experiences.

Salomon August Andrée (18 October 1854–1897)

¹ Geographic location of Örnen‘s landing site from the Comité International d’Aérostation (CIA, the Fédération Aéronautique Internationale Ballooning Commission).

© 2018, Bryan R. Swopes

13 July 1968

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General Dynamics FB-111A 67-0159, the first production aircraft. (U.S. Air Force)

13 July 1968: The first production General Dynamics FB-111A supersonic strategic bomber successfully completed a 30-minute maiden flight at Carswell Air Force Base, Fort Worth, Texas. The FB-111A differed from the F-111A fighter bomber with the substitution of a larger wing, originally designed for the F-111B, giving the bomber a 7 foot (2.134 meter) increase in wingspan. The landing gear was strengthened, the bomb bay enlarged, and it had more powerful engines.

Aardvark (Orycteropus afer)

The airplane’s very long nose earned the nickname “Aardvark,” but this did not become official until 1996.

67-0159 was delivered to the U.S. Air Force 4 September 1968 and assigned to the Air Force Flight Test Center, Edwards Air Force Base, California. (The first six production airplanes were used for flight testing.)

67-0159 was later converted to the F-111G configuration. In 1980 it was sent to the Sacramento Air Logistics Center to test weapons modifications and received a spectacular white and orange paint scheme. It was retired in 1990. 67-0159 is in the collection of the National Museum of the United States Air Force. It is on loan and now on display at the Aerospace Museum of California, Sacramento, California.

General Dynamics FB-111A-CF (F-111G) 67-159

The General Dynamics FB-111A is a two-place, twin-engine, strategic bomber with variable-sweep wings, assigned to the Strategic Air Command. It is 73.54 feet (22.415 meters) long. The wingspan varies from a maximum 70.0 feet (21.336 meters) when fully extended, and a minimum 33.96 feet (10.351 meters) when swept fully aft. Overall height is 17.04 feet (5.194 meters).

The wings of the FB-111A have a total area of 550 square feet (51.10 square meters). When fully extended, the wings’ leading edges are swept aft to 16.0°. The angle of incidence at the root is +1° and -3° at the tip. There is 1.0° dihedral.

The Aardvark’s empty weight is 47,481 pounds (21,537 kilograms). Normal maximum takeoff weight is 116,115 pounds (52,669 kilograms), and the maximum overload takeoff weight is or 119,243 pounds (54,088 kilograms).

The aircraft is powered by two Pratt & Whitney TF30-P-107 engines. This is a two-spool axial-flow turbofan engine with afterburner. It has a 3-stage fan section, 13-stage compressor section (6 low- and 7 high-pressure stages) and 4-stage turbine (1 high- and 3 low-pressure stages). The -107 has a maximum continuous power rating of 10,800 pounds of thrust (48.041 kilonewtons) at 14,150 r.p.m., N2 (static thrust, at Sea Level), and a maximum power rating of 20,350 pounds (90.521 kilonewtons) at 14,550 r.p.m., N2 (45 minute limit) The T30-P-107 is 3 feet, 2.12 inches (0.968 meters) in diameter, 20 feet, 1.4 inches (6.132 meters) long,  and weighs 4,121 pounds (1,869 kilograms).

The FB-111A has an average cruise speed of 415–442 knots (478–509 miles per hour/769-819 kilometers per hour), depending on the mission profile. It’s maximum speed at 50,000 feet (15,240 meters) is 1,262 knots (1,452 miles per hour/2,337 kilometers per hour)—Mach 2.20. The bomber’s service ceiling varies from 50,390 feet to 56,380 feet (15,359–17,185 meters), again, depending on the mission profile. The maximum combat range is 4,920 nautical miles (5,662 statute miles/9,112 kilometers). The airplane can carry as many as six 600 gallon (2,271 liter) external tanks on underwing pylons. This gives the Aardvark a maximum ferry range of 4,313 nautical miles (4,963 statute miles/7,988 kilometers).

General Dynamics FB-111A 67-0159. (fb111.net)
General Dynamics F-111A 66-0011, a test airplane in the FB-111A program, loaded with four AGM-69 SRAM missiles. The dots on the missiles and airplane are for precise tracking from ground stations. (U.S. Air Force)

The FB-111A could carry weapons in an internal bomb bay or on underwing hardpoints. It could be armed with up to 37,500 pounds (17,010 kilograms) of conventional bombs; or six AGM-69A Short Range Attack Missiles (SRAM). The Aardvark could carry maximum of six nuclear weapons (B-43, B-57 or B-61).

General Dynamics YFB-111A 63-9783, the prototype strategic bomber variant. (U.S. Air Force)

In addition to a prototype (63-9783, which was converted from the last production F-111A) General Dynamics built 76 FB-111A strategic bombers. With the introduction of the Rockwell B-1B Lancer, the FB-111As remaining in service were converted to F-111G tactical fighter bombers. They were retired by 2003.

The Royal Australian Air Force bought 15 of the F-111Gs. By 2007, these had also been taken out of service.

Two General Dynamics FB-111As in formation, 1 December 1983. (MSGT Buster Kellum, U.S. Air Force)

© 2018, Bryan R. Swopes

13 July 1928

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Maryse Bastie
Maryse Bastie (FAI)

13 July 1928, Mme Maryse Bastié flew her Caudron C. 109, F-AHFE, from Le Bourget airport, Paris, France, to Trzebiatów, Pomeranina, a distance of 1,058 kilometers (657.4 statute miles). (The Fédération Aéronautique Internationale records database does not show this record.) Mme Bastié is credited with eight FAI world records.

An FAI news article dated 28 July 2019 credits Maryse Bastié with being the first woman to have held a world record in aviation.¹

Maryse Bastié’s Caudron C. 109, F-AHFE. (FAI)

Mme Bastié’s airplane was a two-place, single-engine, Caudron C. 109 parasol-wing monoplane, F-AHFE, serial number 5804.1.

The C. 109 had a length of 6.440 meters (21 feet, 1.5 inches), wing span of 11.50 meters (37 feet, 8.8 inches) and height of 2.530 meters (8 feet, 3.6 inches). Its empty weight was 330 kilograms (727.525 pounds) and gross weight, 532 kilograms (1,173 pounds).

The standard C. 109 had a fuel capacity of 57 liters (15 U.S. gallons), and carried 15 litres (4 U.S. gallons) of lubricating oil for the engine. Its maximum speed was 120 kilometers per hour (75 miles per hour).

F-AHFE was powered by a naturally aspirated, air-cooled, 2,959.8 cubic centimeter (180.62 cubic inches) Société des Moteurs Salmson 9AD nine cylinder radial engine. The 9AD had a cylinder bore diameter of 69.9 millimeters (2.752 inches), and piston stroke of 85.7 millimeters (3.374 inches). It was rated at 45 ch at 2,000 r.p.m. The engine was 69.1 centimeters (27.20472 inches long and 63 centimeters (24.8031 inches) in diameter. It weighed 69.9 kilograms (154.1 pounds).

Salmson 9AD (NASM 2022-01819)

F-AHFE had set two FAI world records. On 25 October 1927, Raymond Delmotte flew over a closed circuit from Villacoublay to Saran in France, for a total distance of 1 535,20 kilometers (953.93 statute miles).² Two days later, 27 October 1927, Max Knipping flew from Le Bourget, Paris, France, to Königsberg, Germany, a distance of 1 581,84 kilometers.³

The airplane was first registered to M. Cuadron as F-ESDE, 06.11.25. It was the sold to M. Bastié at Issy. Later, Guy Bart, Chennevieres-sur-Marne; André Lemoine, Reims; and Pierre Gaston Lapanne at Nancy.

¹ The earliest record credited to Mme Bastié in the FAI online records database is Number 10446, 28 July 1929.  However, the database shows a number of earlier records credited to women: 12219, 2 January 1929, Evelyn Trout; 12216, 31 January 1929, Elinor Smith; 12220, 11 February 1929, Evelyn Trout; 12223, 17 March 1929, Louise McPhetridge; 12217, 24 April 1929, Elinor Smith; 12206, 28 May 1929, Marvel Crosson; 12214, 20 December 1928, Viola Gentry; 12221, 7 December 1928, Louise McPhetridge; 12212, 2 December 1928, Jane Heath; and 8221, 5 July 1927, The Hon. Bailey.

² FAI Record Number 9185

³ FAI Record 9166

© 2023, Bryan R. Swopes