Category Archives: Aviation

19 June 1947

P-80R speed run
Colonel Boyd flies the Lockheed XP-80R over the 3 kilometer course at Muroc Army Air Field, 19 June 1947. (U.S. Air Force)

19 June 1947: At Muroc Army Airfield (now, Edwards Air Force Base) Colonel Albert Boyd, United States Army Air Forces, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course, with an average speed of 1,003.81 kilometers per hour (623.74 miles per hour).¹ This was not just a class record, but an absolute world speed record.

Col. Boyd flew the Lockheed P-80R Shooting Star, serial number 44-85200, four times over the course, twice in each direction. The record speed was the average of the two fastest consecutive runs. As can be seen in the above photograph, these runs were flown at an altitude of approximately 70 feet (21 meters).

Originally a production P-80A-1-LO Shooting Star, 44-85200 had been converted to the XP-80B, a single prototype for the improved P-80B fighter.

Lockheed P-80A-1-LO shooting Star 44-85004, similar to the fighter being test flown by Richard I. Bong, 6 August 1945. (U.S. Air Force)
A very early production Lockheed P-80A-1-LO Shooting Star, 44-85004. (U.S. Air Force)

The P-80A-1-LO was a single-place, single-engine, low-wing monoplane powered by a turbojet engine. It was a day fighter, not equipped for night or all-weather combat operations. The P-80A was 34 feet, 6 inches (10.516 meters) long with a wingspan of 38 feet, 10½ inches (11.849 meters) and overall height of 11 feet, 4 inches (3.454 meters). The fighter had an empty weight of 7,920 pounds (3,592 kilograms) and a gross weight of 11,700 pounds (5,307 kilograms).

The P-80A-1 was powered by an Allison J33-A-9 or -11 turbojet, rated at 3,850 pounds of thrust (17.126 kilonewtons). It had a maximum speed of 558 miles per hour (898 kilometers per hour) at Sea Level and a service ceiling of 45,000 feet (13,716 meters).

The P-80A was armed with six Browning .50-caliber machine guns grouped together in the nose.

Lockheed P-80B-1-LO Shooting Star 45-8554, 1948. (U.S. Air Force)
Lockheed P-80B-1-LO Shooting Star 45-8554, 1948. (U.S. Air Force)

After modification to the XP-80B configuration, 44-85200 was powered by an Allison J33-A-17 with water/alcohol injection. It was rated at 4,000 pounds of thrust (17.793 kilonewtons). Fuel capacity was reduced by 45 gallons (170 liters) to allow for the water/alcohol tank. This was also the first American-built fighter to be equipped with an ejection seat.

The P-80B was heavier than the P-80A, with an empty weight of 8,176 pounds (3,709 kilograms) and gross weight of 12,200 pounds (5,534 kilograms). Visually, the two variants are almost identical.

The XP-80B had a maximum speed of 577 miles per hour (929 kilometers) per hour at 6,000 feet (1,829 meters), a 19 mile per hour (31 kilometers per hour) increase. The service ceiling increased to 45,500 feet (13,868 meters).

This photograph of XP-80R shows the cut-down windscreen an canopy, recontoured leading edges and the NACA-designed engine intakes. (U.S. Air Force)
This photograph of XP-80R shows the cut-down windscreen and canopy, re-contoured wing leading edges and the low-drag, NACA-designed engine intakes. (U.S. Air Force)

44-85200 was next modified to the XP-80R high-speed configuration. The canopy was smaller, the wings were shortened and their leading edges were re-contoured. In its initial configuration, the XP-80R retained the J33-A-17 engine, and incorporated new intakes designed by the National Advisory Committee for Aeronautics (NACA).

The initial performance of the XP-80R was disappointing. The intakes were returned to the standard shape and the J33-A-17 was replaced by a J33-A-35 engine. This improved J33 would be the first turbojet engine to be certified for commercial transport use (Allison Model 400). It was rated at 5,200 pounds of thrust (23.131 kilonewtons) at 11,750 r.p.m. at Sea Level, and 5,400 pounds of thrust (24.020 kilonewtons) with water/methanol injection.

The J33 was a single-spool turbojet with a single-stage centrifugal-flow compressor, 14 combustion chambers, and a single-stage axial-flow turbine. The J33-A-35 had a maximum diameter of 4 feet, 1.2 inches (1.250 meters) and was 8 feet, 8.5 inches (2.654 meters) long. It weighed 1,795 pounds (814 kilograms).

Lockheed P-80R 44-85200 at the National Museum of the United States Air Force
Lockheed P-80R 44-85200 at the National Museum of the United States Air Force

Technicians who modified the XP-80R at Lockheed Plant B-9 Production Flight Test Center, Metropolitan Airport, Van Nuys (just a few miles west of the main plant in Burbank). nicknamed the modified Shooting Star “Racey.”

Lockheed XP-80R 44-85200 is in the collection of the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio.

DAYTON, Ohio -- Lockheed P-80R at the National Museum of the United States Air Force. (U.S. Air Force photo)
Lockheed P-80R 44-85200 at the National Museum of the United States Air Force.

At the time of the speed record flight, Colonel Boyd was chief of the Flight Test Divison at Wright Field, Dayton, Ohio.

Albert Boyd was born 22 November 1906 at Rankin, Tennessee, the first of three sons of Kester S. Boyd a school night watchman, and Mary Eliza Beaver Boyd. In 1924, Boyd graduated from high school in Asheville, North Carolina, then attended Buncombe Junior College in Asheville.

Boyd was one of the most influential officers to have served in the United States Air Force. He entered the U.S. Army Air Corps as an aviation cadet 27 October 1927. After completion of flight training at Maxwell Field, Alabama, Boyd was commissioned as a second lieutenant, Air Corps Reserve, 28 February 1929, and as a second lieutenant, Air Corps, 2 May 1929.

Lieutenant Boyd married Miss Anna Lu Oheim at San Antonio, Texas, 8 September 1933. She was the daughter of Mr. and Mrs. G.F. Oheim of New Braunfels, Texas, (1907–1981).

He was promoted to 1st lieutenant 1 October 1934. Lieutenant Boyd served as a flight instructor at Maxwell Field, Alabama, and then Brooks, Kelly and Randolph Fields in Texas.

In 1934, 1st Lieutenant Boyd was assigned as engineering and operations officer at Chanute Field, Rantoul, Illinois. He completed the Air Corps technical School and the Engineer Armament Course. On 24 July 1936, Boyd was promoted to the temporary rank of captain. This rank became permanent 2 May 1939. In 1939 he was assigned to the Hawaiian Air Depot as assistant engineering officer, and was promoted to major (temporary), 15 March 1941. He and Mrs. Boyd lived in Honolulu. His Army salary was $3,375 per year. In December 1941, he became the chief engineering officer.

On 5 January 1942, Major Boyd was promoted to lieutenant colonel (temporary) and rated a command pilot. Following the end of World War II, Boyd reverted to his permanent rank of major, 2 May 1946.

In October 1945, Major Boyd was appointed acting chief of the Flight Test Division at Wright Field. He became chief of the division, October 1945, and also flew as an experimental test pilot. Boyd believed that it was not enough for Air Force test pilots to be superior pilots. They needed to be trained engineers and scientists in order to properly evaluate new aircraft. He developed the Air Force Test Pilot School and recommended that flight testing operations be centered at Muroc Field in the high desert of southern California, where vast open spaces and excellent flying conditions were available. He was the first commander of the Air Force Flight Test Center.

Colonel Albert G. Boyd with XP-80R 44-85200 (U.S. Air Force)
Colonel Albert G. Boyd with the Lockheed XP-80R, 44-85200. (U.S. Air Force)

When Brigadier General Boyd took command of Muroc Air Force Base in September 1949, he recommended that its name be changed to honor the late test pilot, Glen Edwards, who had been killed while testing a Northrop YB-49 near there, 5 June 1948. Since that time the airfield has been known as Edwards Air Force Base.

Major General Albert Boyd, United States Air Force
Major General Albert Boyd, United States Air Force.

In February 1952, General Boyd was assigned as vice commander of the Wright Air Development Center, and commander, June 1952. His final assignment on active duty was as deputy commander of the Air Research and Development Command at Baltimore, Maryland, from 1 August 1955.

From 1947 until he retired in 1957 as a major general, Albert Boyd flew and approved every aircraft in use by the U.S. Air Force. By the time he retired, he had logged over 21,120 flight hours in more than 700 different aircraft. He had been awarded the Legion of Merit, the Distinguished Flying Cross and the Distinguished Service Medal.

Major General Albert Boyd retired from the Air Force 30 October 1957 following 30 years of service.

General Boyd died at Saint Augustine, Florida, 18 September 1976, at the age of 69 years. He is buried at the Arlington National Cemetery.

¹ FAI Record File Number 9863

© 2018, Bryan R. Swopes

19 June 1937

Amelia Earhart’s Lockheed Electra 10E Special, NR16020, being serviced at Rangoon, Burma. (Purdue University Libraries, Archives and Special Collections)

19 June 1937: Leg 21, Akyab to Rangoon, Burma, 268 nautical miles (308 statute miles/496 kilometers).

“The next day, June 19, we started again from Akyab, with the hope of getting through to Bangkok, Siam, monsoons permitting. But they did not permit, so the flight ended at Rangoon, only 400 miles away. This short hop produced even worse weather than that which turned us back on the previous day. Then we had tried unsuccessfully to sneak underneath the monsoon. Those tactics again failing, this time we pulled up to 8,000 feet to be sure of missing the mountain ridges, and barged through. After two hours of flying blind in soupy atmosphere we let down and the bright green plains beside the Irrawaddy River smiled up at us. Then we dodged about for fifty miles. . .

“The first sight at Rangoon was the sun touching the Shwe Dagon Pagoda. This great structure stands on a considerable prominence and could be seen for miles while the city was still but a shadow on the horizon, its covering of pure gold a burnished beacon for wayfarers of the air. Shortly after our landing, rain poured down so heavily that it was hazardous to take off for Bankok, so we decided to stay where we were for a time at least.”

—Amelia Earhart

The Shwedagon Pagoda, Yangon, Myanmar. (Unattributed)
The Shwedagon Pagoda, Yangon, Myanmar. (Unattributed)
Great Circle route from Akyab to Rangoon, 268 nautical miles (308 statute miles/496 kilometers). (Great Circle Mapper)

© 2019, Bryan R. Swopes

18 June 1981

Lockheed Full Scale Development YF-117A, 79-10780, in light, three-tone desert camouflage. (Lockheed Martin)
Lockheed Full Scale Development YF-117A, 79-10780, in three-tone desert camouflage. (Lockheed Martin)

18 June 1981: At 6:05 a.m., Pacific Daylight Time (1305 UTC), the first Full Scale Development Lockheed YF-117A Nighthawk, 79-10780, made its first flight at Groom Lake, Nevada, with “Skunk Works” test pilot Harold C. (“Hal”) Farley, Jr. at the controls. The super-secret airplane was made of materials that absorbed radar waves, and built with the surfaces angled so that radar signals are deflected away from the source.

Harold "Hal" Farley, Jr., with a Lockheed F-117A Nighthawk.
Harold “Hal” Farley, Jr., with a Lockheed F-117A Nighthawk. (Lockheed Martin)

Hal Farley is a former U.S. Naval Aviator who spent eight years testing F-14 Tomcat fighters for Grumman before going to work at Lockheed’s “Skunk Works.” He flew the Have Blue proof-of-concept prototype and the Senior Trend F-117 program. When he retired from Lockheed, Farley had more that 600 flight hours in the F-117s. His call sign is “Bandit 117.”

Commonly called the “Stealth Fighter,” the Nighthawk is actually a tactical bomber. Five developmental aircraft and 59 operational F-117As were built. They were in service from 1983 until 2008, when the Lockheed F-22 Raptor was planned to assume their mission. They are mothballed and could be returned to service if needed.

A Lockheed F-117A Nighthawk takes off from Groom Lake, Nevada.
A Lockheed F-117A Nighthawk takes off from Nellis Air Force, Base, Nevada. (Lockheed Martin)

The Lockheed F-117A Nighthawk is a single-seat, twin-engine tactical bomber with swept wings and tail surfaces. It is 65 feet, 11 inches (20.091 meters) long with a wingspan of 43 feet, 4 inches (13.208 meters) and height of 12 feet, 5 inches (3.785 meters). The wings’ leading edges are swept aft to 67° 30′. The total wing area is 912.7 square feet ( square meters). The Nighthawk has an empty weight of 29,500 pounds (13,381 kilograms) and a maximum takeoff weight of 52,500 pounds (23,814 kilograms).

The F-117 is powered by two General Electric F404-F1D2 engines. These are two-spool axial-flow turbofan engines which have a 3-stage fan section, 7-stage compressor and 2-stage turbine. They are rated at 10,540 pounds of thrust (46.88 kilonewtons), each. The -F1D2 is 2 feet, 10.8 inches (0.884 meters) in diameter, 7 feet, 3.0 inches (2.210 meters) long and weighs 1,730 pounds (785 kilograms).

The F-117A has a maximum speed of 0.92 Mach (608 miles per hour, 978 kilometers per hour) at 35,000 feet (10,668 meters). The service ceiling is 45,000 feet (13,716 meters) and range is 765 miles (1,231 kilometers), though inflight refueling capability gives it world-wide range.

F-117A drops GBU-28
A Lockheed F-117A Nighthawk drops a 2,000-pound GBU-27 Paveway III laser-guided bomb. (U.S. Air Force)

The Nighthawk has no defensive armament. It can carry two 2,000 pound (907 kilogram) bombs in an internal bomb bay.

Lockheed built 5 YF-117As and 59 production F-117As. The F-117s were retired and placed in climate-controlled storage in 2008.

Scorpion One, 79-10780, is now mounted on a pylon as a “gate guard” at Nellis Air Force Base, Nevada.

Lockheed F-117A Nighthawk in flight. (U.S. Air Force)

© 2018, Bryan R. Swopes

18 June 1937

18 June 1937: Leg 20. Amelia Earhart departed Calcutta, India enroute to Rangoon, Burma. After a fuel stop at Akyab, she and Fred Noonan continued on their way, but monsoon rains forced them to return to Akyab.

“When we reached the airport at dawn nocturnal rains had soaked it. The ground was thoroughly wet, precarious for a take-off. But meteorologists advised that more rain was coming and that likely we could dodge through the intermittent deluges of the day but that if we remained the field might become waterlogged beyond use. That take-off was precarious, perhaps as risky as any we had. The plane clung for what seemed like ages to the heavy sticky soil before the wheels finally lifted, and we cleared with nothing at all to spare the fringe of trees at the airdrome’s edge. For a time we flew through gray skies crowded with clouds that lowered at us as we passed over the many mouths of the Ganges and Brahmapurra rivers…Much of the way from Calcutta to Akyab we flew very low over endless paddies…Akyab is a picturesque place from the air. Two pagodas, covered with gold leaf, stand out…The airport is a port of call for most pilots passing this way. It has two runways and a large hangar. Imperial Airways and Air France stops regularly, and K.L.M., the Dutch line, when necessary to refuel or on account of the weather. . .

“We did not intend to stay at Akyab overnight. Instead we hoped to reach Rangoon at least, and started off from Akyab after checking the weather and fueling. Once in the air the elements grew progressively hostile. The wind, dead ahead, began to whip furiously. Relentless rain pelted us. The monsoon, I find, lets down more liquid per second that I thought could come out of the skies. Everything was obliterated in the deluge, so savage that is beat off patches of paint along the leading edge of my plane’s wings. Only a flying submarine could have prospered. It was wetter even than it had been in that deluge of the mid-South Atlantic. The heavens unloosed an almost unbroken wall of water which would have drowned us had our cockpit not been secure. After trying to get through for a couple of hours we give up, forced to retreat to Akyab.

“Back-tracking, we headed out to sea, flying just off the surface of the water. We were afraid to come low over land on account of the hills. When it’s impossible to see a few hundred yards ahead through the driving moisture the prospect of suddenly encountering hilltops is not a pleasant one. By uncanny powers, Fred Noonan managed to navigate us back to the airport, without being able to see anything but the waves beneath our plane. His comment was, ‘Two hours and six minutes of going nowhere.’ For my part, I was glad that our landing gear was retractable, lest it be scraped on trees or waves. . . .”

—Amelia Earhart

Great Circle route from Calcutta, India, to Akyab, Burma, 290 nautical miles (334 statute miles/537 kilometers). (Great Circle Mapper)

© 2019, Bryan R. Swopes

18 June 1928

Roald Amundsen, 1923 (UPI/Bettmann)

18 June 1928: At 4:05 p.m., Monday afternoon, world-famous Arctic explorer Roald Engelbregt Gravning Amundsen, along with five others, departed Tromsø, Norway, enroute to Spitzbergen, approximately 650 miles away across the Barents Sea.

Airship Italia at Svalbard.

On 25 May, the airship Italia, designed, built and under the command of Umberto Nobile, with a crew of 19, crashed on the arctic ice northeast of the island of Nordlaustlandet in Norway’s Svalbard archipelago. Italia was able to transmit a distress message, and a very large but disorganized search and rescue operation began.

Amundsen made arrangements with the government of France to use a prototype reconnaissance flying boat to look for Nobile and the other survivors.

Built by Société Latham & Cie., the second prototype Latham 47, Nº 02 , was being prepared at the company’s factory at Caudebec-en-Caux, Normandy, to be flown across the Atlantic Ocean to New York City by Capitaine de corvette René Cyprien Guilbaud.

Crew of Latham 47-02, left to right, Emile Valette, Albert Cavelier de Cuverville, René Guilbaud and Gilbert Brazy. (Aerophile)

Guilbaud, with Capitaine de corvette Albert Madeleine Ludovic Alphonse Cavelier de Cuverville; Gilbert George Paul Brazy, mechanic; Émile Valette, radio operator, departed on 16 June. They arrived at Bergen, Norway, the following day, where they picked up Amundsen and pilot Leif Ragnar Dietrichson, who had flown Amundsen on previous expeditions. They continued to Tromsø, north of the Arctic Circle in northern Norway.

“Flybåten Latham 47 registrering 47-02 i Tromsø 18 juni 1928. Kort før Roald Amundsen startet for å lete etter Nobile” (Anders Beer Wilse/Norsk Folkemuseum NF.WB 48692)
Lief Ragnar Dietrichson

At 7:00 p.m. on the 18th, a radio signal was received from the flying boat: “Do not leave listening. . . .”

Nothing more was heard. The rescue flight never arrived at Spitzbergen, and the six men were never seen again.

The Latham 47 was a twin-engine, two-bay biplane flying boat, designed as a naval reconnaissance aircraft for the Marine Nationale (the navy of France). The hydroavion was 16.30 meters (53.48 feet) long, with an upper wingspan of 25.20 meters (82.68 feet) and height of 5.20 meters (17.06 feet). The total wing area was 120.02 square meters (1,291.88 square feet). It had an empty weight of approximately 4,900 kilograms (10,803 pounds) and gross weight of 6,886 kilograms (15,181 pounds).

Latham 47 No. 02 at Tromsø, Norway, 18 june 1928. (Foto: Rognmosamlingen)

The Latham 47 was powered by two water-cooled, 25.485 liter (1,555.166 cubic inch displacement) Société des Avions H. M. et D. Farman 12We “broad arrow” 12-cylinder overhead valve engine with three banks of four cylinders separated by 40°. The engines were mounted in a central nacelle between the upper and lower wings. One was in tractor configuration and the other, a pusher arrangement. The Farman 12We had a compression ratio of 5.3:1,and was rated at 500 chaval vapeur (493 horsepower) at 2,000 r.p.m., and 550 chaval vapeur (543 horsepower) at 2,150 r.p.m. The engines drove four-bladed propellers through a 0.74:1 gear reduction. Each engine weighed 510 kilograms (1,124 pounds), dry.

The Latham 47 had a maximum speed of 170 kilometers per hour (106 miles per hour). Its ceiling was 4,000 meters (13,123 feet), and its range was 900 kilometers (559 miles).

Tromsø 18. juni 1928 (Foto: Vilhjelm Riksheim)

A memorial to the crew of Latham 47 No 02 was designed by architect Léon Rey and sculptor Robert Delandre. It was dedicated at Caudebec-en-Caux, 31 June 1931.

The Latham 47 Memorial at Caudebec-en-Caux, Normandy, France, dedicated 21 June 1931.

In 1969, “The Red Tent,” a Russian/Italian motion picture was made about the search and rescue of the survivors of Italia. The movie starred Sean Connery, Claudia Cardinale, Hardy Krüger and Peter Finch.

A recent photograph of the dramatic Latham 47 memorial at Caudebec-en-Caux, Normandy, France.

© 2018, Bryan R. Swopes