Category Archives: Aviation

15 July 1954

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Boeing test pilot Alvin M. “Tex” Johnston in the cockpit of of the 367–80. (LIFE Magazine)

15 July 1954: At 2:14 p.m., Boeing test pilots Alvin M. “Tex” Johnston and Richard L. “Dix” Loesch lifted off from Renton Field, south of Seattle, Washington, on the first flight of the Boeing 367–80, FAA registration N70700, a prototype military air tanker and commercial airliner.

At 130 miles per hour (209 kilometers per hour), the Boeing Model 367–80 (“Dash Eighty”) lifts off at Renton Municipal Airport on its first flight, 15 July 1954. (Boeing Images)

Tex Johnston wrote about the first flight of the “Dash Eighty” in his autobiography:

     We completed our before-takeoff checklist, Dix worked the tower, and we were cleared for takeoff. I called the theodolite station: “Dash 80, Johnston, stand by, brake release on the count of three.” At full throttle, the four Pratt and Whitney engines at 100-percent power, tail-pipe temperatures and oil pressure on the money, I said, “One, two, three,” and released the brakes. The airplane leaped forward and accelerated rapidly. We obviously would be airborne by midfield. As airspeed passed the calculated V1 speed, I applied back elevator. The nose lifted off. Dix called 130 mph, and we were airborne.

The Boeing Model 367–80 (“Dash Eighty”) takes of from Renton Field on its first flight, 15 July 1954. (Boeing Images)

     Eyeballing the airspeed, I continued to increase the climb angle to avoid exceeding the flap-down placard limit of 225 mph. We were at 1,200 feet as we climbed past end of the runway. Dix commented, “Is this thing going to climb straight up?” Over Lake Washington, I throttled back to climb power, sure that the spectators had never before witnessed takeoff performance and climb attitude like that. . . .

—Tex Johnston: Jet-Age Test Pilot, by A.M. “Tex” Johnston and Charles Barton. Smithsonian Books, Washington, D.C., Chapter 15, Pages 542–543.

The prototype Boeing 367-80, N70700, climbs out at Renton Field, 15 July 1954. (Boeing Images)

For the next 2 hours, 24 minutes they performed high- and low-speed handling tests before landing at Boeing Field, Seattle. When Johnston was asked how the “Dash 80” flew, he replied, “She flew like a bird, only faster.”

Boeing had risked $16,000,000 in a private venture to build the Dash 80 in order to demonstrate its capabilities to potential civilian and military customers, while rivals Douglas and Lockheed were marketing their own un-built jet airliners. Put into production as the U.S. Air Force KC-135 Stratotanker air refueling tanker and C-135 Stratolifter transport, a civil variant was also produced as the Boeing 707, the first successful jet airliner. Though they look very similar, the 707 is structurally different than the KC-135 and has a wider fuselage.

Boeing Aircraft Co. President Bill Allen talks to test pilots Tex Johnston and Dix Loesch after first flight of the Model-367-80 prototype. (Seattle Post-Intelligencer)

The Boeing 707-320B Stratoliner airframe was used for the military E-3A Sentry AWACS command-and-control aircraft, the E-6 Mercury airborne command post, and other versions for reconnaissance, weather, and communications.

820 of the C-135 series and 1,010 Model 707 aircraft were built from 1957–1979.

Boeing Model 367-80 (“Dash Eighty”) in flight. (Joe Parke/Wikipedia)

The prototype Boeing Model 367-80 was operated by a pilot, co-pilot and flight engineer. The airplane’s wing was mounted low on the fuselage and the engine nacelles were mounted on pylons under the wing, as they were on Boeing’s B-47 Stratojet and B-52 Stratofortress. The wings and tail surfaces were swept to 35°. The Dash 80 was 127 feet 10 inches (38.964 meters) long with a wingspan of 129 feet, 8 inches (39.522 meters) and overall height of 38 feet (11.582 meters). Its empty weight was 92,100 pounds (41,775.9 kilograms) and loaded weight was 190,000 pounds (86,182.6 kilograms).

Boeing 367-80 N70700, photographed during its first flight, 15 July 1954. (The Boeing Company)
In tanker configuration, the Boeing 367-80 refuels a Boeing B-52 Stratofortress. The chase plane is a Lockheed T-33A Shooting Star. (U.S. Air Force)
In tanker configuration, the Boeing 367-80 refuels a Boeing B-52 Stratofortress. The chase plane is a Lockheed T-33A Shooting Star. (U.S. Air Force)

N70700 was powered by four Pratt & Whitney Turbo Wasp JT3C engines. This engine is a civil variant of the military J57 series. It is a two-spool, axial-flow turbojet engine with a 16-stage compressor and 2-stage turbine. The JT3C-6 (used in the first production 707s) was rated at 11,200 pounds of thrust (49.82 kilonewtons), and 13,500 pounds (60.05 kilonewtons) with water/methanol injection). The JT3C is 11 feet, 6.6 inches (3.520 meters) long, 3 feet, 2.9 inches (0.988 meters) in diameter, and weighs 4,235 pounds (1,921 kilograms).

These gave the 367-80 a cruise speed of 550 miles per hour (885 kilometers per hour) and a maximum speed of 0.84 Mach (582 miles per hour, 937 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 43,000 feet (13,106 meters). Its range was 3,530 miles (5,681 kilometers).

American Airlines Boeing 707-123 Astrojet, N7501A, Flagship Michigan. (American Airlines)
American Airlines’ Boeing 707-123 Astrojet N7501A, Flagship Michigan. (American Airlines)

Boeing continued to use the 367–80 for testing, finally retiring it 22 January 1970. At that time, its logbook showed 2,346 hours, 46 minutes of flight time (TTAF). It was flown to Davis-Monthan Air Force Base, Tucson, Arizona, and placed in storage. In 1990, Boeing returned it to flyable condition and flew it back it to Renton where a total restoration was completed. Many of those who had worked on the Dash 80, including Tex Johnston, were aboard.

The Dash 80 sat in the Arizona desert for twenty years. (Goleta Air and Space Museum)
The Dash 80 sat in the Arizona desert for twenty years. (Goleta Air and Space Museum)

The pioneering airplane was presented to the Smithsonian Institution and is on display at the National Air and Space Museum, Steven V. Udvar-Hazy Center. The Boeing 367-80 was designated an International Historic Mechanical Engineering Landmark by the American Society of Mechanical Engineers.

820 of the C-135 series and 1,010 Model 707 aircraft were built from 1957–1979.

(The Boeing Model 367-80 is on display at the Steven F. Udvar-Hazy center, Smithsonian Institution National Air and Space Museum. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)
The Boeing Model 367-80 is on display at the Steven F. Udvar-Hazy Center, Chantilly, Virginia. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution) 

© 2020, Bryan R. Swopes

15–22 July 1933

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Wiley Hardeman Post (Underwood and Underwood, Washington)
Wiley Hardeman Post (Underwood and Underwood, Washington)

15 July 1933: At 5:10 a.m., Wiley Hardeman Post took off from Floyd Bennett Field, Long Island, New York, on a solo around-the-world flight. His airplane was a Lockheed Model 5C Vega, NR105W, which he previously flown around the world in 1931 with navigator Harold Gatty.

On this flight, Post flew approximately the same route around the Northern Hemisphere, making 11 stops ¹ over a 15,596 mile (25,099.3 kilometer) flight. He returned to Floyd Bennett Field at 11:50½ p.m., 22 July 1933, after 7 days, 18 hours, 49½ minutes. Post’s total flight time was 115 hours, 36½ minutes. ²

This was the first solo around-the-world flight. Wiley Post was the first pilot to have flown around the world twice.

“With his touchdown at Floyd Bennett on this evening of July, 22, Wiley Post became the first person to circumnavigate the earth twice by aircraft. He was the first person to fly around the world alone, and he had done it with all possible speed. Post’s record remains unique. Fourteen years later in 1947 his record was ostensibly broken; but it was done under such radically different circumstances that the new record was really meaningless.” ³

— Wiley Post, His Winnie Mae, and the World’s First Pressure Suit, by Stanley R. Mohler and Bobby H. Johnson, Smithsonian Annals of Flight Number 8, Smithsonian Institution Press, Washington, D.C., 1971, Chapter 3, at Page 65

Wiley Post with his Lockheed Model 5C Vega, NR105W, at Floyd Bennet Field, Long Island, New York, 15 July 1933. (Rudy Arnold)
Wiley Post with his Lockheed Model 5C Vega, NR105W, at Floyd Bennet Field, Long Island, New York, 15 July 1933. (Rudy Arnold)

The Vega was a single-engine, high-wing monoplane designed by John Knudsen Northrop and Gerard Freebairn Vultee. It was a very state-of-the-art aircraft for its time. It used a streamlined monocoque fuselage made of longitudinal strips of vertical grain spruce pressed into concrete molds and bonded together with cassein glue. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them. They were built of spruce spars and ribs, covered with 3/32-inch (2.4 millimeters) spruce plywood.

The techniques used to build the Vega were very influential in aircraft design. It also began Lockheed’s tradition of naming its airplanes after stars and other astronomical objects.

The Winnie Mae was built by Lockheed Aircraft Company at Burbank, California in 1930 as a Model 5B Vega, serial number 122. It was purchased by an Oklahoma oil driller, Florence C. (“F.C.”) Hall, on 21 June 1930, and named for his daughter, Winnie Mae Hall, The Winnie Mae of Oklahoma. The new airplane was painted white with purple trim. In 1932, NC105W was modified to the Vega 5C standard.

The Lockheed Model 5C Vega is 27 feet, 6 inches (8.382 meters) long with a wingspan of 41 feet, 0 inches (12.497 meters) and overall height of 8 feet, 2 inches (2.489 meters). Its empty weight is 2,595 pounds (1,177 kilograms) and gross weight is 4,500 pounds (2,041 kilograms).

Winnie Mae was powered by an air-cooled, supercharged 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp C, serial number 3088, a single-row, nine cylinder, direct-drive radial engine. The Wasp C was rated at 420 horsepower at 2,000 r.p.m. at Sea Level. It was 3 feet, 6.63 inches (1.083 meters) long with a diameter of 4 feet, 3.44 inches (1.307 meters) and weighed 745 pounds (338 kilograms).

The standard Model 5C had a cruise speed of 165 miles per hour (266 kilometers per hour) and maximum speed of 185 miles per hour (298 kilometers per hour). The service ceiling was 15,000 feet (4,570 meters) and range in standard configuration was 725 miles (1,167 kilometers).

Wiley Post flew the Winnie Mae for F.C. Hall, and flew it around the world in 1931 with Harold Gatty as navigator. Post used it to set several speed records and to compete in the National Air Races. He purchased the airplane from Hall, 8 July 1931.

Winnie Mae was involved in an accident at Chickasha, Oklahoma, 21 April 1933. Flown by another pilot, the engine stopped on takeoff due to fuel starvation. It was found that gasoline had been stolen from the tanks by being siphoned. The damaged Vega was sent to Braniff Airways at Oklahoma City, Oklahoma, for repair and an extensive overhaul. One fuselage half was replaced, and the fuselage covered in balloon cloth. The cockpit was rebuilt, all new control cables installed, and the wing repaired and reinforced. The tail surfaces were recovered and the landing gear was sent to Lockheed to be rebuilt. The Wasp SC1 was completely overhauled modified with new cylinders which increased the compression ratio from 5.25:1 to 6.0:1. The carburetor was overhauled by Bendix-Stromberg, and new magnetos installed. Using 87-octane aviation gasoline, it could produce 500 horsepower at 2,200 r.p.m. (5-minute limit). The airplane’s original two-bladed Standard fixed-pitch steel propeller was replaced by a Smith 450-SI controllable-pitch propeller with Pittsburgh Screw and Bolt hollow steel blades.

Among other modifications, Post had the wing’s angle of incidence decreased 10° which reduced aerodynamic drag and increased the Vega’s speed by 10 miles per hour (16 kilometers per hour). The fixed tail skid was shortened to allow the airplane to reach a higher angle of attack for takeoff and landing. For the 1933 around-the-world flight, six fuel tanks were installed in the fuselage and four in the wings, giving the Vega a total fuel capacity of 645 gallons (2,442 liters). It was also equipped with a Sperry gyroscopic autopilot.

These modifications required the Vega to be licensed in a restricted category, and it was re-registered NR105W.

After Wiley Post was killed in an airplane crash near Barrow, Alaska, 15 August 1935, his widow, Mae Laine Post, sold NR105W to the Smithsonian Institution. It is on display in the Time and Navigation Exhibition at the National Air and Space Museum, Washington, D.C.

Wiley Post's Lockheed 5C Vega, NR105W, "Winnie Mae of Oklahoma", at the National Air and Space Museum.(Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)
Wiley Post’s Lockheed 5C Vega, NR105W, The Winnie Mae of Oklahoma, at the National Air and Space Museum. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)

¹ Berlin, Germany; Königsberg, Germany (now, Kalingrad, Russia); Moscow, Russian Soviet Federative Socialist Republic; Novosibirsk, Siberia, U.S.S.R, ; Irkutsk, Siberia, U.S.S.R.; Rukhlovo, Siberia, U.S.S.R. (Skorvorodino); Khabarovsk, Siberia, U.S.S.R.; Flat, Territory of Alaska; Fairbanks, Territory of Alaska; Edmonton, Alberta, Dominion of Canada; New York City, New York, United States of America.

² The international organization for flight records, the Fédération Aéronautique Internationale, requires that a circumnavigation cross all meridians in one direction and be at least the length of the Tropic of Cancer, 22,858.729 miles (36,787.559 kilometers). Post’s flight was short of the required distance, so no official record was set.

³ Floyd Odom, Douglas A-26 Invader NX67834, 7–10 August 1947: Flight, “Just what he as proved is not clear. . . The late Wiley Post took come 187 hours to do the circuit. . . but that was fourteen years ago, in a Lockheed Vega with one 450 horsepower engine. Post had far less aid from navigational facilities, and almost only one piece of equipment common to the Winnie Mae and the Reynolds Bombshell is the automatic pilot, which in both cases enabled the human pilot to take occasional short snatches of sleep. Captain Odom’s engines had to run for 73 hours only, while Post’s kept going for 87. Pilot strain must have been approximately proportional to the length of time, so if human endurance is the criterion, Post’s was the greater achievement.” —FLIGHT, Vol. 52, August 14, 1947, page 154

© 2018, Bryan R. Swopes

15 July 1916

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The first Boeing Model 1, the very first Boeing airplane, at Duwamish River site, near Seattle, Washington, 1916. (Boeing)
The first Boeing Model 1, the very first Boeing airplane, at Duwamish River site, near Seattle, Washington, 1916. (Boeing)

15 July 1916: Timber merchant William Edward Boeing (1881–1956) incorporated the Pacific Aero Products Company, to manufacture airplanes. The factory was a former boat house on the Duwamish River near Seattle Washington. The first aircraft produced was the Boeing Model 1, a single-engine, float-equipped biplane. Less than a year later, the company name was changed to Boeing Airplane Company.

The original Boeing factory has been relocated to the Museum of Flight. (Boeing)
The original Boeing factory has been relocated to the Museum of Flight. (Boeing)

For over 100 years, Boeing has produced commercial and military aircraft. Today, The Boeing Company is the world’s leading aerospace corporation. It employs 159,469 people. Its 2017 revenues were $93,390,000,000. Boeing received orders  for 912 commercial aircraft in 2017, valued at $134,800,000,000. The company’s backlog for commercial airplanes is 5,864. On the military side, the U.S. Army has ordered 268 AH-64 Apache attack helicopters. The company has contracts for 17 P-8A Poseidon maritime patrol aircraft, and is expected to deliver 18 KC-46 tankers in 2018. It has foreign contracts for 36 F-15 Eagles and 28 F-18 Super Hornets.

William Edward Boeing (1881–1956)

Boeing recently unveiled its new 787–10 Dreamliner:

© 2018, Bryan R. Swopes

14 July 1959

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Major General Vladimir Sergeyevich Ilyushin, Hero of the Soviet Union

14 July 1959: At Podmoskovnoe, USSR, famed Soviet test pilot Vladimir Sergeyevich Ilyushin flew the Sukhoi T-43-1, a prototype of the Su-9 interceptor, to a Fédération Aéronautique Internationale (FAI) World Record for Altitude of 28,852 meters (94,659 feet).¹

Vladimir Sergeyevich Ilyushin was the son of Sergey Ilyushin, the Soviet aircraft designer. He made the first flights of many Sukhoi fighters. A Hero of the Soviet Union, he retired with the rank of major general.

Sukhoi T-43-1
Vladimir Sergeyevich Ilyushin, wearing flight suit and helmet, with a Sukhoi Su-9 in the background.
Vladimir Sergeyevich Ilyushin, wearing flight suit and helmet, with a Sukhoi Su-9 in the background.

The Sukhoi T-43-1 was the prototype for the Su-9 all-weather interceptor, a single-place, single-engine Mach 2+ fighter. It was built from the first pre-production Sukhoi T-3, with a new nose section and enlarged rear fuselage to accommodate a larger engine.

The production Su-9 is similar in appearance to the Mikoyan Gurevich MiG-21, but is much larger and heavier. It is 17.37 meters (56.99 feet) long with a wingspan of 8.43 meters (27.66 feet) and overall height of 4.88 meters (16.01 feet). The interceptor’s empty weight is 8,620 kilograms (19,004 pounds), and the maximum takeoff weight is 13,500 kilograms (29,762 pounds).

Sukhoi T-43-12 prototype.
Sukhoi T-43-12 prototype.

Both the T-43-1 prototype and the production Su-9 are powered by a Lyulka AL-7 nine-stage axial flow turbojet engine which produces 22,050 pounds of thrust with afterburner.

The Su-9 has a maximum speed of Mach 2.0 (2,135 kilometers per hour, 1,327 miles per hour). The service ceiling is 16,760 meters (54,987 feet) and range is 1,125 kilometers (699 miles).

The T-43-1 later set FAI records for sustained altitude and speed over a measured course.

Sukhoi Su-9
Sukhoi Su-9, right front quarter
Sukhoi Su-9
Sukhoi Su-9, right profile

¹ FAI Record File Number 10351

© 2017, Bryan R. Swopes

10–14 July 1938

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Howard Robard Hughes, Jr. (New York Public Library)
Howard Robard Hughes, Jr., ca. 1937 (New York Public Library)

10–14 July 1938: Howard Robard Hughes, Jr., along with a crew of four, departed Floyd Bennett Field, Brooklyn, New York, on a flight to circle the Northern Hemisphere. His airplane was a Lockheed Super Electra Special, Model 14-N2, registered NX18973. Aboard were Harry P. McLean Connor, co-pilot and navigator; 1st Lieutenant Thomas Lawson Thurlow, United States Army Air Corps, navigator; Richard R. Stoddart, a field engineer for the National Broadcasting Company (NBC), radio operator; Edward Lund, flight engineer. Lieutenant Thurlow was the Air Corps’ expert on aerial navigation. Stoddart was an expert in radio engineering. Thurlow, Stoddart and Lund were also rated pilots.

This photograph by aviation photographer Rudy Arnold shows the “nose art” of the Lockheed Model 14-N2 Super Electra, “New York World’s Fair 1939.” Lieutenant Thurlow is “sighting in” the airplane’s navigation instruments prior to the around-the-world flight.(Rudy Arnold Collection, National Air and Space Museum XRA-4763)

Before they took off from Floyd Bennett Field, the Lockheed was christened New York World’s Fair 1939, in keeping with an agreement that Hughes had made with Grover Whalen and the fair’s organizers.

Howard Hughes' Lockheed Model 14-N@ Super Electra, starting its right engine at Floyd Bennett Field, approximately 7:00 p.m., 10 July 1938. (Unattributed)
Howard Hughes’ Lockheed Model 14-N2 Super Electra starting its right engine at Floyd Bennett Field, 10 July 1938. (Unattributed)

Howard Hughes and his crew departed Floyd Bennett Field at 7:19:10 p.m. on 10 July. The route of the flight was from Floyd Bennett Field to Le Bourget Aerodrome, Paris, France, a distance of 3,641 miles (5,860 kilometers), flown in an elapsed time of 16 hours, 38 minutes; Moscow, Russia, USSR, 1,640 miles (2,639 kilometers), 7:51; Omsk, Siberia, 1,400 miles (2,253 kilometers), 7:27; Yakutsk, Yakut ASSR, 2,158 miles (3,473 kilometers), 10:31; Fairbanks, Alaska, 2,457 miles (3,954 kilometers), 12:17; Minneapolis, Minnesota, 2,441 miles (3,928 kilometers), 12:02; and back to Floyd Bennett Field, 1,054 miles (1,696 kilometers) 4:26.

They arrived at Floyd Bennett Field at 2:34 p.m., 14 July. The distance flown was approximately 14,800 miles (23,818 kilometers) (sources differ). The total duration was 91 hours, 14 minutes, 10 seconds. The actual flight time was 71 hours, 11 minutes, 10 seconds. Average speed for the flight was 206.1 miles per hour (331.7 kilometers per hour).

The flight crew of Horad Hughes around-the-world flight, left to right, Hughes,
The flight crew of Howard Hughes’ around-the-world flight, left to right: Howard Robard Hughes, Jr., wearing a fedora and a white shirt; 1st Lieutenant Thomas L. Thurlow, U.S. Army Air Corps; Harry P. McLean Connor; Richard R. Stoddart; and Edward Lund. Standing at the far left of the photograph is Grover Whalen, president of the New York World’s Fair 1939 Committee, who christened the airplane. (Tamara Thurlow Field via Air & Space Smithsonian)

The international organization for flight records, the Fédération Aéronautique Internationale, requires that a circumnavigation cross all meridians in one direction and be at least the length of the Tropic of Cancer, 22,858.729 miles (36,787.559 kilometers). Howard Hughes’ “around the world flight” circled the Northern Hemisphere and was at least 8,058 miles (12,968 kilometers) short of the required distance, so no official record was set. (The same is true of Wiley H. Post’s two earlier “around the world” flights which used a similar route.)

The Robert J. Collier Trophy. (Smithsonian Institution, National Air and Space Museum)
The Robert J. Collier Trophy. (NASM)

The National Aeronautic Association awarded the Aero Club Trophy (after 1944, known as the Robert J. Collier Trophy, or simply, The Collier Trophy) to Howard Hughes and his associates, “For their epoch making round the world flight in 91 hours and 14 minutes.” The Collier is an annual award, “. . . for the greatest achievement in aeronautics or astronautics in America, with respect to improving the performance, efficiency, and safety of air or space vehicles, the value of which has been thoroughly demonstrated by actual use during the preceding year.”

The Lockheed Super Electra 14-N2, serial number 1419, was offered to Hughes by the Lockheed Aircraft Company, Burbank, California, at no cost.

Company officials believed that publicity generated by an around-the-world flight would justify the expense. The airplane underwent modification for two months at the Burbank factory. The Curtiss-Wright Corporation provided new engines. Fuel capacity was increased to 1,844 gallons (6,980.3 liters). Three radio systems were installed.

The Lockheed Model 14 Super Electra was an all-metal, twin-engine, low-wing monoplane with retractable landing gear, designed as a medium-sized airliner. It was flown by two pilots and could carry up to 12 passengers. Based on aerodynamic studies carried out by Clarence L. “Kelly” Johnson on the earlier Model 10 Electra, the airplane was configured with an “H-tail”, with vertical fins and rudders placed at the ends of the horizontal stabilizer. This was a characteristic design feature for Lockheed aircraft through the 1950s.

Cutaway drawing of Howard Hughes' Lockheed Model 14-N2 Super Electra, NX18973. (New York Public Library)
Cutaway drawing of Howard Hughes’ Lockheed Model 14-N2 Super Electra, NX18973. (New York Public Library)

The Model 14 was 44 feet, 4 inches (13.513 meters) long with a wingspan of 65 feet, 6 inches (19.964 meters) and overall height of 11 feet, 5 inches (3.480 meters). Hughes’ Model 14-N2 Special differed, but a Model 14-WF-62 airliner version had an empty weight of 10,750 pounds (4,876 kilograms), gross weight of 15,650 pounds (7,098 kilograms) and maximum takeoff weight of 17,500 pounds (7,938 kilograms). The airliner had maximum speed of 250 miles per hour (402 kilometers per hour) and a service ceiling of 24,500 feet (7,468 meters).

NX18973 was powered by two air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.875 liter) Wright Aeronautical Division Cyclone GR-1820-G102 nine-cylinder radial engines with a normal power rating of 900 horsepower at 2,200 r.p.m., and 1,100 horsepower at 2,200 r.p.m for take-off.  The engines had a compression ratio of 6.7:1 and required 91-octane gasoline. They turned three-bladed Hamilton Standard constant-speed propellers through a 0.6875:1 gear reduction. The GR-1820-102 was 4 feet, 0.12 inches (1.222 meters) long, 4 feet, 7.10 inches (1.400 meters) in diameter, and weighed 1,275 pounds (578 kilograms).

Lockheed Moedl 14-N2 Super Electra NX18973, New York World's Fair 1939, arrives at Floyd Bennett Field, Long Island New York, 14 July 1938. (Associated Press)
Lockheed Model 14-N2 Super Electra NX18973, “New York World’s Fair 1939,” arrives at Floyd Bennett Field, Long Island, New York, 2:34 p.m., 14 July 1938. (Associated Press)

Representative performance figures are maximum speed of 250 miles per hour (402 kilometers per hour) and a service ceiling of 24,500 feet (7,468 meters). NX19783 had an estimated maximum range of 4,500 miles (7,242 kilometers).

Following Hughes’ flight, NX18973 was returned to Lockheed. The manufacturer then sold the Super Electra to the Royal Canadian Air Force. It was assigned fuselage identification AX688. (A militarized version of the Super Electra was produced as the Hudson light bomber.)

On 10 November 1940, the Super Electra took off from Nairobi, Kenya, on a transcontinental ferry flight to from South Africa to Egypt. There were high winds and it was raining. After climbing to 500 feet (152 meters) AGL, the Lockheed banked to the left. It stalled, entered a spin and crashed. The wreck caught fire. All persons on board were killed.

Lockheed Model 14-N2 Super Electra Special, c/1419, NX18973. (San Diego Air and Space Museum Archive)
Lockheed Model 14-N2 Super Electra Special, c/n 1419, NC18973. (San Diego Air and Space Museum Archive)
Lockheed Model 14-N2 Super Electra NC18973 at Alameda, California, 1940. (Bill Larkins/Wikipedia)

© 2018, Bryan R. Swopes