Tag Archives: World Record for Speed Over a Recognized Course

16–17 August 1989

Qantas' Boeing 747-438 Longreach VH-OJA, Spirit of Australia. (Aero Icarus)
Qantas’ Boeing 747-438 Longreach VH-OJA, City of Canberra. (Aero Icarus)

16–17 August 1989: On its delivery flight, Qantas’ first Boeing 747-438 Longreach airliner, VH-OJA, City of Canberra, was flown by Captain David Massey-Green from London Heathrow Airport, England (IATA: LHR, ICAO: EGLL) to Sydney Kingsford Smith Airport, Australia (IATA: SYD, ICAO: YSSY), non-stop. Three other senior Qantas captains, Ray Heiniger, George Lindeman and Rob Greenop completed the flight deck crew. Boeing Training Captain Chet Chester was also aboard.

The distance flown by the new 747 was 17,039.00 kilometers (10,587.54 miles) at an average speed of 845.58 kilometers per hour (525.42 miles per hour). The flight’s duration was 20 hours, 9 minutes, 5 seconds. This set a new Fédération Aéronautique Internationale (FAI) World Record for Distance and World Record for Speed Over a Recognized Course.

The crew of Qantas Flight 741. Front row, left to right: FSD David Cohen, FSD Mal Callender. Back row, left to right: Captain Ray Heiniger, Captain David Massey-Greene, Captain George Lindeman, Captain Rob Greenop.
The crew of Qantas Flight 7741. Front row, left to right: FSD David Cohen, FSD Mal Callender. Back row, left to right: Captain Ray Heiniger, Captain David Massey-Greene, Captain George Lindeman, Captain Rob Greenop. (Unattributed)

FAI Record File Num #2201 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1t (Landplanes: take off weight 300 000 kg to 400 000 kg)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Distance
Performance: 17 039.00 km
Date: 1989-08-17
Course/Location: London (United Kingdom) – Sydney, NSW (Australia)
Claimant David Massy-greene (AUS)
Aeroplane: Boeing 747-400 (VH-OJA)
Engines: 4 Rolls Royce RB 211

FAI Record File Num #2202 [Direct Link]
Status: ratified – current record
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1t (Landplanes: take off weight 300 000 kg to 400 000 kg)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a recognised course
Performance: 845.58 km/h
Date: 1989-08-17
Course/Location: London (United Kingdom) – Sydney, NSW (Australia)
Claimant David Massy-greene (AUS)
Aeroplane: Boeing 747-400 (VH-OJA)
Engines: 4 Rolls Royce RB 211

Boeing 747-438 Longreach VH-OJA, City of Canberra at Sydney, Australia, August 1989. The motto, WE FLY FURTHER has been painted on the fuselage in recognition of the new airliner's distance record. (John McHarg)
Boeing 747-438 Longreach VH-OJA, City of Canberra, at Sydney, Australia, August 1989. The motto, WE GO FURTHER has been painted on the fuselage in recognition of the new airliner’s distance record. (John McHarg)

VH-OJA was the first of four Boeing 747-400 airliners ordered by Qantas more than two years earlier. The company named these “Longreach” both to emphasize their very long range capabilities, but also as a commemoration of the first scheduled passenger flight of the Queensland and Northern Territories Aerial Services Ltd. at Longreach, Queensland, 2 November 1922. Qantas named the new airliner City of Canberra. The new 747, the twelfth -400 built, with U.S. registration N6064P, it made its first flight at Seattle with Boeing’s test pilots on 3 July 1989. It was turned over to Qantas on 9 August.

Planning for the record setting flight began almost as soon as the airplane had been ordered. Although the airplane was complete and ready to enter passenger service on arrival at Sydney, certain special arrangements were made. Shell Germany refined 60,000 gallons (227,000 liters) of a special high-density jet fuel and delivered it to Heathrow. Rolls-Royce, manufacturer of the RB211-524G high-bypass turbofan engines, had agreed to specially select four engines to be installed on VH-OJA at the Boeing plant at Everett, Washington.

On the morning of the flight, City of Canberra was towed to the Hold Short position for Runway 28 Right (28R) so as not to use any of the precious fuel while taxiing from the terminal. Once there, its fuel tanks were filled to overflow. The airport fire department stood by as the excess fuel ran out of the tank vents. In the passenger cabin were two Flight Service Directors, FSD David Cohen and FSD Mal Callender, and eighteen passengers including senior executives from Qantas, Boeing, Shell as well as representatives of the Australian news media. The flight crew planned the engine start to allow for the mandatory three-minute warm-up and at approximately 0840 local, called the Tower, using the call sign Qantas 7441, and said that they were ready for takeoff.

After climbing to altitude they began the cruise portion of the flight at Flight Level 330 (33,000 feet or 10,058 meters). As fuel was burned off the airliner gradually climbed higher for more efficiency, eventually reaching a maximum altitude of 45,100 feet (13,746.5 meters) by the time they had reached the west coast of Australia.

QF7441 touched down at Sydney Airport at 2:19 p.m, local time (0419 UTC) in—well, let’s just call it rain and leave it at that. (There is more to the story. . . .)

City of Canberra, Qantas' first Boeing 747-400-series airliner, touches down at Sydney Airport, 2:19 p.m., local, 17 August 1989. (Qantas Heritage Collection)
City of Canberra, Qantas’ first Boeing 747-400-series airliner, registered VH-OJA, touches down at Sydney Airport, 2:19 p.m., local, 17 August 1989. (Qantas Heritage Collection) 

For a more detailed description of this flight and its planning, see John McHarg’s article, “The Delivery Flight of Qantas Boeing 747-438 VH-OJA” at:

http://www.aussieairliners.org/b-747/vh-oja/vhoja%20article/vhojastory.html

City of Canberra, VH-OJA, remains in Qantas service twenty-four years later. Its distance record stood until 10 November 1995 when another Boeing airliner, a 777-200LR with Captain Suzanna Darcy-Henneman in command, set a new distance record.

Qantas' Boeing 747-438 Longreach VH-OJA, City of Canberra, on takeoff, 2011. (Aero icarus)
Qantas’ Boeing 747-438 Longreach VH-OJA, City of Canberra, on takeoff from Sydney, 1999. (Aero Icarus)

The Boeing 747-400 airliner can carry between 416 and 660 passengers, depending on configuration. It is 231 feet, 10 inches (70.6 meters) long with a wingspan of 211 feet, 5 inches (64.4 meters) and overall height of 63 feet, 8 inches (19.4 meters). Empty weight is 394,100 pounds (178,800 kilograms). Maximum takeoff weight (MTOW) is 875,000 pounds (396,890 kilograms). While the prototype was powered by four Pratt and Whitney PW4056 turbofan engines, production airplanes could be ordered with PW4062, General Electric CF6 or Rolls-Royce RB211 engines, providing thrust ranging from 59,500 to 63,300 pounds. The –400 has a cruise speed of 0.85 Mach (567 miles per hour, 912 kilometers per hour) and maximum speed of 0.92 Mach (614 miles per hour, 988 kilometers hour). Maximum range at maximum payload weight is 7,260 nautical miles (13,450 kilometers).

A Qantas Boeing 747-438 Longreach, VH-OJU, Lord Howe Island, leaves contrails across the sky. (Unattributed)
A Qantas Boeing 747-438 Longreach, VH-OJU, Lord Howe Island, leaves contrails across the sky. (Unattributed)

© 2015, Bryan R. Swopes

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11 June 1971–4 August 1971

Sheila Scott on the wing of her Piper PA-23-250 Aztec D, Mythre, G-AYTO, 1971. (NASA)
Sheila Scott on the wing of her Piper PA-23-250 Aztec D, Mythre, G-AYTO, 1971. (NASA)

11 June 1971: Sheila Scott OBE (née Sheila Christine Hopkins) departed Nairobi, Kenya, on her third solo around-the-world flight. On this flight she used a new airplane, a twin-engine Piper Aztec which she named Mythre. It carried United Kingdom registration G-AYTO. She used a NASA satellite data communication system to constantly relay her position to a NIMBUS satellite, and from there to a ground station at Fairbanks, Alaska.

Sheila Scott's Piper PA-23-250 Aztec D, G-ATYO. Mythre.
Sheila Scott’s Piper PA-23-250 Aztec D, G-ATYO, Mythre, at Kidlington Airport, Oxfordshire, England, 1971. (Tim R. Badham)

On this flight, Sheila Scott planned to not only fly around the world, but to fly from the Equator, over the North Pole, and back to the Equator again. She flew her Aztec from London, England to Nairobi, Kenya, where she began to Equator–North Pole–Equator portion of the flight.

Scott took off from Nairobi on 11 June 1971 and headed northward to Khartoum, Sudan; Bengazi, Libya; Malta; arriving back at London on 21 June. From there she continued to Bodø, Norway; Andøya, Norway; Station Nord, Greenland; across the North Pole on 28 June; then southward to Barrow, Alaska; arriving at Anchorage, Alaska on 3 July; San Francisco, California to Honolulu, Hawaii on 11 July. She recrossed the Equator heading south to Canton Island. On 23 July, Mythre arrived at Nadi, Viti Levu, Fiji, and then flew on to Noumea, New Caledonia. After a stop at Townsville, Scott arrived at Darwin, Australia, 1 August. From there she continued to Singapore; Madras, India; Karachi, Pakistan; Bahrain; Athens, Greece; and finally completed her journey at London on 4 August. Her flight took 55 days.

Sheila Scott set seven Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Recognized Course: Andøya, Norway, to Station Nord, Greenland, 213.61 kilometers per hour (132.73 miles per hour), (FAI Record File Numbers 4622, 4623); Nord to Barrow, Alaska, 183.73 km/h (114.16 mph), (14203); San Francisco, California, to Honolulu, Hawaii, 236.56 km/h (146.99 mph) (4626, 4627); Darwin, Northern Territory, Australia, to London, England, 160.19 km/h (99.54mph) (4624, 4625). Record 4622 is the current record.

The Piper PA-23-250 Aztec D was a six-place twin-engine light airplane based on the earlier PA-23-235 Apache, with a larger cabin and more powerful engines. It was of all-metal construction and had retractable tricycle landing gear. The Aztec D is 30.2 feet (9.205 meters) long with a wingspan of 37 feet (11.278 meters) and overall height of 10.3 feet (3.139 meters). It has an empty weight of 3,042 pounds (1,380 kilograms) and a gross weight of 5,200 pounds (2,359 kilograms).

The Aztec D is powered by two air-cooled, fuel-injected, 541.511-cubic-inch-displacement (8.874 liter) Lycoming IO-540-C4B5 horizontally-opposed 6-cylinder engines. The -C4B5 has a compression ratio of 8.5:1 and is rated at 250 horsepower at 2,575 r.p.m., for takeoff and maximum continuous power. It weighs 374 pounds (170 kilograms). The engines turn two-bladed Hartzell constant-speed propellers through direct drive.

The PA-23-250 has a cruise speed of 206 miles per hour (332 kilometers per hour) at 7,500 feet (2,286 meters) and maximum speed of 216 miles per hour (348 kilometers per hour). The service ceiling was 19,800 feet (6,035 meters). With standard fuel capacity of 144 gallons (545 liters) the airplane’s range was 1,055 miles (1,698 kilometers). Mythre carried an auxiliary fuel tank in the passenger cabin.

After the around-the-world flight, Scott returned Mythre to the Piper Aircraft Company at Lock Haven, Pennsylvania, for overhaul. Following Hurricane Agnes in June 1972, the Piper factory was flooded to a depth of 16 feet (4.9 meters) and Scott’s airplane, along with many others and much of the tooling for aircraft manufacture, was destroyed.

Sheila Scott's Piper Aztec, Mythre, over the North Pole, by Paul Couper, 2008
Sheila Scott over the Top—Piper Aztec, by Paul Couper, Guild of Aviation Artists, 2008. 62 × 52 centimeters, oil/acrylic.

This painting is available from the Guild of Aviation Artists at:

http://www.gava.org.uk/index.php?option=com_phocagallery&searchterm=Paul%20Couper&view=category&id=12&Itemid=534&picsearch=simple

© 2017, Bryan R. Swopes

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31 May–1 June 1967

Left to Right: Major Herbert Zehnder, USAF; Igor Sikorsky; Major Donald B. Murras, USAF, at Le Bourget, 1 June 1967.
Major Herbert R. Zehnder, USAF; Igor Sikorsky; Major Donald B. Murras, USAF, at le Bourget, 1 June 1967. (Sikorsky Historical Archives)

At 0105 hours, 31 May 1967, two Sikorsky HH-3E Jolly Green Giant helicopters, 66-13280 and 66-13281, from the 48th Aerospace Rescue and Recovery Squadron, United States Air Force, took off from Floyd Bennett Field, New York and flew non-stop across the Atlantic Ocean to the Paris Air Show. They arrived at Le Bourget at 1351 hours, 1 June.

The flight covered 4,271 miles (6873.5 kilometers) and took 30 hours, 46 minutes. Nine in-flight refuelings were required from Lockheed HC-130P Combat King tankers. The aircraft commanders were Major Herbert Zehnder and Major Donald B. Murras.

Major Zehnder, in H-211, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course for helicopters, with an average speed of 189.95 kilometers per hour (118.03 miles per hour). This record still stands.¹

One of two 48th ARRS Sikorsky HH-3E Jolly Green Giant lands at Le Bourget after non-stop trans Atlantic flight, 1 June 1967. (Louisiana State Museum)
“H-211,” one of two 48th ARRS Sikorsky HH-3E Jolly Green Giant helicopters, lands at Le Bourget after a non-stop trans Atlantic flight, 1 June 1967. (Louisiana State Museum)
Lieutenant Colonel Travis Wofford, United States Air Force.
Lieutenant Colonel Travis Wofford, United States Air Force.

Both Jolly Green Giants, serial numbers 66-13280 and 66-13281, were later assigned to the 37th Air Rescue and Recovery Squadron. Both were lost in combat during the Vietnam War.

66-13280, “Jolly Green 27” crashed at Kontum, Republic of South Vietnam, 15 April 1970. The pilot, Captain Travis H. Scott, Jr., was killed, and flight engineer Gerald E. Hartzel later died of wounds. The co-pilot, Major Travis Wofford, was awarded the Air Force Cross and the Cheney Medal for his rescue of the crewmembers from the burning helicopter. Captain Scott was posthumously awarded the Air Force Cross.

66-13281, “Jolly Green 28,” was shot down over Laos, 24 October 1969. The crew was rescued and the helicopter destroyed to prevent capture. The pararescueman, Technical Sergeant Donald G. Smith, was awarded the  Air Force Cross for the rescue of the pilot of “Misty 11.” He was also awarded the Airman’s Medal.

Master Sergeant Donald G. Smith, United States Air Force.
Master Sergeant Donald G. Smith, United States Air Force.

Major Herbert Zehnder flew another Sikorsky HH-3E, 65-12785, to intentionally crash land inside the Sơn Tây Prison Camp, 23 miles (37 kilometers) west of Hanoi, North Vietnam. He was awarded the Silver Star.

The SH-3A Sea King (Sikorsky S-61) first flew 11 March 1959, designed as an anti-submarine helicopter for the U.S. Navy. The prototype was designated XHSS-2 Sea King. In 1962, the HSS-2 was redesignated SH-3A Sea King. Many early production aircraft were upgraded through SH-3D, SH-3G, etc. In addition to the original ASW role, the Sea Kings have been widely used for Combat Search and Rescue operations. Marine One, the call sign for the helicopters assigned to the President of the United States, are VH-3D Sea Kings.

A Sikorsky HH-3E Jolly Green Giant (66-13290) of the 37th Air Rescue and Recovery Squadron, hovering in ground effect at Da Nang, Republic of South Vietnam, 1968. (U.S. Air Force)

The Sikorsky HH-3E (Sikorsky S-61R) earned the nickname Jolly Green Giant during the Vietnam War. It is a dedicated Combat Search and Rescue (CSAR) helicopter flown by the U.S. Air Force, based on the CH-3C transport helicopter. The aircraft is flown by two pilots and the crew includes a flight mechanic and gunner. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. It has retractable tricycle landing gear and a rear cargo ramp. The rear landing gear retracts into a stub wing on the aft fuselage. The helicopter has an extendable inflight refueling boom.

The HH-3E is 72 feet, 7 inches (22.123 meters) long and 18 feet, 10 inches (5.740 meters) high with all rotors turning. The main rotor has five blades and a diameter of 62 feet (18.898 meters). Each blade has a chord of 1 foot, 6.25 inches (0.464 meters). The main rotor turns at 203 r.p.m., counter-clockwise, as seen from above. (The advancing blade is on the right.) The tail rotor also has five blades and has a diameter of 10 feet, 4 inches (3.150 meters). The blades have a chord of 7–11/32 inches (0.187 meters). The tail rotor turns clockwise as seen from the helicopter’s left. (The advancing blade is below the axis of rotation.) The tail rotor turns 1,244 r.p.m.

A Sikorsky HH-3E Jolly Green Giant refuels in flight from a Lockheed HC-130 Combat King. (U.S. Air Force)
A Sikorsky HH-3E Jolly Green Giant refuels in flight from a Lockheed HC-130 Combat King. (U.S. Air Force)

The HH-3E has an empty weight of 13,341 pounds (6,051 kilograms). The maximum gross weight is 22,050 pounds (10,002 kilograms).

The Jolly Green Giant is powered by two General Electric T58-GE-5 turboshaft engines, which have a Maximum Continuous Power rating of 1,400 shaft horsepower, each, and Military Power rating of 1,500 shaft horsepower. The main transmission is rated for 2,500 horsepower, maximum.

The HH-3E has a cruise speed of 154 miles per hour (248 kilometers per hour) at Sea Level, and a maximum speed of 177 miles per hour (285 kilometers per hour), also at Sea Level. The service ceiling is 14,000 feet (4,267 meters). The HH-3E had a maximum range of 779 miles (1,254 kilometers) with external fuel tanks.

The Jolly Green Giant can be armed with two M60 7.62 mm machine guns.

Sikorsky built 14 HH-3Es. Many CH-3Cs and CH-3Es were upgraded to the HH-3E configuration. Sikorsky built a total of 173 of the S-61R series.

Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)
Sikorsky HH-3E Jolly Green Giant 67-14709 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)

¹ FAI Record File Number 2092

© 2017, Bryan R. Swopes

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26 May 1961

The flight crew of the Convair B-58A-10-CF Hustler 59-2451, "The Firefly," planning the Washington, D.C.-to-Paris flight, 26 May 1961. Left to right, Captain William L. Polhemus, Captain Raymond R. Wagener and Major William R. Payne. (Jet Pilot Overseas)
The flight crew of the Convair B-58A-10-CF Hustler 59-2451, “The Firefly,” planning the Washington, D.C.-to-Paris flight, 26 May 1961. Left to right, Captain William L. Polhemus, Captain Raymond R. Wagener and Major William R. Payne. (Jet Pilot Overseas)

26 May 1961: The Firefly, the Blériot Trophy-winning Convair B-58A-10-CF Hustler, serial number 59-2451, assigned to the 43rd Bombardment Wing, Carswell Air Force Base, Fort Worth, Texas, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course by flying from Washington, D.C. to Paris in 3 hours, 39 minutes, 49 seconds, for an average speed of 1,687.69 kilometers per hour (1,048.68 miles per hour).¹

During the same flight, the B-58 flew the New York to Paris segment in 3 hours, 14 minutes, 44.53 seconds, at an average speed of 1,753.16 kilometers per hour (1,089.36 miles per hour).

The aircrew, Major William R. Payne, Aircraft Commander, Captain William L. Polhemus, Navigator, and Captain Raymond R. Wagener, Defensive Systems Officer, won the Harmon and Mackay Trophies for this flight.

Convair B-58A-10-CF Hustler 59-2451, The Firefly, lands at le Bourget, Paris, after the record-setting transatlantic flight, 26 May 1961. (University of North Texas Libraries)
Convair B-58A-10-CF Hustler 59-2451, The Firefly, lands at le Bourget, Paris, after the record-setting transatlantic flight, 26 May 1961. (University of North Texas Libraries)
The Mackay Trophy.
The Mackay Trophy
The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)
The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)

On 3 June 1961, while enroute home, The Firefly crashed only 5 miles from Paris, killing the Blériot Trophy-winning  aircrew, Major Elmer E. Murphy, Major Eugene Moses, and First Lieutenant David F. Dickerson. The B-58 was totally destroyed.

Convair B-58A-10-CF Hustler 59-2451, The Firefly.
Convair B-58A-10-CF Hustler 59-2451, The Firefly.

The B-58 Hustler was a high-altitude Mach 2 strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator located in individual cockpits. The aircraft is a delta-winged configuration similar to the Convair F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors.

The Hustler is 96 feet, 10 inches (29.515 meters) long, with a wing span of 56 feet, 10 inches (17.323 meters) and an overall height of 31 feet 5 inches (9.576 meters). The wing’s leading edge is swept back at a 60° angle and the fuselage incorporates the “area rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder, and there are no flaps.

The B-58A was powered by four General Electric J79-GE-5 axial-flow afterburning turbojet engines, suspended under the wings from pylons. This was a single-shaft engine with a 17-stage compressor and 3-stage turbine, rated at 10,300 pounds of thrust (45.82 kilonewtons), and 15,600 pounds (69.39 kilonewtons) with afterburner. The J79-GE-5 was 16 feet, 10.2 inches (5.136 meters) long and 3 feet, 2.0 inches (0.965 meters) in diameter.

The bomber had a cruise speed of 610 miles per hour (981.7 kilometers per hour) and a maximum speed of 1,325 miles per hour (2,132.4 kilometers per hour). The service ceiling is 64,800 feet (19,751 meters). Unrefueled range is 4,400 miles (7,081 kilometers). Maximum weight is 168,000 pounds (76,203.5 kilograms).

The B-58 weapons load was a combination of W-39,  B43 or B61 nuclear bombs. The weapons could be carried in a jettisonable centerline pod, which also carried fuel. The smaller bombs could be carried on underwing hardpoints. There was a defensive 20 mm M61 rotary cannon mounted in the tail, with 1,200 rounds of ammunition and controlled by the Defensive Systems Officer.

Convair B-58A-10-CF Hustler 59-2456 with weapons load. (U.S. Air Force)
Convair B-58A-10-CF Hustler 59-2456 with weapons load. (U.S. Air Force)

¹ FAI Record File Number 4855

© 2017, Bryan R. Swopes

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19 May 1963

Cockpit of Boeing VC-137C 62-6000, SAM 26000, at the national Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)
Cockpit of Boeing VC-137C 62-6000, SAM 26000, at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)

19 May 1963: During a non-stop flight from Andrews Air Force Base, outside Washington, D.C., to Moscow, Russia, Union of Soviet Socialist Republics, a Boeing VC-137C, 62-6000, under the command of Colonel James B. Swindal, United States Air Force, set 15 Fédération Aéronautique Internationale (FAI) World Records for Speed Over a Recognized Course.¹ Colonel Swindal flew the airplane, commonly known as Air Force One, 5,004 miles (8,053.2 kilometers) in 8 hours, 39 minutes, 2 seconds, averaging 490.96 miles per hour (790.12 kilometers per hour). On the return flight, 15 additional records were set.

The fastest segment of the flight was from to Boston, Massachussetts to Oslo, Norway at an average speed of 952.62 kilometers per hour (591.93 miles per hour).

The New York Times reported:

MOSCOW — President Kennedy’s Air Force jet today set a nonstop speed record between Washington and Moscow and shattered 14 other air records. The $8 million Boeing 707, carrying a ten-man party headed by Atomic Energy Commission chairman Glenn T. Seaborg, touched down eight hours 38 minutes and 42 seconds after takeoff — the fastest flight ever made between the U.S. and the Soviet Union. Interred was a Soviet myth that the U.S. lacked a plane able to make a 5,000-mile run nonstop. The black-nosed blue and white jet, piloted by Col. James B. Swindal, 46, of Falls Church, Virginia, made it with fuel for more than two hours of flight remaining, proving that any delays in reaching a commercial agreement are political, not technical.

The New York Times, 19 May 1963

The Washington Post reported that, “. . . On board were a Soviet navigator and a Soviet radio operator, the usual requirements for all international flights over Soviet territory. The two men, both speaking English, flew to Washington to make the flight.”

The Washington Post, 20 May 1963

At the end of its final flight, 20 May 1998, SAM 26000 touches down at Wright-Patterson Air Force Base, Ohio, where it was placed in the collection of the National Museum of the United States Air force. (U.S. Air Force)
At the end of its final flight, 20 May 1998, SAM 26000 touches down at Wright-Patterson Air Force Base, Ohio, where it was placed in the collection of the National Museum of the United States Air Force. (U.S. Air Force)

The Boeing VC-137C was the first of two specially-configured Boeing 707-353B airliners used by the President of the United States, or other senior administration officials. The distinctive white, blue and natural metal livery was created by the famed industrial designer Raymond Loewy.

When the president is aboard, the airplane is designated “Air Force One”. At other times, it uses the Special Air Mission designation, SAM 26000. The airplane entered service in 1962, replacing the three earlier commercial Boeing 707-153 airliners, which were designated VC-137A Stratoliner, USAF serial numbers 58-6970–58-6972.

SAM 26000 was itself replaced by SAM 27000 in 1972, though it remained available as a back-up aircraft. It was retired to the National Museum of the United States Air Force on 20 May 1998. The distinctive white, blue and natural metal livery was created by the famed industrial designer Raymond Loewy.

James Barney Swindal was born 18 August 1917 in West Blocton, Alabama. He enlisted in the Army in 1942, shortly after the Imperial Japanese Navy attacked Pearl Harbor, Hawaii, bringing the United States into the World War. Trained as a pilot in the U.S. Army Air Forces, he flew transports in the China-Burma-India (CBI) theater of operations. After the War, he participated in the Berlin Airlift.

Swindal became President Kennedy’s personal pilot in 1960. He flew JFK to Berlin for his famous “Ich bin ein Berliner” speech, 26 June 1963, and later flew President Kennedy’s casket from Dallas Texas to Washington, D.C.  He retired from the Air Force in 1971. When SAM 26000 arrived at the National Museum of the United States Air Force, he sat in its cockpit for a last time. Colonel Swindal died at Cape Canaveral, Florida, 25 April 2006.

Colonel James B. Swindal, United States Air Force is congrtulated on his promotion by President John F. Kennedy. (Presidential Library)
Colonel James B. Swindal, United States Air Force, is congratulated on his promotion by President John F. Kennedy, 19 March 1962. (Robert Knudsen. White House Photographs. John F. Kennedy Presidential Library and Museum, Boston JFKWHP-1962-03-19-C)

¹ FAI Record File Number 16472

© 2017, Bryan R. Swopes

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