Tag Archives: Non-Stop Flight

19–20 November 1945

Bell-Atlanta B-29B-60-BA Superfortress 44-8061, the Pacusan Dreamboat. (U.S. Air Force)
Bell-Atlanta B-29B-60-BA Superfortress 44-84061, the Pacusan Dreamboat. (U.S. Air Force)

19–20 November 1945: A Bell-Atlanta B-29B-60-BA Superfortress, 44-84061, named Pacusan Dreamboat, piloted by Colonel Clarence Shortridge Irvine and Lieutenant Colonel G.R. Stanley, flew non-stop and unrefueled from Guam, the largest and southernmost island in the Mariana Islands of the Western Pacific, to Washington, D.C. The four-engine heavy bomber covered the 8,198 miles (13,193 kilometers) in 35 hours, 5 minutes. It set a Fédération Aéronautique Internationale (FAI) record for Distance in a Straight Line:  12,739.59 kilometers (7,916.01 miles).¹

Bell Atlanta B-29B-60-BA Superfortress over Seattle, Washington. (Boeing)
Bell Atlanta B-29B-60-BA Superfortress 44-84061, “Pacusan Dreamboat,” over Seattle, Washington. (Boeing)

Pacusan Dreamboat was modified specifically for a series of long-distance flights. A standard production B-29B, a light-weight variant of the Boeing B-29 Superfortress, it did not have the four power gun turrets with their .50-caliber machine guns. A radar-directed 20 mm cannon and two .50-caliber machine guns in the tail were the only defensive weapons. Much of the standard armor plate was also deleted. It weighed 69,000 pounds (31,298 kilograms) empty and 137,000 pounds (62,142 kilograms) fully loaded. Pacusan Dreamboat was further lightened. The tail guns were removed and the tail reshaped. It had an empty weight of 66,000 pounds (29,937 kilograms). Its takeoff weight on this flight was 151,000 pounds (68,492 kilograms).

Pacusan Dreamboat carried a 12-man crew and 10,000 gallons (37,854 liters) of gasoline.

Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J.Benett, G.F.Broughton, Dock West, W.S. O'Hara, F.S. O'Leary, K.L. Royer, F.J.Shannon, J.A. Shinnault, G.R. Stanley. (FAI)
Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J. Benett, G.F. Broughton, Dock West, W.S. O’Hara, F.S. O’Leary, K.L. Royer, F.J.Shannon, J.A. Shinnault, G.R. Stanley. (FAI)

Pacusan Dreamboat set a number of distance and speed records, including Honolulu, Hawaii to Cairo, Egypt and Burbank to New York in 5 hours, 27 minutes, averaging 451.9 miles per hour (727.26 kilometers per hour).

The Pacusan Dreamboat was stricken from the Air Force inventory 8 August 1954 and reclaimed at Tinker Air Force Base, Oklahoma City, Oklahoma.

Bell-Atlanta B-29B-60-BA Superfortress 44-84061, Pacusan Dreamboat. (FAI)
Bell-Atlanta B-29B-60-BA Superfortress 44-84061, Pacusan Dreamboat. (FAI)

¹ FAI Record File Number 9277

© 2017, Bryan R. Swopes

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24–25 October 1928

Harry Tucker’s Lockheed Vega, NX4769. (Unattributed)

24–25 October 1928: Captain Charles B.D. Collyer, Air Service, United States Army, and Harry J. Tucker flew Tucker’s Lockheed Vega, NX4769, from New York to Los Angeles, non-stop, in 24 hours, 55 minutes.

A contemporary newspaper article reported the event:

YANKEE DOODLE SETS NEW MARK

Monoplane Flies Across Continent to Los Angeles in 24 Hours, 55 Minutes

Mines Field, Los Angeles, Oct. 25—(AP)—Setting a new record for a trans-continental non-stop airplane flight from the Atlantic coast to the Pacific, the monoplane Yankee Doodle arrived here at 2:12 p.m. today from New York.

The unofficial time of the flight as announced by Capt. C.D.B. Collyer, pilot and Harry Tucker, owner and passenger, was 24 hours 55 minutes. The best previous time for the westward flight was 26 hours and 50 minutes, made in 1923 by Lieutenants John MacReady [John A. Macready] and Oakley Gelley [Oakley George Kelly].

530 Gallons Carried

The Yankee Doodle hopped off at Roosevelt Field at 4:16:35 p.m. Eastern Standard Time yesterday. The little cigar-shaped white-winged plane was loaded with 530 gallons of gasoline, just about enough for a 24-hour flight, and a check began shortly after landing to determine how much of the fuel was left.

The westward flight covered approximately the course flown over by Col. Arthur Goebel when he piloted his plane to a new West-East non-stop trans-continental record of 18 hours and 55 minutes several weeks ago.

This was the fourth time Tucker has sent his plane into a coast-to-coast grind. The first West to East attempt was unsuccessful but on the second attempt Goebel piloted the machine through to the record.

The Cornell Daily Sun, Ithaca, New York, Friday, October 26, 1928, Volume XLIX, Number 29 at Page 1, Column 5

Captain Charles B.D. Collyer

Charles Bascum Drury Collyer was born at Nashville, Tennessee, 24 August 1896, the son of Rev. Charles Thomas Collyer. He traveled throughout the world, and lived for a time in Seoul, Korea. Collyer attended Virginia Polytechnic Institute, a military college at Blacksburg, Virginia, as a member of the class of 1919.

Collyer served in the United States Army as a private, first class, being discharged 1 May 1919. He held a commission as a second lieutenant, Aviation Section, Signal Reserve Corps. He was employed as chief pilot, Liberty Flyers, Inc., at Savannah, Georgia.

From 28 June to 22 July 1928, Collyer had flown around the world with John Henry Mears. Collyerwas president of the Aviation Services Corporation of New York, which had been formed “to do unusual things in aviation.”

Harry J. Tucker

Harry J. Tucker was variously described as an “auto tycoon” and a “wealthy Santa Monica, California, businessman.” He was born in 1891.

Charles B.D. Collyer and Harry Tucker were killed 3 November 1928 when Yankee Doodle crashed in fog near Venezia, Yavapai County, Arizona. Collyer was buried at Arlington, National Cemetery, Virginia.

Yankee Doodle was the seventh Lockheed Vega produced (c/n 7). The Vega was a very state-of-the-art aircraft for its time. The prototype flew for the first time 4 July 1927 at Mines Field, Los Angeles, California. It used a streamlined monocoque fuselage made of molded plywood. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them.

The Vega was flown by one pilot and could carry four passengers. It was 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). The airplane had an empty weight of 1,875 pounds (851 kilograms) and a gross weight of 3,470 pounds (1,574 kilograms).

The early Vegas were powered by an air-cooled, normally-aspirated 787.26-cubic-inch-displacement (12.901 liter) Wright J-5C Whirlwind nine-cylinder radial engine producing 200 horsepower at 1,800 r.p.m., and 225 horsepower at 2,000 r.p.m. This was a direct-drive engine which turned a two-bladed Hamilton Standard propeller. The Wright J-5C was 2 feet, 10 inches (0.864 meters) long and 3 feet, 9 inches (1.143 meters) in diameter. It weighed 508 pounds (230.4 kilograms).

The Vega had a cruising speed of 118 miles per hour (190 kilometers per hour) and atop speed of 138 miles per hour (222 kilometers per hour)—very fast for its time. The airplane’s range was 900 miles (1,448.4 kilometers). It could fly at an altitude 15,000 feet (4,572 meters).

Lockheed Vega NX4769 at NAS North Island, 1928. (San Diego Air and Space Museum Archives)
Lockheed Vega NX4769 at NAS San Diego, 1928. (San Diego Air and Space Museum Archives)

© 2017, Bryan R. Swopes

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11 July 1935

Laura Ingalls in the cockpit of her Lockheed Orion 9D Special, NR14222, warming up its engine at Floyd Bennett Field, 10 July 1935. (Rudy Arnold)
Laura Ingalls in the cockpit of her Lockheed Orion 9D Special, NR14222, warming up its engine at Floyd Bennett Field, 10 July 1935. (Rudy Arnold)

11 July 1935: At 5:31 a.m., Eastern Daylight Time, (01:31 UTC) Laura Houghtaling Ingalls took off from Floyd Bennett Field, Brooklyn, New York, and flew non-stop across the North American continent to the Union Air Terminal, Burbank, California. She landed there at 8:51 p.m., Pacific Daylight Time (19:31 UTC). Her airplane was a single-engine Lockheed Model 9D Orion, registration NR14222, which she had named Auto da Fé (“act of faith” or “act of penance”).

Ingalls was the first woman to fly across the country from East to West. In 5 October 1930, she flew a de Havilland DH.60 Gipsy Moth from Roosevelt Field to Grand central Air Terminal at Glendale Calif, arriving 9 October. The flight required nine fuel stops, and took 30 hours and 27 minutes over four days.

The elapsed time of her non-stop 1935 transcontinental flight was 18 hours, 20 minutes, 30 seconds.

Laura Ingalls had taken delivery of the Orion 9D Special at Lockheed, Burbank, California, five months earlier. Contemporary newspaper reports said that the “Black Mystery Ship” cost $45,000.

Laura Houghtaling Ingalls' Lockheed Orion 9D Special, NR14222 (San Diego Air and Space Museum Archives)
Laura Houghtaling Ingalls’ Lockheed Orion 9D Special, NR14222 (San Diego Air and Space Museum Archives)

The Lockheed Model 9 Orion was a single-engine, low-wing monoplane, designed in 1931 by Gerard Vultee for airline use and was capable of carrying six passengers in an enclosed cabin. The Orion was the first commercial airliner with retractable landing gear and was faster than any military airplane in service at the beginning of the decade. Like other Lockheed aircraft of the time, it was constructed of strong, light-weight, molded plywood, but the Orion was Lockheed’s last wooden airplane.

Billy Parker, Laura Ingalls and Wiley Post at the 1935 National Air Races. Ingall's Lockheed Orion 9D, NR14222, Auto da Fé, has its engine cowling removed for maintenance. (Monash University)
Billy Parker, Laura Ingalls and Wiley Post at the 1935 National Air Races. Ingall’s Lockheed Orion, NR14222, Auto da Fé, has its engine cowling removed for maintenance. (Monash University)

The Lockheed Orion 9D was 28 feet, 4 inches (8.64 meters) long with a wingspan of 42 feet, 9¼ inches (13.04 meters) and height of 9 feet, 8 inches (2.95 meters). It had an empty weight of 3,640 pounds (1,651 kilograms) and maximum takeoff weight of 5,200 pounds (2,359 kilograms).

Auto da Fé was powered by an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp S1D1 nine-cylinder radial engine, rated 525 horsepower at 2,200 r.p.m. (takeoff and normal power rating). The engine had a compression ratio of 6:1. The S1D1 was a direct-drive engine, which turned a two-bladed Hamilton Standard variable-pitch, constant-speed propeller. The Wasp S1D1 was 4 feet, 3.438 inches (1.307 meters) in diameter, 3 feet, 6.625 inches (1.083 meters) long and weighed 763 pounds (346 kilograms).

The cruise speed of the Orion was 205 miles per hour (330 kilometers per hour) and the maximum speed was 220 miles per hour (354 kilometers per hour) at Sea Level. It had a range of 750 miles (1,159 kilometers) in standard configuration. The service ceiling was 22,000 feet (6,705 meters).

Laura Ingalls shows navigation equipment to be installed aboard her Lockheed Orion. (Corbis)

Ingall’s airplane carried 630 gallons (2,384.8 liters) of gasoline and 40 gallons (151.4 liters) of engine oil. NR14222 was equipped with a Sperry Gyro Pilot and a Westport radio compass and receiver for navigation.

After departing Floyd Bennett Field, Ingalls flew along a commercial airway marked with radio beacons. Her route of flight was from Brooklyn, New York to Pittsburgh, Pennsylvania—Columbus, Ohio—Indianapolis, Indiana—Kansas City, Missouri—Albuquerque, New Mexico—Burbank, California. This was only the third time that a non-stop transcontinental flight had been accomplished.

Laura H. Ingalls stands in front of her Lockheed Orion 9D, NR14222, in this personally inscribed photograph.
Laura H. Ingalls stands in front of her Lockheed Orion 9D Special, NR14222, in this personally inscribed photograph. (San Diego Air and Space Museum Archives)

 

© 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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2–3 May 1923

Lieutenants John A. Macready and Oakley G. Kelly with their Fokker T-2. (NASM)

2–3 May 1923: Air Service, United States Army, pilots Lieutenant John Arthur Macready and Lieutenant Oakley George Kelly made the first non-stop transcontinental flight with a Nederlandse Vliegtuigenfabriek Fokker T-2 single-engine monoplane, A.S. 64233.

The two aviators took off from Roosevelt-Hazelhurst Field, Long Island, New York, at 12:30 p.m. Eastern Time and landed at Rockwell Field (now, NAS North Island), San Diego, California, the next day at 12:26 p.m., Pacific Time. They had flown 2,470 miles (3,975 kilometers) in 26 hours, 50 minutes, 38.8 seconds, for an average speed of 92 miles per hour (148 kilometers per hour).

Macready and Oakley had made two previous attempts, flying West-to-East to take advantage of prevailing winds and the higher octane gasoline available in California. The first flight was terminated by weather, and the second by engine failure.

Fokker T-2 A.S. 64233 (FAI)
Fokker T-2 A.S. 64233 (FAI)

The Fokker F.IV was built by Anthony Fokker’s Nederlandse Vliegtuigenfabriek at Veere, Netherlands in 1921. The Air Service purchased two and designated the type T-2, with serial numbers A.S. 64233 and A.S. 64234.

Several modifications were made to prepare the T-2 for the transcontinental flight. Normally flown by a single pilot in an open cockpit, a second set of controls was installed so that the airplane could be controlled from inside while the two pilots changed positions. Additional fuel tanks were installed in the wing and cabin.

The Fokker F.IV was a single-engine, high-wing monoplane with fixed landing gear. The airplane was designed to carry 8–10 passengers in an enclosed cabin. For its time, the Fokker was a large airplane. Measurements from the Fokker T-2 at the Smithsonian Institution are: 49 feet, 10 inches (15.189 meters) long, with a wing span of 80 feet, 5 inches (24.511 meters), and height 12 feet, 2 inches (3.708 meters). On this flight, it carried 735 gallons (2,782 liters) of gasoline in three fuel tanks. When it took off from Long Island, the gross weight of the T-2 was 10,850 pounds (4,922 kilograms), only a few pounds short of its maximum design weight.

The Fokker F.IV was offered with a choice of engines: A Rolls-Royce Eagle IX V-12, Napier Lion II “broad arrow” W-12, or Liberty L-12 V-12. The T-2 was powered by a water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Ford-built Liberty L-12 single overhead cam (SOHC) 45° V-12 engine with a compression ratio of 5.4:1. (Serial number A.S. No. 5142) The Liberty produced 408 horsepower at 1,800 r.p.m. The L-12 as a right-hand tractor, direct-drive engine. Installed on A.S. 64233, the engine turned turned a two-bladed Curtiss fixed-pitch walnut propeller with a diameter of 10 feet, 5 inches (3.175 meters). The Liberty 12 was 5 feet, 7.375 inches (1.711 meters) long, 2 feet, 3.0 inches (0.686 meters) wide, and 3 feet, 5.5 inches (1.054 meters) high. It weighed 844 pounds (383 kilograms).

Lieutenant Oakley G. Kelly, U.S. Army Air Service (FAI)
First Lieutenant Oakley G. Kelly, U.S. Army Air Service (FAI)
Lt. John A. Macready, U.S. Army Air Service
Lt. John A. Macready, U.S. Army Air Service

John Macready and Oakley Kelley won the 1923 Mackay Trophy for this flight. Macready had previously won the award in 1921 and 1922. He is the only pilot to have won it three times.

During testing to determine the feasibility of the flight, on 16–17 April 1923, Lieutenant Kelly and Lieutenant Macready set six Fédération Aéronautique Internationale (FAI) World Records for speed, distance and duration, flying the Fokker T-2. At Wilbur Wright Field, Dayton, Ohio, they flew 2,500 kilometers (1,553.428 miles) at an average speed of 115.60 kilometers per hour (51.83 miles per hour); 3,000 kilometers (1,864.114 miles) at 115.27 kilometers per hour (71.63 miles per hour); 3,500 kilometers (2,174.799 miles) at 114.82 kilometers per hour (71.35 miles per hour); 4,000 kilometers (2,485.485 miles) at 113.93 kilometers per hour (70.79 miles per hour); flew a total distance of 4,050 kilometers (2,517 miles); and stayed aloft for 36 hours, 4 minutes, 34 seconds. Their overall average speed was 112.26 kilometers per hour (69.76 miles per hour) seconds.

The United States Army transferred Fokker T-2 A.S. 64223, to the Smithsonian Institution in January 1924. It is on display at the National Air and Space Museum.

U.S. Army Air Service Fokker T-2, A.S. 64223, on display at the Smithsonian Institution, National Air and Space Museum. (NASM)

© 2017, Bryan R. Swopes

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