Tag Archives: FAI

19 January 1975

McDonnell Douglas F-15A-6-MC Streak Eagle 72-0119. (U.S. Air Force)
McDonnell Douglas F-15A-6-MC Streak Eagle 72-0119. (U.S. Air Force)
Major Roger J. Smith, u.S. Air Force
Major Roger J. Smith, U.S. Air Force

19 January 1975: Major Roger J. Smith, United States Air Force, a test pilot assigned to the F-15 Joint Test Force at Edwards AFB, California, flew the  McDonnell Douglas F-15A-6-MC 72-0119, Streak Eagle, to its sixth Fédération Aéronautique Internationale (FAI) and U.S. National Aeronautic Association time-to-altitude record.

From brake release at Grand Forks Air Force Base, North Dakota, at 913 feet (278 meters) above Sea Level, the F-15 reached 20,000 meters (65,617 feet) in 122.94 seconds.

This was the seventh time-to-altitude record set by Streak Eagle in just three days.

FAI Record File Num #9066 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 20 000 m
Performance: 2 min 02.94s
Date: 1975-01-19
Course/Location: Grand Forks, ND (USA)
Claimant Roger J. Smith (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

Screen Shot 2015-01-15 at 19.58.24Roger Smith’s United States national record still stands.

Streak Eagle is a very early production F-15A-6-MC Eagle, a single-seat, twin-engine air superiority fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9½ inches (13.043 meters) and overall height of 18 feet, 5½ inches (5.626 meters). The F-15A has an empty weight of 27,000 pounds (12,247 kilograms) and its maximum takeoff weight (MTOW) is 66,000 pounds (29,937 kilograms).

The F-15A is powered by two Pratt & Whitney JTF22A-25A (F100-PW-100) afterburning turbofan engines capable of producing 14,670 pounds of thrust (65.255 kilonewtons), and 23,830 pounds (105.996 kilonewtons), each, with afterburner. The F100 is a two-spool, axial-flow turbine engine with a 3-stage fan section; 10-stage compressor; single chamber combustion section; and 4-stage turbine (2 low- and 2 high-pressure stages). The F100-PW-100 is 191 inches (4.851 meters) long, 46.5 inches (1.181 meters) in diameter, and weighs 3,035 pounds (1,376.7 kilograms).

The cruise speed of the F-15A Eagle is 570 miles per hour (917 kilometers per hour). It has a maximum speed of 915 miles per hour (1,473 kilometers per hour) at Sea Level, and 1,650 miles per hour (2,655 kilometers per hour) at 36,000 feet (10,973 meters). The service ceiling is 65,000 feet (19,812 meters). It can climb in excess of 50,000 feet per minute (254 meters per second), and with a thrust-to-weight ratio of 1.15:1, could climb straight up. The Eagle’s combat radius is 1,222 miles (1,967 kilometers).

The F-15A is armed with one General Electric M61A1 Vulcan 20mm rotary cannon with 940 rounds of ammunition, four AIM-7 Sparrow radar-guided missiles and four AIM-9 Sidewinder heat-seeking missiles.

384 F-15A Eagles were built before production shifted to the improved F-15C version. As F-15Cs became operational, the F-15As were transferred to Air National Guard units assigned to defend continental U.S. airspace. The last F-15A was retired from service in 2009.

Streak Eagle was specially modified for the record attempts. Various equipment that would not be needed for these flights was eliminated: The flap and speed brake actuators, the M61A1 Vulcan 20 mm cannon and its ammunition handling equipment, the radar and fire control systems, unneeded cockpit displays and radios, and one generator.

Other equipment was added: A long pitot boom was mounted at the nose with alpha and beta vanes, equipment for the pilot’s David Clark Company A/P-225-6 full pressure suit, extremely sensitive accelerometers and other instrumentation, extra batteries, an in-cockpit video camera aimed over the pilot’s shoulder, and perhaps most important, a special hold-down device was installed in place of the fighter’s standard arresting hook.

These changes resulted in an airplane that was approximately 1,800 pounds (817 kilograms) lighter than the standard production F-15A. This gave it a thrust-to-weight ratio of 1.4:1.

Streak Eagle, the modified McDonnell Douglas F-15A-6-MC, 72-0119, on the runway at Grand Forks AFB, North Dakota, being prepared for a flight record attempt. (U.S. Air Force)
Streak Eagle, the modified McDonnell Douglas F-15A-6-MC, 72-0119, on the runway at Grand Forks AFB, North Dakota, being prepared for a flight record attempt. (U.S. Air Force)

The flight profiles for the record attempts were developed by McDonnell Douglas Chief Developmental Test Pilot, Charles P. “Pete” Garrison (Lieutenant Colonel, U.S. Air Force, Retired).

Streak Eagle carried only enough fuel for each specific flight, and for the 20,000 meter climb, weighed 29,877 pounds (13,552 kilograms). It was secured to the hold-back device on the runway and the engines were run up to full afterburner. It was released from the hold-back and was airborne in just three seconds.

When the F-15 reached 428 knots (793.4 kilometers per hour), the pilot pulled up into an Immelman, holding 2.5 Gs. Streak Eagle arrived back over the air base, in level flight at about 32,000 feet (9,754 meters), but upside down. Rolling up right, Streak Eagle continued accelerating to Mach 1.5 when the pilot pulled the fighter up at 4.0 Gs until it reached a 55° climb angle until it reached 20,000 meters

Screen Shot 2016-01-18 at 15.55.50Because Streak Eagle was a very early production airplane, its internal structure was weaker than the final production F-15A standard. It was considered too expensive to modify it to the new standard. It was transferred to the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio, in December 1980.

Streak Eagle, the record-setting McDonnell Douglas F-15A-6-MC, 72-0119, in "Compass Ghost" two-tone blue camouflage, at the National Museum of the United States Air Force. (U.S. Air Force)
Streak Eagle, the record-setting McDonnell Douglas F-15A-6-MC, 72-0119, in “Compass Ghost” two-tone blue camouflage, at the National Museum of the United States Air Force. (U.S. Air Force)

© 2017, Bryan R. Swopes

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16 January 1975

McDonnell Douglas F-15A-6-MC 72-0119 Streak Eagle record holder. (U.S. Air Force)
McDonnell Douglas F-15A-6-MC 72-0119, Streak Eagle, FAI world record holder. (U.S. Air Force)

16 January 1975: Three United States Air Force pilots, Majors Roger J. Smith, William R. MacFarlane and David W. Petersen, test pilots assigned to the F-15 Joint Test Force at Edwards Air Force Base, California, set five Fédération Aéronautique Internationale (FAI) time-to-altitude records in one day, flying this unpainted McDonnell Douglas F-15A-6-MC Streak Eagle, serial number 72-0119, from Grand Forks Air Force Base, North Dakota. The airfield’s elevation is 913 feet (278 meters) above Sea Level.

Smith took the first record: from brake release to 3,000 meters (9,843 feet) in 27.571 seconds.

The next three belonged to MacFarlane: 6,000 meters (19,685 feet), 39.335 seconds; 9,000 meters (29,528 feet), 48.863 seconds; and 12,000 meters (39,370 feet), 59.383 seconds.

The last record for the day went to Peterson, who reached 15,000 meters (49,213 feet) in 1 minute, 17.042 seconds.

Over the next two weeks they took the Streak Eagle even higher. On it’s left vertical fin is painted AQUILA MAXIMA. This airplane is in storage at the National Museum of the United States Air Force.

F-15A Streak Eagle record-setting pilots, Majors William MacFarlane, Roger Smith and Dave Peterson. (U.S. Air Force)
F-15A Streak Eagle record-setting pilots, Majors William MacFarlane, Roger Smith and Dave Peterson. (U.S. Air Force)

Screen Shot 2016-01-16 at 20.33.28FAI Record File Num #9077 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 3 000 m
Performance: 27.571s
Date: 1975-01-16
Course/Location: Grand Forks, ND (USA)
Claimant Roger J. Smith (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

Screen Shot 2016-01-16 at 20.37.34FAI Record File Num #8605 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 6 000 m
Performance: 39.335s
Date: 1975-01-16
Course/Location: Grand Forks, ND (USA)
Claimant William R. Macfarlane (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

FAI Record File Num #8600 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 9 000 m
Performance: 48.863s
Date: 1975-01-16
Course/Location: Grand Forks, ND (USA)
Claimant William R. Macfarlane (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

FAI Record File Num #8528 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 12 000 m
Performance: 59.383s
Date: 1975-01-16
Course/Location: Grand Forks, ND (USA)
Claimant William R. Macfarlane (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

Screen Shot 2016-01-16 at 14.43.07FAI Record File Num #8521 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Time to climb to a height of 15 000 m
Performance: 1 min 17.042s
Date: 1975-01-16
Course/Location: Grand Forks, ND (USA)
Claimant David W. Peterson (USA)
Aeroplane: McDonnell Douglas F-15
Engines: 2 Pratt & Whitney F-100

McDonnell Douglas F-15A-8-MC Eagle 73-0090 at Luke Air Force Base. The two aircraft in this photograph are painted “Air Superiority Blue” (F.S. 35450). (U.S. Air Force)

Streak Eagle is a very early production F-15A-6-MC Eagle, a single-seat, twin-engine air superiority fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9½ inches (13.043 meters) and overall height of 18 feet, 5½ inches (5.626 meters). The F-15A has an empty weight of 27,000 pounds (12,247 kilograms) and its maximum takeoff weight (MTOW) is 66,000 pounds (29,937 kilograms).

The F-15A is powered by two Pratt & Whitney JTF22A-25A (F100-PW-100) afterburning turbofan engines capable of producing 14,670 pounds of thrust (65.255 kilonewtons), and 23,830 pounds (105.996 kilonewtons), each, with afterburner. The F100 is a two-spool, axial-flow turbine engine with a 3-stage fan section; 10-stage compressor; single chamber combustion section; and 4-stage turbine (2 low- and 2 high-pressure stages). The F100-PW-100 is 191 inches (4.851 meters) long, 46.5 inches (1.181 meters) in diameter, and weighs 3,035 pounds (1,376.7 kilograms).

The cruise speed of the F-15A Eagle is 570 miles per hour (917 kilometers per hour). It has a maximum speed of 915 miles per hour (1,473 kilometers per hour) at Sea Level, and 1,650 miles per hour (2,655 kilometers per hour) at 36,000 feet (10,973 meters). The service ceiling is 65,000 feet (19,812 meters). It can climb in excess of 50,000 feet per minute (254 meters per second), and with a thrust-to-weight ratio of 1.15:1, could climb straight up. The Eagle’s combat radius is 1,222 miles (1,967 kilometers).

The F-15A is armed with one General Electric M61A1 Vulcan 20mm rotary cannon with 940 rounds of ammunition, four AIM-7 Sparrow radar-guided missiles and four AIM-9 Sidewinder heat-seeking missiles.

384 F-15A Eagles were built before production shifted to the improved F-15C version. As F-15Cs became operation, the F-15As were transferred to Air National Guard units assigned to defend continental U.S. airspace. The last F-15A was retired from service in 2009.

Streak Eagle over St. Louis (McDonnell Douglas Corporation)

Streak Eagle was specially modified by McDonnell Douglas for the record attempts. Various equipment that would not be needed for these flights was eliminated: The flap and speed brake actuators, the M61A1 Vulcan 20 mm cannon and its ammunition handling equipment, the radar and fire control systems, unneeded cockpit displays and radios, and one generator.

Other equipment was added: A long pitot boom was mounted at the nose with alpha and beta vanes, equipment for the pilot’s David Clark Company A/P-225-6 full-pressure suit, extremely sensitive accelerometers and other instrumentation, extra batteries, an in-cockpit video camera aimed over the pilot’s shoulder, and perhaps most important, a special hold-down device was installed in place of the fighter’s standard arresting hook.

These changes resulted in an airplane that was approximately 1,800 pounds (817 kilograms) lighter than the standard production F-15A. This gave it a thrust-to-weight ratio of 1.4:1.

Streak Eagle, the modified McDonnell Douglas F-15A-6-MC, 72-0119, on the runway at Grand Forks AFB, North Dakota, being prepared for a flight record attempt. (U.S. Air Force)
Streak Eagle, the modified McDonnell Douglas F-15A-6-MC, 72-0119, on the runway at Grand Forks AFB, North Dakota, being prepared for a flight record attempt. (U.S. Air Force)

The flight profiles for the record attempts were developed by McDonnell Douglas Chief Developmental Test Pilot, Charles P. “Pete” Garrison (Lieutenant Colonel, U.S. Air Force, Retired). Streak Eagle carried only enough fuel for each specific flight, and weighed from 27,972  to 31,908 pounds (12,688 to 14,473 kilograms). It was secured to the hold-back device on the runway and the engines were run up to full afterburner. It was released from the hold-back and was airborne in just three seconds.

Streak Eagle, the FAI record-setting McDonnell Douglas F-15A-6-MC, 72-0119, at the National Museum of the United States Air Force. (U.S. Air Force)
Streak Eagle, the FAI record-setting McDonnell Douglas F-15A-6-MC, 72-0119, at the National Museum of the United States Air Force. (U.S. Air Force)

© 2017, Bryan R. Swopes

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14 January 1962

Convair B-58A-10-CF Hustler 59-2441, Thompson Trophy winner. (U.S. Air Force)
Convair B-58A-10-CF Hustler 59-2441, Thompson Trophy winner. (U.S. Air Force)

14 January 1961: Lt. Col. Harold E. Confer, Lt. Col. Richard Weir and Major Howard Bialas, flying Convair B-58A-10-CF Hustler 59-2441, Roadrunner, obliterated the FAI closed-course speed records established only two days earlier by another B-58 crew flying 59-2442. They averaged 2,067.58 kilometers per hour (1,284.73 miles per hour) over a 1,000 kilometer closed circuit, more than 200 miles per hour faster, and set three Fédération Aéronautique Internationale records. They were awarded the Thompson Trophy.

59-2441 was sent to The Boneyard in 1970, and along with its sister, 59-2442, scrapped in 1977.

Colonel Harold E. Confer, U.S. Air Force
Colonel Harold E. Confer, U.S. Air Force

FAI Record File Num #4565 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km without payload
Performance: 2 067.58 km/h
Date: 1961-01-14
Course/Location: Edwards AFB, CA (USA)
Claimant Harold E. Confer (USA)
Aeroplane: Convair B-58A Hustler (USAF 92-441)
Engines: 4 G E J79

FAI Record File Num #4566 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km with 1 000 kg payload
Performance: 2 067.58 km/h
Date: 1961-01-14
Course/Location: Edwards AFB, CA (USA)
Claimant Harold E. Confer (USA)
Aeroplane: Convair B-58A Hustler (USAF 92-441)
Engines: 4 G E J79

FAI Record File Num #4567 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km with 2 000 kg payload
Performance: 2 067.58 km/h
Date: 1961-01-14
Course/Location: Edwards AFB, CA (USA)
Claimant Harold E. Confer (USA)
Aeroplane: Convair B-58A Hustler (USAF 92-441)
Engines: 4 G E J79

Thompson Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)
Thompson Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)

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. Four General Electric J79-GE-5 afterburning turbojet engines, producing 15,000 pounds of thrust, each, are suspended under the wings from pylons. 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 59-2441, Thompson Trophy winner, at Davis-Monthan AFB. (U.S. Air Force)
Convair B-58A-10-CF Hustler 59-2441, Thompson Trophy winner, at Davis-Monthan AFB. (U.S. Air Force)

© 2016, Bryan R. Swopes

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14 January 1936

Hoard Hughes with his record-setting Northrop Gamma. (Unattributed)
Howard Hughes with the record-setting Northrop Gamma. (UNLV Special Collections)

14 January 1936: Flying a Northrop Gamma 2G, serial number 11, which he had leased from Jackie Cochran, Howard Robard Hughes, Jr., set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course (Los Angeles, California to New York) in 9 hours, 26 minutes, 10 seconds, at an average speed of 417.0 kilometers per hour (259.1 miles per hour).¹ Most of the flight was made at altitudes of  15,000–18,000 feet (4,572–5,486 meters), and Hughes used supplemental breathing oxygen.

Howard Hughes climbs out of the Northrop Gamma at Newark, New Jersey. (UNLV Digital Collection)
Howard Hughes climbs out of the Northrop Gamma at Newark, New Jersey. (UNLV Digital Collection)

Jack Northrop had designed and built the Gamma as a long-range cargo and mail plane for Transcontinental and Western Air, Inc.  The contract was cancelled, though, and several airplanes became available to other customers. Jackie Cochran purchased s/n 11, which had been completed 15 August 1934, and had it modified by Northrop as a two-place long-distance racer for the 1934 MacRobertson London-to-Australia air race, which she planned to fly with her friend Ted Marshall.

The Gamma’s original engine was replaced with a liquid-cooled, supercharged, 1,570.381-cubic-inch-displacement (25.734 liters) Wright Aeronautical Division Conqueror SGV1570F4 (also known as the Curtiss Conqueror), a DOHC 60° V-12 engine rated at 745 horsepower at Sea Level. The engine drove a two-bladed propeller. The Gamma had 7 fuel tanks: 3 in each wing and 1 in the fuselage. Total capacity was 486 gallons (1,840 liters) of gasoline and 29 gallons (110 liters)of lubricating oil. A second fuselage tank was later added, bring the total fuel capacity to 586 gallons (2,218 liters). The Gamma 2G had an empty weight of 4,727 pounds (2,144 kilograms) and a maximum gross weight of 8,037 pounds (3,646 kilograms). The modified airplane was inspected and a temporary commercial registration, NC13671, was approved 29 September 1934.

The Northrop Corporation Gamma 2G, NC13761, after modification for the MacRobertson Race, 29 September 1934. (The Northrop Corporation)

While being ferried to New York by Jackie and her new copilot, Royal Leonard, problems with the engine’s supercharger forced them to land in Arizona. Cochran continued east by airliner while Leonard and a Curtiss-Wright mechanic continued east in the Gamma. Flying on the night of 1 October 1934, a continuing problem with the supercharger forced them to make an off-field landing near Tucumcari, New Mexico, using light from dropped flares. The Gamma was seriously damaged and had to be returned to Northrop for repair.

The airplane’s temporary registration was suspended. A section of the wing and the forward lower half of the fuselage were replaced, provisions for installing a Pratt & Whitney radial engine were made, and the rear cockpit was removed. (Cochran’s plans for the MacRobertson Race had to be revised,² so she had the airplane modified for the Bendix Trophy Race.) The repairs and modifications were completed 30 November 1934.

The “re-modified” Gamma 2G was now powered by an air-cooled, supercharged, 1,534.94-cubic-inch-displacement (25.153 liters) Pratt & Whitney Twin Wasp Jr. SA1-G 14-cylinder radial engine with a three-bladed Hamilton Standard controllable-pitch propeller. The SA1-G was rated at 700 horsepower at 2,500 r.p.m. at 6,500 feet (1,981 meters). It could be ordered with a 3:2 or 4:3 gear reduction ratio.

The official ownership history of the Gamma is murky. The original application for a Department of Commerce Aeronautics Branch license specified the owner as The Northrop Corporation. On 4 January 1935, Northrop’s registration was cancelled by the Department of Commerce because, “Aircraft not inspected for relicensing.”

Jackie Cochran flew the Gamma in the 1935 Bendix Trophy Race, but did not finish.

When Jackie Cochran requested registration in her name, she failed to submit a Bill of Sale with her application. After repeated written requests by the Bureau of Air Commerce to submit a bill of sale went unanswered, her application for a restricted registration for the airplane was cancelled, 9 January 1936. J Carroll Cone, Assistant Director of Air Commerce (Air Regulation) informed her in writing: “The status of this aircraft is unlicensed and unidentified, according to our records. Any operation thereof would be in violation of the Air Commerce Regulations and subject the offender to the civil penalty provided therefor.”

Finally, a Bill of Sale from The Northrop Corporation, dated 30 November 1935, was provided to the Aeronautics Bureau. It said that Northrop had sold the airplane to Cochran, “for and in consideration of ten dollars ($10.00)”.

Meanwhile, Howard Hughes had seen the Gamma and wanted to buy it. Jackie Cochran tells how Howard Hughes acquired the airplane:

One night about 11:30 I was exhausted in my hotel room and the telephone rang. . .

“Jackie,” the voice says, “this is Howard.”

“Howard who?” I say, still sleepy and getting frustrated.

“Howard Hughes,” the man says.

“Howard who?” I ask again.

“Howard Hughes,” he repeats.

. . . We argued about who he was a bit more. Finally, he says, “I want to buy your airplane.”

I’m thinking that this is an incredible conversation. “It’s not for sale, Howard,” I reply. “I’m going to fly it in the Bendix.”

“I don’t want to fly it in the Bendix,” he answers. “I want to fly it cross-continental.”

“So do I,” I say.

Howard Hughes and I negotiated over the Northrop Gamma for about four weeks. . . Howard wanted my Northrop so badly, but it would break my heart to consider handing over my rights to it. . . when he offered to rent it, with an option to buy, I caved in. . . .

Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, at 152–153.

When Hughes took possession of the Gamma 2G, he had the Pratt & Whitney engine replaced with a 1,823.129 cubic-inch (29.785 liter) Wright Cyclone SGR-1820-G5 nine-cylinder radial engine, and a three bladed-Hamilton Standard constant-speed propeller with a diameter of 11 feet, 3 inches (3.429 meters). The engine had a Normal Power rating of 830 horsepower at 2,100 r.p.m to 4,300 feet (1,311 meters), and 930 horsepower for Takeoff. This engine did not yet have government certification. Three additional fuselage tanks were installed, increasing the Gamma’s fuel capacity to 690 gallons. Hughes did not submit the Gamma for Department of Commerce inspection and licensing. It was not approved in the new configuration.

Jackie Cochran took the Gamma back from Hughes and had the Twin Wasp Jr. reinstalled, and submitted a new application for registration 31 March 1936. This was approved 28 April 1936, and the Gamma received a restricted registration, NR13761. It was damaged beyond repair after an emergency landing, 10 July 1936.

The Northrop Gamma 2G at Newark, New Jersey, 14 Janary 1936. (UNLV Libraries Digital Collection)

¹ FAI Record File Number 13237

² With Northrop unable to repair the airplane in time for the MacRobertson Race, at the last minute Jackie Cochran entered with a different airplane (a Granville Brothers Gee Bee R-6H).

© 2017, Bryan R. Swopes

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13 January 1949

Bill Odom's record-setting Beechcraft 35 Bonanza, N80040. (FAI)
Bill Odom’s record-setting Beechcraft 35 Bonanza, N80040. (FAI)

13 January 1949: William P. Odom set a Fédération Aéronautique Internationale (FAI) World Record for Distance in a Straight Line when he flew a Beechcraft 35 Bonanza, N80040, named Waikiki Beech, from Honolulu, Oahu, Territory of Hawaii, to Oakland, California, an official distance of 3,873.48 kilometers (2,406.87 miles).

Screen Shot 2015-01-17 at 12.26.45

The Chicago Daily Tribune reported the event:

Odom Flight from Hawaii Sets Light Plane Record

Hops Pacific to Oakland in 22 Hours

Oakland, Cal., Jan. 13 (Special)—Flyer Bill Odom set a new light plane record today in a flight across the Pacific from Hawaii, but dwindling gasoline supplies forced him to cut short his eastward flight and he landed here at 6:38 p.m. (8:38 Chicago time).

Odom, who had planned to continue on to Teterboro, N.J., 5,285 miles from his starting place in Hawaii had been in the air 22 hours and six minutes. He left Honolulu at 6:32 p.m. Wednesday (10:32 p.m. Wednesday Chicago time).

The flight over the Pacific, more than 2,300 miles, broke the light plane record of 2,061 miles set by two Russian flyers, A. Goussarov and V. Glebov Sept. 23, 1937, from Moscow to Krasnoyarsk. The record is recognized by the International Aeronautical federation for light planes, first category, 397–549 cubic inches engine displacement.

Uses Most of Fuel

William P. Odom. (FAI)
William P. Odom. (FAI)

Odom was two hours behind schedule and had only about 80 out of his 260 gallons of gasoline when he passed over the Golden Gate at 4:27 p.m. (6:27 p.m. Chicago time.) Head winds had taken a heavy toll of his gasoline load.

He radioed that he intended to add as much mileage as possible to his record before landing. He kept on, reaching Reno, Nev. where ice on his wings and a snowstorm on the airport forced him to turn back.

He then headed for Sacramento airport but no civil aeronautics administration officials were there and he landed at Oakland. There, the plane and its instruments were sealed.

“Boy, am I tired,” Odom said.

He covered more than 2,500 miles from Honolulu to Reno, but as he did not land at Reno the record will remain about 2,300 miles, the distance from Honolulu to Oakland.

Odom had bucked headwinds since he switched his single engined Beechcraft’s course south to fly over San Francisco instead of Seattle. He said he changed his course by mistake this morning. Somehow, he said, he lost his PBY escort from Honolulu and veered to the right.

He first had hunted out and ridden winds that took him northeast toward Seattle, but 1,800 miles out of Hawaii he hit a high pressure area that gave him for a time, tailwinds that enabled him to conserve gasoline.

Late Model Plane

Beechcraft 35 Bonanza N80040. (FAI)
Beechcraft 35 Bonanza N80040. (FAI)

Odom’s plane is a post-war model with a V-type tail, a tricycle landing gear that tucks up into the wings, a tiny little 185 horsepower, six cylinder unsupercharged engine. Its total weight with fuel, pilot, emergency gear, radio, and full equipment at take-off was only 3,750 pounds. It is an all-metal, low-wing monoplane which in its standard form can carry four passengers including pilot.

For his flight Odom had extra radio and a 100 gallon fuel tank installed in the cabin. Each wing tip also has a specially made fuel tank carrying 60 gallons, making 120 gallons total in those two containers. The normal tankage for the Bonanza is 40 gallons.

Odom holds the around the world flight record of 73 hours, 5 minutes and 11 seconds, set Aug. 11, 1947, from Chicago to Chicago in a converted A-20 bomber.

Chicago Daily Tribune, Vol. CVIII, No. 12, Friday, January 14, 1949, Page 1, Column 7.

Beechcraft Model 35 Bonanza NX80040. This is the fourth prototype. It is in the collection of the Smithsonian Institution National Air and Space Museum. (Beech Aircraft Corporation)
Beechcraft Model 35 Bonanza NX80040. This is the fourth prototype. (Beech Aircraft Corporation)

N80040 was the fourth prototype Beechcraft Model 35 Bonanza. (The first two were static test articles.)

The Beechcraft Model 35 Bonanza is a single-engine, four-place all-metal light civil airplane with retractable landing gear. The Bonanza has the distinctive V-tail with a 30° dihedral which combined the functions of a conventional vertical fin and rudder, and horizontal tail plane and elevators.

The Model 35 was 25 feet, 2 inches (7.671 meters) long with a wingspan of 32 feet, 10 inches (10.008 meters) and height of 6 feet, 6½ inches (1.994 meters). It had an empty weight of 1,458 pounds (661 kilograms) and gross weight of 2,550 pounds (1,157 kilograms.)

NX80040, s/n 4, and the following production models were powered by an air-cooled, 471.24-cubic-inch-displacement (7.72 liter) Continental Motors, Inc., E185 horizontally-opposed 6-cylinder engine. This engine was rated at 165 horsepower at 2,050 r.p.m. (NX80150, s/n 3, had been equipped with a 125-horsepower Lycoming O-290-A.) The Bonanza had a two-bladed electrically-controlled variable pitch R-100 propeller with a diameter of 7 feet, 4 inches (2.235 meters) made of laminated wood.

The “V-tail Bonanza” had a maximum speed of 184 miles per hour (296 kilometers per hour) at Sea Level, and a cruise speed of 175 miles per hour ( 282 kilometers per hour)at 10,000 feet (3,048 meters). Its service ceiling was 18,000 feet (5,486 meters). With full fuel, 40 gallons (151.4 liters), the airplane had a range of 750 miles (1,207 kilometers).

The Beechcraft 35 was in production from 1947 to 1982. More than 17,000 Model 35s and the similar Model 36 were built.

Beechcraft Model 35 Bonanza N80040, s/n 4, "Waikiki Beech, at the Smithsonian Institution National Air and Space Museum. (NASM)
Beechcraft Model 35 Bonanza N80040, s/n 4, “Waikiki Beech,” at the Smithsonian Institution National Air and Space Museum. (NASM)

William P. Odom had flown a Douglas A-26 Invader named Reynolds Bombshell around the world in 3 days, 6 hours 55 minutes, 56 seconds, 12–16 April 1947. He made a second around the world flight, 7–11 August 1947, again flying the A-26. The duration of this second trip was 3 days, 1 hour, 5 minutes, 11 seconds. (Neither flight was recognized as a record by the FAI.)

On 8 March 1949, Odom made another FAI World Record flight with Waikiki Beech, from Honolulu to Teterboro, New Jersey, 7,977.92 kilometers (4,957.25 miles). (FAI Record File Number 9112)

With these records and record attempts, Bill Odom persuaded Jackie Cochran to buy a radically-modified P-51C Mustang named Beguine (NX4845N) for him to fly at the 1949 National Air Races at Cleveland Municipal Airport, Ohio.

Though he had never flown in a pylon race, Odom had qualified the P-51 Beguine for the 105 mile Sohio Trophy Race, held 3 September 1949. He won the race, averaging 388.393 miles per hour (625.058 kilometers per hour. He had also entered the Thompson Trophy Race, qualifying with a speed of 405.565 miles per hour (652.694 kilometers per hour.)

The Thompson Trophy Race was held on 5 September. On the second lap, Odom’s P-51 went out of control and crashed into a house near the airport. Bill Odom, along with a woman and child on the ground, were killed.

© 2017, Bryan R. Swopes

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