Tag Archives: Pratt & Whitney J75-P-17

2 February 1970

Convair F-106A Delta Dart of the 71st Fighter Interceptor Squadron, with a Boeing KC-135 Stratotanker, circa 1970. (U.S. Air Force)
Convair F-106A-100-CO Delta Dart 58-0775 of the 71st Fighter Interceptor Squadron with a Boeing KC-135 Stratotanker, circa 1970. This is the same type aircraft flown by Lieutenant Gary Foust, 2 February 1970. (U.S. Air Force)
1st Lt. Gary E. Foust

2 February 1970: At approximately 9:50 a.m., three Convair F-106A Delta Dart supersonic interceptors of the 71st Fighter Interceptor Squadron, 24th Air Division, based at Malmstrom Air Force Base, Montana, were engaged in an air combat training mission.

1st Lieutenant Gary Eugene Foust was flying F-106A-100-CO 58-0787, an airplane usually flown by the squadron’s maintenance officer, Major Wolford.

During the simulated combat, Lt. Foust entered into a vertical climb with his “opponent,” Captain Tom Curtis, who was also flying an F-106, and they both climbed to about 38,000 feet (11,600 meters) while using a “vertical rolling scissors” maneuver as each tried to get into a position of advantage.

Diagram of Vertical Rolling Scissors Maneuver, (Predrag Pavlovic, dipl. ing. and Nenad Pavlovic, dipl. ing.)
Diagram of Vertical Rolling Scissors Maneuver. (Predrag Pavlovic, dipl. ing. and Nenad Pavlovic, dipl. ing.)

Lt. Foust’s interceptor stalled and went in to a flat spin. Captain Curtiss described it: “The aircraft looked like the pitot tube was stationary with the aircraft rotating around it. Very flat and rotating quite slowly.”

Foust tried all the recovery procedures but could not regain control of the Delta Dart. With no options remaining, at about 15,000 feet (4,572 meters), Foust ejected from the apparently doomed airplane.

This F-106A (S/N 58-0787) was involved in an unusual incident. During a training mission, it entered an flat spin forcing the pilot to eject. Unpiloted, the aircraft recovered on its own and miraculously made a gentle belly landing in a snow-covered field. (U.S. Air Force photo)
Convair F-106A Delta Dart 58-0787 made an un-piloted belly landing onto a snow-covered farm field near Big Sandy, Montana, 2 February 1970. (U.S. Air Force)

After the pilot ejected, the F-106 came out of the spin and leveled off.  With its engine still running, -787 continued flying, gradually descending, until it slid in to a landing in a wheat field near Big Sandy, Montana. Eventually the airplane ran out of fuel and the engine stopped at about 12:15 p.m.

Lieutenant Foust safely parachuted into the mountains and was soon rescued.

58-0787 was partially disassembled by a maintenance team from Hill Air Force Base, Utah, and loaded on to a rail car. It was then transported to the Sacramento Air Logistics Center at McClellan Air Force Base, Sacramento, California, where it was repaired and eventually returned to flight status with the 49th Fighter Interceptor Squadron, 21st Air Division, at Griffiss Air Force Base, New York.

After the Convair Delta Dart was retired from active service, 58-0787 was sent to the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.

This F-106A (S/N 58-0787) was involved in an unusual incident. During a training mission, it entered an flat spin forcing the pilot to eject. Unpiloted, the aircraft recovered on its own and miraculously made a gentle belly landing in a snow-covered field. (U.S. Air Force photo)
Convair F-106A Delta Dart 58-0787 sits in a snow-covered Montana farm field, February 1970. (U.S. Air Force)

The Convair F-106A Delta Dart was the primary all-weather interceptor of the United States Air Force from 1959 to 1988, when it was withdrawn from service with the Air National Guard. It was a single-seat, single-engine delta-winged aircraft capable of speeds above Mach 2.

The airplane was a development of the earlier F-102A Delta Dagger, and was initially designated F-102B. However, so many changes were made that it was considered to be a new aircraft.

The F-106A is 70 feet, 8.78 inches (21.559 meters) long with a wingspan of 38 feet, 3.5 inches (11.671 meters). The total area of the delta wing is 697.83 square feet (64.83 square meters). The angle of incidence was 0° and there was no dihedral. The leading edges were swept aft 60°. The top of the vertical fin was 20 feet, 3.3 inches (6.180 meters) high. The Delta Dart weighs 24,028 pounds (10,899 kilograms) empty, and has a maximum takeoff weight (MTOW) of 39,195 pounds (17,779 kilograms).

Convair F-106A Delta Dart three-view illustration with dimensions. (SDASM)

The F-106 was powered by a Pratt & Whitney J75-P-17 afterburning turbojet engine. The J75-P-17 was a two-spool axial-flow turbojet engine with afterburner. It used a 15-stage compressor section (8 high- and 7 low-pressure stages) and a 3-stage turbine section (1 high- and 2-low pressure stages). The J75-P-17 had a maximum continuous power rating of 14,100 pounds of thrust (62.72 kilonewtons), and military power rating of 16,100 pounds (71.62 kilonewtons) (30-minute limit). It produced a maximum of 24,500 pounds (108.98 kilonewtons) with afterburner (5-minute limit). The engine was 3 feet, 8.25 inches (1.124 meters) in diameter, 19 feet, 9.6 inches long (6.035 meters), and weighed 5,875 pounds (2,665 kilograms).

Convair F-106A Delta Dart 58-0787 sits in a snow-covered Montana farm field, February 1970. (U.S. Air Force)

The interceptor has a cruise speed of 516 knots (594 miles per hour/956 kilometers per hour), and a maximum speed of 1,153 knots (1,327 miles per hour/2,135 kilometers per hour) at 35,000 feet (10,668 meters). The F-106A had a maximum rate of climb of 41,400 feet per minute (210 meters per second) at Sea Level. It could climb to 50,000 feet (15,240 meters) in 5 minutes. The service ceiling was 52,700 feet (16,063 meters). Its combat radius was 426 nautical miles (490 statute miles/789 kilometers) with maximum internal fuel (1,514 U.S. gallons/5,731 liters). The maximum ferry range was 1,571 nautical miles (1,808 statute miles/2,909 kilometers), when carrying an additional 454 gallons (1,719 liters) in two external tanks.

A Convair F-106A Delta Dart launches a Genie air-to-air rocket. (U.S. Air Force)
A Convair F-106A-135-CO Delta Dart, 59-0146, of the 194th Fighter Interceptor Squadron, California Air National Guard, launches an AIM-2 Genie air-to-air rocket. (U.S. Air Force)

The Delta Dart was armed with four GAR-3A radar-homing, or -4A (AIM-4F, -4G) infrared-homing Falcon air-to-air guided missiles, and one MB-1 (AIM-2A) Genie unguided rocket with a 1.5 kiloton W-25 nuclear warhead. The missiles were carried in an internal weapons bay. In 1972, the General Electric M61A1 Vulcan 20mm cannon was added to the rear weapons bay with 650 rounds of ammunition. (The number of gun-equipped Delta Darts is uncertain.)

Convair built 342 F-106 interceptors. 277 were F-106As and the remainder were F-106B two-seat trainers.

Convair F-106A-100-CO Delta Dart 58-0787 in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force)
Convair F-106A-100-CO Delta Dart 58-0787 in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force)

© 2024, Bryan R. Swopes

26 December 1956

Convair Chief Test Pilot Richard Lowe Johnson. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Convair Chief Test Pilot Richard Lowe Johnson. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

26 December 1956: Convair’s Chief Test Pilot, Richard Lowe Johnson (1917–2002) made the first flight of the Convair F-106A-1-CO Delta Dart, U.S. Air Force serial number 56-451, at Edwards Air Force Base in the high desert of southern California. It reached 30,000 feet (9,144 meters) and 0.8 Mach during the 20-minute flight, which had to be aborted due to mechanical problems.

Convair F-106A-1-CO Delta Dart 56-451 makes its first flight at Edwards AFB 26 December 1956. (U.S. Air Force)

Built at the Convair Division of General Dynamics at San Diego, California, the delta-winged interceptor was trucked to Edwards on 14 December and prepared for its first flight.

Convair F-106A Delta Dart 56-451 was loaded on a trailer at the Convair plant in San Diego, California, 14 December 1956, to be transported to Edwards Air Force Base for its first flight. (SDASM)

The Convair F-106A Delta Dart was the primary all-weather interceptor of the United States Air Force from 1959 to 1988, when it was withdrawn from service with the Air National Guard. It was a single-seat, single-engine delta-winged aircraft capable of speeds above Mach 2.

The airplane was a development of the earlier F-102A Delta Dagger, and was initially designated F-102B. However, so many changes were made that it was considered to be a new aircraft.

Convair F-106A-1-CO Delta Dart 56-451 during a test flight near Edwards Air Force Base, California. It is marked with high-visibility orange paint. (U.S. Air Force)

The F-106A is 70 feet, 8.78 inches (21.559 meters) long with a wingspan of 38 feet, 3.5 inches (11.671 meters). The total area of the delta wing is 697.83 square feet (64.83 square meters). The angle of incidence was 0° and there was no dihedral. The leading edges were swept aft 60°. The top of the vertical fin was 20 feet, 3.3 inches (6.180 meters) high. The Delta Dart weighs 23,646 pounds (10,726 kilograms) empty, and has a maximum takeoff weight (MTOW) of 38,729 pounds (17,567 kilograms).

Convair F-106A Delta Dart three-view illustration with dimensions. (SDASM)
Convair F-106A-1-CO Delta Dart 56-451, at Edwards Air Force Base. (U.S. Air Force via F-106DeltaDart.com)

The F-106 was powered by a Pratt & Whitney J75-P-17 afterburning turbojet engine. The J75-P-17 was a two-spool axial-flow turbojet engine with afterburner. It used a 15-stage compressor section (8 high- and 7 low-pressure stages) and a 3-stage turbine section (1 high- and 2-low pressure stages). The J75-P-17 had a maximum continuous power rating of 14,100 pounds of thrust (62.72 kilonewtons), and military power rating of 16,100 pounds (71.62 kilonewtons) (30-minute limit). It produced a maximum of 24,500 pounds (108.98 kilonewtons) with afterburner (5-minute limit). The engine was 3 feet, 8.25 inches (1.124 meters) in diameter, 19 feet, 9.6 inches long (6.035 meters), and weighed 5,875 pounds (2,665 kilograms).

Convair F-106A-1-CO Delta Dart 56-451 landing at Edwards Air Force Base, California. (U.S. Air Force)

The interceptor has a cruise speed of 530 knots (610 miles per hour/982 kilometers per hour). and a maximum speed of 1,153 knots 1,327 miles per hour/2,135 kilometers per hour) at 35,000 feet (10,668 meters). The F-106A had a service ceiling is 53,800 feet (16,398 meters) and a rate of climb of 48,900 feet per minute (248 meters per second). Its combat radius was 530 nautical miles (610 statute miles/982 kilometers) and the maximum ferry range was 1,843 nautical miles (2,121 statute miles/3,413 kilometers).

Convair F-106A-1-CO Delta Dart 56-451 landing at Edwards Air Force Base, California. (SDASM)
Convair F-106A-1-CO Delta Dart 56-451 with a drag chute deployed to slow the airplane after landing at Edwards Air Force Base, California. (SDASM)

The Delta Dart was armed with four GAR-3A radar-homing, or -4A (AIM-4F, -4G) infrared-homing Falcon air-to-air guided missiles, and one MB-1 (AIM-2A) Genie unguided rocket with a 1.5 kiloton W-25 nuclear warhead. The missiles were carried in an internal weapons bay. In 1972, the General Electric M61A1 Vulcan 20mm cannon was added to the rear weapons bay with 650 rounds of ammunition. (The number of gun-equipped Delta Darts is uncertain.)

Convair F-106A-1-CO Delta Dart 56-451 at Edwards Air Force Base, California. (U.S. Air Force via F-106DeltaDart.com)

Convair built 342 F-106 interceptors. 277 were F-106As and the remainder were F-106B two-seat trainers.

56-451, the first F-106A to fly, was transferred to the National Museum of the United States Air Force in 1960. In 1989, it was transferred to Selfridge Air Museum, near Mount Clemens, Michigan, marked as 59-0082 of the 171st Fighter Interceptor Squadron, Michigan Air National Guard.

The first F-106, Convair F-106A-1-CO Delta Dart, 56-451, in the markings of the 171st Fighter Interceptor Squadron, Michigan Air National Guard, displayed at the Selfridge Military Air Museum, Selfridge Air National Guard Base, Mount Clemens, Michigan. (TSGT Robert Hanet/Air National Guard 121013-Z-NJ721-180)
Convair Chief Test Pilot Richard Lowe Johnson in the cockpit of an F-106A Delta Dart. (SDASM)

Richard Lowe Johnson ¹ was born at Cooperstown, North Dakota, 21 September 1917. He was the eighth of nine children of Swedish immigrants, John N. Johnson, a farmer, and Elna Kristina Helgesten Johnson, a seamstress.

Dick Johnson attended Oregon State College at Corvallis, Oregon, as a member of the Class of 1943. He was a member of the Sigma Alpha Epsilon (ΣΑΕ) fraternity. Johnson was a pitcher for the college baseball team, and later, played for the Boston Red Sox “farm” (minor league) system.

On 18 June 1942, Johnson enlisted as a private in the Air Corps, United States Army. On 5 November, he was appointed an aviation cadet and assigned to flight training.

Aviation Cadet Johnson married Miss Juanita Blanche Carter, 17 April 1943, at Ocala, Florida. The civil ceremony was officiated by Judge D. R. Smith.

After completing flight training, on 1 October 1943, Richard L. Johnson was commissioned as a second lieutenant, Army of the United States (A.U.S.).

Lieutenant Johnson was assigned to the 66th Fighter Squadron, 57th Fighter Group, Twelfth Air Force, in North Africa, Corsica, and Italy, flying the Republic P-47 Thunderbolt. He was promoted to first lieutenant, A.U.S., 9 August 1944, and just over three months later, 26 November 1944, to the rank of captain, A.U.S. On 14 May 1945, Captain Johnson was promoted to the rank of major, A.U.S. (Major Johnson was assigned a permanent rank of first lieutenant, Air Corps, United States Army, on 5 July 1946, with a date of rank retroactive to 21 September 1945.)

Republic P-47D-25-RE Thunderbolt 42-26421, assigned to the 66th Fighter Squadron, 57th Fighter group, Twelfth Air Force. This airplane was purchased by the employees of Republic Aviation. (American Air Museum in Britain UPL 25505)

During World War II, Major Johnson flew 180 combat missions with the 66th Fighter Squadron. He is officially credited with one air-to-air victory, 1 July 1944. Johnson was awarded the Silver Star, the Distinguished Flying Cross with two oak leaf clusters (3 awards), and the Air Medal with twelve oak leaf clusters (thirteen awards).

In 1946, was assigned to the Air Materiel Command Engineering Test Pilot School at the Army Air Forces Technical Base, Dayton, Ohio (Wright-Patterson Air Force Base). He was the second U.S. Air Force pilot to be publicly acknowledged for breaking the “sound barrier.”

A few weeks after arriving at Dayton, Major Johnson met Miss Alvina Conway Huester, the daughter of an officer in the U.S. Navy. Dick Johnson and his wife Juanita were divorced 8 January 1947, and he married Miss Huester in a ceremony in Henry County, Indiana, 10 January 1947. They would have three children, Kristie, Lisa and Richard.

Richard L. Johnson waves from the cockpit of the record-setting North American Aviation F-86A-1-NA Sabre, 47-611.

Dick Johnson set a Fédération Aéronautique Internationale (FAI) World Record Speed Over a 3 Kilometer Course,² flying the sixth production North American Aviation F-86A-1-NA Sabre, serial number 47-611, at Muroc Air Force Base, California (renamed Edwards AFB in 1949).

During the Korean War, Major Johnson was sent to the war zone to supervise field installations of improvements to the F-86 Sabre. He was “caught” flying “unauthorized” combat missions and was sent home.

Convair YF-102 Delta Dagger 52-7994. (U.S. Air Force)

Lieutenant Colonel Johnson resigned from the Air Force in 1953 to become the Chief Test Pilot for the Convair Division of General Dynamics. He made the first flights of the YF-102 Delta Dagger, 24 October 1953, and the F-106A Delta Dart, 26 December 1956. He also made the first flight of the General Dynamics F-111A on 21 December 1964.

In 1955, Johnson was one of the six founding members of the Society of Experimental test Pilots.

Dick Johnson made the first flight of the General Dynamics F-111A, 63-9766, from Carswell Air Force Base, Fort Worth, Texas, 21 December 1964. (U.S. Air Force)

Dick Johnson was Chief Engineering Test Pilot for the General Dynamics F-111 “Aardvark.” In 1967, the Society of Experimental Test Pilots awarded Johnson its Iven C. Kincheloe Award for his work on the F-111 program. In 1977, Dick Johnson, then the Director of Flight and Quality Assurance at General Dynamics, retired.

In 1998, Dick Johnson was inducted into the Aerospace Walk of Honor at Lancaster, California. His commemorative monument is located in front of the Lancaster Public Library on W. Lancaster Boulevard, just West of Cedar Avenue. ³

Lieutenant Colonel Richard Lowe Johnson, United States Air Force, (Retired), died 9 November 2002 at Fort Worth, Texas. He was buried at Arlington National Cemetery, Arlington, Virginia, on 7 January 2003.

Chief Test Pilot Dick Johnson in the cockpit of a Convair B-58A Hustler. (Courtesy if Neil Corbett, Test and Research Pilots, Flight Test Engineers)

¹ Several sources spell Johnson’s middle name as “Loe.”

² FAI Record File Number 9866

³ Various Internet sources repeat the statement that “Richard Johnson has been honored with. . . the Thompson Trophy, Mackay Trophy, Flying Tiger Trophy, Federation Aeronautique Internationale Gold Medal and Golden Plate Award of the American Academy of Achievement. . . .” TDiA has checked the lists of awardees of each of the appropriate organizations and has not found any support for the statement.

© 2018, Bryan R. Swopes