Tag Archives: First Flight

27 July 1972

Irving L. Burrows prepares for teh first flight of the pre-production YF-15A-1-MC Eagle air superiority fighter at Edwards Air Force Base, California.
Irving L. Burrows prepares for the first flight of the pre-production YF-15A-1-MC Eagle air superiority fighter at Edwards Air Force Base, California. (U.S. Air Force)

27 July 1972: McDonnell Douglas Chief Experimental Test Pilot Irving L. Burrows made the first flight of the prototype YF-15A-1-MC Eagle, 71-0280, at Edwards Air Force Base, California.

Irving L. Burrows
Irving L. Burrows

The F-15A Eagle is a single-seat, twin-engine air superiority fighter, built by the McDonnell Douglas Corporation at St. Louis, Missouri. The fighter has outstanding acceleration and maneuverability. It is 63 feet, 9 inches (19.431 meters) long, with a wingspan of 42 feet, 9.75 inches (13.049 meters) and overall height of 18 feet, 7.5 inches (5.677 meters).

The first pre-production prototype McDonnell Douglas F-15 Eagle, YF-15A-1-MC 72-0280, on its first flight near Edwards Air Force Base, California, 27 July 1972. (U.S. Air Force)

The wings’ leading edges are swept to 45°. The angle of incidence is 0°. The wings have 1° anhedral. The total wing area is 608 square feet (56.5 square meters).

The F-15A has an empty weight of 25,780 pounds (11,694 kilograms), and maximum takeoff weight of 44,497 pounds (20,184 kilograms).

McDonnell Douglas YF-15A-1-MC Eagle 71-0280, with a McDonnell Douglas RF-4C Phantom II chase plane, in flight near Edwards AFB. (U.S. Air Force)

The fighter was powered by two Pratt & Whitney JTF22A-25A (F100-PW-100) turbofan engines. The F100 is a two-spool, axial-flow afterburning 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 has a maximum continuous power rating of 12,410 pounds of thrust (55.20 kilonewtons) and intermediate rating of 14,690 pounds (65.34 kilonewtons), (30 minute limit). Its maximum power rating is 23,840 pounds (106.05 kilonewtons) with afterburner (5 minute limit). The F100-PW-100 is  16 feet, 4.3 inches (4.986 meters) long, 3 feet, 10.5 inches (1.181 meters) in diameter, and weighs 3,179 pounds (1,442 kilograms).

An early production McDonnell Douglas F-15A-8-MC Eagle, 73-0090, at Luke Air Force Base, Arizona. The fighter is painted “air superiority blue.” (U.S. Air Force)

The Eagle is a Mach 2.5+ fighter. The cruise speed of the F-15A Eagle is 502 knots (578 miles per hour/930 kilometers per hour). It has a maximum speed of 1,434 knots (1,650 miles per hour/2,656 kilometers per hour) at 45,000 feet (13,716 meters)—Mach 2.503. The service ceiling is 63,050 feet (19,218 meters). It can climb 67,250 feet per minute (342 meters per second), and with a thrust-to-weight ratio of 1.15:1, the fighter could climb straight up.

The The F-15A’s combat radius is 638 nautical miles (734 statute miles/1,182 kilometers). Its maximum ferry range is 2,362 nautical miles (2,718 statute miles/4,374 kilometers).

A McDonnell Douglas F-15 Eagle over the White Sands Missile Range banks away from the camera to display its air-to-air missile armament, 1 May 1980.. (Technical Sergeant Frank Garzelnick, U.S. Air Force)

The F-15A is armed with one General Electric M61A1 Vulcan 20mm rotary cannon with 938 rounds of ammunition, four AIM-7F Sparrow radar-guided missiles and four AIM-9E/L Sidewinder infrared-homing missiles. The fighter could also carry a variety of bombs.

There were 12 pre-production F-15 aircraft, serial numbers 71-0280–71-0291. 384 F-15A fighters were built from 1972 to 1979, before production switched to the improved F-15C. The last F-15A Eagle in U.S. Air Force service, F-15A-19-MC 77-0098, was retired from the Oregon Air National Guard, 16 September 2009.

The last McDonnell Douglas F-15A Eagle in U.S. Air Force service. F-15A-19-MC 77-0098, prepares for its final flight from Portland, Oregon, to Davis-Monthan AFB, 16 September 2009. The pilot was LCOL Steve Beauchamp, 123rd Fighter Squadron, 142nd Fighter Wing, Oregon Air National Guard. (U.S. Air Force) 09016-F-8260H-184

The first YF-15A, 71-0280, is on display at Lackland Air Force Base, Texas.

© 2018, Bryan R. Swopes

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18 July 1942

Test pilot Fritz Wendel with the Messerschmitt Me 262 V3 prototype, PC+UC. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Chief Test Pilot Fritz Wendel with the Messerschmitt Me 262 V3 prototype, PC+UC. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Test Pilot Fritz Wendel (L) talks with Willy Messerschmitt after the maiden flight of Me 262 V3.
Test Pilot Fritz Wendel (left) talks with Willy Messerschmitt after the maiden flight of Me 262 V3, 18 July 1942.

18 July 1942: (25 March 1942???) In the late 1930s, Germany began developing a fighter powered by a turbojet engine. In early 1942 the first two prototypes of the Messerschmitt Me 262 began flight testing. They had two BMW 003 jet engines mounted on the wings, but for safety, a piston engine and propeller were mounted in the nose.

At 8:40 a.m. on 18 July 1942, V3, the third prototype, call sign PC+UC, made the first pure-jet flight when it took off from Leipheim, Bavaria, with Messerschmitt’s Chief Test Pilot, Flugkapitän Fritz Wendel.

This prototype was powered by two Junkers Jumo 004 turbojet engines. The Jumo 004 had an eight-stage axial flow compressor, six straight through combustion chambers and a single-stage turbine. It produced 1,850 pounds of thrust (8.23 kilonewtons).

Messerschmitt Me 262 V3, PC+UC, takes off on its first flight at Leipheim, 18 July 1942.
Messerschmitt Me 262 V3, PC+UC, takes off on its first flight at Leipheim, 18 July 1942.

There were problems created by the airplane’s use of a tailwheel configuration. Turbulence from the wings and reflected jet exhaust blanked out the tail surface. When the Me 262 prototype reached flying speed, Wendel tapped the brakes. The tail popped up, free of the turbulence, and the jet fighter took off. Beginning with the fifth prototype, V5, all Me 262s were built with tricycle landing gear.

Messerschmitt Me 262 V3, PC+UC
Messerschmitt Me 262 V3, PC+UC

1,430 Me 262s were produced. They entered service during the summer of 1944. Luftwaffe pilots claimed 542 Allied airplanes shot down with the Me 262.

© 2016, Bryan R. Swopes

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17 July 1989

Bruce J. Hinds and Richard Couch. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

17 July 1989: The first Northrop B-2A Spirit, 82-1066, took off from Air Force Plant 42, Palmdale, California, on its first flight. The crew was Northrop Chief Test Pilot Bruce J. Hinds and Colonel Richard Couch, U.S. Air Force. The top secret “stealth bomber” prototype landed at Edwards Air Force Base 1 hour, 52 minutes later.

After completing the flight test program, -1066 was placed in storage until 1993, awaiting upgrade to the Block 10 operational configuration. In 2000 it was again upgraded to the Block 30 standard. It is now named Spirit of America and assigned to the 509th Bomb Wing at Whiteman Air Force Base, Missouri.

Northrop B-2A Spirit, 82-1066, the first “stealth bomber,” during a test flight. (U.S. Air Force)

© 2015, Bryan R. Swopes

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17 July 1965

North American Aviation XB-70A-2-NA 62-0207 takes off for the first time at AF Plant 42, 17 July 1965. (U.S. Air Force)

17 July 1965: At Air Force Plant 42, Palmdale, California, the second North American Aviation B-70 Valkyrie prototype, XB-70A-2-NA 62-0207, took off on its maiden flight enroute Edwards Air Force Base where it would continue the flight test program with its sister ship.

The Valkyrie was designed as a Mach 3+ strategic bomber, capable of flight above 70,000 feet (21,336 meters), with intercontinental range. It’s altitude allowed it to avoid interceptors of the time, but improvements in radar-guided surface-to-air missiles increased its vulnerability. Ultimately, though, political decisions ended the B-70 program.

62-0207 was flown just 46 times, for a total of 92 hours, 22 minutes of flight. Changes to the aircraft corrected the deficiencies discovered in testing the Number 1 XB-70A, 62,-201. The most visible change was 5° dihedral added to the wings for improved stability. On 16 April 1966, 62-0207 reached its maximum design speed, Mach 3.08, which it sustained for 20 minutes.

Less than one year after its first flight, 8 June 1966, the Valkyrie was involved in a mid-air collision with a Lockheed F-104N and crashed just north of Barstow, California. North American’s B-70 test pilot, Al White, was seriously injured and co-pilot, Major Carl Cross, USAF, was killed. NASA test pilot Joe Walker, flying the F-104, was also killed.

© 2015, Bryan R. Swopes

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15 July 1954

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

© 2020, Bryan R. Swopes

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