Tag Archives: Trainer

7 December 1941

Cornelia Clark Fort, with a Fairchild PT-19A Cornell trainer. (U.S. Air Force)
Cornelia Clark Fort, with a Fairchild PT-19A Cornell trainer. (U.S. Air Force)

7 December 1941: Cornelia Clark Fort was an instructor in the Civilian Pilot Training Program at John Rodgers Airport, near Honolulu on the island of Oahu, Territory of Hawaii. Early on this Sunday morning, she and a student, a Mr. Suomala, were practicing touch-and-goes at John Rodgers Airport in an Interstate Cadet, NC37345, a two-place light airplane owned by the local flying club.¹

Shortly before 8:00 a.m., Miss Fort saw a silver military-type airplane approaching her Cadet at high speed. She took over the flight controls from Mr. Suomala and put the trainer into a steep climb. The other airplane flew directly under, close enough that she felt the vibrations of its engine. She saw that its wings carried the “rising sun” insignia of the Empire of Japan.

Fort landed the Cadet at John Rogers Airport, which was being attacked by Japanese airplanes. Another trainer on the ground was destroyed by machine gunfire and its instructor killed.

A page from Cornelia Fort’s pilot logbook with her remarks for December 7, 1941. (Texas Women’s University)
A page from Cornelia Fort’s pilot logbook with her remarks for December 7, 1941. (Texas Women’s University)

Fort’s logbook entry for 7 December 1941 reads: “Cadet, 37345, Cont. 65—Flight interrupted by Japanese attack on Pearl Harbor. An enemy airplane shot at my airplane and missed and proceeded to strafe John Rodgers, a civilian airport. Another airplane machine-gunned the ground in front of me as I taxied back to the hangar.” The logbook shows her total accumulated flight time at the end of this flight as 893 hours, 25 minutes.

Cornelia Clark Fort. (Tennessee State Library and Archives)
Cornelia Clark Fort. (Tennessee State Library and Archives)

Cornelia Clark Fort was born into an affluent family in Nashville, Tennessee, 5 February 1919, the fourth of five children of Dr. Rufus Elijah Fort and Louise Clark Fort. Her father was a prominent surgeon who co-founded the National Life and Accident Insurance Company. The family lived at Fortland, an estate east of Nashville.

Cornelia Clark Fort. (1936 Milestones)

Cornelia attended the Ward-Belmont School in Nashville, then studied at the Ogontz School in Philadelphia. (Amelia Earhart had also attended Ogontz.) In 1937, Miss Fort transferred to Sarah Lawrence College, Yonkers, New York, where she studied Literature. She graduated 10 June 1939.

After taking a flight with a friend, Jack Caldwell, in January 1940, she pursued an interest in aviation, starting flight lessons the following day. She had earned her pilot certificate and flight instructor certificate by June 1940, which made her the first woman to become an instructor at Nashville. With the Civilian Pilot Training Program, she first went to Fort Collins, Colorado, where she taught for about three months, then went on to Honolulu.

Pilots of the Women's Auxiliary Ferrying Squadron at Long Beach Army Airfield, 1943. Left to right, Barbara Towne, Cornelia Clark Fort, Evelyn Sharp, Barbara Erickson and bernice Batten. The airplane is a Vultee BT-13 Valiant. (Texas Women's University)
Pilots of the Women’s Auxiliary Ferrying Squadron at Long Beach Army Airfield, 7 March 1943. Left to right, Barbara Towne, Cornelia Clark Fort, Evelyn Sharp, Barbara Erickson and Bernice Batten. The airplane is a Vultee BT-13 Valiant. (Texas Women’s University)

Following the attack on Pearl Harbor, all civilian aircraft were grounded. Cornelia Fort was able to return to the mainland United States in early 1942. In September she was one of the first 25 women accepted into the Women’s Auxiliary Ferrying Service. She was assigned to the 6th Ferrying Group based at Long Beach, California.

Cornelia Clark Fort’s military identification card. (Nashville Public Library)

On 21 March 1943, while ferrying a new Vultee BT-13A Valiant basic trainer, serial number 42-42432, from the factory at Downey, California, to an airfield in Texas, her left wing was struck from behind by another airplane. With its wing damaged, the BT-13 rolled over and entered an inverted dive. It crashed approximately 10 miles (16 kilometers) south of Merkel, Texas, and Cornelia Fort was killed.

Cornelia Clark Fort was the first female pilot killed while on active military duty. She was 24 years old.

Air & Space/Smithsonian quoted from a letter written by Fort in a January 2012 article:

“I dearly loved the airports, little and big. I loved the sky and the airplanes, and yet, best of all I loved the flying. . . I was happiest in the sky at dawn when the quietness of the air was like a caress, when the noon sun beat down, and at dusk when the sky was drenched with the fading light.”

—Cornelia Clark Fort, 1942.

Interstate Cadet S-1A NC34939, s/n 34, the same type airplane flown by Cornelia Fort on 7 December 1941.

The trainer flown by Cornelia Fort and her student on the morning of 7 December 1941 was a Cadet S-1A, serial number 188, built by the Interstate Aircraft and Engineering Company, El Segundo, California. It was a high-wing monoplane with a tandem cockpit. The fuselage of the Cadet was built of a welded tubular steel framework. The wings had two spruce spars with Alclad metal ribs. The leading edges were covered in Dural sheet and the complete wing then covered in doped fabric. The wing support struts were made of tubular steel. The S-1A was 24 feet, 0 inches (7.315 meters) long with a wingspan of 35 feet, 6 inches (10.820 meters) and height of 7 feet, 3 inches (2.210 meters). The airplane had an empty weight of 720 pounds (327 kilograms) and maximum weight of 1,200 pounds (544 kilograms).

The Interstate Cadet S-1A was powered by an air-cooled, normally-aspirated 171.002-cubic-inch-displacement (2.802 liter) Continental A65-8 horizontally-opposed four cylinder direct-drive engine, with a compression ratio of 6.3:1. It was rated at 65 horsepower at 2,300 r.p.m. at Sea Level, using 73-octane gasoline. The engine turned a two-bladed fixed-pitch wooden propeller with a diameter of 6 feet, 4 inches (1.930 meters).

The Cadet S-1A had a maximum speed of 103 miles per hour (166 kilometers per hour) in level flight, and 139 miles per hour (224 kilometers per hour) in a dive. The service ceiling was 14,500 feet (4,420 meters). The S-1A’s fuel capacity was 15 gallons (57 liters). Its maximum range was approximately 350 miles (563 kilometers).

Approximately 320 Cadets were built by Interstate in 1941–1942. They were sold for $2,095. With the onset of World War II, Interstate switched production to the L-6 Grasshopper.

The fuselage frame, c/n 188, is owned by a retired airline pilot, Kent Pietsch, who owns and has restored four other Cadets.

Interstate Cadet S-1A
Interstate Cadet S-1A NC37266, flown by Greg Anders. (Wikipedia)

¹ Greg Anders, Director of The Heritage Flight Museum, Burlington, Washington, owns an Interstate Cadet that he believes was the one flown by Cornelia Fort on 7 December 1941. It carried the registration number NC37266. In an article in Air & Space Magazine, November 2016, he stated that he believes that Fort’s logbook is actually a copy, and that Fort incorrectly listed NC37345.

© 2018, Bryan R. Swopes

6 October 1961

Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)

6 October 1961: During a two-month series of speed, distance and altitude record attempts at Edwards Air Force Base, California, Jackie Cochran set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 100 Kilometers Without Payload, flying a Northrop T-38A-30-NO Talon, 60-0551. Her average speed over the 62-mile circular course was 1,262.188 kilometers per hour (784.287 miles per hour).¹

Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)
Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)

Jackie’s friend, famed Air Force test pilot Colonel Chuck Yeager, kept notes during the series of record attempts:

September 29: Edwards AFB. Flew the aircraft today to include a practice run on the 100 kilometer course. Jackie did a fine job at 1.2 Mach. Looks like this will be a piece of cake. Aircraft was okay. Average speed 742 miles per hour. Jackie was in the altitude chamber today with the pressure suit (CSU 4/P). Everything went fine and maximum altitude was 65,000 feet. This is the first time a woman was taken up in the chamber in a pressure suit. CSU 4/P was the type of suit.

October 3: Tried a run today but weather moved in from 26,000 to 37,000 feet. Very good landing. Airspeed system iced up and Jackie stalled the aircraft at 35,000 feet. Made a no-sweat recovery.

October 4: Ran the 100 kilometer for record at 1 pm. The first run wasn’t too good but had an average speed of 763 mph. A pylon was cut so the run was voided. Second run was 740 mph. Very poor. Another flight was made at 5:30 pm but both runs were pretty sorry. Jackie was a little late on all of the corrections. Jackie doesn’t seem to be in too good a physical or mental state.

October 5: I flew in the backseat of the T-38 with Jackie on a practice run of the 100 kilometer. I talked her around the course 2 times with a little help on the stick. First run was 782 mph and second run was 787. I think I know what has been Jackie’s trouble on the 100 km. During the flight as she starts gaining a little altitude, she lets off on the back pressure on the stick to stop climbing and this causes the turn to become larger. Jackie and I spent two hours talking this over. She finally understands that in order to fly a constant circle, if the airplane starts to climb, she must increase the bank angle and let off on the back pressure a little and let the nose drop but still hold the same rate of turn. This is what makes the 100 km so hard to fly. Jackie still has a touch of the flu.

October 6: Jackie felt better today and after a delay caused by communication trouble, she flew one of the most perfect runs that has ever been flown on the 100 km course. She learned her lesson well. The record speed was 784 mph. She held 1/4 mile outside the course the entire trip. I was very pleased to watch the reaction of the timers and radar people. I think they expected another 10 or 15 trips like the F-105 tricks. She made one hell of a good flight.

— Brigadier General Charles E. Yeager, U.S. Air Force, quoted in Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, Pages 306–307.

Jackie Cochran and Chuck Yeager at Edwards Air Force Base, California, after a flight in the record-setting Northrop T-38A Talon. (U.S. Air Force)
Jackie Cochran and Chuck Yeager at Edwards Air Force Base, California, after a flight in the record-setting Northrop T-38A Talon. (U.S. Air Force)

The Northrop T-38A Talon is a two-place, twin-engine jet trainer capable of supersonic speed. It is 46 feet, 4 inches (14.122 meters) long with a wingspan of 25 feet, 3 inches (7.696 meters) and overall height of 12 feet, 10 inches (3.912 meters). The trainer’s empty weight is 7,200 pounds (3,266 kilograms) and the maximum takeoff weight is 12,093 pounds (5,485 kilograms).

The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).

Northrop T-38A-30-NO Talon at Edwards Air Force Base, California. (U.S. Air Force)

It has a maximum speed of Mach 1.08 (822 miles per hour, 1,323 kilometers per hour) at Sea Level. The Talon’s service ceiling of 55,000 feet (16,764 meters) and it has a maximum range of 1,093 miles (1,759 kilometers).

In production from 1961 to 1972, Northrop has produced nearly 1,200 T-38s. As of January 2014, the U.S. Air Force had 546 T-38A Talons in the active inventory. It also remains in service with the U.S. Navy, and the National Aeronautics and Space Administration.

Jackie Cochran’s record-setting T-38 is in the collection of the Smithsonian Institution, National Air and Space Museum.

Northrop T-38A Talon 60-0551, now twenty-one years old, sits on the ramp at the Sacramento Air Logistics Center, McClellan Air Force Base, Sacramento, California, 1981. (Photograph by Gary Chambers, used with permission)
Northrop T-38A Talon 60-0551, now twenty-one years old, sits on the ramp at the Sacramento Air Logistics Center, McClellan Air Force Base, Sacramento, California, 1981. (Photograph by Gary Chambers, used with permission)

¹ FAI Record File Number 13036

© 2017, Bryan R. Swopes

26 September 1949

XT-28 48-1471 landing at Edwards AFB 3 Feb 1950
The first of two North American Aviation  XT-28 prototypes, 48-1371, lands at Edwards Air Force Base 3 February 1950. (U.S. Air Force)

26 September 1949: At Vultee Field, a private industrial airport in Downey, California, North American Aviation test pilot Jean LeRoy (“Skip”) Ziegler ¹ took the first of two prototype military flight trainers, the XT-28 (NAA Model 159–2), U.S. Air Force serial number 49-1371, for its first flight. The 45-minute flight was two weeks ahead of schedule.

The Long Beach Press-Telegram reported:

New Training Plane Tested

     LOS ANGELES, Sept 27. (AP) The Air Force’s first postwar training plane—North American’s T-28—has tried her wings and found they work very well.

     The company announced that the twin cockpit craft—designed to train pilots for advanced high speed fighters and bombers—flew 45 minutes yesterday. Said test pilot Skip Ziegler, “It handles more like a fighter than a trainer.” He termed the flight, “completely satisfactory.”

     The T-28 has a ceiling of 29,800 feet and can move 288 miles an hour. The T-6, present Air Force trainer, ceilings at 22,000 and travels 205 m.p.h. top.

Long Beach Press Telegram, Vol. LXII, No. 240, Tuesday, 27 September 1949, Page A-5, Column 1

One of the two North American Aviation XSN2J-1 prototypes in flight of the Southern California shoreline, circa 1946. (North American Aviation, Inc./San Diego Air & Space Museum Archives, Catalog #: 00033269)

The XT-28 was developed from an earlier North American Aviation project for the United States Navy. In 1946, NAA proposed their Model 142, as a replacement for the World War II SNJ/T-6 Texan, a trainer which had also been built by North American, and used by  both the Navy and the U.S. Army Air Forces. The Navy designated the proposed airplane XSN2J-1. Two were built and assigned Bureau of Aeronautics serial numbers (“Bu. No.”) 121449 and 121450. 121449 was the first to fly, 15 February 1947.

The Navy tested both aircraft, but did not order them into production.

One of the two North American Aviation XSN2J-1 prototypes during testing at NATC Patuxent River, Maryland, October 1948. The prototype is armed with with five-inch air-to-surface rockets. (National Archives and Records Administration)

A year later, NAA made a similar proposal to the United States Air Force. The Air Force wanted a trainer to transition pilots into turbojet-powered aircraft. Similar to the XSN2J-1, the XBT-28 was changed to tricycle landing gear, a first for a miltiary trainer. The prototype’s two cockpits were laid out very similar to the new, swept-wing North American XP-86 Sabre. The Air Force ordered the airplane into production as the T-28A. The first T-28A arrived at Eglin Air Force Base, Florida, 15 June 1950, where it would tested for suitability as a flight trainer.

Prototype North American Aviation XBT-28. (T-28 Trojan Foundation)

The North American Aviation T-28 Trojan is an all-metal, two-place airplane with retractable tricycle landing gear. The dual cockpits are arranged in tandem. The T-28A was used by the United States Air Force as a primary training aircraft, while the more powerful T-28B and T-28C were employed by the U.S. Navy. The airplane was noted for its stability and handling qualities, its easy recovery from stalls and spins, and its excellent visibility.

Initially, the T-28 was built at North American Aviation’s Downey Division, in Downey, California, which at the time was primarily a farming community about 13 miles (21 kilometers) south of downtown Los Angeles, California. Production was shifted to North America’s Columbus Division in Columbus, Ohio.

North American Aviation T-28A Trojan internal arrangement. (U.S. Air Force)

The XT-28 and production T-28As were 32.0 feet (9.754) long with a wingspan of 40.6 feet (12.375 meters), and overall height of 12.7 feet (3.871 meters). The wing had an angle of incidence of 2° with 3° of negative twist, and 8° dihedral. The total wing area was 268.0 square feet (24.9 square meters). The vertical fin was offset 1° to the left of the airplane’s centerline. The prototype and early production T-28As had an empty weight of had an empty weight of 6,909 pounds (2,998 kilograms). This was increased in later aircraft to 7,282 pounds (3,303 kilograms). The Maximum Takeoff Weight (MTOW) was 7,751 pounds (3,516 kilograms).² The two prototypes had a belly-mounted speed brake. All T-28As had provisions for this installation.

North American Aviation XT-28 three-view illustration with dimensions. (U.S. Air Force)

The XT-28 and production T-28A were powered by an air-cooled, supercharged, 1,301.868 cubic inch (21.334 liter) Wright Aeronautical Division Cyclone 7 R-1300-1 (853C7BA1) 7-cylinder radial engine with a compression ratio of 6.2:1. This engine required 91/98 octane aviation gasoline. It was rated at 700 horsepower at 2,400 r.p.m., and 800 horsepower at 2,600. r.p.m. for takeoff. The engine also produced some jet thrust from its exhaust system. The engine thrust line was angled downward 5° from fuselage reference line. The R-1300-1 drove a two blade, 10 foot, 0 inch (3.048 meters) diameter Aeroproducts hydraulic variable pitch propeller through 0.5625:1 gear reduction. The engine was 4 feet, 1.12 inches (1.248 meters) long, 4 feet, 2.45 inches (1.281 meters) in diameter, and weighed 1,065 pounds, (483 kilograms).

The XT-28 had a maximum fuel capacity of 125 gallons (473 liters), carried in two wing tanks. Two additional tanks were added to later production T-28As, increasing the capacity to 177 gallons (670 liters).

The T-28A had a cruise speed of 165 knots (190 miles per hour/306 kilometers per hour, and maximum speed of 247 knots (284 miles per hour/457 kilometers per hour) at 5,800 feet (1,768 meters). VNE varied from 190 knots (219 miles per hour/352 kilometers per hour) at 25,000 feet (7,620 meters) with external load, to 340 knots (391 miles per hour/630 kilometers per hour) at Sea Level, clean. The airplane’s best power off glide speed was 105 knots (120 miles per hour/194 kilometers per hour).

The T-28A could climb at a maximum rate of 1,870 feet per minute (9.5 meters per second). Its service ceiling was 24,000 feet (7,315 meters). The maximum range was 720 nautical miles (829 statute miles/1333 kilometers) in early production models, or 880 nautical miles (1,013 statute miles/1,630 kilometers) in aircraft with increased fuel capacity.

For training purposes, the T-28A could be armed with one detachable gun pod under each wing. Each pod contained a .50-caliber AN-M3 Browning Aircraft Machine Gun. These had a rate of fire of approximately 1,100 rounds per minute. Each gun was supplied with 100 rounds of ammunition. The trainer could also be equipped with a removable bomb rack for a 100-pound (45 kilogram) bomb. Three 2.25 inch (5.7 centimeters) Sub-Caliber Aerial Rocket (SCAR)—Rocket, 2.25-Inch Practice—rockets could be carried on pylons mounted to hardpoints under each wing.

The first production North American T-28A Trojan, 49-1494 (North American serial number 159-1), at the National Museum of the United States Air Force. Delivered to Wright-Patterson AFB, this aircraft was used as a static test airframe. (U.S. Air Force 050322-F-1234P-020)

A total of 1,948 T-28s were built from 1950 to 1957. 1,194 of these were T-28As. The Air Force retired its T-28As by 1959. Many USAF T-28As were pulled from storage at Davis-Monthan Air Force Base, Tucson, Arizona, and were converted to the T-28D configuration for combat operations during the Vietnam War. Others were converted to the AT-28D attack variant, which included an ejection seat.

North American Aviation test pilot Robert A. (“Bob”) Hoover, with a U.S. Navy T-28B Trojan, circa 1953. (National Museum of Naval Aviation)

XT-28 48-1371 was sent to “The Boneyard” at Davis-Monthan Air Force Base near Tucson, Arizona, 23 January 1961, and to reclamation, 18 June 1965. In 1974, it was observed, disassembled, at the Hamilton Aviation Company yard in Tucson. (Hamilton produced modified T-28s: the military T-28R-1, and the civilian T-28R-2 Nomair.)

¹ For biographical information about Skip Ziegler, please see “This Day in Aviation” for 12 Nay 1953 at: https://www.thisdayinaviation.com/12-may-1953/

© 2025, Bryan R. Swopes

18 September 1961

Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, California, 1961. (U.S. Air Force)

18 September 1961: Jackie Cochran, acting as a test pilot and consultant for Northrop Corporation, set a Fédération Aéronautique Internationale (FAI) World Record for Distance when she flew the Northrop T-38A-30-NO Talon, 60-0551, from Palmdale, California, to Minneapolis, Minnesota, a distance of 2,401.780 kilometers (1,492.397 miles).¹

Jacqueline Cochran's Diplôme de Record in teh San Diego Air and Space Museum Archives. (Bryan R. Swopes)
Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)

Jackie’s friend, famed Air Force test pilot Colonel Chuck Yeager, kept notes during the series of record attempts:

September 18: Jackie took off from Palmdale at 10:00 am for attempt to set records from points to points. I took off from Edwards with 275-gallon [1,041 liter] drop tanks. During climb Jackie reported rough engine and poor performance. Also the fuel flow was inoperative. Jackie returned to the field where I finally found her takeoff flaps were still down. Also her navigation lights and beacon were on. I was rather disappointed. She’s a little cocky in the airplane. She landed back there at Palmdale with 1500 pounds [680 kilograms] of fuel in each side and made a good heavy-weight landing. The aircraft refueled and another takeoff was made at 12:30 pm. Everything went smooth this flight. We ran into clouds at the edge of Utah which lasted until Cheyenne, Wyo. Clear the rest of the way. Jackie landed with 250 pounds of fuel in each side. Made a beautiful landing and turned off after a 4000 foot [1,220 meters] ground roll. Bob White returned the F-100 to Edwards.

—  Brigadier General Charles Elwood (“Chuck”) Yeager, U.S. Air Force, quoted in Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, Pages 306.

Jackie Cochran and Chuck Yeager at Edwards Air Force Base, California, after a flight in the record-setting Northrop T-38A Talon. (U.S. Air Force)
Jackie Cochran and Chuck Yeager at Edwards Air Force Base, California, after a flight in the record-setting Northrop T-38A Talon. (U.S. Air Force) 

The Northrop T-38A Talon is a two-place, twin-engine jet trainer capable of supersonic speed. It is 46 feet, 4 inches (14.122 meters) long with a wingspan of 25 feet, 3 inches (7.696 meters) and overall height of 12 feet, 10 inches (3.912 meters). The trainer’s empty weight is 7,200 pounds (3,266 kilograms) and the maximum takeoff weight is 12,093 pounds (5,485 kilograms).

The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).

Northrop T-38A-30-NO Talon at Edwards Air Force Base, California. (U.S. Air Force)

It has a maximum speed of Mach 1.08 (822 miles per hour, 1,323 kilometers per hour) at Sea Level. The Talon’s service ceiling of 55,000 feet (16,764 meters) and it has a maximum range of 1,093 miles (1,759 kilometers).

In production from 1961 to 1972, Northrop has produced nearly 1,200 T-38s. As of January 2014, the U.S. Air Force had 546 T-38A Talons in the active inventory. It also remains in service with the U.S. Navy, and the National Aeronautics and Space Administration.

Jackie Cochran’s record-setting T-38 is in the collection of the Smithsonian Institution, National Air and Space Museum.

Northrop T-38A Talon 60-0551, now twenty-one years old, sits on the ramp at the Sacramento Air Logistics Center, McClellan Air Force Base, Sacramento, California, 1981. (Photograph by Gary Chambers, used with permission)
Northrop T-38A Talon 60-0551, now twenty-one years old, sits on the ramp at the Sacramento Air Logistics Center, McClellan Air Force Base, Sacramento, California, 1981. (Photograph by Gary Chambers, used with permission)

¹ FAI Record File Number 12383

© 2017, Bryan R. Swopes

23 May 2000

Beechcraft T-6A Texan II primary trainer. (Master Sgt. David Richards, U.S. Air Force)
Beechcraft T-6A Texan II primary trainer. (Master Sgt. David Richards, U.S. Air Force)

23 May 2000: The United States Air Force received its first Beechcraft T-6A Texan II primary trainer at Randolph Air Force Base, San Antonio Texas. It is  a militarized version of the Pilatus PC-9. The cockpit has a full digital “glass cockpit” instrument panel and is equipped with ejection seats for the student and instructor.

The Texan II is named after the World War II-era North American Aviation AT-6 Texan, which was the advanced trainer used by the United States military from 1940 to 1955. The T-6A is used as a primary trainer by both the U.S. Air Force and the U.S. Navy.

The Texan II is a two-place, single engine low-wing monoplane with retractable tricycle landing gear. It is 33 feet, 4 inches (10.160 meters) long with a wingspan of 33 feet, 5 inches (10.185 meters) and height of 10 feet, 8 inches (3.251 meters). It has an empty weight of 4,707 pounds (2,135 kilograms), gross weight of 6,300 pounds (2,858 kilograms) and maximum takeoff weight of 6,500 pounds (2,948 kilograms).

The airplane is powered by a Pratt & Whitney Canada PT6A-68 turboprop engine which produces 1,100 shaft horsepower and drives a 4-bladed Hartzell propeller.

The Texan II has a cruise speed of 320 miles per hour (515 kilometers per hour), service ceiling of 31,000 feet (9,449 meters) and range of 1,036 miles (1,667 kilometers).

Flight of two Beechcraft AT-6 Texan II trainers. (U.S. Air Force)
Flight of two Beechcraft AT-6 Texan II trainers. (U.S. Air Force)

© 2017, Bryan R. Swopes