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BT-13 Valiant
BT-13 Valiant
BT-13 Valiant in flight
Role Trainer
Manufacturer Vultee
Designer Richard Palmer
First flight March 1939
Primary users United States Army Air Forces
United States Navy
Number built 9,525

The Vultee BT-13 Valiant was an American World War II-era basic trainer aircraft built by Vultee Aircraft for the United States Army Air Corps, and later US Army Air Forces. A subsequent variant of the BT-13 in USAAC/USAAF service was known as the BT-15 Valiant, while an identical version for the US Navy was known as the SNV and was used to train naval aviators for the US Navy and its sister services, the US Marine Corps and US Coast Guard.

Design and development[]

The Vultee BT-13 was the basic trainer flown by most American pilots during World War II. It was the second phase of the three phase training program for pilots. After primary training in PT-13, PT-17, or PT-19 trainers, the student pilot moved to the more complex Vultee for basic flight training. The BT-13 had a more powerful engine and was faster and heavier than the primary trainer. It required the student pilot to use two way radio communications with the ground and to operate landing flaps and a two-position Hamilton Standard controllable pitch propeller. It did not, however, have retractable landing gear nor a hydraulic system. The large flaps are operated by a crank-and-cable system. Its pilots nicknamed it the "Vultee Vibrator."

Due to the demand for this aircraft, and others which used the same Pratt & Whitney engine, some were equipped with Wright powerplants of similar size and power built in 1941-42. The Wright-equipped aircraft were designated BT-15.

The Navy adopted the P&W powered aircraft as their main basic trainer, designating it the SNV. The BT-13 production run outnumbered all other Basic Trainer (BT) types produced.

It was back in 1938 that Vultee Aircraft's chief designer, Richard Palmer, began the design of a fighter. At this time the USAAC issued a requirement and design contest for an advanced trainer for which substantial orders had been promised to the victor. Palmer began to adapt his design concept from a fighter to that of an advanced trainer and the result of this was the V-51 prototype.

Vultee BC-3 prototype in flight c1940

Vultee BC-3 prototype in flight

The aircraft made its maiden flight on 24 March 1939[1] as a cantilever low-wing monoplane of all-metal construction. Despite the use of metal throughout the design the control surfaces remained fabric-covered. The prototype was powered by a Pratt & Whitney R-1340-S3H1-G Wasp radial rated at 600 hp (447 kW) driving a two-blade variable pitch metal propeller. Other features included an enclosed cockpit for the crew of two, integral fuel tanks in the wings, and a hydraulic system for the operation of the flaps and retractable main landing gear.

The V-51 was entered into the USAAC competition as the BC-51 during May 1939. The USAAC instead chose the North American BC-2, but purchased the BC-51 prototype anyway, designating it the BC-3. Despite the disappointment, Palmer was not finished yet. He continued to refine the design of the VF-51 into the VF-54 in an attempt to meet the expectation of an export market for just such a trainer. The VF-54 used the same basic airframe as the VF-51, but was fitted with a lower powered engine. No export sales were made.

From this design, evolved the VF-54A. Instead of retractable gear, it had fixed gear very nicely faired and a revised power plant of a Pratt & Whitney R-985-T3B Wasp Jr. radial rated at 450 hp (335.5 kW) and the Vultee BT-13 Valiant was born.

The USAAC was made aware of the improvements made to the aircraft and in August 1939 the type was ordered as the BT-13. The initial order was for 300 aircraft with a Pratt & Whitney R-985-25 radial and the first of these was accepted by the USAAC in June 1940.

Vultee BT-13A on runway at Minter Field (00910460 147)

Vultee BT-13 on runway at Minter Field, California, 1 March 1943.

The BT-13A was produced to the extent of 7,037 aircraft and differed only in the use of a Pratt & Whitney R-985-AN-1 radial engine and lack of landing gear fairings. There were 1,125 BT-13B's produced and differed from the A model in having a 24-volt, rather than the original 12-volt electrical system.

The next variant was actually designated BT-15 because Pratt & Whitney found it impossible to keep up production of the R-985 engine. Instead a Wright R-975-11 radial was substituted into the 1,263 aircraft produced.

The US Navy began to show an interest in the aircraft as well and ordered 1,150 BT-13A models as the SNV-1. In addition, the Navy ordered some 650 aircraft designated as SNV-2, roughly equivalent to the BT-13B.

Once in service, the aircraft quickly got its nickname of "Vibrator." There are several explanations given for this nickname. 1: Because it had a tendency to shake quite violently as it approached its stall speed. 2. During more adventurous maneuvers the canopy vibrated. 3. On takeoff, the aircraft caused windows on the ground to vibrate. 4. The two-position propeller had an irritating vibration in high pitch. The BT-13 served its intended purpose well. It and its successors were unforgiving aircraft to fly, but were also extremely agile. Thus the BT-13 made a good aircraft to help transition many hundreds of pilots toward their advance trainers and fighters yet to be mastered. The BT-13 was not without its faults. The tail was held on with only three bolts and after several in-flight failures, the Navy restricted the aircraft from aerobatic and violent maneuvers. The Navy declared the SNV obsolete in May 1945 and replaced it in the basic training role with the SNJ (AT-6). The Army also replaced the BT-13 with the AT-6 before the end of the war. After World War II, virtually all were sold as surplus for a few hundred dollars each. Many were purchased just to obtain their engines, which were mounted on surplus biplanes (such as Stearmans) to replace their less powerful engines for use as cropdusters. The BT airframes were then scrapped. Today, some "BT's" (collectively, BT-13s, BT-15s and SNVs) are still flying, though in very limited numbers (and none in military or government service).

Variants[]

Vultee BT-15

BT-15

BC-3
Vultee Model V.51 with retractable landing gear and a 600hp P&W R-1340-45, one built, not developed.
BT-13
Vultee Model V.54 with fixed undercarriage and a 450hp P&W R-985-25 engine, 300 built.
BT-13A
As BT-13 but fitted with a 450hp R-985-AN-1 engine and minor changes, 6407 built, survivors re-designated T-13A in 1948.
BT-13B
As BT-13A but with a 24-volt electrical system, 1125 built.
BT-15
As BT-13A with a 450hp Wright R-975-11 engine, 1693 built.
XBT-16
One BT-13A was re-built in 1942 by Vidal with an all-plastic fuselage as the XBT-16.
SNV-1
BT-13As for the United States Navy, 1350 transferred from USAAF.
SNV-2
BT-13Bs for the United States Navy, 650 transferred from USAAF.
T-13A
Surviving BT-13As were re-designated in 1948, due to dual allocation of T-13 with the PT-13 in practice they were still known as the BT-13 to avoid confusion.

Operators[]

Flag of Argentina Argentina
Flag of Bolivia Bolivia
Flag of Brazil Brazil
Flag of Chile Chile
Flag of the People's Republic of China China
Flag of Colombia Colombia
Flag of the Republic of China Republic of China (1912–1949)[3]
Flag of Cuba Cuba
Flag of the Dominican Republic Dominican Republic
Flag of Ecuador Ecuador
Flag of Egypt (1922–1958) Egypt
Flag of El Salvador El Salvador
Flag of France France
Flag of Guatemala Guatemala
Flag of Haiti Haiti
Flag of Honduras Honduras
Flag of Indonesia Indonesia
Flag of Israel Israel
Flag of Mexico Mexico[2]
Flag of Nicaragua Nicaragua
Flag of Panama Panama
Flag of Paraguay Paraguay[2]
  • Paraguayan Air Arm 10 BT-13A received through Lend-Lease 1942-1943. Two BT-13 bought in Argentina in 1947.
  • Paraguayan Naval Aviation Three BT-13 donated by Argentina in the 1960s.
Flag of Peru Peru
Flag of the Philippines Philippines[3]
Flag of the Soviet Union Soviet Union
US flag 48 stars United States
Flag of Venezuela Venezuela

Aircraft on display[]

  • Mid-Atlantic Air Museum, Reading, Pennsylvania - 1942 BT-13A Valiant
  • Castle Air Museum, Atwater, California
  • Combat Air Museum, Topeka, Kansas
  • Estrella WarBirds Museum, Paso Robles, California
  • Goodfellow Air Force Base, Texas
  • Jimmy Doolittle Air & Space Museum, Travis Air Force Base, Fairfield, California
  • Kalamazoo Air Zoo, Kalamazoo, Michigan
  • Museu Aeroespacial, Rio de Janeiro, Brazil
  • Maxwell Air Force Base Gunter-Annex, Alabama
  • National Museum of the United States Air Force, Dayton, Ohio
  • National Naval Aviation Museum, Pensacola, Florida
  • Museum Pusat TNI-AU Dirgantara Mandala, Jogjakarta, Indonesia
  • Ngurah Rai International Airport, Denpasar, Bali, Indonesia
  • Pima Air and Space Museum, Tucson, AZ. USA

Popular culture[]

Tora BT

N56478, a Tora! Tora! Tora! BT-15, "Val" at The Wings Over Houston Airshow October 2007

One notable post-war "variant" of the BT's are the "Tora" aircraft. In 1968 Twentieth Century Fox purchased nine BT-13/15 and modified them for use in the motion picture "Tora! Tora! Tora!". The "Val" dive bombers seen in this film are actually BT-13 and BT-15. The "Zero" fighters and "Kate" torpedo bombers are mostly Harvard IV's. After the film, these aircraft were sold to private owners. Many are still flying, several of them as part of the Commemorative Air Force's "Tora! Tora! Tora!" squadron, which performs air battle reenactments at air shows. Several "Tora" aircraft also appeared in the later "Pearl Harbor" film.

Specifications (BT-13A)[]

Data from United States Military Aircraft since 1909[5]

General characteristics

  • Crew: 2
  • Length: 28 ft 10 in (8.79 m)
  • Wingspan: 42 ft 0 in (12.80 m)
  • Height: 11 ft 6 in (3.51 m)
  • Wing area: 239 sq ft (22.2 m2)
  • Empty weight: 3,375 lb (1,531 kg)
  • Gross weight: 4,496 lb (2,039 kg)
  • Powerplant: 1 × Pratt & Whitney R-985-AN-1 nine-cylinder air-cooled radial engine, 450 hp (340 kW)

Performance

  • Maximum speed: 180 mph (290 km/h; 156 kn)
  • Range: 725 mi (630 nmi; 1,167 km)
  • Service ceiling: 21,650 ft (6,599 m)
  • Time to altitude: 9.2 minutes to 10,000 ft (3,000 m)

See also[]

Comparable aircraft:

References[]

  1. Wegg 1990, p. 158.
  2. 2.00 2.01 2.02 2.03 2.04 2.05 2.06 2.07 2.08 2.09 2.10 2.11 2.12 2.13 2.14 2.15 Wegg 1990, p. 139.
  3. 3.0 3.1 3.2 3.3 Wegg 1990, p. 160.
  4. Wegg 1990, pp. 159–160.
  5. Swanborough and Bowers 1963, p. 461.
  • Andersson, Lennart (2008). A History of Chinese Aviation: Encyclopedia of Aircraft and Aviation in China to 1949. Taipei, Republic of China: AHS of ROC. ISBN 978-957-28533-3-7. 
  • Swanborough, F. G.; Bowers, Peter M. (1963). U.S. Military Aircraft since 1909. London: Putnam. 
  • Wegg, John (1990). General Dynamics Aircraft and their Predecessors. London: Putnam Aeronautical Books. ISBN 0-85177-833-X. 

External links[]

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