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General Info

Consolidated / Convair
Vultee BT-13 Valiant

Role Trainer
Manufacturer  Vultee Aircraft
First flight March 1939
Introduction June 1940
Primary users United States Army Air Forces
United States Navy
Number built 9,525

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History Consolidated / Convair
Vultee BT-13 Valiant



The Vultee BT-13 Valiant is an American World War II-era basic (a category between primary and advanced) 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

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Design and development

Vultee BC-3 prototype in flight

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 continued 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 (or, more commonly, a constant-speed propeller). It did not, however, have retractable landing gear nor a hydraulic system. The flaps were operated by a crank-and-cable system. Its pilots nicknamed it the "Vultee Vibrator."

Variants

BT-15
SNV-2

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-13AAs 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-16One 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 United States Army Air Corps. SNV-2
BT-13Bs for the United States Navy, 650 transferred from United States Army Air Corps.
T-13ASurviving 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.

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General characteristics

  • Crew: 2
  • Length: 27 ft 9.25 in (8.4646 m)
  • Wingspan: 34 ft 5.5 in (10.503 m)
  • Height: 9 ft 10 in (3.00 m)
  • Wing area: 284 sq ft (26.4 m2)
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Powerplant

  • 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)
  • Propellers: 2-bladed Hamilton-Standard 2-position
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Specifications

  • Maximum speed: 180 mph (290 km/h, 160 kn)
  • Range: 725 mi (1,167 km, 630 nmi)
  • Service ceiling: 21,650 ft (6,600 m)
  • Time to altitude: 9.2 minutes to 10,000 ft (3,000 m)
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Armament

  • None: 

 Wiki Link

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Special Links Consolidated / Convair Vultee

Links to Youtube & Others

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Consolidated Vultee Vultee VT-13 Valiant

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Youtube Link

The Consolidated PT-1 Trusty (company designation Model 1) was a biplane primary trainer used by the United States Army Air Service (USAAS)

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