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Beechcraft T-6 Texan II

Role Trainer aircraft
National origin United States
Manufacturer Beechcraft Textron Aviation
First flight 15 July 1998 
Introduction 2001
Status In production
Primary users United States Air Force United States Navy Royal Canadian Air Force Hellenic Air Force
Produced 2000–present
Number built 850+
Developed from Pilatus PC-9

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History Beech Aircraft Corporation
Beechcraft T-6 Texan II



The Beechcraft T-6 Texan II is a single-engine turboprop aircraft built by the Raytheon Aircraft Company (Textron Aviation since 2014). A trainer aircraft based on the Pilatus PC-9, the T-6 replaced the United States Air Force's Cessna T-37B Tweet and the United States Navy's T-34C Turbo Mentor during the 2010s.

The T-6A is used by the United States Air Force for basic pilot training and Combat Systems Officer (CSO) training, the United States Navy and United States Marine Corps for primary Naval Aviator training and primary and intermediate Naval Flight Officer (NFO) training, and by the Royal Canadian Air Force (CT-156 Harvard II designation), Greek Air Force, Israeli Air Force (with the "Efroni" nickname), and Iraqi Air Force for basic flight training. The T-6B is the primary trainer for U.S. student naval aviators (SNAs). The T-6C is used for training by the Mexican Air Force, Royal Air Force, Royal Moroccan Air Force, and the Royal New Zealand Air Force.

The Model 3000/T-6 is a low-wing cantilever monoplane with enclosed tandem seating for two. It is powered by a single Pratt & Whitney Canada PT6A-68 turboprop engine in tractor configuration with an aluminum, 97-inch (8.1 ft; 2.5 m), four-blade, constant-speed, variable pitch, non-reversing, feathering propeller assembly and has retractable tricycle landing gear. The aircraft is fitted with Martin-Baker Mark 16 ejection seats and a canopy fracturing system. 

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Aeromacchi Leonardo

Beech Aircraft Corporation
Beechcraft T-6 Texan II

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General Info

      • Crew: one
      • Capacity: one passenger
      • Length: 33 ft 4 in (10.16 m)
      • Wingspan: 33 ft 5 in (10.19 m)
      • Height: 10 ft 8 in (3.25 m)
      • Wing area: 177.5 sq ft (16.49 m2)
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Powerplant

      • Empty weight: 4,707 lb (2,135 kg)
      • Gross weight: 6,300 lb (2,858 kg)
      • Max takeoff weight: (2,948 kg)
      • Fuel capacity:  (677.5 liters, 1200 lb)
      • Powerplant: 1 × Pratt & Whitney Canada PT6A-68 turboprop, 1,100 shp (820 kW)
      • Propellers: 4-bladed Hartzell HC-E4A-2 Hub with E9612 blades, 8 ft 1 in (2.46 m) diameter
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Performance

  • Cruise speed: 320 mph (510 km/h, Never exceed speed:  (586 km/h, 
  • Range: 1,000 mi (1,700 km, 900 nmi)
  • Service ceiling: 31,000 ft (9,400 m)
  • g limits: +7.0g/−3.5g
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Armament

  • Roll rate: 450 °/sec
  • Maximum glide ratio: 1:7
  • Rate of climb: 16.59 m/s (3,266 ft/min) in acrobatic flight, 13.82 m/s (2,720 ft/min) in utility flight
  • Fuel flow: 57 L/h (15.1 US gal/h)
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The T-6A was introduced to Moody Air Force Base and Randolph Air Force Base in 2000–2001, and the Air Force awarded the full-rate T-6 production contract in December 2001.

Beechcraft Aircraft 
T+6A Texan II

The T-6 is a development of the Pilatus PC-9, modified by Beechcraft to enter the Joint Primary Aircraft Training System.

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Youtube Link

Learn all about the Aermacchi MB-339 with Curator of Aviation Eric Boehm.

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