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T-6B Texan II Turboprop Trainer

 
Description
The T-6B Texan II is a tandem-seat, turboprop trainer whose primary mission is to train Navy and Marine Corps pilots.
 
Features
The T-6B Texan II is an upgraded avionics variant of the T-6A Texan II and one component of the Joint Primary Aircraft Training System (JPATS) along with simulators, computer-aided academics, and a Training Integration Management System (TIMS). The joint program, of which the Air Force acts as the executive service, will replace Navy T-34C aircraft. The program uses commercial-off-the-shelf (COTS) subsystems to the maximum extent possible. The T-6 aircraft-built by Hawker Beechcraft Aircraft Company is a derivative of the Swiss Pilatus PC-9 aircraft with a Pratt & Whitney PT-6A-68 engine, Martin-Baker ejection seats, cockpit pressurization, and an onboard oxygen-generating system. The T-6B upgraded avionics provide an all-glass cockpit using three 5x7 multifunction displays, head-up display, hands-on throttle and stick, dual redundant Integrated Avionics Computers and an open-architecture design to allow for future growth. The Navy's total T-6B requirement is 252 aircraft.

The T-6 entered development flight test in July 1998. The FAA approved type and production certification for the T-6A aircraft and production line on 30 July 1999. A successful flight test program and a successful Milestone III full rate production decision followed in December 2001. Both the U.S. Air Force and U.S. Navy have since entered into a full rate production contract with Hawker Beechcraft for aircraft. In April 2007, the Navy began procuring an upgraded avionics variant of the Texan II, the T-6B, for primary pilot training. The U.S. Navy has received 140 aircraft to date and the system when fully fielded will be operational at two Navy bases. The T-6B achieved initial operating capability (IOC) in April 2010 at Naval Air Station Whiting Field, Fla.

The Navy aircraft and ground-based training systems will be completely supported and maintained by commercial vendors with intermediate maintenance provided for selected systems at the operating site.
 
Point Of Contact
Naval Air Systems Command
PEO (T) Public Affairs Officer
47123 Buse Road, Bldg. 2272, Rm. 454
Patuxent River, MD 20670-1547
(301) 757-7171
 
General Characteristics
Primary Function: All-purpose jet trainer.
Contractor: Hawker Beechcraft Aircraft Company.
Date Deployed: First flight, July 10, 2009; Operational, April 19, 2010.
Propulsion: One Pratt & Whitney Canada PT-6A-68 turboprop engine; 1,100 horsepower.
Length: 33.3 feet (10.12 meters).
Height: 10.8 feet (3.29 meters).
Wingspan: 33.4 feet (10.18 meters).
Weight: Empty, 5,850 pounds (2,653.52 kg.); maximum takeoff weight, 6,900 pounds (3,129.79 kg.).
Airspeed: 270 knots at 1,000 feet level flight.
Ceiling: 31,000 feet (9,448.8 meters).
Range: Maximum, 900 nautical miles (1,666.8 km).
Crew: Two (instructor pilot, student pilot).
 
Last Update: 4 October 2016