Last site update: 03-10-2008

 

         

 

  

 

Raytheon T-6 Texan II

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Raytheon T-6 Texan II

On June 22, 1995 a considerably redesigned version of the Pilatus PC-9 was declared the winner of the JPATS (Joint Primary Aircraft Training System) competition to select a standard training aircraft type to be used by both the USAF and US Navy. Approximately 780 aircraft in total will be required under this program, built under license as the Raytheon T-6A Texan II. The T-6A's are to replace USAF T-37B and USN T-34C trainer aircraft. Raytheon T-6A Texan II deliveries continuing to 2017.

The T-6A Texan II offers better performance and significant improvements in training effectiveness, safety, cockpit accommodations and operational capabilities than present aircraft. Powered by a single, Pratt & Whitney PT6A-68 turboprop engine with a four-blade propeller, it features a stepped-tandem, cockpit configuration, with the instructor's rear seat raised slightly to improve visibility from the rear cockpit; modern avionics; and improved egress systems. Both T-6A cockpits are covered by a single, side-opening, non-jettisoned canopy. The T-6A offers increased bird strike protection over current training aircraft, and will improve the safety of landing and low-level training at Air Force and Navy bases. It has a pressurized cockpit to permit training at higher, less-congested altitudes and reduce the stress on student pilots. The aircraft is equipped with an onboard oxygen-generating system that reduces the time needed to service the aircraft between flights.

 

Raytheon T-6B Texan II

 

The Raytheon T-6B Texan II features an advanced avionics system from CMC/Flight Visions with three large color displays and a head-up-display. The T-6B has six wing-mounted hardpoints and each wing can carry 680 kg of weapons and fuel tanks.

 

 

Developing nation: Switzerland / USA.
Designer:  Pilatus Aircraft AG.
Manufacturer: Raytheon Aircraft Company .
Production line: Wichita, Kansas, USA.
Task: High-performance military turboprop trainer.
First flight:

- T-6A prototype December 23, 1992, N8284M.

- T-6A production aircraft July 15, 1998, serial 95-3003.

- T-6B May 12, 2004 N3000B.

First delivery: May 23, 2000 to the USAF.
  Raytheon T-6A Texan II
Crew: 2.
Ejection seat: Martin-Baker Mk.16LA.
Wing Span: 10,19 m.
Wing Area: 16,29 mē.
Length: 10,13 m.
Height: 3,26 m.
Wheel track: 2,54 m.
Engines:

One Pratt & Whitney Canada PT6A-68 turboprop rated 1.274 kW.

Propeller: Four-blade Hartzell constant - speed, diameter: 2,44 m.
Weight:

- Empty: 2.085 Kg.

- Internal fuel: 621 liters.

- External fuel: 2 x 248 liters.

- Max. ordnance: 1.415 Kg.

Max. take off weight: 3.500 Kg.
Cruise speed: 426 km/h at 2.285 m.
Max. speed: 574 km/h at 6.100 m.
Service ceiling: 10.670 m.
Range:

- range 1.574 km without drop tanks.

max. endurance 3 hours.

Performance:

- max. rate of climb at sea level 1.247 m per minute.

- climb to 5.000 m in 6 minutes.

- take-off run 437 m at normal take-off weight.

- landing run 740 m at normal landing weight.

g limits: -3.5 / +7.
Underwing hardpoints: 6.
Weapons:

- 2 x 12,5 mm gun pods (HMP-400).
- 6 x BDU-33, 25 kg practice bombs.
- 2 x Mk.82, 225 kg bombs.

- 2 rocket launchers.

                                                        

 

 

Raytheon T-6A Texan II written-off by accidents:

 

  • August 31, 2000    95-3008/RA    T-6A    559th FTS    USAF.

  • April 3, 2004               ?    /MY    T-6A      39th FTS    USAF.

 

 

Raytheon T-6A Texan II operators:

Canada, NATO Flight Training (Bombardier):

- 26 CT-156.

Greece: - 45 T-6A.
United States of America.

- 454 T-6A USAF.

- 328 T-6A US Navy.

Raytheon. - 3 T-6A prototypes.

- 1 T-6B prototype.

 

 

 

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