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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. |
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Developing nation: |
Switzerland /
USA. |
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Designer: |
Pilatus Aircraft
AG. |
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Manufacturer: |
Raytheon Aircraft
Company . |
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Production line: |
Wichita, Kansas,
USA. |
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Task: |
High-performance
military turboprop trainer. |
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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. |
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First delivery: |
May 23,
2000 to the USAF. |
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Raytheon T-6A
Texan II |
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Crew: |
2. |
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Ejection seat: |
Martin-Baker
Mk.16LA. |
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Wing Span: |
10,19 m. |
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Wing Area: |
16,29 mē. |
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Length: |
10,13 m. |
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Height: |
3,26 m. |
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Wheel track: |
2,54 m. |
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Engines: |
One Pratt &
Whitney Canada PT6A-68 turboprop rated 1.274 kW. |
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Propeller: |
Four-blade
Hartzell constant - speed, diameter: 2,44 m.
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Weight: |
- Empty: 2.085 Kg.
- Internal
fuel: 621 liters.
- External
fuel: 2 x 248 liters.
- Max.
ordnance: 1.415 Kg. |
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Max. take off weight: |
3.500 Kg. |
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Cruise speed: |
426 km/h at 2.285
m. |
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Max. speed: |
574 km/h
at 6.100 m.
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Service ceiling: |
10.670 m. |
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Range: |
- range 1.574 km
without drop tanks.
max. endurance 3
hours. |
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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. |
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g limits: |
-3.5 / +7. |
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Underwing
hardpoints: |
6. |
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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:
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August 31, 2000
95-3008/RA T-6A 559th FTS USAF.
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April 3,
2004 ? /MY T-6A 39th FTS
USAF.
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Raytheon T-6A
Texan II operators: |
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Canada, NATO
Flight Training (Bombardier): |
- 26 CT-156. |
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Greece: |
- 45 T-6A. |
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United States of
America. |
- 454 T-6A USAF.
- 328 T-6A US
Navy. |
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Raytheon. |
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3 T-6A
prototypes.
- 1 T-6B
prototype. |
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