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Raytheon BE3000 T-6A Texan II
The T-6A is based on the Pilatus PC-9M, but was subjected to many modifications to meet the US JPATS requirements.
The T-6B features an advanced avionics system from CMC/Flight Visions with three large colour displays and a head-up-display.
General Crew: 2 in tandem on Martin-Baker Mk 16LA ejection seats
Performance Max. level speed: 574 km/h at altitude, 500 km/h IAS at low level Max. cruise speed: 426 km/h at 2285 m (7500 ft) Approach speed: 185 km/h Stall speed: 152 km/h with power off and flaps up Rate of climb: 20 m/s at sea level, or 15,7 m/s according to the USAF Time to climb to 18000 ft: les than 6 minutes Service ceiling: 10670 m(35000 ft) Take-off run: 437 m Take-off to 15 m: 655 m Landing distance from 15 m: 1030 m (was 732 m) Landing run: 740 m (was 580 m) Range: 1574 km at altitude Endurance: 3 h Endurance 3 hg limits: +7/-3,5 Service life: 18720 flight hours
Weights Weight empty: 2136 kg (was 2087 kg) or 2950 kg standard basic empty weight according to the USAF Baggage capacity: 36 kg (was 54 kg) Max. fuel: 499 kg, 621 litres Max. underwing stores: 1415 kg Max. zero-fuel weight: 2495 kg Max. ramp weight: 2971 kg Max. take-off weight: 2950 kg (up from 2857 kg)
Dimensions Length: 10,14 m Height: 3,26 m Span: 10,15 m Wing area: 16,3 sq m Wing aspect ratio: 6,3
Weapons:
Provision for three hardpoints under each wing. Testing was conducted for the following loads:
- 2 x 12,5 mm gun pods (HMP-400)
- 2 x fuel tanks
- 6 x BDU-33, 25 kg practice bombs
- 2 x Mk.82, 225 kg bombs
- 2 gun pods, 2 rocket launchers and 2 BDU-33s