T-1
Trainer and combat aircraft

	Specification:
	Year deployed Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal take-off - maximum take-off Internal fuel, l - internal - AFT Engine Thrust dry, kN Maximum speed, km/h - in altitude - on sea level - cruising Range, km Combat radius, km Rate of climb, m/min Service ceiling, m Crew Armament:	- 1961 - 10.49 - 12.12 - 4.08 - 22.22 - 2420 - 4150 - 5000 - 1400 - 2 x 455 - 1 TJE Rolls-Royce Orpheus BOr.3 Mk 805 - 17.79 - 925 - 859 - 620 - 1860 - 1300 - 1981 - 14400 - 2 1 12.7-mm cannon Browning M53-2 with 200 rounds Warload -  680 kg  in 2 hardpoints 2 AAM AIM-9 Sidewinder or 2 340-kg or 227-kg bombs napalm tanks, or 4 127-mm UR, or 2 ML 7x70-mm UR, or 2 pods with 12.7-mm cannon.