ял.170 MAGISTER
Trainer and combat aircraft

	Specification:	CM.170-1	CM.170-2	CM.175
	Year deployed Wing span, m - with tanks on wingtips Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal without tanks - normal with tanks - maximum take-off Internal fuel, l - internal - in external tanks Engine Thrust dry, kN Maximum speed, km/h - in altitude - in sea level Range, km Combat radius, km Endurance, h - with tanks - with standart fuel Rate of climb, m/min Service ceiling, m Crew	- 1956 - 11.40 - 12.15 - 10.06 - 2.80 - 17.30 - 2150 - 2850 - 3100 - 3200 - 730 - 2 x 250 or 2 x 460 - 2 Turbomeca Marbore IIA - 3.92 - 715 - 650 - 1200 - 925 - 2.40 - 1.55 - 1020 - 11000 - 2	- 1964 - 11.40 - 12.15 - 10.06 - 2.80 - 17.30 - 2310 - 2850 - 3100 - 3260 - 730 - 2 x 250 or 2 x 460 - 2 Turbomeca Marbore VI - 4.71 - 725 - 700 - 1400 - 910 - 2.40 - 1.55 - 1200 - 12000 - 2	- 1960 - 11.40 - 12.15 - 10.06 - 2.80 - 17.30 - 2350 - 3200 - 3350 - 3400 - 730 - 2 x 250 or 2 x 460 - 2 Turbomeca Marbore II - 3.92 - 649 - 630 - 1200 - 925 - 2.40 - 1.55 - 900 - 11000 - 2

Armament:

2 7.62-mm or 7.50-mm machine-gun with 200 rounds Warload - 140 kg in 2 hardpoints ML 18x37-mm or 6x68 or 9x81-mm UR, or 2 50-kg bombs, or 2 ASM  AS.11