PZL-130 TURBO ORLIK
Training 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 AFT Engine Power, kW Maximum speed, km/h Cruising speed, km/h Combat range, km Service ceiling, m Crew Armament:	- 1992 - 9.00 - 9.00 - 3.53 - 13.00 - 1600 - 2000 - 2700 - 540 - 2 У 340 - 1 TE  Motorlet (Walter) M 601E - 1 У 559 - 501 - 454 - 970 - - 2 Warload - 800 kg in 6 hardpoints 100 kg bombs, ML UV-8-57 8У55-mm or UV-4-80 4У80-mm, pod Zeus c 2 7.62-mm machine-guns.