SF-37 (SH-37)
Tactical Reconnaissance plane

	Specification:
	Year deployed Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - maximum take-off Engine Thrust, kN - dry - afterburner Maximum speed, km/h - in altitude - on sea level Range, km Service ceiling, m Crew Armament:	- 1973 - 10.60 - 16.40 - 5.80 - 46.00 - 12000 - 20500 - 1 рдд Volvo Flygmotor RM-8A (Pratt & Whitney JT-8D-22) - 65.70 - 115.52 - 2360 - 1450 - 3000 - 18000 - 1 2 AAM Rb.24 (AIM-9B Sidewinder)