The Blackhawk (UH-60) is a twin turbine engine, single rotor, modular fuselage, rotary wing helicopter. The main rotor system has four rotor blades. The drive train consists of a main transmission, intermediate gear box, and tail rotor gear box with interconnecting shafts. The non-retractable landing gear consists of the main landing gear and a tail wheel. The aircraft has redundancy for Hydraulic, Electrical and Pneumatic systems.
 Maximum Forward Airspeed: 193 Knots Wet Weight, 165 Knots at 22,000 lbs
 Maximum Lift Weight: 22,000 lbs
 Maximum Sling Load Weight: 8000 lbs
 Maximum Performance Vertical Take-Off: 2000 ft per minute
 274 mi or 441 km on one tank of fuel (361 gal)