Sikorsky Black Hawk UH-60A, Max. Operating Weight 15,976 – 16,803 lbs. Max. Take-Off Weight 22,000 lbs. , Cruise Speed 139 – 145 kts at 4,000 ft and 95 F, VNE Speed 193 kts, Service Ceiling 19,000 ft
Sikorsky Black Hawk UH-60A, Max. Operating Weight 15,976 – 16,803 lbs. Max. Take-Off Weight 22,000 lbs. , Cruise Speed 139 – 145 kts at 4,000 ft and 95 F, VNE Speed 193 kts, Service Ceiling 19,000 ft
General Electric T700-GE-700 (2); Max. Continuous Power 1,318 shp per engine Main Rotor: Articulated, main rotor head consisting of titanium hub, elastomeric bearings, lead-lag dampers, and passive vibration absorbers; Ballistically tolerant, main rotor blades (4) constructed from titanium and composite materials Tail Rotor: Tail rotor head consisting of flex beams, and elastomeric bearings; Ballistically tolerant, tail rotor blades (4) constructed from titanium and composite materials Aux. Power Unit (APU): Honeywell GTCP36-150[BH]