The fly-by-wire digital glass cockpit comes with multi-functional displays from Rockwell Collins Ī four-axis fully coupled flight director (autopilot) a H-764G dual embedded GPS inertial navigation (aka dual EGI) system from Honeywell ĪN/AMS-2 integrated stormscope LN-200 inertial measurement unit from Northrop Grumman ĪN/ARC-231 Airborne Communication System from Raytheon The Black Hawk has two sliding cargo doors with pop-out egress windows, two jettisonable cockpit doors, and a three point dual OLEO landing gear with 'kneeling' capability. The aircraft can tolerate small arms fire and most high-explosive, medium-caliber (23mm) ammunition. The UH-60M has four wide-chord composite rotor blades, foldable main and tail rotor blades, foldable tail pylon and stabilatorĭual redundant and isolated flight controls, and dual crashworthy and self-sealing fuel tanks. The UH-60 can be fitted with stub wings to carry additional fuel tanks or weapons. It is also capable of carrying external loads of up to 9,000 lbs. The Black Hawk is designed to carry a crew of four and a combat equipped The older UH-60L is powered by the less powerful 1,890 shp T700-GE-701C. The latest configuration, the UH-60M, is powered by two General Electric T700-GE-701D turboshaft engines with 1,994 shp each. The Sikorsky UH-60 Black Hawk is a four-bladed, single-rotor, medium-lift, utility By Forecast International /// The following is a snapshot of the UH-60 program.įor complete data and a forecast outlook, please view our Rotorcraft Forecast.
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