Duran, Terry L (2007). „UH-60 Black Hawk”. Barron's Military Flight Aptitude Tests (на језику: (језик: енглески)). Barron's Educational Series. стр. 64. ISBN978-0-7641-3517-0. Приступљено 31. октобар 2010. „Description: Two-engine, medium lift, four-bladed, utility helicopter • Mission/branches: Air assault, utility airlift, aeromedevac, command and control; U.S. Army, Air Force, Navy • Crew: Up to four: pilot, copilot, crew, chief/flight engineer, door gunner • Length: 64 ft., 10 in. (19.7 m) • Height: 16 ft., 10 in. (5.1 m) • Rotor diameter: 53 ft., 8 in. (16.3 m) • Empty weight 11,516 lb. (5,234.5 kg) • Max gross weight 22,000 lb. (10,000 kg) • Maximum speed: Up to 165 mph (150 knots) • Maximum altitude: 11,125 ft. (3,400 m) • Maximum range: 362 miles (315 nm) • Powerplant(s): Two GE T700-GE-701C generating 2,000 + shp each • Payload capacity: 9,000 lb. (4,090 kg) • Armament: Two M60D 7.62 mm machine guns • Manufacturer: Sikorsky Aircraft Corp. • Variants: UH-60L (attack), UH-60Q (aeromedevac), MH-60G Pave Hawk (USAF special operations), MH-60K (Army special operations) ”CS1 одржавање: Непрепознат језик (веза)
