UH-60 Black Hawk
Overview
The Sikorsky UH-60 Black Hawk is the U.S. Army’s primary medium-lift utility helicopter, developed to replace the UH-1 Huey. The prototype first flew on 17 October 1974 and entered Army service in 1979. Twin General Electric T700 engines and a four-blade main rotor support troop transport, medevac, logistics, and special operations worldwide.
Typical configurations carry a crew of three to four and about 11 troops or equivalent cargo. Representative figures include a length of about 64 ft 10 in and a main rotor diameter of about 53 ft 8 in; speed and range vary by sub-variant and load. This page covers the Army utility Black Hawk family and is distinct from the Navy MH-60R Seahawk maritime multi-mission helicopter.
Quick Facts
Specifications
| ICAO Type Code | H60 |
|---|---|
| Military Designation | UH-60 |
| First Flight | Oct 17, 1974 |
| Crew | 3-4 |
| Length | 64 ft 10 in |
| Wingspan / Rotor Diameter | 53 ft 8 in |
| Height | 16 ft 10 in |
| Empty Weight | 11624 lb |
| Max Takeoff Weight | 22000 lb |
| Cruise Speed | 150 kt |
| Max Speed | ~183 mph |
| Range | ~320 nm |
| Service Ceiling | 19000 ft |
| Engine Manufacturer | General Electric |
| Engine Model | T700 |
| Engine Count | 2 |
Data verification status: Verified
Source: Lockheed Martin / Sikorsky – UH-60 Black Hawk