| Specifications |
|---|
| Model |
UH-60A
|
| Manufacturer |
Sikorsky Aircraft |
| Folded Length (rotor/tail pylon) | 40 ft, 11in |
| Rotor folded length (pylon flight position) | 53 ft, 3 in |
| Length overall (rotors turning) | 64 ft, 10 in / 19.76m |
| Fuselage length | 50 ft / 15.26m |
| Height: (to top of rotor) head | 3.79m |
| Overall height, (tail rotor turning) | 17 ft / 5.18m |
| Fuselage width | 7 ft, 9 in / 2.36m |
| Folded width | 10 ft, 7 in |
| Main rotor diameter | 53 ft, 8 in / 16.36m |
| Main rotor blade chord | 0.53m |
| Tail rotor diameter | 11 ft / 3.35m |
| Ground clearance | 11.2 in |
| Ground to tail rotor clearance | 6 ft, 8 in |
| Turning radius | 41 ft, 7 in |
| Clearance for 180° | 84 ft |
| Areas |
| Main rotor disc | 210.15m2 |
| Tail rotor disc | 8.83m2 |
| Vertical fin | 3.00m2 |
| Horizontal tail surfaces | 4.18m2; |
| Weights and Loadings |
| Weight empty (ASW) | 6.191kg |
| Mission fuel load (usable) |
| Maximum useful load | (fuel and disposable ordinance) |
| Maximum takeoff and landing weight |
| Maximum disc loading | 47.2kg/m2 |
| Maximum power loading | 3.92kg/m2 |
| Performance |
| Never-exceed speed (Vne) |
| Maximum level speed at S/L (Dash Speed) | 126 knots |
| Rate of climb at S/L, OEI | 213m/min |
| Service ceiling | 5,790m |
| Service ceiling, OEI | 21287 |
| Hovering ceiling | 2,895mIGE |
| Range at S/L with standard fuel, no reserves | 319 nm |
