Empty weight, standard aircraft
(including engine oil & unusable fuel)
|
4 610 kg
|
10 160 lb
|
| Useful load |
4930 kg
|
9 680 lb
|
| Maximum all-up weight
|
9000 kg
|
19 840 lb
|
| Maximum cargo-sling load
|
4500 kg
|
9 920 lb
|
Maximum all-up weight
in external load configuration
|
9350 kg
|
20 615 lb
|
Note: Empty weight accuracy: within + 2%
| Maximum speed, VNE (Never Exceed Speed)
|
278 km/h
|
150 kts
|
| Fast Cruise speed at MCP (Max Continuous Power)
|
258 km/h |
139 kts
|
| Rate of climb (85kt, 2 engines at MCP)
|
7,2 m/s
|
1417 ft/min
|
| Service ceiling (Rate-of-climb : 0,508m/s 100 ft/mn)
|
3450 m
|
11319 ft
|
| Hover ceiling In Ground Effect (IGE)
|
2800 m
|
9196 ft
|
| Hover ceiling Out of Ground Effect (OGE)
|
1650 m
|
5413 ft
|
| Maximum range with standard tank |
776 km
|
4194 m
|
At
Max Gross Weight, at Sea Level (SL), in International Standard
Atmosphere (ISA) and zero wind condition.
| Maximum emergency power (OEI 30”)
|
1400 kW
|
1877 shp
|
| Intermediate emergency power (OEI 2’) |
1330 kW
|
1783 shp
|
| Take-off power
|
1357 kW
|
1819 shp
|
| Maximum continuous power
|
1185 kW
|
1588 shp
|
Power per engine, in standard atmosphere, at sea level |