The AW101 combines the most advanced technologies, safety by design, mission systems and leading-edge manufacturing to provide a proven platform for Heads of State and VVIP operators.
Featuring the largest cabin in its class, 2.49m wide and 1.83m high, passengers are able to walk in the spacious environment, which can be fitted with a range of fixtures and equipment, finished in highest quality materials to customers exacting standards.
The aircraft has been proven in the world's most extreme environments, from the Arctic to the Antarctic.
Leading Features
MTOW: 15,600 kg
Powerplant: 3 x GE CT7-8E (Take-Off: 3 x 2,527 shp) with FADEC
Crew/passengers: 2 pilots and up to 30 passengers
Technical Data
Weights
Max take Off (int. / ext. loads)
15600
kg
34392
lb
Engine Rating (3 x CT7-8E)
Take-Off power (5 min)
3 x 1884
kW
3 x 2527
shp
Intermediate (30 min)
3 x 1855
kW
3 x 2488
shp
Maximum Continuous Power
3 x 1522
kW
3 x 2041
shp
OEI Max Contingency (2 min)
2 x 1880
kW
2 x 2522
shp
Fuel Capacity (VVIP version)
4 cell tanks (self-sealing)
4094
l
1081
USgal
Fuel Capacity (Utility version)
5 cell tanks (self-sealing)
5135
l
1357
USgal
Crew
Pilot
2
Passengers
38
External Dimensions
Overall length
22,83
m
74,92
ft
Overall height
6,66
m
21,83
ft
Main rotor diameter
18.60
m
61,00
ft
Performance
Cruise speed
278
km/h
150
kt
Hovering IGE
3307
m
10850
ft
Max Range (Utility version)
1360
km
735
nm
Max Endurance (Utility version)
6 h 30 min
The AW101 combines the most advanced technologies, safety by design, mission systems and leading-edge manufacturing to provide a proven platform for Heads of State and VVIP operators.
Featuring the largest cabin in its class, 2.49m wide and 1.83m high, passengers are able to walk in the spacious environment, which can be fitted with a range of fixtures and equipment, finished in highest quality materials to customers exacting standards.
The aircraft has been proven in the world's most extreme environments, from the Arctic to the Antarctic.
Leading Features
MTOW: 15,600 kg
Powerplant: 3 x GE CT7-8E (Take-Off: 3 x 2,527 shp) with FADEC
Crew/passengers: 2 pilots and up to 30 passengers
Technical Data
Weights
| Max take Off (int. / ext. loads) | 15600 | kg | 34392 | lb |
Engine Rating (3 x CT7-8E)
| Take-Off power (5 min) | 3 x 1884 | kW | 3 x 2527 | shp |
| Intermediate (30 min) | 3 x 1855 | kW | 3 x 2488 | shp |
| Maximum Continuous Power | 3 x 1522 | kW | 3 x 2041 | shp |
| OEI Max Contingency (2 min) | 2 x 1880 | kW | 2 x 2522 | shp |
Fuel Capacity (VVIP version)
| 4 cell tanks (self-sealing) | 4094 | l | 1081 | USgal |
Fuel Capacity (Utility version)
| 5 cell tanks (self-sealing) | 5135 | l | 1357 | USgal |
External Dimensions
| Overall length | 22,83 | m | 74,92 | ft |
| Overall height | 6,66 | m | 21,83 | ft |
| Main rotor diameter | 18.60 | m | 61,00 | ft |
Performance
| Cruise speed | 278 | km/h | 150 | kt |
| Hovering IGE | 3307 | m | 10850 | ft |
| Max Range (Utility version) | 1360 | km | 735 | nm |
| Max Endurance (Utility version) | 6 h 30 min |