AgustaWestland: AW101

General data

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Names and dates
Market original model designation
AW101
Market model designation (english translation or spelling)
AW101
First flight date and time
1987-10-09
Country of manufacture
Italy
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
15600
kg
External dimensions
Total length (rotors turning)
22.83
m
Overal height
6.66
m
Main rotor
Main rotor diameter
18.60
m
Powerplant
Engine model
General Electric CT7-8E
Engine type
Turboshaft
Number of engines
3
Total maximum continuous power
6123
HP
Total maximum power
7579
HP
Performance
Cruise speed (Vc)
278
km/h
Hover ceiling IGE
3307
m
Maximum range
1000
km
Maximum flight endurance
5.16
h
0.0383