AGUSTAWESTLAND AW-101

Aircraft
Name: 
AW-101
Manufacturer: 
Wing: 
Rotary
WTC
M
Type Code: 
H3T
Engine: 
Turboshaft
Engine Count: 
Multi
Manufacturered as
AGUSTAWESTLAND AW-101
AGUSTAWESTLAND AW-101 Merlin Joint Supporter
AGUSTAWESTLAND EH-101
AGUSTAWESTLAND EH-101 Merlin Joint Supporter
AGUSTAWESTLAND Kestrel
AGUSTAWESTLAND MCH-101
AGUSTAWESTLAND Merlin Joint Supporter
AGUSTAWESTLAND US-101
AGUSTAWESTLAND VH-71 Kestrel
EHI CH-149 Cormorant
EHI Cormorant
EHI EH-101
EHI EH-101 Heliliner
EHI EH-101 Merlin
EHI Heliliner
EHI Merlin
KAWASAKI CH-101
KAWASAKI KHI-01
KAWASAKI MCH-101

EH10

The AgustaWestland AW101 (EH101 until June 2007) is a medium-lift helicopter for military applications but also marketed for civil use. The helicopter was developed as a joint venture between Westland Helicopters in the UK and Agusta in Italy (merged as AgustaWestland).

Technical Data
Wing span: 
18.59 m
Length: 
22.85 m
Height: 
6.65 m
Powerplant: 

3 x Rolls-Royce Turbomeca RTM322-01 turboshafts, 1,725 kW (2,312 shp) each.

Engine Model: 
Rolls-Royce/Turbomeca RTM322
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
14600 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
151 kts
MACH: 
n/a
Ceiling: 
150
Range: 
610 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
n/a

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