EH10

AGUSTAWESTLAND AW-101

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

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 (metric)
18.59 m
Length (metric)
22.85 m
Height (metric)
6.65 m
Powerplant

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

Engine Model(s)
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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