AGUSTAWESTLAND AW-101
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
