AGUSTAWESTLAND AW-189
AGUSTAWESTLAND AW-189
Aircraft
Name:
AW-189
Manufacturer:
Body:
Narrow
Wing:
Rotary
Position:
Five-blade main rotor
Tail:
Four-blade tail rotor
Type Code:
H2T
Engine:
Turboshaft
Engine Count:
Multi
Position:
In fuselage
Landing gear:
Tailwheel retractable
A189
The AgustaWestland AW189 is a twin-engined, medium-lift helicopter developed by AgustaWestland, and is derived from the AW149.
Technical Data
Wing span:
14.60 m
Length:
17.60 m
Height:
5.06 m
Powerplant:
2 x General Electric CT7-2E1 turboshaft engine, 1,492 kW each.
Engine Model:
General Electric CT7
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
n/a
MTOW:
8300 kg
Initial Climb (to 5000 ft)
IAS:
n/a
ROC:
1960 ft/min
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:
155 kts
MACH:
n/a
Ceiling:
n/a
Range:
490 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
