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AGUSTAWESTLAND AW-189

From SKYbrary Wiki
A189
Aircraft
Name AW-189
Manufacturer AGUSTAWESTLAND
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
Mass group 3


Manufacturered as:


AGUSTAWESTLAND AW-189

AGUSTAWESTLAND AW-189 AGUSTAWESTLAND AW-189 3D

Description

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 m47.9 ft
Length 17.60 m57.743 ft
Height 5.06 m16.601 ft
Powerplant 2 x General Electric CT7-2E1 turboshaft engine, 1,492 kW each.
Engine model General Electric CT7

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 155 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC 1960 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 83008,300 kg
8.3 tonnes
kg
Ceiling FL ROD ft/min APC
WTC Range 490490 nm
907,480 m
907.48 km
2,977,296.59 ft
NM

Accidents & Serious Incidents involving A189

None on SKYbrary