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AGUSTAWESTLAND AW-169

From SKYbrary Wiki
A169
Aircraft
Name AW-169
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 Tricycle retractable
Mass group 2


Manufacturered as:


AGUSTAWESTLAND AW-169

AGUSTAWESTLAND AW-169

Description

The AgustaWestland AW169 is a twin-engine, 10-seat helicopter currently developed by AgustaWestland.

Technical Data

Wing span 12.12 m39.764 ft
Length 14.65 m48.064 ft
Height 4.50 m14.764 ft
Powerplant 2 x Pratt & Whitney Canada PW210 turboshaft engine, 750 kW each.
Engine model Pratt & Whitney Canada PW200

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 150 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 45004,500 kg
4.5 tonnes
kg
Ceiling FL ROD ft/min APC
WTC Range 500500 nm
926,000 m
926 km
3,038,057.745 ft
NM

Accidents & Serious Incidents involving A169

None on SKYbrary