AGUSTA A-119

Aircraft
Name: 
A-119
Manufacturer: 
Wing: 
Rotary
Position: 
Four-blade main rotor
Tail: 
Two-blade tail rotor
WTC
L
APC
A
Type Code: 
H1T
Engine: 
Turboshaft
Engine Count: 
Single
Position: 
Above cabin
Landing gear: 
Skids
Manufacturered as
AGUSTA A-119 Koala
AGUSTA AW-119 Koala
AGUSTA Koala
DENEL A-119 Koala
DENEL Koala

A119

The AgustaWestland AW119 Koala (Agusta A119 Koala prior to the Agusta-Westland merger) is an eight-seat utility helicopter powered by a single turboshaft engine and produced for the civil market. The design was derived from Agusta's highly successful AGUSTA A-109, but with only a single engine and with fixed skids replacing the retractable wheeled landing gear.

Technical Data
Wing span: 
10.83 m
Length: 
13.01 m
Height: 
3.77 m
Powerplant: 

1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW

Engine Model: 
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
2720 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: 
144 kts
MACH: 
n/a
Ceiling: 
200
Range: 
535 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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