A119
AGUSTA A-119
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
DENEL A-119 Koala
DENEL Koala
AGUSTA Koala
AGUSTA AW-119 Koala
AGUSTA A-119 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 (metric)
10.83 m
Length (metric)
13.01 m
Height (metric)
3.77 m
Powerplant
1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW
Engine Model(s)
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
