A109

AGUSTA A-109

Aircraft
Name
A-109
Manufacturer
Wing
Rotary
Position
Four-blade main rotor
Tail
Two-blade tail rotor
WTC
L
APC
A
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Position
Above cabin
Landing gear
Skids or tricycle retractable
Manufacturered as
SABCA A-109
DENEL A-109
AGUSTA Grand
AGUSTA Hkp15
AGUSTA Power
AGUSTA AW-109
AGUSTA MH-68 Stingray
AGUSTA A-109
AGUSTA A-109 Grand
AGUSTA A-109 Power
AGUSTA AW-109 Grand
AGUSTA AW-109 Power
AGUSTA AW-109 Nexus
AGUSTA A-109 Nexus
AGUSTA Nexus
AGUSTA Stingray

A109

Twin engined utility and corporate helicopter. About 80 were produced between 1976 and 1980.

Technical Data
Wing span (metric)
11.00 m
Length (metric)
13.08 m
Height (metric)
3.32 m
Powerplant

2 x Pratt & Whitney Canada 206C or Turboméca Arrius 2K1 turboshafts, 423 kW or 426 kW each.

Engine Model(s)
Pratt & Whitney Canada PW200
Turboméca Arrius
Indicative Performance Data
Take-Off
V2
n/a
Distance
0 m
MTOW
2600 kg
Initial Climb (to 5000 ft)
IAS
90 kts
ROC
1600 ft/min
Initial Climb (to FL150)
IAS
100 kts
ROC
1000
Initial Climb (to FL240)
IAS
100 kts
ROC
1000 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
125 kts
MACH
n/a
Ceiling
163
Range
332 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
130 kts
ROD
1000 ft/min
Descent (FL100 & below)
IAS
100 kts
MCS
n/a
ROD
1000 ft/min
Approach
Vapp (IAS)
40 kts
Distance
0 m

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