AGUSTA A-109
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
AGUSTA A-109
AGUSTA A-109 Grand
AGUSTA A-109 Nexus
AGUSTA A-109 Power
AGUSTA AW-109
AGUSTA AW-109 Grand
AGUSTA AW-109 Nexus
AGUSTA AW-109 Power
AGUSTA Grand
AGUSTA Hkp15
AGUSTA MH-68 Stingray
AGUSTA Nexus
AGUSTA Power
AGUSTA Stingray
DENEL A-109
SABCA A-109
A109
Twin engined utility and corporate helicopter. About 80 were produced between 1976 and 1980.
Technical Data
Wing span:
11.00 m
Length:
13.08 m
Height:
3.32 m
Powerplant:
2 x Pratt & Whitney Canada 206C or Turboméca Arrius 2K1 turboshafts, 423 kW or 426 kW each.
Engine Model:
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
