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

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