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Agusta Aerospace Corporation/ August
Grand
Manufacturer/Model Agusta Aerospace Corporation/ Agusta Grand
Total production (all variants) 30
Comments Certified single-pilot IFR Category “A” single
engine performance.
Engine (2) Pratt & Whitney PW207C HP (takeoff) 735 shp
ea.
Dimensions main rotor 35.5 ft/11 m Tail rotor 6.3
ft/1.9 m
Height 11.5 ft/3.5m Length 38.3 ft/11.7 m Width 5.4
ft/1.6 m
Empty weight 3,649 lbs/1,655 kg Gross weight 7,000
lbs/3,175 kg
Useful load 3,351 lbs/1,520 kg External 2,204
lbs/1,000 kg
Vne 168 kts/311 kmh Max cruise 155 kts/288 kmh
Max rate of climb 1,894 fpm/9.6 ms
HIGE 14,270 ft/4,350 m HOGE 9,350 /2,850 m
Service ceiling 18,730 ft/5,710 m
Std fuel 152 gal/575 lit Max fuel 213 gal/806 lit
Max range std fuel (no reserve) 324 nm/600 km
Range with opt fuel 470 nm/870 km
IFR Crew 1/2 Passengers 7/6
Standard avionics FAA SPIFR/DPIFR Package
2005 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland (215) 281-1400
Agusta Aerospace Corporation A 109 POWER Elite
Manufacturer/Model Agusta Aerospace
Corporation A109 POWER Elite
Total production (all variants) >400
Comments Certified single-pilot IFR Category “A” single
engine performance.
Engine (2) Pratt & Whitney P207C HP (takeoff) 640 shp
ea.
Dimensions main rotor 36.1 ft/11 m Tail rotor 6.66
ft/2.03 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width
5.28 ft/1.6 m
Empty weight 3,510 lbs/1,592 kg Gross weight 6,614
lbs/2,856 kg
Useful load 3,104 lbs/1,408 kg External 2,005
lbs/1,002 kg
Vne 168 kts/311 kmh Max cruise 154 kts/285 kmh
Max rate of climb 1,930 fpm/9.7 ms
HIGE 16,000 ft/4,875 m (ISA) HOGE 10,000 /3,050 m
Service ceiling 18,500 ft/5,650 m S/E service ceiling 13,100
ft/3,993 m
Std fuel 160 gal/605 lit Max fuel 214 gal/808 lit
Max range std fuel (no reserve) 356 nm/660 km
Range with opt fuel 521 nm/965 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2005 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland (215) 281-1400
Agusta Aerospace Corporation A109 POWER (PW)
Manufacturer/Model Agusta Aerospace
Corporation A109 POWER (PW)
Total production (all variants) >400
Comments Certified single-pilot IFR Category “A” single
engine performance.
Engine Choices (2) Pratt & Whitney P206C HP (takeoff) 640 shp
ea.
Dimensions main rotor 36.1 ft/11 m Tail rotor 6.66
ft/2.03 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width
5.28 ft/1.6 m
Empty weight 3,461 lbs/1,573 kg Gross weight
6,283lbs/2,850 kg
Useful load 2,823 lbs/1,283 kg External 2,005
lbs/1,002 kg
Vne 168 kts/311 kmh Max cruise 154 kts/285 kmh
Max rate of climb 1,930 fpm/9.7 ms
HIGE 16,600 ft/5,060 m (ISA) HOGE 11,800 /3,597 m
Service ceiling 19,600 ft/5,974 m S/E service ceiling
13,100 ft/3,993 m
Std fuel 160 gal/605 lit Max fuel 230 gal/870 lit
Max range std fuel (no reserve) 356 nm/660 km
Range with opt fuel 521 nm/965 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2005 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland (215) 281-1400
Agusta Aerospace Corporation A 109E POWER
Manufacturer/Model Agusta Aerospace
Corporation A109E POWER
Total production (all variants) >400
Comments Certified single-pilot IFR Category “A” single
engine performance.
Engine (2) Turbomeca Arrius 2K-1 HP (takeoff) 640 shp ea.
Dimensions main rotor 36.1 ft/11 m Tail rotor 6.66
ft/2.03 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width
5.28 ft/1.6 m
Empty weight 3,461 lbs/1,573 kg Gross weight
6,614lbs/3,000 kg
Useful load 3,153 lbs/1,427 kg External 2,005
lbs/1,002 kg
Vne 168 kts/311 kmh Max cruise 152 kts/281kmh
Max rate of climb 1,520 fpm/7.7 ms
HIGE 15,000 ft/4,572 m (ISA) HOGE 7,400 /2,865 m
Service ceiling 18,000 ft/5,485 m S/E service ceiling
10,000 ft/3,048 m
Std fuel 160 gal/605 lit Max fuel 221 gal/836 lit
Max range std fuel (no reserve) 324 nm/600 km
Range with opt fuel 503 nm/932 km
IFR Crew 1/2 Passengers 7/6
Standard avionics FAA SPIFR/DPIFR Package
2005 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland (215) 281-1400
Agusta Aerospace Corporation A109 POWER (T)
Manufacturer/Model Agusta
Aerospace Corporation A109 POWER (T)
Total production (all variants) >400
Comments Certified single-pilot IFR Category “A” single
engine performance.
Engine (2) Turbomeca Arrius 2K-1 HP (takeoff) 670 shp
ea.
Dimensions main rotor 36.1 ft/11 m Tail rotor 6.66
ft/2.03 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width 5.28
ft/1.6 m
Empty weight 3,461lbs/1,573 kg Gross weight 6,283
lbs/2,850 kg
Useful load 2,823 lbs/1,283 kg External 2,005
lbs/1,002 kg
Vne 168 kts/311 kmh Max cruise 154 kts/285 kmh
Max rate of climb 1,930 fpm/9.7 ms
HIGE 16,600 ft/5,060 m (ISA) HOGE 11,800 /3,597 m
Service ceiling 19,600 ft/5,974 m S/E service ceiling
13,100 ft/3,993 m
Std fuel 160 gal/605 lit Max fuel 230 gal/870 lit
Max range std fuel (no reserve) 356 nm/660 km
Range with opt fuel 521 nm/965 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2005 base price ($U.S.) Furnished upon request.
Contact:Robert Cleland (215) 281-1400
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