Manufacturer/Model AgustaWestland Grand
Total production (all variants) >180
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/10.83 m Tail rotor 6.3 ft/1.94 m
Height 11.4 ft/3.4 m Length 38.3 ft/11.7 m Width 5.4 ft/1.6 m
Empty weight 3,660 lbs/1,660 kg Gross weight 7,000 lbs/3,175 kg
Useful load 3,351 lbs/1,520 kg External 3,406 lbs/1.545 kg
Vne 168 kts/311 kmh Max cruise 155 kts/287 kmh
Max rate of climb 1,830 fpm/9.30 ms
HIGE 15,600 ft/4,750 m HOGE 10,600 /3,050 m
Service ceiling 16,200 ft/4,940 m
Std fuel 152 gal/575 lit Max fuel 213 gal/805 lit
Max range std fuel (no reserve) 295 nm/546 km
Range with opt fuel 432nm/800 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2008 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland 215-281-1400

Manufacturer/Model AgustaWestland AW109 Power
Total production (all variants) >500
Comments Certified single-pilot IFR Category “A” single engine performance.
Engine (2) Pratt & Whitney PW206C HP (takeoff) 640 shp ea.
Dimensions main rotor 11.0 ft/36.09 m Tail rotor 6.35 ft/1.94 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width 5.28 ft/1.6 m
Empty weight 3,494 lbs/1,585 kg Gross weight 6,283 lbs/2,850 kg
Useful load 2,789 lbs/1,265 kg External 3,120 lbs/1,415 kg
Vne 168 kts/311 kmh Max cruise 154 kts/285 kmh
Max rate of climb 1,930 fpm/9.8 ms
HIGE 16,600 ft/5,059 m HOGE 11,800 /3,596 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 221 gal/835 lit
Max range std fuel (no reserve) 378 nm/700 km
Range with opt fuel 512 nm/948 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2008 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland 215-281-1400

Manufacturer/Model AgustaWestland AW109 Power (Law Enforcement)
Total production (all variants) >500
Comments Certified single-pilot IFR Category “A” single-engine performance.
Engine (2) Pratt & Whitney PW206C (takeoff) 640 shp ea.
Dimensions main rotor 36.1 ft/11.0 m Tail rotor 6.35 ft/1.94 m
Height 11.5 ft/3.5m Length 37.6 ft/11.46 m Width 5.28 ft/1.6 m
Empty weight 3,494 lbs/1,585 kg Gross weight 6,283lbs/2,850 kg
Useful load 2,789 lbs/1,265 kg External 3,120 lbs/1,415 kg
Vne 168 kts/311 kmh Max cruise 154 kts/285 kmh
Max rate of climb 1,930 fpm/9.8 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 221 gal/835 lit
Max range std fuel (no reserve) 378 nm/700 km
Range with opt fuel 512 nm/948 km
IFR Crew 1 Passengers 7
Standard avionics FAA SPIFR/DPIFR Package
2008 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland 215-281-1400

Manufacturer/Model AgustaWestland AW139
Total production (all variants) >300 First flight Feb 2001
Engine(s) (2) Pratt & Whitney PT6C-67C
HP (takeoff) 2 x 1,679 hp/2 x 1,252 kw ea.
Dimensions main rotor 45.25 ft/13.8 m Tail rotor 8.83 ft/2.70 m
Height 12.25 ft/3.7 m Length 44.33 ft/13.52 m Width 7.42 ft/2.26 m
Empty weight 8,124 lbs/3,685 kg Gross weight 14,110 lbs/6,400 kg
Useful load 5,986 lbs/2,715 kg External 6,868 lbs/3,115 kg
Vne 167 kts/310 kmh Max cruise 165 kts/306 kmh
Max rate of climb 2,140 fpm/10.9 ms
HIGE 15,360 ft/4,682 m HOGE 8,130 ft/2,478 m
Service ceiling 20,000 ft/6,096 m S/E service ceiling 11,600 ft/3,535 m
Std fuel 414 gal/1,568 lit Max fuel 546 gal/2,068 lit
Max range std fuel (no reserve) 437 nm/809 km
Range with opt fuel 573 nm/1,061 km
VFR/IFR Crew 1/2 Passengers up to 15
Standard avionics FAA IFR package with EFIS display and autopilot
2008 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland 215-281-1400

Manufacturer/Model AgustaWestland AW119Ke (Koala Enhanced)
Total production (all variants) >140
Comments Fast cruise speed with large multi-purpose cabin.
Engine(s) (1) Pratt & Whitney PT6B-37A HP (takeoff) 1002 shp/747 kw
Dimensions main rotor 35.53 ft/10.83 m Tail rotor 6.36 ft/1.94 m
Height 12.73 ft/3.77 m Length 42.70 ft/13.02 m (rotors turning)
Width 5.28 ft/1.6 m (M/R blade at 45 degrees)
Empty weight 3,208 lbs/1,455 kg
Max gross weight (internal) 6,283 lb/2,850 kg (external) 6,945 lb/3,150 kg
Useful load (internal) 3,075 lbs/1,395 kg (external) 3,737 lbs/1,695 kg
Vne 152 kts/281 kmh Max cruise 139 kts/257 kmh
Max rate of climb 1,789 fpm/9.1 ms
HIGE 11,400 ft/3,475 m HOGE 7,600 ft/2,316 m
Service ceiling 15,000 ft/4,572 m S/E service ceiling N/A
Std fuel 160 gal/605 lit Max fuel 230 gal/870 lit
Max range std fuel (no reserve) 374 nm/692 km
Max range aux fuel (no reserve) 547 nm/1,013 km
VFR Crew 1 Pilot Passengers 7
Standard avionics Basic VFR Package.
2008 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland 215-281-1400

Manufacturer/Model AgustaWestland AW101
Total production (all variants) 152 + 23 US101 First flight 1987
Comments Production aircraft in service with Tokyo Metropolitan Police, Italian Navy, Canadian Forces., UK’s Royal Air Force, Royal Danish Air Force and the Portuguese Air Force
Engine(s) (3) GE CT7-8E (civil version) or Rolls-Royce Turbomeca RTM322 HP (takeoff) 2,527 (GE) shp ea.
Dimensions main rotor 61.0 ft/18.6 m Tail rotor 13.1 ft/4.0 m
Height 21.7 ft/6.6 m Length 74.8 ft/22.8 m Width 14.83 ft/4.5 m
Empty weight 20,282 lbs/9,200 kg Gross weight 34,392 lbs/15,600 kg
Useful load 13,230 lbs/6,000 kg
Vne 167 kts Max cruise 150 kts/227 kmh
Max rate of climb 2,788 fpm/14.2 m/s
HIGE 10,800 ft HOGE 4,800 ft/1,460 m
Service ceiling 10,000 ft/3,050 m Std fuel 1,136 gal/4,303 lit Max fuel 1,421 gal/5,380 lit Max range std fuel (no reserve) 610 nm/1,130 km
Range with opt fuel 750 nm/1,390 km
VFR Crew 2 + 1 attendant Passengers 30
Standard avionics 4-axis automatic flight control system & full EFIS cockpit.
2008 base price ($U.S.) Provided upon request.
Contact: Jackie Ferko 703-373-8022