August Aerospace Corporation A119 Koala

Manufacturer/Model Agusta Aerospace Corporation A119 Koala
Total production (all variants) 70
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 6.56 ft/2 m
Height 12.37 ft/3.77 m Length 42.68 ft/13.01 m (rotors turning)
Width 25.13 ft/7.66 m (rotor blade at 45 degrees)
Empty weight 3,152 lbs/1,430 kg Gross weight 5,997 lbs/2720 kg (internal) (6,614 lbs)/ (6,945 lbs) external
Useful load 2,845 lbs/1,290 kg External 3,793 lbs/1720 kg
Vne 152 kts/281 kmh Max cruise 144 kts/267 kmh
Max rate of climb 1,850 fpm/9.4 ms
HIGE 14,600 ft/4,450 m HOGE 10,700 ft/3,261 m
Service ceiling >20,000 ft/6,096 m S/E service ceiling N/A
Std fuel 160 gal/605 lit Max fuel 230 gal/869 lit
Max range std fuel (no reserve) 382 nm/707 km
Range with opt fuel 535nm/991 kmh
VFR Crew 1 Passengers 7
Standard avionics Basic VFR Package.
2005 base price ($U.S.) Furnished upon request.
Contact: Robert Cleland (215) 281-1400

August Aerospace Corporation AB 139

Manufacturer/Model Agusta Aerospace Corporation AB139
Total production (all variants) 50+ 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 16.25 ft/4.95 m Length 54.66 ft/16.66 m Width 13.83 ft/4.22 m
Empty weight 7,985 lbs/3,622 kg Gross weight 14,110 lbs/6,400 kg
Useful load 6,124 lbs/2,778 kg External 6,000 lbs/2,722 kg
Vne 167 kts/310 kmh Max cruise 167 kts/310 kmh
Max rate of climb 2,005 fpm/10.19 ms
HIGE 12,400 ft/3,780 m HOGE 5,500 ft/1,676 m
Service ceiling 20,000 ft/6,096 m S/E service ceiling 11,800 ft/3,597 m
Std fuel 419 gal/1,588 lit AUX fuel 132 gal/500 lit
Max range std fuel (no reserve) 437 nm/809 km
Range with opt fuel 579 nm/1,071 km
VFR/IFR Crew 1/2 Passengers up to 15
Standard avionics FAA IFR package with EFIS display and autopilot
2006 base price ($U.S.) Call for information.
Contact: Robert Cleland 215-281-1400

August Westland/EH 101

Manufacturer/Model AgustaWestland/EH101
Total production (all variants) 146 (as of Oct. 2004) First flight 1987
Comments Production aircraft in service with Tokyo Metropolitan Police, Italian Navy, UK’s Royal Air Force and Navy, and Canadian Forces.
Engine(s) (3) GE T700-T6A1or CT7-6A (civil version) or Rolls Royce Turbomeca RTM322 HP (takeoff) 2,145 and 2270 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 32,188 lbs/14,600 kg
Useful load 11,905 lbs External 10,000 lbs
Vne 167 kts Max cruise 150 kts/227 kmh
Max rate of climb 1,964 fpm/670 mpm
HIGE 7,300 ft (w. Rolls Royce eng.) HOGE 3,700 ft (w. Rolls Royce eng.)
Service ceiling 15,000 ft/4,572 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.
2005 base price ($U.S.) Provided upon request.
Contact: Angelica Falchi (703) 243-7733 (US); +44-1252-37212 (UK)

Bell Helicopter 206B-3 JetRanger III

Manufacturer/Model Bell Helicopter 206B-3 JetRanger III
Total production (all variants) 6,000+
Comments Safest, most reliable helicopter with the lowest DOC in class.
Engine(s) (1) Rolls-Royce 250-C20J HP (takeoff) 420 hp/313 kw
Dimensions main rotor 33.3 ft/10.2 m Tail rotor 5.4 ft/1.65 m
Height 9.5 ft/2.9 m Length 39.1 ft/11.9 m Width 6.4 ft/2.0 m
Empty weight 1,710 lbs/777 kg Gross weight 3,200 lbs/1,451 kg
Useful load 1,490 lbs/675 kg External 1,500 lbs/ 680 kg
Vne 122 kts/226 kmh Max cruise 115 kts/213 kmh
Max rate of climb 1,280 fpm/6.5 ms
HIGE 13,200 ft/4,023 m HOGE 5,300 ft/1,387 m
Service ceiling 13,500 ft/4,115 m S/E service ceiling N/A
Std fuel 91 gal/344 lit Max fuel N/A
Max range std fuel 374 nm/694 km
Range with opt fuel N/A
VFR Crew 1 Passengers 4
Standard avionics None.
2005 base price Funished upon request
Contact: Bill Maddox (817) 280-6187

Bell Helicopter 206L-4 LongRanger IV

Manufacturer/Model Bell Helicopter 206L-4 LongRanger IV
Total production (all variants) 1770+
Comments Features compact hangar space requirements. Offers smooth ride with excellent hot-high performance and the lowest DOC in class.
Engine(s) (1) Rolls-Royce 250-C30P HP (takeoff) 726 hp/541 kw
Dimensions main rotor 37.0 ft/11.3 m Tail rotor 5.4 ft/1.65 m
Height 11.69 ft/3.1 m Length 42.5 ft/12.96 m Width 7.68 ft/2.33 m
Empty weight 2,322 lbs/1,047 kg Gross weight 4,450 lbs/2,018 kg
Useful load 2,128 lbs/965 kg External 2,000 lbs/907 kg
Vne 130 kts/241 kmh Max cruise 112 kts/207 kmh
Max rate of climb 1,320 fpm/6.7 ms
HIGE 10,000 ft/3,048 m HOGE 6,500 ft/1,981 m
Service ceiling 10,000 ft/3,048 m S/E service ceiling N/A
Std fuel 110.7 gal/419 lit Max fuel N/A
Max range std fuel (no reserve) 324 nm/600 km
Range with opt fuel N/A
VFR Crew 1 Passengers 6
Standard avionics None.
2005 base price: Funished upon request
Contact: Bill Maddox (817) 280-6187

Bell Helicopter 407

Manufacturer/Model Bell Helicopter 407
Total production (all variants) 550+
Comments Offers smooth ride with electronic engine controls, low operating costs, and excellent hover performance.
Engine(s) Rolls-Royce 250-C47B HP (takeoff) 674 shp/503 kw
Dimensions main rotor 35.0 ft/10.7 m Tail rotor 5.4 ft/1.7 m
Height 11.8 ft/3.6 m Length 41.8 ft/12.7 m Width 7.5 ft/2.29 m
Empty weight 2,663 lbs/1,203 kg Gross weight Std. 5,000 lbs/2,268 kg Opt. 5,250 lbs/2,384 kg External 6,000 lbs/2,722kg
Useful load Std. 2,335 lbs/1,059 kg Opt. 2585 lbs/1,172 kg
External 2,646 lbs/1,200 kg
Vne 140 kts/259 kmh Max cruise 133 kts/246 kmh
Max rate of climb 1,940 fpm/9.8 ms
HIGE 12,200 ft/3,718 m HOGE 10,450 ft/3,170 m
Service ceiling 17,600 ft/5,364 m S/E service ceiling N/A
Std fuel 127.8 gal/484 lit Aux. Fuel: 19.0 gal/72.0 lit
Max range std fuel (no reserve) 330 nm/612 km
Range with opt fuel 380 nm/704 km
VFR Crew 1 Passengers 6
Standard avionics None.
2005 base price: Funished upon request
Contact: Bill Maddox (817) 280-6187

Bell Helicopter 412 EP

Manufacturer/Model Bell Helicopter 412 EP
Total production (all variants) 745+
Comments Versatile utility helicopter with Category “A” Certification, excellent high-hot performance, and single and dual pilot IFR.
Engine(s) (2) Pratt & Whitney Canada PT6T-3D
HP (takeoff) 1,800 hp/1,342kw
Dimensions main rotor 46.0 ft/14.0 m Tail rotor 8.58 ft/2.6 m
Height 11.4 ft/3.5 m Length 56.16 ft/17.1 m Width 9.3 ft/2.8 m
Empty weight 6,863 lbs/3,119 kg Gross weight 11,900 lbs/5,409 kg
Useful load 5,037 lbs/2,285 kg External 4,500 lbs/2,045 kg
Vne 140 kts/259 kmh Max cruise 122 kts/226 kmh
Max rate of climb 1,780 fpm/9.0 ms
HIGE 10,200 ft/3,110 m HOGE 5,200 ft/1,585 m
Service ceiling 16,300 ft/4,970 m S/E service ceiling 7,600 ft/2,316 m
Std fuel 330.5 gal/1,251 lit AUX. fuel 163.4 gal/618.5 lit
Max range std fuel (no reserve) 402 nm/705 km
Range with opt fuel 533 nm/987 km
IFR Crew 1/2 VFR Crew 1 Passengers 14/13
Standard avionics 1 x VHF COMM
2005 base price: Funished upon request
Contact: Bill Maddox (817) 280-6187

Bell Helicopter 430

Manufacturer/Model Bell Helicopter 430
Total production (all variants) 100+
Comments Features electronic engine controls, single pilot IFR, Category “A” Certification, and integrated instrument display (IIDS). Available with either standard skid landing gear or optional retractable wheel gear.
Engine(s) (2) Rolls-Royce 250-C40B HP (takeoff) 808 hp/6.3 kw ea.
Dimensions main rotor 42.0 ft./12.8 m Tail rotor 6.9 ft/2.1 m
Height 13.2 ft/4.0 m Length 50.2 ft/15.3 m Width 11.3 ft/3.5 m
Empty weight 5,331lbs/2,418 kg (skids); 5,364 lbs/2,433 kg (whls)
Gross weight 9,300 lbs/4,218 kg Useful load 3,969 lbs/1,800 kg (skids); 3,936 lbs/1,785 kg (whls) External 2,800 lbs/1,270 kg
Vne 150 kts/278 kmh Max cruise 139 kts/258 kmh (skids); 143 kts/265 kmh (whls) Max rate of climb 1,730 fpm/8.8 ms
HIGE 10,400 lb/3,170 m HOGE 6,200 ft/1,890 m
Service ceiling 16,180 ft/4,932 m S/E service ceiling 7,740 ft/2,359 m
Std fuel 247 gal/935 lit (skids); 187.5 gal/710 lit (whls)
Aux. Fuel 48 gal/182 lit
Max range std fuel (no reserve) 353 nm/654 km (skids); 275 nm/510 km (whls) Range with opt fuel 393 nm/728 km (skids); 315 nm/584 km (whls)
IFR Crew 1 VFR Crew 1 Passengers 9 Standard avionics N/A
2005 base price: Funished upon request

Bell Helicopter 427

Manufacturer/Model Bell Helicopter 427
Total production (all variants) 40+
Comments Features electronic engine controls, flat pack transmission, and integrated instrument display (IIDS).
Engine(s) (2) Pratt & Whitney Canada PW207D
HP (takeoff) 710 hp/529 kw ea.
Dimensions main rotor 37.0 ft/11.3 m Tail rotor 5.7 ft/1.73 m
Height 11.44 ft/3.49 m Length 42.7 ft/13.02 m Width 8.8 ft/2.89 m
Empty weight 3,875 lbs/1,751 kg Max. Gross weight Std. 6,350 lbs/2,880 kg Opt. 6,550 lbs/2,971 kg Useful load 2,475 lbs/1,122 kg Opt. 2,675 lbs/1213 kg External 3,000 lbs/1,361 kg
Vne 140 kts/259 kmh Max cruise 138 kts/256 kmh Max rate of climb 1,600 fpm/8.1 ms
HIGE 17,450 ft/5,319 m HOGE 12,500 ft/3,810 m
Service ceiling 10,000 ft/3,048 m S/E service ceiling 8,000 ft/2,438 m
Std fuel 203.5 gal/770 lit Max fuel N/A
Max range std fuel (no reserve) 385 nm/713 kmh
IFR Crew 1 VFR Crew 1 Passengers 7
Standard avionics None.
2005 base price: Funished upon request
Contact: Bill Maddox (817) 280-6187

Bell/August Aerospace Company BA609 TiltRotor

Manufacturer/Model Bell/Agusta Aerospace Company BA609 TiltRotor
Total production (all variants) 4 First flight March 2003
Comments In development, flight testing
Engine(s) (2) Pratt & Whitney PT6C-67A
HP (takeoff) 1,941hp/1,448 kw ea.
Dimensions main rotor (2) 26.0 ft/7.9 m Tail rotor N/A
Height 15 ft/4.6 m Length 44.0 ft/13.4 m Width 60.0 ft/18.3 m
Empty weight 11,300 lb/5,126 kg Gross weight 16,800 lb/7,612 kg
Useful load 5,500 lb/2,495 kg External N/A
Vne TBD Max cruise 275 kts/509 kmh
Max rate of climb 1,500 fpm/7.6 ms
HIGE N/A HOGE 5,000 ft/1,524 m
Service ceiling 25,000 ft/7,620 m OEI service ceiling 16,000 ft/4,877 m
Std fuel 365 gal/1,381 lit Aux. fuel TBD
Max range std fuel (no reserve) 750 nm/1,389 @ Best Altitude
Range with opt fuel TBD
IFR Crew 1 or 2 Passengers 9
Standard avionics FAA IFR Package.
2005 base price ($U.S.) Call for information.
Contact: Giles LeHoux (940) 552-5451

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