Helicopters

Agusta Westland A109 Power

Rotor diameter: 36 ft 1 in (11 m) Fuselage length: 37 ft 6.78 in (11.45 m) Overall length: 42 ft 9.18 in (13.035 m) rotors turning Powerplant: 2 x 640 shp (477 kW) P&W PW 206C or 670 shp Turbomeca Arrius 2K1 Empty weight: 3,461 lb (1,570 kg) Max take-off weight: 6,284 lb (2,850 kg) Useful load: 2,822 lb (1,280 kg) Cabin length: 6.9 ft (2.1 m) Cabin width: 5 ft 3.38 in (1.61 m) Cabin height: 4.2 ft (1.28 m) Max seating: 8 HIGE: 16,600 ft (5,060 m) HOGE: 11,800 ft (3,600 m) Max cruise: 156 kt (289 kph) Economic cruise: 137 kt (254 kph) Range: 521 nm (965 km), Std tanks, no reserve

Agusta Westland A109S Grand

Rotor diameter: 35 ft 6 in (10.83 m) Fuselage length: 38 ft 3 in (11.65 m) Overall length: 42 ft 6 in (12.96 m) Powerplant: 2 x 735 shp (548 kW) Pratt & Whitney Canada PW207C turboshafts Empty weight: 3,649 lb (1,655 kg) Max take-off weight: 7,000 lb (3,175 kg) Useful load: 3,351 lb (1,520 kg) Cabin length: 6 ft 3.5 in (1.9 m) Cabin width: N/A Cabin height: 4 ft 2 in (1.48 m) Max seating: 8 HIGE: 14,270 ft (4,350 m) HOGE: 9,350 ft (2,850 m) Max cruise: 155 kt (287 kph) Economic cruise: N/A Range: 470 nm (870 km)

Agusta Westland A119 Koala

Rotor diameter: 36 ft 1 in (10.83 m) Fuselage length: 36 ft 3.98 in (11.074 m) Overall length: 42 ft 9.18 in (13.035 m) rotors turning Powerplant: 1 x 1,002 shp (747 kW) P&W PT6B-37 Empty weight: 3,086 lb (1,400 kg) Max take-off weight: 5,732 lb (2,600 kg), 5,997 lb (2,720 kg) with ext load Useful load: 2,845 lb (1,290 kg) 2,911 lb (1,320 kg) with ext load Cabin length: 6.9 ft (2.1 m) Cabin width: 5.5 ft (1.59 m) Cabin height: 4 ft 2.39 in (1.28 m) Max seating: 8 HIGE: 11,000 ft (3,350 m) HOGE: 8,800 ft (2,680 m) Max cruise: 140 kt (260 kph) Economic cruise: 115 kt (210 kph) Range: 330 nm (610 km), Std tanks, no reserve

Agusta Westland AW 139
Agus taWes tland AW 139
Rotor diameter: 45.28 ft (13.8 m) Fuselage length: 44.4 ft (13.53 m) Overall length: 54.64 ft (16.65 m) rotors turning Powerplant: 2 x 1,679 shp (1,252 kW) P&W PT6C-67C Empty weight: 7,227 lb (3,300 kg) Max take-off weight: 13,227 lb (6,000 kg) Useful load: 6,000 lb (2,700 kg) Cabin length: 8.86 ft (2.7 m) Cabin width: 6.56 ft (2 m) Cabin height: 4.66 ft (1.42 m) Max seating: 17 HIGE: N/A HOGE: 12,000 ft (3,600 m) Max cruise: N/A Economic cruise: N/A Range: 400 nm (750 km), Std tanks, no reserve

Bell 206 BIII JetRanger

Rotor diameter: 33 ft 5 in (10.16 m) Fuselage length: 31 ft 2.4 in (9.5 m) Overall length: 38 ft 11.4 in (11.82 m) Powerplant: 1 x 420 shp (313 kW) Allison 250-C20J turboshaft Empty weight: 1,678 lb (761 kg) Max take-off weight: 3,200 lb (1,451 kg) Useful load: 1,522 lb (690kg) Cabin length: 7 ft (2.13 m) Cabin width: 4 ft 2 in (1.28 m) Cabin height: 4 ft 2.5 in (1.28 m) Max seating: 5 HIGE: 12,800 ft (3,900 m) HOGE: 8,800 ft (2,682 m) Max cruise: 114.5 kt (212 kph) Economic cruise: 114.5 kt (212 kph) Range: 365 nm (676 km) no reserve

Bell 206 L4 LongRanger

Rotor diameter: 37 ft (11.28 m) Fuselage length: 33 ft 2.4 in (10.1 m) Overall length: 42 ft 10.2 in (13.02 m) Powerplant: 1 x 557 shp (415 kW) Allison 250- C30P turboshaft Empty weight: 2,307 lb (1,046 kg) Max take-off weight: 4,450 lb (2,018.5 kg) Useful load: 2,143 lb (972 kg) Cabin length: 9 ft (2.74 m) Cabin width: 4 ft 2 in (1.28 m) Cabin height: 4 ft 2.5 in (1.28 m) Max seating: 7 HIGE: 10,000 ft (3,048 m) HOGE: 6,500 ft (1,981 m) Max cruise: 110 kt (204 kph) Economic cruise: 110 kt (204 kph) Range: 321 nm (594 km) no reserve

Bell 212

Rotor diameter: 48 ft (14.6 m) Fuselage length: 41 ft 8.1 in (12.7 m) Overall length: 57 ft 3.25 in (17.45 m) Powerplant: 1 x 1,290 shp (961 kW) Pratt & Whitney Canada PT6T 3P Twin Pac Empty weight: 6,176 lb (2,801 kg) Max take-off weight: 11,200 lb (5,080 kg) Useful load: 5,024 lb (2,279kg) Cabin length: 7 ft 8 in (2.34 m) Cabin width: 8 ft (2.43 m) Cabin height: 4 ft 1 in (1.24 m) Max seating: 15 HIGE: 4,750 ft (1,448 m) HOGE: 8,400 ft (2,560 m) at 10,000 lb (4,545 kg) Max cruise: 111 kt (206 kph) Economic cruise: 104 kt (193 kph) Range: 224 nm (415 km) no reserve

Bell 407

Rotor diameter: 35 ft (10.7 m) Fuselage length: 33 ft 2.4 in (10.1 m) Overall length: 41.8 ft (12.7 m) Powerplant: 1 x 791 shp (589 kW) Allison 250-C47 turboshaft Empty weight: 2,598 lb (1,178 kg) Max take-off weight: 5,000 lb (2,267 kg) Useful load: 2,402 lb (1,090 kg) Cabin length: 9 ft (2.74 m) Cabin width: 4 ft 9 in (1.738 m) Cabin height: 4 ft 2.5 in (1.28 m) Max seating: 7 HIGE: 12,200 ft (3,719 m) HOGE: 10,400 ft (3,170 m) Max cruise: 128 kt (237 kph) Economic cruise: 115 kt (213 kph) Range: 312 nm (578 km)

Bell 412 HP

Rotor diameter: 46 ft (14 m) Fuselage length: 46 ft (14 m) Overall length: 56 ft 2 in (17.1 m) Powerplant: 1 x 1,800 shp (1,341 kW) Pratt & Whitney Canada PT6T 3P Twin Pac Empty weight: 6,789 lb (3,079 kg) Max take-off weight: 11,900 lb (5,398 kg) Useful load: 5,111 lb (2,318 kg) Cabin length: 7 ft 8 in (2.34 m) exc cockpit Cabin width: 8 ft (2.43 m) Cabin height: 4 ft 1 in (1.24 m) Max seating: 15 HIGE: 10,200 ft (3,109 m) HOGE: 5,200 ft (1,585 m) Max cruise: 122 kt (226 kph) Economic cruise: 122 kt (226 kph) Range: 352 nm (652 km)

Bell 427

Rotor diameter: 37 ft (11.3 m) Fuselage length: 37.9 ft (11.55 m) Overall length: 42.9 ft (13.06 m) Powerplant: 2 x 710 shp (528 kW) Pratt & Whitney Canada PW 207D turboshafts (5 minute take-off rating) Empty weight: 3,485 lb (1,581 kg) Max take-off weight: 6,000 lb (2,722 kg) Useful load: 2,515 lb (1,141 kg) Cabin length: 5.2 ft (1.57 m) at floor level Cabin width: 4 ft in (1.23 m) just above floor level Cabin height: 4.2 ft (1.3 m) Max seating: 8 HIGE: 16,200 ft (4,938 m) HOGE: 13,900 ft (4,237 m) Max cruise: 136 kt (252 kph) Economic cruise: 126 kt (233.5 kph) Range: 353 nm (654 km)

Bell 429

Rotor diameter: 42.3 ft (12.9 m) approx Fuselage length: 39.9 ft (12.17 m) Overall length: 53.4 ft (16.28 m) rotors turning, approx Powerplant: 2 x 710 shp (528 kW) Pratt & Whitney Canada PW 207D turboshafts (5 minute take-off rating) Empty weight: 4,300 lb (1,950 kg) Max take-off weight: 7,000 lb (3,175 kg) Useful load: 2,700 lb (1,225 kg) Max seating: 10 HIGE: 12,000 ft (3,658 m) HOGE: 9,300 ft (2,835 m) Max cruise: 142 kt (264 kph) Range: 350 nm (648 km) Endurance: 3.8 hr

Bell 430

Rotor diameter: 42 ft (12.8 m) Fuselage length: 44.1 ft (13.4 m) Overall length: 50.5 ft (15.39 m) Powerplant: 2 x 770 shp (573 kW) Allison 250-C40 turboshafts Empty weight: 5,285 lb (2,397 kg) Max take-off weight: 9,000 lb (4,082 kg) Useful load: 3,715 lb (1,685 kg) Cabin length: 8 ft 6 in (2.59 m) Cabin width: 4 ft 11 in (1.5 m) Cabin height: 4 ft 9.6 in (1.45 m) Max seating: 9 HIGE: 11,350 ft (3,459 m) HOGE: 8,750 ft (2,667m) Max cruise: 135 kt 250 kph Economic cruise: 128 kt (237 kph) Range: 351 nm (650 km)

Bell Agusta 609 tilt rotor

Rotor diameter: 26 ft (7.9 m) each, 60 ft (18.3 m) span Fuselage length: 44 ft (13.31 m) Overall length: 44 ft (13.31 m) Powerplant: 2 x 1,940 shp (1,447 kW) Pratt & Whitney Canada PT6C-67A turboshafts Empty weight: 10,500 lb (4,763 kg) Max take-off weight: 16,000 lb (7,258 kg) Useful load: 5,500 lb (2,495 kg) Cabin length: 12.8 ft (3.84 m) (9 seats) Cabin width: 58.5 in (1.48 m) (2 seats) Cabin height: 56 in (1.42 m) Max seating: 9 HIGE: 25,000 ft (7,620 m) HOGE: 25,000 ft (7,620 m) Max cruise: 275 kts (509.63 kph) Economic cruise: 250 kts (464 kph) Range: 750 nm (1,390 km)

Enstrom 480B

Rotor diameter: 32 ft (9.8 m) Fuselage length: 29 ft 10 in (9.1 m) Overall length: 37 ft 4.3 in (11.39 m) Powerplant: 1 x 420 shp Allison 250-C20W turboshaft derated to 305 shp (227 kW) for take-off and 277 shp (206 kW) continuous Empty weight: 769 kg Max take-off weight: 1,361 kg Useful load: 592 kg Cabin length: 7.3 ft (2.2 m) Cabin width: 5.87 ft (1.79 m) Cabin height: 4.25 ft (1.3 m) Max seating: 5 HIGE: 12,300 ft (3,750 m) HOGE: 5,400 ft (1,645 m) Max cruise: 202 km/h at MTOW Economic cruise: N/A Range: 657 km at 3,000 ft, no reserves

Enstrom F 280 FX

Rotor diameter: 32 ft (9.8 m) Fuselage length: 28.7 ft (8.7 m) Overall length: 37 ft (11.28 m) Powerplant: 1 x 225 hp (168 kW) Lycoming HIO-360-F1AD turbocharged piston engine Empty weight: 1,670 lb (757 kg) with standard equipment Max take-off weight: 2,600 lb (1,179 kg) Useful load: 930 lb (422 kg) Cabin length: 5.6 in (1.7 m) Cabin width: 4 ft 11 in (1.498 m) Cabin height: 4 ft (1.2 m) Max seating: 2 HIGE: 13,200 ft (4,023 m) @ 2,350 lb HOGE: 8,700 ft (2,651 m) @ 2,350 lb Max cruise: 101 kt (188 kph) 117 mph Economic cruise: 93 kt (172 kph) 107 mph Range: 260 nm (483 km) 300 sm no reserve

Enstrom F28F Falcon

Rotor diameter: 32 ft (9.8 m) Fuselage length: 28.1 ft (8.6 m) Overall length: 37 ft (11.28 m) Powerplant: 1 x 225 hp (168 kW) Lycoming HIO-360-F1AD turbocharged piston engine Empty weight: 1,640 lb (744 kg) with standard equipment Max take-off weight: 2,600 lb (1,179 kg) Useful load: 960 lb (435 kg) Cabin length: 5.4 ft (1.7 m) Cabin width: 5 ft 1 in (1.55 m) Cabin height: 4 .2 ft (1.3 m) Max seating: 2 HIGE: 13,200 ft (4,023 m) @ 2,350 lb HOGE: 8,700 ft (2,651 m) @ 2,350 lb Max cruise: 97 kt (180 kph) 112 mph Economic cruise: 89 kt (165 kph) 102 mph Range: 240 nm (423 km) 263 sm no reserve

Erickson S-64E/F Aircrane

Rotor diameter: 72 ft (21.95 m) Fuselage length: 70 ft 3 in (21.41 m) Overall length: 88 ft 6 in (26.97 m) Powerplant: 2 x 4,500 shp (3,356 kW) Pratt & Whitney JTFD12-4A (S-64E) or 4,800 shp (3,579 kW) JTFD12-5A (S-64F) turboshafts Empty weight: 19,234 lb (8,724 kg) Max take-off weight: 42,000 lb (19,050 kg) (S-64E) or 47,000 lb (21319 kg) (S-64F) Useful load: 20,000 lb (9,072 kg) (S-64E) or 25,000 lb (11,340 kg) (S-64F), max external Cabin length: No cabin aft of cockpit but provision to fit container pod or firefighting tank and refill pump system. Cabin width: N/A Cabin height: N/A Max seating: 0 HIGE: 10,600 ft (3,230 m) (S-64E) Service ceiling: 9,000 ft (2,475 m) HOGE: 6,900 ft (2,103 m) (S-64E) Max cruise: 104 kt (193 kph) Economic cruise: N/A Range: 230 sm (370 km) with 10% reserve Endurance: 2 hrs 45 mins (no reserve) (S-64F)

Eurocopter AS 332 L1 Super Puma
Eurocop ter AS 332 L1 Super Puma
Rotor diameter: 51.12 ft (15.58 m) Fuselage length: 53.44 ft (16.29 m) Overall length: 61.35 ft (18.7 m) Powerplant: 2 x 1,820 shp (1,357 kW) Turbomeca Makila 1A1 turboshafts Empty weight: 9,832 lb (4,460 kg) Max take-off weight: 18,960 lb (8,600 kg) Useful load: 9,128 lb (4,140 kg) Cabin length: 16.44 ft (5.01 m) at floor Cabin width: 5.9 ft (1.8 m) Cabin height: 5.09 ft (1.55 m) Max seating: 22 HIGE: 10,663 ft (3,250 m) HOGE: 7,546 ft (2,300 m) Max cruise: 144 kt (267 kph) Economic cruise: 138 kt (256 kph) Range: 655 nm (1,215 km) with std tanks, centre tank + sponson tanks

Eurocopter AS 332 L2 Super Puma 2

Rotor diameter: 53.15 ft (16.2 m) Fuselage length: 55 ft (16.79 m) Overall length: 63.98 ft (19.5 m) Powerplant: 2 x 1,845 shp (1,375.5 kW) Turbomeca Makila 1A2 turboshafts Empty weight: 10,330 lb (4,686 kg) Max take-off weight: 20,500 lb (9,300 kg) Useful load: 10,173 lb (4,614 kg) Cabin length: 18.67 ft (5.69 m) at floor Cabin width: 5.91 ft (1.8 m) Cabin height: 4.76 ft (1.45 m) Max seating: 27 HIGE: 10,236 ft (3,126 m) HOGE: 6,430 ft (1,960 m) Max cruise: 150 kt (278 kph) Economic cruise: 136 kt (251 kph) Range: 655 nm (1,215 km) with std tanks, centre tank + sponson tanks

Eurocopter AS 350 B2

Rotor diameter: 35 ft 0.8 in (10.69 m) Fuselage length: 35.85 ft (10.93 m) Overall length: 42.45 ft (12.94 m) Powerplant: 1 x 732 shp (546 kW) Turbomeca Arriel 1D1 Empty weight: 2,581 lb (1,171 kg) Max take-off weight: 4,960 lb (2,250 kg), 5,511 lb (2,500 kg) with external load Useful load: 2,379 lb (1,079 kg) Cabin length: 7.94 ft (2.42 m) at floor Cabin width: 5 ft 4.9 (1.65 m) Cabin height: 4.27 ft (1.3 m) Max seating: 7 HIGE: 9,843 ft (3,000 m) HOGE: 7,546 ft (2,300 m) Max cruise: 133 kt (246 kph) Economic cruise: 122 kt (226 kph) Range: 362 nm (670 km)

Eurocopter AS 350 B3

Rotor diameter: 35 ft 0.8 in (10.69 m) Fuselage length: 35.85 ft (10.93 m) Overall length: 42.45 ft (12.94 m) Powerplant: 1 x 848 shp (632 kW) Turbomeca Arriel 2B turboshaft Empty weight: 2,588 lb (11,74 kg) Max takeoff weight: 4,960 lb (2,250 kg), 6,062 lb (2,750 kg) with external load Useful load: 2,372 lb (1,076 kg) Cabin length: 7.94 ft (2.42 m) at floor Cabin width: 5 ft 4.9 (1.65 m) Cabin height: 4.27 ft (1.3 m) Max seating: 7 HIGE: 12,927 ft (3,940 m) HOGE: 11,549 ft (3,520 m) Max cruise: 140 kt (260 kph) Economic cruise: 122 kt (226 kph) Range: 356 nm (660 km)

Eurocopter AS 350 BA

Rotor diameter: 35.07 ft (10.69 m) Fuselage length: 35.86 ft (10.93 m) Overall length: 42.45 ft (12.94 m) Powerplant: 1 x 640 shp (477 kW) Turbomeca Arriel 1B turboshaft Empty weight: 2,566 lb (1,164 kg) Max take-off weight: 4,960 lb (2,250 kg),with ext load Useful load: 2,064 lb (936 kg) Cabin length: 7.94 ft (2.42 m) at floor Cabin width: 5.41 ft (1.65 m) Cabin height: 4.27 ft (1.3 m) Max seating: 7 HIGE: 9,154 ft (2,790 m) HOGE: 6,496 ft (1,980 m) Max cruise: 126 kt (234 kph) Economic cruise: 123 kt (228 kph) Range: 394 nm (730 km)

Eurocopter AS 355 N

Rotor diameter: 35.07 ft (10.69 m) Fuselage length: 35.86 ft (10.93 m) Overall length: 42.45 ft (12.94 m) Powerplant: 2 x 456 shp (340 kW) Turbomeca Arrius 1A turboshafts Empty weight: 3,165 lb (1,436 kg) Max take-off weight: 5,731 lb (2,600 kg),with ext load Useful load: 2,567 lb (1,164 kg ) Cabin length: 7.94 ft (2.42 m) Cabin width: 5.41 ft (1.65 m) Cabin height: 4.27 ft (1.3 m) Max seating: 7 HIGE: 6,726 ft (2,050 m) HOGE: 2,625 ft (800 m) Max cruise: 121 kt (224 kph) Economic cruise: 116 kt (215 kph) Range: 386 nm (715 km)

Eurocopter AS 365 N2 Dauphin

Rotor diameter: 39.14 ft (11.93 m) Fuselage length: 38.16 ft (11.63 m) Overall length: 45.05 ft (13.73m) Powerplant: 2 x 736 shp (550 kW) Turbomeca Arriel 1C2 turboshafts Empty weight: 5,006 lb (2,271 kg) Max take-off weight: 9,369 lb (4,250 kg) Useful load: 4,363 lb (1,979 kg) Cabin length: 7.22 ft (2.2 m) at floor Cabin width: 6.30 ft (1.92 m) Cabin height: 4.59 ft (1.4 m) Max seating: 13 HIGE: 6,562 ft (2,000 m) HOGE: 3,937 ft (1,200 m) Max cruise: 150 kt (277 kph) Economic cruise: 137 kt (254 kph) Range: 465 nm (861 km)

Eurocopter AS 365 N3 Dauphin

Rotor diameter: 39.14 ft (11.93 m) Fuselage length: 38.16 ft (11.63 m) Overall length: 45.05 ft (13.73m) Powerplant: 2 x 851 shp (635 kW) Turbomeca Arriel 2C turboshafts Empty weight: 5,072 lb (2,301 kg) Max take-off weight: 9,369 lb (4,250 kg) Useful load: 4,297 lb (1,949 kg) Cabin length: 7.22 ft (2.2 m) at floor Cabin width: 6.30 ft (1.92 m) Cabin height: 4.59 ft (1.4 m) Max seating: 13 HIGE: 6,234 ft (1,900 m) HOGE: 5,085 ft (1,550 m) Max cruise: 150 kt (277 kph) Economic cruise: 146 kt (271 kph) Range: 442 nm (819 km)

Eurocopter BO 105 CB

Rotor diameter: 32.28 ft (9.84 m) Fuselage length: 28.08 ft (8.56 m) Overall length: 38.91 ft (11.86 m) Powerplant: 2 x 420 shp (313 kW) Allison 250-C20B turboshafts Empty weight: 2,813 lb (1,276 kg) Max take-off weight: 5,511 lb (2,500 kg) Useful load: 2,698 lb (1,224 kg) Cabin length: 7.17 ft (2.185 m) Cabin width: 4.27 ft (1.3 m) Cabin height: 3.84 ft (1.17 m) Max seating: 6 HIGE: 5,000 ft (1,524 m) HOGE: 1,500 ft (457 m) Max cruise: 130 kt (240 kph) Economic cruise: 111 kt (205 kph) Range: 300 nm (555 km)

Eurocopter EC 120 B

Rotor diameter: 32.81 ft (10 m) Fuselage length: 31.5 ft (9.6 m) Overall length: 37.86 ft (11.52 m) Powerplant: 1 x 504 shp (376 kW) Turbomeca Arrius 2F turboshaft Empty weight: 1,929 lb (875 kg) Max take-off weight: 3,750 lb (1,700 kg) Useful load: 1,655 lb (750 kg) Cabin length: 7.55 ft (2.3 m) Cabin width: 4.43 ft (1.35 m) Cabin height: 4.10 ft (1.25 m) Max seating: 5 HIGE: 10,499 ft (3,200 m) HOGE: 7,999 ft (2,438 m) Max cruise: 124 kt (230 kph) Economic cruise: 110 kt (204 kph) Range: 395 nm (732 km)

Eurocopter EC 130

Rotor diameter: 35.07 ft (10.69 m) Fuselage length: 35.03 ft (10.68 m) Overall length: 41.47 ft (12.64 m) Powerplant: 1 x 847 shp (632 kW) Turbomeca Arriel 2B1 turboshaft Empty weight: 2,998 lb (1,360 kg) Max take-off weight: 5,291 lb (2,400 kg) Useful load: 2,293 lb (1,040 kg) Cabin length: 7.185 ft (2.19 m) Cabin width: 6.12 ft (1.865 m) Cabin height: 3.85 ft (1.175 m) Max seating: 8 HIGE: 10,720 ft (3,265 ft) HOGE: 8,740 ft (2,660 m) Max cruise: 127 kt (235 kph) Economic cruise: N/A Range: 358 nm (662 km) to dry tanks at fast cruise speed

Eurocopter EC 135 P1

Rotor diameter: 33.46 ft (10.2 m) Fuselage length: 33.33 ft (10.16 m) Overall length: 39.7 ft (12.1 m) Powerplant: 2 x 621shp (463 kW) Pratt & Whitney Canada PW 206Bs Empty weight: 3,174 lb (1,440 kg) Max take-off weight: 6,000 lb (2,720 kg) Useful load: 2,734 lb (1,240 kg) Cabin length: 10.04 ft (3.06 m) at floor Cabin width: 4.91ft (1.496 m) Cabin height: 4.22 ft (1.285 m) Max seating: 8 HIGE: 14,599 ft (4,450 m) HOGE: 11,401 ft (3,600 m) Max cruise: 139 kt (257 kph) Economic cruise: 134 kt (249 kph) Range: 362 nm (670 km)

Eurocopter EC 135 T1

Rotor diameter: 33.46 ft (10.2 m) Fuselage length: 33.33 ft (10.16 m) Overall length: 39.7 ft (12.1 m) Powerplant: 2 x 732 shp (546 kW) Turbomeca Arrius 2B1 Empty weight: 3,148 lb (1,428 kg) Max take-off weight: 6,000 lb (2,720 kg) Useful load: 2,767 lb (1,255 kg) Cabin length: 10.04 ft (3.06 m) at floor Cabin width: 4.91 ft in (1.496 m) Cabin height: 4.22 ft (1.285 m) Max seating: 8 HIGE: 14,205 ft (4,330 m) HOGE: 12,139 ft (3,475 m) Max cruise: 139 kt (257 kph) Economic cruise: 134 kt (249 kph) Range: 356 nm (660 km)

Eurocopter EC 145

Rotor diameter: 36.08 ft (11 m) Fuselage length: 33.43 ft (10.19 m) Overall length: 42.74 ft (13.03 m) Powerplant: 2 x 750 shp (550 kW) Turbomeca Arriel 1E2 turboshafts Empty weight: 1,742 kg Max take-off weight: 3,550 kg Useful load: 1,728 kg Cabin length: 3,44 m, excluding cockpit Cabin width: 1.57 m max, 1.40 m in rear Cabin height: 1.27 m max, 0.99 m in rear Max seating: 12 HIGE: 2,130 m HOGE: 10,000 ft (3,048 m) at 7,500 lb (3,400 kg) in ISA Max cruise: 245 kph Economic cruise: 243 kph Range: 670 km

Eurocopter EC 155

Rotor diameter: 41.34 ft (12.6 m) Fuselage length: 41.76 ft (12.73 m) Overall length: 46.91 ft (14.30 m) Powerplant: 2 x 851 shp (635 kW) Turbomeca Arriel 2C1 turboshafts Empty weight: N/A Max take-off weight: 10,582 lb (4,800 kg) Useful load: 4,887 lb (2,217 kg) including mission fuel Cabin length: 8.2 ft (2.5 m) Cabin width: Four seats Cabin height: 5.18 ft (1.58 m) Max seating: 14 HIGE: N/A HOGE: N/A Max cruise: 143 kt (266 kph) Economic cruise: 136 kt (252 kph) Range: 450 nm (831 km) with std tanks

Eurocopter EC 225

Rotor diameter: 53.14 ft (16.2 m) Fuselage length: 55 ft (16.79 m) Overall length: 63.98 ft (19.5 m) Powerplant: 2 x 2,413 shp (1,800 kW) Turbomeca Makila 1A4 turboshafts Empty weight: N/A Max take-off weight: 22,930 lb (10,400 kg) with internal load, 24,700 lb (11,200 kg) with external load Useful load: 11,870 lb (5,380 kg) with internal load Cabin length: 18.67 ft (5.69 m) at floor Cabin width: 5.91 ft (1.8 m) Cabin height: 4.76 ft (1.45 m) Max seating: 27 HIGE: N/A HOGE: N/A Max cruise: 156 kts Economic cruise: N/A Range: 783 nm

Kaman K-1200 K-MAX

Rotor diameter: 48 ft 4 in (14.68 m) Fuselage length: 41 ft 9 in (12.72 m) Overall length: 52 ft (15.85 m) Powerplant: 1 x derated 1,800 shp (1,343 kW) AlliedSignal Lycoming T53-17A-1 Empty weight: 5,100 lb (2,491 kg) Max takeoff weight: 6,500 lb (2,949 kg) without external load, 12,000 lb (5,862 kg) with external load Useful load: 6,000 lb (2,722 kg) Cabin length: 5 ft (1.52 m) Cabin width: 3.17 ft (0.97 m) Cabin height: 4.17 ft (1.27 m) Max seating: 1 HIGE: 29,120 ft (8,876 m) at max gross weight HOGE: 26,300 ft (8,016 m) at max gross weight Max cruise: 100 kt (185.2 kph) Economic cruise: 85 kt (157 kph) Range: 270 nm (500 km)

Kamov Ka 126

Rotor diameter: 42.65 ft (13 m) Fuselage length: 25.5 ft (7.775 m) Overall length: 42.65 ft (13m) Powerplant: 1 x 720 shp (530 kW) Mars TV-O-100 turboshaft Empty weight: 4,222 lb (1,915 kg) Max take-off weight: 7,165 lb (3,250 kg) Useful load: 2,943 lb (1,335 kg) Cabin length: 6.69 ft (2.04 m) Cabin width: 4.1 ft (1.25 m) Cabin height: 4.5 ft (1.40 m) Max seating: 10 HIGE: 3,182 ft (970 m) HOGE: 262 ft (80 m) Max cruise: 100 kt (180 kph) Economic cruise: 88.9 kt (160 kph) Range: 384.73 nm (713 km) sf

Kamov Ka 226

Rotor diameter: 42.65 ft (13 m) Fuselage length: 26.57 ft (8.1 m) Overall length: 42.65 ft (13m) Powerplant: 2 x 450 shp (331 kW) Allison 250-C20R1 turboshafts Empty weight: 4,303 lb (1,952 kg) Max take-off weight: 7,496 lb (3,400 kg) Useful load: 3,190 lb (1,448 kg) Cabin length: 7.71 ft (2.35 m) Cabin width: 5.5 ft (1.54 m) Cabin height: 4.52 ft (1.40 m) Max seating: 10 HIGE: 10,330 ft (3,150 m) HOGE: 8,100 ft (2,470 m) Max cruise: 118 kt (214 kph) Economic cruise: 108 kt (194 kph) Range: 341 nm (620 km)

Kamov Ka 32

Rotor diameter: 52 ft 2 in (15.9 m) Fuselage length: 37 ft 1 in (11.22 m) Overall length: 52 ft 2 in (15.9 m) RT Powerplant: 2 x 2,200 shp (1,619 kW) Klimov TV3- 117VMA turboshafts Empty weight: 14,990 lb (6,800 kg) Max take-off weight: 24,250 lb (11,000 kg) Useful load: 11,000 lb (5,000 kg) on hook Cabin length: 14 ft 10 in (4.52 m) Cabin width: 4 ft 3 in (1.3 m) Cabin height: 4 ft 4 in (1.24 m) Max seating: 18 HIGE: 14,107 ft (4,300 m) HOGE: 12,140 ft (3,700 m) Max cruise: 144 kt (260 kph) Economic cruise: 126 kt (230 kph) Range: 350 nm (650 km) sf, nr

Kamov Ka-62

Rotor diameter: 44.3 ft (13.5 m) Fuselage length: 43.47 ft (13.25 m) Overall length: 51.84 ft (15.80 m) RT Powerplant: 2 x 1,300 shp (970 kW) RKBM Rybinsk RD-600 turboshafts Empty weight: 8,223 lb (3,730 kg) Max take-off weight: 13,779 lb (6,250 kg) or 14,329 lb (6,500 kg) with external load Useful load: 4,409 lb (2,000 kg) or 5,511 lb (2,770 kg) on hook Cabin length: 7.49 ft (2.28 m) Cabin width: 5.83 ft (1.78 m) Cabin height: 4.26 ft (1.30 m) Max seating: 18 HIGE: 9,514 ft (2,900 m) HOGE: 6,890 ft (2,100 m) Max cruise: 167 kt (300 kph) Economic cruise: 144 kt (260 kph) Range: 378 nm (700 km) sf, nr

Kazan Aktai

Rotor diameter: 32 ft 9.75 in (10 m) Fuselage length: 27 ft 4.75 in (8.35 m) Overall length: 35 ft 8.25 in (10.88 m) Powerplant: 1 x 240 hp (179 kW) RPD VAZ 4265 rotary engine Empty weight: 1,334 lb (605 kg) Max take-off weight: 2,535 lb (1,150 kg) Useful load: 1,201 lb (535 kg) Cabin length: 3 ft 11.75 in (1.2 m) Cabin width: 5 ft 7 in (1.7 m) Cabin height: N/A Max seating: 0 HIGE: 7,550 ft (2,300 m) HOGE: 4,265 ft (1,300 m) Max cruise: 103 kt (190 kph) Economic cruise: 84 kt (155 kph) Range: 324 nm (600 km) Endurance: 7 hr

Kazan Ansat

Rotor diameter: 37.75 ft (11.5 m) Fuselage length: 37.9 ft (11.538 m) Overall length: 45 ft (13.768 m) Powerplant: 2 x Pratt & Whitney/Klimov PK 206C turboshafts Empty weight: N/A Max take-off weight: 7,275 lb (3,300 kg) Useful load: 3,637 lb (1,650 kg) Cabin length: N/A Cabin width: N/A Cabin height: N/A Max seating: 9 HIGE: N/A HOGE: 5,900 ft (1,800 m) Max cruise: 128 kt (238 kph) Economic cruise: 75.5 kt (140 kph) Range: 281 nm (520 km)

MD Helicopters MD 500E

Rotor diameter: 26.4 ft (8.05 m) Fuselage length: 24.6 ft (7.49 m) Overall length: 30 ft 10 in (9.4 m) Powerplant: 1 x 420 shp (313 kW) Allison 250-C20B turboshaft Empty weight: 1,481 lb (672 kg) Max take-off weight: 3,000 lb (1,361 kg) Useful load: 1,519 lb (689 kg) Cabin length: 8 ft (2.44 m) Cabin width: 4 ft 3.5 in (1.31 m) Cabin height: 5 ft (1.52 m) Max seating: 5 HIGE: 8,500 ft (2,590 m) HOGE: 6,000 ft (1,830 m) Max cruise: 134 kt (248 kph) Economic cruise: 129 kt (239 kph) Range: 264 nm (488 km)

MD Helicopters MD 520N

Rotor diameter: 27.4 ft (8.34 m) Fuselage length: 25 ft 6 in (7.8 m) Overall length: 28 ft 6 in (8.7 m) Powerplant: 1 x 450 shp (317 kW) Allison 250-C20R turboshaft Empty weight: 1,586 lb (719 kg) Max take-off weight: 3,350 lb (1,519 kg) Useful load: 1,764 lb (800 kg) Cabin length: 8 ft (2.44 m) Cabin width: 4 ft 3.5 in (1.31 m) Cabin height: 5 ft (1.52 m) Max seating: 5 HIGE: 9,300 ft (2,835 m) HOGE: 5,600 ft (1,707 m) Max cruise: 124 kt (230 kph) Economic cruise: N/A Range: 201 nm (389 km)

MD Helicopters MD 530F

Rotor diameter: 27.4 ft (8.34 m) Fuselage length: 24.6 ft (7.5 m) Overall length: 32 ft 1 in (9.78 m) Powerplant: 1 x 650 shp (484 kW) Allison 250-C30 turboshaft Empty weight: 1,509 lb (684 kg) Max take-off weight: 3,100 lb (1,406 kg) Useful load: 1,591 lb (722 kg) Cabin length: 8 ft (2.44 m) Cabin width: 4 ft 3.5 in (1.31 m) Cabin height: 5 ft (1.52 m) Max seating: 5 HIGE: 16,000 ft (4,877 m) HOGE: 14,400 ft (4,389 m) Max cruise: 133 kt (246 kph) Economic cruise: 131 kt (243 kph) Range: 232 nm (430 km)

MD Helicopters MD 600N
|
Rotor diameter: 27.5 ft (8.4 m) Fuselage length: 30.5 ft (9.3 m) Overall length: 36.9 ft (11.2 m) Powerplant: 1 x 808 shp (603 kW) Allison 250-C47 turboshaft Empty weight: 1,930 lb (875 kg) Max take-off weight: 4,100 lb (1,860 kg) Useful load: 2,120 lb (961 kg) Cabin length: 10.5 ft (3.2 m) Cabin width: 4.6 ft (1.4 m) Cabin height: 5 ft (1.52 m) Max seating: 8 HIGE: 11,100 ft (3,383 m) HOGE: 6,000 ft (1,828m) Max cruise: 136 kt (252 kph) Economic cruise: 125 kt (231 kph) Range: 380 nm (704 km)

MD Helicopters MD Explorer

Rotor diameter: 33 ft 10 in (10.32 m) Fuselage length: 32.4 ft (9.9 m) Overall length: 38 ft 3 in (11.7 m) Powerplant: 2 x 710 shp (529 kW) Pratt & Whitney Canada PW 207E turboshafts Empty weight: 3,375 lb (1,531 kg) Max take-off weight: 6,500 lb (2,948 kg) Useful load: 3,125 lb (1,599 kg) Cabin length: 6 ft 3 in (1.91 m) exc cockpit Cabin width: 4 ft 9 in (1.45 m) Cabin height: 4 ft 7 in (1.4 m) Max seating: 8 HIGE: 12,200 ft (3,719 m) HOGE: 10,000 ft (3,048 m) Max cruise: 135 kt (250 kph) Economic cruise: 123 kt (158kph) Range: 293 nm (543 km)

Mil (Kazan) Mi-17/Mi-172

Rotor diameter: 69 ft 10.5 in (21.29 m) Fuselage length: 60 ft 5.75 in (18.42 m) Overall length: 83 ft 2 in (25.35 m) Powerplant: 2 x 2000 shp (1470 kW) Klimov TV3 117MT turboshafts Empty weight: 15,653 lb (7,100 kg) Max take-off weight: 28,660 lb (13,000 kg) Useful load: 13,007 lb (5,900 kg) Cabin length: 17.51 ft (5.37 m ) Cabin width: 7 ft 8.25 in (2.34 m) Cabin height: 5 ft 10.25 in (1.8 m) Max seating: 24 HIGE: 7,213 ft (2,200 m) HOGE: 5,775 ft (1,760 m) Max cruise: 134.9 kt (250 kph) Economic cruise: 130 kt (240 kph) Range: 318 nm (590 km)

Mil (Ulan Ude) Mi-171

Rotor diameter: 69 ft 10.5 in (21.29 m) Fuselage length: 60 ft 5.75 in (18.42 m) Overall length: 83 ft 2 in (2.535 m) Powerplant: 2 x 2,070 shp (1,545 kW) Klimov TV3 117VM turboshafts Empty weight: 15,653 lb (7,100 kg) Max take-off weight: 28,660 lb (13,000 kg) Useful load: 13,007 lb (5,900 kg) Cabin length: 20 ft 10.25 in (6.36 m) Cabin width: 7 ft 8.25 in (2.34 m) Cabin height: 5 ft 10.25 in (1.8 m) Max seating: 24 HIGE: N/A HOGE: 5,775 ft (1,760 m) Max cruise: 113 kt (210 kph) Economic cruise: N/A Range: 307 nm (570 km)

Mil (Ulan Ude) Mi-8T

Rotor diameter: 69 ft 10.25 in (21.29 m) Fuselage length: 60.80 ft (18.547 m) Overall length: 82 ft 10 in (25.24 m) Powerplant: 2 x 1500 shp (1103 kW) Klimov TV2 117A turboshafts Empty weight: 15,382 lb (6,968 kg) Max take-off weight: 26,455 lb (12,000 kg) Useful load: 11,108 lb (5,032 kg) Cabin length: 17.51 ft (5.37 m) Cabin width: 7 ft 8.25 in (2.34 m) Cabin height: 5 ft 11 in (1.8 m) Max seating: 30 HIGE: 6,235 ft (1,900 m) HOGE: 2,625 ft (800 m) Max cruise: 134.9 kt (250 kph) Economic cruise: 118.7 kt (220 kph) Range: 288.7 nm (535 km)

Mil Mi-26T

Rotor diameter: 105 ft (32 m) Fuselage length: 110 ft 8 in (33.3 m) Overall length: 131 ft 3.75 in (40.03 m) Powerplant: 2 x 10,000 (7352 kW) ZMKB Progress D-136 turboshafts Empty weight: 63,134 lb (28,600 kg) Max take-off weight: 123,458 lb (56,000 kg) Useful load: 60,486 lb (27,400 kg) Cabin length: 39 ft 4.25 in (12 m) Cabin width: 10 ft 6 in (3.2 m) Cabin height: 10 ft 4.25 in (3.17 m) Max seating: 85 HIGE: 8,852 ft (2,700 m) HOGE: 5,574 ft (1,700 m) Max cruise: 159 kt (295 kph) Economic cruise: 137 kt (255 kph) Range: 383 nm (710 km)

Mil Mi-34C

Rotor diameter: 32 ft 10 in (10 m) Fuselage length: 29 ft (8.85 m) Overall length: 37.4 ft (11.71 m) Powerplant: 1 x 325 hp (239 kW) M14 V26 radial piston engine Empty weight: 2,252 lb (1,020 kg) Max take-off weight: 3,201 lb (1,450 kg) Useful load: 949 lb (430 kg) Cabin length: 2.1 ft (0,96 m) exc cockpit Cabin width: 4 ft (1.23 m) Cabin height: 4.13 ft (1.26 m) Max seating: 4 HIGE: N/A HOGE: 2,950 ft (900 m) Max cruise: 116 kt (215 kph) Economic cruise: 92 kt (170 kph) Range: 194 nm (360 km)

Mitsubishi MH2000A

Rotor diameter: 12.2 m (40 ft 0.25 in) Fuselage length: 12.2 m (40 ft 0.25 in) Overall length: 14 m (45 ft 11.25 in) Powerplant: 2 x 876 shp Mitsubishi MG5-110 turboshafts Empty weight: 2,500 kg (5,510 lb) Max take-off weight: 4,500 kg (9,920 lb) Useful load: 2,000 kg (4,410 lb) Cabin length: 6.88 ft (2.1 m) Cabin width: 6.56 ft (2.0 m) Cabin height: 4.59 ft (1.4 m) Max seating: 10 HIGE: 2,700 m (8,860 ft) @ MTOW HOGE: 1,650 m (5,400 ft) @ MTOW Max cruise: 250 kph (135 kt) Economic cruise: 228 kph (123 kt) Range: 780 km (420 nm) @ cruise speed, standard tanks, no reserve

PZL Kania

Rotor diameter: 47.8 ft (14.56 m) Fuselage length: 39.47 ft (12.03 m) Overall length: 57.07 ft (17.4 m) Powerplant: 2 x 426 shp (313 kW) Allison 250-C20B turboshafts Empty weight: 4,320 lb (1,960 kg) Max take-off weight: 7,826 lb (3,550 kg) Useful load: 3,505 lb (1,590 kg) Cabin length: 13.35 ft (4.07 m) Cabin width: 4.92 ft (1.5 m) Cabin height: 4.95 ft (1.51 m) Max seating: 14 HIGE: 8,202 ft (2,500 m) HOGE: 4,511 ft (1,375 m) Max cruise: 113 kt (210 kph) Economic cruise: 103 kt (190 kph) Range: 479 nm (886 km)

PZL Mi-2

Rotor diameter: 47.8 ft (14.56 m) Fuselage length: 39.2 ft (11.94 m) Overall length: 57.4 ft (17.42 m) Powerplant: 2 x 425 shp (312 kW) GTD 350 turboshafts Empty weight: 5,313 lb (2,410 kg) Max take-off weight: 7,826 lb (3,550 kg) Useful load: 2,513 lb (1,140 kg) Cabin length: 7.44 ft (2.27 m) Cabin width: 4.92 ft (1.5 m) Cabin height: 4.6 ft (1.4 m) average Max seating: 10 HIGE: 5,167 ft (1,575 m) HOGE: 2,870 ft (875 m) Max cruise: 105 kt (190 kph) Economic cruise: 99.5 kt (180 kph) Range: 315 nm (580 km)

PZL SW-4

Rotor diameter: 29.5 ft (9 m) Fuselage length: 27 ft (8.25 m) Overall length: 29.7 ft (9.07 m) Powerplant: 1 x 450 shp (336 kW) Allison 250-C20R /2 (SP) turboshaft Empty weight: 2,094 lb (950 kg) Max take-off weight: 3,968 lb (1,800 kg) Useful load: 1,874 lb (850 kg) Cabin length: 7.67 ft (2.34 m) Cabin width: 4.92 ft (1.5 m) Cabin height: 4.3 ft (1.31 m) Max seating: 5 HIGE: 7,544 ft (2,300 m) HOGE: 5,412 ft (1,650 m) Max cruise: 125.4 kt (232 kph) Economic cruise: 108.1 kt (200 kph) Range: 468.9 nm (860 km)

PZL W-3A Sokol

Rotor diameter: 51.5 ft (15.7 m) Fuselage length: 46.6 ft (14.2 m) Overall length: 61.65 ft (18.79 m) Powerplant: 2 x 900 shp (662 kW) PZL -10W turboshafts Empty weight: 8,487 lb (3,850 kg) Max take-off weight: 14,110 lb (6,400 kg) Useful load: 5,623 lb (2,550 kg) Cabin length: 10 ft 6 in (3.2 m) Cabin width: 5.08 ft (1.55 m) Cabin height: 4 ft 8 in (1.4 m) Max seating: 14 HIGE: 9,906 ft (3,020 m) HOGE: 6,232 ft (1,900 m) Max cruise: 127 kt (235 kph) Economic cruise: 120 kt (222 kph) Range: 672 nm (1,244 km)

Robinson R22 Beta II

Rotor diameter: 25.2 ft (7.67 m) Fuselage length: 20.7 ft (6.3 m) Overall length: 28.7 ft (8.76 m) Powerplant: 1 x 131 hp (94.3 kW) Textron Lycoming O- 360-J2A piston engine Empty weight: 845 lb (384 kg) Max take-off weight: 1,370 lb (621 kg) Useful load: 525 lb (239 kg) Cabin length: 4.3 ft (1.31 m) Cabin width: 3.6 ft (1.1 m) Cabin height: 4 ft (1.22 m) Max seating: 2 HIGE: 9,400 ft (2,865 m) HOGE: N/A Max cruise: 96 kt (177 kph) Economic cruise: 83 kt (154 kph) Range: 319 nm (592 km)

Robinson R44

Rotor diameter: 33 ft (10.05 m) Fuselage length: 29.7 ft (9.07 m) Overall length: 38.6 ft (11.76 m) Powerplant: 1 x 225 hp (167 kW) Textron Lycoming O- 540-F1B5 piston engine Empty weight: 1,424 lb (645 kg) Max take-off weight: 2,400 lb (1,089 kg) Useful load: 976 lb (443 kg) Cabin length: 6.9 ft (2.09 m) Cabin width: 4.2 ft (1.27 m) Cabin height: 4.3 ft (1.31 m) Max seating: 4 HIGE: 6,400 ft (1,950 m) HOGE: 5,100 ft (1,554 m) at 2,200 lb (997 kg) gross weight Max cruise: 113 kt (209 kph) Economic cruise: 100 kt (185.2 kph) Range: 347 nm (643 km)

Rotorway EXEC 162 F

Rotor diameter: 25 ft (7.62 m) Fuselage length: 22 ft (6.705 m) Overall length: N/A Powerplant: 1 x 150 hp (111 kW) 4-cyl, 162 in3 RI 162F four-stroke Empty weight: 975 lb (442.2 kg) Max take-off weight: 1,500 lb (680.4 kg) Useful load: 525 lb (238.14 kg) Cabin length: N/A (two seats) Cabin width: N/A (two seats) Cabin height: N/A (two seats) Max seating: 2 HIGE: 7,000 ft (2,134 m) HOGE: 5,000 ft (1,524 m) Max cruise: 100 kt (185 kph) 115 mph Economic cruise: 95 mph (152.9 kph) Range: 180 sm (289.67 km)

Schweizer 300C

Rotor diameter: 26.8 ft (8.2 m) Fuselage length: 22.19 ft (6.76 m) Overall length: 30.8 ft (9.39 m) Powerplant: 1 x 190 hp (141 kW) AlliedSignal Lycoming HIO-360-D1A piston engine Empty weight: 1,100 lb (499 kg) Max take-off weight: 2,050 lb (930 kg) Useful load: 950 lb (431 kg) Cabin length: 4.1 ft (1.25 m) Cabin width: 4.7 ft (1.43 m) Cabin height: 4.2 ft (1.28 m) Max seating: 3 HIGE: 10,800 ft (3,292 m) at 1,700 lb HOGE: 8,600 ft (2,612 m) at 1,700 lb Max cruise: 86 kt (159 kph) Economic cruise: 64 kt (118 kph) VNE is 95 kt (176 kph) Range: 194 nm (360 km)

Schweizer 300CB

Rotor diameter: 26.8 ft (8.2 m) Fuselage length: 22.19 ft (6.76 m) Overall length: 30.8 ft (9.39 m) Powerplant: 1 x 180 hp (134 kW) AlliedSignal Lycoming HO-360-C1A piston engine Empty weight: 1,088 lb (493.5 kg) Max take-off weight: 1,750 lb (793.8 kg) Useful load: 662 lb (300.3 kg) Cabin length: 4.1 ft (1.25 m) Cabin width: 4.7 ft (1.43 m) Cabin height: 4.2 ft (1.28 m) Max seating: 3 HIGE: 7,000 ft (2,133 m) HOGE: 4,800 ft (1,463 m) Max cruise: 85 kt (157 kph) VNE is 94 kt (174 kph) Economic cruise: 72 kt (133 kph) at gross weight Range: 240 nm (386 km) with 35 gal ; 440 nm (708 km) with 65 gal

Schweizer 333

Rotor diameter: 27.51 ft (8.39 m) Fuselage length: 22.38 ft (6.82 m) Overall length: 31.17 ft (9.51 m) Powerplant: 1 x derated 420 shp (313 kW) Allison 250- C20W turboshaft Empty weight: 1,250 lb (567 kg) Max take-off weight: 2,550 lb (1,1257kg) Useful load: 1,300 lb (590 kg) Cabin length: 6.5 ft (1.98 m) Cabin width: 5.7 ft (1.73 m) Cabin height: 4.4 ft (1.34 m) Max seating: 4 HIGE: 11,900 ft (3,627 m) at 2,300 lb HOGE: 8,500 ft (2,591 m) at 2,300 lb Max cruise: 105 kt (192 kph) Economic cruise: 95 kt (176 kph) Range: 310 nm (574 km)

Sikorsky S-76B

Rotor diameter: 44 ft (13.41 m) Fuselage length: 43 ft 4 in (13.22 m) Overall length: 52 ft 6 in (16 m) Powerplant: 2 x 981 shp (731 kW) Pratt & Whitney Canada PT6B-36B turboshafts Empty weight: 8,620 lb (3,909 kg) Max takeoff weight: 11,700 lb (5,306 kg) Useful load: 3,080 lb (1,395 kg) Cabin length: 8 ft 1 in (2.46 m) Cabin width: 6 ft 4 in (1.93 m) Cabin height: 4 ft 5 in (1.35 m) Max seating: 14 HIGE: 8,000 ft (2,438 m) HOGE: 3,750 ft (1,143 m) Max cruise: 155 kt (287 kph) Economic cruise: 139 kt (257 kph) Range: 350 nm (649 km)

Sikorsky S-76C+

Rotor diameter: 44 ft (13.41 m) Fuselage length: 43 ft 4 in (13.22 m) Overall length: 52 ft 6 in (16 m) Powerplant: 2 x 856 shp (638 kW) Turbomeca Arriel 2S1 turboshafts Empty weight: 8,138 lb (3,691 kg) Max take-off weight: 11,700 lb (5,306 kg) Useful load: 3,562 lb (1,616 kg) Cabin length: 8 ft 1 in (2.46 m) Cabin width: 6 ft 4 in (1.93 m) Cabin height: 4 ft 5 in (1.35 m) Max seating: 14 HIGE: 5,650 ft (1,722 m) HOGE: 1,800 ft (549 m) Max cruise: 155 kt (287 kph) Economic cruise: 140 kt (260 kph) Range: 439 nm (813 km)

Sikorsky S-76C++

Rotor diameter: 44 ft (13.41 m) Fuselage length: 43 ft 4 in (13.22 m) Overall length: 52 ft 6 in (16 m) Powerplant: 2 x 923 shp (688 kW) Turbomeca Arriel 2S2 turboshafts Empty weight: 7,005 lb (3,177 kg) in utility configuration Max take-off weight: 11,700 lb (5,306 kg) Useful load: 4,695 lb (2,129 kg) in utility configuration Cabin length: 8 ft 1 in (2.46 m) Cabin width: 6 ft 4 in (1.93 m) Cabin height: 4 ft 5 in (1.35 m) Max seating: 14 HIGE: 7,050 ft (2,149 m) at take-off power Service ceiling: 4,900 ft (1,493 m) single engine HOGE: 3,300 ft (1,006 m) Max cruise: 155 kt (287 kph) Economic cruise: 137 kt (254 kph) Range: 345 nm (639 km) with 30 min reserve

Sikorsky S-92

Rotor diameter: 57 ft 5 in (17.50 m) Fuselage length: 68 ft 6 in (20.67 m) Overall length: 68 ft 6 in (20.87 m) including rotors Powerplant: 2 x 2,520 shp (1,879 kW) General Electric CT7-8 turboshafts Empty weight: 15700 lb (7,030 kg) Max take-off weight: 26,150 lb (11,861 kg) internal load ; 28,300 lb (12,845 kg) external load Useful load: N/A Cabin length: 20 ft 0 in (6.10 m) Cabin width: 6 ft 7 in (2.00 m) Cabin height: 6 ft (1.83 m) Max seating: 22 HIGE: 10,700 ft (3,261 m) HOGE: 6,370 ft (1,942 m) Max cruise: 151 kt (283 kph) Economic cruise: 137 kt (254 kph) Range: 538 nm (997km) with 19 pax and no reserve

Tridair Gemini ST

Rotor diameter: 37 ft (11.28 m) Fuselage length: 33 ft 2.4 in (10.1 m) Overall length: 42 ft 10.2 in (13.02 m) Powerplant: 2 x 450 shp (335 kW) Allison 250- C20R turboshafts Empty weight: 2,850 lb (1,293 kg) Max take-off weight: 4,550 lb (2,064 kg) Useful load: 1,700 lb (771 kg) Cabin length: 9 ft (2.74 m) Cabin width: 4 ft 2 in (1.28 m) Cabin height: 4 ft 2.5 in (1.28 m) Max seating: 7 HIGE: 10,000 ft (3,048 m) Service ceiling: 10,000 ft (3,048 m) one engine, 20,000 ft (6,096 m) two engines HOGE: 6,900 ft (2,130 m) Max cruise: 106 kts (196.3 kph) Economic cruise: 106 kts (196.3 kph) Range: 260 nm (482 km) no reserve

Rent Bell helicopters
Rent Agusta helicopters
Rent Robinson helicopters
Rent a jet or other type of aiplane
Buy a helicopter!

Email this! (click to send an email)

« Home