Fleet

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  General characteristics

· Crew: 1 pilot

· Capacity: 4 passengers

· Length: 39 ft 8 in (12.11 m)

· Rotor diameter: 33 ft 4 in (10.16 m)

· Height: 9 ft 4 in (2.83 m)

· Disc area: 872 ft² (81.1 m²)

· Empty weight: 777 kg

· Max. takeoff weight: 1,451 kg

· Powerplant: 1 × Allison 250-C20B turboshaft,  450 shp (310 kW)

Performance

· Maximum speed: 130 knots (224 km/h, 139 mph)

· Range: 374 nmi (430 mi, 693 km)

· Service ceiling: 13,500 ft (4,115 m)

· Rate of climb: 1,350 ft/min (6.9 m/s)

· Disc loading: 4 lb/ft² (177 N/m²)

· Power/mass: 0.26 hp/lb (420 W/kg)

General characteristics

· Crew: 1

· Capacity: 1 passenger

· Length: 28 ft 8 in (8.7 m)

· Rotor diameter: 25 ft 2 in (7.7 m)

· Height: 8 ft 11 in (2.7 m)

· Disc area: 497 ft² (46.2 m²)

· Empty weight: 389 kg

· Loaded weight: 417 kg

· Max. takeoff weight: 635 kg

· Powerplant: 1 × Lycoming O-320-A2B or
 -A2C flat 4 piston engine, 124 hp (93 kW)

· Main tank total capacity: 75 litres

· Main tank usable capacity: 73 litres

Performance

· Never exceed speed: 189 km/h, 102 kts

· Cruise speed: 177 km/h, 96 kts

· Range: 386 km

· Service ceiling: 14,000 ft (4,267 m)

· Rate of climb: 1,200 ft/min (6.1 m/s)

· Disc loading: 2.61 lb/ft² (13.7 kg/m²)

· Power/mass: 0.095 hp/lb (0.147 kW/kg)

· Endurance: approx. 2 hours, with 30-minute reserve

General characteristics

Crew: 1

Length: 41' 10' 12.5 m

Height: 14' 6" 4.4 m 

Wingspan: 48' 14.6 m

Empty Weight: 2,255 kg

Gross Weight: 4,308 kg

Max Weight: 4,308 kg

Performance

Performance Range: 512 km

Cruise Speed: 204 km/h

Max Speed: 204 km/h

Climb: 1,600 ft/min (487 m/min)

Ceiling: 13,600 ft (4,145 m) 

No. of Engines: 1

Powerplant: Lycoming T53-L-13

Horsepower (each): 1400 

Main Rotor Blades: 2

Tail Rotor Blades: 2

General characteristics

Crew: 1

Capacity: up to 10 passengers

Length: 9.91 m  (fuselage length)

Height: 3.85 m  (rotors turning)

Empty weight: 1,727 kg 

Max takeoff weight: 3,350 kg 

Fuel capacity: 697 L  internal fuel

Powerplant: 2 × Textron Lycoming LTS 101-750B-1 turboshaft, 442 kW (593 hp) each

Main rotor diameter: 11.00 m 

Main rotor area: 95.03 m2

Performance

Maximum speed: 250 km/h (155 mph; 135 kn) at sea level

Never exceed speed: 278 km/h (173 mph; 150 kn)

Range: 541 km (336 mi; 292 nmi)

Service ceiling: 4,575 m  (max certified altitude)

Hover Ceiling: 3,565 m (in ground effect)

Rate of climb: 11.00 m/s

General characteristics

Crew: 1 (two for IFR operation)

Capacity: 14

Length: 57 ft 1.68 in (17.43 m)

Rotor diameter: 48 ft (14.64 m)

Height: 12 ft 6.83 in (3.83 m)

Disc area: 1,809.5 ft² (168.3 m²)

Empty weight: 6529.4 lb (2961.7 kg)

Max. takeoff weight: 11,200 lb (5,080 kg)

Powerplant: 2 × Pratt & Whitney Canada PT6T-3 

Performance

Never exceed speed: 120 knots (138 mph, 223 km/h)

Maximum speed: 120 knots (138 mph, 223 km/h)

Cruise speed: 100 knots (115 mph, 186 km/h)

Range: 237 nm (439 km)

Service ceiling: 17,400 ft (5,305 m) 

Rate of climb: 1,745 ft/min (532 m/min)