Aircraft
Sikorsky S76A
Sikorsky S76A
Specification
- Passengers : 12
- Cabin Volume : 204 cu ft
- Baggage Volume : 38 cu ft
- Baggage Length : 2.9ft
- Baggage Width : 5.8ft
- Baggage Height : 2.25ft
- Payload (w/full fuel) : 1315 lbs
- Payload (w/ one hour fuel) : 2300 lbs
- Nominal Sling Load : 1,800 lbs
- Cruise Speed : 248kmh
- Max Range (w/Full Fuel) : 520 NM
- Fuel Capacity : 1064 litres
- Endurance : 4.0 hours
- Fuel Consumption : 340 litres per hour
Blueprint
Technical Data
Eurocopter AS350B3e (Airbus)
Eurocopter AS350B3e (Airbus)
Specification
General data
- Empty weight of standard aircraft: 2,780 lbs.
- Maximum takeoff weight: 5,225 lbs.
- Useful load: 2,455 lbs.
- Maximum takeoff weight (with external load): 6,172 lbs.
- Usable fuel capacity (standard tank): 143 gal.
- Powerplant: 1 Turbomeca Arriel 2D
- Cabin volume: 105.94 cu. ft.
- Baggage compartment volume: 35.3 cu.ft.
- Standard seating capacity: 1+5
- Max weight: 5,225 lbs.
- Capacity: 1 pilot + 5/6 passengers
- Powerplant: 1 Turbomeca Arriel 2D
Performance data
- Never exceed speed: 155 kts.
- Fast cruise speed: 137 kts.
- Maximum range (with no reserves): 349 nm.
- Maximum endurance (with no reserves): 4.2 hrs.
- Hover In ground effect ceiling (5 ft. skid height): 11,600 ft.
- Hover out of ground effect ceiling: 9,450 ft.
- Takeoff power: 847 shp.
- Rate of climb: 1,818 fpm.
Blueprint
Technical Data
Bell 206 L3 (Longranger)
Bell 206 L3 (Longranger)
Specification
- Type: Light Utility Helicopter
- Crew: 1 to 2
- Passengers: 6
Performance:
- Speed: 241 km/h, 130 kts, 150 mph
- Service Ceiling: 4.115 m, 13.500 ft
- Range: 630 km 340 NM, 391 mi.
Weight:
- Empty Weight: 998 kg, 2.200 lbs
- Max. Takeoff Weight: 1.882 kg, 4.150 lbs
Dimensions:
- Rotor Blades (main/tail): 2/2, 2/2
- Main Rotor Diameter: 11,28 m, 37,0 ft
- Tail Rotor Diameter: 1,65 m, 5,4 ft
- Rotor Disc Area: 99,9 m², 1075 ft²
- Length (Fuselage): 10,44 m, 34,3 ft
- Length: 12,91 m, 42,4 ft Height: 3,14 m, 10,3 ft
Blueprint
Technical Data
Bell 206 B3 (Jetranger)
Bell 206 B3 (Jetranger)
Specification
Type: multi purpose light utility helicopter
Capacity: Plenty of room for 4 passengers and 1 pilot, powerful and dependable turbine engine, best safety record in its class.
Performance:
- Standard max gross weight : 3,350lbs (1,519kg)
- Standard useful load: 1,487lbs (67kg)
- Vne (never-exceed speed): 122kn (226km/h)
- Engine Take-off power: 420shp (313kW)
- Max range: 374nm (694km)
- Max. range of 374 nautical miles at max. cruise speed, endurance of 4.5 hours at loiter speed, low acquisition costs, economical operating costs and great resale value.
Weight:
External loads of up to 1,500 lb., Rolls-Royce 250-C20J engine, rated at 420 SHP, power for speeds to 122 kts. margin-of-safety features include collective-mounted twist-grip engine throttle control and rupture-resistant fuel system.
Blueprint
Technical Data
Agusta Westland 109A
Agusta Westland 109A
Specification
Type: Light Utility Helicopter
Crew: 1 to 2
Passengers: 6 to 7
Performance:
Max. Cruise Speed: 278 km/h, 150 kts, 173 mph
Max. Speed (vne): 311 km/h, 168 kts, 193 mph
Service Ceiling: 4.572 m, 15.000 ft
Rate of climb: 503 m/min, 1650 ft/min
Range: 948 km 512 NM, 589 mi.
Weight:
- Empty Weight: 1.418 kg, 3.126 lbs
- Max. Takeoff Weight: 2.600 kg, 5.732 lbs
Dimensions:
- Rotor Blades (main/tail) : 4/2, 4/2
- Main Rotor Diameter: 11,00 m, 36,1 ft
- Tail Rotor Diameter: 2,03 m, 6,7 ft
- Rotor Disc Area: 95,0 m², 1023 ft²
- Length (Fuselage): 11,45 m, 37,6 ft
- Length: 13,04 m, 42,8 ft
- Height: 3,40 m 11,2 ft
