AirGurus Ltd. Co. | Air Ambulance Manila Philippines | Emergency Air Transport Asia

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)

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.

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Technical Data

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

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Technical Data

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.

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Technical Data

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

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Technical Data

Pilatus PC 12

Specification

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Technical Data