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Augusta Westland 139
Augusta Westland 139: Primary Role - Offshore Oil and Gas Support.
General Specification:
- Crew: 1 to 2
- Capacity: 15 passengers
- Length: 13.77 m (45 ft 2 in)
- Main rotor diameter: × 13.80 m (45 ft 3 in)
- Width: 2.26 m (10 ft 0 in)
- Height: 3.72 m (12 ft 2 in)
- Main rotor area: 149.57 m2 (1609.97 ft2)
- Empty weight: 3,622 kg (7,985 lb)
- Gross weight: 6,400 kg (14,110 lb)
- Powerplant: 2 × Pratt & Whitney Canada PT6C-67C turboshaft engine, 1,142 kW (1,531 hp) each
Performance
- Maximum speed: 310 km/h (193 mph)
- Range: 1,061 km (573 miles)
- Service ceiling: 6,098 m (20,000 ft)
- Rate of climb: 10.9 m/s (2,140 ft/min)
Bell 212 Helicopter
Bell 212: Primary Role - Offshore Oil and Gas Support, Passenger Transport, Aerial Work, Rough Terrain Field Work/Surveys
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: 1 × Pratt & Whitney Canada PT6T-3 or -3B turboshaft, 1,800 shp (1,342 kW)
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)
- Disc loading: 6.19 lb/ft² (30.22 kg/m²)
Bell 206 Long Ranger and Jet Ranger
General Characteristics for the Bell 206L and [Bell 206B3]:
| Crew: | 1 | [1] |
| Capacity: | 6 Max | [4] |
| Length: | 42.4 ft (12.91 m) | [39 ft 8 in (12.11 m)] |
| Main Rotor diameter: | 37 ft (11.28 m) | [33 ft 4 in (10.16 m)] |
| Height: | 10ft 3 in (3.14 m) | [9 ft 4 in (2.83 m)] |
| Disc Area: | 1,075 ft² (99.9 m²) | [872 ft² (81.1 m²)] |
| Empty Weight: | 2200 lb (998 kg) | [1,713 lb (777 kg)] |
| Max Take Off Weight: | 4,150 lbs (1,882 kg) | [3,200 lb (1,451 kg)] |
| Powerplant | 1 × RR/Allison 25C30P turboshaft, rated at 650 shp (485 kw) | 1 × Rolls-Royce Model 250 Allison 250-C20B Turboshaft, 450 shp ,De-rated to 317 shp due to drivetrain limitations (310 kW)] |
Bell 206L Performance
Maximum Speed:
130 knots (150 mph, 223 km/h)
130 knots (150 mph, 223 km/h)
Range:
340 nm (630 km)
340 nm (630 km)
Service Ceiling:
13,500 ft (4,115m)
13,500 ft (4,115m)
Bell 206B3 Performance
Maximum Speed:
130 knots (150 mph, 223 km/h)
130 knots (150 mph, 223 km/h)
Range:
340 nm (630 km)
340 nm (630 km)
Service Ceiling:
13,500 ft (4,115m)
13,500 ft (4,115m)
*Tiltrotor – The Future*
Aerogulf Services will be the first operator in the region and one of the first in the world to operate the AW609 Tiltrotor.
The Tiltrotor is the result of a number of high-technology developments that have allowed the manufacturer to combine the vertical take-off and landing capabilities of a helicopter with the high-speed capability and efficiencies of a conventional airplane.
The AW609 will travel at twice the speed of most conventional helicopters and have twice the range, with a maximum cruising speed of 275 knots (509 km/h) and 700+nm range (possibly achieving 1,000nm with long-range tanks installed).