Aircraft Type

DCH6-300/400

Crew:  2 Pilots
Capacity:  19 Seats or Stretcher Capable
Max. take off weight: 5,670 kg (12,500 lb)
Max. speed:  314 km/h (170 kt)
Range:    1480 (799 NM)
Service ceiling:    7,620 m (25,000 ft)

A high winged, un-pressurized twin engine turbine powered aircraft with fixed tricycle land gear. Designed as a rugged Short Take Off and Landing (“STOL”) commuter, the Twin Otter is capable of carrying passengers and cargo into remote unimproved locations, including ski and water based operations

ATR42-320/500

Crew: 2 Pilots, 1 Cabin Attendant
Capacity:  48 Seats or Stretcher Capable
Max. take off weight:  18,600 kg (41,005 lb)
Cruise Speed:  300kt (556 km/h)
Range:  716 NM (1,326 km)
Service ceiling:  7,620m (25,000 ft)

The ATR 42-320/500 offers a combination of overall performance and comfort unmatched in its class, while keeping the competitive economics which are the trademark of ATR aircraft. A range of improvements in the field of noise and vibration have been implemented.

ATR72-500

Crew:  2 Pilots, 2 Cabin Attendants
Capacity: 70 Seats or Stretcher Capable

Empty Weight: 13,500 kg (30,000 lb)
Cruise Speed:  510 km/h (270kts)
Range:  824 NM

The ATR 72 is derived from the ATR 42 with a 4.5m stretched fuselage. The two aircraft feature a high degree of commonality: the same cross section and the same cockpit for cross-crew qualification.

The ATR 72 is recognised as the most cost effective regional aircraft, positioning it as the industry preference to serve both low-cost/low yields environment. A range of improvements in the field of noise and vibration reduction have been implemented.

Leonardo AW139

Crew: 2 Pilots Capacity: 12 Seats or Stretcher Capable Gross weight:  6,400 kg (7,000 kg or 7t) (14,110 lb) Max. Speed: 310 km/h (193mph) Range: 1061 km (572 nm, 659 mi) Service ceiling: 6,096 m (20,000 ft)

The AW139 is the market-leading medium multi engine helicopter – the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world.

The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS. It has an outstanding power to weight ratio, which provides Category A performance capabilities with no limitation in a wide range of operating conditions.

Sikorsky S76

Crew:  2 Pilots
Capacity:  12 Seats or Stretcher Capable
Gross Weight: 5,307 kg
Speed: 287km/h (155kt, 178 mph)
Range: 761 km (411 nm, 473 mi)

The Sikorsky S-76 is an American medium-size commercial utility helicopter, manufactured by the Sikorsky Aircraft Corporation. The S-76 features twin turboshaft engines, four-bladed main and tail rotors and retractable landing gear. Updated with Turbomeca Arriel 2S2.

Bell 412/212

Crew: 1 or 2 Pilots
Capacity: 12 Seats or Stretcher Capable
Max. take off weight:  5,397 kg (11,900 lb)
Max. speed:  140 kt (161 mph, 259km/h)
Range:    529 NM (up to 980 km)
Service ceiling:    20,000 ft (6,096m)

The Bell 412/212 is the daily workhorse that reliably performs in some of the most extreme climates around the world every day. Its expansive cabin provides mission flexibility.

It is a versatile machine to suit daily requirements. As one of the roomiest, most flexible and cost-effective aircraft on the market.

EC 145

Crew: 2 Pilots
Capacity: 9 Seats or Stretcher Capable
Max. take off weight:  3,584 kg (7,903 lb)
Max. speed: 278 km/h (150 kts)
Range:  439 km (237 NM)
Service ceiling: 5,485 m (18,000ft)

The EC145 is a twin-engine, multi-purpose helicopter in the 3-4 ton class with up to 12 seats for pilot/s and passengers, certified in accordance with EASA Part 29, with the designation BK117 C-2e. The EC145 is certified for single pilot VFR day/night operation with a new cockpit concept, increased payload and an increased pilot visibility in operation.

Bell 407

Crew: 1 Pilot
Capacity: 6 Seats or Stretcher Capable
Max. take off weight: 2,722 kg (6,000 lb)
Max. speed: 260 km/h (140 knots, 161 mp/h)
Range: 598 km (324 NM, 372 mi)
Service ceiling: 5,698 m (18,690 ft)

The 407 uses the four-blade, soft-in-plane design rotor with composite hub. The helicopter is versatile and is an excellent internal and external lifter.

MIL- 8 MTV

Crew: 2 Pilots, 1 Engineer Capacity:  Stretcher Capable or 4,000 kg (8,820 lb) Max. take off weight: 13,000 kg (28,660 lb) Max. speed: 280 km/h (151 knots, 175 mph) Range: 800 km (431 NM, 497 mi) Service ceiling: 6,000m (19,960 ft)

The powerful Mil MI-8-MTV is everything the world has come to expect from this multi-purpose utility helicopter. Dependable, reliable, safe and cost-effective. However, it has another singular advantage. It fits your missions as if it were made for it, as the machine was designed with adaptability in mind. The aircraft can be easily reconfigured with a lengthy list of certified operational equipment for whatever utility mission you have in mind/ With its lifting power, endurance, manoeuvrability and heavy-duty construction the MIL-MI8-MTV is always up to the challenge.

YOUR JOURNEY. OUR MISSION. 
Contact us to discuss your requirements.
search previous next tag category expand menu location phone mail time cart zoom edit close