Helicopter Services
We are offering various services, from helicopter rental for firefighting purposes, to maintenance and complete overhaul.
"The helicopter is probably the most versatile instrument ever invented by man. It approaches closer than any other to fulfillment of mankind's ancient dreams of the flying horse and the magic carpet."
Igor Ivanovitch Sikorsky, comment on twentieth anniversary of the helicopter's first flight Sept. 13, 1959
Learn about the modernization process here (click on image)
The following helicopters are the most desireble in the global market.
This gallery presents the preliminary characteristics specific to each individual helicopter. We offer modernizaton to the buyer's specific requirements which will greately improve flying characteristics with a significant increase in payload.
mi-2
General characteristics
Crew: one
Capacity: 8 passengers or 700 kg (1,543 pounds) of internal, 800 kg (1,764 pounds) of external cargo
Length: 11.40 m (37 ft. 4¾ in.)
Rotor Diameter: 14.50 m (47 ft 6 in)
Height: 3.75 m (12 ft. 3½ in.)
Disc: 165.13 m² (1,777.44 ft² )
Empty weight: 2,372 kg (5,218 pounds)
Load Weight: 3,550 kg (7,826 lbs)Maximum. take-off weight: 3,700 kg (8,155 lbs)
Powerplant: GTD -350Top speed: 200 km / h (108 knots, 124 miles per hour)
Range: 440 km (237 nm, 273 miles) (maximum internal fuel, without reserve)
Service ceiling: 4,000 m (13,125 ft)Climbing Speed: 4.5 m / s (885 ft / min)
Disc load: 22.41 kg / m² (4.59 lb / ft²)
MI-2 (MSB-2)
General characteristics
Crew: one
Capacity: 8 passengers or 700 kg (1,543 pounds) of internal, 800 kg (1,764 pounds) of external cargo
Length: 11.40 m (37 ft. 4¾ in.)
Rotor Diameter: 14.50 m (47 ft 6 in)
Height: 3.75 m (12 ft. 3½ in.)
Drive: 165.13 m² (1,777.44 ft²)
Empty weight: 2,372 kg (5,218 pounds)
Load Weight: 3,550 kg (7,826 lbs)
Maximum. take-off weight: 3,700 kg (8,155 lbs)
Engine: AI-450mTop speed: 200 km / h (108 knots, 124 miles per hour)
Range: 750 km (237 nm, 273 miles) (maximum internal fuel, without reserve)
Service ceiling: 4,000 m (13,125 ft)
Climbing Speed: 4.5 m / s (885 ft / min)
Disc load: 22.41 kg / m² (4.59 lb / ft²)
MI-8T
General characteristics
Crew: 3 (pilot, assistant, flight engineer)
Capacity: 24 passengers or 12 stretchers and space for 1 doctor or 3,000 kg (6,600 lb) at internal / external hard points
Length: 18.17 m (59 ft. 7 in.)
Rotor Diameter: 21.29 m (69 ft 10 in)
Height: 5.65 m (18 ft. 6 in.)Drive: 356 m² (3,832 ft)
Empty Weight: 7,260 kg (16,007 lbs)
Shipping Weight: 11,100 kg (24,470 lbs)
Maximum. take-off weight: 12,000 kg (26,455 pounds)
Powerplant: 2 × Klimov TV2-117 turboshaft shafts, 1.454 kW (1,950 units) each
Maximum Fuel Capacity: 3,700 L (977 US Gallons)
Maximum speed: 260 km / h (140 thousand tons)
Range: 450 km (280 miles)
Ferry line: 960 km (596 miles)
Service ceiling: 4,500 m (14,765 ft)
MI-8MTV-1 (MI-17-1V)
General characteristics
Crew: three - two pilots and one engineer
Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 pounds) of cargo inside / 5,000 kg (11,023 pounds) from the outside.
Length: 18.465 m (60 ft. 7 in.)
Rotor Diameter: 21.25 m (69 ft 10 in)Height: 4.76 m (15 ft. 7¼ in.)
Drive: 356 m² (3,834 ft²)
Empty Weight: 7,489 kg (16,510 lbs)
Shipping Weight: 11,100 kg (24,470 lbs)
Maximum. take-off weight: 13,000 kg (28,660 pounds)
Powerplant: 2 × Klimov TV3-117ВM turboshaft shafts, 1,633 kW (2,190 sh.) Each
Top speed: 250 km / h (135 knots, 155 mph)Range: 465 km (251 nm, 289 miles) (standard fuel)
Service ceiling: 6,000 m (19,690 ft)Climbing speed: 9 m / s (1,575 ft / min)
MI-8MSB
General characteristics
Crew: three - two pilots and one engineer
Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 pounds) of cargo inside / 5,000 kg (11,023 pounds) from the outside.
Length: 18.465 m (60 ft. 7 in.)
Rotor Diameter: 21.25 m (69 ft 10 in)
Height: 4.76 m (15 ft. 7¼ in.)
Drive: 356 m² (3,834 ft²)
Empty Weight: 7,489 kg (16,510 lbs)Shipping Weight: 11,100 kg (24,470 lbs)
Maximum. take-off weight: 12,500 kg (27,557 lbs)
Powerplant: 2 × Klimov TV3-117VMA SBM1V 4ETop speed: 260 km / h (140 knots, 161 mph)Range: 600 km (323 nm, 372 miles) (standard fuel)
Service Ceiling: 9.150 m (30.019 ft)
Climbing speed: 9 m / s (1,575 ft / min)
MI-8AMT (MI-171E) (MI-171C)
General characteristics
Crew: three - two pilots and one engineer
Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 pounds) of cargo inside / 5,000 kg (11,023 pounds) from the outside.
Length: 18.465 m (60 ft. 7 in.)
Rotor Diameter: 21.25 m (69 ft 10 in)
Height: 4.76 m (15 ft. 7¼ in.)Disc: 356 m² (3.834 ft²)Empty Weight: 7,489 kg (16,510 lbs)
Shipping Weight: 11,100 kg (24,470 lbs)Maximum. take-off weight: 13,000 kg (28,660 pounds)Powerplant: 2 × Klimov TV3-117ВM turboshaft shafts, 1,633 kW (2,190 sh.) Each
Top speed: 250 km / h (135 knots, 155 mph)Range: 465 km (251 nm, 289 miles) (standard fuel)
Service ceiling: 6,000 m (19,690 ft)
Climbing speed: 9 m / s (1,575 ft / min)
MI-14 AMPHIBIAN
General characteristics
Crew: 4Length: 18.38 m (60 ft. 3 in.)
Rotor Diameter: 21.29 m (69 ft 10 in)
Height: 6.93 meters (22 feet 9 inches)
Drive: 356 m² (3,832 ft)
Empty Weight: 11,750 kg (25,900 lbs)
Maximum. take-off weight: 14,000 kg (30,865 pounds)
Powerplant: 2 × Klimov TV3-117ВM turboshaft shafts, 1,454 kW (1,950 sh.) Each
Maximum speed: 230 km / h (124 knots)
Ferry line: 1,135 km (705 miles)
Service ceiling: 3,500 m (11,500 ft)
Endurance with maximum fuel: 5 hours, 56 minutes
MI-26T
General characteristics
Crew: five or two pilots, 1 navigator, 1 flight engineer, 1 flight technician
Seating capacity: 90 passengers or 60 stretchers20,000 kg of cargo (44,090 pounds)
Length: 40.025 m (131 ft 3¾ in.) (Rotor rotation)
Rotor Diameter: 32.00 m (105 ft)
Height: 8.145 m (26 ft. 8¾ in.)
Disc Area: 804.25 m2 (8,656.8 ft)
Empty Weight: 28,200 kg (62,170 lbs)
Shipping Weight: 49,600 kg (109,350 lbs)
Maximum. take-off weight: 56,000 kg (123,450 pounds)
Powerplant: 2 × Lotarev D-136 turboshaft shafts, 8 500 kW (11 399 shp) each
Maximum speed: 295 km / h (159 thousand tons, 183 mph)
Cruise Speed: 255 km / h (137 KT, 158 mph)
Range: 1.920 km (1.036 nm, 1.190 miles) (with auxiliary tanks)
Service ceiling: 4,600 m (15,100 ft)
