AN 12 has been designed as the standard medium-range cargo transport aircraft of the Soviet air forces and airlines of many nations. This four engine medium military (and commercial cargo) aircraft is well known throughout the world. This cost effective asset belongs to the category of outstanding aircraft.
Reliable and powerful, AN 12 delivers into and back out of short and unpaved runway unreachable by another aircraft. Its hauling qualities (wide fuselage, rear door, electric traveling crane and hoist) allow him to carry big volumes of specific and critical cargo.
AN 12 SPECIFICATIONS
Maximum payload: 18000 kg (39683 lbs)
Cargo compartment volume: 90 m3/3178’³
Cargo compartment dimensions: length – 13,55 m /533″ maximum width – 2,8 m/110″ maximum height – 2,4 m/94″
Cargo door dimension: 2,98 х 2,95 m/117″x116″
Maximum Take-Off weight: 61000 kg (134482 lbs)
Maximum landing weight: 58000 kg (127868 lbs)
Maximum Range: 3,600 km/1,944 Nm with maximum payload
Derived from the AN 26 transport aircraft, AN 32 is a twin engine, tactical light transport aircraft currently used by various air forces and airlines companies worldwide.
The AN 32 can take-off and landing on rough airfields and unpaved runways. This aircraft has been designed to manoeuvre day as night in tropical and mountainous areas, even in hot and dusty conditions (up to 55°C).
AN 32 features advanced cargo handling devices and a cargo door fitted with a ramp to ease the loading or unloading of freight. The AN 32 is well-known as a reliable workhorse.
AN 26 has been designed as the light to medium range cargo transport aircraft of the Soviet air forces and airline of many nations. This twin-engined military, and commercial cargo, aircraft is well known throughout the world. AN 26-100 model is combo and able to carry up to 38 passengers. This cost effective asset belongs to the category of outstanding aircraft as well.
Reliable and versatile, AN 26 delivers into and back out of short and unpaved runway unreachable by another aircraft. Its hauling qualities (wide fuselage, rear door, electric traveling crane and hoist) allow him to carry interesting volumes of specific and critical cargo.
AN 26 SPECIFICATIONS
Crew :6
Max payload : 5500 kg (12125 lbs)
Cargo compartment volume : 41 m3
Cargo compartment dimensions : 1110x220x170 CM / 437″x86″x66″ length : 15,68 m maximum width : 2,70 m maximum height : 1,70 m
Cargo door dimension : 2,40 х 3.15 m
Maximum Take-Off (landing) weight : 24000 kg (52910 lbs)
Maximum taxiing weight : 24230 kg (53417 lbs)
Take-Off distance (weight 24 000 kg) : 1500 M / 4921Ft26″
Landing distance (aircraft weight 24 000 kg) : 1600 M / 5249Ft4″
Cruising speed : 420 KM/H / 226 Kts
AN 26-100 SPECIFICATIONS
Crew : 6
Max payload: 5000 kg (11023 lbs)
Cargo compartment volume: 34 m3
Cargo compartment dimensions: 930x220x170 CM / 437″x86″x66″ length : 15,68 m maximum width : 2,70 m maximum height : 1,70 m
Cargo door dimension : 2,40 х 3.15 m
Maximum Take-Off (landing) weight : 24000 kg (52910 lbs)
Maximum taxiing weight : 24230 kg (53417 lbs)
Take-Off distance (weight 24 000 kg) : 1500 M / 4921Ft26″
Landing distance (aircraft weight 24 000 kg) : 1600 M / 5249Ft4″
SHERPA C 23 A is a twin-engined high-wing monoplane with a robust landing gear, featuring a steerable nose wheel to provide for operation from short, unprepared runways where hot or high altitude conditions may exist. SHERPA C 23 A is best suited for passenger and/or cargo transportation.
SHERPA C 23 A SPECIFICATIONS
Speed, cruise: 190 kts/ 352 km/h
Max range (ISA + 15 anf 45 mn) : 350 nm/ 550 km (with 2450 kg of cargo) 750 nm/ 1,100 (with 1,500 kg of cargo)
Crew: 2
Passengers: 18 up to 28
Paratroopers : up to 18 with leg bag, up to 22 skydivers
Pallets : 4 LD3 and 2 attendants
Payload : 3240kg / 7142 lbs
MTOW : 10390 kg / 22906 lbs
Loaded weight: 6680 kg / 14727 lbs
Fuel burn rate: 388 kg/hr (Hour bulk fuel/Flt time +15%)
Engine : 2 x Pratt Whitney PT6A-45R turboprops, 900kW
Take-Off distance (weight 10 400 kg) : 1200 m / 3937 ft
Landing distance (weight 10 400 kg) : 1100 m / 3608 ft
Cargo compartment volume: 33 m3/1165’³
Cargo compartment dimensions: length : 8,24 m /27,03″ maximum width : 1,84 m/72 maximum height : 1,88 m/74″
Cargo door dimension : 1,82 х 1,70 m/71″x67″
Rear door and electric cargo hoist
Rear cargo door dimensions : 2.4 m x 1.4 m / 95″x 55″
Left side cargo door dimensions : 1,67 x 1,4 m /65″ x 55″
As compared to Mi 8T, Mi 8MTV and MI 171 are an upgrade version of the famous MI 8 T equipped with superior navigation systems installed, better aerodynamic performance, APU and more powerful engines. These versions can be used for a number of purposes, such as passenger/cargo transportation, aerial patrolling, medical evacuation, and much more.
SPECIFICATIONS
Crew: 3
Capacities, passengers: 24
Capacities, stretchers: 12
Speed, max: 135 kts/ 250 km/h
Speed, cruise: 121 kts/ 225 km/h
Max range: 620 nm/ 1150 km (with 20 min fuel reserve)
Endurance, max: 5h30 (with 20 min fuel reserve)
Cargo hold volume: 23 m3/ 812
Cargo hold dimensions (LxWxH): 5.34 m x 2.25 x 1.8/17.5′ x 7.38′ x 5.9′
Weight, empty (no fuel): 15,602 lbs/ 7,077 kg
Weight, max take off: 28,660 lbs/ 13,000 kg
Weight, internal cargo: 8,818 lbs/ 4,000 kg
Weight, external cargo: 8,818 lbs/ 4,000 kg
Fuel capacity, main tanks: 691 (1,137) US gal/ 2,615 lt (4,305 lt with upper tanks)
Fuel capacity, main plus extra fuel tanks: 1,174 (1,621) US gal/ 4,445 lt (6,135 lt with upper tanks)
Service ceiling: 15,748 ft/ 4,800 m
Operating temperature: -45°C to +50°C
MI 8T HELICOPTER
Mil Mi-8 helicopters are multi-purpose rotorcraft intensively employed in both civil and military aviation. They are one of the most produced helicopters as of today and are used nowadays by over 50 countries worldwide. These versions can be used for a number of purposes, such as passenger/cargo transportation, aerial patrolling, medical evacuation, and much more.
MI 8T SPECIFICATIONS
Crew: 3
Capacities, passengers: 21
Capacities,stretchers: 12
Speed, max: 135 kts/ 250 km/h
Speed, cruise: 119 kts/ 220 km/h
Max range (full main fuel tanks): 335 nm/ 620 km (with 20 min fuel reserve)
Endurance, max: 5 hrs (with 20 min fuel reserve)
Cargo hold volume: 23 m3/ 812
Cargo hold dimensions (LxWxH): 5.34 m x 2.25 x 1.8/17.5′ x 7.38′ x 5.9′
Weight, empty (no fuel): 15,066 lbs/ 6,834 kg
Weight, max take off: 26,455 lbs/ 12,000 kg
Weight, internal cargo: 6,614 lbs/ 3,000 kg
Weight, external cargo: 6,614 lbs/ 3,000 kg
Fuel capacity, main tanks: 691 (1,137) US gal/ 2,615 lt (4,305 lt with upper tanks)
Fuel capacity, main plus extra fuel tanks: 1,174 (1,621) US gal/ 4,445 lt (6,135 litters with upper tanks)
LET 410 is a twin-engined high-wing aircraft with a strong tricycle retractable and a reinforced landing gear. Able to use unpaved runways where hot or high altitude conditions may exist. LET 410 combo is best suited to commit your mission like no other.
Among LET 410 advantages are:
Multirole and mission versatility
Short takeoff & landing (STOL) capability on unpaved, rain-soaked airstrips
Unsurpassed durability and proven reliability in extreme conditions
High useful load, optimized for economical short-haul transport
Large cabin volume and easy and quick conversion
Excellent stability and controllability at low airspeeds
Longstanding reliability & excellent safety record
Extremely cost-effective
LET 410 UVP- E SPECIFICATIONS
Continuous cruise speed : 208 kts/ 385 kmh
Economical cruise speed : 197 kts/ 365kmh
Max range: 375 NM/ 700 km, with full payload
Range with tip tanks : max fuel 1300 kg/ 2870 lbs
Range with tip tanks : payload 1100 kg = approx. 750 nm/1300 km
Crew: 2
Passengers: 17
Max Payload : 3750 lb/1700 kg
Weight, max take off: 14110 lbs/ 6,400 kg
Empty Weight, typical : 9000 lbs/ 4100 kg
Min runway requirements: 2580 ft/ 790m
Cargo hold dimensions (LxWxH): 275” x 72” x 65” – 6.98 x 1.83 x 1.65 m
Cargo door size: 49”x 57” – 1.25 x 1.45 m
Useable volume (cubic ft – cubic m) : 635’³ – 18m3
LCLA (Low Cost Low Altitude parachute)
We provide solutions to air supply of people with food, water, critical spare-parts and other supplies to remote areas and unsafed locations.
It means no travel by land and to avoid IEDs (Improvised explosive devices) peril and ambushed terrorists.
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