Antonov An-124-100 Long-Range Heavy Transport Aircraft, Russia

The An-124 Ruslan, designed by the Antonov ASTC in Kiev, Ukraine, is a very large cargo aircraft with a payload capacity of up to 150t. It is manufactured by Aviant State Aviation Plant, Kiev, and Aviastar, Ulyanovsk, Russia.

The aircraft is designed for long-range delivery and air dropping of heavy- and large-size cargo, including machines, equipment and troops. The aircraft is based on the An-124 Ruslan military transport in service in the Russian Army, which has the NATO reporting name Condor.

The An-124 entered service in 1986 and over 55 aircraft have been built. The An-124-100 received Type Certification in 1992. Volga-Dniepr Airlines of Russia has ten An-124 aircraft. Polet Airlines of Russia operate eight An-124 aircraft.

Aviant State Aviation Plant in Kiev completed an An-124-100 from parts in stock which was sold to the United Arab Emirates in 2004.

Seven An-124-100 aircraft were operated by Antonov Airlines, based at London Stansted Airport, in partnership with Air Foyle HeavyLift. Antonov Airlines did not renew the contract for this partnership in June 2006 and has signed an agreement with Volga-Dniepr Airlines and Aviastar for the modernisation and construction of the An-124.

AN-124-100M

A new version, the An-124-100M-150 has been developed by Aviastar, with investment from the International Finance Corporation. The aircraft payload has been increased from 120t to 150t, the take-off weight increased from 392t to 402t and the flight range with 120t cargo increased from 4,650km to 5,400km.

The crew has been reduced to four. A digital anti-skid braking system has been fitted with monographite wheel brake disks. The aircraft has a new avionics suite supplied by Honeywell of the USA and Aviapribor and Leninets of Russia.

In September 2004, the governments of Russia and the Ukraine announced that series production of the An-124 would be restarted. Up to 80 An-124-100M upgraded aircraft are to be jointly manufactured by Aviastar and Aviant between 2007 and 2020.

Volga-Dnepr Airlines placed an order for five An-124-100M in August 2005. Deliveries are scheduled to begin in 2010. Supplemental type certification was received for the aircraft in June 2007, allowing operations with 402t maximum take-off weight and 150t maximum payload.

In February 2006, NATO signed a contract to lease the An-124, under the Strategic Airlift Interim Solution (SALIS), from Ruslan SALIS GmbH (representing Antonov and Volga-Dnepr). Two aircraft will be constantly based at Leipzig airport and four more will be available on request. The lease is for an initial three years, to be renewed yearly until 2012 when the A400M transport enters service. The Leipzig maintenance base was opened in January 2007.

The US Air Mobility Command has been chartering An-124 aircraft from Volga-Dnieper since 2003 for the transport of oversize cargo.

The unique transport capabilities and the high performance of the aircraft have been proven in operation. The An-124 has served several nations in the transportation of economically important cargoes, for example: 90t hydraulic turbines, large size Liebherr autocranes, American Euclid dump trucks, the fuselage of Tu-204 passenger transporter, a 109t railway locomotive, and a sea yacht more than 25m long.

STRUCTURE

The aircraft fuselage has a double-deck layout. The cockpit, the relief crew compartment and the passenger cabin for 88 seats are on the upper deck. The lower deck is the cargo hold. The flight deck has crew stations arranged in pairs for six crew, the pilot and co-pilot, two flight engineers, the navigator and communications officer. The loadmaster's station is located in the lobby deck.

The An-124 aircraft is fitted with a relatively thick (12%) swept-back supercritical wing to give high aerodynamic efficiency and consequently a long flight range. To decrease the trim drag, the aircraft was designed with a low margin of static stability.

The construction includes extruded skin panels on the wing, extruded plates for the centre-section wing panels and monolithic wafer plates for the fuselage panels. The aircraft structural members are made of composites that make up 1,500m² of the surface area, giving a weight saving of 2,000kg.

High rough-field capacity multi-leg landing gear and the loading equipment ensure self-sufficient operation of the aircraft on prepared concrete runways and on poorly equipped unpaved strips at forward airbases close to the areas of operations where the cargo is needed.

The landing gear is self-orienting and incorporates a kneeling mechanism which allows an adjustable fuselage clearance to assist the loading and unloading of self-propelled equipment.

The aircraft has paradropping and cargo-handling equipment and a 1,000-test point on-board automatic test system as well as two auxiliary power units equipped with electric generators and turbopumps for independent operation of the aircraft.

AVIONICS

All systems are quadruple redundant. The on-board equipment provides the capability to execute airlift and paradrop missions by day and at night, in Visual Flight Rules and Instrument Flight Rules (VFR and IFR) weather conditions and in prolonged operation beyond the main basing airfield.

The systems include an integrated flight control and navigation system, communications facilities and paradropping and cargohandling equipment. There are 34 computers functioning aboard the aircraft, combined into four main systems: navigation, automatic piloting, remote control and monitoring.

The integrated flight control and navigation system comprises an autonomous navigation system, altitude and airspeed indicating system, short-range radio navigation and landing system, global positioning system, automatic radio compass, integrated flight control system, ground surveillance radar, forward-looking weather radar, optical and TV sight and IFF equipment.

Standard communications facilities include an aeronautical-space communications radio station, HF radio set, VHF/UHF radio set, intercom, voice warning and documentation system.

CARGO

The two cargo hatches are a distinctive structural feature. The fuselage nose can be hinged upward to open the front cargo hatch and there is a rear cargo hatch in the rear fuselage to speed up the cargo loading and unloading operations.

The on-board system of cargo handling equipment makes it possible to load and unload the aircraft without the help of ground facilities. The paradropping and cargo-handling equipment comprise two travelling cranes, two winches, rollgang and tiedown equipment. The aircraft is often compared to the US Lockheed Martin C-5 Galaxy. The An-124 has a transportation capability 25% higher than that of the C-5A and 10% higher than the C-5B.

WORLD RECORDS

Since 1989, An-124 airplanes have been making charter freight flights on the international airlines and the aircraft has set 30 world records, the most significant of which are: 171,219kg cargo was lifted to 10,750m altitude in 1985; a 20,161km closed route was flown in 25.5hrs in 1987; and an average speed of 689.1km/hr was achieved in a round-the-world flight over the South and North Poles in 1990.

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