Ilyushin IL-76MD-90A (IL-476) Aircraft

Ilyushin IL-76MD-90A is a new military transport aircraft (code name: IL-476) developed by Ilyushin Aviation Complex, a subsidiary of United Aircraft Corporation (UAC). It is a modernised version of the IL-76MD which itself is based on the IL-76 cargo aircraft platform.

IL-76 cargo aircraft

The IL-76MD-90A cargo aircraft is manufactured at the Aviastar-SP production facility in Ulyanovsk. The factory test flight of the first IL-76MD-90A was concluded in January 2013.

First experienced the upgraded transport plane Sludge-76MD-90A built an aircraft factory “Aviastar-SP”Ulyanovsk and preparing for flight tests.

The aircraft successfully completed its maiden flight test in March 2013, near Moscow. It flew at altitudes of 2,000m to 10,000m for a period of one hour and 55 minutes during the test flight.

The flight test programme of IL-76MD-90A is expected to conclude by the third quarter of 2014.

IL-76MD-90A is developed to transport a range of military equipment, armed personnel, heavy and long size vehicles and cargoes. It will also be used in parachuting cargo / troops and other air borne cargo missions.

Orders and deliveries of the Russian military transport aircraft

The Russian Ministry of Defence (MoD) signed a $4bn contract with UAC for the delivery of 39 IL-76MD-90A aircraft, in October 2012. The deliveries are scheduled to commence in 2014.

First Il-78M-90A tanker aircraft being rolled out to a flight testing

Russian AEW aircraft A-100 made its first flight: Here

A-100 AWACs – Image: UAC

Excerpt

The latest Russian aircraft radar patrol and targeting A-100 made in Saturday’s first flight, reported the press service of the concern “VEGA” (part of the holding Russian electronics of the state Corporation “rostec”), which develops the car.

RUSSIAN AIR FORCE RECEIVES FIRST RUSSIAN-ASSEMBLED IL-76MD: Here

Aviastar

Excerpt

The Russian air force has taken into service the first modernized Ilyushin Il-76MD-90A heavy airlifter.

The aircraft, serial number 0105, was handed over to the military at the Aviastar-SP assembly facility, a subsidiary of United Aircraft Corporation (UAC) in Ulyanovsk, on Dec. 2. It was flown to the 610th Combat and Conversion Training Center of the military transport aviation in Ivanovo, in central Russia, the next day.

This airframe, named after Viktor Livanov, a former CEO and chief designer of the Ilyushin design bureau, became the third serial Il-76MD-90A variant assembled in Ulyanovsk.

Kazakhstan may well be the first Il-76MD-90 customer: Here

Excerpt

The first export order for the Il-76MD-90 cargo plane could very well be Kazakhstan. It’s been reported by Russian media that both defense ministers are in discussions over a number of military-technical issues which not only include the Il-76, but Yak-152 and Yak-130 trainers. Other potential export customers include Algeria, Iran and South Africa.

Russian Il-76 “Candid” Modified To Support Special Operations Conducts Flight Test Over The Black Sea: Here

Excerpt

A really interesting aircraft was spotted conducting flight testing over the Black Sea on Sept. 26, 2017: the Il-76MD-90A “78650”, the first “Candid” modified to carry out special operations.

According to the Russian media outlet “Izvestia” the example “78650” is a flying testbed for a heavily modified Il-76MD-90A variant equipped with “unique on-board radio-electronic systems that would allow the aircraft to stealthily deliver paratroopers and special forces behind the enemy lines, remaining invisible and invulnerable to the enemy.

How the aircraft can evade radars and remain invisible is unclear, anyway, the experimental Candid can be distinguished from the baseline IL-76MD-90A by the presence of an opto-electronic station mounted on the lower nose section of the aircraft and for the “President-C” system used designed to protect aircraft from MANPADS (Man-Portable Air Defense Systems) and IR (heat-seeking) missiles by laser and radiofrequency/electronic jamming of the missile guidance.

Il-76MD-90A Aircraft to Combine Static and Endurance Tests

Russian Ministry of Industry & Trade has financed development of procedure for static and endurance tests of transport airplanes. It will be based on results of design audit over Il-76MD-90A aircraft and integrated into the R&D project codenamed Opora.

According to the R&D project documents available to Mil.Today, after transfer of production facilities from the Tashkent Aircraft Production Company to Ulyanovsk-based Aviastar-SP, “emerged the need for radically new procedure for structural tests that would ensure conducting both static and endurance tests at the same facility”. That must reduce the trials time and costs

As of today, an endurance specimen of upgraded Il-76 has passed fatigue tests in the extent of up to 2,000 flights. Additional calculations and experimental studies shall prove the design service life of 8,000 flights, says the R&D project description. It is planned to finish the tests by the end of 2019.

Mikhail Pestrakov, an aviation engineer and an airspace expert, confirmed to Mil.Today that the in-depth upgrade of the airplane needs new endurance tests and high-tech methods of their studying.

“The aircraft testing procedure must be adjusted in step with technology development”, the expert said

Gen Maj Alexander Akhlyustin, Russia’s honored military pilot of Il-76 aircraft added that due to production transfer the equipment and staff had changed, so assembly technology might change as well, which gave rise for extra tests.

For reference

New version of Il-76MD-90A transport aircraft differs from the predecessors by several parameters. The plane has ‘glass cockpit’, new communications and protection system, and new piloting and navigation equipment. Besides, it has more powerful engines PS-90A-76 thrusting up to 14.5 tons, which helps the airplane lift up to 60 tons payload.

Service life of the new version of widely-known military transport aircraft reaches 30 years with an extension potential. The plane got upgraded wing and reinforced landing gear. Source mil.today

IL-76MD-90A design, based on the IL-76

The IL-76MD-90A is based on the same airframe and fuselage of IL-76 aircraft. The cargo aircraft integrates advanced features such as redesigned wing section, new cockpit with modern avionics and powerful engines.

The aircraft has a length of 46.6m, height of 14.76m, wing span of 50.50m and a wing area (trapezoidal) of 300m². The landing gear track (outer wheels) and fuselage mid-section diameter of the aircraft are 8.16m and 4.8m respectively.

The IL-76MD-90A has a maximum take-off weight of 210t and can carry a maximum payload of 52t. It can accommodate up to five crew members.

Cockpit and avionics of the Ilyushin aircraft

The advanced glass cockpit of the IL-76MD-90A is installed with three intelligent control panels and a KSEIS-KN-76 aircraft status master monitor display system with eight multifunctional liquid crystal displays. The glass cabin provides better view to the cabin crew.

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The IL-76MD-90A also integrates a digital ACS-76 auto flight control system and a new Kupol-III-76M flight sight navigation system with a display indication.

Kupol-III-76M flight sight navigation system

53-5Image: aviadejavu.ru

IL-76MD-90A cargo handling capabilities

The cargo cabin of the aircraft is designed with a length of 24.5m (with ramp), width of 3.45m, and height of 3.4m. The cargo cabin offers an interior volume of 321m³.

ilyushin.org
“The IL-76MD-90A is based on the same airframe and fuselage of IL-76 aircraft.”

Il-76MD-90A is capable of carrying 126 parachutists or 145 troops in single deck arrangement and 225 troops in double-deck arrangement. It can also be installed with special equipment to carry 114 injured persons.

The aircraft is installed with an Aerial-Delivery System (ADS) for dropping of cargoes, transportation of armed forces cargo containers and pallets, and troop parachutes.

The ADS installed onboard the IL-76MD-90A facilitates dropping of parachutists from an altitude of 8,000m at 220km/h to 400km/h speeds. It also enables equipment dropping with the help of parachutes from altitudes of 300m to 4,000m at 260km/h to 400km/h speeds.

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On the cargo compartment floor and ramps are installed with four roller monorail track in two versions: in special niches for landing platforms on the beams for the transport of air containers and pallets. Source survincity.com

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The cargo dropping system aboard the aircraft ensures the dropping of platforms laden with shipments and equipment. The under-ladder devices, roller ways and winches in the cabin allow the loading of cargoes and equipment into the aircraft.

Engine of Russia’s Ilyushin military cargo aircraft

IL-76MD-90A is installed with four fourth generation PS-90A-76 turbofan bypass engines with 4:4 bypass ratios. Each engine develops a maximum continuous thrust of 14,500kgf. It consumes 12% lesser fuel and offers an increased flight range of 18%.

4 x PS-90A-76 turbofan bypass engines

IL76TDPS90-2

PS-90A-76 engine (PS – Pavel Soloviev) is a modification of PS-90A turbofan bypass engine. It extends service life of the large fleet of the IL-76 transport airplanes and raises their efficiency by installation of the PS-90A-76 engine instead of the D-30KP. It allowed to build a new modification of the IL-76 airplane – the IL-76MF military cargo aircraft which meets modern requirements.

Turbofan, bypass, two-shaft, mixed flow, with a thrust reverser in a fan duct and noise absorbing system. 

It is intended for various versions of the IL-76 long-range cargo aircraft and the IL-76MF aircraft.The engine was certified in 2003.

 Performance

Thrust, kg

  • take-off: TH< +30°C , PH > 730 mm Hg, H=0
  • cruise: Н=11 km, М=0.8
 14500
3500
Specific fuel consumption (with real nozzle), kg/kgf hour 0.595
Flight altitude, m up to 13100
Air temperature at sea level (for start and operation), ° С -47…+45
Airfield height (versus sea level) , m up to 3500
Wind speed for ground operation, no more, m/s

  • cross wind
  • tail wind
 15
5
Engine length, mm 4964
Fan tip diameter, mm 1900
Dry weight, kg 2950
Thrust reverser weight, kg 450
Delivery weight, kg 4160

Advantages of the PS-90A-76 engine compared to D-30KP

  • Conformity of ecological parameters on emission and noise to ICAO  regulations
  • Increase of reliability and life
  • Improvement of efficiency
  • Availability of thrust augmentation up to 16000 kg
  • Parameter stability of running
  • Improvement of fire safety in connection with replacement of some fuel accessory units by pneumatic
  • Feasibility of the fan impeller replacement when running

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Dimensions:

Cargo Compartment Height 3.4 m, Cargo Compartment Length 31.1 m, Cargo Compartment Width 3.5 m, Fuel Tank Capacity 109,500 l (28,816 gl), Fuselage Diameter 4.8 m, Height 14.3 m, Length 53.2 m, Payload Capacity 400 metric ton, Wing Area 300 square meter, Wingspan 50.5 m

Weights:

Max Weight 210 t, Payload 60 t

Engine/s Performance:

Thrust 141,000 lb (63,958 kg)

Performance:

Ceiling 12,000 m (39,370 ft), Cruise Speed 850 kph (528 mph), Landing Run Distance 990 m (3,248 ft), Max Range 6,300 km (3,402 nm) carrying a 40t payload or 4,000km carrying a 60t payload, Service Life 30 yr, Take Off Run Distance 1,800 m (5,906 ft)

Other:

Number of Engines 4, Service Life (Flight Hours) 30,000, Service Life (Flights) 10,000

Source generalequipment.info

24491885652_808f1d88bd_b.jpgImage: hiveminer.com

The PS-90A-76 engine on board the IL-76MD-90A aircraft is compliant with latest ICAO requirements for noise and emission levels. An Auxiliary Power Unit (APU) TA-12A is installed onboard the aircraft.

TA-12A APU

ta-12

TA12-60 is a single-shaft auxiliary gas-turbine engine with the equivalent power of 360 kWt. This engine is designed for aircraft and helicopter APUs. It is used for air turbine start of the helicopter and aircraft mid-flight engines, AC electric power of 115/200 V, power up to 60 kWA and providing air conditioning for cockpit and cabins.

High overall efficiency of the engine is based on the use of a 4-stage axial compressor. An annular reverse-flow combustion chamber of evaporative type provides 0,99 burning and low content of hydrocarbons in the exhaust gases. The engine contains a 3-stage axial turbine. Driving units, including alternator, are installed on the engine’s gearbox.

The noise level of the TA12-60 engine, when installed on the craft, does not exceed 90 dB.

The engine complies with the Norms of Aircraft Airworthiness (NLGS-3); this is confirmed by a type certificate No 101-VD issued by the Aviation Register of the IAC.

Since 2005 the TA 12-60 APU has been operated under the second strategy. The TA 12-60 APU is operated subject to the technical condition till the specified life time of the principle components is terminated (4,000 hr/starts).

The TA12-60 engine has been in serial production since 1996.

APPLICATION: Tu-204, Tu-214, Tu-334, Be-200, An-70, Yak-42.

Technical features:

Absorbed electric power of AC, kVA 60
Bleed air consumption, kgf 1,6
Bleed air pressure, kgf/sm2 4,9
Bleed air temperature, °С 250
Start and operation altitude, m 7000/9000
Environmental temperature, °С ± 60
Weight (without generator), kg 297
Specified number of operating hours/starts 2000/4000
Overall dimensions, mm 1588х682х718

Source aerosila.ru

Performance of the IL-76MD-90A

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The aircraft can cruise at a speed of 820-850km/h. It can fly at a maximum altitude of 12,000m. The maximum range of the aircraft is 8,500km. The aircraft requires 1,700m take-off distance on concrete runway.

The life expectancy of the IL-76MD-90A military transport aircraft is 30 years. The aircraft can accumulate a maximum of 30,000 flying hours throughout its service life.

Specifications (Il-76TD-90)

ilyushin.org

Characteristics

Overall geometry dimensions

Length of the aircraft, m 46,60
Height of the parked aircraft, m 14,76
Wing span, m 50,50
Wing area (trapezoidal), m2 300,0
Landing gear track (outer wheels), m 8,16
Fuselage mid-section diameter, m 4,8

Characteristics of the turbofan bypass engine PS-90A-76

Quantity of engine 4
Bypass ratio 4,4
Thrust, kgf
Maximum continuous thrust 14500
Overspeed condition regime 16000
Cruising power 3300
Reverse thrust 3600
Compliance with ICAO requirements п.16, Гл.IV
Specific fuel consumption at cruising power 0,59

Weight characteristics

Maximum takeoff weight, t 210
Maximum payload, t 52
Fuel tanks total capacity, l 109500

Flight data

Cruising speed, km/h 820 … 850
Flight range, km
with 50 tons load 4100
with 40 tons load 5400
with 20 tons load 8500
Flight altitude, m 9000…12000
Takeoff ground run, m 1450
Takeoff distance required on the concrete runway, m 1700
Landing ground run when using engines thrust reverser, m 930

Cargo cabin dimensions

Length with ramp, m 24,50
Width, m 3,45
Height, m 3,40
Cargo cabin capacity, m3 321

Aircraft service life

Calendar years 30
Number of landings 10000
Number of flying hours 3

Source: aviastar-sp.ru/airforce-technology.com/flickr.com/photos/lystseva

Updated Dec 01, 2017

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