2GeneralThe IL T aircraft is a cargo version of well-known IL passenger aircraft with increased fuel capacity, stretched by 9.35 m and equipped with new turbofan engines and improved avionics.Designed by Ilyushin Aviation Complex (Moscow, Russia) and manufactured by Voronezh Aircraft Manufacturing Company (Voronezh, Russia), IL T is capable of transporting up to 92 tones.The aircraft is powered by four turbofan two-shaft PS-90A1 engines complying with the international ecological requirements and with approved license to operate worldwide.
3Specification Operating Weights & Fuel Capacity Max taxi weight, t 266 / 271*Max takeoff weight, t265 / 270*Max payload, t92Max landing weight, t220Max zero fuel weight, t208 / 210*Max fuel, t116,3Aircraft Performance Characteristics (ISA)Cruising speed, km/hMaximum flight altitude, km13.1Required takeoff distance (with MTOW), m2450Required landing distance (with MLW), m1700Range with maximum payload, km4750 / 5000*Range with 40 t payload, km12000Range with maximum fuel, km14500Airfield elevation (relative to sea level)-300 ÷ 1800Range of operational temperatures, С-45…+42Crew3Maximum number of people on board9
4Specification Main Deck: Large cargo door (4850x2875 mm) port side Lower deck:Cargo door 1 (2690x1840 mm) starboardCargo door 2 (2690x1730 mm) starboard
7Cargo Compartment Lower Deck Pallets Types LD-3 LD-6 P9 / P6 / P1 P 2 1625 mm (64 in)1625 mm (64 in)1625 mm (64 in)1625 mm (64 in)1625 mm (64 in)3175 mm (125 in)3175 mm (125 in)1534 mm (60,4 in)1562 mm (61,5 in)1534 mm (60,4 in)1534 mm (60,4 in)2235 mm (88 in)2235 mm (88 in)2743mm (108 in)1562 mm (61,5 in)1534 mm (60,4 in)2438 mm (96 in)LD-3LD-63175 mm (125 in)P9 / P6 / P12743 mm (108 in)P 21562 mm (61,5 in)P 81562 mm (61,5 in)1562 mm (61,5 in)3175 mm (125 in)
8Cargo Compartment Lower Deck Variant Pallet type Dimensions inch mm Max weightpound kgQuantityFront Back1LD – 360,4х61,5х641534х1562х16253300150018142LD – 660,4х125х641534х3175х162570003175973P8 size K, NAS 36104P9 size L, NAS3610,LD-5/10/11660030005P2 size B, NAS 361088х108х642235х2743х1625800036286P1 size A, NAS3610, LD-7/9/2988х125х642235х3175х1625102004627P6 size M, NAS 361096х125х642438х3175х16251100050008Half size from size M NAS 361096х61,5х642438х1562х16255535250010
10Cargo Compartment Upper Deck Р6 (one row) Р2 Р6 (two row) Р1 Р4 Р 4 2438 mm (96 in)3175 mm (125 in)Р22743 mm (108 in)2235 mm (88 in)Р6 (two row)2438 mm (96 in)3175 mm (125 in)Р12235 mm (88 in)2438 mm (96 in)Р44978mm (196 in)3175 mm (125 in)Р 4Р 62438 mm (96 in)2438 mm (96 in)Р 6Р 62438 mm (96 in)2438 mm (96 in)4978 mm (196 in)3175 mm (125 in)
11Cargo Compartment Upper Deck Variant Pallet type Dimensions inch mm Max weightPound kgQuantity1Р6 (two row)96х125х962438х3175х243815000680025+1Р22Р188х125х882235х3175х22351000060803Р288х108х882235х2743х223580004530264Р6 (one row)12+2Р25Р 496х196х962438х4978х24382500011340
12Cargo AreaThe cargo floor has mechanization for moving of containers and pallets along the cargo compartment.
14CockpitThe IL T aircraft operated by 3 crew members is equipped with modern avionics which includes six multifunctional color-LCD displays (EFIS), Flight Management System (FMS), Inertial Navigation System, Collision avoidance System (CAS) including mode “S” transponder, EGPWS system, VHF communications (compliant with ICAO requirements of item 4.7 Appendix 10), and equipment permitting flights in RVSM conditions.The avionics complex comply with modern requirements on international routes in Europe and North America (RNP-1, RNP-5, RNP-10, RNP-12.6, RNP-20) and allows to navigate and land under ICAO CAT II category (IIIA category is optional), speed hold, automatic voice warning system (in English).The crew and cargo cabins correspond to aircraft requirements for protection against the illegal intrusion (the Amendment 27 to a Part 1 of the Appendix 6 to ICAO) and to safety requirements (Chapter 11 of the Appendix 8 to ICAO).
15Cockpit Seat for supernumerary Crew member Co-pilot Flight engineer CaptainCo-pilotFlight engineerFirst observerSeat for supernumeraryCrew memberCargo netRest places
16CertificationIL T aircraft has Supplement to Type Certificate № /Д20 issued by Interstate Aviation Committee (MAK), corresponds to national aviation regulations and meets ICAO requirements (Chapter 4 of the Appendix 6).PS-90A1 engine has Supplement to Type Certificate № 16-Д/Д29 issued by Interstate Aviation Committee (MAK), corresponds to NLGS-3 national aviation regulations.Noise requirements – IL T aircraft has Noise Type Certificate №СШ175-Ил Т and is in compliance with requirements of Chapter 4 International Standard “Environmental protection”.Emissions – in compliance with requirements of Annex 16 to the Chicago Convention on International Civil Aviation (volume II “Aircraft Engine Emissions”, issue 1981 with Amendments 1-4).
18Avionics specification Radio Unit Control PanelWith radio navigation system control separately fromFlight Management System (FMS);and 8,33/25 kHz frequency range.Aerodynamic stability and controllability systemWith preflight control panelFlight Management Systemcompliance with RNP-1 requirements;correction according satellite navigation system;data base loading according to ARINС-424;amount of non-volatile memory (data base) 4 Mb;FDR access provision.FMS Interface Unitdata transmitting for FMS;signals generation to voice alert system (on reaching the radio altitude)Multifunctional Flight Display (MFD) with MFD control panelInertial Navigation SystemEGPWSContains data base on terrain relief and provides early ground proximity warning of terrain relief data along trajectory having characteristics of TAWS level, A class. From 1 January, 2004 (Amendment 27 to Part 1 of Addendum 6, ICAO).EFISIncludes liquid crystal displays of 6,25” x 6,25” size, 1 set. TCAS-II, Early Ground Proximity Warning System and weather radar data display.Air data computerCritical Condition Warning System
19Avionics specification Collision Avoidance System (CAS)With changes 7, Mode S, 1 set providing aerial collision prevention and 2 Mode –S respondersEICAS with 6,25" x 6,25“ LCDFlight Data Recorder with solid state data storage.Weather Radar SystemFeaturing wind shear warning and turbulence detectionFault Detection Isolation Systeminteraction with upgraded equipment;failure information indication on FMS display control panelAutomatic Direction FinderVHF Omni directional Radio Range (VOR)Dual setDispatch transponder (Doubled)Distance Measuring Equipment with scanning mode (DME)Radio AltimeterFeaturing Rz code (H3)Instrument Landing SystemTripled set, improved jamming resistance of HF broadcast.Electronic ChronometerSet of stand-by equipment including - Radio Magnetic Indicator, Standby Giro Horizon, Magnetic Compass, Instrumental Speed Indicator, Mechanic Pressure Foot-Graduated Altimeter.Automatic Flight Control System and Thrust Control System enable:automatic approach;automatic go-around;vertical speed hold with automatic and manual thrust control;override control;
20Avionics specification altitude hold;“reaching of the prescribed level” with automatic and manual thrust control;heading hold;thrust hold;automatic hold of speed and Mach number via thrust channel on route flight modes;automatic mode of horizontal navigationSelective Calling Systemproviding selective crew radio call (up to 5 channels VHF-HF).3 VHF RadioSatellite communication system operating in Inmarsat standard.2 HF Radio with Intercom functionEmergency VHF RadioTwo emergency locator-transmitter (ELT) portable radio buoy providing operation in COSPAS-CARCAT (in compliance with ICAO Part 5 vol.III Appendix 10 requirements )Cockpit Voice Recorder providing record of crew members talks and cockpit sound situation (4 channels) with keeping data records for more than 2 flight hours.