Presentation on theme: "Presenting IL-96-400T. The IL-96-400T aircraft is a cargo version of well-known IL-96-300 passenger aircraft with increased fuel capacity, stretched by."— Presentation transcript:
Presenting IL T
The 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. General
Specification Operating Weights & Fuel Capacity Max taxi weight, t 266 / 271* Max takeoff weight, t 265 / 270* Max payload, t 92 Max landing weight, t 220 Max zero fuel weight, t 208 / 210* Max fuel, t 116,3 Aircraft Performance Characteristics (ISA) Cruising speed, km/h Maximum flight altitude, km13.1 Required takeoff distance (with MTOW), m2450 Required landing distance (with MLW), m1700 Range with maximum payload, km4750 / 5000* Range with 40 t payload, km12000 Range with maximum fuel, km14500 Airfield elevation (relative to sea level)-300 ÷ 1800 Range of operational temperatures, С-45…+42 Crew3 Maximum number of people on board 9
Specification Main Deck: Large cargo door (4850x2875 mm) port side Lower deck: Cargo door 1 (2690x1840 mm) starboard Cargo door 2 (2690x1730 mm) starboard
Cargo Compartment Lower Deck
Cargo Compartment Lower Deck 3175 mm (125 in) P9 / P6 / P mm (60,4 in) 1625 mm (64 in) 1562 mm (61,5 in) 1534 mm (60,4 in) 2235 mm (88 in) 2438 mm (96 in) 2235 mm (88 in) 1562 mm (61,5 in) 3175 mm (125 in) 2743mm (108 in) 3175 mm (125 in) 1562 mm (61,5 in) LD-3LD-6P9 / P6 / P1P 2P mm (61,5 in) P mm (108 in) P 2 LD-6 LD-3 Pallets Types
Cargo Compartment Lower Deck VariantPallet typeDimensions inch mm Max weight pound kg Quantity Front Back 1LD – 360,4х61,5х641534х1562х LD – 660,4х125х641534х3175х P8 size K, NAS ,4х61,5х641534х1562х P9 size L, NAS3610,LD-5/10/11 60,4х125х641534х3175х P2 size B, NAS х108х642235х2743х P1 size A, NAS3610, LD-7/9/29 88х125х642235х3175х P6 size M, NAS х125х642438х3175х Half size from size M NAS х61,5х642438х1562х
Cargo Compartment Upper Deck
Cargo Compartment Upper Deck Р6 (two row) 2438 mm (96 in) 3175 mm (125 in) Р6 (one row) 2438 mm (96 in) 3175 mm (125 in) 2438 mm (96 in) Р4Р4 4978mm (196 in) Р2Р mm (108 in) 2235 mm (88 in) 3175 mm (125 in) Р1Р mm (88 in) Р mm (96 in) Р 4 Р mm (96 in) 3175 mm (125 in) 4978 mm (196 in)
Cargo Compartment Upper Deck VariantPallet typeDimensions inch mm Max weight Pound kg Quantity 1Р6 (two row) 96х125х962438х3175х Р2 2Р188х125х882235х3175х Р2 3Р288х108х882235х2743х Р6 (one row) 96х125х962438х3175х Р2 5Р 496х196х962438х4978х Р2
Cargo Area The cargo floor has mechanization for moving of containers and pallets along the cargo compartment.
Range Operating Weights & Range Payload 92 t 5200 km Payload 70 t 7400 km Payload 62 t 9000 km Payload 40 t12000 km Main deck, cubic m580 Lower deck, cubic m 196 (114+82) Tones Range, km
Cockpit The 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).
Captain Co-pilot Flight engineer First observer Seat for supernumerary Crew member Cargo net Rest places Cockpit
Certification IL 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).
Radio Unit Control Panel With radio navigation system control separately from Flight Management System (FMS); and 8,33/25 kHz frequency range. Aerodynamic stability and controllability system With preflight control panel Flight Management System compliance 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 Unit data transmitting for FMS; signals generation to voice alert system (on reaching the radio altitude) Multifunctional Flight Display (MFD) with MFD control panel Inertial Navigation System EGPWS Contains 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). EFIS Includes 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 computer Critical Condition Warning System Avionics specification
Collision Avoidance System (CAS) With changes 7, Mode S, 1 set providing aerial collision prevention and 2 Mode –S responders EICAS with 6,25" x 6,25 LCD Flight Data Recorder with solid state data storage. Weather Radar System Featuring wind shear warning and turbulence detection Fault Detection Isolation System interaction with upgraded equipment; failure information indication on FMS display control panel Automatic Direction Finder VHF Omni directional Radio Range (VOR) Dual set Dispatch transponder (Doubled) Distance Measuring Equipment with scanning mode (DME) Radio Altimeter Featuring Rz code (H3) Instrument Landing System Tripled set, improved jamming resistance of HF broadcast. Electronic Chronometer Set 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; Avionics 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 navigation Selective Calling System providing selective crew radio call (up to 5 channels VHF-HF). 3 VHF Radio Satellite communication system operating in Inmarsat standard. 2 HF Radio with Intercom function Emergency VHF Radio Two 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. Avionics specification