helicopter for u.n. missions mi-171a2mi-171a2. improved performances improved performances...

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  • Slide 1
  • HELICOPTER FOR U.N. MISSIONS Mi-171A2Mi-171A2
  • Slide 2
  • IMPROVED PERFORMANCES IMPROVED PERFORMANCES UP-TO-DATE AVIONICS UP-TO-DATE AVIONICS NEW LEVEL OF SAFETY AND COMFORT NEW LEVEL OF SAFETY AND COMFORT WIDE RANGE OF OPTIONS WIDE RANGE OF OPTIONS NEW SYSTEM OF MAINTENANCE NEW SYSTEM OF MAINTENANCE IMPROVED PERFORMANCES IMPROVED PERFORMANCES UP-TO-DATE AVIONICS UP-TO-DATE AVIONICS NEW LEVEL OF SAFETY AND COMFORT NEW LEVEL OF SAFETY AND COMFORT WIDE RANGE OF OPTIONS WIDE RANGE OF OPTIONS NEW SYSTEM OF MAINTENANCE NEW SYSTEM OF MAINTENANCE GOALS TO ACHIEVE of 19 2 2 2014 Russian Helicopters, JSC All rights reserved
  • Slide 3
  • of 19 MTOW MTOW with external load Cruise speed Maximum speed Flight range (normal TOW, ISA) Weight of cargo on external load Operation limitations Crew Maiden flight: 2012 First commercial delivery: 2015 Any time of day and night Any weather conditions VFR and IFR Hot / High / Humidity 3 3 13 000 kg 13 500 kg 260 km/h 280 km/h 800 km 5 000 kg 3 3 MAIN PERFORMANCES 2014 Russian Helicopters, JSC All rights reserved 28 660 lb 29 762 lb 141 kts 152 kts 432 nm 11 023 lb -50C +50C 1.. 2
  • Slide 4
  • of 19 4 4 4 4 WHAT DOES IN MEAN FOR YOU? 2014 Russian Helicopters, JSC All rights reserved 14% FASTER 25% MORE EFFECTIVE
  • Slide 5
  • of 19 POWER PLANT FADEC HUMS Service Life Limit doubled 95% dust/sand protection efficiency 5 5 2014 Russian Helicopters, JSC All rights reserved PALL dust Protection System 2x VK-2500 with separate engines fuel supply system APU Safir 5K/G
  • Slide 6
  • of 19 AND MAIN ROTOR HUB MODIFIED SWASHPLATE Number of lubricant points reduced by half Total weight reduced for 56 kg SLL doubled 6 6 2014 Russian Helicopters, JSC All rights reserved
  • Slide 7
  • of 19 ROTORS AND TRANSMISSION Cruise speed increased by 13% MGB 30-minute dry-run, Tail shaft power increased Service Life Limit Increased by 3 times for TR blades and 4,5 times for MR blades Capability of flight in icing condition 7 7 2014 Russian Helicopters, JSC All rights reserved Composite blades 8M Enforced transmission Modified main gearbox X-Shaped tail rotor
  • Slide 8
  • of 19 UP-TO-DATE AVIONICS Reduced crew Piloting, navigation, mission info on MFDs Helicopter laser radar GPS/GLONASS Automatic flight control 8 8 2014 Russian Helicopters, JSC All rights reserved
  • Slide 9
  • of 19 ROUND-THE-CLOCK SURVEILLANCE SYSTEM Observation, search and detection Look-down coverage On-board recording of video/audio and operational information Control of rescue and lifting 9 9 2014 Russian Helicopters, JSC All rights reserved
  • Slide 10
  • of 19 CARGO TRANSPORTATION PASSENGER TRANSPORTATION SEARCH AND RESCUE PATROLLING MEDEVAC VIP MISSIONS 10 2014 Russian Helicopters, JSC All rights reserved
  • Slide 11
  • of 19 Fast loading (2 sliding doors + ramp) Automatic weight measuring system CCTV system for the cargo on external sling Roller-track conveyer The largest volume of cargo cabin 11 TRANSPORT 2014 Russian Helicopters, JSC All rights reserved CAPABILITIES Humanitarian missions
  • Slide 12
  • of 19 4-point safety harness Shock-absorbing seats for 24 pax High level of safety and comfort Fast conversion Peacekeepers and refugees transportation 12 PASSENGER TRANSPORTATION 2014 Russian Helicopters, JSC All rights reserved UN missions capability
  • Slide 13
  • of 19 Round-the-clock SAR operations Patrolling missions Wide range of lifting equipment 13 SAR AND EMS 2014 Russian Helicopters, JSC All rights reserved MISSIONS Round-the-clock surveillance system Hoist for 132/272 kg Searchlights First-aid systems Red Cross, Red Crescent missions
  • Slide 14
  • of 19 ULTIMATE COMFORT IN VIP VERSION 14 pax accompanied by steward Tailored interior of VIP-cabin Up-to-date communication and computer equipment 14 2014 Russian Helicopters, JSC All rights reserved
  • Slide 15
  • of 19 MAIN COMPONENTS TIME BETWEEN OVERHAUL / SERVICE LIFE LIMIT 15 Tail rotor blades Main rotor blades Swash plate Tail rotor hub Main rotor hub Main gearbox Engines Airframe - - 3,000 / 12 TIME BETWEEN OVERHAULS, FLIGHT HOURS / YEARS 3,000 / 12 9,000 / 20 6,000 / - 9,000 / - 18,000 / -- SERVICE LIFE, FLIGHT HOURS / YEARS 2014 Russian Helicopters, JSC All rights reserved
  • Slide 16
  • of 19 LIFE CYCLE MANAGEMENT 16 2014 Russian Helicopters, JSC All rights reserved Fleet monitoring from production to disposal Enhanced safety and performance due to the use of monitoring data Continuous component quality control Safety, reliability and efficiency as a result
  • Slide 17
  • of 19 SAFETY RELIABILITY ULTIMATE TRANSPORT EFFICIENCY SUMMARY 17 2014 Russian Helicopters, JSC All rights reserved
  • Slide 18
  • of 19 Mi-171A2 18 2014 Russian Helicopters, JSC All rights reserved FOR A BETTER WORLD UNITING NATIONS
  • Slide 19
  • 2014 Russian Helicopters, JSC All rights reserved

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