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Мi-38 Utility Helicopter
of © 2014 Russian Helicopters, JSC All rights reserved Mi-38 concept Advanced technologies, components, systems and materials have been applied Full compliance with aviation regulations AP-29 (Russia), CS-29 и FAR-29 High cargo capacity, range and fuel efficiency Legacy of Mi-17 helicopters
of 23 OVERVIEW © 2014 Russian Helicopters, JSC All rights reserved 21, 1 m 4,44 m Ø 3,84 m 25,22 m 5,10 m
of © 2014 Russian Helicopters, JSC All rights reserved Mi-38-2 (Prototype 1) Мi-38-1 (Prototype 2) ТV7-117V (KLIMOV)PW127TS (PRATT & WHITNEY) POWER PLANT OPTION
of © 2014 Russian Helicopters, JSC All rights reserved 7.0 m 8.63 m 1.86 m1.86 m 2.36 m2.36 m Clamshell/ramp with hydraulic actuator 1.43 m wide sliding door Up to 6,000 kg of cargo (up to 29.9 м 3 in volume carriage) inside the cabin Fast loading of wheeled vehicles CARGO CABIN
of © 2013 Russian Helicopters, JSC All rights reserved EC-225 S-92 Mi-8 AW-101 Mi-38 Cabin Volume 29.9 m 3 CARGO CABIN
of © 2014 Russian Helicopters, JSC All rights reserved Internal/External cargo transportation Passenger transportation Corporate / VIP Offshore Search and rescue Medevac MISSIONS
of © 2014 Russian Helicopters, JSC All rights reserved External sling allows transporting up to 7 tons of cargo Equipment installed: system of standard and emergency cargo drop cable inertia reel automatic damping of underslung cargo oscillations INTERNAL AND EXTERNAL CARGO TRANSPORTATION kg
of © 2013 Russian Helicopters, JSC All rights reserved PASSENGER HELICOPTER 29 passengers + flight attendant
of © 2014 Russian Helicopters, JSC All rights reserved Emergency floatation system OFFSHORE
of © 2014 Russian Helicopters, JSC All rights reserved FLIR SAR
of © 2014 Russian Helicopters, JSC All rights reserved 4 VIP seats; Table-cabinet with on-board entertainment system accommodating DVD-player, amplifier Two four-seater sofas with seatbelts LCDs, acoustic systems Additional thermal and acoustic insulation Dual-pane windows reducing noise level VIP/Corporate
of 23 MEDEVAC 13 © 2014 Russian Helicopters, JSC All rights reserved
of © 2014 Russian Helicopters, JSC All rights reserved Cruise speed (TOW=14,200 kg) 290 km/h Max speed (TOW=14,200 kg) 320 km/h Hover ceiling OGE, ISA (TOW=14,200 kg) 3,510 m Service ceiling, ISA (TOW=14,200 kg) 6,000 m Flight range with 3,000 kg of cargo ( Н=500 m, ISA +, 30-min fuel reserve)1000 km Flight range with 5,000 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30-min fuel reserve) 490 km Flight range with auxiliary fuel tanks and 2,700 kg of cargo at MTOW (Н=1,000 m, ISA+10°С, 30- min fuel reserve) 1,350 km Number of passengers30 MTOW15,600 kg Max payload: at the external cargo sling7,000 kg inside transport cabin 6,000 kg Fuel capacity of main fuel tanks (at 0.8 g/cm³ fuel density)3,160kg (3,955l) Fuel capacity with auxiliary fuel tanks (at 0.8 g/cm3 fuel density)3,992 kg (4,990l) FLIGHT PERFORMANCE
of © 2014 Russian Helicopters, JSC All rights reserved Titanium MR hub with elastomeric bearings Composite main rotor blades Х-shape tail rotor AIRFRAME AND SYSTEMS
of © 2014 Russian Helicopters, JSC All rights reserved SAFETY improved fuel system anti-icing protection of blades crashworth y seats jettisonable emergency doors
of © 2014 Russian Helicopters, JSC All rights reserved IBKO-38 by TRANSAS includes: flight and navigation management systems data control system test and control system BSK-38 radio emergency kits emergency and reserve indicators AVIONICS
of 23 Databases of IBKO-38 can be regularly updated: Navigation database (including regional airlines) Landscape database All databases can be updated by developer through the Internet. 18 © 2014 Russian Helicopters, JSC All rights reserved IBKO-38 provides control of all radio equipment by two multifunctional control desks and has pre-flight control of all systems. IBKO-38 can be connected with different devices: Video cameras Electronic optical system Surveillance system AVIONICS
of © 2014 Russian Helicopters, JSC All rights reserved Compliance with AP-29, FAR -29, CS-29 standards Reliability and safety Low operating costs On-condition maintenance Operational range +50ºC÷ -50ºC Operations in icing conditions Bearing ratio 3…5 kg/sq.cent Safe emergency evacuation Centralized tank fuelling Helicopter hydro systems of improved reliability Spacious cargo cabin Low noise and vibration level Independent electrics and air conditioning Energy absorbing landing gear WHY MI-38?
of © 2014 Russian Helicopters, JSC All rights reserved Gate Research and design Completed Prototypes, flight tests Certification Contracts/Deliveries Prototype OP-4 (TV7-117V engine) Prototype OP-3 (TV7-117V engine) Russian Aviation Authorities TC (+6) Prototype OP-2 (PW 127/5 engine) Prototype OP-1 (TV7-117V engine) MILESTONES
© 2014 Russian Helicopters, JSC All rights reserved THANK YOU!
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