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!