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Мi-38 Utility Helicopter

Mi-38

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Мi-38

Utility Helicopter

of 23 2 © 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

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OVERVIEW

3 3 © 2014 Russian Helicopters, JSC All rights reserved

21, 1 m 4,44 m

Ø 3,84 m

25,22 m

5,1

0 m

of 23 4 © 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 23 5 © 2014 Russian Helicopters, JSC All rights reserved

7.0 m

8.63 m

1.86 m

2.36 m

• Clamshell/ramp with hydraulic actuator

• 1.43 m wide sliding door

• Up to 6,000 kg of cargo (up to 29.9 м3 in

volume carriage) inside the cabin

• Fast loading of wheeled vehicles

CARGO CABIN

of 23 7 © 2013 Russian Helicopters, JSC All rights reserved

EC-225

S-92

Mi-8

AW-101

Mi-38

Cabin Volume 29.9 m3

CARGO CABIN

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Internal/External cargo transportation

Passenger transportation

Corporate / VIP

Offshore

Search and rescue

Medevac

MISSIONS

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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

7 000 kg

of 23 9 © 2013 Russian Helicopters, JSC All rights reserved

PASSENGER HELICOPTER

29 passengers + flight attendant

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Emergency floatation system

OFFSHORE

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FLIR

SAR

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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

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MEDEVAC

13 © 2014 Russian Helicopters, JSC All rights reserved

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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 passengers 30

MTOW 15,600 kg

Max payload:

at the external cargo sling 7,000 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

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Titanium MR hub with elastomeric bearings

Composite main rotor blades

Х-shape tail rotor

AIRFRAME AND SYSTEMS

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© 2014 Russian Helicopters, JSC All rights reserved

SAFETY

improved fuel system

anti-icing protection of blades

crashworthy seats

jettisonable emergency

doors

17

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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

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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 23 19 © 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 23 20 © 2014 Russian Helicopters, JSC All rights reserved

Gate 2013 2014 2015 2016

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!