3 MC-21 Aircraft Are Engaged in MAKS-2019 Airshow in Flight

PREMIER 3 MC-21 aircraft In Flight program are engaged At Static exhibition in MAKS-2019 Airshow An Aircraft with interior installed

www. irkut.com 2 МС-21-300 MEDIUM RANGE NEW GENERATION AIRCRAFT MOSCOW

CAPACITY OF 163–211 SEATS

RANGE — 6000 KM

Flight range is sufficient Single-class Mixed-class to cover distance from Moscow 211 pax 163 pax to any destination within Europe

Estimated demand till 2038 is: KRASNOYARSK • Russian Federation — over 1000 a/c • Entire world — over 30 000 a/c

www. irkut.com 3 MC-21 CORE CONSEPT

Enhanced passenger comfort: - convenience and comfort demand rises, anthropometric changes: the average passenger became higher Maximum Efficiency www. irkut.com 4 IMPROVING THE PASSENGER COMFORT

Extended fuselage diameter provides: More private space- passenger cabin width is 4.06 m More trespassing — avails to move around the cabin during in-flight service More cabin baggage — 20–25% volume extension of the overhead bins

www. irkut.com 5 INNOVATIONS FOR COMFORT

More natural light due to extended in 15–30% window size More comfortable cabin pressure: equivalent to pressure at 1830 m

www. irkut.com 6 WIDE VARIETY OF OPTIONAL SOLUTIONS

Satellite communication system

Inflight access to internet via Wi-Fi for passengers

Inflight entertainment system

Multifunctional cabin light system

In-seat power socket for passengers

Special sockets for intricate medical equipment

And much more both for passengers and airlines

www. irkut.com 7 WIDER FUSELAGE STIPULATES THE ADDITIONAL ADVANTAGES Boarding and leaving the airplane requires less time Turnaround time gets cut Aircarriers are free to choose either wider seats or wider aisle Spacious cargo compartments contain more payload

www. irkut.com 8 IMPROVING EFFICIENCY COMPOSITE WING OF HIGH ASPECT RATIO • Provides 5–7% of aerodynamic quality improvement • Higher wing bearing capacity, lower drag • Improves flight performance characteristics • Cuts fuel burn • Manufactured by latest innovative infusion technology patented in Russia

www. irkut.com 9 IMPROVING EFFICIENCY

INNOVATIVE ENGINES

PW1400G or UEC PD-14 engine options

• High by-pass ratio cuts fuel burn • Matching the current and perspective ecological standards for CO2, NOx & noise emissions

www. irkut.com 10 NEW Fly-By-Wire System Ergonomic flight deck: - Big 15” LCD screens GENERATION - EFB - Windshield indication option SYSTEMS & - Integrated maintenance System supporting transfer of information to Ground handling services AVIONICS - Enhanced Vision system with IR- & UV-sensors option

www. irkut.com 11 NEW GENERATION SYSTEMS & AVIONICS For the first time Fly-by-wire system aggregated with active side-sticks with full feedback effect • Improve coordination between the Captain and the 2nd pilot • Positively affect the pilotage accuracy and safety • Highly rated by test pilots www. irkut.com 12 NEW TECHNOLOGICAL ENVIRONMENT

IMPLEMENTING MULTIPLE INNOVATIONS STIPULATED CREATION OF NEW TECHNOLOGICAL ENVIRONMENT: Facility retooling and re-equipment fulfilled The technology for producing big Automated technological lines provide scale composite power structures using vacuum significant fuselage mounting quality infusion had been elaborated and implemented (E.g.: wing caisson) www. irkut.com 13 NEW TECHNOLOGICAL ENVIRONMENT

Design, manufacturing and utilization of aircraft are now covered in digital

New testing and stand facility had been created

The personnel had been trained in order to work in a modern technological environment

MC-21 PROGRAM BRINGS THE AEROSPACE INDUSTRY OF RUSSIA TO A NEW TECHNOLOGICAL LEVEL

www. irkut.com 14 FLIGHT TESTS

Certification tests are en route

MC-21-300 shall be certified in accordance with both Russian and European standards

Currently 3 test MC-21 aircraft are engaged in flight tests

www. irkut.com 15 FLIGHT TESTS Test flights are made by: The 4th aircraft intended for flight tests has been • Test-pilots of Yakovlev Design Bureau assembled, systems montage is underway • Expert pilots of Gromov Flight Research Institute, GosNIIGA, EASA MC-21-300 equipped with UEC PD-14 engines and intended to join flight tests is under construction www. irkut.com 16 FLIGHT TESTS

ACHIEVED RESULTS The aircraft performed flights in a wide range of speeds and altitudes corresponding the main flight regimes

During the test program the following numbers had been achieved: - altitude of 12,500 m - M = 0.89 - true air speed of 949 km/h The results of bot flight and - flight duration — 6.2 hours ground tests confirm correctness of main design and technological solutions

www. irkut.com 17 FLIGHT TESTS

HARSH REGIMES The tests of maximum calculated angles of attack and The efficiency of the instrumental landing flutter in various configurations have been fulfilled system, as well as of the equipment for navigation, landing and external lighting Starting the main engines and auxiliary power units has been confirmed during the night flight have been performed in-flight. The characteristics of the take-off and landing with simulation of the Minimum take-off speed evaluation tests engine failure have been evaluated had been done

www. irkut.com 18 START OF MASS PRODUCTION

Units and components for the aircraft intended for customers are under production The Cooperation participants involved in MC-21 Program are extending their industrial potential

Manufacturing Pool output shall stepwise achieve 72 aircraft per year

www. irkut.com 19 CABIN

CONFIGURATION FOR OUR CUSTOMERS WE OFFER A WIDE RANGE OF CABIN CONFIGURATION VARIANTS

High Density cabin configuration shall be embedded on MC-21-300-004 test aircraft

Economy Seats 211 Seat pitch: - in forepart of the cabin 28 - in rear part 29 Seat type Slim Plus Seat width 18.5 Aisle width 19.6

www. irkut.com 20 MC-21-300 CABIN CONFIGURATION AT MAKS-2019 THE TEST MC-21-300-003 AIRCRAFT EXHIBITED AT MAKS-2019 AIRSHOW

2 class LOPA with 163 seats Avails the passenger to pass the service trolley Instead of 24 seats in Economy a special equipment for tests is installed

Business Economy Seats 16 147 Seat pitch 36 32 Seat type CCII Z85 Seat width 21.5 18 Aisle width 31.5 22.5