Typical Reserve Policy

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2 Three View Drawing Payload Range Length Height Wingspan m / 98.2 ft.28 m /.7 ft m / ft Flight Techniques: Climb: 20Kts/280Kts/M 0.78 Cruise: M 0.78 / FL 70 Descent: 0.78/280Kts/20Kts Typical Reserve Policy 2

3 Superiority Weights Performance SSJ0 Basic SSJ0 LR Basic SSJ0 LR SSJ0 Passengers (Standard Single 2 seat pitch) Abreast Maximum Takeoff Weight (MTOW), kg / lb 4,880 / 1, 49,40 / 9,019 Maximum Payload, kg / lb 12,24 12,24 Maximum Landing Weight (MLW), kg / lb 41,000 / 90,90 41,000 / 90,90 Maximum Zero Fuel Weight (MZFW), kg / lb 40,000 / 88,18 40,000 / 88,18 Maximum Fuel Weight, kg / lb 12,690 / 27,976 12,690 / 27,976 Engine SaM, SaM, Thrust Class (APR SLS/ISA+1 C), lb 17,00 17,800 Take-off Thrust (NTO SLS/ISA), lb 1,400 16,0 Range, nm 1,64 2,470 Maximum Cruise Speed, Mach Maximum Flight Level Time to Climb to FL 00, min Take-off Field (ISA, SL), m / ft 1,71 /,679 2,02 / 6,72 Take-off Field (ISA, SL, 98 Pax), m / ft 1,90 / 4,8 1,90 / 4,8

4 Separated passengers and baggage movement to reduce TAT Reduced main LG wheel track and base facilitates operations in small airports (ft) (m) (m) (ft) 1 Passenger loading bridge 2 Passenger ramp Cargobelt loader 4 Baggage cart Catering truck 6 Fueling truck 7 Potable water 8 Waste water Aft Cargo door height Between 1.48 m and 1.68 m Main LG wheel base m Main LG wheel track.74 m 4

5 Sukhoi Superjet 0/9 (SSJ0/9) Baggage capabilities Flexible configuration SSJ0 E190 CRJ900NG CRJ 00 0,7 m 2 OVH Bin Cross Section + 2 * 0,11 m 2 2* 0,4 m 2 2* 0,4 m 2 0,19 m 2 Dual Class 88 Pax 8 /2 ) OVH Bin Volume (m / ft ),62 m / 198,4 ft, m / 186,1 ft 4,29 m / 11, ft 4,66 m / 164, ft Cargo Compartment Height (mm / in) 1,016 mm / 40 in 940 mm / 7 in 60 mm / 22 in 60mm / 22 in Cargo Volume (m / ft ) 21,7 m / 768, ft 21,9 m / 772 ft 16,8 m / 9, ft 17, m / 619, ft Volume Per Pax (m / ft ) 0,28 m / 9,866 ft 0,27 m / 9,776 ft 0, m / 7,02 ft 0,22 m / 7,997 ft Standard Single Class 98 Pax 2 )

6 Cabin configuration layout of passengers double class 87 8, 2 Cabin configuration layout of passengers accommodation pitch 2 pitch 2 pitch Interior Items Q.ty G1 - FWD Galley (Wet & Powered) 1 G2 - AFT (Wet & Powered) 1 G4 - FWD (Dry & Powered) 1 L - Lavatory 2 S - Wardrobe / Stowage 2 Galley Details G1 G2 G4 (*) Half-Size Trolley 2 Inserts Full-Size Trolley Standard Container(**) oven (2 Portions) 2 1 Beverage Maker 1 2 Interior Items Q.ty G1 - FWD Galley (Wet & Powered) 1 G2 - AFT (Wet & Powered) 1 L - Lavatory 2 S - Wardrobe / Stowage 1 Miscellaneous Stowage 1 2 (**) = Std Container location can accommodate ice drawer (*) = Galleys Inserts are BFE and ATLAS Standard Galley Details G1 G2 Half-Size Trolley 2 Inserts Full-Size Trolley Standard Container(**) 2 4 oven (2 Portions) 2 Beverage Maker 1 2 Miscellaneous Stowage 1 6

7 Superior passenger comfort 6 4 Ground service connections Ground HP air start connector 2 IDG oil filling connector Engine oil filling connector 4 Pressure fueling coupling Pressure fueling coupling (optional) 6 Fueling control panel 7 1 hydraulic system service panel, hydraulic fluid drain connector and 1, 2 and bootstrap reservoirs top-up connector 8 hydraulic system service panel and hydraulic fluid drain connector 9 Waste service panel 2 hydraulic system service panel and hydraulic fluid drain connector 11 APU oil filling connector 12 Potable water service panel 1 Brake system hydraulic accumulators charging ports 14 LP conditioned air connector 1 Oxygen refill connector 16 Ground crew communication connectors 17 Ground electrical power panel 18 FWD ground service panel 19 Landing gear doors closing button Water drain ports 21 Ground ports 7

8 This document, and all information contained herein, is proprietary information. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document and its content shall not be used for any purpose other than that for which it is supplied. All data in this document is approximate, may change without notice and is subject to certain operating rules, assumptions, and conditions. This document does not constitute an offer, commitment, representation, guarantee or warranty of any kind. The final configuration and performance of this aircraft, and any related commitment, representation, guarantee or warranty shall be determined in a final purchase agreement.

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