1. Ка-226 Helicopter Ka-226 helicopter Program Director Zarschikov Denis © 2011 ОАО «Вертолёты России». Все права защищены

2. Contents Ka-226 helicopter. General Information Helicopter operation milestones Modifications & Development Helicopter systems After Sales Support

3. Ka-226 helicopter. General Information

4. Ka-226 – light multipurpose helicopter with coaxial rotor, twin «ROLLS-ROYCE» engines. Main applications of Ka-226 «250-C20R/2» helicopter model: © 2011 ОАО «Вертолёты России». Все права защищены Patrol, Law enforcement EMS

5. Compact design Excellent maneuverability and controllability for flights in dense urban conditions Take-off/landing capability in constrained conditions Helicopter Ка-226. Main Advantages

6. Maximum safety in flight (Category А) Continues take-off and safe landing in case on one engine failure OEI flight ability in a wide temperature/altitude range independently of gross weight Absence of a tail rotor – safety on the ground Helicopter Ка-226. Safe Application

7. Torsion type hubs No lubrication points Latent defect manifestation excluded Damage resistance Favorable operation experience © 2011 JSC Russian Helicopters. All rights reserved Main Rotor System

8. The main distinctive feature of the Ка-226Т is its fuselage modular design enabling its multifunctional operation by application of unified easily detachable modules containing mission equipment. © 2011 JSC Russian Helicopters. All rights reserved Modular Design

9. Helicopter operation milestones

10. - Ministry of Interior Affairs - Federal Security Service of Russia - «International Airport Orenburg» - EMERCOM of Ukraine - «Gazpromavia» - 9 AC - 6 AC - 2 AC - 1 AC - 4 AC The beginning of Ка-226 helicopter operation: February 2006 Number of in-operation helicopters: 22 Ka-226 helicopter operators: Helicopter operation © 2011 ОАО «Вертолёты России». Все права защищены

11. Kazan (Republic of Tatarstan) Astrahan Nalchik Sankt-Petersburg Voronezh Moscow Operation areas © 2011 ОАО «Вертолёты России». Все права защищены Orenburg Krasnodar Stavropol Gelendgik Yoshkar-Ola

12. Total fleet utilisation: 6307 flight hours (June 2011) © 2011 ОАО «Вертолёты России». Все права защищены 17% 66% 14% 3% 0,15%

13. © 2011 ОАО «Вертолёты России». Все права защищены Since 2006 to the present time Kamov company has collected information about 205 failures of Ка-226 helicopter. 29% 9%9% 2,5% 5,25% 2% 5% 20% 11% 5,25% 2% 7% Helicopter system failures

14. © 2011 ОАО «Вертолёты России». Все права защищены №Year Number of failures in flights Average FH before failure 120091595,2 2201018126 Note: Data extractions from reports №№ 226-93-47/10 и 226-93-16/11 Helicopter Ка-226 reliability : years 2009-2010

15. Modifications & Development © 2011 ОАО «Вертолёты России». Все права защищены

16. Helicopter Ка-226Т Deliveries to civil and military Customers in the RF and world markets Main application versions – transportation/passenger, cargo, EMS, emergency rescue, patrol, reconnaissance/surveillance, fire fighting. Helicopter Ка-226Т, Modification of a serially produced Ка-226 helicopter Proposed certification : to АП-29 Requirements (IAC AR) – 4 th quarter 2012 to CS-29 Requirements (EASA) – 4th quarter 2013 © 2011 JSC Russian Helicopters. All rights reserved Helicopter Ка-226T

17. The Ka-226T can be operated in the following conditions: IFR&VFR both day and night standard and adverse weather conditions icing conditions over vast water surface in tropical conditions within (  ) 50  C to (  ) 50C  temperature range at max wind speeds of 16 m/s at hover 18 m/s at rotor speed up 18 m/s at take-off and landing 5 m/s at tail wind take-off and landing from ground sites of min 4 kgf/cm2 soil density from sloped sites with lower limit (  ) 5 , upper limit (  ) 10  and lateral limit (  ) 6  to max altitude 7000 m © 2011 JSC Russian Helicopters. All rights reserved Helicopter Ка-226Т. Operating conditions

18. PerfomanceКа-226Ка-226Т Max take-off/landing weight3400 kg3600 кг Maximum flight weight масса3600 kg3800 кг OEW2230 kg2000 кг Max internal load weight in transportation cabin1100 kg1200 кг Max external load weight at the sling1300 kg1500 кг Hover ceiling OGE2600 м4100 м Service ceiling5500 м5700 м Max non-exceeded speed 210 km/h250 km/h Max cruising speed 190 km/h220 km/h Crew1 pilot Passenger7 pax © 2011 ОАО «Вертолёты России». Все права защищены Flight performance

19. NosDescription Time to overhaul hrs/years Service life limit hrs/years 1Fuselagenone18000 / 30 2Engine3000 / -Not limited 3Gear box2000 / -6000/30 4Main rotor mast3000 / -6000 / 30 5Main rotor blades3000 / -6000 / 30 6Dual actuator unit3000 / -6000 / 30 © 2011 JSC Russian Helicopters. All rights reserved Ка-226Т. SERVICE LIFE LIMITS OF MAIN COMPONENTS

20. Helicopter systems © 2011 ОАО «Вертолёты России». Все права защищены

21. Main gear ВР-226Н «Turbomeca» Arrius 2G1 Engines AERAZUR anticrash fuel system Dual actuator unit КАУ-165М Windscreen mitigates the consequences of a birdstrike Integrated Flight & Navigation System. © 2011 ОАО «Вертолёты России». Все права защищены Ка-226Т Main Modifications & Development

22. Power ratings, hp.  Contingency 705  Tale-off 580  Max continuous 580 Output shaft speed, rpm 6 000 Fuel consumption, kg/hp per hour  at take-off rating 0,260  At max continuous rating 0,283 Engine installation weight, kg 118 © 2011 JSC Russian Helicopters. All rights reserved Arrius 2G1 Engine

23. Modern piloting and navigational equipment Integrated navigational system Autopilot Several variants of equipment configuration are available providing for VFR and IFR flights for one and two pilots © 2011 ОАО «Вертолёты России». Все права защищены © 2011 JSC Russian Helicopters. All rights reserved Integrated Flight & Navigation System

24. Fuel tank volume 920 L Single point pressure fuelling provided Auxilliary tanks can be installed and connected 1.Front fuel tanks 2.Fuel quantity transmitters 3.Pumps 4.Drain output 5.Aft fuel tank 6.Overflow pipes 7.Tank attachments 8.Filler ports 9.Residue drain cocks © 2011 JSC Russian Helicopters. All rights reserved AERAZUR anticrash fuel system

25. Crashworthy crew and passenger seats from Fisher+Entwicklunger GmbH & Co KG are certified to JTSO-C127a standard and comply with the FAR-27/29 requirements, endure longitudinal load 18.4 g and vertical load to 30 g. Crew seats can be adjusted to individual pilot parameters both vertically and horizontally. © 2011 JSC Russian Helicopters. All rights reserved Crashworthy crew and passenger seats

26. Skies allow to operate the helicopter from sites of soil density below 4 kgf/cm2 © 2011 JSC Russian Helicopters. All rights reserved Optional equipment Skies

27. Attachment points are provided on the helicopter to install hoisting devices like an ЛПГ-300 or a Goodrich winch of up to 300 kg capacity © 2011 JSC Russian Helicopters. All rights reserved Optional equipment Winch

28. External sling can be used to transport loads weighing to 1500 kg on the helicopter with its transportation cabin module installed or not installed © 2011 JSC Russian Helicopters. All rights reserved Optional Equipment External Load Sling

29. Attachment points are available on the helicopter to mount an inlet particle used separator to clean the air supplied to the engines of dust, sand and foreign objects during taxiing, take off and landing at sandy airfields or dusty sites. 95 % air purification is provided. © 2011 JSC Russian Helicopters. All rights reserved PALL IPS

30. Aircraft diagnostic system monitors operation and performs diagnostics of engines and main gear box condition and main rotor balance status in flight and on the ground in order to reveal potentially dangerous defects © 2011 JSC Russian Helicopters. All rights reserved Aircraft diagnostic system. БСДВ-226

31. Skies allow to operate the helicopter from sites of soil density below 4 kgf/cm2 © 2011 JSC Russian Helicopters. All rights reserved Optional equipment. Skies

32. © 2011 ОАО «Вертолёты России». Все права защищены EMS Universal platform with oxygen bottle Removable stretcher (1 pc) Support for infusions Oxygen control panel, the wall for medical equipment installation

33. © 2011 ОАО «Вертолёты России». Все права защищены Easily cleaned cabin paneling Operation lights in transportation cabin for sliding and aft doors Auxiliary technical systems Medical equipment Dry wash stand Medical personnel seats (2 pcs) Hydro insulating floor cover EMS

34. © 2011 ОАО «Вертолёты России». Все права защищены Thank you