The Ansat helicopter began development in 1995 and first flew in 1999. It received type certification in 2004 and additional certifications through 2012. Key features include a single main rotor and tail rotor design, composite blades, and a choice of fly-by-wire or hydromechanical flight control systems. The Ansat is used for cargo, passenger, executive, search and rescue, and medical transport. It has seen operational use in Russia and South Korea for tasks like forest monitoring, firefighting, and law enforcement.

1. «ANSAT Helicopter»

2. 1995 – development star 17 августа 1999 года – first flight 2002–certification test flights 2004 – type certificate 2005 – type certificate for two pilot helicopter 2005 – supplementary certificate for emergency splashdown system Aerazur 2005– serial production start Key dates Авторские права.2011.ОАО "Вертолеты России". Все права защищены 2

3. Supplementary certificate on hydro-mechanic control system -June 2012. Supplementary certificate on HEMS module – October 2012. Key dates Авторские права.2011.ОАО "Вертолеты России". Все права защищены 3

4. General view Авторские права.2011.ОАО "Вертолеты России". Все права защищены 4

6. Design with single main rotor and tail rotor

7. Hinge-free hubof main rotor

8. Fiberglass plastic of main and tail rotors’ blades

9. Two different control systems

10. 4-fold redundant Fly-by-wire control system

11. hydromechanicalcontrol system

12. PW-207K engines by Pratt&Whitney (Canada)

13. Onboard information check system

14. Skid landing gearMain technical characteristics Авторские права.2011.ОАО "Вертолеты России". Все права защищены 5

15. Main flight performance Авторские права.2011.ОАО "Вертолеты России". Все права защищены 6

16. Comprises of twoPW-207K engines with single-stage centrifugal compressor and single-stage axial turbine of gas generators Digital electronic regulators(FADEC)ensures continuous rotation speed of main rotor Emergency mechanical system of manual control is available Electric start-up in automatic or manual modes PW-207K operating modes: 2.5 minOEI 710 hp ContinuousOEI 648hp Take-off 630 hp Max continuous558 hp Power plant Авторские права.2011.ОАО "Вертолеты России". Все права защищены 7

18. Two jettisonable doors

19. Traditional controls

20. Windscreen wipersfor one pilot (basic variant) Cockpit Авторские права.2011.ОАО "Вертолеты России". Все права защищены 8

21. for two pilots for two pilots (basic variant) Cockpit Авторские права.2011.ОАО "Вертолеты России". Все права защищены 9

23. MR brake control

24. Manual engines control

25. Rafts (floats) emergency release control

27. Ease of routing in the helicopter

28. No maintenance is requiredControl system – hydromechanical control system Авторские права.2011.ОАО "Вертолеты России". Все права защищены 10

30. System provides for installation of electrical actuators

31. Stability augmentation system (SАS-А) allows application of electrical actuatorsControl system – hydromechanical control system Авторские права.2011.ОАО "Вертолеты России". Все права защищены 11

33. Electronic module (computer)

34. Panel

35. Electrohydraulic control actuator

36. Roll rate sensors

37. Swash plate

38. Rods in aft-booster bayFly-by-wireControl system Авторские права.2011.ОАО "Вертолеты России". Все права защищены 12

39. Main rotor blade is rectangularin plan, made of composites, featureserosion-preventivebinding and trimmer plate. Main rotor hug is hinge-free, torsion bar is a resilient element, made of composite materials. No lubrication required. Main rotor Авторские права.2011.ОАО "Вертолеты России". Все права защищены 13

41. computation and formation unitБВФ-А

43. formationand output of information to protected data storage device

44. input of pre-flight details

46. Complex intra-cockpit warning

47. Data loading and off-loading to portable computer

48. Pre-flight and post-flight check of systems’ and aggregates’ statusOnboard information check system Авторские права.2011.ОАО "Вертолеты России". Все права защищены 14

50. Most of the sorties performed at economical speed

53. Cleared for operation with MTOW 3,600 kgOperational features Авторские права.2011.ОАО "Вертолеты России". Все права защищены 15

54. Operational experience Авторские права.2011.ОАО "Вертолеты России". Все права защищены 16

56. Flight engineer introduced to the crew

58. Training of instructorsAnsat – U Авторские права.2011.ОАО "Вертолеты России". Все права защищены 17

59. 29.10.2008 – signed Act on State Joint Trials 2 prototypes built 2009 – launch of production Delivered: 2009 – 6 helicopters 2010 – 2 helicopters 2011 – 5 helicopters (in production) Over 40 helicopters to be produced by 2018 Ansat - U Авторские права.2011.ОАО "Вертолеты России". Все права защищены 18

60. Operation of Ansat - U Авторские права.2011.ОАО "Вертолеты России". Все права защищены 19

61. Total flight hours Авторские права.2011.ОАО "Вертолеты России". Все права защищены 20

62. Assigned service life Авторские права.2011.ОАО "Вертолеты России". Все права защищены 21

64. Lift facilities

65. Assembly access facilities

66. Assembly-dismantling facilitiesGround support facilities Авторские права.2011.ОАО "Вертолеты России". Все права защищены 22

68. Handling facilities of the systems and units

69. Helicopter protection facilities on the ground

70. Helicopter support tool

71. Power source Ground support facilities Авторские права.2011.ОАО "Вертолеты России". Все права защищены 23

72. Visual laboratory resources Training computer class Ground based complex of training Training simulator Flight-navigation simulator Training Complex - Structure Авторские права.2011.ОАО "Вертолеты России". Все права защищены 24

74. Operation specifics

75. Flight crew instructions

77. 7 Technical stuff instructionsTraining complex visual aid Авторские права.2011.ОАО "Вертолеты России". Все права защищены 25

79. electronic technical documentation;

80. electronic cockpit.Training complex – training computer class Авторские права.2011.ОАО "Вертолеты России". Все права защищены 26

82. intended for initial training;

84. Registration Action trainee for analysisProcedural simulator Авторские права.2011.ОАО "Вертолеты России". Все права защищены 27

86. Total simulation of the flight

87. Intended for initial training (engine start, takeoff)

89. reducing (50-70%) fuel consumption;

90. reducing the preparation time;

91. improving safetyFlight simulator Авторские права.2011.ОАО "Вертолеты России". Все права защищены 28

93. Global Service Net

94. Rise of aircrew and technical staff level

95. New cooperation format

96. IT technology (web-portal, cMRO system)

97. Complex service contracts

98. Power by the hour schemeILS. Development prospects Авторские права.2011.ОАО "Вертолеты России". Все права защищены 29

100. PASSENGER

101. EXECUTIVE

102. SEARCH & RESCUE

103. MEDEVAC

104. SCAUTConfigurations Авторские права.2011.ОАО "Вертолеты России". Все права защищены 30

105. Program «Ansat» The overall cabin volume is 8 m3 and there aresix cargo retainers available… … Simple transformation for 8 passengers transportation. CARGO & PASSENGER Configurations Авторские права.2011.ОАО "Вертолеты России". Все права защищены 31

106. ANSAT PASSENGER specialized configuration provides comfortable transportation of 6 persons. Emergency exit Passenger seat «Sigma» Helios Wardrobe PASSENGER Configuration Авторские права.2011.ОАО "Вертолеты России". Все права защищены 32

107. ANSAT EXECUTIVE Configuration is a combination of the high level comfort and mobility. The cabin provides an opportunity to install different types of interior parts, cloakroom, luggage compartment and lavatory. EXECUTIVE Configuration Авторские права.2011.ОАО "Вертолеты России". Все права защищены 33

109. Unique performances of Ansat permit to operate helicopter in all-weather conditions at Day and Night time.SEARCH & RESCUE Configurations Авторские права.2011.ОАО "Вертолеты России". Все права защищены 34

111. Rendering emergency medical aid to the injured and suffering;

112. Evacuation of casualties and survivors to healthcare facilitiesMEDEVAC Configurations Авторские права.2011.ОАО "Вертолеты России". Все права защищены 35

113. Compliance with SAR helicopter requirements Up to 2stretchers installation SAR winch installation High climb rate (12 m/s) maximum speed ( 270 km/h) wide sliding door, HOT&HIGH operations HIGE 3000 м Service ceiling 4 800 м ОАТ -50 до +50 Transportation up to 7 passengers 2 patients and 2paramedics in HEMS configuration Largest capacity in light twin turbo class 8 m3 Functionality Авторские права.2011.ОАО "Вертолеты России". Все права защищены 36

114. Ansat – is the best proposal for your business. Balanced performance Price – more than 20% lower than other in class Lower operational expenses It is best in terms price-vs-functionality Why Ansat Авторские права.2011.ОАО "Вертолеты России". Все права защищены 37

115. We would be proud to give you more information on the static. We would be glad to provide you with information about PRICE on every configuration. We are waiting for your interest. Ivancov AndreyV. +7 (495) 6275545 +7 (915) 3848193 ivancov@rus-helicopters.com Kiyamov MaratR. +7 (843) 550 0000 kiyamov_mr@kazanhelicopters.com Let us know you need Ansat Авторские права.2011.ОАО "Вертолеты России". Все права защищены 38

116. Thank you for your attention! Россия, 107113, Москва Сокольнический вал 2А, стр. 2 Тел.: +7(495) 6275545 add. 228 Моб.: +7(915) 384-8193 E-mail: ivancov@rus-helicopters.com Авторские права.2011.ОАО "Вертолеты России". Все права защищены 39