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 star17 августа 1999 года – first flight2002–certification test flights2004 – type certificate 2005 – type certificate for two pilot helicopter2005 – supplementary certificate for emergency splashdown system Aerazur2005– serial production startKey datesАвторские права.2011.ОАО "Вертолеты России". Все права защищены2

3. Supplementary certificate on hydro-mechanic control system -June 2012. Supplementary certificate on HEMS module – October 2012.Key datesАвторские права.2011.ОАО "Вертолеты России". Все права защищены3

4. General viewАвторские права.2011.ОАО "Вертолеты России". Все права защищены4

5. Meets AP-29 requirements to rotorcraft category А

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 characteristicsАвторские права.2011.ОАО "Вертолеты России". Все права защищены5

15. Main flight performanceАвторские права.2011.ОАО "Вертолеты России". Все права защищены6

16. Comprises of twoPW-207K engines with single-stage centrifugal compressor and single-stage axial turbine of gas generatorsDigital electronic regulators(FADEC)ensures continuous rotation speed of main rotorEmergency mechanical system of manual control is availableElectric start-up in automatic or manual modesPW-207K operating modes:2.5 minOEI 710 hpContinuousOEI 648hpTake-off 630 hpMax continuous558 hpPower plantАвторские права.2011.ОАО "Вертолеты России". Все права защищены7

17. Two shock-absorbing seatsFisher

18. Two jettisonable doors

19. Traditional controls

20. Windscreen wipersfor one pilot (basic variant)CockpitАвторские права.2011.ОАО "Вертолеты России". Все права защищены8

21. for two pilots for two pilots (basic variant)CockpitАвторские права.2011.ОАО "Вертолеты России". Все права защищены9

22. СВА Flexball control linkageApplied by: Eurocopter (EC120, Ecureuil, Dauphin, Super Puma, EC155, EC175 , EC135, EC145, NH90), Airbus (A320, A330, A380), DassaultAviation (Falcon family)СВА FlexballAreas of application in the helicopters:Main and tail rotor control (+ fenestron)

23. MR brake control

24. Manual engines control

25. Rafts (floats) emergency release control

26. Fire extinguishers controlAdvantages:Light weight

27. Ease of routing in the helicopter

28. No maintenance is requiredControl system – hydromechanical control systemАвторские права.2011.ОАО "Вертолеты России". Все права защищены10

29. Current statusMain and tail rotor mechanical control system with the use of CBA Flexball flexible control linkage is developed

30. System provides for installation of electrical actuators

31. Stability augmentation system (SАS-А) allows application of electrical actuatorsControl system – hydromechanical control systemАвторские права.2011.ОАО "Вертолеты России". Все права защищены11

32. Control system is electrohydraulic with 4-fold electric redundancy and 2-fold hydraulic redundancyIncludes:Traditional controls with electric sensors

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 systemАвторские права.2011.ОАО "Вертолеты России". Все права защищены12

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 rotorАвторские права.2011.ОАО "Вертолеты России". Все права защищены13

40. Composition:two electronic raster multifunctional displaysИМ-14

41. computation and formation unitБВФ-А

42. indication control panel ПУИ-АFunctions:input of parametric and signaling information from engines and systems

43. formationand output of information to protected data storage device

44. input of pre-flight details

45. data gathering and real-time processing, output of data on systems’ status and remaining service lifeProvides:Duplicate check of onboard systems

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 systemАвторские права.2011.ОАО "Вертолеты России". Все права защищены14

49. Features of Ansat operation by Forestry Aviation of South KoreaMonitoring of forests, fire-fightingand pest control

50. Most of the sorties performed at economical speed

51. Performs terrain following flights in mountainous areasFeatures of Ansat operation by Aviation of Russian Federal Security BureauSupervision and flight crew training

52. Nap-of-the-earth flights, hot and high sortiesFeatures of Ansat operation byRadar-MMS, JSCTesting of special electronic equipment, including in the areas of HIRF impact

53. Cleared for operation with MTOW 3,600 kgOperational featuresАвторские права.2011.ОАО "Вертолеты России". Все права защищены15

54. Operational experienceАвторские права.2011.ОАО "Вертолеты России". Все права защищены16

55. Program «Ansat»Main differences:Derived from AnsatSkid landing gear replaced with wheels

56. Flight engineer introduced to the crew

57. Amended onboard equipment suiteKey tasks: Initial pilot training

58. Training of instructorsAnsat – UАвторские права.2011.ОАО "Вертолеты России". Все права защищены17

59. 29.10.2008 – signed Act on State Joint Trials2 prototypes built2009 – launch of productionDelivered:2009 – 6 helicopters2010 – 2 helicopters2011 – 5 helicopters(in production)Over 40 helicopters to be produced by 2018Ansat - UАвторские права.2011.ОАО "Вертолеты России". Все права защищены18

60. Operation of Ansat - UАвторские права.2011.ОАО "Вертолеты России". Все права защищены19

61. Total flight hoursАвторские права.2011.ОАО "Вертолеты России". Все права защищены20

62. Assigned service lifeАвторские права.2011.ОАО "Вертолеты России". Все права защищены21

63. Supply supportFacilities of towing, containment, tie-down, transport

64. Lift facilities

65. Assembly access facilities

66. Assembly-dismantling facilitiesGround support facilitiesАвторские права.2011.ОАО "Вертолеты России". Все права защищены22

67. Supply supportOperating stock

68. Handling facilities of the systems and units

69. Helicopter protection facilities on the ground

70. Helicopter support tool

71. Power source Ground support facilitiesАвторские права.2011.ОАО "Вертолеты России". Все права защищены23

72. Visual laboratory resourcesTraining computer class Ground based complex of trainingTraining simulatorFlight-navigation simulator Training Complex - Structure Авторские права.2011.ОАО "Вертолеты России". Все права защищены24

73. НазначениеDesign description

74. Operation specifics

75. Flight crew instructions

76. Technical stuff instructionsСоставPosters set(6 sets) Printed materials(19 books)12 flight crew instructions

77. 7 Technical stuff instructionsTraining complex visual aid Авторские права.2011.ОАО "Вертолеты России". Все права защищены25

78. Purposefor theoretical training:Computer aided training programs;

79. electronic technical documentation;

80. electronic cockpit.Training complex – training computer classАвторские права.2011.ОАО "Вертолеты России". Все права защищены26

81. Purpose:Aircrew training;

82. intended for initial training;

83. “light” version of flight-simulator;ВозможностиSelecting various training exercises

84. Registration Action trainee for analysisProcedural simulatorАвторские права.2011.ОАО "Вертолеты России". Все права защищены27

85. Purpose:Aircrew training

86. Total simulation of the flight

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

88. Crew training on the main training stage on the entire task complexEffect:reducing the cost of training;

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

90. reducing the preparation time;

91. improving safetyFlight simulatorАвторские права.2011.ОАО "Вертолеты России". Все права защищены28

92. “One stop shop” concept

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 prospectsАвторские права.2011.ОАО "Вертолеты России". Все права защищены29

99. CARGO & PASSENGER

100. PASSENGER

101. EXECUTIVE

102. SEARCH & RESCUE

103. MEDEVAC

104. SCAUTConfigurationsАвторские права.2011.ОАО "Вертолеты России". Все права защищены30

105. Program «Ansat»The overall cabin volume is 8 m3 and there aresix cargo retainers available…… Simple transformation for 8 passengers transportation. CARGO & PASSENGER ConfigurationsАвторские права.2011.ОАО "Вертолеты России". Все права защищены31

106. ANSAT PASSENGER specialized configuration providescomfortable transportationof 6 persons.Emergency exitPassenger seat «Sigma» HeliosWardrobe PASSENGER ConfigurationАвторские права.2011.ОАО "Вертолеты России". Все права защищены32

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 ConfigurationАвторские права.2011.ОАО "Вертолеты России". Все права защищены33

108. ANSAT Basic Multipurpose can be easily transformed to Search and Rescue (SAR) configuration by special equipment setting.

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 защищены34

110. Light medical issues can be solved by ANSAT Basic Multipurpose with limited medical equipment. The Medevac is used for the following purposes:Urgent delivery of an emergency medical team to the scene of accident;

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

112. Evacuation of casualties and survivors to healthcare facilitiesMEDEVAC ConfigurationsАвторские права.2011.ОАО "Вертолеты России". Все права защищены35

113. Compliance with SAR helicopter requirementsUp to 2stretchers installationSAR winch installationHigh climb rate (12 m/s)maximum speed ( 270 km/h)wide sliding door,HOT&HIGH operationsHIGE 3000 мService ceiling 4 800 мОАТ -50 до +50Transportation up to 7 passengers2 patients and 2paramedics in HEMS configurationLargest capacity in light twin turbo class 8 m3FunctionalityАвторские права.2011.ОАО "Вертолеты России". Все права защищены36

114. Ansat – is the best proposal for your business.Balanced performancePrice – more than 20% lower than other in classLower operational expenses It is best in terms price-vs-functionality Why AnsatАвторские права.2011.ОАО "Вертолеты России". Все права защищены37

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. IvancovAndreyV.+7 (495) 6275545+7 (915) 3848193ivancov@rus-helicopters.comKiyamovMaratR.+7 (843) 550 0000kiyamov_mr@kazanhelicopters.comLet us know you need AnsatАвторские права.2011.ОАО "Вертолеты России". Все права защищены38

116. Thank you for your attention!Россия, 107113, МоскваСокольнический вал 2А, стр. 2Тел.: +7(495) 6275545 add. 228Моб.: +7(915) 384-8193 E-mail: ivancov@rus-helicopters.comАвторские права.2011.ОАО "Вертолеты России". Все права защищены39