Авторские права ОАО "Вертолеты России". Все права защищены – 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

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

Авторские права ОАО "Вертолеты России". Все права защищены 4

5 Meets AP-29 requirements to rotorcraft category А Design with single main rotor and tail rotor Hinge-free hub of main rotor Fiberglass plastic of main and tail rotors blades Two different control systems 4-fold redundant Fly-by-wire control system hydromechanical control system PW-207K engines by Pratt & Whitney (Canada) Onboard information check system Skid landing gear

Авторские права ОАО "Вертолеты России". Все права защищены 6 MTOW3,300 kg Usefull Load1,184 kg Max speed275 km/h Cruise speed250 km/h Optimum speed220 km/h Economic speed120 km/h Max rate of climb12 m/s Max flight range510 km Max endurance3,5 hrs. Hover ceiling (IGE)3,300 m Hover ceiling (OGE)2,900 m Service ceiling5,500 m

Авторские права ОАО "Вертолеты России". Все права защищены 7 Comprises of two PW-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 min OEI710 hp Continuous OEI 648 hp Take-off630 hp Max continuous 558 hp

Авторские права ОАО "Вертолеты России". Все права защищены 8 Two shock-absorbing seats Fisher Two jettisonable doors Traditional controls Windscreen wipers for one pilot (basic variant)

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

Авторские права ОАО "Вертолеты России". Все права защищены 10 СВА Flexball СВА Flexball control linkage Applied by: Eurocopter (EC120, Ecureuil, Dauphin, Super Puma, EC155, EC175, EC135, EC145, NH90), Airbus (A320, A330, A380), Dassault Aviation (Falcon family) Areas of application in the helicopters: Main and tail rotor control (+ fenestron) MR brake control Manual engines control Rafts (floats) emergency release control Fire extinguishers control Advantages: Light weight Ease of routing in the helicopter No maintenance is required

Авторские права ОАО "Вертолеты России". Все права защищены 11 Current status Main and tail rotor mechanical control system with the use of CBA Flexball flexible control linkage is developed System provides for installation of electrical actuators Stability augmentation system (SАS-А) allows application of electrical actuators

Авторские права ОАО "Вертолеты России". Все права защищены 12 Control system is electrohydraulic with 4-fold electric redundancy and 2-fold hydraulic redundancy Includes: Traditional controls with electric sensors Electronic module (computer) Panel Electrohydraulic control actuator Roll rate sensors Swash plate Rods in aft-booster bay

Авторские права ОАО "Вертолеты России". Все права защищены 13 Main rotor hug is hinge-free, torsion bar is a resilient element, made of composite materials. No lubrication required. Main rotor blade is rectangular in plan, made of composites, features erosion-preventive binding and trimmer plate.

Авторские права ОАО "Вертолеты России". Все права защищены 14 Composition : two electronic raster multifunctional displays ИМ-14 computation and formation unit БВФ-А indication control panel ПУИ-А Functions : input of parametric and signaling information from engines and systems formation and output of information to protected data storage device input of pre-flight details data gathering and real-time processing, output of data on systems status and remaining service life Provides : Duplicate check of onboard systems Complex intra-cockpit warning Data loading and off-loading to portable computer Pre-flight and post-flight check of systems and aggregates status

Авторские права ОАО "Вертолеты России". Все права защищены 15 Features of Ansat operation by Forestry Aviation of South Korea Monitoring of forests, fire-fighting and pest control Most of the sorties performed at economical speed Performs terrain following flights in mountainous areas Features of Ansat operation by Radar-MMS, JSC Testing of special electronic equipment, including in the areas of HIRF impact Cleared for operation with MTOW 3,600 kg Features of Ansat operation by Aviation of Russian Federal Security Bureau Supervision and flight crew training Nap-of-the-earth flights, hot and high sorties

Helicopter No. OperatorInduction date Flight hours 410А01Police of South Korea А02Forestry aviation of South Korea А03Forestry aviation of South Korea А04Forestry aviation of South Korea Radar-MMS, JSC Aviation of Russian Federal Security Bureau Aviation of Russian Federal Security Bureau Авторские права ОАО "Вертолеты России". Все права защищены 16

Авторские права ОАО "Вертолеты России". Все права защищены 17 Program «Ansat» Main differences: Derived from Ansat Skid landing gear replaced with wheels Flight engineer introduced to the crew Amended onboard equipment suite Key tasks: Initial pilot training Training of instructors

Авторские права ОАО "Вертолеты России". Все права защищены – 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

Авторские права ОАО "Вертолеты России". Все права защищены 19 Helicopter No. OperatorInduction date Flight hours 330ХХRussian MoD ХХRussian MoD ХХRussian MoD ХХRussian MoD ХХRussian MoD ХХRussian MoD ХХRussian MoD ХХRussian MoD

Авторские права ОАО "Вертолеты России". Все права защищены 20 ModelProducedLeaderCumulative flight hours Prototypes ,510 Ansat; Ansat - К101891,069 Ansat -U82271,027 TOTAL243,606

Авторские права ОАО "Вертолеты России". Все права защищены 21 Description Assigned service life, h Service time, years Helicopter Fuselage Tail boom Main rotor blade Main rotor hub Tail rotor Transmission accessories Swash plate Actuating portion of main rotor control system Actuating portion of tail rotor control system Landing gear10000 t/l12

Авторские права ОАО "Вертолеты России". Все права защищены 22 Supply support Facilities of towing, containment, tie-down, transport Lift facilities Assembly access facilities Assembly-dismantling facilities

Авторские права ОАО "Вертолеты России". Все права защищены 23 Supply support Operating stock Handling facilities of the systems and units Helicopter protection facilities on the ground Helicopter support tool Power source

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

Авторские права ОАО "Вертолеты России". Все права защищены 25 Назначение Design description Operation specifics Flight crew instructions Technical stuff instructions Состав Posters set (6 sets) Printed materials (19 books) 12 flight crew instructions 7 Technical stuff instructions

Авторские права ОАО "Вертолеты России". Все права защищены 26 Purpose for theoretical training: Computer aided training programs; electronic technical documentation; electronic cockpit.

Авторские права ОАО "Вертолеты России". Все права защищены 27 Возможности Selecting various training exercises Registration Action train ee for analysis Purpose: Aircrew training; intended for initial training; light version of flight-simulator;

Авторские права ОАО "Вертолеты России". Все права защищены 28 Purpose: Aircrew training Total simulation of the flight Intended for initial training (engine start, takeoff) Crew training on the main training stage on the entire task complex Effect: reducing the cost of training; reducing (50-70%) fuel consumption; reducing the preparation time; improving safety

Авторские права ОАО "Вертолеты России". Все права защищены 29 One stop shop concept Global Service Net Rise of aircrew and technical staff level New cooperation format IT technology (web-portal, cMRO system) Complex service contracts Power by the hour scheme

Авторские права ОАО "Вертолеты России". Все права защищены 30 CARGO & PASSENGER PASSENGER EXECUTIVE SEARCH & RESCUE MEDEVAC SCAUT

Авторские права ОАО "Вертолеты России". Все права защищены 31 The overall cabin volume is 8 m 3 and there are six cargo retainers available… CARGO & PASSENGER Configurations Program «Ansat» … Simple transformation for 8 passengers transportation.

Авторские права ОАО "Вертолеты России". Все права защищены 32 PASSENGER Configuration 1.Emergency exit 2.Passenger seat « Sigma » Helios 3.Wardrobe ANSAT PASSENGER specialized configuration provides comfortable transportation of 6 persons.

Авторские права ОАО "Вертолеты России". Все права защищены 33 EXECUTIVE Configuration 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.

Авторские права ОАО "Вертолеты России". Все права защищены 34 ANSAT Basic Multipurpose can be easily transformed to Search and Rescue (SAR) configuration by special equipment setting. Unique performances of Ansat permit to operate helicopter in all-weather conditions at Day and Night time. SEARCH & RESCUE Configurations

Авторские права ОАО "Вертолеты России". Все права защищены 35 MEDEVAC Configurations 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; Rendering emergency medical aid to the injured and suffering; Evacuation of casualties and survivors to healthcare facilities

Авторские права ОАО "Вертолеты России". Все права защищены 36

Авторские права ОАО "Вертолеты России". Все права защищены 37

Авторские права ОАО "Вертолеты России". Все права защищены 38 Ivancov Andrey V. +7 (495) (915) Kiyamov Marat R. +7 (843)

Авторские права ОАО "Вертолеты России". Все права защищены 39 Россия, , Москва Сокольнический вал 2А, стр. 2 Тел.: +7(495) add. 228 Моб.: +7(915)