Company

Beriev Aircraft Company

a UAC Company

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Design Bureau Flight Test Facility Hydroaviation Training Centre

Production

Test Base at the Black Sea Airlines

Service Centre

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Be-200ESBe-200ES MultipurposeMultipurpose AmphibiousAmphibious AircraftAircraft

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4 567 8 9 10 11 12

Flight crew: two pilots 13 14 15 16 17 18

3 2 1 21 11 20 19

1 – cockpit; 2 – first pilot station; 3 – co-pilot station; 4 – weather radar compartment; 5 – equipment units; 6 – forward maintenance door; 7 – cargo hatch; 8 – blister; 9 – life raft; 10 – liquid retardant tanks; 11 – drain ducts; 12 – aft maintenance door; 13 – forward water tank; 14 – retractable water scoops; 15 – rear water tank; 16 – service compartment; 17 – rear technical compartment; 18 – aft compartment; 19 – lavatory; 20 – aft entrance door; 21 – left emergency door.

This document contains information which is property of BERIEV Aircraft Company and can not be used or published without prior written consent. BERIEV Aircraft Company Powerplant Composition • Two high-bypass ratio cruise engines • Engines are mounted above center-wing with the thrust of 7500 kgf each to protect engines inlets against sprays. • Auxiliary power unit

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• Fly-By-Wire • IFR, pressurized and de-iced • Glass Cockpit • Built-in automated test system • ICAO CAT I, II compliant

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• Fire fighting • Search-and-Rescue, maritime patrol • Ecological monitoring and pollution control • Medevac • Freight and passenger

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Fast to reach fire zone, cruise speed up to 367 kts

Maximum take-off weight, kg……….……………………………………..…………………41000 Operating ceiling, m..……………………………………………………………….…………8100 Economic speed, km/h..……………………… …………………………………………….…550 Range of flight with one-hour fuel reserve, km.…………………………….....…………….3150 Take-off distance up to altitude 10.7 m (ISA, sea level), m: from land……………………………………………………………………1350 from water…..……………………………………………………….…..…1600 Landing distance from altitude 15 m (ISA, sea level), m on land………………………………………………..……………….…....1050 on water……………………………………………………………….…….1300 Seaworthiness, m..……………………………………………………………… up to 1.2 (state 3)

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Aerodrome B-class (1,800 m paved runway)

Hydrodrome fitted 18 m (59 ft) with ramp, minimum water depth 2.6 m

Mooring to standard pier up to 48 hours (131 ft ft 3 in) (131 40 m min.

Max. inclination 7 deg 2.5 m (8 ft m 2 ft) 2.5

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Maximum water/retardant weight 12,000 kg (3,170 US gal) Water scooping time 14 seconds Dropping speed 175 km/h (94 kts) Turn radius 250 m (833 ft)

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Integrated water tanks are placed under the cabin floor.

Tanks are divided into 8 sections, each equipped with the dedicated door.

Four tanks for liquid fire foam.

Two low-drag scoops ensure intake of full load of water.

Pre-programmed water release sequence with water tanks doors opened simultaneously, separately, or consecutively.

This document contains information which is property of BERIEV Aircraft Company and can not be used or published without prior written consent. BERIEV Aircraft Company Fire Fighting System Water filling indication (System status monitor display) SFS Control panel Water amount picked up (Overhead panel) Selector switch of water amount to be scooped Drop modes selector switch Liquid chemicals mixing Scoopers extension/retraction indication Tanks doors closed/opened position indication

Controls • water release button (safety guarded) • scoopers extension/retraction pushbutton (for each pilot)

TANKS FULL

Emergency drop Co-pilot

Emergency drop Captain

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Water Scooping Pattern

1800-2300 m

t

f

5

3

o

t

b

m

i

l

C

Approachft from 50 900 m (2,955 ft)

Total distance includes approach from 15-m (50-ft) and climb up to 10.7-m (35-ft) altitude

Conditions: ISA

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• Safety for piloting in fire fighting missions

Angle of attack limiter for enhanced protection in all configurations, including flights in icing conditions.

• High thrust-to-weight ratio

Climb rate of 16.5 m/sec (3300 ft/min) ensures safety in mountains.

Capable of climbing after engine failure during scooping.

High speed

High cruise speed 680 km/h (367kts) to reach fire quicker.

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In September, 2010 EASA issued Type Certificate for Bе-200ES-Е amphibious aircraft. In parallel the Supplement to Type Certificate for the Bе-200ES-Е aircraft was issued by IAC AR.

This document contains information which is property of BERIEV Aircraft Company and can not be used or published without prior written consent. BERIEV Aircraft Company Be-200ES Fleet Status as of 2013

2012 Countries Total Fleet status

Be-200 in Russia Azerbaijan 9 Operation 8 1

Russia Be-200 on 6 in USA 16 Order 2013-2014 10 6 in option 6 in option

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Beriev-200 Production and Delivery Rate

Production Rate: up to 10 Aircraft / Year Total

Year 2013 2014 2015 2016 2017 2018 2019 2020 8 Years No. of aircraft Production 2 3 6 6 6 6 6 6 41 Output

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Low utilization make cost per hour expensive for new equipment

Total cost nearly divided by Two

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 Target to increase Aircraft utilization beyond 300 h/year  FF in northern hemisphere in Summer and in South hemisphere in Winter  Other mission: SAR, Freight  Hourly rate could be divided nearly by two

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 Beriev offers different lease option:  Long term lease (20 years) including sustained steadiness  Operating lease Be-200 with seasonal steadiness  Be-200 available with FF crew and maintenance  Flight training including private land and sea base and flight simulator  Operational design and production plants to tune your Be- 200 to your requirement

This document contains information which is property of BERIEV Aircraft Company /EADS IRKUT SEAPLANE SAS and can not be used or published without prior written consent. BERIEV Aircraft Company Operation The Be-200ES aircraft have been in fire fighting operations by Beriev Aircraft, Russian EMERCOM and Disaster Relief Ministry of Azerbaijan:

- Italy: 2004 and 2005

- Portugal: 2006 and 2007

- Indonesia: 2006

- Greece: 2007

- Russia: 2004 – 2012

- France: 2011

- Serbia: 2011-2012

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Operation in 2004-2005

• Operation for Protezione Civile

• Based in Olbia, Sardegna to cover all Italian territory within 45 minutes – 1 hour.

• 4 Italian pilots trained at Beriev Training Center and type rated for Be-200ES

• Operated by joint Russian-Italian crews

• 20 minutes time span from fire call to T/O.

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In total the Be-200 made in 2004 & 2005 operation:

215 flight hours of fire fighting and familiarization flights

Dropped 5415 tons of water mixed with chemical foam

Average number of drops per block hour: 4,76/h

Average drop in Fire mission: 9,5 tons of water

Average intervention speed: 555km (300nm)/hour

This document contains information which is property of BERIEV Aircraft Company and can not be used or published without prior written consent. BERIEV Aircraft Company Operation in Italy: evaluation of results • With the Italian pilots in control of the aircraft in every flight, response to ground communication was immediate.

• Familiarization was important to pre-identify the applicable scooping points.

• Speed and powerful engines allowed to make drops in climb and use more headings for scooping in the lakes.

• The Be-200 made around 40% of all scoopings in the open sea with the wind around 15m/sec (30 kts).

• The aircraft was operated together with Canadair aircraft and complementing each other at different stages of fire.

• The aircraft integrated in the existing fire protection system.

• Technical requirements were updated based on the operation.

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Contracted by the Portuguese Ministry of Interior, the Be- 200ES was engaged in fire fighting operation in Portugal in summer 2006 (one aircraft) and 2007 (two aircraft). The Be-200 was based in central Portugal at the Air Force Base in Monte Real. The Portuguese evaluator and coordinator participated in all flights.

Base:MonterealBase:Montereal

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Portugal 2006

26 fire fighting missions were performed by one aircraft with 200 water scoopings in total:

• Total flight time in fighting fires 80h 45min • Total amount of water dropped on fires 1621 tons • Total flight time 100h 20min

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Total block-time hours:minutes 181:36

Total quantity of water t 3817 dropped

Average distance airfield- km 125 fire

Average distance fire- km 30 scooping area

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Moscow Ryazan

Volgograd

Emergency situation was announced inside 7 subjects of the Russian Federation. More than 7,000 natural fire centers were observed within the area of more than 430 000 ha. The estimated damage exceeds 14 bln. roubles. More than 50 people lost their lives in fire and about 2,500 homes were burned.

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The aircraft performed over 700 flight hours during two months with minimum time in maintenance.

About 600 tons of water in average were dropped by one Be-200ES per day.

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July 2011 –Experimental Fire Fighting Operation in France

Total flight hours 51 h 12 min.

Water areas researched for scooping 44

Number of scoopings/drops performed 185

Total water dropped 1387 tons

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French pilots gave positive comments on the following aircraft performance:

• The cockpit is spacious and comfortable, ergonomics is good • Avionics and displays are excellent; the feeling of “Airbus” cockpit. • Voice and visual indication and warning system are very useful and informative. • Radio communication with ground functions well. • Weather radar is very useful in flights in difficult weather conditions. • Autopilot is very important for ferry/transit flights. • Pressurized cabin is very useful. • Exceptional engines thrust. • Excellent speed characteristics.

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Experimental Fire Fighting Flights in France Beriev pilots assessment:

• Be-200 can operate in the most of the water areas used by Canadairs

• Due to the high thrust the aircraft is capable to: o fast climb to high altitude to reach mountainous fires: overall cycle “fire-scooping area” is reduced. o safe drop in direction of steep shores and mountains: even in the case of one engine failure the aircraft can climb out of the canyon after water drop.

• Due to high speed the aircraft is capable to: o reach quickly the alternate scooping area in case of adverse sea and wind conditions: overall cycle on fire is maintained. o get fast to remote areas and stop fires before they start growing.

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• SAFETY: improved painting scheme for better visibility, additional emergency drop buttons on pilot and co-pilot sticks, relocation of fuel filling opposite to APU, indication and warning system modifications, angle of attack limiter, introduction of map.

• FOAM SYSTEM: increase of chemical tanks volume up to 1200 liters, installation of chemical tank level gauge inside the cabin.

• WATER SYSTEM: modification of water tank system, scooping and drops indication the cockpit.

• HULL: bottom reinforcement to withstand shocks during rough water operation.

• FLIGHT HANDLING: reduction of extension/retraction time for wing high-lift devices, modification of control stick loads for easier handling.

• OTHER: autopilot version capable of category 2 landing.

This document contains information which is property of BERIEV Aircraft Company and can not be used or published without prior written consent. BERIEV Aircraft Company Operational results and conclusions • The work in Europe confirmed the design solution and helped to identify and modify critical areas.

• Today the Be-200 is the robust fire fighting aircraft which has been tested and proved reliable in the sea operation.

• The aircraft is fully adapted to the infrastructure of the airports and aircraft bases of different European countries.

• The aircraft has integrated in the existing organization, technology and strategy of fire fighting of the European countries.

• Range of the aircraft allows to deploy the aircraft on one or two bases to cover the extensive territory. The effect of the aircraft engagement was specifically noticeable due to the fast response to fires in the most remote areas.

• Operation of the Be-200 in the mixed aerial groups of the amphibious and non-amphibious fixed-wing aircraft and helicopters showed excellent interaction of various aerial means and complemented the existing operational solutions.

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ThankThank YouYou

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