Beriev - Be-200ES amphibious aircraft

Be-200ES

AMPHIBIOUS AIRCRAFT
Be-200ES

Multipurpose amphibious aircraft for the Russian Ministry for Emergency Situations is intended for:
- firefighting;
- rendering urgent help in critical areas of emergency;
- search&rescue missions in the sea, ambulance missions;
- air freighting.

The Be-200ES amphibian is equipped with two bypass turbojet engines D-436TP (Motor Sich, Ukraine), 7650 kg take-off thrust each.

On June 20, 2003 Type Certificate for Restricted Category Aircraft 220--200 was issued.

On December 29, 2003 Type Certificate 229--200 was issued.

On August 17, 2004 Supplement to Type Certificate 220--200/1 was issued, allowing the international airroute operations.

On January 31, 2007 Supplement to Type Certificate 229--200/-02 was issued, allowing the aircraft passenger version operation.

On May 25, 2010, a supplement to Type Certificate 229--200/03 for Be-200ES- aircraft equipped with "English cockpit" was received.

On September 7, 2010, a Type Certificate EASA.IM.A.114 for Be-200ES- aircraft was awarded by European Aviation Safety Agency.

Currently, activities related to the contract with the Ministry of Emergency Situations of Russia associated with delivery of seven Be-200ES aircraft are being conducted. The first serial Be-200ES amphibian took off on its maiden flight from the aerodrome in Irkutsk on June 17, 2003 and was handed over to the aviation group of the Russian Ministry for Emergency Situations.

One Be-200ES aircraft was delivered to foreign customer in Azerbaijan in 2008.

In 2010, Beriev Aircraft Company and Ministry of Emergency Situations of Russia signed a pre-contract agreement related to delivery of eight Be-200ES aircraft.




Aircraft Performance
OVERALL DIMENSIONS
Wing span, m
32.78
Aircraft lenght, m
32.05
Aircraft height, m
8.9
Wing area, m2
117.4
Wheelbase, m
11.143
Track, m
4.3
Cargo compartment:
    - Lenght, m
18.7
    - Height, m
1,895
    - Maximum width, m
2.5
    - Floor area, m2
41
    - Volume, m3
80.8
WEIGHTS
Operational empty weight, kg
27.6
Maximum take-off weight:
     - from ground, kg
41000
     - from water, kg
38000
Maximum landing weight:
     - from ground, kg
41000
     - from water, kg
38000
Maximum fuel capacity, kg
12500
Maximum take-off weight after water scooping during hydroplaning, kg

43000
PERFORMANCE
Maximum cruise speed (ISA, 8,000 m), km/h
700
Economic cruise speed (ISA, 8,000 m), km/h
560
Operational altitude, m
8,000
Maximum range (ISA, 8,000 m, 1 hour fuel reserve), km/h
3,300
Take-off distance (ISA, sea level):
     - from ground, m
1,270
     - from water, m
1,000
Landing distance (ISA, sea level):
     - on ground, m
1,020
     - on water, m
1,300
Seaworthiness:
     - Sea state
3
     - Wave height, m
1.2
Minimum depth of water for optrations, m
2.6
FIRE FIGHTING
Water tanks maximum capacity, m3
12
Chemical retardant tanks capacity, m3
1.2
Rate of climb after water scooping (43 t, sea level), m/s
9.5
Speed during water scooping at hydroplaning, km/h
150-190
Time required for water scooping during hydroplaning, sec
14
Minimum speed of water dropping, km/h
200-250
Minimum altitude for water dropping, m
50
SEARCH&RESCUE MISSIONS ON WATER,
AIR AMBULANCE
Patrol altitude, m
100-8,000
Patrol speed, km/h
300-560
Survivors:
     - Arrangement on folding seats
64
     - Arrangement on stretches
30
Flight range with 64 survives onboard
(8,000, 1 hour fuel reserve), km

1,850
Patrolling time, h
up to 6.5
FREIGHT
Payload, kg
7,500
Range (8,000 m, 1 hour fuel reserve), km
1,000
Cargo door dimensions, mm
2,050X1,760
Cargo pallets, type PA 1.5, pcs
up to 9
Cargo containers, type LD3
up to 7



General View of Aircraft




Photo of the Be-200ES passenger cabin (click to view)



Photo of the Be-200ES cockpit


 
[  Home  |  Introduction  |  Aircraft  |  Photos  |  Press-releases  |  Links  |  Contact Us  ]
Copyright Beriev Aircraft Company.