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Multipurpous amphibious aircraft for the Russian Ministry for Emergency Situations is
intended for:
- firefighting,
- renering urgent help in creatical areas of emergency,
- search&rescue missions in the sea,
- ambulance missions,
- freight.
The Be-200ES amphibian is equipped with two bypass jet engines, type D-436TP, 7650 kg
take-off thrust each (Motor Sich, Ukraine).
On June 20, 2003 the aircraft obtained the type certificate for restricted category aircraft
¹ ÑÒÎÊ 220-Áå-200×Ñ.
On December 29, 2003 the type certificate
¹ ÑÒ229-Áå-200×Ñ was obtained too.
Be-200 amphibious aircraft got the addition to the Russian type certificate ¹ÑÒOK220-Áå-200×Ñ/DO1, allowing the international airlines operation.
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
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