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Be-200ES

Be-200ES

Passenger Regional Jets
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Basic Information
Name
Be-200ES
Designation
Be-200ES
Alternate Designation
Be-200ChS (firefighting), Be-200PS (without firefighting equipment), Be-210 (passenger variant)
Equipment Type
Passenger Regional Jets
Manufacturer
Beriev, IRKUT Corporation
Date of Introduction
2001
Description

The Beriev Be-200 is a variant of the A-40/Be-42 aircraft which first flew on September, 24, 1998. The aircraft was awarded type certification in August 2001. The amphibious airplane is capable of search and rescue (SAR), transportation of passengers and freight, ambulance, and maritime surveillance applications highlighting the firefighting role. In the firefighting role, the Be-200 can airdrop up to 12 tons of water in just 17 seconds. The Be-200 retains the basic characteristics from A-40/Be-42 except the fuselage size which was reduced to make the aircraft smaller and the powerplants which have been replaced by more powerful Ivchenko-Progress D-436TP turbofan engines. The Be-210 is a version of Be-200 intended to transport up to 72 passengers in the its fully pressurized cabin on routes of up to 1,850 km. The Be-200ES is a fully multipurpose amphibious aircraft version of Be-200 and features enhanced performance and increased maximum takeoff weight. It was awarded type certification in June 2003. The Be-200ES is certified for at sea operations with sea state 3, at least 2.6 meters depth, and waves of up to 1.3 meters tall. Currently, Be-200ES is the production standard for the Be-200 aircraft. In August 2005 EADS purchased 10% share on Irkut - the Be-200 manufacturer - and boosted the Be-200 program through close cooperation between EADS and Irkut on marketing and international type certification. As of 2005, Be-200 was being operated by Russian Ministry of Disaster Relief and the Italian Protezione Civile authorities.

Air & Air Defense Specifications
Max Speed 700.0 km/h
Range 3300.0 km
Wingspan 32.80 m
Overview (Deagel)
Group Passenger Regional Jets
Status Active
Also Known As Be-200ChS (firefighting), Be-200PS (without firefighting equipment), Be-210 (passenger variant)
Origin Russia
Contractors Beriev, IRKUT Corporation
Initial Operational Capability (IOC) August 2001
First Flight September 24, 1998
Total Production ?
Unitary Cost RUB 1.0 billion
Specifications (Deagel)
Number of Engines 2
Passengers 72
Area — Wing Area 117 square meter
Dimensions — Cargo Compartment Height 1.9 meter
Dimensions — Cargo Compartment Length 18.7 meter
Dimensions — Cargo Compartment Width 2.5 meter
Dimensions — Height 8.9 meter
Dimensions — Length 32.1 meter
Dimensions — Wingspan 32.8 meter
Mass — Fuel Load 12,500 kilogram
Mass — Max Landing Weight 41,000 kilogram
Mass — Max Takeoff Thrust 33,730 pound
Mass — Max Takeoff Weight 41,000 kilogram
Mass — Operational Weight 27,600 kilogram
Mass — Payload 7,500 kilogram
Performance — Landing Run Distance 1,020 meter
Performance — Max Range 3,300 kilometer
Performance — Operational Altitude 8,000 meter
Performance — Take Off Run Distance 1,270 meter
Speed — Climb Rate 9.5 mps
Speed — Cruise Speed 560 kph
Speed — Top Speed at High Altitude 700 kph
Volume — Payload Capacity 80.8 liter
Gear (Deagel)
Item 1 Turbofan Engines: D-436TP (2)
Item 2 Turbofan Engines: PD-8 (2)
Item 3 Turbofan Engines: SaM146 (2)
Variants
Variant 1 A-40
Variant 2 Be-200ES
Details
Country of Origin Russia
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
32.1 m
Width
32.8 m
Height
8.9 m
Weight
41000 kg
Operators (7)
Russia
China
United States
Italy
Azerbaijan
Chile
Venezuela
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