Be-103

Initial Operational Capability (IOC) : December 2001
First Flight : July 1997
Total Production : ?

Model Status Year Produced
Be-103 Active 2001 ?



Be-103

Group : Turboprop Airplanes
Status : Active
Origin : Russia
Contractors : Beriev, KnAAPO
Initial Operational Capability (IOC) : December 2001
First Flight : July 1997
Total Production : ?

The Beriev Be-103 is a light, amphibious, twin-engine, multi-purpose turboprop airplane designed to carry cargo and passengers, provide urgent medical aid, assist in firefighting, and environmental control of bodies of water. The aircraft can takeoff and landing based on both ground and water. Powered by two TCM-IO-360ES4 piston engines each rated at 210-hp and driving a three-blade propeller, the Be-103 is capable of flying at 3,000 meters of altitude and 210 kph on routes of 1,000 kilometers carrying up to five passengers or 368 kg of cargo. The airplane is being manufactured at KnAAPO aviation plant, Russia, which belongs to the Sukhoi aviation holding.

The Be-103 amphibious aircraft can operate with sea state 2 and wage heights of up to 0.5 meters at shallow waters of at least 1.25 meters of depth. With such characteristics the aircraft is suitable for operations at lake, rivers, water reservoirs and seas. Moreover, the Be-103 has been fitted with modern navigation and communication systems allowing flights at night and in adverse weather conditions. A weather radar is available as optional equipment.

So far, the Be-103 aircraft type has been certified in Russia (AP-23 standard December 2001), Europe, the United States (FAR-23 July 2003), Brazil (August 2005), China (December 2005) and is planned for certification in Canada. Beriev TANTK engineering company expects to sell many aircraft in the Latin America region following the Brazilian certification. As of September 2005, US-based customers had taken delivery of three Be-103s.

Operators
Country Status State Notes
ChinaActive 20
IndonesiaActive 8
RussiaActive ?
United States of AmericaActive ?
Specifications
Notes
Crew 2
Number of Engines 2
Passengers 5
Area
Wing Area 25.1 square meter
Dimensions
Cabin Height 1.2 meter
Cabin Length 3.4 meter
Cabin Width 1.3 meter
Height 3.8 meter
Length 10.7 meter
Wingspan 12.7 meter
Mass
Empty Weight 1,834 kilogram
Fuel Load 245 kilogram
Max Landing Weight 2,270 kilogram
Max Takeoff Weight 2,270 kilogram at takeoff
Operational Weight 1,902 kilogram
Payload 368 kilogram
Performance
Ceiling 5,020 meter
Landing Run Distance 400 meter on ground or 360 meters on water
Max Range 1,070 kilometer
Operational Altitude 3,000 meter
Take Off Run Distance 350 meter on ground or 560 meters on water
Power
Max Power at TakeOff 420 hp
Speed
Cruise Speed 210 kph
Top Speed at High Altitude 240 kph

News

Tuesday, 23 January, 2007
China Orders Six Be-103 Amphibious Aircraft

The signing of a contract to deliver six Be-103 amphibian aircraft to took place on 21 January this year.

Friday, 24 November, 2006
KnAAPO has preliminary requests for supply of over 100 new Su-80s to Russian and foreign companies

KnAAPO (Komsomolsk-na-Amure Aircraft Production Association) comprised by the Sukhoi Holding, is compiling a book of orders for a new Su-80 multi-role aircraft, Sergey Drobyshev,

Photo Gallery

Notes

* Prime Contractor
State Latest Known holdings/Original Procurement
Com - Date of Commissioning
Decom - Date of Decommissioning

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