GENERAL   EQUIPMENT   INC.                    

 

8724 Sunset Drive #191 ● Miami FL 33173 · USA                                  

                                                  
Email: info@generalequipment.info ● www.generalequipment.info                                                       

 

 

 

AMPHIBIOUS BE-103

 

 

TYPE:

Aircraft

DESCRIPTION:

Amphibious Plane Be-103

PRICE:

Upon Request

PACKING:

Ex-works

 

 

AMPHIBIOUS PLANE BE-103

 

 

 

 

 

 

 

Performance

 

Service ceiling 17000 ft (5200 m)
Maximum cruising speed at H=3000m 135 kts (250 km/h)
Economy speed at H=9800ft (3000m) 120 kts (220 km/h)
Maximum range (H=9800ft (3000m), 0.5 hour fuel reserve) 713 nm (1321 km)
Flight endurance (H=9800ft (3000 m), 0.5 hour fuel reserve) 6 h
Fuel consumption 14-16 g/h (38-43 kg/h)
Take-off run (SL, ISA) (water/ground) 1804/1017 ft (550/310 m)
Landing roll (SL, ISA) (water/ground) 984/1280 ft (300/390 m)
Seaworthiness, sea state 2 (1.64 ft (0.5 m) wave height)
 

Weights

Max take-off weight 5004 lbs (2270 kg)
Empty weight 3704 lbs (1680 kg)
Payload 849 lbs (385 kg)
Maximum fuel capacity 540 lbs (245 kg)

Dimensions

Length 34.94 ft (10.65 m)
Wing span 41.73 ft (12.72 m)
Overall height at rest 12.33 ft (3.757 m)
Wing area 270.18 sq.ft (25.1 sq.m)
Propeller diameter 6 ft (1.83 m)
Wheel track 7.46 ft (2.273 m)
Wheelbase 13.51 ft (4.118 m)

Cabin internal dimensions

Length 12 ft (3.65 m)
Height 4.035 ft (1.23 m)
Width 4.1 ft (1.25 m)
Luggage compartment volume 28.2528 cub.ft (0.8 cub.m)
Crew 1 (pilot)
Passengers 5

 

 

Be-103 is a light multipurpose twin-engine amphibious aircraft, intended for:

 

  • business and passenger transportation;
  • tourism and recreation;
  • coastal and maritime patrol;
  • ecological monitoring of waterways;
  • maritime search and rescue;
  • rendering urgent medical aid;
  • fishery reconnaissance;
  • forestry monitoring and fire patrol.
Click to enlarge

The Be-103 light multipurpose amphibious aircraft is a monoplane with low-set water-displacement wing with a root strake, all-moving horizontal tail located in the propeller blow zone, and tricycle landing gear.

A unique feature of the amphibious aircraft includes implementation of a water-displacement wing concept, which improves seaworthiness and stability when moving on water. Power plants are two IO-360ES4 piston engines made by Teledyne Continental Motors (USA) each rated at 210 h.p. The engines are mounted on horizontal pylons on both sides of the hull above the rear part of the center wing section, providing protection to the propellers against water spray during take-off and landing on water. The aircraft is fitted with MTV-12-D-C-F-R (M) variable-pitch three-blade reversible propellers.

The low-set wing (in relation to hull) provides for wing-in-ground effect during take-off and landing. Thanks to this feature the aircraft does not need flaps and can skim on the wing trailing edges. This also makes aircraft construction simpler.

The hull is wide enough to provide a comfortable cabin for passengers and sufficient space for cargo and luggage.

There are a total of 6 seats (1 pilot/5 passenger).

When in basic configuration, the aircraft is fitted with flight/navigation equipment for Visual Flight Rules (VFR). At customer's option, the aircraft may be fitted with flight/navigation equipment for Instrument Flight Rules (IFR). The aircraft meets Russian Air Regulations AĻ-23 and FAA (FAR 23) requirements.

 

 

 

 

Specification and photos are not contractual and are subject to verification upon inspection

 

NB: Aircraft offered for sale subject to contract, prior sale, withdrawal from the market and information regarding any aircraft or helicopter and provided verbally or in written documentation and/or contained within this email or associated paper-work should be taken as a guide only in determining the suitability, including that aircraft or helicopters specification and/or performance.  We highly recommend that any buyer or lessee perform their own inspections and due diligence to verify any and all technical, performance and specification information contained therein including OEM claims.

 

PLEASE NOTE: AIRCRAFT SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION. WE DO NOT ACCEPT ANY LIABILITY FOR AIRCRAFT DEFECTS, HISTORY OR TECHNICAL RECORD ERRORS. IT IS THE BUYERS RESPONSIBILITY TO INDEPENDENTLY VERIFY THE AIRCRAFT AND COMPONENT HISTORY.

 

 

 

TAKE NOTICE!

 

PLEASE BE ADVISED THAT INFORMATION INCLUDED IS CONFIDENTIAL IN NATURE AND IS BASED ON PRE-EXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION THE RECEIVER ACKNOWLEDGES THAT ANY UNAUTHORIZED CONTACT WITH SAID LEGAL SELLER WILL BE CHARACTERIZED AS A BREACH OF CONFIDENTIALITY AND SAID AGREEMENT MAY BE ENFORCED UNDER EXISTING LAW OR IN EQUITY.

 

This paper was prepared by General Equipment Inc.
The paper represents an offer of a partner of General Equipment Inc.
All rights are reserved by and for General Equipment Inc.
All content and ideas of this paper are the property of General Equipment Inc.