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Be-12 Chayka (Mail) Russian Amphibious Aircraft

Amphibious Aircraft
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Basic Information
Name
Be-12 Chayka (Mail) Russian Amphibious Aircraft
Designation
Alternate Designation
Equipment Type
Amphibious Aircraft
Manufacturer
Beriev OKB (design bureau), Taganrog, Russia
Date of Introduction
1968
Description

Be-12 Chayka (Mail) Russian Amphibious Aircraft is a Soviet turboprop-powered amphibious aircraft designed for anti-submarine and maritime patrol duties. The Beriev Be-12 was a successor to the Beriev Be-6 flying boat, whose primary roles were as an anti-submarine and maritime patrol bomber aircraft. Though tracing its origins to the Be-6, the Be-12 inherited little more than the gull wing and twin oval tailfin configuration of the older aircraft. The Be-12 has turboprop engines, which gave it an improved speed and range over the Be-6. The Be-12 also had retractable landing gear, which enabled it to land on normal land runways, as well as water. The Be-12 was first flown on October 18, 1960, at Taganrog airfield, and made its first public appearance at the 1961 Soviet Aviation Day festivities at Tushino airfield. A total of 150 aircraft were produced, in several variations, with production ending in 1973. The Be-12 was "something old, something new, something borrowed", incorporating lessons learned on earlier Beriev flying boats, with a number of innovations incorporated. It was of all-metal construction, with a high-mounted gull wing, twin tailfins, and tricycle landing gear -- all with single wheels, the main gear pivoting upwards over the boat hull into the sides, the tailwheel pivoting backward up into the end of the aircraft. It featured fixed floats, a sea rudder at the end of the boat hull, and strakes alongside the nose to deflect seaspray. Trials with the first prototype demonstrated that seawater impacts tended to "ding" the propellers, so the second set of strakes was added lower on the fuselage under the cockpit after initial trials; the prototype's engines had also been underneath the wings, but they were relocated to the top for all following aircraft, for the same reason.

Air & Air Defense Specifications
Crew 6
Engine Turboprop (4190 hp)
Max Speed 610.0 km/h
Cruise Speed 320.0 km/h
Endurance 15.00 hrs
Variants
Be-12 Twin-engined maritime reconnaissance, anti-submarine warfare flying-boat. 2 prototypes and 130 production airframes built.
Be-12EKO Projected ecological reconnaissance version. Not built.
Be-12I Projected scientific research version designed in 1991. Not built.
Be-12LL Conversion for testing the 3M-80 'Moskit' anti-shipping missile. Nose radar replaced with missile seeker head. One aircraft converted in 1980.
Be-12N ASW version fitted with new sensors, avionics, MAD sensor and Nartsiss search/attack system. 27 aircraft converted.
Be-12Nkh Utility transport, experimental passenger transport version. Military equipment removed, additional windows fitted. 2 built, both converted from Be-12.
Be-12P Firefighting version. One 4,500 l tank and two 750 l tanks installed. Four aircraft converted in 1992.
Be-12P-200 Technology demonstrator for the Beriev Be-200. Fire-fighting configuration. One aircraft converted.
Be-12PS Maritime Search and rescue version. Life rafts and survival equipment carried. 6 crew. 10 built new, 4 converted from Be-12.
Be-12SK One aircraft converted in 1961 for use in SK-1 nuclear depth charge tests.
Be-14 All weather, day/night SAR version. Additional SAR and medical equipment. 6 crew. AI-20D engines. One built.
M-12 Stripped-down Be-12 used for record-setting flights. 2 Crew. Later returned to standard configuration.
System
Alternate Designation(s) Be-12 Chayka; NATO: Mail
Type Amphibious Aircraft
Manufacturer Beriev OKB (design bureau), Taganrog, Russia
Crew 6-10 (5 flight crew, 1-5 mission crew)
Number of Engines 2 ea
Number of Hard Points Underwing Pylons: 4 x ASW torpedoes
Normal Payload Capacity 5,000 kg
Maximum Payload Capacity 10,000 kg
Dimensions
Length 30.17 m
Height 7.00 m
Width (Wing Span) 29.71 m
Wing Area 105 sq m
Empty Weight 18,000 kg
Maximum Takeoff Weight 31,000 kg
Normal Payload Capacity 5,000 kg
Maximum Payload Capacity 10,000 kg
Automotive
Engine Name 2 x Ivchenko AI-20D
Engine Type Turboprop
Engine Power 4,190 shaft hp each
Internal Fuel Capacity 11,000 liters
Maximum Speed 610 km/h
Cruise Speed 320 km/h
Normal Patrol Radius 371 km
Maximum Patrol Range 4,000 km
Maximum Ferry Range 7,500 km
Climb Rate 912 m per minute
Ceiling 11,280 m
Endurance 15 hours
Main Weapon System
Internal Bay depth bombs and mines
Underwing Pylons 4 x ASW torpedoes
Radar Systems
Surface / Search Radar 1 x A304 surface search radar in nose radome
Protection
Stealth Properties None
Heat Signature Reduction No
Add on Armor INA
EW Counter Measures INA
Chaffs/Flares INA
Details
Country of Origin Russia
Category Maritime Patrol
Air > Maritime Patrol
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
30.17 m
Width
29.71 m
Height
7 m
Weight
31000 kg
Operators (5)
Russia
Ukraine
Egypt
Syria
Vietnam
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