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AIRCRAFT ENGINEERING AND MAINTENANCE<br />

EQUIPMENT, KITS<br />

AND AGGREGATES<br />

DCN42<br />

ENGINE DRIVEN CENTRIFUGAL PUMP<br />

It is a fuel system booster pump. The engine driven<br />

centrifugal pump consists of the screw pump, impeller<br />

pump, shaft seal unit.<br />

DF42<br />

AFTERBURNER FUEL METERING DEVISE<br />

It is designed for fuel dispensing into afterburner ducts of AI-<br />

222K-25F turbojet engine by input commands from engine<br />

control system.<br />

EMA-750, 100<br />

ELECTROMECHANICAL ACTUATORS<br />

Designed for linear movement of mechanisms’ executive<br />

elements. Electromechanical actuator consists of valve<br />

electro-motor and gearbox.<br />

EMP3<br />

ELECTROMECHANICAL ACTUATOR<br />

Designed for linear movement of mechanisms’ executive<br />

elements. Electromechanical actuator consists of valve<br />

electro-motor and gearbox.<br />

ENA15<br />

INDEPENDENT FLIGHT CONTROL ACTUATOR<br />

EHA 15 is used for<br />

civil aircraft rudder<br />

actuation by input<br />

control signal from<br />

the flight control<br />

system.<br />

KV-38<br />

CAT-IN VALVE<br />

It is designed to control the working fluid flow to the actuator<br />

by pressure connection under the edge of the pilot distribution<br />

spool. Application: AN-38, AN-140<br />

115

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