
Aircraft Turbocharged Fuel System
The Aircraft Turbocharged Fuel System Trainer RA-AF-53 is equipped with a complete Fuel flow assembly to simulate fuel flow installed in an aircraft turbocharged engine including plumbed fuel lines using both fixed and flexible fuel lines which are played from the fuel tank to fuel strainer, fuel pump, fuel control unit, turbocharger to fuel injector. Fuel flow instruments and indicators allow students and users to check fuel system conditions during operations.
Features
A compact, portable, and ready to operate unit to demonstrate the operations of aircraft turbocharged fuel system.
Perform Operation, servicing, and maintenance of the fuel injection system including fuel plumbing.
Equipped with 2 (two) fuel pressure measurements to compare the fuel pressure before and after the turbocharger.
Instructor / User manual including student Lab. Practice.
Include interactive CBT
Components & Specifications
Combustion Chamber, engine-drive fuel pump.
Fuel tank, fuel boost pump, fuel filter, fuel pump
Fuel control assembly, fuel manifold, fuel injector
Turbocharger
Plumbed fuel lines using both fixed and flexible
Control Panel including switches, circuit breakers, and indicators
Fuel Pressure Gauge
Fuel Pressure transmitter and Indicator
Fuel Flow transmitter and Indicator {Optional)
Training Stand with caster wheel and brakes
Requirements
220-240 VAC/50 Hz.
Dimensions L x W x H (mm): 1,651 x 483 x 1,900
