Phase III Block II Flashcards
Always perform FOD walk down in front of and around engine ingestion area prior to engine start.
Always perform FOD walk down in front of and around engine ingestion area prior to engine start.
Do not use the entry/exit corridor when the engine is in operation.
Do not use the entry/exit corridor when the engine is in operation.
Stay out of the inlet and exhaust areas when the engine is in operation.
Stay out of the inlet and exhaust areas when the engine is in operation.
The beacon light must be in while the engines are operating.
The beacon light must be in while the engines are operating.
If the wind is over 25 knots, increase the inlet hazard area by 20 percent.
If the wind is over 25 knots, increase the inlet hazard area by 20 percent.
For additional safety, wear a safety harness when the engine is in operation.
For additional safety, wear a safety harness when the engine is in operation.
Ensure engine turn screens are installed during maintenance turns.
Ensure engine turn screens are installed during maintenance turns.
The fan is located at the front of the engine downstream from the air inlet Cowl.
The fan is located at the front of the engine downstream from the air inlet Cowl.
The fan increases the speed of the air to generate thrust; it also increases the pressure of the air directed to the compressor.
The fan increases the speed of the air to generate thrust; it also increases the pressure of the air directed to the compressor.
The high-pressure compressor increases the pressure of the air from the low pressure compressor and send it to the combustor.
The high-pressure compressor increases the pressure of the air from the low pressure compressor and send it to the combustor.
The primary function of the combustion section is to burn the fuel-air mixture, thereby adding heat energy to the air.
The primary function of the combustion section is to burn the fuel-air mixture, thereby adding heat energy to the air.
The high-pressure turbine is a single stage turbine. It provides the necessary power to drive the compressor rotors.
The high-pressure turbine is a single stage turbine. It provides the necessary power to drive the compressor rotors.
The low pressure turbine is a four stage turbine. It changes the energy of the hot gases into a mechanical energy to drive the fan and booster rotar.
The low pressure turbine is a four stage turbine. It changes the energy of the hot gases into a mechanical energy to drive the fan and booster rotar.
The accessory drive extracts part of the core engine power and transmits it through a series of gearboxes and shafts in order to drive the engine and aircraft accessories.
The accessory drive extracts part of the core engine power and transmits it through a series of gearboxes and shafts in order to drive the engine and aircraft accessories.
The accessory drive consist of these components:
Inlet gear box Radial drive shaft Transfer gear box Horizontal drive shaft Accessory gear box
The accessory drive consist of these components:
Inlet gear box Radial drive shaft Transfer gear box Horizontal drive shaft Accessory gear box