Phase III Block II Flashcards
(30 cards)
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
There are three tanks on the C-40. Main tank #1 is in the wing box of the left-wing. Main tank #2 is in the wing box of the right wing. The center tank is in the fuselage and the left and right wing root.
There are three tanks on the C-40. Main tank #1 is in the wing box of the left-wing. Main tank #2 is in the wing box of the right wing. The center tank is in the fuselage and the left and right wing root.
The vent tanks are located outboard of each wing. The fuel vent system keeps the pressure of the fuel tanks near the ambient pressure.
The vent tanks are located outboard of each wing. The fuel vent system keeps the pressure of the fuel tanks near the ambient pressure.
There are two center tank boost pumps that are located on the rear spar. Access to the center tank boost pumps is through the wheel wells.
There are two center tank boost pumps that are located on the rear spar. Access to the center tank boost pumps is through the wheel wells.
There are forward and aft boost pumps in main tank number one and number two. The forward boost pumps are on the front spar, the aft boost pumps are on the rear spar.
There are forward and aft boost pumps in main tank number one and number two. The forward boost pumps are on the front spar, the aft boost pumps are on the rear spar.
Access to the Fwd boost pumps is through extended Krueger Flaps. Access to the aft boost pumps is through the wheel wells.
Access to the Fwd boost pumps is through extended Krueger Flaps. Access to the aft boost pumps is through the wheel wells.
The APU DC boost pump supplies fuel to the APU.
The APU DC boost pump supplies fuel to the APU.
The APU DC boost pump has a pump assembly and a housing assembly. The housing assembly is inside the fuel tank. The pump assembly attaches to the outside of the fuel tank.
The APU DC boost pump has a pump assembly and a housing assembly. The housing assembly is inside the fuel tank. The pump assembly attaches to the outside of the fuel tank.
The APU DC boost pump is on the left wing rear spar.
The APU DC boost pump is on the left wing rear spar.
The pressure fueling system allows refueling of all tanks and may also be used during fuel transfer from tank to tank.
The pressure fueling system allows refueling of all tanks and may also be used during fuel transfer from tank to tank.
