Engine Fuel Systems Flashcards
- During what period does the fuel pump bypass valve open and remain open?
a. When the fuel pump pressure is greater than the demand of the engine.
b. When the boost pump pressure is greater than the fuel pump pressure.
c. When the fuel pump output is greater than the demand of the carburetor.
b.
- Which of the following statements concerning a centrifugal-type fuel boost pump located in a fuel supply tank is NOT true?
a. Air and fuel vapors do not pass through a centrifugal-type pump.
b. Fuel can be drawn through the impeller section of the pump when it is not in operation.
c. The centrifugal-type pump is classified as a positive displacement pump.
c.
- Where is the engine fuel shutoff valve usually located?
a. Aft of the firewall.
b. Adjacent to the fuel pump.
c. Downstream of the engine-driven fuel pump.
a.
- Boost pumps in a fuel system
a. operate during takeoff only.
b. are primarily used for fuel transfer.
c. provide a positive flow of fuel to the engine pump.
c.
- What is the purpose of an engine-driven fuel pump bypass valve?
a. To divert the excess fuel back to the main tank.
b. To prevent a damaged or inoperative pump from blocking the fuel flow of another pump in series with it.
c. To divert the excess fuel from the pressure side of the pump to the inlet side of the pump.
b.
- Most large aircraft reciprocating engines are equipped with which of the following types of engine-driven fuel pumps?
a. Rotary-vane-type fuel pump.
b. Centrifugal-type fuel pump.
c. Gear-type fuel pump.
a.
- When an electric primer is used, fuel pressure is built up by the
a. internal pump in the primer solenoid.
b. suction at the main discharge nozzle.
c. booster pump.
c.
- The fuel pump relief valve directs excess fuel to the
a. fuel tank return line.
b. inlet side of the fuel pump.
c. inlet side of the fuel strainer.
b.
- Which type of pump is commonly used as a fuel pump on reciprocating engines?
a. Gear.
b. Impeller.
c. Vane.
c.
- The purpose of the diaphragm in most vane-type fuel pumps is to
a. maintain fuel pressure below atmospheric pressure.
b. equalize fuel pressure at all speeds.
c. compensate fuel pressures to altitude changes.
c.
- The primary condition(s) that allow(s) microorganisms to grow in the fuel in aircraft fuel tanks is (are)
a. warm temperatures and frequent fueling.
b. the presence of water.
c. the presence of dirt or other particulate contaminants.
b.
- It is desirable that fuel lines have a gentle slope upward or downward and not have sharp curves or sharp rises and/or falls in order to
a. prevent vapor lock.
b. prevent stagnation or ‘pooling’ of fuel in the fuel lines.
c. minimize the generation of static electricity by decreasing fluid friction the lines.
a.
- The fuel systems of aircraft certificated in the standard classification must include which of the following?
a. An engine-driven fuel pump and at least one auxiliary pump per engine.
b. A positive means of shutting off the fuel to all engines.
c. A reserve supply of fuel, available to the engine only after selection by the flightcrew, sufficient to operate the engines at least 30 minutes at METO power.
b.
- Where should the main fuel strainer be located in the aircraft fuel system?
a. Downstream from the wobble pump check valve.
b. At the lowest point in the fuel system.
c. At any point in the system lower than the carburetor strainer.
b.
- Where physical separation of the fuel lines from electrical wiring or conduit is impracticable, locate the fuel line
a. below the wiring and clamp the line securely to the airframe structure.
b. above the wiring and clamp the line securely to the airframe structure.
c. inboard of the wiring and clamp both securely to the airframe structure.
a.