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Questions and Answers
How many MLIs are present in each INNER tank?
What should be done to check the total fuel quantity on the aircraft?
What is indicated by the G7508471 - G7UT0TU - FM28B1000000003 code?
Which function must be used to access roll and pitch data from the ADIRU?
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To determine the volume of fuel for odd-numbered MLIs, what method is used?
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What type of correction may be applied to the INNER tank volume?
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What is the correct procedure to use the MLI for checking fuel levels?
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What is the attitude reading for the RIGHT wing MLI number - 6?
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What action does the FCMC take when an inner tank low level sensor becomes dry?
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At what low level quantity does the inner tank trigger the FCMC action?
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From where do the FCMCs receive fuel data?
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What information do both FCMCs also receive besides fuel data?
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What environmental factors do the Air Data and Inertial Reference Units (ADIRUs) provide to the FCMC?
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What is not directly monitored by the FCMCs?
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Which aircraft models are mentioned in the context of FCMC operations?
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What is the primary purpose of the FCMC in relation to fuel management?
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What is the main function of the COM and MON processors in each FCMC?
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How do the COM and MON processors determine the usable fuel quantity?
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What role does the independent level sensing board in each FCMC play?
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What data is accessed through the FUEL QUANTITIES menu?
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What is the significance of the FCMC's cross-wired discretes?
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Which parameter is NOT included in the INPUT PARAMETERS menu?
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What additional functions does each FCMC provide apart from measuring fuel quantity?
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In what way do COM and MON processors differ in function?
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What action does the FCMC take when the center tank low level sensor is dry?
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What is the function of the overflow sensor in the fuel system?
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Which of the following sensors is NOT explicitly mentioned in connection with the fuel level sensing?
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What happens when the trim tank low level sensor indicates a dry condition?
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When does the FCMC trigger an ECAM warning?
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Which of the following describes the purpose of the ETOPS sensors?
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What does the FCMC do when the overflow sensor becomes wet during refueling?
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Which component is responsible for managing the transfer of fuel from the center tank?
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What systems are included in the fuel tank indicating systems?
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What do the Fuel Control and Monitoring Computers (FCMCs) do with the data they receive?
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Which aircraft models are referenced in the context of fuel tank venting?
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What is the purpose of the fuel tank venting systems?
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When was the fuel tank venting document last revised?
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Which component does NOT play a role in the fuel tank indicating systems?
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What function does the ECAM FUEL page serve in the context of fuel management?
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Which of the following statements regarding the refuel/defuel control panel is true?
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What activates the APU pump in the event of low pressure in the trim transfer line?
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Which component closes in response to an APU fire detection?
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What is the function of the fuel/air separator in the fuel transfer line?
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What does the main transfer system primarily control?
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What power sources can automatic refueling utilize?
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How does the APU fuel isolation valve operate?
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What is a significant role of the FCMC in managing fuel?
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What does the fuel isolation valve primarily do?
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Which function is NOT performed by the fuel system?
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What is the minimum tank content required for gravity purging in the trim tank?
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Which tool is specifically mentioned for operating the drain valves?
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How many drain valves are located in each wing tank?
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What should you verify after draining the water from the drain valves?
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What is the recommended procedure if the drain valve leaks?
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What is the reason for waiting one hour after refueling before draining water from the tanks?
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What is one of the environmental precautions mentioned regarding waste fluids?
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What is the purpose of the THS adjustment to 0° trim during drain procedures?
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What action can be taken if the refuel isolation valve solenoid fails during refueling?
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In the event of a crossfeed valve failure, what is the protocol according to the MEL/deactivation procedures?
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What is the main consequence of a failure in the electrical control of the refuel isolation valve solenoid?
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What type of valve is specifically mentioned in relation to the fuel line maintenance briefing?
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Which component failure requires manual intervention during the refueling process?
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What energizes the refuel isolation valve solenoid during the refueling process?
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Which of the following statements accurately describes an action taken during refueling if a valve failure occurs?
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What is the function of the solenoid in the refuel isolation valve system?
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What is the appropriate action when there is a crossfeed valve failure during normal operations?
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During routine checks, what is essential for daily maintenance of the fuel system?
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What is the purpose of the MEL in the context of a valve failure?
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What is indicated by the presence of water in the fuel system?
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What procedure must be followed if the aircraft is in Extended Range operations and experiences a crossfeed valve failure?
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What could potentially happen if regular checks for water content in the fuel are overlooked?
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Which of the following statements is true regarding the closed position of a crossfeed valve?
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Why is environmental precaution important during daily fuel checks?
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What is the primary function of the FQI probes in the fuel tanks?
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Which statement about the compensators in the fuel system is correct?
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What is the role of the densitometers in the fuel management system?
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How do FCMCs utilize the capacitance values from the FQI probes?
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What distinguishes the A330-200 configuration of the fuel system?
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What is the electrical property measured by the FQI probes?
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In what condition do the fuel compensators provide accurate readings?
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What does the FCMCs use the data from the densitometers for?
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Study Notes
Fuel Quantity Indicating (FQI) System
- FQI probes are used to measure fuel quantity
- The FQI system uses an indicator rod to determine wing volume during fuel quantity checks.
- The most outboard MLI indicates fuel in the tank.
Fuel Level Sensors
- Fuel level sensors in each wing tank are used to indicate fuel quantity.
- Each FCMC has a maximum of 14 level-sensing channels that are connected to the FCMCs, with one connected to FCMC 1 and the other to FCMC 2.
- The FCMC uses level-sensing data from these channels, along with other factors, for fuel quantity calculation.
Attitude
- The aircraft attitude determines which fuel table is used for calculating fuel quantity.
- The ADIRU determines aircraft attitude, which is derived from Air Data Inertial Reference Units (ADIRU) using the ALPHA call-up function in the ACMS.
Fuel Control and Monitoring Computers (FCMCs)
- FCMCs receive fuel level sensing data from FQI probes.
- FCMCs receive flight data on THS position from Flight Control Data Concentrators (FCDCs) and roll and pitch data from Air Data and Inertial Reference Units (ADIRUs).
- They compute fuel quantity and temperature and transmit the information to the ECAM FUEL page and refuel panel indicator.
Fuel Quantity Calculation
- FCMC uses fuel level data from fuel probes, fuel permittivity, and density to calculate fuel mass.
- FQI measurements are used to monitor usable fuel in the tank.
- The FCMC monitors fuel level data and activates warnings based on the data.
- Fuel quantity data from opposite FCMCs is received by cross-wired discretes.
Fuel Tank Venting
- Center and wing tank venting is controlled by an FCMC.
- The FCMC closes the trim tank isolation valve when detecting low levels.
- The FCMC closes all inlet valves, the refuel isolation valve, and triggers an ECAM warning when an overflow sensor becomes wet.
- When any inner tank low level sensor is dry, the FCMC stops the jettison operation.
- When the center tank low level sensor is dry, the FCMC stops the center tank transfer pumps.
Fuel Volume Measurement
- Fuel volume is measured in liters and is calculated for odd numbers by interpolation between even numbers.
Fuel Weight Calculation
- Fuel weight is based on volume and specific gravity.
- Fuel weight is measured in kilograms (Kg).
Fuel Temperature Measurement
- Each FCMC contains a number of temperature sensors that measure fuel temperature.
- Temperature sensors send data to the FCMC.
- The FCMC displays temperature information on the ECAM FUEL page.
MEL/Deactivation - Refuel Isolation Valve Failure
- If the refuel isolation valve solenoid fails, the valve can be manually operated.
MEL/Deactivation - Crossfeed Valve Failure
- If the crossfeed valve fails, in normal operations the aircraft can be dispatched with the valve inoperative (CLOSED) position.
Daily Checks - Drain Water Content
- Two drains are in the center tank, seven in each wing, and three in the trim tank.
- Water should be drained before refueling, or one hour after refueling.
- The center tank drain valves are found in an access panel on either side of the fuselage.
- The wing drain valves are accessible from the underside of the wing.
- For gravity purging, the center and wing tanks need > 10% tank content, while the trim tank needs at least 1000 kg (2200lb).
- The THS (Trim Hydraulic System) should also be moved to 0° trim.
- Use the PURGER tool to operate the drain valves, ensuring at least one liter of fuel is drained.
- If the drain valve leaks, push up and release the drain valve again.
Daily Checks - Environmental Precautions
- Do not discharge oil, fuel, solvent, or lubricant into trash bins, soil, or the water network.
- Use specific waste disposal containers for each product.
- Store each product in a fire-resistant and sealed cupboard.
System Overview - A330-300 Overview
- The aft APU pump starts if a low pressure is detected in the trim transfer line.
- The APU fuel isolation valve controls fuel flow from the FWD inner tank to the trim transfer line.
- The APU LP valve closes if an APU fire is detected.
- The fuel/air separator, installed in the trim tank fuel transfer line, maintains sufficient fuel for APU operation if air enters the line.
- The main transfer system controls fuel flow from the outer tanks to the two inner tanks for engine feeding.
Servicing
- Automatic refueling can be done with normal electrical power or with battery power only.
Indicating - FQI Probes
- Capacitive probes in each fuel tank measure fuel level.
- The FCMCs (Fuel Content Measuring Computers) measure capacitance values to determine fuel volume.
Indicating - Compensators
- Compensator probes measure fuel permittivity and are fully immersed in fuel.
Indicating - Densitometers
- One densitometer is installed near the lowest point of each inner tank.
- Densitometers measure fuel density.
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Description
This quiz explores the mechanisms and components involved in the aircraft Fuel Quantity Indicating (FQI) System. Gain insights into fuel level sensors, aircraft attitude impact on fuel calculations, and the role of Fuel Control and Monitoring Computers (FCMCs). Perfect for students learning about aviation systems and fuel management.