Recall the function of the FUEL QTY A/B button
Selects the alternate channel of the fuel quantity gauging system
Recall the function of the FUEL SYS TEST button
Button is a MAINTENANCE function only – no crew action required. When pushed
and held, starts a fuel system test display on the FUEL SD
Recall the function of the START PUMP
A DC start pump, located in the right main tank, provides fuel pressure for starting the APU or engines when AC power is not available
Recall the function of the FUEL USED RESET button
Resets fuel used digits on the fuel synoptic
Recall approximate fuel tank capacities
Left Wing Tank: 9,266 lbs
Center Wing Tank: 6,077 lbs
Right Wing Tank: 9,266 lbs
TOTAL: 24,609 lbs
Recall the number of fuel pumps available for each tank
Recall the Fuel Return to Tank (RTT) process
• Excess warmed fuel cycling through the engine fuel system is returned to the inboard, cooled corner of each main tank
• This process warms the fuel in the tank and retards wing ice formation due to cooled fuel
• Fuel return to tank flow may be inhibited by the EEC for many reasons, including:
takeoff, landing, main tank fuel low, or high fuel temperature
Describe the use of FUEL X-FEED lever
A FUEL X-FEED lever, on the pedestal, permits routing of fuel from either main fuel tank to one or both operating engines. Cross-feeding is enabled when the valve is opened and the boost pumps on the receiving side are turned off
Recall features of the Fuel Venting system
Recall how the APU is supplied fuel
The APU normally is supplied fuel from the right main tank, however, if the center tank contains fuel and its pumps are on, the center tank will supply the APU
Recall APU fuel usage for ground operations
350 pounds/hour