用来确定飞机上某一点的位置的数据是

ON THE REFUEL/DEFUEL PANEL, THE "END" LIGHT:

THE AMBER OPEN LIGHT ON THE REFUEL/DEFUEL PANEL:

IF THE FUEL TEMPERATURE EXCEEDS A HIGH OR A LOW LIMIT, THE FUEL TEMPERATURE INDICATION ON THE ECAM:

TOTAL FUEL ON BOARD (FOB) IS DISPLAYED:

ENGINE LOW PRESSURE VALVE INDICATIONS ON THE ECAM ARE SHOWN GREEN AND IN LINE WHEN:

THE EDP (ENGINE DRIVEN PUMP) "OFF" STATUS IS VERIFIED BY:

THE PURPOSE OF THE PRIORITY VALVE IS TO:

THE MAIN PUMPS NORMALLY USED TO PRESSURIZE THE HYDRAULIC POWER SYSTEMS IN FLIGHT ARE:

THE COMPONENT(S) WHICH TRIGGER(S) A WARNING AND "FAULT" SIGNALS ON THE HYDRAULIC CONTROL PANEL IS (ARE):

THE POWER TRANSFER UNIT (PTU) ALLOWS: