50 PSI pressure.

fuel pumps supply pressure for pressure defueling, and an external defuel source provides suction for suction defueling.

150% of the take-off fuel flow when the tank contains the minimum fuel allowable.

strict adherence to configuration, methods, techniques, and practices as prescribed is required to ensure the CDCCL is necessary.

non-return valve and a pressure switch.

it is important not to fill the expansion space in the tank.

prevent the CG of the aircraft from moving forwards as fuel is burned.

more than one engine to lose power.

the slide valve is not correctly seated.

2 fuel inlets and 1 fuel outlet

must be replaced.

water

engine inlet.

build up of static electricity.

high wing aircraft.

in direct contact with the aircraft skin.

reduce the landing weight in emergencies.

the closed position

air spaces interconnected.

brown black slime.

the expansion space must be 2% of the tank capacity.

to resist fuel surging within the fuel tank.

sump

sometimes called ejector pump

releases air trapped in the engine fuel feed line.

capacitor

Ultrasonic Probes

nitrogen

0.8