Lower limit of this arc of the airspeed indicator is maximum weight stalling speed in landing configuration.

If the humidity changes frequently, put a cover on the unit.

Do the leak test.

Tell person A to remove the chocks.

Two resolvers measure the position of the fuel metering valve.

Fuel flows from the HMU to the fuel flow transmitter.

All engine fuel and control components are on the engine.

There are 24 wide-chord, titanium fan blades.

The number 4 bearing holds the rear of the N2 shaft.

A splitter fairing divides the air into these two air flows.

The fan increases the speed of the air.