When the pilot needs to do no more than switch on and tune the receiver to an in range station in order to obtain a continuous indication of the bearing to the VOR station on the RMI?

What would occur on the RMI in the cone of confusion?

What angle is the cone of confusion felt at?

What range does the glideslope antenna operate between?

What angle above the horizontal does the two signals from the glideslope equal?

How many channels are there is glideslope?

What range does the localiser operate between?

What must be inserted in the NAV system if an indicator is removed for servicing to keep it balanced?

What channel are the signals from the radio navigation beacon (VOR) sent to?

How do you prevent other VOR radials which may confuse the aircraft which cuts off the roll channel for a predetermined period?

What height is glideslope flare initiated from the radar altimeter of the pitch computer?

How many discrete inputs and outputs channels are there in a FMS?

What does the FMS select and tunes to in order to constantly update the position and speed of the aircraft?

What provides guidance between waypoints of the active flight plan in guidance management of an FMS?

When can vertical navigation be accomplished in an FMS?

On the CDU, where is information stored?

When can maintenance pages of the CDU we accessed?

What data input does the CDU communicate to the FMC via?

How frequent is the background data on the map display of an FMC updated?

Limiting the effect of a runaway and allowing enough authority to the control system so that the required flight path may be followed even though the aircraft encounters disturbances are requirements for which system?

During auto land, what must the AFCS be capable of?

The ability of a system to withstand a failure without producing excessive deviations from the flight path is called?

What is the system which one failure can occur but leaves the overall system still functioning without causing degradation of performance outside the limits required for automatic landing called?

A system comprising of two or more independent simplex system used collectively, so that in the event of a failure of a system, the remaining system can perform the controlling function is called?

A fail-operational system of three complete systems or channels, which are interconnected, and together provide continuous control is called?

A system comprising two systems in parallel and with separate power suppliesis called?

Land 2 signifies there is dual redundancy of engaged flight control computers, sensors and servos

Land 3 signifies triple redundancy of power sources, engaged flight control computers, sensors and servos

What is selected in take off mode for the servo actuators to advance the throttles to obtain the correct N1 value to obtain aircrafts take off speed?