In an autopilot system, the guidance modes are:

 1 - Pitch angle hold 

 2 - IAS and Mach number hold

3 - Altitude hold

4 - Glide slope intercept and track

 The combination that regroups all of the correct statements is..

An inner loop control (stabilisation) is...

During a climb with the autopilot engaged in the V/S mode (holding of vertical speed), the auto-throttle:

If a large transport aeroplane is flown in Control Wheel Steering mode, the pitch attitude is controlled with the...

What is the purpose of the autothrust system?

Which statements below that applies best to an ADIRU?

The positions of the mode selector of an inertial navigation unit are: OFF - STBY - ALIGN NAV - ATT:

 1 - in "STBY", the unit aligns on the local geographic co-ordinate system 

 2 - the "ATT" position is used during autom: landing (LAND mode)

 3 - in "NAV" the co-ordinates of the start position can be entered

 4 - the platform is levelled before azimuth alignment

 5 -  in cruise, the unit can only be used in "NAV" mode. 

 The combination that regroups all of the correct statements is:

A pilot is flying a GNSS non-precision approach using the autopilot. The pilot intends to disconnect

The alignment time, at mid-latitudes, for an Inertial Reference System using laser ring gyros is approximately:

"Contingency Fuel" is the amount of fuel that should account for (1) — to the (2) _ aerodrome.