Question 66-1 : Flying manually during a final approach the flight director system is engaged in the loc mode holding of localizer axis if the aircraft is left of the localizer axis the vertical command bar ? [ Experience lift off ]

Question 66-2 : Flying manually during a final approach the flight director system is engaged in the loc mode holding of localizer axis if the aircraft is right of the localizer axis the vertical command bar ?

May be centred if the pilot is correcting to come back on the localizer axis.

Question 66-3 : The flight director is engaged in the heading select mode hdg sel heading 180° selected when heading is 160° the vertical bar of the fd ?

Is centered if the bank angle of the aircraft is equal to the bank angle computed by the flight director calculator.

Question 66-4 : The flight director provides information for the pilot ?

To join to a desired path with the optimum attitude.

Question 66-5 : The horizontal command bar of a flight director ?

Question 66-6 : The horizontal command bar of a flight director 1 repeats the position information given by the ils in the horizontal plane 2 repeats the position information given by the ils in the vertical plane 3 gives information about the direction and the amplitude of the corrections to be applied on the ?

3.

Question 66-7 : The parameters taken into account by the flight director computer in the altitude hold mode alt hold are 1 altitude deviation2 engine rpm3 ground speed4 pitch attitudethe combination regrouping all the correct statements is ?

Question 66-8 : The purpose of a flight director is to ?

Reduce the pilots workload by presenting data in the form of control commands.

Question 66-9 : The vertical command bar of a flight director ?

Gives information about the direction and the amplitude of the corrections to be applied on the bank of the aircraft.

Question 66-10 : The vertical command bar of a flight director 1 repeats the position information given by the ehsi 2 repeats the position information given by the vor 3 supplies information about the direction and magnitude of the corrections to be applied to the bank of the aircraftthe combination regrouping ?

3.

Question 66-11 : To allow the coupling of a dual channel flight director ?

Both autopilot channels must be selected on.

Coupling of both flight director is necessary to perform a full autolandwhen establish on an ils between 3000 ft and 1500 ft above ground you can switch on both autopilot it allows the coupling of a dual channel flight director to realize the full autoland

Question 66-12 : An aircraft flies steadily on a heading 270° the flight director is engaged in the heading select mode hdg sel heading 270° selected if a new heading 360° is selected the vertical trend bar ?

Deviates to the right and will be centred as soon as you roll the aircraft to the bank angle calculated by the flight director.

Question 66-13 : An automatic ils approach can be flown only ?

Within a range of crosswinds and levels of turbulence.

Question 66-14 : The 'guidance' functions of a autopilot consist in ?

Monitoring the movements of the centre of gravity in the three dimensions of space.

The basic function of an autopilot is stabilisation the stabilisation of the aircraft around its centre of gravity basic function is achieved by the inner loop systemsthe advanced function is 'guidance' monitoring the movements of the centre of gravity in the three dimensions of space outer loop systems offer the guidance facilities altitude hold heading hold vnav lnav outer loops act from an external position on the inner loop and 'fool' the inner loop into manoeuvrig the aircraft into achieving its aim

Question 66-15 : The 'airspeed hold' mode can be engaged and maintained during ?

Climbs descents turns and power changes.

Question 66-16 : The output data of the flight director computer are ?

Two channels pitch and roll.

Question 66-17 : The initiation of an automatic go around can be ?

In a range of approach airspeeds.

A go around will be initiated while established on approach usually between 5 nm and the runway threshold you are in the approach configuration flaps deployed possibly slats deployed and gear down you will initiate the automatic go around procedure by pressing toga switch located on the engine thrust lever

Question 66-18 : During a final approach if the flight director system is engaged in the gs mode holding of ils glide slope the position of the horizontal command bar indicates ?

The correction on the pitch to be applied to join and follow the ils glide slope.

Question 66-19 : If in the event of a failure there is no significant out of trim condition or deviation of flight path or attitude but the landing is not completed automatically such an automatic landing system is considered as ?

Fail passive.

The question specifically states that the failure has occured and the landing was not completed automatically this is 'fail passive' with a three autopilot system the failure of one system still leaves two operating so that is fail operational

Question 66-20 : If in the event of a failure the approach flare and landing can be completed by the remaining part of the automatic system such an automatic landing system is considered as ?

Question 66-21 : Considering a flight director of the 'command bars' type ?

The horizontal bar is associated with the pitch channel.

Question 66-22 : The command bars of a flight director ?

May be displayed when flying manually or with the autopilot engaged.

Question 66-23 : The purpose s of the flight director system is are to 1 give the position of the aircraft according to radioelectric axis2 give the position of the aircraft according to waypoints3 to aid the pilot when flying manuallythe combination that regroups all of the correct statements is ?

3.

Question 66-24 : Concerning the command bars of a flight director ?

It is possible to remove them by switching the flight director off.

Question 66-25 : The lateral flight path modes of an autopilot system are 1 speed hold2 localiser intercept and track3 track hold4 fms lateral navigation5 pitch attitude holdthe combination that regroups all of the correct statements is ?

2 3 4.

Autopilot lateral mode roll attitude heading vor mode navigation mode gpsfmsins autopilot longitudinal mode altitude hold and capture speed hold and capture with at ias andor mach thrust hold and capture with at pitch attitude

Question 66-26 : The purpose of the autopilot control wheel steering cws mode is ?

To consider as target parameters the current pitch and roll angles at the time the mode becomes active.

Pushing a cws engage switch engages the ap pitch and roll axes in the cws mode and displays cws p and cws r on the fmaswith cws engaged the ap maneuvers the airplane in response to control pressures applied by the pilot the control pressure is similar to that required for manual flightwhen control pressure is released the ap holds existing attitude

Question 66-27 : When engaged in the fms lateral navigation mode lnav the autopilot uses the command provided by the ?

Fms.

Question 66-28 : In an autopilot system the flight path modes are 1 pitch attitude hold2 ias and mach number hold3 altitude hold4 glide slope intercept and trackthe combination regrouping all the correct statements is ?

2 3 4.

Question 66-29 : The lateral flight path modes of an autopilot system are 1 heading hold2 speed hold3 fms lateral navigation4 tas hold5 localizer intercept and trackthe combination that regroups all of the correct statements is ?

1 3 5.

Autopilot lateral mode roll attitude heading vorils mode navigation mode gpsfmsins autopilot longitudinal mode altitude hold and capture speed hold and capture with at ias andor mach thrust hold and capture with at pitch attitude

Question 66-30 : The vertical flight path modes of an autopilot system are 1 pitch attitude hold2 altitude hold3 track hold4 glide slope intercept and trackthe combination that regroups all of the correct statements is ?

2 4.

The question is about the vertical flight path modes onlypitch attitude holding horizontal wing holding yaw damper are parts of the 'basic' function of the autopilot the stabilisation of the aircraft around its centre of gravity 'track hold' is a function of the horizontal flight path modes

Question 66-31 : The automatic synchronisation function of an autopilot control system 1 operates only when the autopilot is engaged 2 prevents the aircraft's control system from jerking when disengaging the autopilot 3 prevents the aircraft's control system from jerking when engaging the autopilot the ?

3.

Before the autopilot can be engaged certain conditions must be met these conditions vary with aircraft type eg no force is being applied to the control wheel it must also be ensured that on engagement the 'take over' is affected smoothly and without 'snatching' of the aircraft's control system in other words the aircraft must be trimmed for the desired flight attitude before engagement and the automatic control system must be synchronised to maintain that attitude on engagement the automatic synchronisation operates before the autopilot is engaged

Question 66-32 : The components of an autopilot system are the 1 actuators2 mode control panel3 mode annunciator panel4 computerthe combination that regroups all of the correct statements is ?

1 2 3 4.

Ashahabpour hithere is another question that looks like this i think it's exactly the same but the answer is different the mode annunciator panel is not in the combination that regroups all of the correct statements do you have an explanation the question you are talking about is n°882'the computer of the autopilot system uses among others input signals from the 1 attitude reference system2 mode annunciator panel3 adc4 mode control panelanswer 1 3 4as you can see the question is slightly different it talks about the computer of the autopilot only

Question 66-33 : Concerning a fail passive flight control system in the event of a failure 1 there may be a significant deviation of flight path or attitude 2 there is no significant deviation of flight path or attitude 3 there is no significant out of trim condition 4 there may be a significant out of trim ?

2 3.

fail passive flight control system a flight control system is fail passive if in the event of a failure there is no significant out of trim condition or deviation of flight path or attitude but the landing is not completed automatically for a fail passive automatic flight control system the pilot assumes control of the aeroplane after a failure fail operational flight control system a flight control system is fail operational if in the event of a failure below alert height the approach flare and landing can be completed automatically in the event of a failure the automatic landing system will operate as a fail passive system

Question 66-34 : Concerning a fail passive flight control system in the event of a failure there may be a significant deviation of flight path or attitude2 there is no significant deviation of flight path or attitude3 the landing is not completed automatically4 the landing is completed automaticallythe ?

2 3.

fail passive flight control system a flight control system is fail passive if in the event of a failure there is no significant out of trim condition or deviation of flight path or attitude but the landing is not completed automatically for a fail passive automatic flight control system the pilot assumes control of the aeroplane after a failure fail operational flight control system a flight control system is fail operational if in the event of a failure below alert height the approach flare and landing can be completed automatically in the event of a failure the automatic landing system will operate as a fail passive system

Question 66-35 : For a fms designed with the lateral navigation lnav capability coupled to the autopilot the fms lateral command output is ?

A roll angle or a heading target.

Question 66-36 : The cs 25 gives the following definition 'where the pilot has the ability to make inputs to the automatic pilot by movement of the normal control wheel'the corresponding mode is ?

Control wheel steering cws .

Question 66-37 : When engaging the autopilot the function providing a smooth 'take over' is the ?

Automatic synchronisation function.

When engaging the autopilot automatic synchronisation functionwhen disengaging the autopilot automatic pitch trim function

Question 66-38 : When disengaging the autopilot the function providing a smooth 'hand over' is the ?

Automatic pitch trim function.

When engaging the autopilot automatic synchronisation functionwhen disengaging the autopilot automatic pitch trim function

Question 66-39 : During an autocoupled ils approach followed by an automatic landing the guidance signals in the vertical plane under 200 ft are computed according to the ?

Radio altitude.

Question 66-40 : The computer of the autopilot system uses among others the following parameters ?

Cas altitude vertical speed heading attitude.