Un compte Premium offert sur le site FCL.055 ! Rendez-vous sur www.fcl055-exam.fr puis créez un compte avec le même email que celui...   [Lire la suite]


The essential components of a flight director are .1 a computer .2 an ? [ Test maintenance ]

Question 52-1 : 1 4 1 2 2 4 2 3

exemple 152 1, 4.1, 4.

The control law of a transport airplane autopilot control channel may be ?

Question 52-2 : Computer input deviation data and the output control deflection signals input and output signals at the amplifier level respectively control deviation data and control deflection signals crew inputs to the computer and the detector responses returned to the airplane computer input deviation data and the signals received by the servoactuators

The autopilot control laws determine how the computer interprets a performance demand in terms of a control response exemple 156 Computer input deviation data and the output control deflection signals.Computer input deviation data and the output control deflection signals.

In a transport airplane an autopilot comprises in addition to the mode display ?

Question 52-3 : 2 3 4 5 6 1 2 6 1 3 4 6 2 3 4 5

exemple 160 2, 3, 4, 5, 6.2, 3, 4, 5, 6.

A pilot engages the control wheel steering cws of a conventional autopilot and ?

Question 52-4 : Maintain the flight attitude obtained at that moment roll wings level and maintain the heading obtained at that moment maintain the track and the flight attitude obtained at that moment restore the flight attitude and the rate of turn selected on the autopilot control display unit

exemple 164 Maintain the flight attitude obtained at that moment.Maintain the flight attitude obtained at that moment.

The basic modes of an autopilot consist in ?

Question 52-5 : Stabilizing the aircraft around its centre of gravity controlling the movement of the centre of gravity of the aircraft controlling the path of the aircraft horizontally or vertically controlling the path of the aircraft vertically only

Admin .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 systems .the 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 exemple 168 Stabilizing the aircraft around its centre of gravity.Stabilizing the aircraft around its centre of gravity.

On a modern aircraft the flight director modes are displayed on the ?

Question 52-6 : Upper strip of the pfd primary flight display upper strip of the nd navigation display upper strip of the ecam electronic centralized a/c management control panel of the flight director only

exemple 172 Upper strip of the pfd (primary flight display).Upper strip of the pfd (primary flight display).

In order to know in which mode the auto throttles are engaged the crew will ?

Question 52-7 : Pfd primary flight display nd navigation display tcc thrust control computer throttles position

exemple 176 Pfd (primary flight display)Pfd (primary flight display)

An automatic landing system necessitating that the landing be continued ?

Question 52-8 : 'passive' 'safe' 'redundant' 'operational'


When an aircraft operating in the vor coupled mode approaches the 'cone of ?

Question 52-9 : Temporarily maintains a heading is damped by a trim input signal from the lateral trim system remains always coupled to the selected vor radial is temporarily disconnected

exemple 184 Temporarily maintains a heading.Temporarily maintains a heading.

The command bars of a flight director are generally represented on an ?

Question 52-10 : Adi attitude director indicator hsi horizontal situation indicator rmi radio magnetic indicator ils instrument landing system


After having programmed your flight director you see that the indications of ?

Question 52-11 : Increase the flight attitude until the command bars recentre on the symbolic airplane decrease the flight attitude until the command bars recentre on the symbolic airplane increase the flight attitude until the command bars recentre on the horizon decrease the flight attitude until the command bars recentre on the horizon

exemple 192 Increase the flight attitude until the command bars recentre on the symbolic airplane.Increase the flight attitude until the command bars recentre on the symbolic airplane.

An autopilot capable of holding at least altitude and heading mode is compulsory ?

Question 52-12 : For ifr or night flights with only one pilot on multipilot airplanes for vfr and ifr flights with only one pilot on airplanes over 5 7 t

For a private flight an autopilot is not compulsory but for cpl/atpl we are talking about commercial air transportation .ops 1 655 additional equipment for single pilot operation under ifr .an operator shall not conduct single pilot ifr operations unless the aeroplane is equipped with an autopilot with at least altitude hold and heading mode exemple 196 For ifr or night flights with only one pilot.For ifr or night flights with only one pilot.

Among the following functions of an autopilot those related to the airplane ?

Question 52-13 : 3 4 and 5 1 3 4 and 5 1 2 and 6 1 2 3 and 6

Admin .the question is asking about the 'guidance' functions of the autopilot .the 'guidance' functions of a autopilot consist in monitoring the movements of the centre of gravity in the three dimensions of space 'guidance' functions are .altitude hold heading hold airspeed hold vnav vertical navigation lnav lateral navigation .pitch 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 exemple 200 3, 4 and 5.3, 4 and 5.

The ias or mach hold mode is provided by .1 the autopilot pitch channel in the ?

Question 52-14 : 1 4 1 3 2 3 2 4

Admin .during climb when ias or mach hold speed mode is engaged speed mode the speed is maintained by the autopilot pitch channel by adjusting the elevator position in order to decrease the climb angle thrust is maintained constant .when you are established at your cruising level or when established on the glide path the autothrottles will maintain speed constant by increasing or decreasing thrust the elevator is not adjusted for controlling the speed in alt hold or app mode exemple 204 1, 4.1, 4.

After having programmed your flight director you see that the indications of ?

Question 52-15 : Increase the flight attitude and bank your airplane to the left until the command bars recentre on the symbolic aeroplane increase the flight attitude and bank your aeroplane to the right until the command bars recentre on the symbolic aeroplane decrease the flight attitude and bank your airplane to the left until the command bars recentre on the symbolic aeroplane decrease the flight attitude and bank your airplane to the right until the command bars recentre on the symbolic aeroplane

exemple 208 Increase the flight attitude and bank your airplane to the left until the command bars recentre on the symbolic aeroplane.Increase the flight attitude and bank your airplane to the left until the command bars recentre on the symbolic aeroplane.

When being engaged and without selecting a particular mode an automatic pilot ?

Question 52-16 : Aeroplane stabilisation with attitude hold or maintaining vertical speed and possibly automatic trim aeroplane piloting and guidance functions a constant speed on track wings horizontal all aeroplane piloting and guidance functions except maintaining radio navigation course lines

.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 systems .the 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 exemple 212 Aeroplane stabilisation with attitude hold or maintaining vertical speed and possibly automatic trim.Aeroplane stabilisation with attitude hold or maintaining vertical speed and possibly automatic trim.

The position of a flight director command bars ?

Question 52-17 : Indicates the manoeuvres to execute to achieve or maintain a flight situation repeats the adi and hsi information enables the measurement of deviation from a given position only displays information relating to radio electric deviation

exemple 216 Indicates the manoeuvres to execute, to achieve or maintain a flight situation.Indicates the manoeuvres to execute, to achieve or maintain a flight situation.

In an auto pilot slaved powered control circuit the system which ensures ?

Question 52-18 : Can itself when it fails prevent the automatic pilot from being engaged intervenes only when the automatic pilot has been engaged prevents uncommanded surface deflection when the automatic pilot is disengaged is inhibited when the automatic pilot is engaged

exemple 220 Can itself, when it fails, prevent the automatic pilot from being engaged.Can itself, when it fails, prevent the automatic pilot from being engaged.

An autopilot system ?

Question 52-19 : Must provide at least aircraft stabilisation functions must provide at least aircraft guidance functions must provide automatic take off functions may provide automatic take off functions

exemple 224 Must provide at least aircraft stabilisation functions.Must provide at least aircraft stabilisation functions.

During an automatic landing between 50 ft agl and touch down the autopilot ?

Question 52-20 : A vertical speed according to the radio altimeter height a constant vertical speed a vertical speed according to the gps height a constant flight path with reference to the ground

Admin .the autopilot flares out at this stage by progressively reducing the vertical velocity exemple 228 A vertical speed according to the radio altimeter height.A vertical speed according to the radio altimeter height.

A flight control system which can in the event of a failure complete ?

Question 52-21 : Operational passive soft hard

exemple 232 Operational.Operational.

Command bars of the flight director may be present on the . 1 hsi. 2 cdu. 3 ?

Question 52-22 : 3 1 2 3 1 3 1

exemple 236 33

Considering a flight director of the 'command bars' type ?

Question 52-23 : The vertical bar is associated with the roll channel the vertical bar is associated with the pitch channel the horizontal bar is associated with the roll channel the horizontal bar may be associated with the roll channel

exemple 240 The vertical bar is associated with the roll channel.The vertical bar is associated with the roll channel.

Considering a flight director of the 'command bars' type .1 the vertical bar ?

Question 52-24 : 1 4 1 2 4 1 3 4 1 2 3 4

exemple 244 1, 4.1, 4.

During a final approach the flight director system is engaged in the loc mode ?

Question 52-25 : The correction on the bank to be applied to join and follow the localizer axis the position of the aircraft relative to the localizer axis the instantaneous deviation between the aircraft position and the localizer axis the roll attitude of the aircraft

exemple 248 The correction on the bank to be applied to join and follow the localizer axis.The correction on the bank to be applied to join and follow the localizer axis.

Flying manually during a final approach the flight director system is engaged ?

Question 52-26 : May be centred if the pilot is correcting to come back on to the ils glide slope cannot be centred is automatically centred since the g/s mode is engaged will be centred only when establish on the ils glide slope

exemple 252 May be centred if the pilot is correcting to come back on to the ils glide slope.May be centred if the pilot is correcting to come back on to the ils glide slope.

Flying manually during a final approach the flight director system is engaged ?

Question 52-27 : May be centred if the pilot is correcting to come back on the ils glide slope is automatically centred since the g/s mode is engaged deviates upward whatever the attitude of the aircraft is deviates downward whatever the attitude of the aircraft is

exemple 256 May be centred if the pilot is correcting to come back on the ils glide slope.May be centred if the pilot is correcting to come back on the ils glide slope.

Flying manually during a final approach the flight director system is engaged ?

Question 52-28 : May be centred if the pilot is correcting to come back on the localizer axis is automatically centred since the loc mode is engaged deviates to the left whatever the attitude of the aircraft is deviates to the right whatever the attitude of the aircraft is

exemple 260 May be centred if the pilot is correcting to come back on the localizer axis.May be centred if the pilot is correcting to come back on the localizer axis.

Flying manually during a final approach the flight director system is engaged ?

Question 52-29 : May be centred if the pilot is correcting to come back on the localizer axis cannot be centred is automatically centred since the loc mode is engaged will be centred only when establish on the localizer axis

exemple 264 May be centred if the pilot is correcting to come back on the localizer axis.May be centred if the pilot is correcting to come back on the localizer axis.

The flight director is engaged in the heading select mode hdg sel heading ?

Question 52-30 : Is centered if the bank angle of the aircraft is equal to the bank angle computed by the flight director calculator is centered if the aircraft has a 20° left drift is centered if the aircraft has a 20° right drift cannot be centered

exemple 268 Is centered if the bank angle of the aircraft is equal to the bank angle computed by the flight director calculator.Is centered if the bank angle of the aircraft is equal to the bank angle computed by the flight director calculator.

The flight director provides information for the pilot ?

Question 52-31 : To join to a desired path with the optimum attitude to remain within the flight envelope to join a desired track with a 45° intercept angle to join a desired track with a constant bank angle of 25°

exemple 272 To join to a desired path with the optimum attitude.To join to a desired path with the optimum attitude.

The horizontal command bar of a flight director ?

Question 52-32 : Gives information about the direction and the amplitude of the corrections to be applied on the pitch of the aircraft repeats the position information given by the ils in the horizontal plane repeats the position information given by the ils in the vertical plane gives information only about the direction of the corrections to be applied on the pitch of the aircraft

exemple 276 Gives information about the direction and the amplitude of the corrections to be applied on the pitch of the aircraft.Gives information about the direction and the amplitude of the corrections to be applied on the pitch of the aircraft.

The horizontal command bar of a flight director .1 repeats the position ?

Question 52-33 : 3 1 3 2 3 2

exemple 280 33

The parameters taken into account by the flight director computer in the ?

Question 52-34 : 1 4 1 3 1 2 1

Admin .the action taken by the autopilot to maintain an altitude depends on how far the aircraft is from the required altitude altitude deviation .pitch attitude and present altitude deviation are required exemple 284 1, 4.1, 4.

The purpose of a flight director is to ?

Question 52-35 : Reduce the pilots workload by presenting data in the form of control commands convey air traffic control information to the pilot provide an automatic landing system function automatically steer the aircraft to waypoints selected on the cdu

exemple 288 Reduce the pilots workload by presenting data in the form of control commands.Reduce the pilots workload by presenting data in the form of control commands.

The vertical command bar of a flight director ?

Question 52-36 : Gives information about the direction and the amplitude of the corrections to be applied on the bank of the aircraft repeats the position information given by the ils in the horizontal plane repeats the position information given by the ils in the vertical plane gives information only about the direction of the corrections to be applied on the bank of the aircraft

exemple 292 Gives information about the direction and the amplitude of the corrections to be applied on the bank of the aircraft.Gives information about the direction and the amplitude of the corrections to be applied on the bank of the aircraft.

The vertical command bar of a flight director .1 repeats the position ?

Question 52-37 : 3 1 2 3 1 3 2 3

exemple 296 3.3.

To allow the coupling of a dual channel flight director ?

Question 52-38 : Both autopilot channels must be selected on only one autopilot channel must be selected on both vhf comms channels must be serviceable both vhf nav channels must be serviceable

.coupling of both flight director is necessary to perform a full autoland .when 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 exemple 300 Both autopilot channels must be selected on.Both autopilot channels must be selected on.

An aircraft flies steadily on a heading 270° the flight director is engaged in ?

Question 52-39 : Deviates to the right and will be centred as soon as you roll the aircraft to the bank angle calculated by the flight director deviates to the right and remains in that position until the aircraft has reached heading 360° disappears the new heading selection has deactivated the hdg mode deviates to its right stop as long as the aeroplane is more than 10° off the new selected heading

exemple 304 Deviates to the right and will be centred as soon as you roll the aircraft to the bank angle calculated by the flight director.Deviates to the right and will be centred as soon as you roll the aircraft to the bank angle calculated by the flight director.

An automatic ils approach can be flown only ?

Question 52-40 : Within a range of crosswinds and levels of turbulence within a range of crosswinds and no limit for turbulence within a range of levels of turbulence and no limit for crosswinds without limits for crosswind or turbulence

exemple 308 Within a range of crosswinds and levels of turbulence.Within a range of crosswinds and levels of turbulence.


~

Exclusive rights reserved. Reproduction prohibited under penalty of prosecution.

2039 Free Training Exam