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The gpws can warn the crew in case of .1 excessive deviation below selected ? [ Control visibility ]

Question 64-1 : 2 3 1 2 3 3 1

Excessive deviation below selected altitude warning is given by the altitude alert system .predictive windshear alert can not be performed by the gpws but when windshear occurs the gpws can detect it and warn the crew the operation of the gpws is governed by laws taking the aircraft height into account as well as the descent rate and the aircraft configuration flaps/gear deployed or retracted exemple 164 2, 3.2, 3.

Concerning the tcas 2 when receiving a resolution advisory ra crew members ?

Question 64-2 : Immediatly initiate the required manoeuvre try to establish visual contact with the intruder before taking any evasive action immediatly engage autopilot which will be temporarily controlled by the tcas disregard this ra if they have a mode s transponder

exemple 168 Immediatly initiate the required manoeuvre.Immediatly initiate the required manoeuvre.

According to cs25 concerning the electronic display systems the amber/yellow ?

Question 64-3 : Caution advisory status warning

Admin . cs 25 1322 flight crew alerting . . e visual alert indications must . 1 conform to the following colour convention . i red for warning alert indications . ii amber or yellow for caution alert indications . iii any colour except red or green for advisory alert indications exemple 172 Caution.Caution.

The stall warning is inhibited .1 when the flaps are retracted.2 when the ?

Question 64-4 : 2 1 2 2 4 2 3

The stall warning computer uses the angle of attack and slats/flaps configuration the stall warning is inhibited when the aeroplane is on the ground exemple 176 2.2.

On a large aeroplane and according to the cs25 the stall warning system must ?

Question 64-5 : With the flaps and landing gear in any normal position with the flaps down and gear up only with the flaps fully extended and gear down only with the flaps not retracted only whatever the position of the landing gear

.the stall warning computer uses the angle of attack and slats/flaps configuration the stall warning is inhibited when the aeroplane is on the ground

The gpws warns the crew in case of . 1 excessive descent rate. 2 excessive ?

Question 64-6 : 1 2 5 1 2 3 5 1 2 4 5 4

exemple 184 1, 2, 5.1, 2, 5.

The egpws may propose the following functions . 1 abnormal take off ?

Question 64-7 : 2 4 5 1 2 3 5 1 3 4 2 3 4 5

Egpws enhanced ground proximity warning system .enhanced gpws uses essentially an electronic map of the world giving ground elevation and information from the aircraft's navigational system ins/gps or any combination given the location of the aircraft its course and height either from the adc or derived from gps a display can be created showing the locations of terrain that could threaten the safety of the aircraft .the operation of the egpws is governed by laws taking the aircraft height into account as well as the descent rate and the aircraft configuration flaps/gear deployed or retracted but it can not provide an abnormal take off configuration warning .predictive windshear alert can not be performed by the egpws but when windshear occurs the egpws can warn the crew

The flight warning system fws .1 draws the attention of the crew to the ?

Question 64-8 : 1 2 5 1 2 4 1 4 2 4 5

.the purpose of the flight warning system fws is to produce cautions and warnings for the crew to increase their situation awareness and to give them suitable indications of the action necessary to avoid impending danger the proliferation of various warning systems in today's aircraft poses a severe problem in that the crew could be confused by the multiplicity of warnings it is therefore necessary to install an integrated flight warning system that will prioritize the warnings by producing warnings relevant to a particular stage of flight and inhibiting other warnings the system enables the crew to respond to the warning posing the most immediate threat to safety .the flight warning system generates alerts and warnings for the following situations . engine and airframe systems malfunctions. aerodynamic limits exceeded. presence of external hazards exemple 192 1, 2, 5.1, 2, 5.

On a large aeroplane the input data of the stall warning system are .1 angle ?

Question 64-9 : 1 4 1 2 4 2 3 4 1 2

.the stall warning computer uses the angle of attack and slats/flaps configuration the stall warning is inhibited when the aeroplane is on the ground exemple 196 1, 41, 4

Concerning the tcas ii .1 neither advisory nor traffic display is provided for ?

Question 64-10 : 1 2 3 1 2 1 3 2 3

Admin .for aircraft to be visible to a tcas equipped aircraft they must have a minimum of a mode 'a' transponder if the transponder is switched off or is unserviceable the intruding aircraft are invisible to the tcas equipment and a collision risk exists .tcas operation is independent of ground based air traffic control .the tcas ii has inputs from the radio altimeter in order to gradually inhibit the resolution advisories ras when getting closer to the ground exemple 200 1, 2, 3.1, 2, 3.

The aural alert associated with the mode 5 excessive deviation below glideslope ?

Question 64-11 : 'glideslope' 'caution glideslope' 'too low glideslope' 'monitor glideslope'

Admin .gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 204 'glideslope'.'glideslope'.

The aural alert associated with the mode 1 excessive descent rate of the gpws is ?

Question 64-12 : 'sink rate' 'don't sink' 'too low terrain' 'terrain'

Gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 208 'sink rate'.'sink rate'.

The aural alert associated with the mode 3 altitude loss after take off or go ?

Question 64-13 : 'don't sink' 'sinkrate' 'too low terrain' 'terrain'

Admin .gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 212 'don't sink'.'don't sink'.

The aural alert associated with the mode 2 excessive terrain closure rate of ?

Question 64-14 : 'terrain' 'sinkrate' 'don't sink' 'climb'

Admin .gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 216 'terrain'.'terrain'.

The radio altimeter supplies data to the following system s .1 altitude alert ?

Question 64-15 : 2 3 4 1 4 3 3 4

.tcas use the radio altimeter input to inhibit warnings at low altitude gpws ground proximity warning system is governed by laws taking the aircraft height into account to provide warnings when approaching ground without the automatic landing system will allow the aircraft to fully complete the flare at landing .the function of the altitude alerting system is to warn the pilots that the aircraft is approaching or deviating from the altitude selected on the autopilot control panel it does this in certain height bands above and below the selected altitude .the radio altimeter does not supply data to the altitude alert system exemple 220 2, 3, 4.2, 3, 4.

The input data to the gpws originate from the .1 transponder.2 angle of ?

Question 64-16 : 4 1 4 2 3 4

Admin .the air data computer adc provides speed altitude and sink rate to the gpws .the transponder is a receiver/transmitter which will generate a reply signal upon proper interrogation .autothrottle controls selected speed or n1 .angle of attack sensor is an input to the stall warning system not to the gpws exemple 224 4.4.

The main function s of a tcas is to .1 alert the crew to ground proximity.2 ?

Question 64-17 : 2 1 3 1 2 3 4 2 4

exemple 228 2.2.

The aural alert s associated with the mode 1 excessive descent rate of the gpws ?

Question 64-18 : 3 4 2 4 1 2

exemple 232 3, 4.3, 4.

The aural alert s associated with the mode 3 altitude loss after take off or go ?

Question 64-19 : 1 2 2 4 3 4

Admin .gpws .mode 1 pull up .mode 2 terrain .mode 3 don't sink .mode 4 to low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 236 1.1.

The aural alert s associated with the mode 5 excessive deviation below ?

Question 64-20 : 3 2 2 4 1

Admin .gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 240 3.3.

A tcas resolution advisory ra voice message 'climb climb now' repeated twice ?

Question 64-21 : After a 'descend' ra when a reversal in the vertical manoeuvre sense is required after a 'climb' ra when the climb vertical rate is too weak each time a 'climb' ra is announced by a voice message when cleared of conflict and below the cruise altitude

Admin . ra reversal . 1014 exemple 244 After a 'descend' ra when a reversal in the vertical manoeuvre sense is required.After a 'descend' ra when a reversal in the vertical manoeuvre sense is required.

When comparing a tcas traffic advisory ta and a resolution advisory ra which ?

Question 64-22 : A ta indicates the relative position of the intruding traffic an ra provides a vertical traffic avoidance manoeuvre an ra indicates the relative position of the intruding traffic a ta provides a vertical traffic avoidance manoeuvre a ta provides the display of the traffic on the navigation display and the red arc on the vertical speed indicator an ra provides the voice alerts an ra generates the intruders colour codes on the navigation display according to the threat a ta manages the other tcas functions

exemple 248 A ta indicates the relative position of the intruding traffic; an ra provides a vertical traffic avoidance manoeuvre.A ta indicates the relative position of the intruding traffic; an ra provides a vertical traffic avoidance manoeuvre.

On a large aeroplane and according to the cs 25 207 when the speed is reduced ?

Question 64-23 : At a speed exceeding the stall speed by not less than 5 kt or 5% cas whichever is greater at a speed exceeding the stall speed by not less than 10 kt or 10% cas exactly at the stall speed at the stall speed +/ 5% cas

exemple 252 At a speed exceeding the stall speed by not less than 5 kt or 5% cas, whichever is greater.At a speed exceeding the stall speed by not less than 5 kt or 5% cas, whichever is greater.

If a tcas resolution advisory ra requires an immediate descent while at the ?

Question 64-24 : Follow the tcas ra and inform the atc comply with the atc request consider both requests and remain at the same level start a climb first and then follow the tcas ra

exemple 256 Follow the tcas ra and inform the atc.Follow the tcas ra and inform the atc.

Your aircraft and an intruding traffic are tcas ii equipped .your tcas can ?

Question 64-25 : Coordinated resolution advisories coordinated traffic advisories resolution advisories coordinated with the atc instructions traffic advisories coordinated with the atc instructions

exemple 260 Coordinated resolution advisories.Coordinated resolution advisories.

Which of these statements about the activation of the take off warning when a ?

Question 64-26 : I is incorrect ii is incorrect i is correct ii is correct i is correct ii is incorrect i is incorrect ii is correct

Admin .if the elevator is not in a safe position elevator is moved by the pilot via the control column or the sidestick on airbus you will not get an aural warning but you will have an aural warning if the stabilisator is not in a valid trim range for take off .in green the normal stablizer trim set for a boeing 737 at take off . 1020.also there is no automatique detection for a low brake pressure level .before take off or landing brake pressure can be monitored on a gauge in the cockpit . 1021 exemple 264 I is incorrect, ii is incorrect.I is incorrect, ii is incorrect.

Which of these statements about the activation of the take off warning when a ?

Question 64-27 : I is correct ii is incorrect i is incorrect ii is incorrect i is correct ii is correct i is incorrect ii is correct

.if the elevator is not in a safe position elevator is moved by the pilot via the control column or the sidestick on airbus you will not get an aural warning but you will have an aural warning if the stabilisator is not in a valid trim range for take off .in green the normal stablizer trim set for a boeing 737 at take off .. 1020. you will hear the aural warning if the stabiliser is not in a safe position for take off .also there is no automatique detection for a low brake pressure level .before take off or landing brake pressure can be monitored on a gauge in the cockpit . 1021. exemple 268 I is correct, ii is incorrect.I is correct, ii is incorrect.

Which of these statements about the activation of the take off warning when a ?

Question 64-28 : I is incorrect ii is correct i is incorrect ii is incorrect i is correct ii is incorrect i is correct ii is correct

Admin .if the elevator is not in a safe position elevator is moved by the pilot via the control column or the sidestick on airbus you will not get an aural warning but you will have an aural warning if the stabilisator is not in a valid trim range for take off .in green the normal stablizer trim set for a boeing 737 at take off . 1020.also you will have an aural warning if parking brake is still on it makes sense exemple 272 I is incorrect, ii is correct.I is incorrect, ii is correct.

The stick pusher is a part of the ?

Question 64-29 : Stall protection system automatic flight control system afcs flight envelope protection fep system stall warning system sws

Admin .a stick pusher is a device installed in some aircraft to prevent from entering an aerodynamic stall some aircraft display poor post stall handling characteristics or are vulnerable to deep stall to prevent such an aircraft approaching the stall the aircraft designer may install a hydraulic or electro mechanical device that pushes forward on the elevator control system whenever the aircraft's angle of attack reaches the pre determined value and then ceases to push when the angle of attack falls sufficiently .a stick pusher should not be confused with a stick shaker a stick shaker is a stall warning device whereas a stick pusher is a stall avoidance device stall protection system .notice for cpl a stall protection system is not part of the cpl learning objectives but since you can find stick pusher on 'small' airplane such as pilatus pc 12 jetstream 31 or swearingen metro it is important to understand what is a stick pusher exemple 276 Stall protection system.Stall protection system.

The egpws ?

Question 64-30 : Is an enhanced gpws which has a its own world terrain database is an enhanced gpws which warns the crew if the airplane is not in the appropriate configuration for take off is an enhanced gpws which is able to provide resolution advisories in the lateral plane has nothing to do with the gpws

exemple 280 Is an enhanced gpws which has a its own world terrain database.Is an enhanced gpws which has a its own world terrain database.

The stall warning computer of a large aeroplane uses the following data .1 ?

Question 64-31 : 2 3 1 2 1 2 3 1 3

.the stall warning computer uses the angle of attack and slats/flaps configuration the stall warning is inhibited when the aeroplane is on the ground exemple 284 2, 3.2, 3.

When a tcas is operating a failure of the active transponder will cause the ?

Question 64-32 : No longer operate normally operate in the traffic advisory ta mode only operate normally operate in the resolution advisory ra mode only

exemple 288 No longer operate normally.No longer operate normally.

The stall warning system of a large aeroplane includes .1 an angle of attack ?

Question 64-33 : 1 2 4 1 2 3 1 3 2 4

.the stall warning computer uses the angle of attack and slats/flaps configuration the stall warning is inhibited when the aeroplane is on the ground exemple 292 1, 2, 4.1, 2, 4.

The gpws receives data from the following systems .1 landing gear and flaps ?

Question 64-34 : 1 3 1 2 3 4 3 4 1 2

exemple 296 1, 3.1, 3.

For compatibility between the different components of a flight warning system ?

Question 64-35 : Stall windshear gpws tcas stall tcas gpws windshear tcas stall windshear gpws gpws stall tcas windshear

exemple 300 Stall, windshear, gpws, tcas.Stall, windshear, gpws, tcas.

When a tcas resolution advisory ra climb instruction is generated the required ?

Question 64-36 : Does not take into account the stall margin takes into account a 1 3 vs stall margin always takes into account the stall margin takes into account a 1 1 vs stall margin

.the tcas system does not take into account your true altitude your actual mass or the outside air temperature for density the tcas system can not compute your stall speed thus the tcas can not take into account the stall margin when a ra climb instruction is generated .the pilot must ensure that he remains in a safe flight envelope exemple 304 Does not take into account the stall margin.Does not take into account the stall margin.

The aural alert s associated with the mode 4 of the gpws unsafe terrain ?

Question 64-37 : 1 2 3 1 2 2 2 4

Admin .gpws .mode 1 sink rate pull up .mode 2 terrain pull up .mode 3 don't sink .mode 4 too low gear too low flaps too low terrain .mode 5 glideslope .mode 6 bank angle .mode 7 windshear exemple 308 1, 2, 3.1, 2, 3.

When enhanced gpws egpws terrain is displayed if the computed aircraft position ?

Question 64-38 : The terrain display will diverge from the real terrain environment around the aircraft position the egpws will perform a correction of position thus the terrain display accuracy won't be degraded the egpws will fail the terrain display function and the terrain will be removed from the navigation display the egpws has its own position sensors thus the terrain display accuracy won't be degraded

exemple 312 The terrain display will diverge from the real terrain environment around the aircraft position.The terrain display will diverge from the real terrain environment around the aircraft position.

With a tcas ii when a corrective resolution is generated ?

Question 64-39 : The vertical speed must be effectively modified without delay the heading must be effectively modified without delay the ias must be effectively modified without delay no action is required vertical speed heading and ias can remained unchanged

exemple 316 The vertical speed must be effectively modified without delay.The vertical speed must be effectively modified without delay.

At high angles of attack and according to the type of aeroplane the stall ?

Question 64-40 : 2 1 2 1 3 1 2 3

Cqb15 may 2012 ..only the slats will extend to the full position the autoslat system is designed to enhance airplane stall characteristics at high angles of attack during takeoff or approach to landing on boeing 737 as the airplane approaches the stall angle the slats automatically begin driving to the full extended position prior to stick shaker activation the slats return to the extend position when the pitch angle is sufficiently reduced below the stall critical attitude .the stall protection system can increase thrust if autothrottle is armed it will engages and power will be advanced to maintain at least vmin airspeed the trim will be inhibited to nose up exemple 320 2.2.

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