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Theoretical > lift > off : On a large aeroplane and according to the cs25 the stall warning system must ?

Question 62-1 : 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 exemple 162 with the flaps and landing gear in any normal position.with the flaps and landing gear in any normal position.

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

Question 62-2 : 1 2 5 1 2 3 5 1 2 4 5 4

exemple 166 1, 2, 5.1, 2, 5.

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

Question 62-3 : 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 exemple 170 2, 4, 5.2, 4, 5.

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

Question 62-4 : 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 174 1, 2, 5.1, 2, 5.

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

Question 62-5 : 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 178 1, 41, 4

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

Question 62-6 : 1 2 3 1 2 1 3 2 3

.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

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

Question 62-7 : 'glideslope' 'caution glideslope' 'too low glideslope' 'monitor glideslope'

.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 186 'glideslope'.'glideslope'.

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

Question 62-8 : '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

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

Question 62-9 : 'don't sink' 'sinkrate' '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 194 'don't sink'.'don't sink'.

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

Question 62-10 : 'terrain' 'sinkrate' 'don't sink' 'climb'

.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 198 'terrain'.'terrain'.

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

Question 62-11 : 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 202 2, 3, 4.2, 3, 4.

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

Question 62-12 : 4 1 4 2 3 4

.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 206 4.4.

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

Question 62-13 : 2 1 3 1 2 3 4 2 4

exemple 210 2.2.

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

Question 62-14 : 3 4 2 4 1 2

exemple 214 3, 4.3, 4.

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

Question 62-15 : 1 2 2 4 3 4

.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 218 1.1.

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

Question 62-16 : 3 2 2 4 1

.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 222 3.3.

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

Question 62-17 : 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

. ra reversal . 1014 exemple 226 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 62-18 : 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 230 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 62-19 : 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 234 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 62-20 : 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 238 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 62-21 : Coordinated resolution advisories coordinated traffic advisories resolution advisories coordinated with the atc instructions traffic advisories coordinated with the atc instructions


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

Question 62-22 : I is incorrect ii is incorrect i is correct ii is correct i is correct ii is incorrect 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.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 246 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 62-23 : 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 250 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 62-24 : I is incorrect ii is correct i is incorrect ii is incorrect i is correct ii is incorrect i is correct 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.also you will have an aural warning if parking brake is still on it makes sense exemple 254 i is incorrect, ii is correct.i is incorrect, ii is correct.

The stick pusher is a part of the ?

Question 62-25 : Stall protection system automatic flight control system afcs flight envelope protection fep system stall warning system sws

.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 258 stall protection system.stall protection system.

The egpws ?

Question 62-26 : 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 262 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 62-27 : 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 266 2, 3.2, 3.

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

Question 62-28 : No longer operate normally operate in the traffic advisory ta mode only operate normally operate in the resolution advisory ra mode only

exemple 270 no longer operate normally.no longer operate normally.

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

Question 62-29 : 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 274 1, 2, 4.1, 2, 4.

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

Question 62-30 : 1 3 1 2 3 4 3 4 1 2

exemple 278 1, 3.1, 3.

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

Question 62-31 : Stall windshear gpws tcas stall tcas gpws windshear tcas stall windshear gpws gpws stall tcas windshear

exemple 282 stall, windshear, gpws, tcas.stall, windshear, gpws, tcas.

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

Question 62-32 : 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 286 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 62-33 : 1 2 3 1 2 2 2 4

.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 290 1, 2, 3.1, 2, 3.

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

Question 62-34 : 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 294 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 62-35 : 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 298 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 62-36 : 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 302 2.2.

To stop the warning generated by the overspeed warning system the pilot may .1 ?

Question 62-37 : 3 1 2 3 1 3 2 3

Cqb15 may 2012 exemple 306 3.3.

To warn the flight crew an overspeed warning system can use .1 an aural ?

Question 62-38 : 1 1 2 2 1 2 3

Cqb15 august 2012..the overspeed warning system provides an audible overspeed warning in the event aircraft speed exceeds a mach or airspeed limit the overspeed warning hom is activated by the air data computers when the position of the airspeed pointer and the maximum allowable pointer barber pole coincide .the overspeed warning horn will sound under.any of the following conditions . airspeed exceeds vmo . mach exceeds mmo.notice .for large aeroplanes an aural warning must be associated to the overspeed warning if an electronic display is used exemple 310 1.1.

When a tcas resolution advisory ra is generated the required vertical speed ?

Question 62-39 : Is displayed on the vsi shows a red arc on the vsi as your target rate of climb/ descent is vocally announced takes account of a stall margin

exemple 314 is displayed on the vsi.is displayed on the vsi.

A tcas generates traffic advisory ta or resolution advisory ra according to ?

Question 62-40 : Time speed distance flight level

exemple 318 time.time.


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