Question 76-1 : The gpws cpu central processing unit is able to detect 1 excessive descent rate2 excessive rate of terrain closure3 excessive angle of attack4 too high descent attitude5 loss of altitude after take off6 abnormal gearflaps configuration7 excessive glidepath deviationthe combination that ? [ Mandatory landing ]

Question 1

Question 76-1 : The gpws cpu central processing unit is able to detect 1 excessive descent rate2 excessive rate of terrain closure3 excessive angle of attack4 too high descent attitude5 loss of altitude after take off6 abnormal gearflaps configuration7 excessive glidepath deviationthe combination that ? [ Mandatory landing ]

1 2 5 6 7

Answer

That advises the pilot to avoid certain deviations from the current vertical rate but does not require any change to be made to that rate.

A corrective 'resolution advisory' ra is a 'resolution advisory' asking the pilot to modify effectively the vertical speed of his aircraft only on a vertical plan armetiz the answer is 'ra is asking the pilot to modify effectively the vertical speed of his aircraft' but when i choose this answer i get an errori don't understandyes apologies for that it was not clear we were talking about 'corrective ra' instead of a 'prevenive ra'find hereafter the icao recommandations icao annex 10 vol iv aeronautical telecommunications surveillance and collision avoidance systems resolution advisory ra an indication given to the flight crew recommending a a manoeuvre intended to provide separation from all threats or b a manoeuvre restriction intended to maintain existing separationcorrective ra a resolution advisory that advises the pilot to deviate from the current flight pathpreventive ra a resolution advisory that advises the pilot to avoid certain deviations from the current flight path but does not require any change in the current flight pathtraffic advisory ta an indication given to the flight crew that a certain intruder is a potential threat

Asking the pilot to modify effectively the vertical speed of his aircraft. asking the pilot to modify the heading of his aircraft. asking the pilot to modify the speed of his aircraft.

Answer

A red full square.

Img956resolution advisory ra a warning issued by the traffic collision avoidance system tcas indicating an immediate threat of collision with another aircraftthis warning takes the form of a command to perform a vertical avoidance maneuver eg climb climb

Answer

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 offin 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 an aural warning when you intend to take off while the parking brake is still on

I is incorrect, ii is incorrect. i is correct, ii is incorrect. i is incorrect, ii is correct.

Answer

An electronic map of the world giving ground elevation.

Enhanced gpws with the terrain threat display uses essentially an electronic map of the world giving ground elevation and information from the aircraft's navigational system be that insgps 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

Answer

2 3.

Excessive deviation below selected altitude warning is given by the altitude alert systempredictive 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 flapsgear deployed or retracted

Answer

Immediatly initiate the required manoeuvre.

Answer

Caution.

cs 251322 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

Answer

2.

The stall warning computer uses the angle of attack and slatsflaps configuration the stall warning is inhibited when the aeroplane is on the ground

Answer

With the flaps and landing gear in any normal position.

The stall warning computer uses the angle of attack and slatsflaps configuration the stall warning is inhibited when the aeroplane is on the ground

Answer

2 4 5.

Egpws enhanced ground proximity warning systemenhanced gpws uses essentially an electronic map of the world giving ground elevation and information from the aircraft's navigational system insgps 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 aircraftthe operation of the egpws is governed by laws taking the aircraft height into account as well as the descent rate and the aircraft configuration flapsgear deployed or retracted but it can not provide an abnormal take off configuration warningpredictive windshear alert can not be performed by the egpws but when windshear occurs the egpws can warn the crew

exemple 220: 2 4 5 — 1, 2, 3, 5. 1, 3, 4. 2, 3, 4, 5.

Answer

1 2 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 safetythe flight warning system generates alerts and warnings for the following situations engine and airframe systems malfunctions aerodynamic limits exceeded presence of external hazards

exemple 224: 1 2 5 — 1, 2, 4. 1, 4. 2, 4, 5.

Answer

1 4.

The stall warning computer uses the angle of attack and slatsflaps configuration the stall warning is inhibited when the aeroplane is on the ground

exemple 228: 1 4 — 1, 2, 4. 2, 3, 4. 1, 2.

Answer

1 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 existstcas operation is independent of ground based air traffic controlthe tcas ii has inputs from the radio altimeter in order to gradually inhibit the resolution advisories ras when getting closer to the ground

Answer

'glideslope'.

Gpws mode 1 sink rate pull upmode 2 terrain pull upmode 3 don't sinkmode 4 too low gear too low flaps too low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

'sink rate'.

Gpws mode 1 sink rate pull upmode 2 terrain pull upmode 3 don't sinkmode 4 too low gear too low flaps too low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

'don't sink'.

Gpws mode 1 sink rate pull upmode 2 terrain pull upmode 3 don't sinkmode 4 too low gear too low flaps too low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

'terrain'.

Gpws mode 1 sink rate pull upmode 2 terrain pull upmode 3 don't sinkmode 4 too low gear too low flaps too low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

2 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 landingthe 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 altitudethe radio altimeter does not supply data to the altitude alert system

Answer

4.

The air data computer adc provides speed altitude and sink rate to the gpwsthe transponder is a receivertransmitter which will generate a reply signal upon proper interrogationautothrottle controls selected speed or n1angle of attack sensor is an input to the stall warning system not to the gpws

Answer

1.

Gpws mode 1 pull upmode 2 terrainmode 3 don't sinkmode 4 to low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

3.

Gpws mode 1 sink rate pull upmode 2 terrain pull upmode 3 don't sinkmode 4 too low gear too low flaps too low terrainmode 5 glideslopemode 6 bank anglemode 7 windshear

Answer

After a 'descend' ra when a reversal in the vertical manoeuvre sense is required.

Answer

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

Answer

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

Answer

Follow the tcas ra and inform the atc.

Answer

Coordinated resolution advisories.

Answer

I is incorrect ii is incorrect.

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 offin green the normal stablizer trim set for a boeing 737 at take off 1020also there is no automatique detection for a low brake pressure levelbefore take off or landing brake pressure can be monitored on a gauge in the cockpit 1021

Answer

I is correct ii is incorrect.

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 offin 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 levelbefore take off or landing brake pressure can be monitored on a gauge in the cockpit 1021

Answer

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 offin green the normal stablizer trim set for a boeing 737 at take off 1020also you will have an aural warning if parking brake is still on it makes sense

Answer

Stall protection system.

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 sufficientlya 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

Answer

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

Answer

2 3.

The stall warning computer uses the angle of attack and slatsflaps configuration the stall warning is inhibited when the aeroplane is on the ground

Answer

No longer operate normally.

Answer

1 2 4.

The stall warning computer uses the angle of attack and slatsflaps configuration the stall warning is inhibited when the aeroplane is on the ground

exemple 324: 1 2 4 — 1, 2, 3. 1, 3. 2, 4.

Answer

Stall windshear gpws tcas.

Question 2

Question 76-2 : On a tcas 2 traffic collision avoidance system the preventive 'resolution advisory' ra is a 'resolution advisory' ?

Question 3

Question 76-3 : On the display of a tcas 2 traffic alert and collision avoidance system a resolution advisory ra is generated for ?

Question 4

Question 76-4 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the stabiliser is not in a safe position for take offii an aural warning is given when the parking brake is still on ?

Question 5

Question 76-5 : The egpws may propose the terrain look ahead alerting functionthis function uses ?

Question 6

Question 76-6 : The gpws can warn the crew in case of 1 excessive deviation below selected altitude2 windshear3 excessive terrain closing ratethe combination that regroups all of the correct statements is ?

Question 7

Question 76-7 : Concerning the tcas 2 when receiving a resolution advisory ra crew members should ?

Question 8

Question 76-8 : According to cs25 concerning the electronic display systems the amberyellow colours are associated with the following alert ?

Question 9

Question 76-9 : The stall warning is inhibited 1 when the flaps are retracted2 when the aeroplane is on the ground3 when encountering a windshear4 upon receiving a gpws alertthe combination regouping all the correct statements is ?

Question 10

Question 76-10 : On a large aeroplane and according to the cs25 the stall warning system must provide an alarm with sufficient margin to prevent inadvertent stalling ?

Question 11

Question 76-11 : The gpws warns the crew in case of 1 excessive descent rate 2 excessive terrain closure rate 3 potential midair collision threat 4 serious midair collision threat 5 unsafe terrain clearance with landing gear not down the combination that regroups all of the correct statements is ?

1 2 5.

exemple 216: 1 2 5 — 1, 2, 3, 5. 1, 2, 4, 5. 4.

Question 12

Question 76-12 : The egpws may propose the following functions 1 abnormal take off configuration atc 2 terrain clearance floor tcf 3 predictive wind shear pws 4 terrain look ahead alerting 5 terrain alerting and display tad the combination regrouping all of the correct statements is ?

Question 13

Question 76-13 : The flight warning system fws 1 draws the attention of the crew to the existence of an abnormal condition2 gives indications to the crew to identify an abnormal condition3 transmits automatically to atc urgency messages4 can not generate alerts in case of engine malfunctions5 prioritises ?

Question 14

Question 76-14 : On a large aeroplane the input data of the stall warning system are 1 angle of attack2 weight3 bank angle4 configuration slats flaps the combination that regroups all of the correct statements is ?

Question 15

Question 76-15 : Concerning the tcas ii 1 neither advisory nor traffic display is provided for aircraft that do not have an operating transponder2 tcas ii operation is independent of ground based air traffic control3 tcas ii has feeds from the radioaltimeterthe combination that regroups all of the correct ?

Question 16

Question 76-16 : The aural alert associated with the mode 5 excessive deviation below glideslope of the gpws is ?

Question 17

Question 76-17 : The aural alert associated with the mode 1 excessive descent rate of the gpws is ?

Question 18

Question 76-18 : The aural alert associated with the mode 3 altitude loss after take off or go around of the gpws is ?

Question 19

Question 76-19 : The aural alert associated with the mode 2 excessive terrain closure rate of the gpws is ?

Question 20

Question 76-20 : The radio altimeter supplies data to the following system s 1 altitude alert system2 tcas3 gpws4 automatic landing systemthe combination that regroups all the correct statements is ?

Question 21

Question 76-21 : The input data to the gpws originate from the 1 transponder2 angle of attack sensor3 auto throttle system4 adcthe combination that regroups all of the correct statements is ?

Question 22

Question 76-22 : The main function s of a tcas is to 1 alert the crew to ground proximity2 alert the crew to possible conflicting traffic3 provide terrain alerting and display4 automatically resolve conflict when autopilot engagedthe combination that regroups all of the correct statements is ?

2.

exemple 260: 2 — 1, 3. 1, 2, 3, 4. 2, 4.

Question 23

Question 76-23 : The aural alert s associated with the mode 1 excessive descent rate of the gpws is are 1 'terrain'2 'don't sink'3 'sinkrate'4 'pull up'the combination that regroups all of the correct statements is ?

3 4.

Question 24

Question 76-24 : The aural alert s associated with the mode 3 altitude loss after take off or go around of the gpws is are 1 don't sink 2 sink rate 3 terrain 4 pull up the combination that regroups all of the correct statements is ?

Question 25

Question 76-25 : The aural alert s associated with the mode 5 excessive deviation below glideslope of the gpws is are 1 terrain 2 too low glideslope 3 glideslope 4 pull up the combination that regroups all of the correct statements is ?

Question 26

Question 76-26 : A tcas resolution advisory ra voice message 'climb climb now' repeated twice is generated ?

Question 27

Question 76-27 : When comparing a tcas traffic advisory ta and a resolution advisory ra which of the following statements is correct ?

Question 28

Question 76-28 : On a large aeroplane and according to the cs 25207 when the speed is reduced the stall warning must begin ?

Question 29

Question 76-29 : If a tcas resolution advisory ra requires an immediate descent while at the same time atc requests an immediate climb the crew should ?

Question 30

Question 76-30 : Your aircraft and an intruding traffic are tcas ii equipped your tcas can generate ?

Question 31

Question 76-31 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the elevator is not in a safe position for take offii an aural warning is given when the brake pressure is too low ?

Question 32

Question 76-32 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the stabiliser is not in a safe position for take offii an aural warning is given when the brake pressure is too low ?

Question 33

Question 76-33 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the elevator is not in a safe position for take offii an aural warning is given when the parking brake is still on ?

Question 34

Question 76-34 : The stick pusher is a part of the ?

Question 35

Question 76-35 : The egpws ?

Question 36

Question 76-36 : The stall warning computer of a large aeroplane uses the following data 1 pitch attitude2 angle of attack3 configuration slats flaps the combination that regroups all of the correct statements is ?

Question 37

Question 76-37 : When a tcas is operating a failure of the active transponder will cause the tcas to ?

Question 38

Question 76-38 : The stall warning system of a large aeroplane includes 1 an angle of attack sensor 2 a computer3 an independent pitot probe4 a transmitter of the flapslat position indicating systemthe combination that regroups all of the correct statements is ?

Question 39

Question 76-39 : The gpws receives data from the following systems 1 landing gear and flaps systems2 engine control computer fadec or ecu 3 radio altimeter4 tcasthe combination that regroups all of the correct statements is ?

1 3.

exemple 328: 1 3 — 1, 2, 3, 4. 3, 4. 1, 2.

Question 40

1 2 5 6 7

Question 76-2 : On a tcas 2 traffic collision avoidance system the preventive 'resolution advisory' ra is a 'resolution advisory' ?

That advises the pilot to avoid certain deviations from the current vertical rate but does not require any change to be made to that rate.

Question 76-3 : On the display of a tcas 2 traffic alert and collision avoidance system a resolution advisory ra is generated for ?

A red full square.

Question 76-4 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the stabiliser is not in a safe position for take offii an aural warning is given when the parking brake is still on ?

I is correct ii is correct.

Question 76-5 : The egpws may propose the terrain look ahead alerting functionthis function uses ?

An electronic map of the world giving ground elevation.

Question 76-6 : The gpws can warn the crew in case of 1 excessive deviation below selected altitude2 windshear3 excessive terrain closing ratethe combination that regroups all of the correct statements is ?

2 3.

Question 76-7 : Concerning the tcas 2 when receiving a resolution advisory ra crew members should ?

Immediatly initiate the required manoeuvre.

Question 76-8 : According to cs25 concerning the electronic display systems the amberyellow colours are associated with the following alert ?

Caution.

Question 76-9 : The stall warning is inhibited 1 when the flaps are retracted2 when the aeroplane is on the ground3 when encountering a windshear4 upon receiving a gpws alertthe combination regouping all the correct statements is ?

2.

Question 76-10 : On a large aeroplane and according to the cs25 the stall warning system must provide an alarm with sufficient margin to prevent inadvertent stalling ?

With the flaps and landing gear in any normal position.

Question 76-11 : The gpws warns the crew in case of 1 excessive descent rate 2 excessive terrain closure rate 3 potential midair collision threat 4 serious midair collision threat 5 unsafe terrain clearance with landing gear not down the combination that regroups all of the correct statements is ?

1 2 5.

Question 76-12 : The egpws may propose the following functions 1 abnormal take off configuration atc 2 terrain clearance floor tcf 3 predictive wind shear pws 4 terrain look ahead alerting 5 terrain alerting and display tad the combination regrouping all of the correct statements is ?

2 4 5.

1 2 5.

Question 76-14 : On a large aeroplane the input data of the stall warning system are 1 angle of attack2 weight3 bank angle4 configuration slats flaps the combination that regroups all of the correct statements is ?

1 4.

1 2 3.

Question 76-16 : The aural alert associated with the mode 5 excessive deviation below glideslope of the gpws is ?

'glideslope'.

Question 76-17 : The aural alert associated with the mode 1 excessive descent rate of the gpws is ?

'sink rate'.

Question 76-18 : The aural alert associated with the mode 3 altitude loss after take off or go around of the gpws is ?

'don't sink'.

Question 76-19 : The aural alert associated with the mode 2 excessive terrain closure rate of the gpws is ?

'terrain'.

Question 76-20 : The radio altimeter supplies data to the following system s 1 altitude alert system2 tcas3 gpws4 automatic landing systemthe combination that regroups all the correct statements is ?

2 3 4.

Question 76-21 : The input data to the gpws originate from the 1 transponder2 angle of attack sensor3 auto throttle system4 adcthe combination that regroups all of the correct statements is ?

4.

Question 76-22 : The main function s of a tcas is to 1 alert the crew to ground proximity2 alert the crew to possible conflicting traffic3 provide terrain alerting and display4 automatically resolve conflict when autopilot engagedthe combination that regroups all of the correct statements is ?

2.

Question 76-23 : The aural alert s associated with the mode 1 excessive descent rate of the gpws is are 1 'terrain'2 'don't sink'3 'sinkrate'4 'pull up'the combination that regroups all of the correct statements is ?

3 4.

Question 76-24 : The aural alert s associated with the mode 3 altitude loss after take off or go around of the gpws is are 1 don't sink 2 sink rate 3 terrain 4 pull up the combination that regroups all of the correct statements is ?

1.

Question 76-25 : The aural alert s associated with the mode 5 excessive deviation below glideslope of the gpws is are 1 terrain 2 too low glideslope 3 glideslope 4 pull up the combination that regroups all of the correct statements is ?

3.

Question 76-26 : A tcas resolution advisory ra voice message 'climb climb now' repeated twice is generated ?

After a 'descend' ra when a reversal in the vertical manoeuvre sense is required.

Question 76-27 : When comparing a tcas traffic advisory ta and a resolution advisory ra which of the following statements is correct ?

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

Question 76-28 : On a large aeroplane and according to the cs 25207 when the speed is reduced the stall warning must begin ?

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

Question 76-29 : If a tcas resolution advisory ra requires an immediate descent while at the same time atc requests an immediate climb the crew should ?

Follow the tcas ra and inform the atc.

Question 76-30 : Your aircraft and an intruding traffic are tcas ii equipped your tcas can generate ?

Coordinated resolution advisories.

Question 76-31 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the elevator is not in a safe position for take offii an aural warning is given when the brake pressure is too low ?

I is incorrect ii is incorrect.

Question 76-32 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the stabiliser is not in a safe position for take offii an aural warning is given when the brake pressure is too low ?

I is correct ii is incorrect.

Question 76-33 : Which of these statements about the activation of the take off warning when a take off is initiated are correct or incorrect i an aural warning is given when the elevator is not in a safe position for take offii an aural warning is given when the parking brake is still on ?

I is incorrect ii is correct.

Question 76-34 : The stick pusher is a part of the ?

Stall protection system.

Question 76-35 : The egpws ?

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

Question 76-36 : The stall warning computer of a large aeroplane uses the following data 1 pitch attitude2 angle of attack3 configuration slats flaps the combination that regroups all of the correct statements is ?

2 3.

Question 76-37 : When a tcas is operating a failure of the active transponder will cause the tcas to ?

No longer operate normally.

Question 76-38 : The stall warning system of a large aeroplane includes 1 an angle of attack sensor 2 a computer3 an independent pitot probe4 a transmitter of the flapslat position indicating systemthe combination that regroups all of the correct statements is ?

1 2 4.

Question 76-39 : The gpws receives data from the following systems 1 landing gear and flaps systems2 engine control computer fadec or ecu 3 radio altimeter4 tcasthe combination that regroups all of the correct statements is ?

1 3.

Question 76-40 : For compatibility between the different components of a flight warning system the priority from the highest to the lowest is ?

Stall windshear gpws tcas.