The stall warning system of a large aeroplane includes .1 an angle of attack ? [ Quiz topography ]

Question 77-1 : 1 2 4 1 2 3 1 3 2 4

exemple 177 1, 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 1, 2, 4.

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

Question 77-2 : 1 3 1 2 3 4 3 4 1 2

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

Question 77-3 : Stall windshear gpws tcas stall tcas gpws windshear tcas stall windshear gpws gpws stall tcas windshear

exemple 185 Stall, windshear, gpws, tcas. — Stall, windshear, gpws, tcas.

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

Question 77-4 : 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

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

Question 77-5 : 1 2 3 1 2 2 2 4

exemple 193 1, 2, 3. — 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 1, 2, 3.

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

Question 77-6 : 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 197 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 77-7 : 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 201 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 77-8 : 2 1 2 1 3 1 2 3

exemple 205 2. — 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 2.

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

Question 77-9 : 3 1 2 3 1 3 2 3

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

Question 77-10 : 1 1 2 2 1 2 3

exemple 213 1. — 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 1.

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

Question 77-11 : 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 217 Is displayed on the vsi. — Is displayed on the vsi.

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

Question 77-12 : Time speed distance flight level

For an aircraft efis equipped . 1 the nd displays flight director command bars. ?

Question 77-13 : 2 2 4 1 3 1 4

The primary flight display pfd displays information dedicated to ?

Question 77-14 : Piloting weather situation engines and alarms systems

According to cs 25 section 3 concerning the electronic display systems the ?

Question 77-15 : Armed mode engaged mode warning caution

exemple 233 Armed mode. — Admin .for electronic display systems .engaged mode selected data green .armed mode fixed reference symbols current data white .selected heading active route/flight plan magenta Armed mode.

According to cs25 concerning the electronic display systems the colour ?

Question 77-16 : Green white magenta amber

exemple 237 Green. — Admin .for electronic display systems .engaged mode selected data green .armed mode fixed reference symbols current data white .selected heading active route/flight plan magenta Green.

The primary flight display pfd of an efis equipped aircraft displays the ?

Question 77-17 : 1 2 3 4 5 2 5 1 2 3 5 3 4

When two waypoints are entered on the fms flight plan page a track between the ?

Question 77-18 : A great circle arc a rhumb line two great circle arcs joined by a straight segment two rhumb lines joined by a straight segment

exemple 245 A great circle arc. — Fms determines the shortest track between the two fixes and the shortest track is a great circle arc A great circle arc.

According to cs25 concerning the electronic display systems the green colour is ?

Question 77-19 : Engaged mode armed mode advisory status

Admin .for electronic display systems .engaged mode selected data green .armed mode fixed reference symbols current data white .selected heading active route/flight plan magenta

The primary flight display pfd of an efis equipped aircraft can display ?

Question 77-20 : Altitude capture tcas resolution advisory autopilot and flight director mode changes altitude capture braking system autopilot and flight director mode changes low engine oil pressure terrain alerts windshear detection pressurization failure altitude capture tcas resolution advisory

exemple 253 Altitude capture, tcas resolution advisory, autopilot and flight director mode changes. — . 1016. 1015. Altitude capture, tcas resolution advisory, autopilot and flight director mode changes.

According to amc 25 11 concerning the electronic display systems when exceeding ?

Question 77-21 : Red amber yellow magenta

exemple 257 Red. — 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 . note green is usually used to indicate 'normal' conditions safe operation therefore it is not an appropriate colour for an advisory alert an advisory alert is used to indicate a 'non normal' condition Red.

The primary flight display pfd of an efis equipped aircraft displays the ?

Question 77-22 : Ias attitude altitude heading attitude heading altitude systems information altitude attitude heading engine parameters attitude heading ias navigation map in plan layout mode

exemple 261 Ias, attitude, altitude, heading. — . 1016. Ias, attitude, altitude, heading.

The navigation display nd of an efis equipped aircraft can display the ?

Question 77-23 : Flight plan weather radar terrain map intruding traffics flight plan engine failure navaids resolution advisories terrain map navaid bearings flight director active modes intruding traffics altitude autopilot active modes weather radar

exemple 265 Flight plan, weather radar, terrain map, intruding traffics. — . 1007.flight plan is the magenta line track via tau and col vor tcas symbols intruding traffics are white lozenge . 1008.weather radar mode . 1009.terrain map Flight plan, weather radar, terrain map, intruding traffics.

An efis includes the following components ?

Question 77-24 : Symbol generator display unit s control panel fms symbol generator display unit s display unit s only adc inertial navigation computer display unit s

exemple 269 Symbol generator, display unit(s), control panel. — Admin .symbol generators provide the analogue discrete and digital signal interfaces between an aircraft's systems the display units and the control panel and they also perform symbol generation monitoring power control and the main control functions of the 'efis' overall .the display units may be cathode ray tubes crt's or liquid crystal displays lcd's lcd's have the advantage of being smaller and generate less heat therefore need less cooling the pfd and nd are usually identical units to facilitate spares commonality and are often interchangeable with the systems display units eicas or ecam .a control panel is provided for each efis system Symbol generator, display unit(s), control panel.

According to amc 25 11 concerning the electronic display systems the colour ?

Question 77-25 : White or cyan green yellow magenta

exemple 273 White or cyan. — White or cyan.

The navigation display nd modes can be . 1 arc or map covering 45 degrees on ?

Question 77-26 : 1 2 3 1 2 1 3 2 3

On the navigation display nd of an efis equipped aircraft the colours used are ?

Question 77-27 : Magenta or white for the active waypoint to waypoint green for light precipitation magenta or red for the active waypoint to waypoint amber for medium precipitation white or blue for the active waypoint to waypoint red for medium precipitation amber or white for the active waypoint to waypoint yellow for high precipitation

exemple 281 Magenta or white for the active waypoint (to waypoint), green for light precipitation. — Admin .answer is from easa cs 25 amendement 12. 1024 Magenta or white for the active waypoint (to waypoint), green for light precipitation.

According to cs25 concerning the electronic display systems the colours used are ?

Question 77-28 : Red for flight enveloppe and system limits green for autopilot or flight director engaged modes red for warnings magenta for autopilot or flight director engaged modes red for caution abnormal sources white for flight enveloppe limits amber for the system limits white for autopilot or flight director engaged modes

exemple 285 Red for flight enveloppe and system limits, green for autopilot or flight director engaged modes. — 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 . note green is usually used to indicate 'normal' conditions safe operation therefore it is not an appropriate colour for an advisory alert an advisory alert is used to indicate a 'non normal' condition Red for flight enveloppe and system limits, green for autopilot or flight director engaged modes.

According to cs25 concerning the electronic display systems the colour ?

Question 77-29 : Amber or yellow red white magenta

exemple 289 Amber or yellow. — . 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 Amber or yellow.

The sideslip indication diplayed on the pfd primary flight display is generated ?

Question 77-30 : The inertial system the automatic flight control system afcs the yaw damper the stall protection system

exemple 293 The inertial system. — Admin .since the airplane sideslip angle is the difference between the airplane yaw angle and the direction of the velocity the sideslip angle can be calculated if both the attitude and velocity of the airplane are known inertial navigation systems ins could provide these values by integrating gyro measurements to get the attitude and integrating accelerometer measurements with gravity compensation to get the velocity The inertial system.

On a electronic flight instrument systems efis the following egt parameters may ?

Question 77-31 : 1 3 4 1 4 1 2 3 4 1 2 3

exemple 297 1, 3, 4. — Cqb15 may 2012 ..electronic flight instrument systems efis is composed by the primary flight display pfd or the electronic attitude director indicator eadi the navigation display nd or the electronic horizontal situation indicator ehsi and the engine parameters crew warnings aircraft systems procedure and mission display systems .engine parameters crew warnings aircraft systems and procedures display systems are . multi function display unit mfdu . engine indication and crew alerting systems eicas . engine and warning display ewd . electronic centralised aircraft monitor ecam . 1028. 1 exhaust gas temperature egt redlines .displayed red maximum takeoff egt limit . 2 exhaust gas temperature egt amber bands .displayed amber lower end of band displays maximum continuous egt limit . 3 exhaust gas temperature egt start limit lines .displayed red until the engine achieves stabilized idle approximately 59%.n2 . 4 exhaust gas temperature egt readouts digital .displayed white normal operating range degrees c .displayed amber maximum continuous limit exceeded color change inhibited for up to 5 minutes during takeoff or go around.displayed red maximum takeoff limit or start limit exceeded.on ground after both engines are shut down red box indicates an exceedance has occurred. 5 exhaust gas temperature egt indications .displayed white normal operating range .displayed amber maximum continuous limit exceeded color change inhibited.for up to 5 minutes during takeoff or go around.displayed red maximum takeoff limit or start limit exceeded 1, 3, 4.

The following information can be displayed on the navigation display nd with ?

Question 77-32 : 1 2 3 2 3 4 1 2 3 4 1 4 5

exemple 301 1, 2, 3. — Revised ecqb03 july 2016 ..the following information that can be displayed with the map or arc mode on a navigation display nd unit . selected and current track . selected and current heading magnetic or true north reference . cross track error . origin and destination airport with runway selected . bearings to or from the tuned and selected stations . active and/or secondary flight plan . range marks . ground speed . tas and ground speed . wind direction and speed . next waypoint distance and estimated time of arrival . additional navigation facilities sta waypoint wpt and airports arpt . weather radar information . traffic information from the acas tcas . terrain information from the taws or htaws egpws . failure flags and messages 1, 2, 3.

On an electronic flight instrument system efis the following fuel data may be ?

Question 77-33 : 2 3 4 1 2 3 2 3 1 2 3 4

exemple 305 2, 3, 4. — Cqb15 august 2012 2, 3, 4.

The following information can be displayed on a primary flight display pfd .1 ?

Question 77-34 : 1 2 3 4 1 2 4 5 1 2 5 1 3 5

exemple 309 1, 2, 3, 4. — Cqb15 august 2012 ..the following information can be displayed on the primary flight display pfd unit . flight mode annunciation. basic t attitude ias altitude heading/track indications . vertical speed. maximum airspeed warning. selected airspeed. speed trend vector. selected altitude. current barometric reference. steering indications fd command bars . selected heading. flight path vector fpv . radio altitude. decision height. ils indications. acas tcas indications. failure flags and messages .for large aeroplane atpl learning objectives only the pfd can also displayed . take off and landing reference speeds. minimum airspeed. lower selectable airspeed. mach number 1, 2, 3, 4.

The following information can be displayed on a primary flight display pfd .1 ?

Question 77-35 : 1 2 4 5 1 2 3 4 5 1 5 2 3 4

exemple 313 1, 2, 4, 5. — Ecqb03 july 2016 ..the following information can be displayed on the primary flight display pfd unit . flight mode annunciation. basic t attitude ias altitude heading/track indications . vertical speed. maximum airspeed warning. selected airspeed. speed trend vector. selected altitude. current barometric reference. steering indications fd command bars . selected heading. flight path vector fpv . radio altitude. decision height. ils indications. acas tcas indications. failure flags and messages .for large aeroplane atpl learning objectives only the pfd can also displayed . take off and landing reference speeds. minimum airspeed. lower selectable airspeed. mach number 1, 2, 4, 5.

The following information can be displayed on a primary flight display pfd .1 ?

Question 77-36 : 2 3 4 5 1 2 3 4 5 1 3 4 5 2 4 5

exemple 317 2, 3, 4, 5. — Ecqb03 july 2016 ..the following information can be displayed on the primary flight display pfd unit . flight mode annunciation. basic t attitude ias altitude heading/track indications . vertical speed. maximum airspeed warning. selected airspeed. speed trend vector. selected altitude. current barometric reference. steering indications fd command bars . selected heading. flight path vector fpv . radio altitude. decision height. ils indications. acas tcas indications. failure flags and messages .for large aeroplane atpl learning objectives only the pfd can also displayed . take off and landing reference speeds. minimum airspeed. lower selectable airspeed. mach number 2, 3, 4, 5.

The following information can be displayed on the navigation display nd with ?

Question 77-37 : 1 3 4 5 2 3 4 1 2 3 1 4 5

exemple 321 1, 3, 4, 5. — Ecqb03 july 2016 ..the following information that can be displayed with the map or arc mode on a navigation display nd unit . selected and current track . selected and current heading magnetic or true north reference . cross track error . origin and destination airport with runway selected . bearings to or from the tuned and selected stations . active and/or secondary flight plan . range marks . ground speed . tas and ground speed . wind direction and speed . next waypoint distance and estimated time of arrival . additional navigation facilities sta waypoint wpt and airports arpt . weather radar information . traffic information from the acas tcas . terrain information from the taws or htaws egpws . failure flags and messages 1, 3, 4, 5.

On an electronic flight instrument system efis the following egt parameters ?

Question 77-38 : 1 2 3 4 1 2 3 2 3 4 1 4

exemple 325 1, 2, 3, 4. — Ecqb03 july 2016 .warning this question is in the database n°995 with the following statements .1 instantaneous egt.2 commanded egt.3 maximum continuous egt limit.4 maximum take off egt limi.in this case the correct combination is 1 3 4 ..electronic flight instrument systems efis is composed by the primary flight display pfd or the electronic attitude director indicator eadi the navigation display nd or the electronic horizontal situation indicator ehsi and the engine parameters crew warnings aircraft systems procedure and mission display systems .engine parameters crew warnings aircraft systems and procedures display systems are . multi function display unit mfdu . engine indication and crew alerting systems eicas . engine and warning display ewd . electronic centralised aircraft monitor ecam . 1028. 1 exhaust gas temperature egt redlines .displayed red maximum takeoff egt limit . 2 exhaust gas temperature egt amber bands .displayed amber lower end of band displays maximum continuous egt limit . 3 exhaust gas temperature egt start limit lines .displayed red until the engine achieves stabilized idle approximately 59%.n2 . 4 exhaust gas temperature egt readouts digital .displayed white normal operating range degrees c .displayed amber maximum continuous limit exceeded color change inhibited for up to 5 minutes during takeoff or go around.displayed red maximum takeoff limit or start limit exceeded.on ground after both engines are shut down red box indicates an exceedance has occurred. 5 exhaust gas temperature egt indications .displayed white normal operating range .displayed amber maximum continuous limit exceeded color change inhibited.for up to 5 minutes during takeoff or go around.displayed red maximum takeoff limit or start limit exceeded 1, 2, 3, 4.

What can be interpreted from the flight path vector fpv ?

Question 77-39 : Glide angle speed trend pitch reference for resolution advisory ra intruder traffic with excessive vertical speed

Except for airplanes under 5 7 t airworthiness certificate of which is ?

Question 77-40 : 25 hours 30 minutes 60 minutes 10 hours

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