Question 77-1 : When a tcas resolution advisory ra climb instruction is generated the required vertical speed range displayed on the vertical speed indicator ? [ Quiz topography ]

Question 77-2 : The aural alert s associated with the mode 4 of the gpws unsafe terrain clearance while not in the landing configuration is are 1 too low gear 2 too low terrain 3 too low flaps 4 pull up the combination that regroups all of the correct statements is ?

Question 77-3 : When enhanced gpws egpws terrain is displayed if the computed aircraft position becomes less accurate ?

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

Question 77-4 : With a tcas ii when a corrective resolution is generated ?

Question 77-5 : At high angles of attack and according to the type of aeroplane the stall protection system can 1 extend the flaps to the full position2 increase thrust3 inhibit the pitch trim to the down directionthe combination that regroups all of the correct statements is ?

2.

Cqb15 may 2012only 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 attitudethe 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

Question 77-6 : To stop the warning generated by the overspeed warning system the pilot may 1 push the inhibit aural warning button2 switch off the overspeed warning system3 reduce the speedthe combination that regroups all of the correct statements is ?

3.

Cqb15 may 2012

Question 77-7 : To warn the flight crew an overspeed warning system can use 1 an aural warning2 a stick shaker connected to the control column3 a vibration device connected to the autothrottlethe combination that regroups all of the correct statements is ?

1.

Cqb15 august 2012the 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 coincidethe overspeed warning horn will sound underany of the following conditions airspeed exceeds vmo mach exceeds mmonotice for large aeroplanes an aural warning must be associated to the overspeed warning if an electronic display is used

Question 77-8 : When a tcas resolution advisory ra is generated the required vertical speed ?

Is displayed on the vsi.

Question 77-9 : A tcas generates traffic advisory ta or resolution advisory ra according to ?

Time.

Question 77-10 : For an aircraft efis equipped 1 the nd displays flight director command bars 2 the pfd displays the altimeter setting 3 the nd displays the attitude of the aircraft 4 the flight mode annunciator is part of the nd the combination regrouping all the correct statements is ?

2.

Img967

Question 77-11 : The primary flight display pfd displays information dedicated to ?

Piloting.

Question 77-12 : According to cs 25 section 3 concerning the electronic display systems the whitecyan colours are associated with the following indication ?

Armed mode.

For electronic display systems engaged mode selected data greenarmed mode fixed reference symbols current data whiteselected heading active routeflight plan magenta

Question 77-13 : According to cs25 concerning the electronic display systems the colour associated with an engaged mode is ?

Green.

For electronic display systems engaged mode selected data greenarmed mode fixed reference symbols current data whiteselected heading active routeflight plan magenta

Question 77-14 : The primary flight display pfd of an efis equipped aircraft displays the following parameters 1 radio height 2 ias 3 localizer and glide slope deviation pointers 4 flight director modes 5 autopilot modes the combination that regroups all of the correct statements is ?

1 2 3 4 5.

Question 77-15 : When two waypoints are entered on the fms flight plan page a track between the two fixes is computed and can be displayed on the navigation map display nd this leg created is ?

A great circle arc.

Fms determines the shortest track between the two fixes and the shortest track is a great circle arc

Question 77-16 : Concerning the electronic display systems the green colour is associated with the following indication ?

Engaged mode.

For electronic display systems engaged mode selected data greenarmed mode fixed reference symbols current data whiteselected heading active routeflight plan magenta

Question 77-17 : The primary flight display pfd of an efis equipped aircraft can display information relative to the following conditions ?

Question 77-18 : According to amc 25 11 concerning the electronic display systems when exceeding the limits of the flight envelope the colour accepted to alert the flight crew is ?

Red.

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 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

Question 77-19 : The primary flight display pfd of an efis equipped aircraft displays the following parameters ?

Question 77-20 : The navigation display nd of an efis equipped aircraft can display the following data ?

Flight plan weather radar terrain map intruding traffics.

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

Question 77-21 : An efis includes the following components ?

Symbol generator display unit s control panel.

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' overallthe 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

Question 77-22 : According to amc 25 11 concerning the electronic display systems the colour associated with an armed mode is ?

White or cyan.

Question 77-23 : The navigation display nd modes can be 1 arc or map covering 45 degrees on either side of the instantaneous track 2 rose or map centered rose with current heading up 3 plan map orientated to true north the combination that regroups all of the correct statements is ?

1 2 3.

Question 77-24 : On the navigation display nd of an efis equipped aircraft the colours used are ?

Magenta or white for the active waypoint to waypoint green for light precipitation.

Answer is from easa cs 25 amendement 12 1024

Question 77-25 : According to cs25 concerning the electronic display systems the colours used are ?

Red for flight enveloppe and system limits green for autopilot or flight director engaged modes.

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 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

Question 77-26 : According to cs25 concerning the electronic display systems the colour associated with a caution type alert is ?

Amber or yellow.

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

Question 77-27 : The sideslip indication diplayed on the pfd primary flight display is generated by ?

The inertial system.

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

Question 77-28 : On a electronic flight instrument systems efis the following egt parameters may be displayed 1 instantaneous egt2 commanded egt3 maximum continuous egt limit4 maximum take off egt limitthe combination that regroups all of the correct statements is ?

1 3 4.

Cqb15 may 2012electronic 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 systemsengine parameters crew warningsaircraft 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 arounddisplayed red maximum takeoff limit or start limit exceededon ground after both engines are shut down red box indicates an exceedance has occurred 5 exhaust gas temperature egt indications displayed white normal operating rangedisplayed amber maximum continuous limit exceeded color change inhibitedfor up to 5 minutes during takeoff or go arounddisplayed red maximum takeoff limit or start limit exceeded

Question 77-29 : The following information can be displayed on the navigation display nd with the map or arc mode 1 selected and current heading2 next waypoint distance3 weather radar information4 autopilot mode5 landing capacitythe combination regrouping all the correct statements is ?

1 2 3.

Revised ecqb03 july 2016the 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 andor 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

Question 77-30 : On an electronic flight instrument system efis the following fuel data may be displayed 1 fuel density2 fuel quantity in each tank3 total fuel quantity4 fuel temperaturethe combination regrouping all the correct statements is ?

2 3 4.

Cqb15 august 2012

Question 77-31 : The following information can be displayed on a primary flight display pfd 1 attitude2 maximum airspeed warning3 selected heading4 decision height5 ground speedthe combination regrouping all the correct statements is ?

1 2 3 4.

Cqb15 august 2012the following information can be displayed on the primary flight display pfd unit flight mode annunciation basic t attitude ias altitude headingtrack 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 messagesfor large aeroplane atpl learning objectives only the pfd can also displayed take off and landing reference speeds minimum airspeed lower selectable airspeed mach number

Question 77-32 : The following information can be displayed on a primary flight display pfd 1 ias2 vertical speed3 tas4 selected airspeed5 radio altitudethe combination that regroups all of the correct statements is ?

1 2 4 5.

Ecqb03 july 2016the following information can be displayed on the primary flight display pfd unit flight mode annunciation basic t attitude ias altitude headingtrack 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 messagesfor large aeroplane atpl learning objectives only the pfd can also displayed take off and landing reference speeds minimum airspeed lower selectable airspeed mach number

Question 77-33 : The following information can be displayed on a primary flight display pfd 1 traffic information from the acas2 flight path vector3 altitude4 ils indications5 lower selectable airspeedthe combination that regroups all of the correct statements is ?

2 3 4 5.

Ecqb03 july 2016the following information can be displayed on the primary flight display pfd unit flight mode annunciation basic t attitude ias altitude headingtrack 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 messagesfor large aeroplane atpl learning objectives only the pfd can also displayed take off and landing reference speeds minimum airspeed lower selectable airspeed mach number

Question 77-34 : The following information can be displayed on the navigation display nd with the map or arc mode 1 selected and current track2 decision height3 tas4 ground speed5 wind direction and speedthe combination that regroups all of the correct statements is ?

1 3 4 5.

Ecqb03 july 2016the 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 andor 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

Question 77-35 : On an electronic flight instrument system efis the following egt parameters may be displayed 1 instantaneous egt2 maximum continuous egt3 maximum takeoff egt limit4 maximum start egt limitthe combination that regroups all of the correct statements is ?

1 2 3 4.

Ecqb03 july 2016warning this question is in the database n°995 with the following statements 1 instantaneous egt2 commanded egt3 maximum continuous egt limit4 maximum take off egt limiin 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 systemsengine parameters crew warningsaircraft 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 arounddisplayed red maximum takeoff limit or start limit exceededon ground after both engines are shut down red box indicates an exceedance has occurred 5 exhaust gas temperature egt indications displayed white normal operating rangedisplayed amber maximum continuous limit exceeded color change inhibitedfor up to 5 minutes during takeoff or go arounddisplayed red maximum takeoff limit or start limit exceeded

Question 77-36 : What can be interpreted from the flight path vector fpv ?

Glide angle.

Question 77-37 : Except for airplanes under 57 t airworthiness certificate of which is subsequent to 31 march 1998 a flight data recording system must be able to store the recorded data for a minimum of the last ?

25 hours.

Question 77-38 : The cvr cockpit voice recorder includes 1 a microphone2 a recorder in compliance with the shock and fire resistance standards3 an independent battery4 a flight data recorderthe combination regrouping all the correct statements is ?

1 2.

Eu ops 1700 cockpit voice recorders a cockpit voice recorderwhich with reference to a time scale records voice communications transmitted from or received on the flight deck by radio the aural environment of the flight deck voice communications of flight crew members on the flight deck using the aeroplane's interphone system voice or audio signals identifying navigation or approach aids voice communications of flight crew members on the flight deck using the public address system if installedin fact a cockpit voice recorder needs plenty of microphone the cvr must be crash resistantthe cvr doesn't have a battery his power comes from the airplane electrical systema flight data recorder is similar to a cvr unless it records data time altitude attitude heading airspeed engine power the cvr must be fitted with a device to assist in locating it in water but the battery of this device is not a battery for the cvr work

Question 77-39 : On a modern transport category aeroplane the engagement of the automatic pilot is checked on the display of ?

The pfd primary flight display .

Question 77-40 : According to cs25 a cvr cockpit voice recorder must record 1 communications transmitted from or received in the aeroplane by radio 2 communications of flight crew members on the flight deck via the area microphone 3 communications of flight crew members on the flight deck using the aeroplane's ?

1 2 3 4.