The primary flight display pfd of an efis equipped aircraft displays the ? [ Control visibility ]

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

exemple 164 1, 2, 3, 4, 5. — 1, 2, 3, 4, 5.

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

Question 64-2 : 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 168 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 64-3 : Engaged mode armed mode advisory status

exemple 172 Engaged 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 Engaged mode.

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

Question 64-4 : 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 176 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 64-5 : Red amber yellow magenta

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

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

Question 64-6 : Ias attitude altitude heading attitude heading altitude systems information altitude attitude heading engine parameters attitude heading ias navigation map in plan layout mode

exemple 184 Ias, attitude, altitude, heading. — . 1016. Ias, attitude, altitude, heading.

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

Question 64-7 : 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

. 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

An efis includes the following components ?

Question 64-8 : 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 192 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 64-9 : White or cyan green yellow magenta

exemple 196 White or cyan. — White or cyan.

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

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

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

Question 64-11 : 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 204 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 64-12 : 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 208 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 64-13 : Amber or yellow red white magenta

exemple 212 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 64-14 : The inertial system the automatic flight control system afcs the yaw damper the stall protection system

exemple 216 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 64-15 : 1 3 4 1 4 1 2 3 4 1 2 3

exemple 220 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 64-16 : 1 2 3 2 3 4 1 2 3 4 1 4 5

exemple 224 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 64-17 : 2 3 4 1 2 3 2 3 1 2 3 4

exemple 228 2, 3, 4. — Cqb15 august 2012 2, 3, 4.

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

Question 64-18 : 1 2 3 4 1 2 4 5 1 2 5 1 3 5

exemple 232 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 64-19 : 1 2 4 5 1 2 3 4 5 1 5 2 3 4

exemple 236 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 64-20 : 2 3 4 5 1 2 3 4 5 1 3 4 5 2 4 5

exemple 240 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 64-21 : 1 3 4 5 2 3 4 1 2 3 1 4 5

exemple 244 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 64-22 : 1 2 3 4 1 2 3 2 3 4 1 4

exemple 248 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 64-23 : 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 64-24 : 25 hours 30 minutes 60 minutes 10 hours

The cvr cockpit voice recorder includes .1 a microphone.2 a recorder in ?

Question 64-25 : 1 2 2 4 1 2 3 4 1 4

exemple 260 1, 2. — Eu ops 1 700 cockpit voice recorders .a cockpit voice recorder.which 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 installed .in fact a cockpit voice recorder needs plenty of microphone .the cvr must be crash resistant .the cvr doesn't have a battery his power comes from the airplane electrical system .a 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 1, 2.

On a modern transport category aeroplane the engagement of the automatic pilot ?

Question 64-26 : The pfd primary flight display the nd navigation display the ecam electronic centralized aircraft monitoring left screen the nd navigation display of the pilot in command

exemple 264 The pfd (primary flight display). — The pfd (primary flight display).

According to cs25 a cvr cockpit voice recorder must record . 1 communications ?

Question 64-27 : 1 2 3 4 1 2 2 4 1 3

The purpose of the flight data recorder fdr is to record specific parameters ?

Question 64-28 : 1 2 4 1 2 3 4 2 3 1 2

exemple 272 1, 2, 4. — Cqb15 may 2012 ..the following main parameters are recorded on the fdr . time or relative time count. attitude pitch and roll . airspeed. pressure altitude. heading. normal acceleration. propulsive/thrust power on each engine and cockpit thrust/power lever position if applicable. flaps/slats configuration or cockpit selection. ground spoilers and/or speed brake selection.the audio environment in the flight deck is recorded on the cvr cockpit voice recorder 1, 2, 4.

The purpose of the flight data recorder fdr is to record specific parameters ?

Question 64-29 : 1 2 3 4 2 3 4 2 3 1 2 3

exemple 276 1, 2, 3, 4. — Cqb15 may 2012 ..the following main parameters are recorded on the fdr . time or relative time count. attitude pitch and roll . airspeed. pressure altitude. heading. normal acceleration. propulsive/thrust power on each engine and cockpit thrust/power lever position if applicable. flaps/slats configuration or cockpit selection. ground spoilers and/or speed brake selection 1, 2, 3, 4.

The purpose of the cockpit voice recorder cvr is to record .1 communications ?

Question 64-30 : 1 2 1 3 1 3

exemple 280 1, 2. — Revised ecqb03 july 2016 ..the main parameters recorded on the cvr are . voice communications transmitted from or received on the flight deck. the aural environment of the flight deck. voice communication of flight crew members using the aeroplane's interphone system. voice or audio signals introduced into a headset or speaker. voice communication of flight crew members using the public address system when installed 1, 2.

The purpose of the cockpit voice recorder cvr is to record .1 the audio ?

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

exemple 284 1, 3. — Ecqb03 july 2016 ..a cockpit voice recorder 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 installed .in fact a cockpit voice recorder needs plenty of microphone .the cvr must be crash resistant .the cvr doesn't have a battery his power comes from the airplane electrical system .a 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 1, 3.

When pressing the push button event on the unit control of a flight data ?

Question 64-32 : A mark is set on the recording enabling this event to be found rapidly at a subsequent analysis the recording is stopped during one minute it erases the last minute recorded it records the flight data for 10 minutes

exemple 288 A mark is set on the recording, enabling this event to be found rapidly at a subsequent analysis. — A mark is set on the recording, enabling this event to be found rapidly at a subsequent analysis.

Regarding the operating system used for an on board documentation charts and ?

Question 64-33 : There are no certificate requirements the certification requirements are detailed in easa air ops the certification requirements are detailed in cs 23/25 the certification requirements are detailed in eurocae standards

exemple 292 There are no certificate requirements. — Revised ecqb03 july 2016 There are no certificate requirements.

In computing what is the function of a control unit ?

Question 64-34 : It ensures sequencing and co ordination of operations it performs complex arithmetic operations it performs simple arithmetic operations it is a user/computer interface

exemple 296 It ensures sequencing and co-ordination of operations. — It ensures sequencing and co-ordination of operations.

The central processing unit cpu of a computer essentially consists of .1 an ?

Question 64-35 : 1 2 3 2 3 1 1 3

exemple 300 1, 2, 3. — Admin .central processing unit cpu it is the heart or core component of cpu . 1030. its major structural components are control unit alu registers and cpu interconnections . control unit it controls the operations of the cpu and hence the computer system . arithmetic logic unit alu it performs the computers data processing functions. registers it forms the internal memory for cpu it provides storage internal to the cpu 1, 2, 3.

Regarding computer design architecture identify whether the following ?

Question 64-36 : 1 is correct and 2 is incorrect 1 and 2 are incorrect 1 is incorrect and 2 is correct 1 and 2 are correct

exemple 304 1 is correct and 2 is incorrect. — Admin .multitasking multiple tasks share common resources such as the same central processing unit cpu .multitasking method is a software solution .multiprocessing two or more central processing units cpus are used within a single computer .multiprocessing configuration is a hardware solution .a multiprocessing configuration results in more powerful performance than the multitasking method it's like having 2 engines instead of 1 1 is correct and 2 is incorrect.

Which of these statements about computer architecture are correct or incorrect ?

Question 64-37 : 1 is correct and 2 is incorrect 1 and 2 are incorrect 1 is incorrect and 2 is correct 1 and 2 are correct

exemple 308 1 is correct and 2 is incorrect. — Admin .multitasking multiple tasks share common resources such as the same central processing unit cpu .multitasking method is a software solution .multiprocessing two or more central processing units cpus are used within a single computer .multiprocessing configuration is a hardware solution .a multiprocessing configuration results in more powerful performance than the multitasking method it's like having 2 engines instead of 1 1 is correct and 2 is incorrect.

The software used to run the atsu application atc and aoc ?

Question 64-38 : Is certified according to an equipment certification standard ed12b do178b is only approved and tested by the manufacture only approved and tested by the company is certified according to cs25/cs29

exemple 312 Is certified according to an equipment certification standard (ed12b, do178b). — Admin .the software used to run the atsu air traffic service unit application for air traffic communications and airline operations communications atc and aoc is certified according to an equipment certification standard see document referenced rtca/do 178b or eurocae ed 12b .'software considerations in airborne systems and equipment certification' rtca/do 178b or eurocae ed 12b is a document dealing with the safety of software used in airborne systems .the failure conditions are categorized by their effects on the aircraft crew and passengers .eurocae document ed 12b was developed to establish software considerations for developers installers and users when the aircraft equipment design is implemented using software based techniques current and future avionics designs will make extensive use of this technology the eurocae document provides guidelines for establishing software levels software life cycle planning development verification configuration management and quality assurance disciplines to be used in software based systems .examples of airline operations communications aoc datalink messages . oooi out of the gate off the ground on the ground into the gate . load sheet. passenger information connecting flights . weather reports metar taf . maintenance reports engine exceedances . free text messages.examples of of air traffic communications atc datalink messages . departure clearance. oceanic clearance Is certified according to an equipment certification standard (ed12b, do178b).

Which document deals with considerations of software use in on board aircraft ?

Question 64-39 : Rtca/do 178b eurocae doc 178 jar 17 ec directive 485/2002

exemple 316 Rtca/do-178b — Admin .'software considerations in airborne systems and equipment certification' document referenced as rtca/do 178b or eurocae ed 12b Rtca/do-178b

Which of these statements about computer architecture are correct or incorrect ?

Question 64-40 : 1 is incorrect 2 is incorrect 1 is correct 2 is correct 1 is incorrect 2 is correct 1 is correct 2 is incorrect

exemple 320 1 is incorrect, 2 is incorrect. — Admin .the operating system os is a software that acts as intermediary between applications and computer hardware .hardware part includes the physical components of the computer cpu hard drive memory .at the exam this question also appears with the statements the software part includes the programmes that make up the operating system os and the hardware part includes the physical components of the computer which in this case is correct/correct 1 is incorrect, 2 is incorrect.

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