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Under easa regulations color code rules for efis displays the recommended color ? [ Analysis topography ]

Question 72-1 : White magenta green cyan

exemple 172 White.White.

Which of the following procedures must be adopted if on a flight under ifr ?

Question 72-2 : It may be continued using conventional navigation systems the pilot must determine the reason for the deviation and correct the error or switch off the faulty system it may be continued using navstar/gps prior to the next flight all systems must be checked it must be continued under vfr conditions

exemple 176 It may be continued using conventional navigation systems.It may be continued using conventional navigation systems.

What datum is used for the minimum descent altitude mda on a non precision ?

Question 72-3 : Barometric altitude if using differential gps d gps the altitude obtained from the d gps otherwise barometric altitude radar altitude gps altitude

.icao doc 8168 part ii section 3 chapter 1 .all fmcs and some stand alone basic gnss receivers provide altitude information however the pilot must still comply with the published minimum altitudes using the barometric altimeter where the fmc provides vertical information flight director guidance cues or coupled autopilot operation the pilot should follow the appropriate information or cues along with any necessary cross checks with the barometric altimetry

Which of the distances indicated will be shown on a basic vor/dme based area ?

Question 72-4 : 9 nm 14 nm 11 nm 8 nm

Admin .a basic rnav equipment will see a vor/dme at the position of the 'phantom station' . 2393.the distance indicated will be 9 nm the principle is to move the position of a real vor/dme to a desired position a useful position for your navigation exemple 184 9 nm.9 nm.

Erratic indications may be experienced when flying towards a basic vor/dme ?

Question 72-5 : When operating at low altitudes close to the limit of reception range from the reference station because under adverse conditions relative bearing to the phantom station other than 180°/360° it takes the computer more time to calculate the necessary information when in the cone of silence overhead the phantom station when the phantom station is out of range


Which of the following is one of the functions of the computer in a basic rnav ?

Question 72-6 : It transfers the information given by a vor/dme station into tracking and distance indications to any chosen phantom station/waypoint it checks the ground station accuracy using a built in test programme it automatically selects the two strongest transmitters for the area nav mode and continues working by memory in case one of the two necessary station goes off the air it calculates cross track information for ndb approaches

Area navigation rnav can be defined as a method of navigation that permits aircraft operation on any desired course within the coverage of station referenced navigation signals or within the limits of a self contained system capability or a combination of these ..the computer in a basic rnav system transfers the information given by a vor/dme station into tracking and distance indications to any chosen phantom station/waypoint .this is one of the rnav's computer main functions exemple 192 It transfers the information given by a vor/dme station into tracking and distance indications to any chosen phantom station/waypoint.It transfers the information given by a vor/dme station into tracking and distance indications to any chosen phantom station/waypoint.

Which one of the following lists information given by a basic vor/dme based ?

Question 72-7 : Crosstrack distance alongtrack distance distance to go aircraft position in latitude and longitude wind velocity true airspeed drift angle

.crosstrack xtk is the aircraft position relative to the path .crosstrack distance is the shortest distance shortest path between actual aircraft position and an active waypoint selected on the track even if we are not on the planned path .alongtrack distance distance to go is the remaining distance to reach the phantom waypoint while tracking inbound exemple 196 Crosstrack distance ; alongtrack distance (distance to go).Crosstrack distance ; alongtrack distance (distance to go).

Which of the following lists information required to input a waypoint or ?

Question 72-8 : Radial and distance from a vor/dme to the waypoint or 'phantom station' magnetic track and distance from the aircraft to the waypoint or 'phantom station' magnetic track and distance to a vor/dme from the waypoint or 'phantom station' radials from a minimum of two vors to the waypoint or 'phantom station'

Basic vor dme based area navigation system is a 2d rnav system the navigation computer of the simple 2d rnav system computes the navigational problems by simple sine and cosine mathematics solving the triangular problems .input data to the navigation computer is . actual vor radial and dme distance from selected vor station. radial and distance to phantom waypoint. desired magnetic track inbound to the phantom waypoint.a 2d rnav system is able to navigate in the horizontal plane only exemple 200 Radial and distance from a vor/dme to the waypoint or 'phantom station'.Radial and distance from a vor/dme to the waypoint or 'phantom station'.

Which of the distances indicated will be shown on a basic vor/dme based area ?

Question 72-9 : 12 nm 11 nm 10 nm 21 nm

Admin .brnav equipments are intended to help pilot so you will directly read the distance to reach the station . 2392 exemple 204 12 nm.12 nm.

Which one of the following inputs to an area navigation system r nav comes from ?

Question 72-10 : Vor/dme radial/distance magnetic heading inertial navigation system ins position pressure altitude

exemple 208 Vor/dme radial/distance.Vor/dme radial/distance.

Which one of the following sensors/systems is self contained ?

Question 72-11 : Inertial navigation system gps basic rnav system vor/dme

exemple 212 Inertial navigation system.Inertial navigation system.

In relation to area navigation systems rnav which of the following is an air ?

Question 72-12 : True airspeed inertial navigation system ins position vor/dme radial/distance doppler drift

exemple 216 True airspeed.True airspeed.

In the flight management computer fmc of the flight management system fms data ?

Question 72-13 : Performance database air data computer navigation database auto flight computers

Admin . 1952 exemple 220 Performance database.Performance database.

In the flight management computer fmc of the flight management system fms data ?

Question 72-14 : Performance database air data computer navigation database auto flight computer

Admin . 1952 exemple 224 Performance database.Performance database.

In the flight management computer fmc of the flight management system fms data ?

Question 72-15 : Navigation database air data database performance database auto flight database

exemple 228 Navigation database.Navigation database.

In the flight management computer fmc of the flight management system fms data ?

Question 72-16 : Navigation database air data computer performance database auto flight computers

Admin . 1953 exemple 232 Navigation database.Navigation database.

Under which of the following circumstances does a vor/dme area navigation ?

Question 72-17 : The system is receiving information from only one vor the system is receiving information from one vor and one dme the system is receiving information from one vor and two dmes the system is receiving information from the two dmes

Navigation computer vor/dme navigation .the vor/dme area navigation system computer calculates track error in relation to desired track this data can easily be interfaced with the automatic flight control and when done so enables the aircraft to automatically follow the flight plan loaded into the rnav computer .the computer is able to perform great circle navigation when receiving vor/dme stations if out of range the system reverts to dr dead reckoning mode where it updates the position by means of last computed wind and tas and heading information . operation in dr mode is time limited exemple 236 The system is receiving information from only one vor.The system is receiving information from only one vor.

In the flight management computer fmc of the flight management system fms data ?

Question 72-18 : Performance database air data computer navigation database auto flight computers

Admin . 1952 exemple 240 Performance database.Performance database.

Which facility associated with the ils may be identified by a two letter ?

Question 72-19 : Locator inner marker outer marker glide path

Reference data for airports four letter icao identifier . vor/dme station data three letter icao identifier . waypoint data five letter icao identifier exemple 244 Locator.Locator.

Under which of the following circumstances does a vor/dme area navigation ?

Question 72-20 : Vor/dme area navigation computer is receiving neither radial nor distance data information from vor/dme stations vor/dme area navigation computer is not receiving information from the air data computer vor/dme area navigation computer is not receiving information from the aircraft compass system when 'dr' is selected by the pilot

.in navigation 'dead reckoning mode' is the process of calculating one's current position by using a previously determined position or fix and advancing that position based upon known or estimated speeds over elapsed time and course .the rnav computer on board the airplane will switch to dead reckoning mode when it lost radial or distance data information from vor/dme stations exemple 248 Vor/dme area navigation computer is receiving neither radial nor distance data information from vor/dme stations.Vor/dme area navigation computer is receiving neither radial nor distance data information from vor/dme stations.

How does a vor/dme area navigation system selects the dme stations to be used ?

Question 72-21 : The vor/dme area navigation system has its own nav tuner and the system itself tunes the dme stations providing the most accurate position the pilot tunes the closest vor/dme stations within range on the vor/dme area navigation control panel the vor/dme area navigation system uses whatever stations are tuned on the aircraft's normal vhf nav selector the vor/dme area navigation system has its own vhf nav tuner and it always tunes the dme stations closest to the aircraft position

.dme stations that have the best range and geometry for computing the most accurate position on our course are automatically selected by a rnav system which has its own nav tuner exemple 252 The vor/dme area navigation system has its own nav tuner and the system itself tunes the dme stations providing the most accurate position.The vor/dme area navigation system has its own nav tuner and the system itself tunes the dme stations providing the most accurate position.

Apart from radials and distances from vor/dme stations what information is ?

Question 72-22 : Heading from the aircraft compass system and true airspeed from the air data computer true airspeed from the air data computer heading from the aircraft compass system vertical speed from the air data computer

exemple 256 Heading from the aircraft compass system and true airspeed from the air data computer.Heading from the aircraft compass system and true airspeed from the air data computer.

The flight management system fms is organized in such a way that ?

Question 72-23 : The navigation database is read only to the pilot the pilot is able to modify the navigation database in the fmc between two updates the navigation database of the fmc is valid for one year the navigation database of the fmc is created by the pilot

.you are not allowed to modify the navigation database imagine that one pilot deleted one or more waypoints by accident or by negligence you are flying after him it could be very dangerous .for this reason the navigational database is read only but additional space exists so that crew created navigational data may be saved in the computer memory .such additional data will also be deleted at the 28 days navigational update of the database exemple 260 The navigation database is read only to the pilot.The navigation database is read only to the pilot.

Precision rnav p rnav requires a track keeping accuracy of ?

Question 72-24 : +/ 1 0nm for 95% of the flight time +/ 10 0nm for 95% of the flight time +/ 5 0nm for 95% of the flight time +/ 8 0nm for 95% of the flight time

Area navigation rnav icao annex 11 is a method of navigation permitting aircraft operations on any desired track within the coverage of station referenced navigation signal or within the limits of a self contained navigation system . precision rnav prnav systems require rnp 1 +/ 1 0nm for 95% of the flight time .for information basic rnav b rnav systems require rnp 5 required navigation performance 5 .b rnav requires only a track keeping accuracy of +/ 5nm or better for 95% of the flight time exemple 264 +/- 1.0nm for 95% of the flight time.+/- 1.0nm for 95% of the flight time.

On what data is a vor/dme area navigation system operating in the dead ?

Question 72-25 : Tas from the air data computer heading from the aircraft compass the last computed w/v tas from the air data computer heading from the aircraft compass radial from one vor distances from two dmes radial from one vor distances from two dmes tas from the air data computer heading from the aircraft compass

. navigation computer vor/dme navigation .the vor/dme area navigation system computer calculates track error in relation to desired track this data can easily be interfaced with the automatic flight control and when done so enables the aircraft to automatically follow the flight plan loaded into the rnav computer .the computer is able to perform great circle navigation when receiving vor/dme stations if out of range the system reverts to dr dead reckoning mode where it updates the position by means of last computed wind and tas and heading information . operation in dr mode is time limited exemple 268 Tas from the air data computer; heading from the aircraft compass; the last computed w/v.Tas from the air data computer; heading from the aircraft compass; the last computed w/v.

In the flight management computer fmc of the flight management system fms data ?

Question 72-26 : Navigation database air data computer performance database auto flight computers

Admin . 2400 exemple 272 Navigation database.Navigation database.

A fms with only a multiple dme sensor operating shall have a position error 95% ?

Question 72-27 : 0 3 nm 0 06 nm 1 nm 0 5 nm

Icao doc 8168 .departure procedures are normally based on rnp 1 .where necessary and appropriate they may be based on rnp 0 5 or rnp 0 3 .departures are not associated with an rnp less than rnp 0 3 .. non precision approach procedures are normally based on .rnp 0 5 initial approach only or . rnp 0 3 initial intermediate final approach .. non precision approach procedures are not associated with an rnp less than rnp 0 3 exemple 276 0.3 nm.0.3 nm.

What is the cross track deviation xtk indicated on an rnav system area ?

Question 72-28 : The distance between the actual position and the great circle track between two active waypoints the distance along a track between two waypoints the distance between the air position and the great circle track between two active waypoints the distance between the air position and the planned track

Xtk is the aircraft position relative to the path .xtk distance is the shortest distance shortest path between actual aircraft position and an active waypoint selected on the track even if we are not on the planned path exemple 280 The distance between the actual position and the great circle track between two active waypoints.The distance between the actual position and the great circle track between two active waypoints.

In what piece of fms equipment will the pilot enter the waypoint information ?

Question 72-29 : The control display unit cdu the symbol generator the navigation display nd the primary flight display pfd

Admin . flight management system .the flight management system fms is comprised of the following components . flight management computer system fmcs . autopilot/flight director system afds . autothrottle a/t . inertial reference systems irs . global positioning system gps ..each of these components is an independent system and each can be used independently or in various combinations the term fms refers to the concept of joining these independent components together into one integrated system which provides continuous automatic navigation guidance and performance.management .the integrated fms provides centralized flight deck control of the airplane's flight path and performance parameters the flight management computer or fmc is the heart of the system performing navigational and performance computations and providing control and guidance commands .the primary flight deck controls are the afds mcp two control display units cdu's two electronic flight instrument system efis control panels and an fmc source selector switch the primary displays are the cdus outboard display units inboard display units and upper display unit .the fmc uses crew entered flight plan information airplane systems data and data from the fmc navigation database and performance database to calculate airplane present position and pitch roll and thrust commands required to fly an optimum flight profile the fmc sends these commands to the autothrottle autopilot and flight director map and route information are sent to the respective pilot's navigation displays the efis control panels are used to select the desired.information for navigation display the mode control panel is used to select the autothrottle autopilot and flight director operating modes . the final preparation of the flight via the cdu are being completed by the captain . 2401 exemple 284 The control display unit (cdu).The control display unit (cdu).

3d rnav fixing gives you ?

Question 72-30 : Horizontal and vertical profile guidance horizontal vertical profile and time guidance 2d rnav plus time guidance 2d rnav plus speed control

Area navigation rnav icao annex 11 is a method of navigation permitting aircraft operations on any desired track within the coverage of station referenced navigation signal or within the limits of a self contained navigation system. a 3d rnav system is able to navigate in the horizontal plane and in addition has a guidance capability in the vertical plane exemple 288 Horizontal and vertical profile guidance.Horizontal and vertical profile guidance.

Which of the following are stored in the navigation database of the flight ?

Question 72-31 : 1 2 4 1 2 3 4 2 4 5 1 2 3

Admin . 2402 exemple 292 1, 2, 4.1, 2, 4.

From which of the following combination of navigational sources provide enough ?

Question 72-32 : Irs and air data computer irs and gps gps and compass output compass system and irs

Tothdaniel .the right answer seems to be close but i cannot figure out how wind can be calculated without heading information ..the output data of an irs include present position acceleration and true heading ground speed is calculated by integrating measured acceleration air data computer will provide tas exemple 296 Irs and air data computer.Irs and air data computer.

The flight management system fms is organized in such a way that the pilot can ?

Question 72-33 : Insert additional temporary navigation data between two database updates modify the data in the database between two updates modify the database every 14 days read and write at any time in the database

.the navigational database is read only but additional space exists so that crew created navigational data may be saved in the computer memory .such additional data will also be deleted at the 28 days navigational update of the database exemple 300 Insert additional temporary navigation data between two database updates.Insert additional temporary navigation data between two database updates.

A pilot is flying between two waypoints defined by suitably located vor/dmes ?

Question 72-34 : Reads cross track error and the distance to go on cdi or hsi must update any altitude change in rnav system to have correct cross track error reads vor/dme bearing and distance on cdi or hsi to compute himself the cross track error enters relative position between his aircraft and the vor/dmes on cdu to calculate the cross track error

The navigation computer of the simple 2d rnav system computes the navigational problems by simple sine and cosine mathematics solving the triangular problems .output data from the navigation computer are . desired magnetic track to the next waypoint shown on the cdi or hsi at the course pointer. distance from present position to the next waypoint. deviations cross track error from desired track as follows . in enroute mode full scale deflection on the cdi or hsi is 5 nm. in approach mode full scale deflection on the cdi or hsi is 1 25 nm. in vor/dme mode full scale deflection of the cdi or hsi is 10° exemple 304 Reads cross track error and the distance to go on cdi or hsi.Reads cross track error and the distance to go on cdi or hsi.

The control and display unit cdu on an fms is ?

Question 72-35 : Used by the crew to input data into fmc the system used to update the navigation database the autopilot control panel used on ground only to monitor the maintenance procedure

exemple 308 Used by the crew to input data into fmc.Used by the crew to input data into fmc.

A 2 dimensional rnav system has a capability in the ?

Question 72-36 : Horizontal plane vertical plane timing function horizontal and vertical planes

A 2d rnav system is able to navigate in the horizontal plane only ..a 3d rnav system is able to navigate in the horizontal plane and in addition has a guidance capability in the vertical plane ..a 4d rnav system is able to navigate in the horizontal plane has a guidance capability in the vertical plane and in addition has a timing function exemple 312 Horizontal plane.Horizontal plane.

A fix obtained by rho rho navigation is based on information from two ?

Question 72-37 : Dmes vors ndbs vdfs

Admin .rho rho navigation uses distance from two sources for position information .rho rho navigation is quite a bit more complicated than either theta theta vor vor or theta rho vor dme and requires an onboard computer to do all but the easiest calculations .however it is very accurate much more than any system that uses theta vor for simple reason that dme is so much more accurate than any other azimuth based navigation system . 2394 exemple 316 Dmes.Dmes.

The fms navigation data base usually contains .1 airport reference data .2 atc ?

Question 72-38 : 1 3 and 4 1 2 and 3 1 and 3 1 2 3 and 4

exemple 320 1, 3 and 4.1, 3 and 4.

The inputs of information used to achieve the rnav required accuracy may be .1 ?

Question 72-39 : 2 3 4 1 2 3 1 2 3 4 2 4

exemple 324 2, 3, 4.2, 3, 4.

Benefits of area navigation include .1 shorter flight distance.2 reduction in ?

Question 72-40 : 1 2 and 4 1 2 4 and 5 2 4 and 5 3 4 and 5

.area navigation rnav icao annex 11 is a method of navigation permitting aircraft operations on any desired track within the coverage of station referenced navigation signal or within the limits of a self contained navigation system .rnav can be used in all phases of flight and when implemented correctly can result in . improved situational awareness for the pilot . reduced workloads for both controller and pilot . reduced environmental impact from improved design of routes and procedures . reduced fuel consumption from shorter more direct routes exemple 328 1, 2 and 4.1, 2 and 4.


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