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Question 71-1 : The component used to enter the flight plan route on the fms is the ? [ Practice protocol ]
Mcdu
Question 71-2 : The database of a fms flight management system is divided into major sections ?
Aircraft performance and navigation.
Cqb15 august 2012Navigation and meteorology. aircraft performance and fuel saving. inertial and navigation.
Question 71-3 : For most fms the fuel prediction function which computes the remaining fuel among the flight plan takes into account the following parameters 1 the additional drag in case the landing gear can not be retracted2 the cruise flight level3 the additional drag in case the flaps are blocked and partly ?
2 4.
Cqb15 august 20121, 2, 3, 4. 1, 3. 1, 2, 4.
Question 71-4 : Under normal conditions in a dual fms architecture the master fmc sends its commands to the fmc=flight management computer ?
Autopilot flight director and autothrottle.
Ecqb03 july 2016Flight director and autothrottle. autopilot and autothrottle. autopilot.
Question 71-5 : The purpose of the flight management system fms is to provide ?
Continuous automatic navigation guidance and performance management.
Revised ecqb04 october 2017Continuous automatic navigation guidance as well as manual performance management. manual navigation guidance and automatic performance management. both manual navigation guidance and performance management.
Question 71-6 : A fms can correct its fuel computations for the following non standard configurations 1 landing gear down2 speed brakes extended3 one engine out4 slatsflaps not fully retractedthe combination which regroups all of the correct statements is ?
3.
1, 2, 4. 2, 3, 4. 1.
Question 71-7 : The fms 'autotune' function can automatically tune frequencies for ?
Vor and dme.
The 'auto tune' function will automatically selects your vors and dmes en routeNavaids, vhf and hf radio. navaids and vhf radio. vhf radio only.
Question 71-8 : In order to enter a phantom waypoint that is designated by a vordme simple rnav system the vordme ?
Does not have to be in range when entered but must be when used.
Area navigation systems the control unit allows the flight crew to tune the vordme station used to define the phantom waypoint define the phantom waypoint as a radial and distance dme form the selected vordme station select desired magnetic track to follow inbound to the phantom waypoint select between an en route mode an approach mode of operation and the basic vordme mode of operationthose operations can be done without being in range of the vordme but while in flight in order to receive information to compute our position station must be in rangeDoes not have to be in range when entered or used. must be in range. has to be positively identified by one of the pilots.
Question 71-9 : Which of the following combinations is likely to result in the most accurate area navigation rnav fixes ?
Dmedme.
Dme dme rho rho navigation uses distance from two sources for position informationrho 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 2394Vor/dme. ndb/vor. vor/vor.
Question 71-10 : Which of the following gives the best information about the progress of a flight between 2 en route waypoints from a 'rnav' equipment ?
Eto.
Etd. ata. elapsed time on route.
Question 71-11 : If an aircraft flies along a vor radial it will follow a ?
Great circle track.
When you follow a radial you follow a straight line on a sphere which can only be great circle radio waves travel over the surface of the earth along great circle paths and if the direction of a great circle is measured at two selected meridians there will be a difference between two directions it can not be a constant magnetic track Rhumbline track. line of constant bearing. constant magnetic track.
Question 71-12 : Which of the figures depicts an electronic flight instrument system efis display in expanded exp vorils mode with an ils frequency selected 2067 ?
Figure 1.
1943Figure 4. figure 2. figure 3.
Question 71-13 : Which of the figures depicts an electronic flight instrument system efis display in expanded exp vorils mode with a vor frequency selected 2103 ?
Figure 4.
1943all fgures are in expanded mode here is the full mode 1707 mode fullFigure 1. figure 3. figure 2.
Question 71-14 : Which of the figures depicts an electronic flight instrument system efis display in full vorils mode with an vor frequency selected 2102 ?
Figure 1.
2391figure 1 full vorils mode with an vor frequency selectedfigure 6 full vorils mode with an ils frequency selected mode full 1707Figure 4. figure 5. figure 6.
Question 71-15 : Which of the figures depicts an electronic flight instrument system efis display in plan mode 2100 ?
Figure 2.
2391Figure 3. figure 4. figure 1.
Question 71-16 : Which of the figures depicts an electronic flight instrument system efis display in map mode 2100 ?
Figure 3.
2391Figure 5. figure 2. figure 4.
Question 71-17 : Which of the figures depicts an electronic flight instrument system efis display in expanded exp vorils mode with an vor frequency selected 2100 ?
Figure 4.
2391expanded vorils mode with a vor frequency selectedFigure 5. figure 6. figure 1.
Question 71-18 : Which of the figures depicts an electronic flight instrument system efis display in expanded exp vorils mode with an ils frequency selected 2100 ?
Figure 5.
2391Figure 3. figure 2. figure 6.
Question 71-19 : Which of the figures depicts an electronic flight instrument system efis display in full vorils mode with an ils frequency selected 2100 ?
Figure 6.
2391 mode full 1707Figure 2. figure 3. figure 5.
Question 71-20 : What drift is being experienced 2096 ?
8° left.
Left 8° between track line and our current heading 239520° right. 20° left. 12° right.
Question 71-21 : What is the value of the track from tbx to ytb 2094 ?
097° t .
Efis is in plan mode it's a 'chart' with an arrow pointing north at the bottom right hand corner 1706140°(m). 280°(t). 170°(m).
Question 71-22 : What wind velocity is indicated 2095 ?
105° m 20kt.
2396030°(m)/20kt. 255°(m)/20kt. 285°(m)/20kt.
Question 71-23 : What is the value of the selected vor loc course 2093 ?
298° m .
2395272°(m). 260°(m). 280°(m).
Question 71-24 : What is the aircraft track 2092 ?
272° m .
2395300°(m). 260°(m). 280°(m).
Question 71-25 : The letters qtx and adjacent symbol indicate a 2091 ?
Vordmevortac.
2397Tacan. vor. airport.
Question 71-26 : The 'o' followed by the letters kabc indicate 2090 ?
An off route airport.
2398A designated alternate airport. an off-route vor/dme. the destination airport.
Question 71-27 : At reference what is the heading bug selected to 2089 ?
260° m .
2395272°(m). 280°(m). 300°(m).
Question 71-28 : The diagram indicates that the aircraft is to the 2087 ?
Right of the localizer and below the glidepath.
2395Right of the localizer and above the glidepath. left of the localizer and below the glidepath. left of the localizer and above the glidepath.
Question 71-29 : In which screen modes of an electronic horizontal situation indicator ehsi will radar returns not be shown ?
Full nav full vorils and plan.
Weather radar returns can be displayed in expanded vorils mode but cannot be in 'full nav' vor or ils mode neither in plan mode 2399Exp vor/ils, plan and map. full nav, plan and map. full vor/ils, exp vor/ils and plan.
Question 71-30 : Icao annex 11 defines area navigation rnav as a method of navigation which permits aircraft operation on any desired flight path ?
Within the coverage of station referenced navigation aids or within the limits of the capability of self contained aids or a combination of these.
Icao annex 11 air traffic services area navigation rnav a method of navigation which permits aircraft operation on any desired flight path within the coverage of ground or space based navigation aids o rwithin the limits of the capability of self contained aids or a combination of these note area navigation includes performance based navigation as well as other operations that do not meet the definition of performance based navigation Outside the coverage of station-referenced navigation aids provided that it is equipped with a minimum of one serviceable self-contained navigation aid. within the coverage of station-referenced navigation aids provided that it is equipped with a minimum of one serviceable self-contained navigation aid. outside the coverage of station-referenced navigation aids provided that it is equipped with a minimum of two serviceable self-contained navigation aids.
Question 71-31 : Basic rnav requires a track keeping accuracy of ?
+ 5nm or better 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 basic rnav b rnav systems require rnp 5 required navigation performance 5 b rnav requires a track keeping accuracy of + 5nm or better for 95% of the flight time for information precision rnav prnav systems require rnp 1 + 10nm for 95% of the flight time +/- 3nm or better for 90% of the flight time. +/- 2nm or better for 75% of the flight time. +/- 5nm or better throughout the flight.
Question 71-32 : The flight management computer fmc position is ?
The computed position based on a number of sources irs radio ils gps etc .
The actual position of the aircraft at any point in time. the same as that given on the no. 1 irs. another source of aircraft position; it is independent of other navigation sources (irs, radio, ils, etc).
Question 71-33 : Under easa cs 25 color code rules features displayed in red on an electronic flight instrument system efis indicate ?
Warnings flight envelope and system limits.
Flight envelope and system limits; engaged modes. warnings; cautions and abnormal sources. cautions and abnormal sources; engaged modes.
Question 71-34 : Under easa cs 25 colour code rules features displayed in amberyellow on an electronic flight instrument system efis indicate ?
Cautions abnormal sources.
Flight envelope and system limits. warnings. engaged modes.
Question 71-35 : Under easacs 25 colour code rules features displayed in green on an efis should indicate ?
Engaged modes.
Cautions, abnormal sources. the earth. the ils deviation pointer.
Question 71-36 : Under easa cs 25 colour code rules features displayed in cyanblue on an electronic flight instrument systems efis indicate ?
The sky.
Engaged modes. the flight director bars. flight envelope and system limits.
Question 71-37 : In an electronic flight instrument system efis data relating primarily to navigation in the fmc is provided by ?
Question 71-38 : Under easa regulations color code rules for efis displays the recommended color for the aircraft symbol is ?
White.
Magenta. green. cyan.
Question 71-39 : Which of the following procedures must be adopted if on a flight under ifr conditions using a navstargps satellite navigation system receiver the position fix obtained from the gps receiver differs from the position of conventional navigation systems by an unacceptable amount ?
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.
Question 71-40 : What datum is used for the minimum descent altitude mda on a non precision approach when using the navstargps satellite navigation system ?
Barometric 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 altimetryIf using differential-gps (d-gps) the altitude obtained from the d-gps, otherwise barometric altitude. radar altitude. gps altitude.
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