Under normal conditions in a dual FMS architecture the master FMC sends its commands to the FMC=Flight Management Computer ?
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The purpose of the Flight Management System FMS is to provide ?
A FMS can correct its fuel computations for the following non standard configurations 1 Landing gear down2 Speed brakes extended3 One engine out4 Slats/flaps not fully retractedThe combination which ?
The fms 'autotune' function can automatically tune frequencies Continuous automatic navigation guidance performance management. the 'auto tune' function will automatically selects your vors dmes en route. 
In order to enter a phantom waypoint that designated a vor/dme simple rnav system vor/dme Does not have to be in range when entered but must be when used. area navigation systems the control unit allows flight crew to tune vor/dme station used to define phantom waypoint define phantom waypoint as a radial distance (dme) form selected vor/dme station select desired magnetic track to follow inbound to phantom waypoint select between an en route mode an approach mode of operation the basic vor/dme mode of operation those operations can be done without being in range of vor/dme but while in flight in order to receive information to compute our position station must be in range. 
Which of following combinations likely to result in most accurate area navigation rnav fixes Does not have to be in range when entered but must be when used. Dme dme (rho rho) navigation uses distance from two sources position information rho rho navigation quite a bit more complicated than either theta theta (vor vor) or theta rho (vor dme) requires an onboard computer to do all but easiest calculations however it very accurate much more than any system that uses theta (vor) simple reason that dme so much more accurate than any other azimuth based navigation system . 
Which of following gives best information about progress of a flight between 2 en route waypoints from a 'rnav' equipment Does not have to be in range when entered but must be when used. Dme dme (rho rho) navigation uses distance from two sources position information rho rho navigation quite a bit more complicated than either theta theta (vor vor) or theta rho (vor dme) requires an onboard computer to do all but easiest calculations however it very accurate much more than any system that uses theta (vor) simple reason that dme so much more accurate than any other azimuth based navigation system . Question 55-8
If an aircraft flies along a vor radial it will follow a Does not have to be in range when entered but must be when used. When you follow a radial you follow a straight line on a sphere which can only be great circle (radio waves travel over surface of earth along great circle paths) and if direction of a great circle measured at two selected meridians there will be a difference between two directions it can not be a 'constant magnetic track'. Question 55-9
Which of figures depicts an electronic flight instrument system efis display in expanded exp vor/ils mode with an ils frequency selected 2067 Does not have to be in range when entered but must be when used. . Question 55-10
Which of figures depicts an electronic flight instrument system efis display in expanded exp vor/ils mode with a vor frequency selected 2103 Does not have to be in range when entered but must be when used. all fgures are in expanded mode here the full mode mode full. Question 55-11
Which of figures depicts an electronic flight instrument system efis display in full vor/ils mode with an vor frequency selected 2102 Does not have to be in range when entered but must be when used. figure 1 full vor/ils mode with an vor frequency selected figure 6 full vor/ils mode with an ils frequency selected mode full . Question 55-12
Which of figures depicts an electronic flight instrument system efis display in plan mode 2100 Does not have to be in range when entered but must be when used. . Question 55-13
Which of figures depicts an electronic flight instrument system efis display in map mode 2100 Does not have to be in range when entered but must be when used. . Question 55-14
Which of figures depicts an electronic flight instrument system efis display in expanded exp vor/ils mode with an vor frequency selected 2100 Does not have to be in range when entered but must be when used. expanded vor/ils mode with a vor frequency selected. Question 55-15
Which of figures depicts an electronic flight instrument system efis display in expanded exp vor/ils mode with an ils frequency selected 2100 Does not have to be in range when entered but must be when used. . Question 55-16
Which of figures depicts an electronic flight instrument system efis display in full vor/ils mode with an ils frequency selected 2100 Does not have to be in range when entered but must be when used. mode full . Question 55-17
What drift being experienced 2096 Does not have to be in range when entered but must be when used. left 8° between track line our current heading . Question 55-18
What the value of track from tbx to ytb 2094 Does not have to be in range when entered but must be when used. efis in plan mode it's a 'chart' with an arrow pointing north at bottom right hand corner . Question 55-19
What wind velocity indicated 2095 Does not have to be in range when entered but must be when used. . Question 55-20
What the value of selected vor loc course 2093 Does not have to be in range when entered but must be when used. . Question 55-21
What the aircraft track 2092 Does not have to be in range when entered but must be when used. . Question 55-22
The letters qtx and adjacent symbol indicate a 2091 Does not have to be in range when entered but must be when used. . Question 55-23
The 'o' followed the letters kabc indicate 2090 An off route airport. . Question 55-24
At reference what the heading bug selected to 2089 An off route airport. . Question 55-25
The diagram indicates that aircraft to 2087 Right of localizer below glidepath. . Question 55-26
In which screen modes of an electronic horizontal situation indicator ehsi will radar returns not be shown Full nav full vor/ils plan. weather radar returns can be displayed in expanded vor/ils mode but cannot be in 'full nav' (vor or ils) mode neither in plan mode . Question 55-27
Icao annex 11 defines area navigation rnav as a method of navigation which permits aircraft operation on any desired flight path Within coverage of station referenced navigation aids or within limits of 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 coverage of ground or space based navigation aids o rwithin limits of 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 definition of performance based navigation. Question 55-28
Basic rnav requires a track keeping accuracy of +/ 5nm or better 95% of flight time. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-29
The flight management computer fmc position The computed position based on a number of sources (irs radio ils gps etc). Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-30
Under easa cs 25 color code rules features displayed in red on an electronic flight instrument system efis indicate Warnings flight envelope system limits. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-31
Under easa cs 25 colour code rules features displayed in amber/yellow on an electronic flight instrument system efis indicate Cautions abnormal sources. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-32
Under easa/cs 25 colour code rules features displayed in green on an efis should indicate Cautions abnormal sources. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-33
Under easa cs 25 colour code rules features displayed in cyan/blue on an electronic flight instrument systems efis indicate Cautions abnormal sources. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-34
In an electronic flight instrument system efis data relating primarily to navigation in fmc provided Navigation radios gps inertial reference systems. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-35
Under easa regulations color code rules efis displays recommended color the aircraft symbol Navigation radios gps inertial reference systems. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-36
Which of following procedures must be adopted if on a flight under ifr conditions using a navstar/gps satellite navigation system receiver position fix obtained from gps receiver differs from position of conventional navigation systems an unacceptable amount It may be continued using conventional navigation systems. Area navigation rnav (icao annex 11) a method of navigation permitting aircraft operations on any desired track within coverage of station referenced navigation signal or within 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 95% of flight time for information precision rnav (prnav) systems require rnp 1 (+/ 1 0nm 95% of flight time). Question 55-37
What datum used the minimum descent altitude mda on a non precision approach when using navstar/gps satellite navigation system It may be continued using conventional navigation systems. icao doc 8168 part ii section 3 chapter 1 all fmcs some stand alone basic gnss receivers provide altitude information however pilot must still comply with published minimum altitudes using barometric altimeter where fmc provides vertical information flight director guidance cues or coupled autopilot operation pilot should follow appropriate information or cues along with any necessary cross checks with barometric altimetry. Question 55-38
Which of distances indicated will be shown on a basic vor/dme based area navigation equipment when using a 'phantom station' at position 'x' 2088 It may be continued using conventional navigation systems. a basic rnav equipment will see a vor/dme at position of 'phantom station' the distance indicated will be 9 nm the principle to move position of a real vor/dme to a desired position (a useful position your navigation). Question 55-39
Erratic indications may be experienced when flying towards a basic vor/dme based area navigation system 'phantom station' When operating at low altitudes close to limit of reception range from reference station. a basic rnav equipment will see a vor/dme at position of 'phantom station' the distance indicated will be 9 nm the principle to move position of a real vor/dme to a desired position (a useful position your navigation). Question 55-40
Which of following one of functions of computer in a basic rnav system It transfers information given a vor/dme station into tracking distance indications to any chosen phantom station/waypoint. Area navigation (rnav) can be defined as a method of navigation that permits aircraft operation on any desired course within coverage of station referenced navigation signals or within limits of a self contained system capability or a combination of these the computer in a basic rnav system transfers information given a vor/dme station into tracking distance indications to any chosen phantom station/waypoint this one of rnav's computer main functions.
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