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Students > VFR : The fms provides the following functions .1 lateral and vertical flight plan ?

Question 56-1 : 1 3 1 2 3 1 3 4 4

exemple 156 1, 3.1, 3.

Concerning the fms the parameters used to work out the vertical flight profile ?

Question 56-2 : 1 2 3 1 2 3 5 1 2 5 3 4 5

Oxygen quantity available for flight crew and minimum safe enroute altitude are not values that are incorporated in the performance database or the navigation database exemple 160 1, 2, 3.1, 2, 3.

Components of the fms are .1 cdu control and display unit .2 database.3 fmc ?

Question 56-3 : 1 2 3 1 2 4 5 1 3 3 4

exemple 164 1, 2, 3.1, 2, 3.

The fms provides the following functions .1 vertical flight plan management .2 ?

Question 56-4 : 1 2 3 1 2 4 2 3 4 1 3 4

exemple 168 1, 2, 3.1, 2, 3.

The fmc determines and update present aircraft position from the following ?

Question 56-5 : 1 2 3 1 2 4 1 2 3 4 3

.the most common sensors interfacing a fms to compute the aircraft position along the flight plan are . irs. dme. gps. vor..mls ils ndb localizer can be used as inputs to the fmc position but only on departure or on arrival.the acars system is used to transmit non vocal messages between an aircraft and the ground by vhf or satellite communication it can be used in particular by operators to transmit information in real time meteorological data flight progress information etc exemple 172 1, 2, 3.1, 2, 3.

The fmc determines and update present aircraft position from the following ?

Question 56-6 : 2 3 4 1 2 4 2 4 1 3

.the most common sensors interfacing a fms to compute the aircraft position along the flight plan are . irs. dme. gps. vor..mls ils ndb localizer can be used as inputs to the fmc position but only for departure or arrival exemple 176 2, 3, 4.2, 3, 4.

The fms enables to fly an optimum flight profile for this the fmc flight ?

Question 56-7 : 1 2 3 5 1 2 5 2 3 4 1 3 5

.the flight plan is generally determined on the ground before departure it is entered into the fms either by typing it in selecting it from a saved library of common routes company routes or via an acars datalink with the airline dispatch center .the output data from the adc are used by the fms adc feds the fmc with mach number/tas/altitude etc .aircraft position is provided by gps/irs/vor/dme/adf .the fms navigation database includes data for airports navaids airways sid star magnetic variation

The fms flight plan or leg page displays the following parameters relative to ?

Question 56-8 : 2 3 4 1 3 4 1 2 1 2 3 4

exemple 184 2, 3, 4.2, 3, 4.

The fms provides the following functions.1 traffic advisories emission.2 ?

Question 56-9 : 3 4 1 3 4 1 2 3 1 4


The fms flight plan or leg page displays the following parameters relative to ?

Question 56-10 : 1 4 1 3 3 4 1 2 4

exemple 192 1, 4.1, 4.

For most fms the fuel prediction function which computes the remaining fuel ?

Question 56-11 : 2 1 3 2 4 3

exemple 196 2.2.

For most fms the fuel prediction function which computes the remaining fuel ?

Question 56-12 : 4 1 4 3 3 1 2

exemple 200 4.4.

The duration of a fms navigation database loaded before expiring is ?

Question 56-13 : 28 days 15 days 2 months 3 months

exemple 204 28 days.28 days.

The role of the fms is to .1 aid the crew with navigation.2 shut down the ?

Question 56-14 : 1 4 5 2 3 4 5 1 2 3 1 3 4

exemple 208 1, 4, 5.1, 4, 5.

The role of the fms is to aid the flight crew with .1 immediate actions in ?

Question 56-15 : 2 3 2 3 4 3 4 1 2

exemple 212 2, 3.2, 3.

In a fms mcdus are used pre flight to manually initialise with dispatch ?

Question 56-16 : 1 4 2 1 3 2 3 4

exemple 216 1, 4.1, 4.

The 'overfly' symbol related to a waypoint on an fms page indicates that ?

Question 56-17 : The aircraft is required to pass directly over this waypoint a time estimate is given for this waypoint a turn anticipation is permited a fuel prediction is given for this waypoint

exemple 220 the aircraft is required to pass directly over this waypoint.the aircraft is required to pass directly over this waypoint.

The fms required time of arrival rta function can provide ?

Question 56-18 : A speed target to satisfy a time constraint entered at a flight plan waypoint a time slot computed for the arrival time at destination using the current aircraft speed and speed constraints along the flight plan a time prediction at the active to waypoint complying with the wind computation a time prediction at the flight plan waypoints based on the current speed and speed constraints along the flight plan

exemple 224 a speed target to satisfy a time constraint entered at a flight plan waypoint.a speed target to satisfy a time constraint entered at a flight plan waypoint.

The fuel management performed by most fms along the flight plan is considered as ?

Question 56-19 : A function which helps the crew to estimate the remaining fuel quantity along the flight plan but should not be considered as an accurate and reliable source an accurate function which can be considered as the prime source to determine the remaining fuel quantity along the flight plan an accurate and very reliable function providing that the fuel on board quantity has been properly initialized by the crew before start up the prime source to manage the fuel consumption along the flight

exemple 228 a function which helps the crew to estimate the remaining fuel quantity along the flight plan but should not be considered as an accurate and reliable source.a function which helps the crew to estimate the remaining fuel quantity along the flight plan but should not be considered as an accurate and reliable source.

Some of the fms have a navigation mode called dead reckoning mode dr computing ?

Question 56-20 : A back up navigation mode to compute a fms position when the other navigation sensors are no longer operating an operating mode used to intercept radials to or from a flight plan waypoint a navigation mode used to monitor the fms position the normal navigation mode for fms which do not use inertial navigation systems ins to compute the aircraft position

exemple 232 a back up navigation mode to compute a fms position when the other navigation sensors are no longer operating.a back up navigation mode to compute a fms position when the other navigation sensors are no longer operating.

The fms lateral offset function consists in ?

Question 56-21 : Flying along the flight plan legs with a constant right or left offset manually entered on the fms cdu displaying the lateral cross track deviation xtk of the aircraft according to the active flight plan leg creating a new waypoint using a reference flight plan waypoint and a distance from this waypoint along the flight plan legs flying a fms selected lateral pattern used for search and rescue operations

.a lateral offset may be specified up to 99 9 nautical miles left or right of course .on the nd navigation display an offset route selected through the fmc is displayed with a dot dash line magenta parallel to the active route exemple 236 flying along the flight plan legs with a constant right or left offset manually entered on the fms cdu.flying along the flight plan legs with a constant right or left offset manually entered on the fms cdu.

The fms navigation database includes the following data.1 airports.2 ?

Question 56-22 : 1 3 4 1 2 3 2 5 1 3 4 5

exemple 240 1, 3, 4.1, 3, 4.

The most common sensors interfacing a fms to compute the aircraft position ?

Question 56-23 : 1 3 1 2 3 2 3 1 4

exemple 244 1, 3.1, 3.

For a fms designed with the vertical navigation vnav capability coupled to the ?

Question 56-24 : 2 3 1 2 1 3 2

.vertical guidance vnav enables the system to calculate optimum cruise altitudes and to determine the best combination of auto throttle control and speed during climb and descent.with the vnav mode engaged the fms commands afds autopilot flight director system pitch and a/t modes to fly the vertical profile selected on the fms cdus the profile includes pre selected climbs cruise altitudes speeds descents and can also include altitude constraints at specified way points exemple 248 2, 3.2, 3.

The fms navigation database includes the following data .1 obstacles.2 ?

Question 56-25 : 2 3 4 5 1 2 3 4 5 1 2 4 1 3 5

exemple 252 2, 3, 4, 5.2, 3, 4, 5.

The fms provides the following functions .1 aid for fuel management.2 lateral ?

Question 56-26 : 1 2 4 1 2 3 2 3 3 4

exemple 256 1, 2, 4.1, 2, 4.

The fms cross track xtk is ?

Question 56-27 : The abeam distance error to the left or right from the desired flight plan leg to the aircraft position the angular distance error to the left or right from the desired track dtk to the aircraft track tk the distance error between the fms computed position and the irs computed position the distance error between the fms computed position and the gps computed position

exemple 260 the abeam distance error, to the left or right from the desired flight plan leg to the aircraft position.the abeam distance error, to the left or right from the desired flight plan leg to the aircraft position.

The fms vertical navigation management is generally performed based on ?

Question 56-28 : The baro altitude input from the adc the gps altitude computed by the gps receiver a mix of baro and gps altitudes the geometric altitude input from the terrain awareness and warning system taws

exemple 264 the baro altitude input from the adc.the baro altitude input from the adc.

The fms navigation database includes the following data.1 airports.2 take off ?

Question 56-29 : 1 3 5 1 2 3 3 4 5 1 2 5

exemple 268 1, 3, 5.1, 3, 5.

In a dual fms architecture when an incompatibility between the two fmc's occurs ?

Question 56-30 : Both fmc's are working independently they are linked only to their own peripherals only the left one remains active only the right one remains active they will have to be disconnected

exemple 272 both fmc's are working independently: they are linked only to their own peripherals.both fmc's are working independently: they are linked only to their own peripherals.

Considering a two fms architecture working in dual mode. fmc flight management ?

Question 56-31 : One fmc is stated as 'master' the other as 'slave' both fmc are synchronized via an exchange bus a fmc is used by the captain the other by the copilot the fmc are not synchronized only one fmc feeds the two fms the main fmc is working the other on standby in the event of a failure of the 'master' fmc

exemple 276 one fmc is stated as 'master', the other as 'slave'; both fmc are synchronized via an exchange bus.one fmc is stated as 'master', the other as 'slave'; both fmc are synchronized via an exchange bus.

The component used to enter the flight plan route on the fms is the ?

Question 56-32 : Mcdu cmu fmc lcd

Cqb15 may 2012.the mcdu multi function control display unit is a man machine interface .it is a part of the flight management system fms exemple 280 mcdu.mcdu.

The database of a fms flight management system is divided into major sections ?

Question 56-33 : Aircraft performance and navigation navigation and meteorology aircraft performance and fuel saving inertial and navigation

Cqb15 august 2012 exemple 284 aircraft performance and navigation.aircraft performance and navigation.

For most fms the fuel prediction function which computes the remaining fuel ?

Question 56-34 : 2 4 1 2 3 4 1 3 1 2 4

Cqb15 august 2012 exemple 288 2, 4.2, 4.

Under normal conditions in a dual fms architecture the master fmc sends its ?

Question 56-35 : Autopilot flight director and autothrottle flight director and autothrottle autopilot and autothrottle autopilot

Ecqb03 july 2016 exemple 292 autopilot, flight director and autothrottle.autopilot, flight director and autothrottle.

The purpose of the flight management system fms is to provide ?

Question 56-36 : Continuous automatic navigation guidance and performance management continuous automatic navigation guidance as well as manual performance management manual navigation guidance and automatic performance management both manual navigation guidance and performance management

Revised ecqb04 october 2017 exemple 296 continuous automatic navigation guidance and performance management.continuous automatic navigation guidance and performance management.

A fms can correct its fuel computations for the following non standard ?

Question 56-37 : 3 1 2 4 2 3 4 1

exemple 300 3.3.

The fms 'autotune' function can automatically tune frequencies for ?

Question 56-38 : Vor and dme navaids vhf and hf radio navaids and vhf radio vhf radio only

.the 'auto tune' function will automatically selects your vors and dmes en route exemple 304 vor and dme.vor and dme.

In order to enter a phantom waypoint that is designated by a vor/dme simple ?

Question 56-39 : Does not have to be in range when entered but must be when used does not have to be in range when entered or used must be in range has to be positively identified by one of the pilots

Area navigation systems .the control unit allows the flight crew to. tune the vor/dme station used to define the phantom waypoint.. define the phantom waypoint as a radial and distance dme form the selected vor/dme 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 vor/dme mode of operation...those operations can be done without being in range of the vor/dme but while in flight in order to receive information to compute our position station must be in range exemple 308 does not have to be in range when entered but must be when used.does not have to be in range when entered but must be when used.

Which of the following combinations is likely to result in the most accurate ?

Question 56-40 : Dme/dme vor/dme ndb/vor vor/vor

Dme dme 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 312 dme/dme.dme/dme.


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