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Question 70-1 : Concerning the fms flight management system entering a high cost index results in ? [ Exam pilot ]
High airspeed and high fuel trip
Question 70-2 : Concerning the fms flight management system entering a cost index of zero results in ?
Maximum range airspeed.
Cost index is the ratio of time related costs crew salaries maintenance etc to fuel cost as one of the independent variables in the speed schedule computation cost index ci = flight time related costfuel cost the cost index allows airlines to weight time and fuel costs based on their daily operationsa high cost index will result in a high cruising speeda cost index of zero results in minimum trip fuel you will fly at 'maximum range airspeed' cost index is about fuel cost not quantitycost index is a made up figure which when input into the fmc is used to calculate econ speed the higher the cost index number the faster the aircraft flies basically the company decides on the cost of keeping the aircraft in the air and includes all sorts of costs such as crew aircraft operating costs fuel etc they then decide whether they want the aircraft to fly faster or slower and adjust the cost index as neededMaximum cruising airspeed. minimum range airspeed. minimum airspeed.
Question 70-3 : The fms is approved for localizer approaches ?
If the localizer signals are used by the fms.
If the gps only is used as navigation sensor. if the gps and dmes only are used as combined navigation sensors. if the dmes only are used as navigation sensors.
Question 70-4 : Concerning the fms flight management system entering a cost index of zero ?
Results in minimum trip fuel.
Cost index is the ratio of time related costs crew salaries maintenance etc to fuel cost as one of the independent variables in the speed schedule computation cost index ci = flight time related costfuel cost the cost index allows airlines to weight time and fuel costs based on their daily operationsa high 'cost index' will result in a high cruising speeda cost index of zero results in minimum trip fuel you will fly at 'maximum range airspeed' cost index is about fuel cost not quantitycost index is a made up figure which when input into the fmc is used to calculate econ speed the higher the cost index number the faster the aircraft flies basically the company decides on the cost of keeping the aircraft in the air and includes all sorts of costs such as crew aircraft operating costs fuel etc they then decide whether they want the aircraft to fly faster or slower and adjust the cost index as neededResults in maximum trip fuel. does not influence fuel consumption. modifies only cruising airspeed.
Question 70-5 : The fms is approved to provide guidance for the following approaches 1 rnav 2 par 3 vordme vor 4 mls the combination which regroups all of the correct statements is ?
1 3.
On some aircraft the fms takes inputs from vor adf dme rad alt ssr ils gps mls loran etc of these only ils and mls provide their own guidance information to position the aicraft on the required approach path the remainder require help from the fms to position the aircraft on the required track and to calculate the glide pathprecision approach radar par is a type of radar guidance system designed to provide lateral and vertical guidance to an aircraft pilot for landing until the landing threshold is reached it is similar to an instrument landing system ils but requires control instructionsair traffic controllers must transmit a minimum of every 5 seconds to the pilot their relation to the azimuth portion and once intercepting the glidepath their elevation2, 4. 1, 3, 4. 1, 2.
Question 70-6 : The fms is approved to provide guidance for the following approaches 1 rnav 2 ils 3 mls 4 vor ndb the combination which regroups all of the correct statements is ?
1 4.
Kouniouche ndb in fms yes you can select on the fms all possible kind of approach rnav ils mls gps ndb vor vordme but ils and mls provide their own guidance information to position the aicraft on the required approach path2, 3. 1, 2, 4. 1, 3, 4.
Question 70-7 : The fms is approved to provide guidance for the following approaches ?
Non precision approaches.
Ils mls and par are precision approaches and they provide their own guidanceNon precision approaches and ils cat i precision approaches only. non precision and precision approaches. precision approaches limited to cat ii.
Question 70-8 : The fms navigation database includes the following data 1 obstacles2 waypoints3 sid star4 relief 5 magnetic variationthe combination that regroups all of the correct statements is ?
2 3 5.
1, 2, 3. 1, 3, 5. 1, 2, 4.
Question 70-9 : The purpose of the fms temperature compensation function is ?
To provide compensated altitudes for temperatures different from standard atmosphere along the vertical approach profile.
To provide compensated temperatures at the waypoints along the vertical approach profile. to provide the destination airport air temperature. to provide the destination airport or runway elevation.
Question 70-10 : The fms provides the following functions 1 lateral and vertical flight plan management 2 de icing management3 aircraft position computation4 terrain awareness and warningthe combination that regroups all of the correct statements is ?
1 3.
1, 2, 3. 1, 3, 4. 4.
Question 70-11 : Concerning the fms the parameters used to work out the vertical flight profile are 1 zero fuel weight2 cost index3 fuel quantity4 oxygen quantity available for flight crew5 minimum safe enroute altitude the combination that regroups all of the correct statements is ?
1 2 3.
Oxygen quantity available for flight crew and minimum safe enroute altitude are not values that are incorporated in the performance database or the navigation database1, 2, 3, 5. 1, 2, 5. 3, 4, 5.
Question 70-12 : Components of the fms are 1 cdu control and display unit 2 database3 fmc flight management computer 4 electronic check lists5 gpws mode controllerthe combination that regroups all of the correct statements is ?
1 2 3.
1, 2, 4, 5. 1, 3. 3, 4.
Question 70-13 : The fms provides the following functions 1 vertical flight plan management 2 aid for fuel management3 lateral flight plan management4 terrain awareness and warningthe combination that regroups all of the correct statements is ?
1 2 3.
1, 2, 4. 2, 3, 4. 1, 3, 4.
Question 70-14 : The fmc determines and update present aircraft position from the following systems 1 gps2 irs3 navigation radios4 acarsthe combination that regroups all of the correct statements is ?
1 2 3.
The most common sensors interfacing a fms to compute the aircraft position along the flight plan are irs dme gps vormls ils ndb localizer can be used as inputs to the fmc position but only on departure or on arrivalthe 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 1, 2, 4. 1, 2, 3, 4. 3.
Question 70-15 : The fmc determines and update present aircraft position from the following systems 1 satcom2 gps3 dme4 irsthe combination that regroups all of the correct statements is ?
2 3 4.
The most common sensors interfacing a fms to compute the aircraft position along the flight plan are irs dme gps vormls ils ndb localizer can be used as inputs to the fmc position but only for departure or arrival1, 2, 4. 2, 4. 1, 3.
Question 70-16 : The fms enables to fly an optimum flight profile for this the fmc flight management computer uses 1 flight crew entered flight plan data2 data from adc3 aircraft position4 a memorised relief world data base5 data from the fmc navigation data basethe combination that regroups all of the correct ?
1 2 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 centerthe output data from the adc are used by the fms adc feds the fmc with mach numbertasaltitude etc aircraft position is provided by gpsirsvordmeadfthe fms navigation database includes data for airports navaids airways sid star magnetic variation1, 2, 5. 2, 3, 4. 1, 3, 5.
Question 70-17 : The fms flight plan or leg page displays the following parameters relative to the flight plan legs or waypoints 1 aircraft position long lat 2 speed3 distance4 trackthe combination that regroups all of the correct statements is ?
2 3 4.
1, 3, 4. 1, 2. 1, 2, 3, 4.
Question 70-18 : The fms provides the following functions 1 traffic advisories emission2 resolution advisories emission3 aid for fuel management4 lateral flight plan managementthe combination that regroups all of the correct statements is ?
3 4.
1, 3, 4. 1, 2, 3. 1, 4.
Question 70-19 : The fms flight plan or leg page displays the following parameters relative to the flight plan legs or waypoints 1 track2 magnetic variation3 waypoint elevation4 speedthe combination that regroups all of the correct statements is ?
1 4.
Question 70-20 : For most fms the fuel prediction function which computes the remaining fuel along the flight plan takes into account the following situations 1 the additional drag resulting in a flight carried out with the landing gear extended2 the current wind computed or the resulting ground speed3 the ?
2.
1, 3. 2, 4. 3.
Question 70-21 : For most fms the fuel prediction function which computes the remaining fuel along the flight plan takes into account the following situations 1 the additional drag resulting in a flight carried out with the landing gear extended2 the additional drag resulting in a missing fuselage or wing element ?
4.
1, 4, 3. 3. 1, 2.
Question 70-22 : The duration of a fms navigation database loaded before expiring is ?
28 days.
15 days. 2 months. 3 months.
Question 70-23 : The role of the fms is to 1 aid the crew with navigation2 shut down the engine in case of a malfunction 3 automatically avoid conflicting traffic when autopilot engaged4 reduce crew workload5 aid fuel efficiency the combination that regroups all of the correct statements is ?
1 4 5.
2, 3, 4, 5. 1, 2, 3. 1, 3, 4.
Question 70-24 : The role of the fms is to aid the flight crew with 1 immediate actions in case of emergency procedure2 navigation3 in flight performance optimization4 electronic check liststhe combination that regroups all of the correct statements is ?
2 3.
2, 3, 4. 3, 4. 1, 2.
Question 70-25 : In a fms mcdus are used pre flight to manually initialise with dispatch information the 1 inertial reference system when installed 2 flight director and auto flight control system3 air data computer4 flight management computerthe combination regrouping all of the correct statements is ?
1 4.
2. 1, 3. 2, 3, 4.
Question 70-26 : The 'overfly' symbol related to a waypoint on an fms page indicates that ?
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.
Question 70-27 : The fms required time of arrival rta function can provide ?
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.
Question 70-28 : The fuel management performed by most fms along the flight plan is considered as ?
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.
Question 70-29 : Some of the fms have a navigation mode called dead reckoning mode dr computing airspeed heading wind data ground speed and time this mode is ?
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.
Question 70-30 : The fms lateral offset function consists in ?
Flying along the flight plan legs with a constant right or left offset manually entered on the fms cdu.
A lateral offset may be specified up to 999 nautical miles left or right of courseon the nd navigation display an offset route selected through the fmc is displayed with a dot dash line magenta parallel to the active routeDisplaying 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.
Question 70-31 : The fms navigation database includes the following data 1 airports2 obstacles3 navaids4 airways5 reliefthe combination that regroups all of the correct statements is ?
1 3 4.
1, 2, 3. 2, 5. 1, 3, 4, 5.
Question 70-32 : The most common sensors interfacing a fms to compute the aircraft position along the flight plan are 1 gps2 ndb3 dme4 localizerthe combination that regroups all of the correct statements is ?
1 3.
1, 2, 3. 2, 3. 1, 4.
Question 70-33 : For a fms designed with the vertical navigation vnav capability coupled to the autopilot the fms vertical command output can be 1 an angle of attack2 a flight path angle3 a speed targetthe combination that regroups all of the correct statements is ?
2 3.
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 descentwith the vnav mode engaged the fms commands afds autopilot flight director system pitch and at 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 points1, 2. 1, 3. 2.
Question 70-34 : The fms navigation database includes the following data 1 obstacles2 navaids3 sid star and approaches procedures4 waypoints5 airwaysthe combination that regroups all of the correct statements is ?
2 3 4 5.
1, 2, 3, 4, 5. 1, 2, 4. 1, 3, 5.
Question 70-35 : The fms provides the following functions 1 aid for fuel management2 lateral flight plan management3 check list completion4 aircraft position computationthe combination that regroups all of the correct statements is ?
1 2 4.
1, 2, 3. 2, 3. 3, 4.
Question 70-36 : The fms cross track xtk is ?
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.
Question 70-37 : The fms vertical navigation management is generally performed based on ?
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).
Question 70-38 : The fms navigation database includes the following data 1 airports2 take off speeds 3 navaids4 relief 5 runwaysthe combination that regroups all of the correct statements is ?
1 3 5.
1, 2, 3. 3, 4, 5. 1, 2, 5.
Question 70-39 : In a dual fms architecture when an incompatibility between the two fmc's occurs fmc=flight management computer ?
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.
Question 70-40 : Considering a two fms architecture working in dual mode fmc flight management computer or fms calulator ?
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.
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