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Question 208-1 : In order to measure the radial from a vor the aircraft vor receiver ? [ Exam pilot ]
Measures the phase difference between the reference phase and the variable phase of the signal
Question 208-2 : Assuming a five dot display on either side of the ils localiser cockpit display what is the angular displacement of the aircraft from the localiser centreline when the cdi is deflected 2 dots to the right ?
10° to the left.
Five dot display on either side course deviation indicator cdi 2586if the cdi is deflected 2 dots to the right we have to turn right to correct our path so we are on the left of the centerline exactly 1° to the left2.0° to the left. 2.0° to the right. 1.0° to the right.
Question 208-3 : An ndb is on a relative bearing of 316° from an aircraft given compass heading 270° deviation 2°wat aircraft variation 30°e at station variation 28°ecalculate the true bearing of the ndb from the aircraft ?
254°.
2587compass heading deviation west = magnetic heading270° 2°w = 268°magnetic heading + variation east = true heading268° + 30° = 298°the ndb is on a relative bearing of 316° from the aircraft 360° 316° = 44° left of the nose the true bearing to the beacon is 298° 44° = 254°252°. 072°. 074°.
Question 208-4 : If you are on an ils approach and in case your glide slope indicator shows a deviation of more than half scale deflection downwards ?
You should commence a go around because obstacle clearance is no longer ensured.
You maintain pitch until you regain the desired glide slope. you may keep on flying the approach if you are on centerline. there will be significant beam bends encountered.
Question 208-5 : An aircraft at fl 100 should be able to receive a vor groundstation at 100 ft above msl at an approximate maximum range of ?
135 nm.
For coverage and range to calculate the range in nm official learning objectives formula is 123 x square root transmitter height in feet + 123 x square root receiver height in feet123 x sqrt100 + 123 sqrt10000 = 1353 nm sqrt square root 123 nm. 130 nm. 145 nm.
Question 208-6 : An aeroplane flies over position a which is due north of a vor station sited at position bthe magnetic variation at a is 18°w and at b is 10°wwhat radial from b is the aircraft on ?
010°.
The aircraft is positioned due north of the vor on a bearing of 000° true magnetic variation is applied at the vor ground station therefore in this case a magnetic variation of 010°w is appliedwhen variation is west this means that at the vor magnetic north is to the west of true north 2588the aircraft is on the 010° radial from the vor018°. 350°. 342°.
Question 208-7 : Full deflection on a glide slope indicator indicates that the aircraft is ?
07° above or below the correct glide path.
25891.25° above or below the correct glide path. 1.5° above or below the correct glide path. 2.5° above or below the correct glide path.
Question 208-8 : On what carrier frequency does the inner marker transmit ?
75 mhz.
According to icao annex 10 all marker beacons operate on 75 mhz carrier frequency modulation frequencies are outer marker 400 hzmiddle marker 1300 hzinner marker 3000 hzSame frequency as the localizer. same frequency as the glide path. 3000 hz.
Question 208-9 : The indicated range from a dme station is ?
Slant range.
The indicated range from a dme station is slant range 2590Ground range. 0 when passing overhead the station. ground range only if the beacon is co-located with vor.
Question 208-10 : According to icao 8168 what is regarded as the maximum safe deviation below the glide path during ils approach ?
Half scale deflection.
Icao doc 8168 33 flight procedures for racetrack and reversal procedures 334 descent the aircraft shall cross the fix or facility and fly outbound on the specified track descending as necessary to the procedure altitudeheight but no lower than the minimum crossing altitudeheight associated with that segment if a further descent is specified after the inbound turn this descent shall not be started until the aircraft is established on the inbound track an aircraft is considered established when it is a within half full scale deflection for the ils and vor orb within ±5° of the required bearing for the ndbOne quarter scale deflection. three quarter scale deflection. full scale deflection.
Question 208-11 : On which of the following displays are you able to get a direct read out no calculation is necessary from the pilot of the magnetic bearing from the aircraft to the ndb ?
Moving card adf and rmi.
2591a fixed card is aligned with a heading of 000° and therefore only displays relative bearingson a rmi on top of the instrument you can read your actual heading on a moving card adf you have to manually align your actual heading with the knobFixed card adf and rmi. moving and fixed card adf. fixed card adf only.
Question 208-12 : What according to icao annex 10 is the range of a locator ?
10 25 nm.
25 - 50 nm. 50 - 100 nm. 100 - 300 nm.
Question 208-13 : According to icao annex 10 in which frequency band s does a locator normally transmit ?
Lfmf.
Vor operating frequencies vhflocaliser vhfmarker beacon vhfdme operating frequencies uhfglide slope uhfgnssgps uhfl1 and l2 frequencies used by navstargps uhfils localiser and glide slope vhf and uhf bandsmicrowave landing system mls shfairborne weather radars shflocator lfmfMf/hf. hf. hf/vhf.
Question 208-14 : A vor and an ndb are co located an aircraft equipped with an rmi is flying away from the beacons on a radial of 090° through an area where magnetic variation is changing rapidlywhich statement is correct ?
The adf needle moves the vor needle does not.
Application of magnetic variation is at beacon position for a vor and at aircraft position for a ndb only the adf relative bearing will show the change of magnetic variationNeither the vor or the ndb needles move. both vor and adf needles move. the vor needle moves, the adf needle does not.
Question 208-15 : Which of these markers has the highest audible frequency ?
Inner.
Outer. middle. airways.
Question 208-16 : A mls without dme p provides ?
An ils like approach.
An approach with a curved path but not staged. a category 3 approach. a staged approach but not with a curved path.
Question 208-17 : False beams on the ils glidepath are ?
Only found above the correct glideslope.
Only found if flying the backbeam ils approach. only found if more than 10° left or right of localiser centreline. only found below the correct glideslope.
Question 208-18 : On an ils approach the glidepath needle is fully down how much deflection does this indicate ?
07°.
2589full scale deflection on the glidepath needle corresponds to approximately 07° from the ils glidepath centre line2.5°. 10°. 5°.
Question 208-19 : The audio modulation of the middle marker is keyed to give ?
Alternating dots and dashes at a rate of 2 dashes per second and 6 dots per second.
Continuous dashes at a rate of 2 per second. continuous dots at a rate of 6 per second. a sequence of 3 dashes, 3 dots and 3 dashes every second.
Question 208-20 : If you are flying a back course ils you are flying a ?
Non precision approach on the reciprocal runway of the precision approach runway.
In a conventional localizer the signal radiates outwards from the end of the runway along the extended center line of the runway usually a by product of this is a signal that radiates in the reverse direction some installations take advantage of this 'spurious signal' and use it for an instrument approach 2592localizer signal also 'propagating' in the opposite direction back down the runwayfor information a non precision approach is an instrument approach and landing which utilises lateral guidance but does not utilise vertical guidancea precision approach is an approach in which range azimuth and glide slope information are provided to the pilotNon precision approach on the precision approach end of the runway. precision approach on the reciprocal runway of the precision approach runway. precision approach on the precision approach runway.
Question 208-21 : What is a vdf referenced to ?
Magnetic north at the station.
Vdf stations are capable of measuring the direction of arrival of radio transmissions from aircraft vdf measures the bearing of the aircraft with reference to true or magnetic north at the stationMagnetic north at the aircraft. true north at the aircraft. relative bearing to the aircraft.
Question 208-22 : A locator 1 is a low powered beacon2 is a high powered beacon3 has a range of 10 25 nm4 has a range of 10 400 nm ?
1 and 3.
1 and 4. 2 and 3. 2 and 4.
Question 208-23 : Which of the following alternatives is correct regarding audio and visual signals in the cockpit when passing overhead a middle marker ?
Audio 1300 hz alternating dots and dashesvisual amber.
Audio: 400 hz, 2 dashes per second. xsxvisual: blue. audio: 75 mhz, 2 dashes per second. xsxvisual: blue. audio: 3000 hz, alternating dots and dashes. xsxvisual: amber.
Question 208-24 : Concerning the localiser principle of operation in an ils the needle of the aircraft indicator is centred when the difference in depth of modulation ddm is ?
Null.
Maximum. less than 90 hz. more than 150 hz.
Question 208-25 : Concerning the glidepath principle of operation in an ils system the needle of the indicator is centred when the difference in depth of modulation ddm is ?
Null.
Maximum. less than 90 hz. 150 hz or 90 hz.
Question 208-26 : An ils receiver ?
Measures the difference in depth of modulation of the two transmitted signals.
Measures the phase difference between the two transmitted signals. compares the difference in frequency of the two transmitted signals. measures the phase rotation of the two transmitted signals.
Question 208-27 : Mls is primarily being installed at airports where ?
Ils encounters difficulties because of surrounding buildings andor the terrain or interference from local music stations.
Meteorological conditions are likely to cause ils ducting by super refraction. the main approach paths lead over water. topographical conditions preclude the installation of ils marker beacons.
Question 208-28 : The ils marker identified audibly by a series of dots 6 per second is the ?
Inner marker.
Middle marker. locator. outer marker.
Question 208-29 : With regard to the range of ndb's and the accuracy of the bearings they provide can be stated that in general at night ?
The range increases and the accuracy decreases.
The range decreases and the accuracy increases. the range and the accuracy both increase. the range and the accuracy both decrease.
Question 208-30 : Which statement is correct with respect to the range of an ndb ?
With propagation over sea the range will be greater than the range with propagation over land.
Ndb signals follow the curvature of the earth so they can be received at much greater distances at lower altitudes a major advantage over vorhowever ndb signals are also affected more by atmospheric conditions mountainous terrain coastal refraction and electrical storms particularly at long rangeThe range depends on the altitude of the aircraft. during the night the range of an ndb will decrease due to the interference of the direct and earth reflected wave. in order to double the range of an ndb, the transmission power should be increased with a factor 16.
Question 208-31 : Which statement is correct for homing towards an ndb in an area with constant wind and constant magnetic variation ?
The relative bearing of the ndb should be kept 000°.
If the pilot is flying directly to the station the bearing indicator points to 0° 2593relative bearing is the angle formed by the intersection of a line drawn through the centerline of the aircraft and a line drawn from the aircraft to the radio station this angle is always measured clockwise from the nose of the aircraft and is indicated directly by the pointer on the bearing indicator pay attention a question looks similar but instead of 'homing' you have 'tracking' and it is different homing you are following the adf needle direction you will drift you constantly change heading to reach the stationtracking you fly at constant course to reach the beacon you apply a wind correction angleThe relative bearing of the ndb should be equal (in magnitude and sign) to the experienced drift angle. the relative bearing of the ndb should be equal (in magnitude and sign) to the applied wind correction angle. the relative bearing of the ndb should be equal to the qdm.
Question 208-32 : Which statement is correct for tracking towards an ndb in an area with constant wind and constant magnetic variation ?
The relative bearing of the ndb should be equal in magnitude and sign to the experienced drift angle.
Relative bearing is the direction of the station expressed as an angle measured clockwise from the forward point of the longitudinal axis of an aircraftin order to fly directly onto the station you must apply a drift except if it's headwind or tailwind com encom062 390jpg pay attention the question 389 looks similar but instead of 'tracking' you have 'homing' and it is different tracking you fly at constant course to reach the beacon you apply a wind correction anglehoming you are following the adf needle direction you will drift you constantly change heading to reach the stationThe relative bearing of the ndb should be kept 000°. the relative bearing of the ndb should be equal (in magnitude and sign) to the applied wind correction angle. the relative bearing of the ndb should be equal to the qdm.
Question 208-33 : The dme line of position is a circle with radius at ?
The ground distance and centre the dme station.
Dme line of position definition a position line using dme is a circle with the station at its centre the distance measured by dme is slant range however the circle is at the ground distance and centre the dme station 2590The slant range and centre the dme-station. the ground distance and centre the aircraft. the slant range and centre the aircraft.
Question 208-34 : The localiser transmits in ?
The vhf band.
Vor operating frequencies vhflocaliser vhfmarker beacon vhfdme operating frequencies uhfglide slope uhfgnssgps uhfl1 and l2 frequencies used by navstargps uhfils localiser and glide slope vhf and uhf bandsmicrowave landing system mls shfairborne weather radars shflocator lfmfThe uhf band. the hf band. both uhf and vhf bands.
Question 208-35 : What is the effect of fm broadcast stations that transmit on frequencies just below 108 mhz on the performance of ils ?
These transmissions may interfere with the ils localizer signal which may lead to erroneous localizer deviation indication.
Fm broadcast stations that transmit on frequencies just below 108 mhz may lead to erroneous localizer deviation indicationthis factor affecting range and accuracy of the ils localizer signalThese transmissions may interfere with the ils localizer and glide path signals which may lead to erroneous deviation indications. these transmissions may activate the fm immune filter which results in the appearance of the localizer failure flag. these transmissions may activate the fm immune filter which results in the appearance of the localizer and glide path failure flag.
Question 208-36 : What is the function of a fm immune filter ?
To make the ils localizer receiver less susceptible to interference from commercial fm stations radio and television .
Jomargra why the ils glide path is not affected gs is in the uhf range and tv is also in the uhf fm immunity relates in reality solely to the bottom end of the vhf nav band and solely to receiversit all happened when the government sold off the 'guard band' the gap in the frequency allocation between fm broadcasting and aircraft navigation so the fm broadcasters now come right up to the edge by 108 mhz but not the tv broadcastersTo make both the ils-localizer- and glide path receiver less susceptible to interference from commercial fm-stations (radio and television). to make the ils localizer receiver less susceptible to interference from earth-reflected localizer-signals. to make both the ils-localizer- and glide path receiver less susceptible to interference from earth-reflected localizer-signals.
Question 208-37 : On the rmi the tip of a vor needle indicates 060°with the crs set on 055° the indications on the hsi are ?
To half scale deflection to the right.
2594to avoid risks of confusion we assume that we are on course to the station our heading is superposed with the rmi indication note that the result will be the same whatever your heading is we are on the radial 240°half scale deflection to the right vor has 5 dots to either side of center and eah dot represents 2° of deviation we are on radial 240° and we selected a crs 055° radial 235° 5° deviation half scale deflectionfor training purpose luizmonteiro learning vorTo, half scale deflection to the left. from, half scale deflection to the left. from, half scale deflection to the right.
Question 208-38 : To provide a pilot with the position of the aircraft in the absence of radar atc must have at its disposal at least ?
Two vdf's at different locations able to take bearings simultaneously on the transmitted frequency.
Vdf is the abbreviation for 'vhf direction finder' vdf stations are capable of measuring the direction of arrival of radio transmissions from aircraft vdf measures the bearing of the aircraft with reference to true or magnetic north at the stationwith two vdf's at different locations atc is able to provide the position of the aircraftTwo co-located vdf's, able to take bearings simultaneously on the transmitted frequency. one vdf able to take simultaneous bearings on different frequencies. three vdf's at different locations able to take simultaneous bearings on different frequencies.
Question 208-39 : Vdf is the abbreviation for ?
Vhf direction finder.
Vdf direction finder. very direct finder. very high frequency deviation finding station.
Question 208-40 : The transmission of the glide slope beacon is characterised by a ?
Uhf frequency with a minimum range of 10 nm.
Vor operating frequencies vhflocaliser vhfmarker beacon vhfdme operating frequencies uhfglide slope uhfgnssgps uhfl1 and l2 frequencies used by navstargps uhfils localiser and glide slope vhf and uhf bandsmicrowave landing system mls shfairborne weather radars shflocator lfmfVhf frequency modulated with a 90 hz am and 150 hz am navigation signal. 300 to 3000 hz amplitude modulation for the atis. uhf carrier frequency with a possible 'voice ident'.
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