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RADNAV-RH-CHAPTER2-NDB
1.
An NDB has a range of 50 nm with a power output of 80 watts: The power required to increase the range to 75 nm is:
a) 120 watts
b) 150 watts
c) 180 watts
d) 320 watts
2.
NDB operate in the:
a) VLF and LF bands
b) LF and MF bands
c) VLF, LF and MF bands
d) VLF and MF bands
3.
When converting VOR and ADF bearings to true, the variation at the (i) should be used for VOR and at the (ii) for ADF:
a) (i) Aircraft; (ii) aircraft
b) (i) Aircraft; (ii) station
c) (i) Station; (ii) aircraft
d) (i) Station; (ii) station
4.
The allocated coverage of NDBs is:
a) 250 – 450 KHz
b) 190 – 1750 KHz
c) 108 – 117.95 MHz
d) 200 – 500 KHz
5.
NDBs transmit mainly in the:
a) VHF band
b) UHF band
c) HF band
d) MF band
6.
When receiving an NDB signal on an ADF receiver the BFO can be selected OFF for the:
a) tone signal on NONA1A
b) ident signal on NONA1A
c) tone signal on NONA2A
d) ident signal on NONA2A
7.
Which of the following may cause inaccuracies in ADF bearings?
a) static interference, height effect, lack of failure warning
b) station interference, mountain effect, selective availability
c) coastal refraction, slant range, night effect
d) lack of failure warning, station interference, static interference
8.
An aircraft is HOMING to a radio beacon whilst maintaining a relative bearing of zero. If the magnetic heading decreases, the aircraft is experiencing:
a) left drift
b) right drift
c) a wind from the west
d) zero drift
9.
Using an NDB it is possible to experience which of the following errors or limitations?
a) Coastal refraction, timing error and night effect
b) Night effect, station interference and latitude error
c) Night effect, station interference and lack of a failure warning system
d) Coastal refraction, timing error and lack of a failure warning system
10.
With a transmission from an NDB aerial, the ___ component travels in the ___ plane and the signal is ___ polarised.
a) magnetic; horizontal; vertically
b) electrical; horizontal; vertically
c) electrical; vertical; horizontally
d) magnetic; vertical; horizontally
11.
The BFO selector on an ADF receiver is used to:
a) find the loop NULL position
b) stop loop rotation
c) hear the IDENT and must always be switched ON
d) hear the IDENT of some NDB stations radiating a continuous wave signal
12.
When considering the propagation of ADV transmissions night effect is most pronounced:
a) at dusk and dawn
b) during the long winter nights
c) at or near the coast
d) when flying at low altitude
13.
In order to obtain an ADF bearing the:
a) signal must be received by both the sense and loop aerials
b) sense aerial must be tuned separately
c) mode selector should be switched to LOOP
d) BFO switch must be selected to ON
14.
An NDB signal crossing from land to sea will ___ speed and bend ___ the normal.
a) decrease, towards
b) increase, towards
c) decrease, away from
d) increase, away from
15.
Errors caused by the effect of coastal refraction on bearings at lower altitudes are maximum when the NDB is:
a) near the coast and the bearing crosses the coast at right angles
b) inland and the bearing crosses the coast at an acute angle
c) inland and the bearing crosses the coast at right angles
d) near the coast and the bearing crosses the coast at an acute angle
16.
Which one of the following disturbances is most likely to cause the greatest inaccuracy in ADF bearings?
a) Coastal effect
b) Local thunderstorm activity
c) Quadrantal error
d) Precipitation interference
17.
Which of the following is the ICAO allocated frequency band for ADF receivers?
a) 255 – 455 kHz
b) 190 – 1750 kHz
c) 300 – 3000 kHz
d) 200 – 2000 kHz
18.
The accuracy of ADF within the DOC by day is:
a) +/-1 deg
b) +/-2 deg
c) +/-5 deg
d) +/-10 deg
19.
The D layer of the ionosphere affects the accuracy of NDB bearings:
a) by day and night
b) by day only
c) by night only
d) never
20.
An RMI indicates aircraft heading. To convert the RMI bearings of NDBs and VORs to true bearings the correct combination for the application of magnetic variation is:
a) NDB: aircraft position
VOR: aircraft position
b) NDB: beacon position
VOR: beacon position
c) NDB: beacon position
VOR: aircraft position
d) NDB: aircraft position
VOR: beacon position
21.
The signal to noise ratio for an NDB is ___ allowing a maximum error of ___ on 95% of occasions during ___
a) 3/1, ±5 degrees, daylight hours only
b) 3/1, ±5 degrees, 24 hours
c) 5/1, ±3 degrees, 24 hours
d) 5/1, ±3 degrees, daylight hours only
22.
When is coastal error at its worst for an aircraft at low level?
a) Beacon inland at an acute angle to the coast
b) Beacon inland at 90o
c) Beacon close to the coast at an acute angle to the coast
d) Beacon close to the coast at 90o to the coast
23.
An aircraft over the sea is receiving a signal from an NDB 50nm from the coast and another from an NDB 20nm from the coast. Which of the following statements is most correct?
a) The bearing information from relative bearings of 90o and 270o would be most correct
b) The bearing information from relativebearings of 360o and 180o would be most correct
c) The bearing information from the beacon 20nm inland would be most correct
d) The bearing information from the beacon 50nm inland would be most correct
24.
Which of the following is likely to have the greatest effect on ADF accuracy?
a) Interference from other NDBs, particularly during the day
b) Frequency drift at the ground station
c) Interference from other NDBs, particularly at night
d) Mutual interference between aircraft aerials
25.
There are two NDBs, one 20 NM inland, and the other 50 NM inland from the coast. Assuming that the error caused by coastal refraction is the same for both propagations, the extend of the error is a position line plotted by an aircraft that is over water will be:
a) the same from both beacons when the aircraft is on a relative bearing of 180o and 360o
b) greater from the beacon that is 20 NM inland
c) the same from both beacons when the aircraft is on a relative bearing of 090o and 270o
d) greater from the beacon that is 50 NM inland
26.
An ADF uses a sense aerial to:
a) determine the null position
b) resolve ambiguous bearings
c) transmit the beacon ident
d) detect the receiver test signal
27.
The BFO:
a) creates the audio ident for an NDB
b) is used to make the ident from an A2A NDB audible
c) is used to make the ident from an A1A NDB audible
d) is used to determine the signal strength of an NDB
28.
What is the role of a ground direction finder?
a) To aid pilot navigation
b) To halt ground movements
c) To map airfields
d) To assist planners in the construction of airfield approaches
29.
With regard to the following types of NDB which statements is correct?
a) Locators have 200 W power, 50 nm range and are NON A2A
b) Locators have 15 W power, 10-25 nm range and are NON A2A
c) Locators have 5000 W power, 50 nm range and are NON A2A
d) Locators have 5000 W power, 50 nm range and are NON A1A
30.
If an NDB with a transmitter power of 25 KW which has a range of 50 nm is adjusted to give a power output of 100 KW the new range of the NDB will be approximately:
a) 100 nm
b) 200 nm
c) 300 nm
d) 400 nm
31.
A cumulonimbus cloud in the vicinity of an aeroplane can cause certain navigation systems to give false indications. This is particularly true of the:
a) ADF
b) VOR
c) weather radar
d) DME
32.
An RMI indicates aircraft heading and bearing. To convert the RMI bearings of NDBs and VORs to true bearings the correct combination for the application of magnetic variation is:
a) NDB: aircraft position
VOR: aircraft position
b) NDB: beacon position
VOR: beacon position
c) NDB: beacon position
VOR: aircraft position
d) NDB: aircraft position
VOR: beacon position
33.
In order to obtain an ADF bearing on a system using sense and loop aerials, the:
a) mode selector should be switched to ‘loop’
b) sense aerial must be tuned separately
c) signal must be received by both the sense and loop aerials
d) BFO switch must be selected to ‘ON’
34.
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?
a) Fixed card ADF and RMI
b) Moving card ADF and RMI
c) Moving and fixed card ADF
d) Fixed card ADF only
35.
The BFO selector switch on the ADF control panel must be in the ‘on’ position to enable the pilot to:
a) stop the loop rotation
b) adjust the loop to the aural null position
c) hear the IDENT of NDBs using NON A1A transmissions
d) hear the IDENT of NDBs using NON A2A transmissions
36.
There are two NDBs, one 20 NM inland, and the other 50 NM inland from the coast. Assuming that the error caused by coastal refraction is the same for both propagations, the extent of the error in a position line plotted by an aircraft that is over water:
a) greater from the beacon that is 20 NM inland
b) the same from both beacons when the aircraft is on a relative bearing of 180o and 360o
c) greater from the beacon that is 50 NM inland
d) the same from both beacons when the aircraft is on a relative bearing of 090o and 270o
37.
What according to ICAO Annex 10 is the range of a locator?
a) 50 – 100 NM
b) 25 – 50 NM
c) 10 – 25 NM
d) 100 – 300 NM
38.
What actually happens in the ADF receiver when the BFO position is selected?
a) The BFO circuit is activated, and the receiver accepts only A1A modulated signals
b) The BFO circuit oscillates at an increased frequency in order to allow identification of A2A NDBs
c) The BFO circuit is de-activated
d) The BFO circuit imposes a tone onto the carrier wave to make the NDB’s ident audible
39.
Which of the following is correct regarding the range of an NDB?
a) The range is limited to the line of sight
b) Aircraft height is not limiting for the reception of signals from the NDB
c) The range of an NDB will most likely increase at day time compared to night time
d) The transmitter power of the NDB station has no affect on the range
40.
You are on a magnetic heading of 055o and your ADF indicates a relative bearing of 325o. The QDM is:
a) 235o
b) 200o
c) 055o
d) 020o
41.
What gives the greatest error in ADF:
a) Coastal effect
b) Night effect
c) Static interference from thunderstorms
d) Quadrantal error
42.
The nominal maximum range of an NDB ith a transmitter power is 200 watts is:
a) 40 to 45 NM
b) 100 to 120 NM
c) 150 to 170 NM
d) 200 to 220 NM
43.
The ICAO allocated band of frequencies for NDB is:
a) 255 – 455 KHz
b) 200 – 1750 KHz
c) 255 – 1750 KHz
d) 200 – 455 KHz
44.
An aircraft 10 nm from a north-south coastline takes two three-position line fixes from an inland NDB. The aircraft’s indicated position is:
a) Nearer to the coastline than its actual position
b) Further from the coastline than its actual position
c) Correct because the coastal refraction errors will cancel out because two fixes have been taken
d) Correct in azimuth but false in range
45.
Using an ADF loop aerial the maximum signal will be received when:
a) The loop is in line with the NDB aerial
b) The loop is at 90o to the NDB aerial
c) Within the promulgated range
d) During daytime only
46.
When identifying an NDB (NON A1A) it is necessary to:
a) Turn the BFO on
b) Turn the BFO off
c) Turn the ANT on
d) Turn the ANT off
47.
Which of the following are all errors associated with ADF:
a) selective availability, coastal refraction, night effect
b) night effect, quadrantal error, lane slip
c) mountain effect, station interference, static interference
d) selective availability, coastal refraction, quadrantal error
48.
What action must be taken to receive a bearing from an ADF:
a) BFO on
b) Select the loop position
c) Both the loop and sense aerials must receive the signal
d) Select the ANT position
49.
Which of the following is the most significant error in ADF:
a) quadrantal error
b) coastal refraction
c) precipitation static
d) static from Cb
50.
When using ADF (i), the accuracy is (ii) than iii), because the surface wave is (iv):
a) (i) by day; (ii) greater; (iii) by night; (iv) not present
b) (i) by night; (ii) greater; (iii) by day; (iv) not present
c) (i) by night; (ii) less; (iii) by day; (iv) contaminated by sky waves
d) (i) by day; (ii) less; (iii) by night; (iv) contaminated by sky waves
51.
Snow will affect ADF by:
a) Decreasing the range
b) Decreasing the accuracy
c) Having no effect
d) Decreasing the range and accuracy
52.
Do all ADF systems have a sense aerial:
a) Always
b) Only when a rotating loop system is being used
c) Never
d) Only when a fixed loop system is being used
53.
If an NDB signal is received at a range of 1000 nm:
a) The signal is a surface wave and is quite usable
b) It will be a ground wave and will be inaccurate
c) It is a space wave and will be inaccurate
d) It is a sky wave and is inaccurate
54.
The maximum errors when using ADF will occur in which of the following situations: (i) Position of the NDB (ii) Angle of cut at the coast
a) (i) On the coast; (ii) 90o
b) (i) Well inland; (ii) 90o
c) (i) On the coast; (ii) 15o
d) (i) Well inland; (ii) 20o
55.
When considering the use of NDB, night effect has its greatest effect during:
a) Autumn and winter
b) When using inland beacons
c) When using a horizontally polarised signal
d) At dawn and dusk
56.
An aircraft over the sea will experience (i) coastal refraction effect when the radio waves cross the coastline at (ii) and the NDB is (iii):
a) (i) More; (ii) 90o; (iii) Near the coast
b) (i) Less; (ii) 45o; (iii) Well inland
c) (i) Less; (ii) 90o; (iii) Near the coast
d) (i) More; (ii) 45o; (iii) On the coast
57.
An ADF is correctly tuned to an NDB, the needle is “hunting” and the signal is fading and growing louder alternately, the reason for this is:
a) The required sky wave is being interfered with by the ground wave from another NDB
b) The required ground wave is being contaminated by sky waves
c) Scalloping
d) The aircraft is flying outside the designated operational coverage
58.
Two NDBs, one 20 nm from the coast and the other 50 nm further inland. Assuming Coastal Refraction is the same for each, from which NDB will an aircraft flying over the sea receive the greatest error?
a) The NDB at 20 nm
b) The NDB at 50 nm
c) Same when the relative bearing is 090/270
d) Same when the relative bearing is 180/360
59.
What antennae must be used to obtain an ADF bearing?
a) Loop
b) Sense
c) Loop and sense
d) Radome
60.
For long range NDB’s the most common type is:
a) LF NON A1A
b) LF NON A2A
c) MF NON A1A
d) MF NON A2A
61.
The 95% accuracy for ADF bearings of an NDB by day is:
a) ±2o
b) ±7o
c) ±10o
d) ±3o
62.
A radio beacon has range of 10 nm. By what factor should the power be increased to achieve a range of 20 nm?
a) 16
b) 2
c) 4
d) 8
63.
A NDB transmits a signal pattern which is:
a) A 30 Hz polar diagram
b) Omni-directional
c) A bi-lobal pattern
d) A beam rotating at 30 Hz
64.
The frequency band chosen for NDB’s is:
a) upper MF and lower LF
b) VLF
c) upper LF and lower MF
d) LF
65.
An NDB transmits a signal pattern in the horizontal plane which is:
a) a beam rotating at 20 Hz
b) bi-local circular
c) a cardioid balanced at 30 Hz
d) omnidirectional
66.
Factors liable to affect most NDB/ADF system performance and reliability include:
a) height error – station interference – mountain effect
b) static interference – station interference – latitude error
c) static interference – night effect – absence of failure warning system
d) coastal refraction – lane slip – mountain effect
67.
When ADF equipment which incorporates a sense aerial and a loop aerial is tuned to a NDB and the loop aerial is rotated so that a sharp null is found the aerial is:
a) either at right angles or in line with the incoming signals
b) in line with the incoming signals
c) at right angles to the incoming signals
d) aligned with the aircraft nose
68.
Quadrantal errors associated with aircraft Automatic Direction Finding (ADF) equipment are caused by:
a) misalignment of the loop aerial
b) signal bending caused by electrical interference from aircraft wing
c) signal bending by the aircraft metallic surfaces
d) sky wave/ground wave contamination
69.
A radio beacon has an operational range of 10 NM. By what factor should the transmitter power be increased in order to achieve an operational range of 20 NM?
a) Eight
b) Six
c) Four
d) Two
70.
Which of the following factors could cause an error of an ADV bearing of an NDB?
a) Scalloping
b) Atmospheric scatter
c) Phase interference
d) Night effect
71.
Night Effect which causes loss of signal and fading, resulting in bearing errors from NDB transmissions, is due to:
a) sky wave distortion of the null position and is maximum at dawn and dusk
b) interference from other transmissions and is maximum at dusk when east of the NDB
c) static activity increasing at night particularly in the lower frequency band
d) the effect of the Aurora Borealis
72.
An aircraft heading 315oM shows an NDB bearing 180o on the RMI. Any quadrantal error affecting the accuracy of this bearing is likely to be:
a) zero, as quadrantal errors are not found on the RMI
b) at a maximum
c) at a minimum
d) zero, as quadrantal errors affect only the VOR
73.
The purpose of the BFO switch on the ADF receiver is to:
a) make the signal audible
b) cut out the static noise
c) improve the strength of the received signal
d) attenuate the received signal
74.
A long range NDB is likely to transmit on ___ and be classified as ___ Select the answer to complete this statement
a) 200 Khz; A2A
b) 800 Khz; A2A
c) 200 Khz; A1A
d) 800 Khz; A1A
75.
The nominal maximum range of an NDB with a transmitter power is 200 watts is:
a) 50 to 60 nm
b) 100 to 120 nm
c) 150 to 170 nm
d) 200 to 200 nm
76.
An aeroplane is flying parallel to a coast. Which of the following NDBs will give the greatest costal refraction LOP error?
a) NDB sited on the coast-RBI 330o
b) NDB sited 30 nm inland-RBI 330o
c) NDB sited on the coast-RBI 300o
d) NDB sited 30 nm inland-RBI 300o
77.
Which of the following is true about the ADF?
a) Its accuracy is the same by day and by night
b) It does not have a signal failure warning
c) It should not be used at night because of sky waves
d) Sky waves do not affect the bearing accuracy provided they come from the correct NDB
78.
What is the approved frequency band assigned to aeronautical NDBs?
a) 190-1750 Hz
b) 190-1750 KHz
c) 190-1750 MHz
d) 190-1750 GHz
79.
An NDB aerial is (i) so as to ensure the range is (ii) by minimising (iii) due to (iv):
a) (i) horizontal; (ii) maximum; (iii) diffraction; (iv) the ground wave
b) (i) vertical; (ii) maximum; (iii) attenuation; (iv) energy losses to the surface
c) (i) horizontal; (ii) maximum; (iii) refraction; (iv) the D layer
d) (i) vertical; (ii) maximum; (iii) attenuation; (iv) atmospheric refraction
80.
ADF bearings by an aeroplane by day within the published protection range should be accurate to within a maximum error of:
a) +/-10o
b) +/-2.5o
c) +/-2o
d) +/-5o
81.
An ADF provides the aircraft with bearing information with respect of a ground station. To do this, the ground station emits a signal pattern which is:
a) a beam rotating at 30 Hertz
b) frequency modulated at 30 Hertz
c) omni-directional
d) unidirectional
82.
In accordance with Doc 8168, a pilot flying an NDB approach must achieve a tracking accuracy within ___ of the published approach track.
a) +/-1
b) +/- 5o
c) +/- 2.5o
d) +/- 2o
83.
Which combination gives the greatest reduction in reliability of ADF:
a) Station interference; Static interference; Lane slip
b) Mountain effect; Station interference; site error
c) Night effect; Static interference; Quadrantal error
d) Nigh effect; Quadrantal error; Station interference
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