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CPL Test Series
Question Bank
Questions for INDIGO RADIO NAVIGATION
Answer the following questions
Test Mode
Training Mode
1. ADF bearings by an aeroplane by day within the published protection range should be accurate to within a maximum error of
+/-2.5°
+/-5°
+/-10°
+/-2°
2. In an Airborne Weather Radar that has a colour cathode ray tube (CRT) the areas of greatest turbulence are indicated on the screen by
blank iso-echo areas where there is no colour
large areas of flashing red colour
iso-echo areas which are coloured black
colour zones being closest together
3. What is the wavelength of an NDB transmitting on 375 kHZ?
80 m
800 m
8000 m
8 m
4. In which frequency band do most airborne weather, and ground based ATC, radar systems operate?
SHF
EHF
VHF
UHF
5. What is the colour sequence when passing over an Outer, Middle and Inner Marker beacon?
blue - green - white
blue - amber - white
amber - white - green
white - amber - blue
6. An aircraft tracking to intercept the Instrument Landing System (ILS) localiser inbound on the approach side, outside the published ILS coverage angle
will not normally receive signals
can expect signals to give correct indications
will receive signals without identification coding
may receive false course indications
7. For a conventional DME facility 'Beacon Saturation' will occur whenever the number of simultaneous interrogations exceeds
200
100
60
80
8. Which one of the following is an advantage of a Microwave Landing System (MLS) compared with an Instrument Landing System (ILS)?
There is no restriction on the number of ground installations that can be operated because there is an unlimited number of frequency channels available
It is insensitive to geographical site and can be installed at sites where it is not possible to use an ILS
The installation does not require to have a separate method (marker beacons or DME) to determine range
It does not require a separate azimuth (localiser) and elevation (azimuth) transmitter
9. In which navigation system does the master station transmit a continuous string of pulses on a frequency close to 100 kHz?
Loran C
GPS
Doppler
Decca
10. Under JAR-25 colour code rules for Electronic Flight Instrument Systems (EFIS), turbulence is coloured
white or magenta
black
red
cyan
11. During a flight at FL 210, a pilot does not receive any DME distance indication from a DME station located approximately 220 NM away.The reason for this is that the
range of a DME system is always less than 200 NM
aeroplane is below the 'line of sight' altitude
aeroplane is circling around the station
altitude is too high
12. The OUTER MARKER of an Instrument Landing System (ILS) facility transmits on a frequency of
200 MHz and is modulated by alternate dot/dash in morse
75 MHz and is modulated by alternate dot/dash in morse
75 MHz and is modulated by morse at two dashes per second
300 MHz and is modulated by morse at two dashes per second
13. Ignoring pulse length, the maximum pulse repetition frequency (PRF) that can be used by a primary radar facility to detect targets unambiguously to a range of 200 NM is:(pps = pulses per second)
308 pps
375 pps
782 pps
405 pps
14. In relation to the satellite navigation system NAVSTAR/GPS, which of the following statements correctly describes the term 'Pseudo Random Noise (PRN)' signal?
PRN occurs in the receiver. It is caused by the signal from one satellite being received from different directions (multipath effect)
PRN describes the continuous electro-magnetical background noise that exists in space
PRN is a code used for the identification of the satellites and the measurement of the time taken by the signal to reach the receiver
PRN is the atmospheric jamming that affects the signals transmitted by the satellites
15. Under JAR-25 colour code rules, features displayed in green on an Electronic Flight Instrument System (EFIS), indicate
the ILS deviation pointer
engaged modes
cautions, abnormal sources
the earth
16. A DME that has difficulty obtaining a ""lock-on"":(NOTE: PRF = pulse recurrence frequency, PPS = pulses per second)
stays in search mode but reduces PRF to max. 60 PPS after 100 seconds
alternates search mode with periods of memory mode lasting 10 seconds
stays in search mode but reduces PRF to max. 60 PPS after 15000 pulse pairs have been transmitted
stays in search mode without a reduction in PRF
17. What is the approximate angular coverage of reliable navigation information for a 3° ILS glide path out to a distance of 10 NM?1.35° above the horizontal to 5.25° above the horizontal and 8° each side of the localiser centreline
0.45° above the horizontal to 1.75° above the glide path and 8° each side of the localiser centreline
0.7° above and below the glide path and 2.5° each side of the localiser centreline
3° above and below the glide path and 10° each side of the localiser centreline
1.35° above the horizontal to 5.25° above the horizontal and 8° each side of the localiser centreline
18. A radar facility transmitting at a Pulse Recurrence Frequency (PRF) of 1200 pulses/second will have a maximum unambiguous range of approximately
27 NM
69 NM
270 NM
135 NM
19. The geometric shape of the reference system for the satellite navigation system NAVSTAR/GPS, defined as WGS 84, is
a geoid
a mathematical model that describes the exact shape of the earth
an ellipsoid
a sphere
20. In civil aviation, the height value computed by the receiver of the satellite navigation system NAVSTAR/GPS is the
flight level
geometric height above ground
height above the WGS-84 ellipsoid
height above Mean Sea Level (MSL)
21. Under JAR-25 colour code rules for Electronic Flight Instrument Systems (EFIS), the active route/flight plan is coloured
cyan
magenta
yellow
green
22. Given:VOR station position N61° E025°, variation 13°E,Estimated position of an aircraft N59° E025°, variation 20°E.What VOR radial is the aircraft on?
160°
193°
347°
167°
23. In a primary radar using pulse technique, the ability to discriminate between targets in azimuth is a factor of
beam width
aerial rotation rate
Pulse Recurrence Rate (PRR)
pulse length
24. What is the minimum level that an aircraft, at a range of 113 NM, must fly in order to contact the tower on R/T for a VDF bearing from an airport sited 169 FT above MSL?
FL80
FL100
FL50
FL60
25. In an Electronic Flight Instrument System (EFIS) data relating primarily to navigation is provided by
Navigation radiosFlight Management ComputerInertial Reference Systems
Inertial Reference SystemsNavigation radiosTrue airspeed and drift inputs
Flight Management ComputerAircraft Mapping RadarNavigation radios
Inertial Reference SystemsAircraft Mapping RadarNavigation radios
26. 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 will be
greater from the beacon that is 50 NM inland
the same from both beacons when the aircraft is on a relative bearing of 180° and 360°
the same from both beacons when the aircraft is on a relative bearing of 090° and 270°
greater from the beacon that is 20 NM inland
27. What is the procedure to be followed if, on a flight under IFR conditions using the NAVSTAR/GPS satellite navigation system, the number of satellites required to maintain the RAIM (Receiver Autonomous Integrity Monitoring) function are not available?
The flight has to be continued under VFR conditions
The flight may be continued using other certificated navigation systems
The flight may be continued as planned if at least 4 satellites are available and the pilot monitors the GPS-System manually
A constant heading and speed must be flown until the required number of satellites are again available
28. An apparent increase in the transmitted frequency which is proportional to the transmitter velocity will occur when
the transmitter moves away from the receiver
both transmitter and receiver move towards each other
the transmitter moves towards the receiver
the receiver moves towards the transmitter
29. Which one of the following disturbances is most likely to cause the greatest inaccuracy in ADF bearings?
Coastal effect
Precipitation interference
Local thunderstorm activity
Quadrantal error
30. Which one of the following lists information given by a basic VOR/DME-based Area Navigation System?
Wind velocity
True airspeed, drift angle
Aircraft position in latitude and longitude
Crosstrack distance, alongtrack distance, angular course deviation
31. ILS is subject to false glide paths resulting from
back-scattering of antennas
spurious signals reflected by nearby obstacles
ground returns ahead of the antennas
multiple lobes of radiation patterns in the vertical plane
32. The principle used in VOR bearing measurement is:phase comparison
difference in depth of modulation
phase comparison
envelope matching
beat frequency discrimination
33. The ISO-ECHO facility of an airborne weather radar is provided in order to
inhibit unwanted ground returns
extend the mapping range
give an indication of cloud tops
detect areas of possible severe turbulence in cloud
34. How does the Electronic Flight Instrument System display of a B737-400 respond to the failure of a VHF navigation (VOR) receiver?
Flight Management ComputerAircraft Mapping RadarNavigation radios
Inertial Reference SystemsAircraft Mapping RadarNavigation radios
Inertial Reference SystemsNavigation radiosTrue airspeed and drift inputs
Navigation radiosFlight Management ComputerInertial Reference Systems
35. The reason why the measured distance between a NAVSTAR/GPS satellite navigation system satellite and a receiver is called a 'Pseudo-Range' is because the
movement of satellite and receiver during the distance calculation is not taken into account
measured distance is based on the Pseudo Random Noise code
calculated range is based on an idealised Keplerian orbit
calculated range includes receiver clock error
36. Complete the following statement. Aircraft Surface movement Radar operates on frequencies in the (i) .......... band employing an antenna that rotates at approximately (ii) .......... revolutions per minute, it is (iii) ......... possible to determine the type of aircraft from the return on the radar screen.
(i) SHF (ii) 60 (iii) sometimes
(i) EHF (ii) 30 (iii) never
(i) EHF (ii) 100 (iii) never
(i) SHF (ii) 10 (iii) always
37. Which of the following NAVSTAR/GPS satellite navigation system codes can be processed by 'unauthorised' civil aviation receivers?
P and Y
C/A- and P
P
C/A
38. The maximum range of primary radar depends on
frequency
pulse length
pulse recurrence frequency
wave length
39. The prime factor in determining the maximum unambiguous range of a primary radar is the
height of the transmitter above the ground
size of parabolic receiver aerial
power output
pulse recurrence rate
40. Instrument Landing Systems (ILS) Glide Paths provide azimuth coverage (i) .......... ° each side of the localiser centre-line to a distance of (ii) .......... NM from the threshold
(i) 5 (ii) 8
(i) 35 (ii) 25
(i) 25 (ii) 17
(i) 8 (ii) 10
41. What datum is used for the Minimum Descent Altitude (MDA) on a non-precision approach when using the NAVSTAR/GPS satellite navigation system?
Radar altitude
GPS altitude
If using Differential-GPS (D-GPS) the altitude obtained from the D-GPS, otherwise barometric altitude
Barometric altitude
42. Ignoring pulse length and fly-back, a radar facility designed to have a maximum unambiguous range of 50 km will have a PRF (pulses per second) of
330
6000
3000
167
43. An NDB transmits a signal pattern in the horizontal plane which is
bi-lobal circular
a beam rotating at 30 Hz
a cardioid balanced at 30 Hz
omnidirectional
44. A typical frequency employed in Distance Measuring Equipment (DME) is
100 MHz
1000 MHz
100 GHz
10 MHz
45. Due to 'Doppler' effect an apparent decrease in the transmitted frequency, which is proportional to the transmitter's velocity, will occur when
the transmitter moves away from the reciever
the transmitter and receiver move towards each other
the transmitter moves toward the reciever
both transmitter and receiver move away from each other
46. In which frequency band do VOR transmitters operate?
SHF
EHF
UHF
VHF
47. A VOR and DME are co-located.You want to identify the DME by listening to the callsign.Having heard the same callsign 4 times in 30 seconds the
DME callsign was not transmitted, the distance information is sufficient proof of correct operation
VOR and DME callsigns were the same and broadcast with the same pitch
DME callsign is the one with the higher pitch that was broadcast only once
DME callsign is the one with the lower pitch that was broadcast several times
48. An aircraft on a heading of 280°(M) is on a bearing of 090°(M) from a VOR. The bearing you should select on the OMNI bearing selector to centralise the VOR/ILS left/right deviation needle with a 'TO' indication is
280°
270°
100°
090°
49. The amplitude modulation and the colour of an outer marker (OM) is
1300 Hz, blue
400 Hz, blue
400 Hz, amber
3000 Hz, blue
50. Which of the following cloud types is most readily detected by airborne weather radar when using the 'weather beam'?
altostratus
cumulus
cirrocumulus
stratus
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