Email
info@vayudootaviation.com
Phone No
+91 7276526726
become a pilot
Home
About us
courses
CPL
ATPL
RTR(A)
Airline Cadet Program
IGRUA Entrance Prep
B.Sc. Aviation
Pilot Training
INDIA
USA
CANADA
SOUTH AFRICA
NEW ZEALAND
EUROPE
Aircraft Type-Rating
Airbus A320
Boeing 737
Blogs
contact
CPL Test Series
Question Bank
Questions for RADIO AIDS OX BACK QUESTIONS
Answer the following questions
Test Mode
Training Mode
1. What is the maximum distance apart a VOR and TACAN can be located and have the same identification
60m
2000m
6m
600m
2. The frequencies used by LORAN C are
190 – 1750 kHz
108 – 112 MHz
70 – 130 kHz
90 – 110 kHz
3. The almanac in the receiver
assigns the PRN codes to the satellites
is used to determine which satellites are above the horizon
is used to determine receiver clock error
determines selective availability
4. The audio frequency of the outer marker is
3000 Hz
1300 Hz
400 Hz
1000 Hz
5. The frequency band of the NAVSTAR/GPS L1 and L2 frequencies is
UHF
SHF
VHF
EHF
6. The colour recommended in JAR25 for engaged modes is
cyan
white
green
magenta
7. In a certain VORTAC installation the VOR is coding STN and the DME is coding STZ. This means that the distance between the two beacons is in excess of
300m
600m
100m
2000m
8. An aircraft GNSS receiver is using 5 satellites for RAIM. If the receiver deselects one satellite then the flight should be continued
using 4 satellites with the pilot monitoring the receiver output
using inertial reference systems only
using alternative radio navigation systems only
using alternative navigation systems
9. The NAVSTAR/GPS constellation comprises
8 SVs each in 3 orbits
4 SVs each in 6 orbits
3 SVs each in 8 orbits
6 SVs each in 4 orbits
10. The range arcs in the expanded and map modes are recommended by JAR25 to be coloured
magenta
white
green
cyan
11. The number of satellites required to produce a 4D fix is
3
5
6
4
12. The inputs the pilot will make to the FMC during the pre-flight initialisation will include
Planned route, aircraft position, and departure runway
Departure runway, planned route and ETD.
Navigation data base, aircraft position and departure aerodrome
ETD, aircraft position, and planned route
13. The ETA generated by the FMS will be most accurate
If the groundspeed is correct and the take-off time has been entered.
when the forecast W/V equals the actual W/V and the FMS calculated Mach No. equals the actual Mach No.
If the groundspeed and position are accurate.
If the forecast W/V at take-off is entered.
14. Which GPS frequencies are available for commercial air transport?
1227.6 MHz and 1575.42 MHz
1227.6 MHz or 1575.42 MHz
1575.42 MHz only
1227.6 MHz only
15. The sensitive area of an ILS is the area aircraft may not enter when
the ILS is undergoing calibration
category 1 ILS operations are in progress
category II/III ILS operations are in progress
ILS operations are in progress
16. The accuracy of ADF within the DOC by day is
+/-10°
+/-2°
+/-5°
+/-1°
17. The contents of the navigation and systems message from NAVSTAR/GPS SVs include
satellite clock error, almanac data, satellite position error
position accuracy verification, satellite clock time and clock error
satellite clock error, almanac data, ionospheric propagation information
ionospheric propagation information, X, Y & Z co-ordinates and corrections, satellite clock time and error
18. Doppler navigation systems use …… to determine the aircraft groundspeed and drift
DME range measurement
Phase comparison of signals from ground station
Frequency shift in signals reflected from the ground
DVOR
19. Which of the following is an advantage of a VDF let down?
no special equipment required in the aircraft or on the ground
it is pilot interpreted, so ATC is not required
no equipment required in the aircraft
only a VHF radio is needed in the aircraft
20. The availability of 4096 codes in SSR is applicable to mode
C
All
S
A
21. The airborne weather radar (AWR) cannot detect
moderate rain
dry hail
snow
wet hail
22. The optimum climb and descent speeds used byn the FMC are found
in the operating manual and input to the FMC
in the performance database
in the navigation database
n the checklist and input manually
23. If, during a manoeuvre, a satellite being used for position fixing is shadowed by the wing, the effect on position will be
the GPS will maintain lock using reflections of the signals from the fuselage
the position will degrade
another satellite will be selected, so there will be no degradation of position
none
24. The amplitude modulation of the ILS outer marker is ……. and it illuminates the …… light in the cockpit
400 Hz, blue
1300 Hz, amber
400 Hz, amber
1300 Hz, blue
25. If the signal from a VOR is lost, how is this shown on the B737-400 EHSI display?
an amber FAIL message appears in the frequency location
by removal of the deviation bar and pointer
a flashing red FAIL message appears in the frequency location
by showing a fail flag alongside the deviation bar
26. A category III ILS system provides accurate guidance down to
less than 200 ft
less than 50 ft
less than 100 ft
the surface of the runway
27. What information does military TACAN provide for civil aviation users?
magnetic bearing
DME
DME and magnetic bearing
Nothing
28. In an RNAV system which combination of external reference will give the most accurate position?
GPS/rho
GPS/theta
Rho/rho
Rho/theta
29. In a primary pulsed radar the ability to discriminate in azimuth is a factor of
Beamwidth
Pulse recurrence rate
Pulse width
Rate of rotation
30. The quoted accuracy of VOR is valid
at all times except night
by day only
at all times
at all times except dawn and dusk
31. In the approach phase with a two dot lateral deviation HSI display, a one dot deviation from track would represent
0.5 nm
5 nm
0.5°
5°
32. In the NAV and EXP NAV modes one dot on the EHSI represents
2nm
2°
5°
5 nm
33.
On an EFIS display the pictured symbol represents
DME
VORTAC
aerodrome
VOR/DME
34. The principle of operation of LORAN C is
differential range by pulse technique
range by pulse technique
range by phase comparison
differential range by phase comparison
35. On which radial from a VOR at 61N025E (VAR 13°E) is an aircraft at 59N025E (VAR 20°E)?
193
167
347
160
36. The colour used on the B737-400 EHSI weather display to show turbulence is
magenta
white or magenta
flashing red
high colour gradient
37. The indications from a basic RNAV are behaving erratically. The reason is likely to be
the aircraft is in the cone of confusion of the reference VOR
the aircraft is below line of sight range of the reference VOR/DME
The aircraft is outside the DOC of the reference VOR/DME
the aircraft is in the cone of confusion of the phantom station
38. The definition of a radar display will be best with
wide beamwidth and narrow pulsewidth
narrow beamwidth and wide pulsewidth
narrow beamwidth and narrow pulsewidth
wide beamwidth and wide pulsewidth
39. Primary radar operates on the principle of
transponder interrogation
pulse technique
continuous wave emission
phase comparison
40. The ILS glideslope transmitter generates false glidepaths because of
multiple lobes in the radiation pattern
reflections from obstacles in the vicinity of the transmitter
ground returns from the vicinity of the transmitter
back scattering of the signals
41. An aircraft is tracking inbound to a VOR beacon on the 105 radial. The setting the pilot should put on the OBS and the CDI indications are
105, TO
105, FROM
285, FROM
285, TO
42. The orbital height of geostationary satellites is
10898 nm
35800 km
19330 km
10313 nm
43. The DME counters are rotating continuously. This indicates that
the DME is unserviceable
the DME is receiving no response from the ground station
the DME is trying to lock onto frequency
the DME is trying to lock onto range
44.
Refer to appendix A diagram C. The wind velocity is
129°(T)/20 kt
129°(T)/20 ms-1
129°(M)/20kt
129°(M)/20 ms-1
45. When tracking a VOR radial inbound the aircraft would fly
a great circle track
a rhumb line track
a constant heading
a constant track
46. The frequency band of the ILS glidepath is
VLF
UHF
SHF
VHF
47. The frequency band of VOR is
UHF
VHF
HF
LF & MF
48. The function of the receiver in the GNSS user segment is to
interrogate the satellites to determine range
track the satellites to calculate range
track the satellites to calculate time
determine position and assess the accuracy of that position
49. The EHSI is showing 5° fly right with a TO indication. The aircraft heading is 280°(M) and the required track is 270°. The radial is
095
085
275
265
50. A typical DME frequency is
1000 kHz
1575 MHz
1300 MHz
1000 MHz
Submit
Make New Set