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CPL Test Series
Question Bank
Questions for VOR
Answer the following questions
Test Mode
Training Mode
1. An airway 15 NM wide is to be defined by two VORs each having a resultant bearing accuracy of plus or minus 5.5°. In order to ensure accurate track guidance within the airway limits the maximum distance apart for the transmitter is approximately?
165 NM.
50 NM.
155 NM.
210 NM.
2. Given: Aircraft heading 160 (M), aircraft is on radial 240 from a VOR. Selected course on the HSI is 250 degrees. The HSI indications are deviation bar?
Behind the aeroplane symbol with FROM flag showing.
Ahead of the aeroplane symbol with the FROM flag showing.
Behind the aeroplane symbol with the TO flag showing.
Ahead of the aeroplane symbol with the TO flag showing.
3. An aircraft on a heading of 180 (M) is on bearing 270 (M) from a VOR. The bearing you should select on the OMNI Bearing Selector to centralise the VOR/ILS left/right deviation bar is?
360 degrees.
090 degrees.
180 degrees.
270 degrees.
4. Given: Aircraft heading 300°(M), Aircraft is on radial 280° from a VOR, Selected course on HSI is 270°. The HSI indications are deviation bar?
Behind the aeroplane symbol with the TO flag showing.
Ahead of the aeroplane symbol with the TO flag showing.
Behind the aeroplane symbol with the FROM flag showing.
Ahead of the aeroplane symbol with the FROM flag showing.
5. Tuned to a VOR station, with OBS needle central, the instrument reads 140 degrees with FROM indicated, Relative to the VOR station the receiver is in the?
Northeast or Southeast sector, depending on the heading of the aircraft when the reading is taken.
Southwest sector.
Northwest sector.
Southeast sector.
6. The maximum theoretical range at which an aircraft at FL210 may receive signals from a VOR facility sited 340 feet above mean sea level is approximately
204 nm.
245 nm.
183 nm.
163 nm.
7. The maximum theoretical range at which an aircraft at FL230 may received signals from VOR facility sited at mean sea level is
190 NM.
151 NM.
170 NM.
230 NM.
8. A VOR is sited at position A (35°00'N, 020°00'E). An aircraft is located at position B(34°00'N, 020°00'E). Assuming that the magnetic variation at A is 15°W and at B is 20°W, the aircraft is on VOR radial
180°
175°
195°
185°
9. Given: Course Deviation Indicator (CDI) for a VOR is selected to 090°. From/To indicator indicates "TO". CDI needle is deflected halfway to the right. On what radial is the aircraft?
265.
85.
275.
95.
10. An aircraft at 6400 ft will be able to receive a VOR ground station at 100 ft above MSL at an approximate range of?
113 nm.
98 nm.
90 nm.
123 nm.
11. If the reference phase differs 30° with the variable phase the radial from the VOR station will be
210°
150°
030°.
330°.
12. If VOR bearing information is used beyond the published protection range, errors could be caused by
Interference from other transmitters.
Sky wave interference from the same transmitter.
Noice from precipitation static exceeding the signal strength of the transmitter.
Sky wave interference from distant transmitters on the same frequency.
13. The principle used in VOR bearing measurement is
Envelope matching
Beat frequency discrimination.
Phase comparison
Difference in depth of modulation.
14. Given: VOR station position N66° E025° , variation 20°E; Estimated position of an aircraft N56° E025°, variation 25°E. What VOR radial is the aircraft on?
195
165°
160°
345°
15. Under which of the following circumstance does a VOR/DME Area Navigation System switch to Dead Reckoning mode?
When "DR" is selected by the pilot
VOR/DME Area Navigation computer is not receiving information from the aircraft compass system
VOR/DME Area Navigation computer is not receiving information for the Air Data Computer.
VOR/DME Area Navigation computer is receiving neither radial nor distance data information from the VOR/DME station.
16. In order to plot a bearing from a VOR station, a pilot needs to know the magnetic variation
At the aircraft location.
At the VOR.
At the halfway point between the aircraft and the station.
At both the VOR and aircraft.
17. An airway 12 NM wide is to be defined by two VORs each having a resultant bearing accuracy of plus or minus 5.5°. In order to ensure accurate track guidance within the airway limits the maximum distance apart for the transmitter is approximately?
124 NM.
165 NM.
50 NM.
210 NM.
18. An aircraft, on a heading of 180(M) is on a bearing of 270 (M) from a VOR. The bearing you should select on the OMNI bearing selector to centralise the VOR/ILS left/right needle with a TO indication is?
360 degrees.
090 degrees.
180 degrees.
270 degrees.
19. The VOR to obtain CDI (course deviation indicator) indications in the correct sense when tracking towards a VOR on radial 255 degrees, the pilot should set on the OBS (Omni bearing selector)?
055 degrees with FROM indicated.
235 degrees with FROM indicated.
235 degrees with TO indicated.
075 degrees with TO indicated.
20. The OBS is set to 235 degrees. "TO" appears in the window. The needle is close to full right deflection. The VOR radial is approximately?
240 degrees
050 degrees
060 degrees
230 degrees
21.
An aircraft is flying on a MH of 010 degrees. The magnetic variation at the VOR is 10W and at the aircraft 12W. Which VOR RMI corresponds to the indications on the CDI in the diagram?
Figure C.
Figure B.
Figure A.
Figure D.
22. The two signals transmitted by a conventional VOR ground station are 180° out of phase on magnetic
West
North.
East.
South
23. You are on compass heading 090 on the 255 radial from a VOR. You set the course 190 on your OBS. The deviation bar will show?
Full scale deflection right with a "FROM" indication.
Full scale deflection left with a "TO" indication.
Full scale deflection right with a "TO" indication.
Full scale deflection left with a "FROM" indication.
24. An aircraft is on the 120 degree radial from a VOR. Course 340 degrees is selected on the HSI (Horizontal Situation Indicator). If the magnetic heading is 070 degrees, the deviation bar relative to the aeroplane model will be?
Left
In front
Right.
Behind
25.
An aircraft is flying on the 050 radial with a MH of 250 degrees. On the HSI the CRS is set to 060. Which HSI in the diagram shows the correct indications?
Figure A.
Figure D.
Figure C.
Figure B.
26. An aircraft has a magnetic heading of 290 degrees and is on VOR radial 280. Which value has to be selected on the OBS to get a TO indication and the CDI centred?
110.
100.
290.
280.
27. Which of the following statements about the scalloping (path deflection) of VOR radials, in relation to the accuracy of navigation using a VOR/DME RNAV system is correct?
Scalloping has no effect on the accuracy of navigation because the accuracy is independent of VOR or DME measurements.
Scalloping has a positive effect on the accuracy of navigation.
Scalloping has no effect on the accuracy of navigation because it only results in the movement of the needle of the Course Deviation Indicator.
Scalloping has a negative effect on the accuracy of navigation.
28. In order to measure the radial from a VOR, the aircraft VOR receiver?
Measures the times difference between sending the interrogation signal and receiving the transponder signal.
Measures the time difference between reception of the two signals transmitted from the ground station.
Uses the pulse technique to determine the radial
Measures the phase difference between the reference phase and the variable phase of the signal.
29.
An aircraft is flying on a MH of 010 degrees. The magnetic variation at the VOR is 10W and at the aircraft 12W. Which VOR RMI corresponds to the indications on the CDI shown in the diagram?
Figure A.
Figure B.
Figure C.
Figure D.
30. Given: Aircraft position 52 09 S 024 E, magnetic variation 14W, FL310. BIT VOR/DME position 54 42 S 024 E. Magnetic variation 14E. In order to read the most accurate ground speed given by the DME receiver from this positive, the pilot must follow which BIT radial?
194 degrees.
014 degrees.
346 degrees.
166 degrees.
31. An aeroplane flying on a heading of 280 degrees magnetic is on a bearing of 180 degrees magnetic from of VOR. The bearing to the VOR that should be selected on the OMNI bearing selector to centralise the VOR/ILS deviation needle is?
360.
180.
90.
270.
32. The captain of an aircraft flying at FL100 wishes to obtain weather information at the destination airfield from the airfield's VOR. At what maximum theoretical range will it be possible to obtain this information?
123 km.
12.3 NM.
125 Nm.
1230 km.
33. You are flying along an airway, which is 10 nm wide (5 nm either side of the centreliner). The distance to the VOR/DME you are using is 100 nm. If you are on the airway boundary, how many dots deviation will the VOR needle show if I dot represents 2 degrees?
3.0.
4.5.
6.0.
1.5.
34. An aircraft is on radial 120 with a magnetic heading of 300°, the track selector (OBS) reads : 330. The indications on the Course Deviation Indicator (CDI) are 'fly'
Right with 'TO' showing.
Right with 'FROM' showing.
Left with 'TO' showing.
Left with 'FROM' showing.
35. An Omni-bearing selector (OBS) shows full deflection to the left when within range of a serviceable VOR. What angular deviation are you from the selected radial?
2.5 or more.
10° or more.
Less than 10°
1.5° or more.
36. A VOR is sited at position A, (45 00 N, 010 00 E), An aircraft if located at position B, (44 00 N, 010 00 E). Magnetic variation at position A = 10 degrees West, and at position B it is 15 degrees West. The aircraft is on VOR radial?
185 degrees
195 degrees
190 degrees
180 degrees
37. An aeroplane flying on a heading of 280 degrees magnetic is on a bearing of 180 degrees magnetic from of VOR. The bearing from the VOR that should be selected on the OMNI bearing selector to centralise the VOR/ILS deviation needle is?
270
180
360.
90
38. An aircraft is situated at 30N, 005E, with magnetic variation of 10W, A VOR is located at 30N 013E with a magnetic variation of 15W. The aircraft is situated on the VOR radial?
101.
286.
256
281.
39. An aircraft at 6400 ft should be able to receive a VOR ground station at 100 ft above msl at an approximate maximum range of?
113 nm.
90 nm.
98 nm.
123 nm.
40. An aircraft at FL 100 should be able to receive a VOR ground station at 100 FT above MSL at an approximate maximum range of
142 NM.
130 NM.
135 NM.
123 NM.
41.
An aircraft is flying on a MH of 210. The magnetic variation at the VOR is 5W and at the aircraft it is 10W; Which VOR RBI corresponds to the indications on the HSI in the diagram?
Figure C.
Figure D.
Figure B.
Figure A.
42. What is the maximum distance between VOR and DME/TACAN ground installations if they are to have the same morse code identifier?
2000 m.
600 m.
60 m.
300 m.
43. Two aircraft are located on the same radial but at (arbitray) different distances from a VOR station. Which statement is true?
At a certain moment of time the phase of the reference signals is equal and the phases of the variable signals is equal for both.
At a certain moment of time, both the phase of the reference signals and the phase of the variable signals are equal for both aircraft.
At a certain moment of time, both the phase of the reference signals and the phase of the variable signals are unequal for both aircraft.
At a certain moment of time the phase of the reference signals is equal and the phases of the variable signals is unequal for both.
44.
An aircraft is flying on a MH of 010. The magnetic variation at the VOR is 10W and at the aircraft it is 12W; Which VOR RBI in the diagram corresponds to the indications on the VOR HSI?
Figure D.
Figure A.
Figure B.
Figure C.
45. Given: Aircraft position 34 15N 098E, nagnetic variation 28W, FL 280, PTC VOR/DME position 36 12N 098E, magnetic variation 13E. In order to read the most accurate ground speed given by the DME receiver from his present position, the pilot must fly on which PTC Radia?
Aircraft will not receive DME information from PTC due to the line of sight rule.
167
332.
193.
46.
An aircraft is flying on a MH of 210 degrees. The magnetic variation at the VOR is 5W and at the aircraft is 10W. According to the CDI in the diagram, the aircraft is on radial?
195 radial.
015 radial.
205 radial.
025 radial.
47. A VOR and an NDB are located at the same position. Both the VOR and the ADF readings are displayed on the RMI. The aircraft is tracking away from the beacons along the 090 radial. The magnetic variation is changing rapidly. Which of the following is correct?
Both the direction of the ADF pointer and the direction of the VOR pointer will change.
The direction of the ADF pointer will change, the direction of the VOR pointer will not change.
Neither the direction of the ADF pointer nor the direction of the VOR pointer will change.
The direction of the VOR pointer will change, the direction of the ADF pointer will not change.
48. If an aircraft flies along a VOR radial it will follow a
Line of constant bearing.
Rhumbline track.
Constant magnetic track.
Great circle track.
49. The maximum theoretical range at which an aircraft at FL 230 can receive signals from a VOR facility sited at MSL is?
151 nm.
230 nm.
190 nm.
170 nm.
50. An aeroplane flying on heading of 180 degrees magnetic is on a bearing of 270 degrees magnetic from of VOR. The bearing from the VOR that should be selected on the OMNI bearing selector to centralise the VOR/ILS deviation needle is?
180
360.
90.
270
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