ALP >> Navigation >> Test-3

1 / 20

1. As the INS position of the departure aerodrome, coordinates 35°32.7'N 139°46.3'W are input instead of 35°32.7'N 139°46.3'E. When the aircraft subsequently passes point 52°N 180°W, the longitude value shown on the INS will be:

A) 080° 27.4'W

B) 099° 32.6'W

C) 099° 32.6'E

D) 080° 27.4'

2 / 20

2. Given: True track 180°Drift 8°RCompass heading 195°Deviation -2°Calculate the variation?

A) 21°W

B) 25°W

C) 5°W

D) 9°W

3 / 20

3. Given:Magnetic track = 075°,HDG = 066°(M),VAR = 11°E,TAS = 275 ktAircraft flies 48 NM in 10 MIN.Calculate the true W/V °?

A) 340°/45 kt

B) 320°/50 kt

C) 210°/15 kt

D) 180°/45 kt

4 / 20

4. (For this question refer to annex 061-12602A)Given:CON VOR/DME (N5354.8 W00849.1)Castlebar aerodrome (N5351 W00917)What is the CON radial and DME distance when overhead Castlebar aerodrome?

A) 086° - 18 NM

B) 265° - 17 NM

C) 077° - 18 NM

D) 257° - 17 NM

5 / 20

5. (For this question refer to annex 061-12626A)Which aeronautical chart symbol indicates a non-compulsory reporting point?

A) 15

B) 6

C) 7

D) 8

6 / 20

6. (For this question refer to annex 061-12624A)Which aeronautical chart symbol indicates an uncontrolled route?

A) 3

B) 4

C) 5

D) 2

7 / 20

7. At the magnetic equator, when accelerating after take off on heading West, a direct reading compass :

A) underreads the heading

B) indicates a turn to the south

C) indicates the correct heading

D) overreads the heading

8 / 20

8. Given: True HDG = 035°,TAS = 245 kt,Track (T) = 046°,GS = 220 kt.Calculate the W/V?

A) 340/45kt

B) 340/50kt

C) 335/45kt

D) 335/55kt

9 / 20

9. Given: TAS = 250 kt,HDG (T) = 029°,W/V = 035/45kt.Calculate the drift and GS?

A) 1L - 205 kt

B) 1R - 205 kt

C) 1L - 265 kt

D) 1R - 295 kt

10 / 20

10. When decelerating on a westerly heading in the Northern hemisphere, the compass card of a direct reading magnetic compass will turn :

A) anti-clockwise giving an apparent turn towards the north

B) clockwise giving an apparent turn toward the south

C) anti-clockwise giving an apparent turn towards the south

D) clockwise giving an apparent turn towards the north

11 / 20

11. With reference to inertial navigation systems, a TAS input is:

A) required for Polar navigation

B) required for rhumb line navigation

C) required to provide a W /V read out

D) not required

12 / 20

12. An aircraft is planned to fly from position 'A' to position 'B',distance 320 NM, at an average GS of 180 kt. It departs 'A' at 1200 UTC.After flying 70 NM along track from 'A', the aircraft is 3 MIN ahead of planned time.Using the actual GS experienced, what is the revised ETA at 'B'?

A) 1333 UTC

B) 1401 UTC

C) 1347 UTC

D) 1340 UTC

13 / 20

13. Given: TAS = 170 kt,HDG(T) = 100°,W/V = 350/30kt.Calculate the Track (°T) and GS?

A) 091 - 183 kt

B) 103 - 178 kt

C) 098 - 178 kt

D) 109 - 182 kt

14 / 20

14. What is the source of magnetic variation information in a Flight Management System (FMS)?

A) Magnetic variation information is stored in each IRS memory; it is applied to the true heading calculated by the respective IRS

B) The main directional gyro which is coupled to the magnetic sensor (flux valve) positioned in the wingtip

C) The FMS calculates MH and MT from the FMC position

D) Magnetic variation is calculated by each IRS based on the respective IRS position and the aircraft magnetic heading

15 / 20

15. Given: Runway direction 230°(T), Surface W/V 280°(T)/40 kt. Calculate the effective cross-wind component?

A) 26 kt

B) 31 kt

C) 36 kt

D) 21 kt

16 / 20

16. Complete the following statement regarding magnetic variation. The charted values of magnetic variation on earth normally change annually due to:

A) magnetic pole movement causing numerical values at all locations to increase or decrease

B) magnetic pole movement causing numerical values at all locations to increase.

C) a reducing field strength causing numerical values at all locations to decrease.

D) an increasing field strength causing numerical values at all locations to increase.

17 / 20

17. Given: GS = 480 kt.Distance from A to B = 5360 NM.What is the time from A to B?

A) 11 HR 15 MIN

B) 11 HR 10 MIN

C) 11 HR 06 MIN

D) 11 HR 07 MIN

18 / 20

18. Given:Position A 45°N, ?°EPosition B 45°N, 45°15'EDistance A-B = 280 NMB is to the East of ARequired: longitude of position A?

A) 49°57'E

B) 51°51'E

C) 40°33'E

D) 38°39'E

19 / 20

19. (For this question use annex 061-12564A)What is the average track (°M) and distance between WTD NDB (N5211.3 W00705.0) and KER NDB (N5210.9 W00931.5)?

A) 098° - 90 NM

B) 278° - 90 NM

C) 090° - 91 NM

D) 270° - 89 NM

20 / 20

20. In which of the following situations is the FMC present position of a B737-400 Electronic Flight Instrument System likely to be least accurate?

A) On final approach

B) Just after take-off

C) At top of climb

D) At top of descent

Your score is

The average score is 0%

Navigation Test-3

Related