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Questions for Indigo gen NAV 4090-4604

Answer the following questions

1.

On a Transverse Mercator chart, scale is exactly correct along the

2.

When is the magnetic compass most effective?

3.

An aircraft travels from point A to point B, using the autopilot connected to the aircraft's inertial system. The coordinates of A (45°S 010°W) and B (45°S 030°W) have been entered.The true course of the aircraft on its arrival at B, to the nearest degree, is

4.

Approximately how many nautical miles correspond to 12 cm on a map with a scale of 1 : 2 000 000?

5.

Given:A polar stereographic chart whose grid is aligned with the zero meridian. Grid track 344°, Longitude 115°00'W,Calculate the true course?

6.

An aircraft departing A(N40º 00´ E080º 00´) flies a constant true track of 270º at a ground speed of 120 kt. What are the coordinates of the position reached in 6 HR?

7.

The following information is displayed on an Inertial Navigation System:GS 520 kt,True HDG 090°,Drift angle 5° right,TAS 480 kt.SAT (static air temperature) -51°C.The W/V being experienced is

8.

Given: Distance 'A' to 'B' is 475 NM,Planned GS 315 kt,ATD 1000 UTC,1040 UTC - fix obtained 190 NM along track.What GS must be maintained from the fix in order to achieve planned ETA at 'B'?

9.

Given: GS = 236 kt.Distance from A to B = 354 NMWhat is the time from A to B?

10.

An aircraft at FL370, M0.86, OAT -44°C, headwind component 110 kt, is required to reduce speed in order to cross a reporting point 5 MIN later than planned. If the speed reduction were to be made 420 NM from the reporting point, what Mach Number is required?

11.

The angle between True North and Magnetic North is called

12.

What is the meaning of the term ""standard time"" ?

13.

Given:Distance 'Q' to 'R' 1760 NMGroundspeed 'out' 435 ktGroundspeed 'back' 385 ktSafe endurance 9 HR The distance from 'Q' to the Point of Safe Return (PSR) between 'Q' and 'R' is

14.

At 47° North the chart distance between meridians 10° apart is 5 inches. The scale of the chart at 47° North approximates

15.

A ground feature appears 30° to the left of the centre line of the CRT of an airborne weather radar. If the heading of the aircraft is 355° (M) and the magnetic variation is 15° East, the true bearing of the aircraft from the feature is

16.

When turning right from 330°(C) to 040°(C) in the northern hemisphere, the reading of a direct reading magnetic compass will

17.

One of the errors inherent in a ring laser gyroscope occurs at low input rotation rates tending towards zero when a phenomenon known as 'lock-in' is experienced. What is the name of the technique, effected by means of a piezo-electric motor, that is used to correct this error?

18.

An aircraft is following a true track of 048° at a constant TAS of 210 kt. The wind velocity is 350° / 30 kt. The GS and drift angle are

19.

On a transverse Mercator chart, the scale is exactly correct along the

20.

For a landing on runway 23 (227° magnetic) surface W/V reported by the ATIS is 180/30kt. VAR is 13°E. Calculate the cross wind component?

21.

What is the time required to travel along the parallel of latitude 60° N between meridians 010° E and 030° W at a groundspeed of 480 kt?

22.

The azimuth gyro of an inertial unit has a drift of 0.01°/HR.After a flight of 12 HR with a ground speed of 500 kt, the error on the aeroplane position is approximately

23.

The automatic flight control system (AFCS) in an aircraft is coupled to the guidance outputs from an inertial navigation system (INS) and the aircraft is flying from waypoint No. 2 (60°00'S 070°00'W) to No. 3 (60°00'S 080°00'W).Comparing the initial track (°T) at 070°00'W and the final track (°T) at 080°00'W, the difference between them is that the initial track is approximately

24.

Given:ILS GP angle = 3.5 DEG,GS = 150 kt.What is the approximate rate of descent?

25.

An aircraft flies a great circle track from 56° N 070° W to 62° N 110° E. The total distance travelled is?

26.

Which one of the following statements is correct concerning the appearance of great circles, with the exception of meridians, on a Polar Stereographic chart whose tangency is at the pole ?

27.

The constant of the cone, on a Lambert chart where the convergence angle between longitudes 010°E and 030°W is 30°, is

28.

An aircraft at FL120, IAS 200kt, OAT -5° and wind component +30kt, is required to reduce speed in order to cross a reporting point 5 MIN later than planned. Assuming flight conditions do not change, when 100 NM from the reporting point IAS should be reduced to

29.

A negative (westerly) magnetic variation signifies that

30.

Given: Distance 'A' to 'B' is 100 NM,Fix obtained 40 NM along and 6 NM to the left of course.What heading alteration must be made to reach 'B'?

31.

Given: TAS = 132 kt,HDG (T) = 053°,W/V = 205/15kt.Calculate the Track (°T) and GS?

32.

Some inertial reference and navigation systems are known as ""strapdown"". This means that

33.

On the 27th of February, at 52°S and 040°E, the sunrise is at 0243 UTC. On the same day, at 52°S and 035°W, the sunrise is at

34.

Which of the following statements concerning earth magnetism is completely correct?

35.

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

36.

Isogonals are lines of equal

37.

The nominal scale of a Lambert conformal conic chart is the

38.

Given:FL120, OAT is ISA standard, CAS is 200 kt,Track is 222°(M),Heading is 215° (M),Variation is 15°W.Time to fly 105 NM is 21 MIN.What is the W/V?

39.

Given: TAS = 198 kt,HDG (°T) = 180,W/V = 359/25.Calculate the Track(°T) and GS?

40.

61.4.7.0 (4483) An aircraft was over 'A' at 1435 hours flying direct to 'B'.Given:Distance 'A' to 'B' 2900 NMTrue airspeed 470 ktMean wind component 'out' +55 ktMean wind component 'back' -75 ktSafe endurance 9 HR 30 MIN The distance from 'A' to the Point of Safe Return (PSR) 'A' is

41.

An aircraft takes-off from an airport 2 hours before sunset. The pilot flies a track of 090°(T), W/V 130°/ 20 kt, TAS 100 kt. In order to return to the point of departure before sunset, the furthest distance which may be travelled is

42.

The main reason for mounting the detector unit of a remote reading compass in the wingtip of an aeroplane is

43.

The flight log gives the following data :""True track, Drift, True heading, Magnetic variation, Magnetic heading, Compass deviation, Compass heading""The right solution, in the same order, is

44.

An aircraft is flying with the aid of an inertial navigation system (INS) connected to the autopilot. The following two points have been entered in the INS computer:WPT 1: 60°N 030°WWPT 2: 60°N 020°WWhen 025°W is passed the latitude shown on the display unit of the inertial navigation system will be

45.

Given:Magnetic heading 311°Drift angle 10° leftRelative bearing of NDB 270°What is the magnetic bearing of the NDB measured from the aircraft?

46.

What is the final position after the following rhumb line tracks and distances have been followed from position 60°00'N 030°00'W?South for 3600 NM, East for 3600 NM, North for 3600 NM, West for 3600 NM.The final position of the aircraft is

47.

On a polar stereographic projection chart showing the South Pole, a straight line joins position A (70°S 065°E) to position B (70°S 025°W).The true course on departure from position A is approximately

48.

An aircraft departs from position A (04°10' S 178°22'W) and flies northward following the meridian for 2950 NM. It then flies westward along the parallel of latitude for 382 NM to position B. The coordinates of position B are?

49.

In an Inertial Navigation System (INS), Ground Speed (GS) is calculated:

50.

Given:Runway direction 305°(M),Surface W/V 260°(M)/30 kt. Calculate the crosswind component?