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CPL Test Series
Question Bank
Questions for Indigo gen NAV 4090-4604
Answer the following questions
Test Mode
Training Mode
1.
3016 NMTrue airspeed 480 ktMean wind component 'out' -90 ktMean wind component 'back' +75 ktSafe endurance 10:00 HR The distance from 'Q' to the Point of Safe Return (PSR) 'Q' is
1510 NM
2290 NM
1310 NM
2370 NM
2.
The lines on the earth's surface that join points of equal magnetic variation are called
isoclines
isogonals
isotachs
isogrives
3.
Which of the following statements concerning the position indicated on the Inertial Reference System (IRS) display is correct?
It is constantly updated from information obtained by the FMC
The positions from the two IRSs are compared to obtain a 'best position' which is displayed on the IRS
It is updated when 'go-around' is selected on take-off
It is not updated once the IRS mode is set to NAV
4.
The lines on the earth's surface that join points of equal magnetic variation are called
isogonals
isotachs
isoclines
isogrives
5.
An aeroplane flies from A (59°S 142°W) to B (61°S 148°W) with a TAS of 480 kt. The autopilot is engaged and coupled with an Inertial Navigation System in which AB track is active.On route AB, the true track
varies by 4°`
decreases by 6°
varies by 10°
increases by 5°
6.
What is the source of magnetic variation information in a Flight Management System (FMS)?
Magnetic variation information is stored in each IRS memory, it is applied to the true heading calculated by the respective IRS
Magnetic variation is calculated by each IRS based on the respective IRS position and the aircraft magnetic heading
The FMS calculates MH and MT from the FMC position
The main directional gyro which is coupled to the magnetic sensor (flux valve) positioned in the wingtip
7.
At 47° North the chart distance between meridians 10° apart is 5 inches. The scale of the chart at 47° North approximates
1 : 6 000 000
1 : 8 000 000
1 : 2 500 000
1 : 3 000 000
8.
265 US-GAL equals? (Specific gravity 0.80)265 US-GAL equals? (Specific gravity 0.80)
940 kg
895 kg
803 kg
862 kg
9.
Given:Distance A to B = 120 NM,After 30 NM aircraft is 3 NM to the left of course.What heading alteration should be made in order to arrive at point 'B'?
8° right
8° left
6° right
4° right
10.
An aircraft at FL330 is rerquired to commence descent when 65 NM from a VOR and to cross the VOR at FL100. The mean GS during the descent is 330 kt. What is the minimum rate of descent required?
1750 FT/MIN
1850 FT/MIN
1950 FT/MIN
1650 FT/MIN
11.
The constant of cone of a Lambert conformal conic chart is quoted as 0.3955. At what latitude on the chart is earth convergency correctly represented?
66°42'
68°25'
21°35'
23°18'
12.
Which of the following statements concerning the alignment procedure for Inertial Navigation Systems(INS)/Inertial Reference Systems (IRS) at mid-latitudes is correct?
INS/IRS can be aligned in either the ALIGN or NAV mode
INS/IRS can be aligned in either the ALIGN or ATT mode
INS/IRS can only be aligned in NAV mode
INS/IRS can only be aligned in the ALIGN mode
13.
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
97 NM
105 NM
115 NM
84 NM
14.
Given: true track is 348°, drift 17° left, variation 32° W, deviation 4°E. What is the compass heading?
337°
007°
033°
359°
15.
Given:TAS = 470 kt,True HDG = 317°W/V = 045°(T)/45ktCalculate the drift angle and GS?
3°R - 470 kt
5°R - 475 kt
5°L - 470 kt
5°L - 475 kt
16.
In the B737-400 Flight Management System the CDUs are used during preflight to
automatically initialize the IRSs and FMC with dispatch information
manually initialize the Flight Director System and FMC with dispatch information
manually initialize the IRSs and FMC with dispatch information
manually initialize the IRSs, FMC and Autothrottle with dispatch information
17.
How many NM would an aircraft travel in 1 MIN 45 SEC if GS is 135 kt?
3.94
3.25
2.36
39.0
18.
A Rhumb line is
a line convex to the nearest pole on a Mercator projection
the shortest distance between two points on a Polyconic projection
any straight line on a Lambert projection
a line on the surface of the earth cutting all meridians at the same angle
19.
Given:True HDG = 233°,TAS = 480 kt,Track (T) = 240°,GS = 523 kt.Calculate the W/V?
110/80kt
110/75kt
105/75kt
115/70kt
20.
The horizontal component of the earth's magnetic field
is approximately the same at all magnetic latitudes less than 60°
is approximately the same at magnetic latitudes 50°N and 50°S
weakens with increasing distance from the magnetic poles
weakens with increasing distance from the nearer magnetic pole
21.
For a distance of 1860 NM between Q and R, a ground speed ""out"" of 385 kt, a ground speed ""back"" of 465 kt and an endurance of 8 HR (excluding reserves) the distance from Q to the point of safe return (PSR) is
1685 NM
930 NM
1865 NM
1532 NM
22.
Given :True altitude 9000 FT,OAT -32°C,CAS 200 kt.What is the TAS?
220 kt
215 kt
210 kt
200 kt
23.
Given : Position 'A' N60 W020,Position 'B' N60 W021, Position 'C' N59 W020. What are, respectively, the distances from A to B and from A to C?
60 NM and 52 NM
30 NM and 60 NM
52 NM and 60 NM
60 NM and 30 NM
24.
The great circle distance between position A (59°34.1'N 008°08.4'E) and B (30°25.9'N 171°51.6'W) is
10 800 km
10 800 NM
5 400 NM
2 700 NM
25.
The distance measured between two points on a navigation map is 42 mm (millimetres). The scale of the chart is 1:1 600 000.The actual distance between these two point is approximately
36.30 NM
370.00 NM
3.69 NM
67.20 NM
26.
The ICAO definition of ETA is the
estimated time of arrival at destination
estimated time of arrival at an en-route point or fix
actual time of arrival at a point or fix
estimated time en route
27.
An aircraft at FL310, M0.83, temperature -30°C, is required to reduce speed in order to cross a reporting point five minutes later than planned. Assuming that a zero wind component remains unchanged, when 360 NM from the reporting point Mach Number should be reduced to
M0.78
M0.76
M0.74
M0.80
28.
Given: TAS = 485 kt,HDG (T) = 168°,W/V = 130/75kt.Calculate the Track (°T) and GS?
175 - 420 kt
174 - 428 kt
175 - 432 kt
173 - 424 kt
29.
Given: GS = 510 kt.Distance A to B = 43 NMWhat is the time (MIN) from A to B?
7
6
4
5
30.
The angle between Magnetic North and Compass North is called
compass deviation
magnetic variation
compass error
alignment error
31.
Given: True HDG = 206°,TAS = 140 kt,Track (T) = 207°,GS = 135 kt.Calculate the W/V?
000/05kt
180/05kt
180/10kt
000/10kt
32.
The north and south magnetic poles are the only positions on the earth's surface where
a freely suspended compass needle will stand vertical
a freely suspended compass needle will stand horizontal
isogonals converge
the value of magnetic variation equals 90°
33.
Given:The coordinates of the heliport at Issy les Moulineaux are:N48°50' E002°16.5'The coordinates of the antipodes are
S41°10' E177°43.5'
S48°50' W177°43.5
S48°50' E177°43.5'
S41°10' W177°43.5'
34.
Given: True course 300°drift 8°Rvariation 10°Wdeviation -4° Calculate the compass heading?
278°
294°
306°
322°
35.
Deviation applied to magnetic heading gives
magnetic course
true heading
magnetic track
compass heading
36.
A Lambert conformal conic chart has a constant of the cone of 0.75. The initial course of a straight line track drawn on this chart from A (40°N 050°W) to B is 043°(T) at A, course at B is 055°(T). What is the longitude of B?
38°W
36°W
41°W
34°W
37.
The maximum difference between geocentric and geodetic latitude occurs at about
0° North and South (equator
90° North and South
45° North and South
60° North and South
38.
The chart that is generally used for navigation in polar areas is based on a
Direct Mercator projection
Gnomonic projection
Lambert conformal projection
Stereographical projection
39.
The circumference of the parallel of latitude at 60°N is approximately
34 641 NM
20 000 NM
10 800 NM
18 706 NM
40.
Civil twilight is defined by
sun upper edge tangential to horizon
sun altitude is 18° below the celestial horizon
sun altitude is 6° below the celestial horizon
sun altitude is 12° below the celestial horizon
41.
The distance between positions A and B is 180 NM. An aircraft departs position A and after having travelled 60 NM, its position is pinpointed 4 NM left of the intended track. Assuming no change in wind velocity, what alteration of heading must be made in order to arrive at position B?
8° Right
4° Right
6° Right
2° Left
42.
Given: GS = 95 kt.Distance from A to B = 480 NM.What is the time from A to B?
5 HR 03 MIN
4 HR 59 MIN
5 HR 08 MIN
5 HR 00 MIN
43.
Given: GS = 236 kt.Distance from A to B = 354 NMWhat is the time from A to B?
1 HR 09 MIN
1 HR 30 MIN
1 HR 40 MIN
1 HR 10 MIN
44.
Given: Runway direction 230°(T), Surface W/V 280°(T)/40 kt. Calculate the effective cross-wind component?
21 kt
36 kt
26 kt
31 kt
45.
The main reason that day and night, throughout the year, have different duration, is due to the
inclination of the ecliptic to the equator
earth's rotation
gravitational effect of the sun and moon on the speed of rotation of the earth
relative speed of the sun along the ecliptic
46.
An aircraft is descending down a 12% slope whilst maintaining a GS of 540 kt.The rate of descent of the aircraft is approximately
4500 FT/MIN
650 FT/MIN
6500 FT/MIN
3900 FT/MIN
47.
Given: GS = 345 kt.Distance from A to B = 3560 NM.What is the time from A to B?
11 HR 00 MIN
10 HR 19 MIN
11 HR 02 MIN
10 HR 05 MIN
48.
The term drift refers to the wander of the axis of a gyro in
the vertical and horizontal plane
the vertical plane
the horizontal plane
any plane
49.
A straight line on a chart 4.89 cm long represents 185 NM.The scale of this chart is approximately
1 : 5 000 000
1 : 3 500 000
1 : 7 000 000
1 : 6 000 000
50.
On a Lambert Conformal Conic chart earth convergency is most accurately represented at the
parallel of origin
Equator
north and south limits of the chart
standard parallels
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