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CPL Test Series
Question Bank
Questions for CRP5
Answer the following questions
Test Mode
Training Mode
1. The reported surface wind from the Control Tower is 240°/35 kt. Runway 30 (300°). What is the cross-wind component?
35kt
26kt
25kt
30kt.
2. Given: IAS 97 kt, FL 75, OAT -15°C. What is the TAS?
109.0 kt.
111.5 kt.
105.5 kt.
107.5 kt.
3. Fuel flow per HR is 22 US-GAL, total fuel on board is 83 IMP GAL. What is the endurance?
3 hr 32 min.
3 hr 46 min.
4 hr 32 min.
4 hr 46 min.
4. Given: Compass Heading 090°, Deviation 2°W, Variation 12°E, TAS 160 kt. Whilst maintaining a radial 070° from a VOR station, the aircraft files a ground distance of 14 NM in 6 MIN. What is the W/V°(T)?
150°/60 kt.
160°/50 kt.
160°/60 kt.
150°/50 kt.
5. Given: Magnetic track = 075°, HDG = 066°(M), VAR = 11°E, TAS = 275 kt Aircraft files 48 NM in 10 MIN. Calculate the true W/V°?
345°/40 kt.
340°/35 kt.
340°/45 kt.
345°/35 kt.
6. Given: True HDG =307°, TAS = 230 kt, Track (T) = 313°, GS = 210 kt, Calculate the W/V?
263/33kt.
260/30kt.
260/33kt.
263/30kt.
7. What is the ETA at Z if TAS = 120 Kts?
1325 UTC.
1305 UTC.
1255 UTC.
1320 UTC.
8. What is the ISA temperature value at FL 330?
-53°C.
-50°C.
-56.5°C.
-52°C.
9. Given: True HDG =002°, TAS = 130 kt, Track (T) = 353°, GS = 132 kt, Calculate the W/V?
095/20kt.
098/25kt.
090/30kt.
090/25kt
10. Given: IAS 130 kt, FL 60, OAT +20°C. What is the TAS?
146.5 kt.
149.0 kt
150.0 kt.
139.5 kt.
11. Given: true track 352° variation 11° W deviation is -5° drift 10°R. Calculate the compass heading?
350°.
355°.
348°.
358°.
12. Given: TAS =270 kt, Track (T) = 260°, W/V = 275/30kt. Calculate the HDG (°T) and GS?
263 -241 kt.
260 - 242 kt.
260 - 241 kt.
261 - 240 kt.
13. Given: For take-off an aircraft requires a headwind component of at least 10 kt and has a cross-wind limitation of 35 kt. The angle between the wind direction and the runway is 60°, calculate the minimum and maximum allowable wind speeds?
25 kt and 30 kt.
25 kt and 35 kt.
20 kt and 40 kt.
20 kt and 45 kt.
14. Given: Course 095°(T), TAS is 220 kt, Wind speed 70 kt, Maximum drift angle will be obtained for a wind direction of
185°.
335°.
165°.
215°.
15. Given: GS = 135 kt. Distance from A to B = 433 NM, What is time from A to B?
3 hr 12 min.
3 hr 16 min.
3 hr 20 min.
2 hr 05 min.
16. Given: TAS = 225 kt, HDF(°T) = 123°, W/V = 090/60kt. Calculate the Track (°T) and GS?
134 - 168 kt.
130 - 178 kt.
130 - 168 kt
134 - 178 kt.
17. 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?
320° / 45 kt.
321° / 50 kt.
320° / 60 kt.
322° / 60 kt.
18. Given: True HDG =145°, TAS = 240 kt, Track (T) = 150°, GS = 210 kt, Calculate the W/V?
112/30kt.
115/40kt.
118/33kt
115/35kt.
19. Given: FL 120, 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?
070°(T) / 70 kt.
050°(T) / 70 kt.
050°(T) / 75 kt.
050°(T) / 50 kt.
20. Given: True Heading = 090° TAS = 200 kt W/V = 220°/30 kt. Calculate the GS?
180 kt.
220 kt.
240 kt.
200 kt.
21. Given: TAS = 250 kt, HDG (T) = 029°, W/V = 035/45kt. Calculate the drift and GS?
1R - 202 kt.
1R - 205 kt.
1L - 202 kt.
1L - 205 kt.
22. Given: Magnetic track = 210°, Magnetic HDG = 215°, VAR = 15°E, TAS = 360 kt, Aircraft files 64 NM in 12 MIN. Calculate the true W/V?
265°/40 kt.
260°/50 kt.
260°/40 kt.
265°/50 kt.
23. Given: True Heading = 180° TAS = 500 kt W/V 225°/100 kt Calculate the GS?
350 kt.
575 kt.
435 kt.
400 kt.
24. Given: IAS 89 kt, FL 25, OAT +10°C. What is the TAS?
91.0 kt.
95.5 kt.
90.5 kt.
92.5 kt.
25. Given: course required = 085° (T), Forecast W/V 030/100kt, TAS = 470 kt, Distance = 265 NM. Calculate the true HDG and flight time?
075°, 42 min.
070°, 39 min.
073°, 42 min.
075°, 39 min.
26. Given: GS = 120 kt. Distance from A to B = 84 NM, What is time from A to B?
00 hr 40 min.
00 hr 44 min.
00 hr 42 min.
00 hr 41 min.
27. Given: TAS = 155 kt, Tract (T) = 305°, W/V = 160/18kt. Calculate the HDG(°T) and GS?
293 - 169 kt.
301 - 165 kt.
293 - 165 kt.
301 - 169 kt.
28. Given: TAS = 132 kt, HDG (T) = 053°, W/V = 205/15kt. Calculate the Track (°T) and GS?
055 - 145 kt.
050 - 150 kt.
050 - 145 kt.
055 - 140 kt.
29. Given: GS = 236 kt. Distance from A to B =354 NM, What is time from A to B?
1 hr 35 min.
1 hr 15 min.
2 hr 03 min.
1 hr 30 min.
30. Given: GS = 345 kt. Distance from A to B = 3560 NM, What is time from A to B?
10 hr 19 min.
10 hr 25 min.
10 hr 23 min.
10 hr 15 min.
31. Given: TAS = 270 kt, True HDG = 270°, Actual wind 205°(T)/30kt, Calculate the drift angle and GS?
6L - 259kt.
6R - 269kt.
6R - 259kt.
12R - 269kt.
32.
What is the ETA at Z if TAS = 120 Kts?
1330 UTC.
1255 UTC.°
1325 UTC.
1320 UTC.
33. Given: TAS =227 kt, Track (T) = 316°, W/V = 205/15kt. Calculate the HDG (°T) and GS?
314 - 230 kt.
310 - 231 kt.
312 - 232 kt.
310 - 222 kt.
34. Given: TAS = 370 kt, True HDG = 181°, W/V = 095°(T)/35kt. Calculate the true track and GS?
186 - 370 kt.
176 - 350 kt.
176 - 370 kt.
186 - 350 kt.
35. An aircraft travels 2.4 statute miles in 47 seconds. What is its groundspeed?
266 kt.
166 kt.
160 kt.
26.6 kt.
36. Given: GS = 122 kt. Distance from A to B = 985 NM, What is time from A to B?
8 hr 24 min.
4 hr 08 min.
8 hr 04 min.
6 ht 15 min.
37. Given: FL250, OAT -15°C, TAS 250 kt. Calculate the Mach No.?
0.38.
0.40.
0.46.
0.45.
38. Given: TAS = 95 kt, HDG(T) = 075°, W/V = 310/20kt. Calculate the drift and GS?
9L - 108 kt.
9R - 104 kt.
9R - 108 kt.
9L - 104 kt
39. What is the time to go if groundspeed is 240 knots distance to go is 500 nm?
134 Min.
125 Min.
29 Min.
25 Min.
40. How far will an aircraft fly in 42 minutes at a ground speed of 400 knots?
280 Min.
260 Min.
328 Min.
305 Min.
41. Given: TAS =465 kt, Track (T) = 007°, W/V = 300/80kt. Calculate the HDG (°T) and GS?
356 - 428 kt.
356 - 424 kt.
358 - 428 kt.
358 - 420 kt.
42. Given the following : Magnetic heading : 060 ° Magnetic variation: 8°W Drift angle: 4° right, what is the true track?
056°
058°
054°
052°
43. Given: True HDG =133°, TAS = 225 kt, Track (T) = 144°, GS = 206 kt, Calculate the W/V?
072/45kt.
072/50kt.
075/50kt.
075/40kt.
44. What is the true altitude if OAT = +35°C and Pressure Altitude = 5000 feet?
4290 ft.
4555 ft.
5550 ft.
5320 ft.
45. Given: TAS = 290 kt, True HDG = 171°, W/V = 310°(T)/30kt Calculate the drift angle and GS?
4°R - 314 kt.
4°L - 314 kt.
5°R - 325 kt.
5°L - 325 kt.
46. Given: TAS = 140 kt, HDG(T) = 005°, W/V = 265/25kt. Calculate the drift and GS?
10R -144 kt.
10L -144 kt.
10R -146 kt.
10L -146 kt.
47. Given: TAS = 235 kt, HDG(T) = 076° W/V = 040/40kt. Calculate the drift angle and GS?
7L - 210 kt
7L - 204 kt.
7R - 204 kt
7R - 214 kt.
48. Given: TAS = 132 kt, True HDG = 257° W/V = 095°(T)/35kt. Calculate the drift angle and GS?
4°L - 155 kt.
4°R - 165 kt.
4°R - 155 kt.
4°L - 165 kt.
49. Given: TAS = 270 kt, True HDG = 145°, Actual wind = 205°(T)/30kt. Calculate the drift angle and GS?
6°R - 275 kt.
6°R - 256 kt.
6°L - 275 kt.
6°L - 256 kt.
50. Given: Pressure Altitude 29000 FT, OAT -55°C. Calculate the Density Altitude?
27850 ft.
27500 ft.
28000 ft.
28900 ft.
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