Email
info@vayudootaviation.com
Phone No
+91 7276526726
become a pilot
Home
About us
courses
CPL
ATPL
RTR(A)
Airline Cadet Program
IGRUA Entrance Prep
B.Sc. Aviation
Pilot Training
INDIA
USA
CANADA
SOUTH AFRICA
NEW ZEALAND
EUROPE
Aircraft Type-Rating
Airbus A320
Boeing 737
Blogs
contact
CPL Test Series
Question Bank
Questions for CRP5
Answer the following questions
Test Mode
Training Mode
1. Given: TAS =227 kt, Track (T) = 316°, W/V = 205/15kt. Calculate the HDG (°T) and GS?
310 - 222 kt.
310 - 231 kt.
314 - 230 kt.
312 - 232 kt.
2. Given: TAS =200 kt, Track (T) = 110°, W/V = 015/40kt. Calculate the HDG (°T) and GS?
096 - 200 kt.
099 - 202 kt.
099 - 199 kt.
096 - 199 kt.
3. 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?
20 kt and 45 kt.
25 kt and 35 kt.
25 kt and 30 kt.
20 kt and 40 kt.
4. Given: Maximum allowable tailwind component for landing 10 kt. Planned runway o5 (047° magnetic). The direction of the surface wind reported by ATIS 210°. Variation is 17°E. Calculate the maximum allowable windspeed that can be accepted without exceeding the tailwind limit?
14 kt.
5 kt.
11 kt.
18 kt.
5. What is the time to go if groundspeed is 440 knots distance to go is 500 nm?
59 Min.
114 Min.
120 Min.
68 Min.
6. Given: FL 350, Mach 0.80, OAT - 55°C. Calculate the values for TAS and local speed of sound (LSS)?
465 kt, LSS 575 kt.
460 kt, LSS 575 kt.
460 kt, LSS 567 kt.
460 kt, LSS 570 kt.
7. Given: IAS 100 kt, FL 45, OAT +15°C. What is the TAS?
113.5 kt.
119.5 kt.
108.5 kt.
112.0 kt.
8. Given: TAS = 190 kt, True HDG = 085°,W/V = 110°(T)/50kt. Calculate the drift angle and GS?
8°L - 146 kt.
8°L - 140 kt.
8°L - 140 kt.
8°R - 146 kt.
9. Given: TAS 487kt, FL 330, Temperature ISA + 15. Calculate the MACH Number?
0.83.
0.80.
0.81.
0.79.
10. Given: TAS = 95 kt, HDG(T) = 075°, W/V = 310/20kt. Calculate the drift and GS?
9L - 108 kt.
9L - 104 kt
9R - 104 kt.
9R - 108 kt.
11. Given: IAS 125 kt, FL 60, OAT+25°C. What is the TAS?
124 kts.
121 kts.
115 kts.
142 kts.
12. Given: True HDG =035°, TAS = 245 kt, Track (T) = 046°, GS = 220 kt, Calculate the W/V?
340/45kt.
340/55kt.
345/50kt.
340/50kt.
13. Given: GS = 435 kt. Distance from A to B = 1920 NM, What is time from A to B?
4 hr 30 min.
4 hr 35 min.
4 hr 20 min.
4 hr 25 min.
14. 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?
321° / 50 kt.
322° / 60 kt.
320° / 45 kt.
320° / 60 kt.
15. Given: Magnetic heading = 255° VAR = 40°W GS = 375 kt W/V = 235°(T)/ 120 kt Calculate the drift angle?
9° left.
7° left.
4° left.
7° right.
16. Given: TAS = 270 kt, True HDG = 270°, Actual wind 205°(T)/30kt, Calculate the drift angle and GS?
12R - 269kt.
6R - 269kt.
6L - 259kt.
6R - 259kt.
17. Given: IAS 89 kt, FL 25, OAT +10°C. What is the TAS?
91.0 kt.
90.5 kt.
95.5 kt.
92.5 kt.
18. 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°/50 kt.
160°/50 kt.
160°/60 kt.
150°/60 kt.
19. Given: Course 040°(T), TAS is 120 kt, Wind speed 30 kt, Maximum drift angle will be obtained for a wind direction of
210°.
120°.
330°.
130°.
20. Given: TAS = 132 kt, True HDG = 257° W/V = 095°(T)/35kt. Calculate the drift angle and GS?
4°R - 155 kt.
4°R - 165 kt.
4°L - 165 kt.
4°L - 155 kt.
21. How long will it take to fly 5 NM at a groundspeed of 269 Kt?
1 min 11 sec.
1 min 07 sec.
1 min 17 sec.
1 min 10 sec.
22. Given: TAS = 140 kt, True HDG = 302°, W/V = 045°(T)/45kt Calculate the drift angle and GS?
16°R - 166 kt.
16°R - 156 kt.
16°L - 156 kt.
16°L - 166 kt.
23. Given: GS = 510 kt, DIstance A to B = 43 NM What is the time (MIN) fro A to B?
4.5.
6.5.
5.
4.
24. Given: Pressure Altitude 29000 FT, OAT -55°C. Calculate the Density Altitude?
27850 ft.
28900 ft.
28000 ft.
27500 ft.
25. Given: TAS =270 kt, Track (T) = 260°, W/V = 275/30kt. Calculate the HDG (°T) and GS?
263 -241 kt.
261 - 240 kt.
260 - 241 kt.
260 - 242 kt.
26. What is the ETA at Z if TAS = 120 Kts?
1320 UTC.
1305 UTC.
1325 UTC.
1255 UTC.
27. Given: True course A to B = 250° Distance A to B = 315 NM TAS = 450 kt. W/V = 200°/60kt. ETD A = 0650 UTC. What is the ETA at B?
0732 UTC.
0659 UTC.
0736 UTC.
0726 UTC.
28. 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 - 256 kt.
6°L - 275 kt.
29. Given: TAS = 205 kt, HDG (T) = 180°, W/V = 240/25kt. Calculate the drift and GS?
6L - 196 kt.
6R - 194 kt.
6L - 194 kt.
6L - 192 kt.
30. Given: TAS = 485 kt, HDG (T) = 168°, W/V = 130/75kt. Calculate the Track (°T) and GS?
179 - 425 kt
170 - 425 kt.
172 - 428 kt.
174 - 428 kt.
31. Given the following : Magnetic heading : 060 ° Magnetic variation: 8°W Drift angle: 4° right, what is the true track?
056°
054°
052°
058°
32. Given: True HDG =002°, TAS = 130 kt, Track (T) = 353°, GS = 132 kt, Calculate the W/V?
090/25kt
090/30kt.
095/20kt.
098/25kt.
33. For a given track the : Wind component = +45 kt Drift angle = 15° left TAS = 240 kt What is the wind component on the reverse track?
85 kts.
-45 kts.
-65 kts.
-85 kts.
34. What is the true altitude if OAT = +35°C and Pressure Altitude = 5000 feet?
5320 ft.
5550 ft.
4290 ft.
4555 ft.
35. Given: GS = 120 kt. Distance from A to B = 84 NM, What is time from A to B?
00 hr 42 min.
00 hr 40 min.
00 hr 44 min.
00 hr 41 min.
36. Given: GS = 236 kt. Distance from A to B =354 NM, What is time from A to B?
2 hr 03 min.
1 hr 35 min.
1 hr 30 min.
1 hr 15 min.
37. Fuel flow per HR is 22 US-GAL, total fuel on board is 83 IMP GAL. What is the endurance?
3 hr 32 min.
4 hr 32 min.
3 hr 46 min.
4 hr 46 min.
38. Given: TAS = 230 kt, HDG (T) = 250°, W/V = 205/10kt. Calculate the drift and GS?
2L - 220 kt.
2L - 223 kt.
2R - 223 kt.
2R - 220 kt.
39. Given: True Heading = 090° TAS = 180 kt GS = 180 kt Drift 5° right Calculate the W/V?
300° / 15 kt.
360° / 5 kt.
360° / 15 kt.
360° / 25 kt.
40. How far will an aircraft fly in 47 minutes at a ground speed of 420 knots?
329 Min.
360 Min.
338 Min.
380 Min.
41. Given: TAS = 485 kt, OAT = ISA +10°C, FL 410. Calculate the Mach number?
0.833.
0.815.
0.825.
0.852.
42. An aircraft travels 100 statute miles in 20 min, how long does it take to travel 215 nm?
48 min.
50 min.
51 min.
46 min.
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. Given: True Heading = 090° TAS = 200 kt W/V = 220°/30 kt. Calculate the GS?
200 kt.
220 kt.
240 kt.
180 kt.
45. Given: Course 095°(T), TAS is 220 kt, Wind speed 70 kt, Maximum drift angle will be obtained for a wind direction of
335°.
215°.
165°.
185°.
46. How many NM would an aircraft travel in 1 MIN 45 SEC if GS is 135 kt?
4.35.
3.25.
3.45.
3.95.
47. Given: true track is 348°, drift 17° left, variation 32° W, Deviation 4°E. What is the compass heading?
041°.
044°.
141°.
033°.
48. Given: GS = 480 kt. Distance from A to B = 5360 NM, What is time from A to B?
11 hr 15 min.
11 hr 10 min.
11 hr min.
11 hr 20 min.
49. Given: True heading = 310° TAS = 200 kt GS = 176 kt Drift angle 7° right. Calculate the W/V?
270° / 43 kt.
273° / 33 kt.
265° / 30 kt.
270° / 33 kt.
50. Given: TAS = 472 kt, True HDG = 005°, W/V = 110°(T)/50kt. Calculate the drift angle and GS?
4°L - 487 kt.
6°L - 487 kt.
4°R - 487 kt.
6°R - 487 kt.
Submit
Make New Set