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CPL Test Series
Question Bank
Questions for R* B*LI FLIGHT PLANNING
Answer the following questions
Test Mode
Training Mode
1. The fuel burn off is 200kg/h with a relative fuel density of 0.8. If the relative density is 0.75, the fuel burn will be
188kg
200kg
267kg
2. How many feet you have to climb to reach FL 75? Departure aerodrome elevation = 1500ft QNH = 1023 hPa. Temperatue = ISA. 1 hPa = 30ft
6600 ft
6000 ft
6300 ft
3. An airfield elevation of 900 ft and a QNH of 1019 hPa, determine the aerodrome pressure altitude
750 ft
720 ft
780 ft
4. The maximum permissible take-off mass of an aircraft for the L wake turbulence category on a flight plan is
5700kg
10000kg
7000kg
5. To indicate to ATC that you are evacuating a critically injured on board, following will be added in box 18 of flight plane form
PAN MED
STS
MEDEVAC
6. An aircraft, following a 215° true track, must fly over a 10600ft obstacle with a minimum obstacle clearance of 1500ft. Knowing the QNH received from an airport close by, which is almost at sea-level, is 1035 and the temperature is ISA-15°C, the minimum flight level will be
130
120
140
7. True course (TC) 017°, W/V 340°/30kt, True air speed (TAS) 420kt find: Wind correction angle (WCA) and ground speed (GS)
WCA -2°, GS 396kt
WCA -2°, GS 426kt
WCA +2°, GS 396kt
8. You are flying a constant heading of 252°. Variation is 22°E, deviation is 3°W and your INS is showing a drift of 9° right. The true track is?
280°
242°
224°
9. The measured course 042° T. The variation in the area is 6°W and the wind is calm. The deviation is 4° W. In order to follow this course, the pilot must fly a compass heading of
044°
058°
052°
10. On a given path, it is possible to choose between four flight levels (FL), each associated with a mandatory flight Mach Number (M). The flight conditions, static air temperature (SAT) and headwind component (HWC) are given below: FL 370; M=0.80; Ts=-60°C; HWC=-15kt FL330; M=0.78; Ts=-60°C; HWC = -5kt FL290; M=0.80; Ts=-55°C; HWC = -15kt FL270; M=0.76; Ts=-43°C; HWC=0kt The flight level allowing the highest ground speed is
FL 330
FL 290
FL 270
11. When an ATS flight plan has been submitted for a controlled flight, the flight plan should be amended or canceled in the event of the off-block time being delayed by
90 minutes or more
30 minutes or more
60 minutes or more
12. Letter W in ITEM 10 of flight plan indicates
Weather Radar on board
Route designator in India
RVSM approved
13. In the appropriate box of a flight plan form, concerning equipment, the letter to be used to indicate that the aircraft is equipped with a mode A4096 codes transponder with altitude reporting capcability is
C
A
S
14. A flight plan is required to be filed by
Any flight with in advisory airspace
Any IFR or VFR flight with in controlled airspace
Only IFR flights within controlled airspace
15. At an airfield where the Relative Humidity is high
Take-off performance of an aircraft will be enhanced
There will be no change in performance of the aircraft
The climb performance of an aircraft will be degraded
16. Unless otherwise shown on charts for standard instrument departure routes the routes are given with
true headings
magnetic course
magnetic headings
17. If your destination airport has no ICAO indicator, in the appropriate box of your flight plan, you write
XXXX
AAAA
ZZZZ
18. In the ATS flight plan item 19, emergency and survival equipment carried on the flight should be indicated by
crossing out the box relevant to any equipment not carried
circling the relevant box
listing the items carried on the "REMARKS" line
19. Item 9 of the ATS flight plan includes "NUMBER AND TYPE OF AIRCRAFT". In this case "NUMBER" means
the registration number of the aircraft
the ICAO type designator number as set in ICAO Doc 8643
the number of aircraft flying in a group
20. A flight plan can be submitted
24 hrs before ETD
30 days before EOBT
120 hrs before EOBT
21. In the appropriate box of a flight plan form, corresponding to the estimated time of departure, the time indicated is that at which the aircraft intends to
pass the departure beacon
start-up
go off-blocks
22. In the ATS flight plan item 10 (equipment), the letter to indicate the carriage of a serviceable transponder-mode A (4 digits-4096 codes) and mode C, is
A
C
P
23. On a flight plan you are required to indicate in the box marked "speed" the planned speed for the first part of the cruise or for the entire cruise. This speed is
The indicated airspeed
The estimated ground speed
The true airspeed
24. In order to Take-Off an aircraft requires a Runway Headwind Component of at least 15 Kts. The maximum permitted Cross Wind Component is 30 Kts. The Runway in use is 09 and the Wind Direction is 130°. The minimum and maximum wind speeds that will allow take-off are
46 and 25 kts
20 and 46 kts
25 and 46 kts
25. You are to determine the maximum fuel load which can be carried in the following conditions: - dry operating mass: 2800 kg -trip fuel: 300kg -payload: 400kg -maximum take-off mass: 4200 kg - maximum landing mass: 3700kg
800kg
1000kg
1800kg
26. The still air distance in the climb is 189 Nautical Air Miles (NAM) and the time 30 minutes. What ground distance would be covered in a 30kt headwind?
174NM
188NM
193NM
27. When completing an ATS flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in Item8 (FLIGHT RULES) would be
Y
G
X
28. You have a flight plan IFR from Amsterdam to London. In the flight plan it is noted that you will deviate from the ATS route passing the FIR boundary Amsterdam/London. The airway clearance reads: Cleared to London via flight planned route. Which of the following statements is correct?
The filed deviation is not accepted
It is not allowed to file such a flight plan
The route according to the flight plan is accepted
29. A twin-jet aero plane carries out the X-Y flight. When it reaches point K (35°N, 048°W) a non-mechanical event makes the Captain consider rerouting to one of the three following fields. The flight conditions are: - from K to A (distance 847NM, headwind component =18kt) -from K to B (distance 1112NM, tailwind component = 120kt) - from K to C (distance 883NM, wind component = 0) With an aero plane true airspeed of 460 kt, the field selected will be that more rapidly reached
A
B
A or C, or B
30. When calculating the fuel required to carry out a given flight, one must take into account: 1. the wind 2. foreseeable airborne delays 3. other weather forecasts 4. any foreseeable conditions which may delay landing. The combination of correct statements is
1, 3
1, 2, 3
1, 2, 3, 4
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