#2. 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?
#3. 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:
#4. 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:
#5. How many feet you have to climb to reach FL 75? Departure aerodrome elevation = 1500ft QNH = 1023 hPa. Temperatue = ISA. 1 hPa = 30ft.
#6. 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;
#7. 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
#8. 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?
#9. An airfield elevation of 900 ft and a QNH of 1019 hPa, determine the aerodrome pressure altitude:
#10. At an airfield where the Relative Humidity is high:
#11. 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:
#12. 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:
#13. Unless otherwise shown on charts for standard instrument departure routes the routes are given with:
#14. A flight plan is required to be filed by:
#15. A flight plan can be submitted:
#16. Letter W in ITEM 10 of flight plan indicates.
#17. To indicate to ATC that you are evacuating a critically injured on board, following will be added in box 18 of flight plane form
#18. 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:
#19. 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:
#20. 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:
#21. 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:
#22. In the ATS flight plan item 19, emergency and survival equipment carried on the flight should be indicated by:
#23. Item 9 of the ATS flight plan includes “NUMBER AND TYPE OF AIRCRAFT”. In this case “NUMBER” means:
#24. 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:
#25. 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:
#26. The maximum permissible take-off mass of an aircraft for the L wake turbulence category on a flight plan is:
#27. 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:
#28. 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:
#29. If your destination airport has no ICAO indicator, in the appropriate box of your flight plan, you write:
#30. 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?
