Flight Planning and Monitoring - ATPL - Airline Transport Pilot license

Test 10 domande ATPL - Airline Transport Pilot license - Flight Planning and Monitoring, tempo libero

1 - When completing an ATC flight plan, an elapsed time (Item 1 6) of 1 hour 55 minutes should be entered as:

0155 0115 115M 1H55

2 - The fuel burn off is 200 kg/h with a relative fuel density of 0.8. If the relative density is 0.75, the fuel burn will be: 213 kg/h 188 kg/h 200 kg/h 267 kg/h

3 - The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is: 2 700 kg 7 000 kg 10 000 kg 5 700 kg

4 - Given:Distance from departure to destination 2800 NM True track 140W/V 140/100TAS 500 kt What is the distance and time of the PET from the departure point? Distance: 1400 NM Time: 168 min Distance: 1120 NM Time: 112 min Distance: 1120 NM Time: 134 min Distance: 1680 NM Time: 252 min

5 - For a planned flight the calculated fuel is as follows: Flight time: 2h42minThe reserve fuel, at any time, should not be less than 30% of the remaining trip fuel. Taxi fuel: 9 kgBlock fuel: 136 kgHow much fuel should remain after 2 hours flight time? 33 kg trip fuel and 10 kg reserve fuel. 25 kg trip fuel and 8 kg reserve fuel. 33 kg trip fuel and no reserve fuel. 23 kg trip fuel and 10 kg reserve fuel.

6 - What is the the worst hazard, if any, that could be associated with the type of feature at 38°N 015°E ? Reduced visibility Severe attenuation in the HF R/T band There is no hazard Engine flame out and windscreen damage[see Annex]

7 - Refer to the General Student Pilot Route Manual - VFR Chart ED-4Flying VFR from PEITING (47°48.0'N, 010°55.5'E) to IMMENSTADT (47°33.5'N, 010°13.0'E)determine the distance.

46 NM 58 NM 32 NM 36 NM

8 - 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 = -15 kt FL 330 - M = 0.78 Ts = -60°C HWC= - 5 kt FL 290 - M = 0.80 Ts = -55°C HWC = -15 ktFL 270 - M = 0.76 Ts = -43°C HWC = 0 The flight level allowing the highest ground speed is: FL290 FL270 FL370 FL330

9 - When completing an ATC flight plan for a flight commencing under IFR but possibly changing to VFR, the letters entered in Item 8 (FLIGHT RULES) would be: G N/S X Y

10 - An aircraft is in cruising flight at FL 095, GS 155 KT. The pilot intends to descend at 500 fpm to arrive overhead the MAN VOR at 2000' (QNH 1030 hPa). The TAS remains constant in the descent, wind is negligible, temperature standard. At which distance from MAN should the pilot commence the descent? 48 NM 38 NM 41 NM 45 NM

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