Test 10 Questions ATPL - Airline Transport Pilot license - Flight Planning and Monitoring, no time limit

1 - Which of the following statements is (are) correct with regard to computer flight plans1. The computer takes account of bad weather on the route and adds extra fuel.2. The computer calculates alternate fuel sufficient for a missed approach, climb, cruise, descent and approach and landing at the destination alternate.
2 - Refer to the General Student Pilot Route Manual ED-4:Flying VFR from PEITING (47°48.0'N, 010°55.5'E) to IMMENSTADT (47°33.5'N, 010°13.0'E).Determine the minimum altitude within a corridor 5 NM left and 5 NM right of the courseline in order to stay 1000' clear of obstacles.
question fp7.webp
3 - An aircraft plans to depart London at 1000 UTC and arrive at Munich (EDDM) at 1215 UTC. In the ATC flight plan Item 16 (destination/EET) should be entered with:
4 - Given:Distance from departure to destination: 180 NM Endurance: 2 hTAS: 120 ktGround Speed Out: 135 kt Ground Speed Home: 105 ktWhat is the distance and time of the PSR from the departure point?
5 - Which is the heaviest type of precipitation, if any, forecast for BORDEAUX/MERIGNAC at 1000 UTC ?
6 - Prior to an IFR flight, when filling in the ATC flight plan, the time information which should be entered in box 16: 'Total estimated time' is the time elapsed from:
question fp34.webp
7 - Given: Maximum allowable take-off mass 64 400 kg maximum landing mass 56200 kgmaximum zero fuel mass 53 000 kgdry operating mass 35 500 kgestimated load 14 500 kg estimated trip fuel 4 900 kgminimum take-off fuel 7 400 kg.Find: maximum additional load
8 - Which of the following statements regarding filing a ATC flight plan is correct?
9 - Given:Dry operating mass (DOM)= 33510 kg Traffic Load= 7600 kgTrip fuel (TF)= 2040 kg Final reserve fuel= 983 kg Alternate fuel= 1100 kgContingency fuel= 5% of trip fuelWhich of the listed estimated masses is correct?
10 - See Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.4 Given:Distance B - C: 350 NM Cruise 300 KIAS at FL 210 Temperature: - 40°C Tailwind component:70 kt Gross mass at B: 53 200 kgThe fuel required from B - C is: