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EN ATPL Flight Planning and Monitoring Questions in English
Practise Flight Planning and Monitoring
Given: Distance from departure to destination: 180 NM Endurance: 2 h TAS: 120 kt Ground Speed Out: 135 kt Ground Speed Home: 105 kt. What is the distance and time of the PSR from the departure point?
Given: Distance from departure to destination: 2000 NM Endurance: 5 h TAS: 500 kt Ground Speed Out: 480 kt Ground Speed Home: 520 kt. What is the distance of the PSR from the departure point?
Given: Distance from departure to destination: 950 NM Endurance: 3,5 h TAS: 360 kt Ground Speed Out: 320 kt Ground Speed Home: 400 kt. What is the distance and time of the PSR from the departure point?
Given: Distance from departure to destination: 210 NM Endurance: 2,5 h True Track: 035 W/V: 250/20 TAS: 105 kt. What is the distance of the PSR from the departure point?
For computer-generated operational flight plans under the EU basic fuel scheme for performance class A aeroplanes, which statements are correct? 1. The computer independently decides how much discretionary fuel to add for bad weather, without a decision by the commander. 2. Destination alternate fuel includes a missed approach at the destination, climb, cruise, descent, approach and landing at the destination alternate.
Given: FL 330 long range cruise OAT -63°C gross mass 50 500 kg. Find: true airspeed (TAS)
Using the attached MRJT1 training Figure 4.2 (Short Distance Cruise Altitude), which listed pressure altitude is closest to the chart reading for brake-release mass 45 000 kg, ISA +20 degrees C and trip distance 50 nautical air miles (NAM)?
Planning an IFR-flight from Paris (Charles de Gaulle) to London (Heathrow) for the twin jet aeroplane. Given: Estimated Take-off Mass (TOM) 52000 kg, Airport elevation 387 ft, FL 280, W/V 280°/40 kt, ISA Deviation -10°C, Average True Course 340° Find: Time to the top of climb (TOC)
According to ICAO rules for the ATC flight plan (Item 9), the wake turbulence category 'H' (Heavy) indicates an aircraft with a maximum certificated take-off mass of:
