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EN ATPL Flight Planning and Monitoring Questions in English
Practise Flight Planning and Monitoring
Given: Distance from departure to destination: 400 NM Endurance: 2,5 h TAS: 115 kt Ground Speed Out: 130 kt Ground Speed Home: 105 kt What is the distance of the PSR from the departure point?
Given: Distance from departure to destination: 210 NM Endurance: 3,5 h True Track: 310 W/V: 270/30 TAS: 120 kt What is the distance of the PSR from the departure point?
Given: Distance from departure to destination: 3750 NM Endurance: 9,5 h True Track: 360 W/V: 360/50 TAS: 480 kt What is the distance of the PSR from the departure point?
In a simplified constant-condition flight-planning exercise, departure-to-destination distance is 330 NM, outbound true track is 170 degrees, wind is from 140 degrees true at 25 kt, and TAS is 125 kt on both outbound and return legs. Safe endurance after protecting the required reserves is 5 hours, with the same constant fuel flow in both directions. Use the complete wind triangle. What is the distance of the point of safe return (PSR) from departure, rounded to the nearest whole nautical mile?
Which of the following statements is (are) correct with regard to the advantages of computer flight plans? 1. The computer can file the ATC flight plan. 2. Wind data used by the computer is always more up-to-date than that available to the pilot.
Use the attached MRJT1 training Figure 4.5.1 for an en-route climb at 280 KIAS/Mach 0.74 from a sea-level airport to FL280. Brake-release mass is 57 500 kg, ISA deviation is -10 degrees C and the headwind component is 16 kt. What still-air distance (NAM) and ground distance (NGM), rounded to whole nautical miles, are obtained using the table and its ground-distance correction?
'Integrated range' curves or tables are presented in the Aeroplane Operations Manuals. Their purpose is
Refer to Performance Manual MRJT1 Page 21 Figure 4.5.1 En-route Climb 280/0.74 (continued) Find: Time, Fuel, Still-Air Distance and TAS for an enroute climb 280/.74 to FL 350. Given: Brake release mass 64000 kg, ISA +10°C, airport elevation 3000'
A minimum sector altitude (MSA) is defined in relation to a radio navigation facility. Unless a different distance is specified, this altitude is valid within:
Using the attached CAA CAP 697 SEP1 training Figure 2.1 (July 2006 corrected edition), estimate time, fuel and still-air distance to climb. Initial climb mass: 3 500 lb; departure pressure altitude: 2 500 ft; departure OAT: +10°C; cruising pressure altitude: 14 000 ft; cruise OAT: -5°C. Use the associated climb conditions and subtract the departure cumulative readings from the cruise cumulative readings.
