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EN ATPL Flight Planning and Monitoring Questions in English
Practise Flight Planning and Monitoring
Use the attached MRJT1 training Figure 4.7.3 for a one-engine-inoperative diversion. Distance to the alternate is 720 NM, tailwind component 25 kt, mass at diversion 55 000 kg, temperature ISA and available diversion fuel 4250 kg. Which is the lowest of the listed pressure altitudes at which the chart indicates these conditions can be met?
Refer to Performance Manual MRJT1 Figure 4.7.2 (One Engine Inop): An aircraft on an extended range operation is required never to be more than 120 minutes from an alternate, based on 1 engine inoperative LRC conditions in ISA. Using the above table and a given mass of 40000 kg at the most critical point, the maximum air distance to the relevant alternate is:
Refer to Performance Manual MRJT1 Figure 4.5.4 (Descent) A descent is planned at.74/250KIAS from 35000 ft to 5000 ft. How much fuel will be consumed during this descent?
Refer to the original fictional route-network diagram. Every drawn segment may be flown in either direction. Which route follows the labelled segments from START to FINAL via NODAL and then CROSS, in that order?
Using only the published level allocation and minimum level on the attached historical E LO 2 training chart, which listed flight level is appropriate on airway B3 from CHATILLON (CTL, 49°08'N 003°35'E) to CAMBRAI (CMB, 50°14'N 003°09'E)?
The navigation plan reads: Trip fuel: 100 kg Flight time: 1h35min Taxi fuel: 3 kg Block fuel: 181 kg The endurance on the ICAO flight plan should read:
The maximum permissible take-off mass of an aircraft for the L wake turbulence category on an ATC flight plan is:
For an ATC flight plan filed before the flight, the indicated time of departure is:
Refer to the original fictional training-route diagram. The planned route is DEP-FIX1-FIX2-DEST, with consecutive leg distances of 18 NM, 27 NM and 36 NM. Top of climb (TOC) is reached 32 NM after DEP, measured along this route. What distance remains from TOC to DEST along the planned route?
An aeroplane has the following masses: ESTLWT= 50.000 kg; Trip fuel= 4.300 kg; Contingency fuel= 215 kg; Alternate fuel (final reserve included)= 2.100 kg Taxi= 500 kg; Block fuel= 7.115 kg; Before departure the captain orders to make the block fuel 9.000 kg. The trip fuel in the operational flight plan should read:
