35 - ATPL - The maximum zero-fuel mass: 1- is a regulatory limitation 2- is calculated for a maximum load factor of +3.5 g 3- is based on the maximum permissible bending moment at the wing root 4- is defined on the assumption that fuel is consumed from the outer wings tank first 5- is defined on the assumption that fuel is consumed from the centre wing tank first The combination of correct statements is:
Question 35 - Mass and Balance - ATPL - Airline Transport Pilot license
1, 3, 5
2, 3, 4
2, 3, 5
1, 2, 3
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