35 - ATPL Question Bank in English - For a conventional transport aeroplane whose maximum zero-fuel mass is limited by wing-root bending loads, which statements are correct? 1 - It is an approved structural mass limitation. 2 - It is always calculated using a maximum load factor of +3.5 g. 3 - It limits the permissible wing-root bending loads for the certificated loading conditions. 4 - It always requires the outer wing tanks to be used first. 5 - The certified fuel-distribution assumptions and approved tank-use sequence must be respected. The combination of correct statements is:

Question 35 - Mass and Balance - ATPL - Airline Transport Pilot Licence