masses
Is there an easy way of figuring out the relationships between masses eg BEM ZFM TOM Traffic load etc. From the descriptions given in the training manuals and 697 it seems almost impossible.
Question: Given that: - Maximum structural take-off mass: 146 000 kg, - Maximum structural landing mass: 93 900 kg, - Maximum zero fuel mass: 86 300 kg, - Trip fuel: 27 000 kg, - Taxi fuel: 1 000 kg, - Contingency fuel: 1350 kg, - Alternate fuel: 2650 kg, - Final reserve fuel: 3000 kg, Determine the actual take-off mass