E) In reality a slightly larger tail surface area is chosen than the one computed in the previous question. What is/are the operational advantage(s) the user will experience when using this aircraft? (Multiple answers can be correct) The larger tail will produce more lift, relieving the lift production of the wings. This reduces their drag and increases the range. The pilot has to worry less about positioning his payload, as the range of allowed centre of gravity positions is larger. The aircraft becomes more stable and hence easier to fly. The aircraft becomes easier to fly, as the larger tail surface makes it more agile. unanswered