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A Class I weight estimate is characterised by

  • A.Statistical fractions applied at aircraft level
  • B.Component-by-component analysis of every part
  • C.Weighing the finished aircraft
  • D.Finite element analysis of the structure

Answer: A

Correct answer: Statistical fractions applied at aircraft level

A Class I estimate is made at the very start of a design, when nothing is defined in detail. It takes the take-off weight and applies fractions drawn from a database of similar aircraft - an empty weight fraction, a fuel fraction - to get a first consistent set of weights. It is quick and it closes the sizing loop; what it cannot do is tell you which group is heavy, because it never looks below aircraft level.

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