FAA Airline Transport Pilot (ATM)Aircraft Performance and Weight and BalanceMedium

A turbojet transport is in cruise flight and steadily burning fuel, reducing its gross weight over time. Assuming a constant Mach number, how does the airplane's optimum cruise altitude typically change as weight decreases, and why?

  1. AOptimum altitude increases, because at lower weight the airplane can fly at a higher altitude while still operating near its best lift-to-drag ratio for maximum specific range
  2. BOptimum altitude remains constant regardless of weight, since it depends only on outside air temperature
  3. COptimum altitude decreases, because thinner air at higher altitude increases fuel consumption as weight is reduced
  4. DOptimum altitude decreases, because lower weight requires less lift and thus lower altitude for efficiency
Show answer & explanation

Correct answer: A. Optimum altitude increases, because at lower weight the airplane can fly at a higher altitude while still operating near its best lift-to-drag ratio for maximum specific range

As fuel burns off and weight decreases, less lift is required, so the airplane can climb to a higher altitude while still operating at its optimum angle of attack for best L/D and specific range. This is the basis for step climbs during long-range cruise, allowing the airplane to trade decreasing weight for increasing efficient altitude.

Why the other options are wrong

  • B. Optimum altitude is a function of weight (and speed/temperature), not temperature alone.
  • C. Higher altitude at lower weight typically improves, not worsens, fuel efficiency near optimum L/D.
  • D. This reverses the actual relationship; lower weight allows higher, not lower, optimum altitude.

Optimum Cruise Altitude

The altitude at a given weight and Mach number that yields the best specific range (maximum distance per pound of fuel), which increases as weight decreases during cruise.

  • Lower weight allows higher optimum altitude at constant Mach
  • Basis for step-climb cruise procedures
  • Optimum altitude corresponds to best lift-to-drag ratio
  • Differs from maximum (service) ceiling, which is thrust-limited

Memory trick: Lighter plane, higher home — burn fuel, climb higher for best mileage

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