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A climb gradient required is 3.3%. For an aircraft maintaining 100 kt true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately:

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Question 6: A climb gradient required is 3.3%. For an aircraft maintaining 100 kt true airspeed, no wind, this climb gradient corresponds to a rate of climb of approximately:

  1. Identify the given values and the formula for climb gradient.

    Climb Gradient (CG) = 3.3% = 0.033 (in decimal form)
    True Airspeed (TAS) = 100 kt
    The relationship between climb gradient, rate of climb (RoC), and true airspeed is:

    CG=RoCTASCG = \frac{RoC}{TAS}

  2. Convert True Airspeed (TAS) to feet per minute.

    1 knot is 1 nautical

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