Hi all.
I have a query regarding what I suspect was a trick question within the Performance exam (which I answered incorrectly).
An aircraft with a IAS of 110 and subject to a 15 kt headwind would require what ROC to achieve a minimum 3.2% climb gradient?
Now, I answered the question based on the information provided as it didn't state whether the aircraft was in a take-off or landing configuration. Should I have assumed the info was for an aircraft was in a take-off configuration? I guess so as I was incorrect and the calculation itself is not complicated.
Thanks, Rich
It really doesn't matter what configuration the aircraft is in. The climb gradient of any thing that flies, including ducks and geese, is a function of its ground speed and its rate of climb. In this case, in the absence of any information on pressure height and temperature, you can assume that the IAS is also the TAS. Therefore the ground speed would be 110 - 15 = 95kt. The rate of climb required would be 95 x 3.2 = 304 ft/min.
Thanks, Bob.
I must have missed something within the question. I can't recall the exact wording.
