PPRuNe Forums - View Single Post - A320 loss of all pitot vs Mach
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Old 16th Feb 2010, 09:30
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john_tullamarine
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It does NOT depend on IAS but on TAS M = TAS / a

.. respectfully suggest you might do a bit more homework. Your equation is quite correct but the normal calculation for M works on CAS and Hp, I suggest. No point using less accurate data when you have immediate inputs.

Example thread plucked out of the air is this one.
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