The Maximum Certificated Take-off Mass is:
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A
a take-off limiting mass which is affected by the aerodrome altitude and temperature.
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B
a structural limit which may not be exceeded for any take-off.
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C
a take-off limiting mass which is governed by the gradient of climb after reaching V2 .
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D
limited by the runway take-off distance available. It is tabulated in the Flight Manual.
The Maximum Certificated Take-off Mass is the maximum mass at which the aircraft is certified for take-off due to structural or other limits.
It is a fixed value, does not vary with changes in temperature, altitude or runway available and is usually measured in units of kilograms or pounds.
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