Doc. No.: SHARK600_MA_075
Indicated airspeed as shown on the airspeed
indicator
International Standard Atmosphere
Calibrated airspeed on knots
Indicated airspeed in knots
The horizontal distance from the reference
datum to the center of gravity (of a
component)
Manifold (intake) Pressure
MCPMaximum permissible
continuous engine output power
during flight
Maximum mass (weight) permissible for
landing
The mass (weight) of a component multiplied
by its lever arm
Miles (nautical) per US gallon
Maximum Take-off Mass (Weight), the
maximum mass (weight) permissible for take-
off
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