Doc. No.: SHARK600_MA_075
1.13 List of Abbreviations
Calibrated airspeed; Indicated speed corrected
for installation and instrument errors. CAS is
equal to TAS at standard atmospheric
conditions at MSL
Point of equilibrium for the airplane mass
(weight)
Distance from the reference datum to the CG,
it is determined by dividing the total moment
(sum of the individual moments) by the total
mass (weight)
The CG range which an airplane with a given
mass must be operated within
Demonstrated
crosswind
component
The max. speed of the crosswind component
at which the maneuverability of the airplane
during take-off and landing has been
demonstrated during test flights
Empty Mass (Weight) of the airplane including
unusable fuel, all operating fluids and
maximum oil amount. Movable ballast is not
included in Empty Weight
Ground Speed. Speed of the airplane relative
to the ground