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CS 23.2100 Mass and centre of gravity
Available versions for ERULES-1963177438-6801
ED Decision 2017/013/R
found in: CS-23 Amdt 5 AMC-GM Issue 3 - Normal-Category Aeroplanes (Jul 2020)
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CS 23.2100 Mass and centre of gravity ED Decision 2017/013/R (a) The applicant must determine limits for mass and centre of gravity that provide for the safe operation of the aeroplane. (b) The applicant’s design must comply with each requirement of this Subpart at critical combinations of mass and centre of gravity within the aeroplane’s range of loading conditions using acceptable tolerances. (c) The condition of the aeroplane at the time of determining its empty mass and centre of gravity must be well defined and easily repeatable.
CS 23.2100 Mass and centre of gravity ED Decision 2017/013/R (a)    The applicant must determine limits for mass and centre of gravity that provide for the safe operation of the aeroplane. (b)    The applicant’s design must comply with each requirement of this Subpart at critical combinations of mass and centre of gravity within the aeroplane’s range of loading conditions using acceptable tolerances. (c)     The condition of the aeroplane at the time of determining its empty mass and centre of gravity must be well defined and easily repeatable.
#### CS 23.2100 Mass and centre of gravity *ED Decision 2017/013/R* (a) The applicant must determine limits for mass and centre of gravity that provide for the safe operation of the aeroplane. (b) The applicant’s design must comply with each requirement of this Subpart at critical combinations of mass and centre of gravity within the aeroplane’s range of loading conditions using acceptable tolerances. (c) The condition of the aeroplane at the time of determining its empty mass and centre of gravity must be well defined and easily repeatable.