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CS 23.2225 Component loading conditions
Available versions for ERULES-1963177438-6836
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 23.2225 Component loading conditions ED Decision 2017/013/R (a) The applicant must determine the loads acting upon all relevant structural components, in response to: (1) interaction of systems and structures; (2) structural design loads; (3) flight load conditions; and (4) ground and water load conditions. (b) The complete pressurised cabin, including doors, windows, canopy and valves, is exposed as a pressure vessel for the maximum relief valve setting multiplied by a factor of 1.33, without considering other loads.
CSÂ 23.2225 Component loading conditions ED Decision 2017/013/R (a)Â Â Â Â The applicant must determine the loads acting upon all relevant structural components, in response to: (1)Â Â Â Â interaction of systems and structures; (2)Â Â Â Â structural design loads; (3)Â Â Â Â flight load conditions; and (4)Â Â Â Â ground and water load conditions. (b)Â Â Â Â The complete pressurised cabin, including doors, windows, canopy and valves, is exposed as a pressure vessel for the maximum relief valve setting multiplied by a factor of 1.33, without considering other loads.
#### CSÂ 23.2225 Component loading conditions *ED Decision 2017/013/R* (a) The applicant must determine the loads acting upon all relevant structural components, in response to: (1) interaction of systems and structures; (2) structural design loads; (3) flight load conditions; and (4) ground and water load conditions. (b) The complete pressurised cabin, including doors, windows, canopy and valves, is exposed as a pressure vessel for the maximum relief valve setting multiplied by a factor of 1.33, without considering other loads.