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AMC 25.1583(i) Manoeuvring Flight Load Factors
Available versions for ERULES-1963177438-8805
ED Decision 2003/2/RM
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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CS-25 Amdt 27 - La... (Jan 2023)
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AMC 25.1583(i) Manoeuvring Flight Load Factors ED Decision 2003/2/RM The flight manoeuvring limit load factors for which the structure is approved, expressed in terms of normal acceleration, or g, should be included. If more restrictive flight load factors are established for particular operations outside the normal operating envelope (e.g. landing flap position with maximum take-off weight) such factors should be presented and defined.