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CS 25.371 Gyroscopic loads
Available versions for ERULES-1963177438-9391
ED Decision 2005/006/R
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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CS 25.371 Gyroscopic loads ED Decision 2005/006/R The structure supporting any engine or auxiliary power unit must be designed for the loads, including gyroscopic loads, arising from the conditions specified in [CS 25.331](#_DxCrossRefBm1709820915), [CS 25.341](#_DxCrossRefBm1709820927), [CS 25.349](#_DxCrossRefBm1709820948), [CS 25.351](#_DxCrossRefBm1709820961), [CS 25.473](#_DxCrossRefBm1709820981), [CS 25.479](#_DxCrossRefBm1709820980), and [CS 25.481](#_DxCrossRefBm1709820925), with the engine or auxiliary power unit at the maximum rpm appropriate to the condition. For the purposes of compliance with this paragraph, the pitch manoeuvre in [CS 25.331(c)(1)](#_DxCrossRefBm1709820915) must be carried out until the positive limit manoeuvring load factor (point A2 in [CS 25.333(b)](#_DxCrossRefBm1709820896)) is reached. [Amdt 25/1]