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AMC 25.149(e) Minimum control speed
Available versions for ERULES-1963177438-8277
ED Decision 2003/2/RM
found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)
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AMC 25.149(e) Minimum control speed ED Decision 2003/2/RM During determination of VMCG, engine failure recognition should be provided by: a. The pilot feeling a distinct change in the directional tracking characteristics of the aeroplane, or b. The pilot seeing a directional divergence of the aeroplane with respect to the view outside the aeroplane.