Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
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)
Version
CS-25 Amdt 27 - La... (Jan 2023)
Section
Share
Version
Show details
Hide details
Version
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.