John, very integrated understanding of reliability and diagnoses in aviation. Salute!!! Would maybe worth it to mention that:
Climb Gradient Relative to Speed in a Specific Flaps’ Configuration
If one engine is lost before reaching V2, then the initial climb is flown at V2. If thrust is lost at a speed between V2 and V2+10, then the current speed is maintained, to ensure the most efficient climb speed. It is not necessary to increase pitch, in order to reduce the speed to V2, when a higher speed has already been reached.
Cheers.
