Originally Posted by
Goldenrivett
That’s not what crews should have to be doing.
If you can’t make the published stop altitude or MSA within 10 mins of TOGA, then the procedure needs to be changed - not the number of engine cycles at TOGA.
Crews should be able to determine the maximum landing weight which would give them enough performance on an engine out GA to comply with one application of GA thrust of <10 mins.
We had that necessary software enabled.
I agree with that. Though the problem will be takeoff from there then OEI and during landing back and go around. I am not certain whether that will restrict takeoff weight also.