Originally Posted by
JABBARA
Thank you Sonicbum
You are right I mistakenly wrote LCG, I corrected it as ACG (Approach Climb Gradient)
That is right if available,
In our FSA there was no such a calculation
The only one on FSA was based on to meet requirement as in EASA CS 25.121 Climb: one-engine-inoperative (d) (1),
If the entered landing weight for given landing condition (including selected CONF) was too much to be able to meet a momentary 2.1 % with single engine +GA Flap + L/G UP, further landing parameters are not calculated.
However the way you describe is not clear for me, if you enter a standart Missed approach gradient (2.5%) up to 4000 from SL GA, what does it calculate?
Does FSA calculates a max weight, so that at given conditions, when airplane reaches 4000 feet, reducing gradient as ascending finally hits down to to 2.5% ?
Have a look at
about the computation strategies of the flysmart, I really find it interesting.