Mo Heekan
25th May 2002, 20:06
Hi all knowing techies,
I'm pondering and need help please; under N1 thrust control, our in flt perf book says that there is a reductive weight penalty to be applied if in N1 mode. These weights range from 28-45 Tons depending on normal g/a weight.
I'm stuck on;
a. These weight decrements seem massive. Does anyone know why they are so huge?
b. If they are to be applied to 1 engine ops (not your day), what do you do to your single engine g/a weight that you've calculated (i.e. with the 2.5 % g/a requirement we have on 1 engine)?
c. If I read it correct, as an example; there is a 32 Ton penalty if landing around your normal configuration weight. This would mean you need to run out of fuel before you could be down to the weight to g/a. It doesn't sound right.
What am i doing wrong? I'd appreciate any feedback please
Thanks
I'm pondering and need help please; under N1 thrust control, our in flt perf book says that there is a reductive weight penalty to be applied if in N1 mode. These weights range from 28-45 Tons depending on normal g/a weight.
I'm stuck on;
a. These weight decrements seem massive. Does anyone know why they are so huge?
b. If they are to be applied to 1 engine ops (not your day), what do you do to your single engine g/a weight that you've calculated (i.e. with the 2.5 % g/a requirement we have on 1 engine)?
c. If I read it correct, as an example; there is a 32 Ton penalty if landing around your normal configuration weight. This would mean you need to run out of fuel before you could be down to the weight to g/a. It doesn't sound right.
What am i doing wrong? I'd appreciate any feedback please
Thanks