He asked at what N1 the PUBLISHED thrust is.
(the one given in the FAA certificate and other publications)
There is only ONE EXACT answer to that question = 111,8 N1
That is just not correct. It is not possible to give an exact answer until the variables have been defined.
May I suggest that you read the post by barit1, as I get the impression that there are a few things here, that you don't quite understand.