It sounds to me like we have a situation where…..for the same aircraft type(at least for certain types), some companies do a calculation(or whatever it may be called) for a target pitch attitude on rotation while others do not.
For those that so, is this a recommendation in the manufacturers manuals or a company procedure.
I am used to the target of 15 degrees and adjust as required.
Last edited by punkalouver; 8th March 2022 at 19:47.