A newbies impression of the 109 and spit

[NZtyphoon]

Originally Posted by 41Sqn_Stormcrow

My guess is that they do not address thrust increase otherwise they would have written it I think.

Reading more closely the phrase I come to think that they perhaps wanted to say "as long as g level remained low during maximum lift pulls" meaning that the absolut lift was low while providing maximum lift for that given speed.

The report includes a series of graphs recording the information; incidentally

Reference 1. REQUIREMENTS FOR SATISFACTORY FLYING QUALITIES
OF AIRPLANES can be found here