Alright.
MiG-29A
300mph = 7,334kgf
500mph = 8,556kgf
700mph = 10,587kgf
800mph = 11,421kgf
900mph = 12,000kgf
950mph = 12,206kgf
980mph (max) = 12,298kgf
F-14B
400mph = 11,250kgf
600mph = 13,116kgf
800mph = 12,301kgf
850mph = 11,135kgf
F-16A
400mph = 11,709kgf
600mph = 13,640kgf
800mph = 14,880kgf
880mph = 15,098kgf
900mph = 14,722kgf
925mph = 14,371kgf
Tornado F.3
300mph = 7107kgf
500mph = 7413kgf
600mph = 7715kgf
700mph = 7939kgf
750mph = 8025kgf
800mph = 8064kgf
850mph = 8119kgf
900mph = 8044kgf
910mph = 8027kgf
FGR.2
400mph = 8762kgf
500mph = 9208kgf
600mph = 9755kgf
700mph = 10098kgf
800mph = 10188kgf
900mph = 10085kgf
907mph (max) = 10073kgf
MiG-23MLA
400mph = 11,448kgf
600mph = 13,397kgf
800mph = 15,263kgf
900mph = 15,789kgf
920mph (max)= 15,858kgf
F-4S
400mph = 7,606kgf
600mph = 8,839kgf
800mph = 10,005kgf
835mph (max)= 10,188kgf
So what have we found? Every single jet except the MiG-29, 23, and the F-4S (and possibly a few other exceptions) has a significant thrust drop that occurs as it approaches it’s top speed. The vast majority of these aircraft should have a thrust INCREASE around these speeds due to intake ramps and certainly should not decrease.