$1.$ A $\backslash (50,000\backslash$mathrm$\{$~N$\}\backslash )$ heavy Jet aircraft is cruising at $\backslash (200\backslash$mathrm$\{$~m$\}/\backslash$mathrm$\{$s$\}\backslash ),$ with respect to ground, at its design lift coefficient $0\mathrm{.}627$ at minimum required thrust conditions. If for the wing the aspect ratio is $8\mathrm{.}2,$ and span efficiency factor is $0\mathrm{.}83,$ what is the amount of thrust produced by the engines?

$($A$)4252\mathrm{.}1$ N

$($B$)2932\mathrm{.}4$ N

$($C$)2527\mathrm{.}9$ N

$($D$)3577\mathrm{.}3$ N