is there are something wrong in the 6dof (euler angles) block in Simulink ?

I'm dealing with Matlab (R2009b) the equation of motion for the airplane (Forces) F=m*a ( a in the inertial axis because newtons lows is applicable only in the inertial axis ) so... F/m=a(inertial) =a(body)+omega x v(body)

------------------------------- the problem here in the 6DOf block is that he considered F/m=a(body) and this is wrong ... my correction : since forces are given then a(inertial ) is known .. a(body) =a(inertial) -omega x v(body) ... not + as in the block .. am I right ?