Resulting aircraft speed:
"\\vec{v} = \\vec{u} + \\vec{w},"
where "\\vec{u}" is the own aircraft airspeed, "\\vec{w}" is the wind speed.
Since wind is blowing in 45 degrees angle,
"w_y = w\\cos45\\degree = w_x = w\\sin45\\degree."
Projecting the vectors on axes in absolute values:
(here "v_x=0" because we know the aircraft in result is heading due north).
From the 2nd equation,
"\\sin\\alpha = \\frac{w}{u}\\sin45\\degree; \\\\\n\\alpha = \\arcsin(\\frac{w}{u}\\sin45\\degree) = \\arcsin(\\frac{50\\frac{\\text{km}}{\\text{h}}}{250\\frac{\\text{km}}{\\text{h}}}\\frac{\\sqrt2}{2}) \\approx 8.13\\degree."
The above angle is the direction of pointing the nose of the aircraft, west of north.
From the 1st equation,
"v = v_y = u\\sqrt{1-\\sin^2\\alpha} - w\\cos45\\degree = u\\sqrt{1-(\\frac{w}{u}\\sin45\\degree)^2} - w\\cos45\\degree = \\\\ = 250\\frac{\\text{km}}{\\text{h}}\\sqrt{1-(\\frac{50\\frac{\\text{km}}{\\text{h}}}{250\\frac{\\text{km}}{\\text{h}}}\\frac{\\sqrt2}{2})^2} - 50\\frac{\\text{km}}{\\text{h}}\\frac{\\sqrt2}{2} \\approx 212.13 \\frac{\\text{km}}{\\text{h}}."
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