An aeroplane of mass 5000 kg is flying at an altitude of 3 km. if the area of the wings is 50m^2 and pressure at the lower surface of wings is 0.6*10^5 pa, the pressure on the upper surface of wings is (in pascal) g=10m/s^2

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An aeroplane of mass 5000 kg is flying at an altitude of 3 km. if the area of the wings is 50m^2 and pressure at the lower surface of wings is 0.6*10^5 pa, the pressure on the upper surface of wings is (in pascal) g=10m/s^2

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At vero eos et accusamus et iusto odio dignissimos ducimus qui blanditiis praesentium voluptatum deleniti atque corrupti quos dolores et quas molestias excepturi sint occaecati cupiditate non provident, similique sunt in culpa qui officia deserunt mollitia animi, id est laborum et dolorum fuga. Et harum quidem rerum facilis est et expedita distinctio. Nam libero tempore, cum soluta nobis est eligendi optio cumque nihil impedit quo minus id quod maxime placeat facere possimus, omnis voluptas assumenda est, omnis dolor repellendus. Itaque earum rerum hic tenetur a sapiente delectus, ut aut reiciendis voluptatibus maiores alias consequatur aut perferendis doloribus asperiores repellat.

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Since, the plane is perfectly balanced and flying in air. The balance on lower end must be equal to pressure on upper surface. Think, if pressure on upper surface is greater than lower surface then the plane will fall off!!
yes, just factor in the mass/weight of the plane \[P_{up} \times A = P_{down} \times A + mg\]

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