Consider an airplane with a weight of 700,000N with a total wing surface of 150 square meters. At a certain speed, the difference in the air pressure below and above the wing is 5% of atmospheric pressure (105N). Calculate the lift on the airplane. Please express your answer in long hand (No scientific notation) and no need to worry about significant figures as this is more of a back of the envelope type problem. It is assumed your answer will be in Newtons.