What is the torque produced on the airplane in the image below if the tail force is 55 N and 10 meters from the CG (tarm) and the lift produced by the main wing is 848 N and 2 meters from the CG (warm)? Refer to the image for the direction the force acts in. Sarm Warm Assuming the airplane is in straight and level flight, find the lift | produced if tarm is 8 m and warm is 1 m. Assume the system is in equilibrium (sum of forces and torques equal O) and the weight of the aircraft is 7000 N. (Enter just the numerical value you calculate without units) fam and tail force Warm