In this segment we'll watch the four forces work together in real time. As we add full power on the takeoff roll, thrust now exceeds drag and the airplane accelerates down the runway. Watch the airspeed build — and notice I'm holding right rudder to counter those left-turning tendencies we discussed: torque, P-factor, and the spiraling slipstream all pushing the nose left. As we rotate, we increase the angle of attack, the wing's coefficient of lift rises, and lift now exceeds weight, so we climb. Notice we stay in ground effect just for a moment — the airplane feels light because induced drag is reduced near the surface. Now in the climb, I'll demonstrate stability. I'll displace the nose with a brief pitch input and release — see how the airplane oscillates and then returns to its trimmed attitude? That's positive static and dynamic longitudinal stability doing its job. Finally, watch this gentle stall entry: I'll raise the nose, the airspeed bleeds off, the stall horn sounds as we approach the critical angle of attack, and at the break the nose drops. Recovery is simple and immediate — reduce the angle of attack by lowering the nose, add power, and we're flying again. Remember: it's always about angle of attack, not airspeed.