For context on this, the description includes the flaps and airspeed. Increasing flaps increases lift. The Boeing 777 has flap settings of 1, 5, 15, 20 (the 5 - 20 settings are used for takeoff depending on performance needs) and then 25 and 30, which are landing settings (other flap settings are sometimes used for landing but not pertinent for this). Flaps have maximum airspeed limitations - increasing flaps reduces the maximum speed limit, and this limit is displayed on the airspeed indicator. Below is an example, with the red indication showing the maximum speed for the aircraft limited due to flap position. Could you explain the Aircraft Physical Components for this case