FAA-H-8083-25C · Source PDF page 159

Flight Controls

Antiservo Tabs · PHAK page 6-11

Original FAA PHAK page 6-11
Faithful view of source page 6-11. Select it to enlarge.

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helps to move the entire flight control surface in the direction Nose-down trim that the pilot wishes it to go. A servo tab is a dynamic device that deploys to decrease the pilots work load and de-stabilize Elevator the aircraft. Servo tabs are sometimes referred to as flight tabs Trim tab and are used primarily on large aircraft. They aid the pilot in moving the control surface and in holding it in the desired position. Only the servo tab moves in response to movement of the pilot’s flight control, and the force of the airflow on the servo tab then moves the primary control surface. Tab up—elevator down Antiservo Tabs Nose-up trim Antiservo tabs work in the same manner as balance tabs except, instead of moving in the opposite direction, they move Elevator in the same direction as the trailing edge of the stabilator. In addition to decreasing the sensitivity of the stabilator, an Trim tab antiservo tab also functions as a trim device to relieve control pressure and maintain the stabilator in the desired position. The fixed end of the linkage is on the opposite side of the surface from the horn on the tab; when the trailing edge of the stabilator moves up, the linkage forces the trailing edge of the tab up. When the stabilator moves down, the tab also moves Tab up—elevator up down. Conversely, trim tabs on elevators move opposite of Figure 6-20. The movement of the elevator is opposite to the the control surface. [Figure 6-21] dFiriegcutiroen 5 o-1f 6m.o Tvheme menot voefm theen te loefv tahteo re ltervimat otar bis. opposite to the direction of movement of the elevator trim tab. Ground Adjustable Tabs control pressures that may exist for that flight condition. As Many small aircraft have a nonmovable metal trim tab on the power, pitch attitude, or configuration changes, retrimming rudder. This tab is bent in one direction or the other while on is necessary to relieve the control pressures for the new the ground to apply a trim force to the rudder. The correct flight condition. displacement is determined by trial and error. Usually, small Balance Tabs The control forces may be excessively high in some aircraft, and, in order to decrease them, the manufacturer may use balance tabs. They look like trim tabs and are hinged in approximately the same places as trim tabs. The essential difference between the two is that the balancing tab is coupled to the control surface rod so that when the primary control surface is moved in any direction, the tab automatically moves in the opposite direction. The airflow striking the tab Stabilator counterbalances some of the air pressure against the primary control surface and enables the pilot to move the control more Pivot point easily and hold the control surface in position. If the linkage between the balance tab and the fixed surface is adjustable from the flight deck, the tab acts as a Antiservo tab combination trim and balance tab that can be adjusted to a desired deflection. Servo Tabs Figure 6-21. An antiservo tab attempts to streamline the control Servo tabs are very similar in operation and appearance to the surface and is used to make the stabilator less sensitive by opposing trim tabs previously discussed. A servo tab is a small portion the force exerted by the pilot. of a flight control surface that deploys in such a way that it 6-11