As follows FGD
Cockpit/Cabin check - Trim Tabs SET TO "0" UNITS - Caution - The elevator trim system must not be forced past the limits which are indicated on the elevator trim indicator scale, either manually, electrically, or by action of the autopilot.
Left Wing & Nacelle - Aileron and Tab - CHECK
Right Wing & Nacelle - Aileron and Bendable Tab - CHECK
Tail - Rudder, Rudder Tab, Stinger and Static Wicks (4) CHECK
Tail - Elevator, Tab, and Static Wicks (3 each side) CHECK, Verify Tabs are in "0" (Neutral) Position. NOTE - The elevator trim tab "0" (neutral) position is determined by observing that the trailing edge of the elevator trim tab aligns with the trailing edge of the elevator when the elevator is resting against the down stops.