TM 1-1520-238-23
Change 9
2-418.7/(2-418.8 blank)
2.114B. HORIZONTAL STABILATOR PIVOT BEARING REMOVAL/INSTALLATION (AVIM) - continued
utilized for this task. The bolt is inserted into the spacer sleeve and the notches on the spacer sleeve are
inserted into the slots of the inboard side of the bearing. Turning the bolt with a torque wrench per Aircraft
Mechanics tool kit (Item 376, App H) can then check the torque. Torque shall not exceed 180 inch-lbs.
f.
Position bracket with alignment marks and install Horizontal Stabilator Position Sensor
bracket. (Ref TM 1-1500-204-23).
g.
Install Horizontal Stabilator Sensor Clamp (paragraph 2.114A).
h.
Install Horizontal Stabilator (2) (paragraph 2.113).
i.
Inspect (QA).
