The normal pitch control law is basically the closed loop control of the load factor, and includes flight envelope protections.

If an engine fire detection system is available, describe, give principle of opreation, and explain how to use it.

Keep personnel away from the aircraft when the thrust reverser deploys.

Remove the rigging pins and equipment that prevent free movement of the control surfaces.

Do an inspection of the component interface and the adjacent area.

Carefully put the valve assembly in its position and install the spacers and the bolts.

Install the O-ring in the internal groove of the spherical bearing.

Temporarily attach the cable to the adjacent structure.

Do steps 1 thru 4 to make sure that no axial load is applied on the rod.

On pages requiring folding, make the fold in a manner that permits the page number to be visible.

Continuing Airworthiness Program lnspections usually consist of two pages: one text page and one illustration page.