No one is allowed to access the airplane during its functional test.

The lighting subsystems in the areas in which the passengers are seated and in buffet/galley, lavatories, lounges and coat rooms. Includes items such as direct and indirect illumination, passenger call system, lighted signs, etc.

That portion of the system provides the major support for the aircraft while on the ground, including items such as shock struts, bogie axles, drag struts, doors, linkages, attach bolts, etc.

The units and components which give audible or visual warning of conditions in unrelated systems.

The portion of the system which is used to eliminate or prevent the formation of ice on propellers.

For turbine type power plants using air as the anti-icing medium, engine anti-icing is contained under Air System.

The units and components which provide a means of preventing or disposing of formation of ice and rain on various parts of the aircraft.

That portion of the systems includes items such as control handle, cables, jackscrews, motors, warning systems, linkages, control surfaces, position indicators, etc.

That portion of the systems which controls the position and movement of the elevator/elevon and tabs.

That portion of the systems which controls the position and movement of the ailerons and aileron tabs. Includes items such as the control wheels, cables, boosters, linkages, control surfaces, indicators, etc., as applicable.

The section containing "Emergency Procedures" shall have a red plasticized tab divider.