If the airplane has a built-in auxiliary power unit, describe it and explain how it fits in with the electrical system.

Though techniques such as shading, crosshatching, screening or similar means are recommended, the use of color is permissible.

STE was developed to help the readers of English-language documentation understand what they read, particularly when these readers are non-native English speakers.

For ease of reading and cross reference, illustrations, figures and tables should be presented in a vertical layout, if practical.

The main text of each section shall be preceded by a Table of Contents, listing the paragraph heads in numerical page order.

The manufacturer＇s masthead, publication title, airplane model, and issue or revision date must appear on all pages of loose-leaf document.

Recommended fuel conservation information shall be integrated into this section to show the pilot how to minimize fuel usage during operation of the airplane.

Close inspection in cable critical fatigue areas can be performed by rubbing a rag along the cable.

Existing analyses were reviewed to identify components and areas that may have exhibited lower margins of safety.

Do not place thermocouple wires adjacent to or crossing the power cord to prevent erroneous temperature readings caused by magnetic flux lines.

Only when both manufacturer and operator do their job can remain an entire fleet of airplanes continuously airworthy.