Basic control and operation information describe how the airplane components are controlled and how they operate, including any special procedures, and limitations that apply.

A 406 MHz digital signal identifies the emergency locator transmitter and its location.

Any technical data published in the ATA No. 100 format will meet the requirements of this specification although it is expected that the Paragraph 19 format will be used where no ATA-100 requirement is foreseen.

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.