The adjustment test description shall provide instructions for accomplishment of a test or check to assure the integrity as an operational component of a system, subsystem or unit assembly.

The resistance of the fuel temperature bulb changes with fuel temperature.

Divide the crosswind component by the aircraft speed to get the correction.

If it is necessary to decrease the cable tension more, use the turnbuckle.

Make sure that the servicing cart does not hit the aircraft.

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.