Directional Indicating System (Turbine Powered Subsonic Aircraft)(STABILIZED Apr 2020)
This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1°/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2° accuracy.
This Technical Report contains no changes from the previous revision, other than the addition of a Stabilization Notice Page. This document has been determined to contain stable technical information which is not dynamic in nature.
Combustion and combustion processes
Connectors and terminals
Also known as: SAE ARP 416
Subscribers can view annotate, and download all of SAE's content.
Learn More »