Directional Indicating System (Turbine Powered Subsonic Aircraft)(STABILIZED Apr 2020)
ARP416B
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.
Rationale:
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.
Related Topics:
Electronic equipment
Performance tests
Commercial aircraft
Freighter aircraft
Ignition systems
Combustion and combustion processes
Pressure
Connectors and terminals
Wheel wells
Also known as: SAE ARP 416
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