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SAE ARP416 Rev B

Current Revision

Directional Indicating System (Turbine Powered Subsonic Aircraft)

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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.

SDO SAE: SAE International
Document Number ARP416
Publication Date April 14, 2020
Language en - English
Page Count 16
Revision Level B
Supercedes
Committee
Publish Date Document Id Type View
April 14, 2020 ARP416B Revision
Oct. 1, 2001 ARP416A Revision
Feb. 28, 1963 ARP416 Revision