Superseded , Reaffirmed Standard
Historical

SAE ARP 416A:2008-02-16

Directional Indicating System (Turbine Powered Subsonic Aircraft)

Summary

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.

Notes

Approuvée 2008-02-16, 2008-02-00.

Technical characteristics

Publisher SAE International
Publication Date 02/16/2008
Confirmation Date 02/16/2008
Page Count 15
Themes Aerospace
EAN ---
ISBN ---
Weight (in grams) ---
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