SAE ARP416A PDF
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Directional Indicating System (Turbine Powered Subsonic Aircraft)
Description
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.
History
| ARP416B | 2020-04-14 | Latest | Stabilized |
| ARP416A | 2008-02-16 | Historical | Reaffirmed |
| ARP416 | 1991-05-01 | Historical | Reaffirmed |
| ISSUING COMMITTEE | A-4 Aircraft Instruments Committee |
|---|---|
| DATE | 2008-02-16 |
| DOI | |
| ISCURRENT | |
| PAGE | 15 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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