Superseded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) | --- |
No products.
Previous versions
16/02/2008
Superseded
, Reaffirmed
Historical