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SAE ARP 416A:2008-02-16
New product
SAE ARP 416A:2008-02-16
Directional Indicating System (Turbine Powered Subsonic Aircraft)More info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2008-02-16 |
| ICS | 49.090 : On-board equipment and instruments
|
| Number of pages | 15 |
| Replace | SAE ARP 416:1991-05-01 |
| Set | AEROPAKS10U-10 |
| Year | 2008 |
| Document history | SAE ARP 416:1991-05-01 |
| Country | USA |
| Keyword | SAE 416;SAE ARP416A;SAE ARP416A;SAE ARP 416 |