SAE AS397 PDF
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DIRECTION INDICATOR, NON-MAGNETIC, STABILIZED TYPE (Directional Gyro)
Description
This specification covers two basic types as follows:
Type I
–
Air Operated.
Type II
–
Electrically Operated.
Revision History
Related Info
AS397B
2012-08-22
Latest
Stabilized
AS397A
2008-02-16
Historical
Reaffirmed
AS397
1947-02-01
Historical
Issued
DOI: https://doi.org/10.4271/AS397
Issuing Committee:
A-4 Aircraft Instruments Committee
Publisher:
SAE International
Pages: 4
Related Topics:
Aircraft instruments
Aircraft
Roll
Pitch
Pressure
Yaw
Humidity
Identification numbers
Vehicle acceleration
Performance tests
Also known as: SAE AS 397
History
| AS397B | 2012-08-22 | Latest | Stabilized |
| AS397A | 2008-02-16 | Historical | Reaffirmed |
| AS397 | 1947-02-01 | Historical | Issued |
| ISSUING COMMITTEE | A-4 Aircraft Instruments Committee |
|---|---|
| DATE | 1947-02-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 4 |
| PUBLISHER | SAE International |
| REVISED | ISSUED |
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