Directional Indicating System (Turbine Powered Subsonic Aircraft)
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Product Code: ARP416
Revision Number: A
Date Published: 2001-10-01
Date Reaffirmed: February 2008
Issuing Committee:
A-4 Aircraft Instruments Committee
Scope
To recommend the essential minimum safe performance requirements for gyroscopically stabilized Directional Indicating System, primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This recommended practice covers the requirements for gyroscopically stabilized Directional Indicating Systems, which will operate as a 1 degree/hour latitude corrected, free directional gyro or as a slaved gyro, magnetic compass with 1/2 degree accuracy.
Product Status: In Stock
File Size:
174K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| ARP416A |
2001-10-01 |
Reaffirmed |
| ARP416 |
1963-02-28 |
Reaffirmed |
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