ARP416A Directional Indicating System (Turbine Powered Subsonic Aircraft)

Reaffirmed

02/16/2008

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/ARP416A
Pages
1
Citation
SAE International Recommended Practice, Directional Indicating System (Turbine Powered Subsonic Aircraft), SAE Standard ARP416A, Reaffirmed February 2008, Revised October 2001, Issued February 1963, https://doi.org/10.4271/ARP416A.
Additional Details
Publisher
Published
Feb 16, 2008
Product Code
ARP416A
Content Type
Recommended Practice
Status
Reaffirmed
Language
English

Revisions