Terminology and Definitions for Aerospace Fluid Power, Actuation and Control Technologies
- Aerospace Standard
- ARP4386D
- Revised
Scope
Rationale
Recommended Content
Aerospace Standard | General Requirements for Hydraulic System Reservoirs |
Aerospace Standard | Testing of Airplane Installed Environmental Control Systems (ECS) |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Table 1 | Standard Atmosphere Properties | |
Table 2 | Notation for body axes | |
Unnamed Dataset 5 | ||
Unnamed Dataset 6 |
Issuing Committee
A-6 Aerospace Actuation, Control and Fluid Power Systems
The committee A-6 is a service organization to promote the advancement of actuation, control and fluid power in sciences, technologies, engineering practices, and standards associated with the design, manufacture, operation, and support of aerospace vehicles. The Committee A-6 is comprised of a parent committee, subcommittees, panels, and a Steering Council. The Steering Council may from time to time create or dissolve subcommittees and panels and amend their responsibilities. The current panels include A-6A1, A-6A2, A-6A3, A-6B1, A-6B2, A-6B3, A-6C1, A-6C2, A-6C3, A-6C4 and A-6C5. The Committee A-6 is the approval body for all documents developed by its subcommittees and panels.
Reference
Number | Title |
---|---|
AS1290 | GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
ISO 8625-1 | This document is not part of the subscrption. |
ISO 8625-2 | This document is not part of the subscrption. |
ISO 8625-3 | This document is not part of the subscrption. |
ISO6771 | This document is not part of the subscrption. |