IMPULSE TESTING OF AEROSPACE HYDRAULIC ACTUATORS, VALVES, PRESSURE CONTAINERS, AND SIMILAR FLUID SYSTEM COMPONENTS
- Aerospace Standard
- ARP1383A
- Revised
Scope
Recommended Content
| Aerospace Standard | Specification Guide for Power Drive Units (PDUs) |
| Aerospace Standard | Crashworthy Landing Gear Design |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE B1 | Determination of Fatigue Test Cycles Typical Aileron Actuator, 62 000 Flights - 1 Life (References to procedure steps in text are indicated by <x>) | |
| TABLE B2 | Aircraft Manufacturers Data for the Example Chosen | |
| TABLE B3 | G-A-G Cycle for the Example Chosen | |
| TABLE B4 | Stress/Pressure Ratio for the Example Chosen | |
| TABLE B7 | n/N, Σ n/N for Example Chosen |
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 |
|---|---|
| AIR1228 | Standard Impulse Machine Equipment and Operation |
| ARP603 | Impulse Testing of Hydraulic Hose Tubing and Fittings Assemblies |