AEROSPACE FLUID POWER - CONTAMINATION SENSITIVITY - CONSIDERATIONS FOR ESTABLISHING TEST PROCEDURES FOR FLIGHT CONTROL ACTUATORS
SAE International
1. SCOPE
2. APPLICABLE DOCUMENTS
3. BACKGROUND
4. TEST PROCEDURES
5. NOTES
Defines the design conditions under which tests should be conducted to demonstrate satisfactory performance of a flight critical servo-actuator under the maximum allowable particulate contamination in the associated airplane hydraulic system.
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
| Committee | A-6B1 |
