This SAE Aerospace Recommended Practice (ARP) describes 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. Additionally, this document also describes the recommended tests and the required acceptance criteria. ARP5941 has been reaffirmed to comply with the SAE five-year review policy.
Aerospace Fluid Power - Contamination Sensitivity - Considerations for Establishing Test Procedures for Flight Control Actuators
2020-10-09
Conference paper
English
British Library Conference Proceedings | 2000
|Aerospace – Test Methodology for Electrohydrostatic Actuators
SAE Technical Papers | 2010
Aerospace Fluid Power - Contamination Classification for Hydraulic Fluids
SAE Technical Papers | 2020
Collaborative robotics: Enhance maintenance procedures on primary flight control servo-actuators
BASE | 2021
|