This document recommends minimum requirements for antiskid brake control to provide total aircraft systems compatibility. Design and operational goals, general theory, and functions, which should be considered by the aircraft brake system engineer to attain the most effective skid control performance, are covered in detail. Methods of determining and evaluating antiskid system performance are discussed. While this document specifically addresses antiskid systems which are a part of a hydraulically actuated brake system, the recommended practices are equally applicable to brakes actuated by other means, such as electrically actuated brakes.
SAE ARP1070C-2013 history
2019SAE ARP1070E-2019 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2014SAE ARP1070D-2014 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2013SAE ARP1070C-2013 Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
2008SAE ARP1070C-2008 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2006SAE ARP1070B-2006 Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
1991SAE ARP1070B-1991 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
1982SAE ARP1070A-1982 DESIGN OF SKID CONTROL & ASSOCIATED AIRCRAFT EQUIPMENT FOR TOTAL SYSTEM COMPATIBILITY
1969SAE ARP1070-1969 DESIGN OF AIRCRAFT SKID CONTROL SYSTEMS FOR COMPATIBILITY WITH AIRPLANE EQUIPMENT