SAE ARP1070E-2019 PDF

Scope: This document outlines the development process and makes recommendations for total antiskid/aircraft systems compatibility. These recommendations encompass all aircraft systems that may affect antiskid brake control and performance. It focuses on recommended practices specific to antiskid and its integration with the aircraft@ as opposed to more generic practices recommended for all aircraft systems and components. It defers to the documents listed in Section 2 for generic aerospace best practices and requirements. The documents listed below are the major drivers in antiskid/aircraft integration: 1. ARP4754 2. ARP4761 3. RTCA DO-178 4. RTCA DO-254 5. RTCA DO-160 6. ARP490 7. ARP1383 8. ARP1598 In addition@ it covers 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@ as well as methods of determining and evaluating antiskid system performance. For definitions of terms used herein@ see Section 7. Purpose To recommend minimum antiskid brake control design practices@ laboratory and aircraft test requirements to provide total aircraft system compatibility.

SAE ARP1070E-2019 history

2019 SAE ARP1070E-2019 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2014 SAE ARP1070D-2014 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2013 SAE ARP1070C-2013 Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
2008 SAE ARP1070C-2008 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
2006 SAE ARP1070B-2006 Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
1991 SAE ARP1070B-1991 Design and Testing of Antiskid Brake Control Systems For Total Aircraft Compatibility
1982 SAE ARP1070A-1982 DESIGN OF SKID CONTROL & ASSOCIATED AIRCRAFT EQUIPMENT FOR TOTAL SYSTEM COMPATIBILITY
1969 SAE ARP1070-1969 DESIGN OF AIRCRAFT SKID CONTROL SYSTEMS FOR COMPATIBILITY WITH AIRPLANE EQUIPMENT