SAE ARP 1070E : 2019
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
Available format(s)
Hardcopy , PDF
Superseded date
20-05-2024
Superseded by
Language(s)
English
Published date
22-07-2019
Publisher
This document outlines the development process and makes recommendations for total antiskid/aircraft systems compatibility.
Committee |
A-5A
|
DocumentType |
Revision
|
Pages |
60
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
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SAE AMSQQP416E | Plating, Cadmium (Electrodeposited) |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
IEEE 12207.1-1997 | IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) - Software Life Cycle Processes - Life Cycle Data |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE ARP4955A | Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires |
SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
NAS1638:2011 | CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS |
SAE AIR1739B | Information on Antiskid Systems |
ARINC 629 : 90 SUPP 5 | MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
ASME Y14.24 : 2012 | TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
SAE AS22759C | Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy |
MIL-PRF-81322 Revision G:2005 | GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395 |
MIL-STD-1568 Revision D:2015 | Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems |
MIL-HDBK-5400 Base Document:1995 | Electronic Equipment, Airborne General Guidelines for |
MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
MIL-STD-882 Revision E:2012 | System Safety |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
IEEE 12207.0-1996 | IEEE/EIA Standard - Industry Implementation of International Standard ISO/IEC 12207:1995 (ISO/IEC 12207) Standard for Information Technology -- Software Life Cycle Processes |
RTCA DO 248 : C2011 | SUPPORTING INFORMATION FOR DO-178C AND DO-278A |
SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
SAE ARP598D | Aerospace Microscopic Sizing and Counting of Particulate Contamination for Fluid Power Systems |
MIL-DTL-26500 Revision G:2011 | CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING OR HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
FAA AC 25-7 : 2012 | FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES |
SAE ARP490F | Electrohydraulic Servovalves |
MIL-P-8564 Revision D:1970 | PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
IEEE 12207.2-1997 | IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) Standard for Information Technology- Software Life Cycle Processes - Implementation considerations |
MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
FAA AC 121.195-1 : 0 | OPERATIONAL LANDING DISTANCES FOR WET RUNWAYS; TRANSPORT CATEGORY AIRPLANES |
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