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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
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Superseded date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Superseded by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
Important note : All end users must be registered with an Account prior to user licenses being assigned.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Superseded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 |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| SAE AMS QQ P 416 : 2016 | 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 ARP 4955 A: 2012(R2018) | RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC AND DYNAMIC CHARACTERISTIC PROPERTIES OF AIRCRAFT TIRES |
| SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
| NAS1638:2011 | CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS |
| SAE AIR 1739 : 2016 | 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 ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| SAE AS 22759 : 2014 | 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 ARP 598 : 2016 | 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 ARP 490 : 2008 | 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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