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CURRENT
2017-10-11
Standard
AS6089
This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that this verification document only verifies the specific requirements from AS5653 and does not verify all of the requirements invoked by documents that are referenced by AS5653. The procuring authority may require further testing to verify the requirements not explicitly defined in AS5653 and in this verification document.
CURRENT
2017-09-13
Standard
AS5659/4
This Aerospace Standard (AS) 5659/4 Physical Layer Specification provides guidance for the physical layer of optical networks which use Wavelength Division Multiplexing (WDM), within the AS5659 WDM LAN specification document family. The physical layer consists of the optical interconnections between the functional components of the network. Performance requirements for general interconnections are described. For guidance, standards are identified, corresponding to each of several environments, which describe physical layer design, installation, maintenance, and training.
CURRENT
2017-08-15
Standard
AS4115A
This test plan consists of two major sections for testing of MIL-STD-1553B data bus systems: Bus Network and System Integration Tests.
CURRENT
2017-08-14
Standard
AS4116A
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
CURRENT
2017-08-14
Standard
AS4114A
This test plan consists of two major sections for the production testing of bus controllers: Electrical tests and Protocol tests.
CURRENT
2017-08-10
Standard
AS4111A
This SAE Aerospace Standard (AS) contains a sample test plan for AS15531 or MIL-STD-1553B Remote Terminals (RT) that may serve several different purposes. This document is intended to be contractually binding when specifically called out in a specification, Statement of Work (SOW), or when required by a Data Item Description (DID). Any and all contractor changes, alterations, or testing deviations to this section shall be separately listed for easy review.
CURRENT
2017-08-10
Standard
AS4112A
This test plan is broken into two major sections for the production testing of remote terminals: Electrical and Protocol.
CURRENT
2017-08-10
Standard
AS4117A
This test plan defines the requirements of data bus components which comply with the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
2017-08-09
WIP Standard
AS42702
This document establishes techniques for verifying that a Mission Store Interface (MSI) complies with the interface requirements delineated in MIL-STD-1760 Revision E.
2017-08-01
WIP Standard
ARP7208
This ARP establishes guidelines for the use of IEEE-802.3 as a data bus network in military and aerospace vehicles. It encompasses the data cable and its connections for a system utilizing 10Base-T, 100Base-T, 1000BASE-T and 10GBASE-T over copper medium dependent interfaces (MDI). This document contains extensions/restrictions to “off-the-shelf” IEEE-802.3 standards, and assumes that the reader already has a working knowledge of IEEE-802.3.
CURRENT
2017-06-28
Standard
AS47642B
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
CURRENT
2017-06-28
Standard
AS47641A
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
CURRENT
2017-06-27
Standard
AIR6027A
The information presented in this AIR is intended to provide designers of armed unmanned systems with guidelines that may be applied to ensure safe integration and operation of weapons on unmanned platforms. The guidelines have been developed from experiences gained in the design and operation of weapons on manned aircraft that have been accepted by relevant safety authorities in the USA and Europe and proven effective over many years. Whilst the guidelines have been developed from experience with aircraft operations, the concepts are considered equally applicable to non-aircraft systems, such as those used on the surface or undersea environments. This document does not attempt to define or describe a comprehensive safety program for unmanned systems. System Safety is a system characteristic and a non-functional requirement. It has to be addressed at each level of system design, system integration and during each phase of system operation.
CURRENT
2017-06-27
Standard
AS4270A
This document establishes techniques for validating that a mission store complies with the interface requirements delineated in MIL-STD-1760.
CURRENT
2017-06-27
Standard
AS4764A
This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760.
2017-05-23
WIP Standard
AS5680B
This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: - Physical envelope of the fuze well at the interface with the fuze. - Load bearing surfaces of the fuze well. - Physical envelope of the fuze and its connector. - Mechanical features (e.g., clocking feature). - Connector type, size, location and orientation. - Retaining ring and its mechanical features (e.g., thread, tool interface). - Physical envelope of the retaining ring at the interface with the fuze. - Physical space available for installation tools. - Torque that the installation tool shall be capable of providing. This standard does not address: - Materials used or their properties. - Protective finish. - Physical environment of the weapon. - Explosive interface or features (e.g., insensitive munitions (IM) mitigation). - Charging tube. - Torque on the retaining ring or loads on the load bearing surfaces.
CURRENT
2017-05-18
Standard
AS20708/81B
No Scope Available
2017-04-13
WIP Standard
AIR5875A
This SAE Aerospace Information Report (AIR) outlines comprehensive aircraft flight control system fault isolation methodology that has proven to be effective. The methodology presented in this Information Report has been used in several successful fault isolation efforts on military aircraft.
2017-04-11
WIP Standard
ARP6539
This SAE Aerospace Recommended Practice (ARP) provides a process for the verification and validation of monitors used in flight control, utility control, and related components and systems. It is intended to serve as a system specific companion document to SAE ARP 4754.
2017-04-11
WIP Standard
AIR6920
This AIR is for use by OEM's and Suppliers developing process gate checklists for highly integrated, complex flight control and vehicle management systems to support the life cycle development validation and verification activities prescribed by ARP4754.
2017-03-22
WIP Standard
ARP6389
This ARP provides guidelines for improving the Failure Mode and Effect Analysis process, including alternative or additional methods, for flight critical actuation equipment electronics and software.
CURRENT
2017-02-21
Standard
AS4074B
This standard specifies the characteristics of the SAE Linear Token Passing Bus (LTPB) Interface Unit. The LTPB provides a high reliability, high bandwidth, low latency serial interconnection network suitable for utilization in real time military and commercial applications. Multiple redundant data paths can be implemented to enhance reliability and survivability in those applications which require these attributes. The token passing and data exchange protocols are optimized to provide low latency and fast failure detection and correction. Physical configurations with bus lengths up to 1000 m can be accommodated. This specification defines the following: General Description (3.1): An overview of the LTPB protocol. Physical Media Interface (3.2): This portion of the standard defines the physical interface to both optical and electrical bus media.
2017-01-25
WIP Standard
ARP6283/1
Provide user information on best practice methods and processes for the in-service inspection, evaluation and cleaning of expanded beam fiber optic interconnect components, test equipment, and test leads based on the information provided in AIR6031. This document provides the user with a decision making tool to be able to determine if the fiber optic components are acceptable for operation with expanded beam fiber optic termini.
2017-01-19
WIP Standard
ARP6283/2
Provide user information on best practice methods and processes for the in-service inspection, evaluation and cleaning of expanded beam fiber optic interconnect components, test equipment, and test leads based on the information provided in AIR6031. This document provides the user with a decision making tool to be able to determine if the fiber optic components are acceptable for operation with multi-fiber fiber optic termini.
CURRENT
2016-11-18
Standard
AIR6234
This Handbook is intended to provide useful information on the application of AS5716A. It is for use by System Program Offices, aircraft prime contractors, avionics and store system designers, system integrators and equipment manufacturers and users. This Handbook was prepared to provide users of the standard of the rationale and principles considered during the development of the standard. It is anticipated that the handbook will serve to assist developers in introducing new technology to achieve compliance with the standard and the underlying principles of the standard. It is intended that the Handbook be used alongside the standard, as it does not contain significant extracts of the standard.
CURRENT
2016-10-21
Standard
AIR5683A
MIL-STD-1553 establishes requirements for digital command/response time division multiplexing (TDM) techniques on military vehicles, especially aircraft. The existing MIL-STD-1553 network operates at a bit rate of 1 Mbps and is limited by the protocol to a maximum data payload capacity of approximately 700 kilobits per second. The limited capacity of MIL-STD-1553 buses coupled with emerging data rich applications for avionics platforms plus the expense involved with changing or adding wires to thousands of aircraft in the fleet has driven the need for expanding the data carrying capacity of the existing MIL-STD-1553 infrastructure.
CURRENT
2016-10-21
Standard
AIR4886A
The purpose of this document is to establish the requirements for Real-Time Communication Protocols (RTCP). Systems for real-time applications are characterized by the presence of hard deadlines where failure to meet a deadline must be considered a system fault. These requirements have been driven predominantly, but not exclusively, by aerospace type military platforms and commercial aircraft, but are generally applicable to any distributed, real-time, control systems. These requirements are primarily targeted for the Transport and Network Layers of peer to peer protocols, as referenced in the Open System Interconnect Reference Model (2.2.1 and 2.2.2), developed by the International Standards Organization (ISO). These requirements are intended to complement SAE AS4074 (2.1.1) and AS4075 (2.1.2), and future SAE communications standards.
CURRENT
2016-09-16
Standard
AIR6114
This document was prepared by the SAE AS-1B1 IMM Task Group to explain and document background information and design decisions made during the development of AS5726. This handbook is published separately to preserve information that is not required or provided in the AS5726 but may be important to system designers to ensure interoperability between the Micro Munition Host and Micro Munition. As a handbook, it cannot be invoked as a requirement in a contract. The structure and numbering of this document mirrors that of AS5726 for the convenience of readers. Headings such as “Requirements” in this handbook should not be interpreted as invoking requirements.
CURRENT
2016-07-18
Standard
AIR4094A
This SAE Aerospace Information Report (AIR) supplies information on the flight control systems incorporated on various current and historic fixed wing, rotary wing, and tilt rotor aircraft. A brief description of the aircraft is followed by a description of the flight control system, some specific components, drawings of the internal arrangement, block diagrams, and schematics. System operation redundancy management is also presented.
CURRENT
2016-06-22
Standard
AS19692B
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance, and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps used in military aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjunction with this AS. The hydraulic pumps defined by this AS are generally for use in aircraft hydraulic systems conforming to and as defined in AS5440 and MIL-H-8891, as applicable.
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