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CURRENT
2017-02-21
Standard
AS6023
The scope of this document is to: • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry. • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry.Identify the minimum performance requirements for active RFID tags to be used on or in close proximity to aircraft. • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry.Specify the test requirements specific to active RFID tags for aircraft use, in addition to RTCA DO-160 compliance requirements separately called out in this document. • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry.Identify existing standards applicable to active RFID Tag. • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry.Provide a certification standard for RFID tags which will use permanently-affixed installation on aircraft and aircraft parts. • Provide a requirements document for RFID Tag Manufacturers to produce active RFID tags for the Aerospace industry.Battery standards are separately captured and not included in this document.
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: a. General Description (3.1): An overview of the LTPB protocol. b. Physical Media Interface (3.2): This portion of the standard defines the physical interface to both optical and electrical bus media. c.
CURRENT
2017-02-08
Standard
TS200AR-44
No Scope available.
CURRENT
2017-02-07
Standard
AIR1812B
The purpose of this document is to provide qualitative information on life cycle cost (LCC) aspects of environmental control systems (ECS) design. This report contains background information on life cycle cost elements and key ECS cost factors. Elements of life cycle costs are defined from initial design phases through operational use. Information on how ECS designs affect overall aircraft cost and information on primary factors affecting ECS costs are discussed. Key steps or efforts for comparing ECS designs on the basis of LCC are outlined. Brief descriptions of two computer programs for estimating LCC of total aircraft programs and their use to estimate ECS LCC, are included.
CURRENT
2017-02-02
Standard
ARP577E
This SAE Aerospace Recommended Practice (ARP) specifies criteria for the design, development, standardization, and comprehension testing of placards containing pictures, drawings, symbols, and/or written instructions for locating and operating aircraft emergency equipment. This ARP also provides guidance in the selection and implementation of warning placards intended to instruct occupants inside, and rescue personnel outside, the aircraft.
2017-02-01
WIP Standard
AS6171/4A
This method standardizes inspection, test procedures and minimum training and certification requirements to detect Suspect/Counterfeit (SC) Electrical, Electronic, and Electromechanical (EEE) components or parts utilizing Delid/Decapsulation Physical Analysis. The methods described in this document are employed to either delid or remove the cover from a hermetically sealed package or to remove the encapsulation or coating of an EEE part, in order to examine the internal structure and to determine if the part is suspect counterfeit. Information obtained from this inspection and analysis may be used to: a. prevent inclusion of counterfeit parts in the assembly b. identify defective parts c. aid in disposition of parts that exhibit anomalies This test method should not be confused with Destructive Physical Analysis as defined in MIL-STD-1580. MIL-STD-1580 describes destructive physical analysis procedures for inspection and interpretation of quality issues.
2017-01-24
WIP Standard
AS6171/2A
This document describes the requirements of the following test methods for counterfeit detection of electronic components: a. Method A: General External Visual Inspection (EVI), Sample Selection, and Handling b. Method B: Detailed EVI c. Method C: Testing for Remarking and Resurfacing d. Method D: Surface Texture Analysis by SEM NOTE: The scope of this document was focused on leaded electronic components, microcircuits, multi-chip modules (MCMs), and hybrids. Other electronic components may require evaluations not specified in this procedure. Where applicable this document can be used as a guide but additional inspections or criteria would need to be developed and documented to thoroughly evaluate these additional part types.
2017-01-18
WIP Standard
AS5553C
This standard is for use by organizations that procure and/or integrate EEE parts and/or assemblies containing such items. The requirements of this standard are generic and intended to be applied/flowed down, as applicable, through the supply chain to all organizations that procure EEE parts and/or assemblies, regardless of type, size, and product provided. The mitigation of counterfeit EEE parts in this standard is risk-based and these mitigation steps will vary depending on the application, desired performance, and reliability of the equipment/hardware. The requirements of this document are intended to supplement the requirements of a higher level quality standard (e.g., AS/EN/JISQ9100, ISO-9001, ANSI/ASQC E4, ASME NQA-1, AS9120, AS9003, and ISO/TS 16949 or equivalent) and other quality management system documents.
CURRENT
2017-01-12
Standard
AS5609A
This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of Interface Control documents. The Common Interface Control Document Format Standard defines a common format for aircraft/store interface documents to foster increased interoperability. It is designed with the versatility to serve differing “ICD” philosophies and organizations. This aerospace standard defines the common technical data sections for the Common Interface Control Document Format down to the third header level for the majority of sub-sections. The Common Interface Control Document Format Aerospace Standard provides a structured document format in appendixes supported by example paragraphs, drawings, etc.
CURRENT
2017-01-04
Standard
ARP6239
This SAE Aerospace Recommended Practice (ARP) recommends the design and features of aircraft demonstration emergency equipment for use in passenger safety briefings.
2017-01-03
WIP Standard
AS6294/2
This standard documents and establishes common industry practices, and screening and qualification testing, of Plastic Encapsulated Microcircuits (PEMs) for use in military and avionics application environments.
2016-12-28
WIP Standard
AS8049D

This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in the applicable Federal Regulations 14 CFR 23, 25, 27, or 29.

Guidance for test procedures, measurements, equipment, and interpretation of results is also presented to promote uniform techniques and to achieve acceptable data.

While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant.

CURRENT
2016-12-20
Standard
AS6522
The UCS technical governance comprises a set of policies, processes, and standard definitions to establish consistency and quality in the development of architecture artifacts and documents. It provides guidance for the use of adopted industry standards and modeling conventions in the use of Unified Modeling Language (UML) and Service Oriented Architecture Modeling Language (SoaML), including where the UCS Architecture deviates from normal UML conventions. This document identifies the defining policies, guidelines, and standards of technical governance in the following subjects: - Industry standards adopted by the AS-4UCS Technical Committee: These are the industry standards and specifications adopted by AS-4UCS in the generation and documentation of the architecture. - UCS Architecture Development: UCS specific policies on the development of the UCS Architecture. The AS-4UCS Technical Committee governance policies are intentionally minimal.
CURRENT
2016-12-20
Standard
AIR6521
This platform specific Interface Control Document (ICD) provides an example mapping to the Object Management Group’s (OMG) Data Distribution Service (DDS) infrastructure middleware. The mapping is based on the Unmanned Systems (UxS) Control Segment (UCS) Architecture: Model, AS6518. A series of non-normative implementation choices have been made that are specific to this ICD. These implementation choices may not be appropriate for different system implementations. The machine readable ICD and result of this mapping and implementation choices are provided with AIR6521. Use and understanding of this document assumes a working knowledge of the UCS Architecture, the model structure and its contents.
CURRENT
2016-12-20
Standard
AIR6520
Governance of the Unmanned Aircraft System (UAS) Control Segment (UCS) Architecture was transferred from the United States Office of the Secretary of Defense (OSD) to SAE International in April 2015. Consequently, a subset of the UCS Architecture Library Release 3.4(PR) has been published under SAE as the Unmanned Systems (UxS) Control Segment (UCS) Architecture, AS6512. This Version Description Document (VDD) describes the correspondence and differences between the two architecture libraries.
CURRENT
2016-12-20
Standard
AIR6519
The Use Case Trace (UCTRACE) is SAE publication AIR6519 of the Department of Defense Unmanned Control Segment (UCS) Architecture. This document is the SAE publication of the Department of Defense UAS Control Segment (UCS) Architecture: Use Case Trace (UCTRACE) Version 3.4(PR) approved for Distribution A public release 15.S-1859. This information is produced from a script run against the System Use Case Model contained in the UCS Architecture Model AS6518-MODEL.eap configuration item. The System Use Case Model includes, at its lowest level of elaboration, use cases Level 2/3 (L2/L3) that describe specific scenarios of message exchanges between Actors and internal system Participants via ServiceInterfaces. These message exchanges provide a way to create detailed traces that answer the question: “What UCS service interfaces must my components implement to satisfy functional requirements represented by a given Level 2/3 UCS use case?”
2016-12-09
WIP Standard
AS6171/20
To define capabilities and limitations of X-Ray Photoelectron Spectroscopy (XPS) as it pertains to detection of suspect/counterfeit EEE parts and suggest possible applications to these ends. Additionally, this document outlines requirements associated with the application of XPS including: operator training and requirements; sample preparation; data interpretation; and data reporting procedures.
2016-12-09
WIP Standard
AS6171/19
This document defines capabilities and limitations of Auger Electron Spectroscopy (AES) as it pertains to detection of suspect/counterfeit EEE parts and suggests possible applications to these ends. Additionally, this document outlines requirements associated with the application of AES including: operator training and requirements; sample preparation; data interpretation and reporting of data.
2016-12-09
WIP Standard
AS6171/21
This document defines capabilities and limitations of Gas Chromatography/Mass Spectrometry (GC/MS) as it pertains to detection of suspect/counterfeit EEE parts and suggests possible applications to these ends. Additionally, this document outlines requirements associated with the application of GC/MS including: operator training; sample preparation; various sampling techniques; data interpretation; computerized spectral matching; equipment maintenance; and reporting of data. The discussion is limited to unit mass resolution spectrometers such as quadrupole systems and electron impact ionization.
2016-12-09
WIP Standard
AS6171/18
This test method provides the capabilities, limitations, and suggested possible applications of TMA as it pertains to detection of suspect/counterfeit EEE parts. Additionally, this document outlines requirements associated with the application of TMA including: equipment requirements, test sample requirements, methodology, control and calibration, data analysis, reporting, and qualification and certification.
2016-12-08
WIP Standard
AS6294/1
1. Review existing standards for PEM qualification & screening  NASA: PEM-INST-001, MSFC-STD-3012  QML Class N, Class Y (non-hermetic microcircuits)  QML Class F, Class L (non-hermetic hybrids)  etc. 2. Provide recommendations for unification  Address concerns for Space & terrestrial applications  Address possible holes in current documents  Make recommendations to improve QML Class N and Class Y 3. Be resource to industry when questions come up that are not being addressed by current PEM flows
CURRENT
2016-12-08
Standard
J3114_201612
The aim of this Information Report is to provide terms and definitions that are important for the user’s interaction with L2 through L4 driving automation system features per SAE J3016, which provides a basis for this document.
CURRENT
2016-12-01
Standard
ARP1821B
This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields with application to both commercial and military aircraft.
CURRENT
2016-11-22
Standard
AMS2817G
This specification covers procedures which will provide protection of elastomeric seals and seal assemblies such as O-rings, cap seal assemblies, and other designs from contamination by foreign materials and handling / transportation / storage damage prior to installation and ensure positive identification by part number of each piece until it is installed.
CURRENT
2016-11-08
Standard
TB0003A
This Technical Bulletin covers the following areas of concern. Prevention: Actions recommended for procuring parts and materials with a full warranty; Actions recommended for minimizing risks and protecting your Program from counterfeiting; Actions recommended when buying from a non-authorized supplier. Detection: Actions recommended when procuring parts from an unauthorized supplier or otherwise suspect that a part or material at risk of being counterfeit has been procured. Risk Mitigation: Actions recommended when no reasonable alternatives exist (e.g., a redesign is required, an unacceptable schedule delay will result, the program or customer cannot bear the additional cost) and the decision has been made to procure from a non-authorized supplier.
CURRENT
2016-11-08
Standard
ARP9136
The objective of any organization, as part of continual improvement, is to reduce the number of issues (i.e., undesirable conditions, defects, failures) and to minimize their impact on quality, delivery performance, and cost. This includes having processes in place to detect and eradicate significant and recurrent issues, which implies having well identified problems, a common understanding of their impact and associated root causes, and having defined and implemented adequate actions so that these problems, including similar issues will not happen again.
CURRENT
2016-11-08
Standard
AS9162
This document identifies the basic elements and provides a standard for structuring operator self-verification programs within the aviation, space, and defense industry for producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines, and composite components. The requirements specified in this standard are complementary (not alternative) to contractual and applicable statutory and regulatory requirements. Should there be a conflict between the requirements of this standard and applicable statutory or regulatory requirements, the latter shall take precedence.
CURRENT
2016-11-01
Standard
AS9120B
Price increases in effect for this document as of January 2017 reflect a new copyright agreement for use of ISO 9001:2015. This standard includes ISO 9001:2015 quality management system requirements and specifies additional aviation, space, and defense industry requirements, definitions, and notes. It is emphasized that the requirements specified in this standard are complementary (not alternative) to customer and applicable statutory and regulatory requirements. If there is a conflict between the requirements of this standard and customer or applicable statutory or regulatory requirements, the latter shall take precedence.
CURRENT
2016-10-31
Standard
AS9101F
This standard defines requirements for the preparation and execution of the audit process. In addition, it defines the content and composition for the audit reporting of conformity and process effectiveness to the 9100-series standards, the organization's QMS documentation, and customer and statutory/regulatory requirements. The requirements in this standard are additions or represent changes to the requirements and guidelines in the standards for conformity assessment, auditing, and certification as published by ISO/IEC (i.e., ISO/IEC 17000, ISO/IEC 17021-1). When there is conflict with these standards, the requirements of the 9101 standard shall take precedence. NOTE 1: In this standard, the term “9100-series standards” comprises the following Aerospace Quality Management System (AQMS) standards: 9100, 9110, and 9120; developed by the IAQG and published by various national standards bodies.
Viewing 1 to 30 of 410