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2017-05-23
WIP 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.
2017-05-23
WIP 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.
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
2017-05-11
Standard
AS6171/2A
This document describes the requirements of the following test methods for counterfeit detection of electronic components: Method A: General EVI, Sample Selection, and Handling Method B: Detailed EVI, including Part Weight measurement Method C: Testing for Remarking Method D: Testing for Resurfacing Method E: Part Dimensions measurement Method F: Surface Texture Analysis using SEM The scope of this document is focused on leaded electronic components, microcircuits, multi-chip modules (MCMs), and hybrids. Other EEE components may require evaluations not specified in this procedure. Where applicable this document can be used as a guide. Additional inspections or criteria would need to be developed and documented to thoroughly evaluate these additional part types. If SAE AS6171/2 is invoked in the contract, the base document, AS6171 General Requirements shall also apply.
2017-05-09
WIP Standard
AS6174/3
This document standardizes requirements for bearings: (a) supply chain management, procurement, inspection, parts management, and test/evaluation to assure the authenticity of bearings being acquired/used, and (b) response strategies when suspect or confirmed counterfeit bearings are discovered. Though developed primarily for critical application bearings, the document also may be applicable, at the discretion of the user, to other bearings with similar characteristics and applications. The bearings slash sheet is not intended to replace, conflict with, or duplicate requirements in quality system or AMS series material specs but rather to augment them with regards to counterfeit prevention and risk mitigation.
CURRENT
2017-05-09
Standard
EIASTD4899C
This document applies to the development of Plans for integrating and managing electronic components in equipment for the military and commercial aerospace markets; as well as other ADHP markets that wish to use this document. Examples of electronic components, as described in this document, include resistors, capacitors, diodes, integrated circuits, hybrids, application specific integrated circuits, wound components, and relays. It is critical for the Plan owner to review and understand the design, materials, configuration control, and qualification methods of all “as-received” electronic components, and their capabilities with respect to the application; identify risks, and where necessary, take additional action to mitigate the risks. The technical requirements are in Clause 3 of this standard, and the administrative requirements are in Clause 4.
CURRENT
2017-05-08
Standard
AIR6211A
This test method provides stakeholders (runway deicing chemical manufacturers, users, regulators, and airport authorities) with a relative ice penetration capacity of runway deicing/anti-icing chemicals, by measuring the ice penetration as a function of time. Such runway deicing/anti-icing chemicals are often also used on taxiways and other paved areas. This test method does not quantitatively measure the theoretical or extended time of ice penetration capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form.
2017-04-20
WIP Standard
AS9104/1A
These requirements are applicable to IAQG global sectors when utilizing Aerospace Industry Controlled Other Party (ICOP) schemes for the assessment and certidication of supplier quality systems in accordance with the requirements AS/EN/SJAC 9104.
CURRENT
2017-04-18
Standard
AS6416
This SAE Aerospace Standard provides definitions for terms and requirements used in SAE AS procurement specifications for fasteners (bolts, screws, studs, nuts, and other threaded parts).
2017-04-14
WIP Standard
STD0016A
This document defines the requirements for developing a DMSMS Management Plan, hereinafter also called the Plan, to assure customers that the Plan owner is using a proactive DMSMS process for minimizing the cost and impact that part and material obsolescence will have on equipment delivered by the Plan owner. The technical requirements detailed in clause 5 ensure that the Plan owner can meet the requirement of having a process to address obsolescence as required by Industry Standards such as EIA-4899 "Standard for Preparing an Electronic Components Management Plan" and DoD Programs as required by MIL-STD-3018 "Parts Management". Owners of DMSMS Management Plans include System Integrators, Original Equipment Manufacturers (OEM), and logistics support providers.
CURRENT
2017-04-11
Standard
AS6174/1
To assure compliance to AS6174A requirements, a set of standard assessment verification criteria is utilized to evaluate and establish uniform compliance assessment. This document standardizes verification compliance criteria for AS6174A requirements.
CURRENT
2017-03-21
Standard
AS15531A
This SAE Aerospace Standard (AS) contains requirements for a digital time division command/response multiplex data bus, for use in systems integration, that is functionally equivalent to MIL-STD-1553B with Notice 2. Even with the use of this document, differences may exist between multiplex data buses in different system applications due to particular application requirements and the options allowed in this document. The system designer must recognize this fact and design the multiplex bus controller (BC) hardware and software to accommodate such differences. These designer selected options must exist to allow the necessary flexibility in the design of specific multiplex systems in order to provide for the control mechanism, architectural redundancy, degradation concept, and traffic patterns peculiar to the specific application requirements.
2017-03-13
WIP Standard
ARP5283B
The purpose of this specification is to provide airplane operators and tow vehicle manufacturers with: a. General design and operating requirements pertinent to test and evaluation of towbarless tow vehicles. Specific design requirements are provided in ARP4852 and ARP4853. b. Test and evaluation requirements. The results of these test evaluations will determine if the loads induced by the tow vehicle will exceed the design loads of the nose gear, or are within the aircraft manufacturer’s limits so that they do not affect the certified safe limit of the nose gear. The results of these test evaluations will also determine if a stability problem may occur during pushback and/or maintenance towing operations with the tested airplane/tow vehicle combination. This document specifies general test requirements and a test evaluation procedure for towbarless tow vehicles (TLTV) intended for pushback and maintenance towing only.
2017-03-02
WIP Standard
ARP1962B
This document requires that the company (facility) employing the personnel ensure a verifiable program of on-the-job training, experience, education, classroom instruction, and evaluation of personnel using either company-created programs or programs described herein. It describes the requirements for training and approval of personnel performing certain heat-treating and associated operations. It also establishes that only approved personnel may perform or monitor the functions listed for the processes and materials listed.
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. Identify the minimum performance requirements for active RFID tags to be used on or in close proximity to aircraft. 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. Identify existing standards applicable to active RFID Tag. Provide a certification standard for RFID tags which will use permanently-affixed installation on aircraft and aircraft parts. 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: 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.
CURRENT
2017-02-08
Standard
TS200AR-44
No Scope available.
CURRENT
2017-02-07
Standard
AIR1812B
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.
2017-01-18
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
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?”
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
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
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.
Viewing 1 to 30 of 406