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This document provides background information, rationale, and data (both physical testing and computer simulations) used in defining the component test methods and similarity criteria described in SAE Aerospace Recommended Practice (ARP) 6330. ARP6330 defines multiple test methods used to assess the effect of seat back mounted IFE monitor changes on blunt trauma to the head and post-impact sharp edge generation. The data generated is based on seat and IFE components installed on type A-T (transport airplane) certified aircraft. While not within the scope of ARP6330, generated test data for the possible future development of surrogate target evaluation methods is also included
Aircraft Seat Committee
This SAE Aerospace Recommended Practice (ARP) provides recommendations for: The audit process in general A list of specific areas of attention to be audited Maintaining the test facility in such a manner that it meets audit requirements
EG-1E Gas Turbine Test Facilities and Equipment
This SAE Standard was prepared to assist manufacturers of tractors and implements in providing suitable means of transmitting power from the tractor power take-off to the Implement and satisfactory hitching of the implement to the tractor
Agricultural Tractor Standards Committee (ATSC)
The scope of this SAE Standard is to provide methods to determine display optical performance in all typical automotive ambient light illumination, with focus on high ambient contrast ratio, which is critical for display legibility in a sunshine environment. It covers indoor measurements and simulated outdoor lighting. It is not the scope of this document to set threshold values for automotive compliance. However, some recommended values are presented for reference. The present revision does not address the usage of polarized sunglasses
Vehicular Flat Panel Display Standards Committee
This SAE Standard describes a procedure for the evaluation of operator seats which may be fitted to agricultural wheeled tractors per SAE J1150 and/or earthmoving machines per SAE J1057. This procedure evaluates only the vertical vibration performance and should not be considered a comprehensive seat evaluation procedure
HFTC4, Operator Seating and Ride
This standard defines requirements for the identification, assessment, mitigation, and prevention of risk in the manufacturing process through the application of Process Flow Diagrams (PFDs), Process Failure Mode and Effects Analysis (PFMEA) and Control Plans throughout the life cycle of a product. This standard aligns and collaborates with the requirements of AS9100, AS9102, AS9103, and AS9145. The requirements specified in this standard apply in conjunction with and are not alternative to contractual and applicable statutory and regulatory requirements. In case of conflict between the requirements of this standard and applicable statutory or regulatory requirements, the latter shall take precedence
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
The requirements defined in this AIR are applicable to Accreditation Bodies (ABs), Certification/Registration Bodies (CRBs), and Original Equipment Manufacturers (OEMs), during assessment and/or certification/registration to the applicable quality management system standard to meet industry accepted practices
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
Operator Self-Verification can apply to a variety of processes. The primary focus is on traditional manufacturing operations, but applications can be made wherever traditional inspection methods are employed. The practices recommended in this document are intended to identify the basic elements for structuring Operator Self-Verification programs within the aerospace industry; applicable to producers of commercial and military aircraft and weapons platforms, space vehicles, and all related hardware, software, electronics, engines and composite components. Operator Self-Verification programs are applied to improve overall efficiency and product quality to processes considered mature, as judged by the organization. Operator Self-Verification programs are not stand-alone processes, but augment existing quality management system standard requirements. The identified program elements are for voluntary organizational application, and are not intended for contractual flow-down unless otherwise
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
These requirements are applicable to IAQG sector schemes when making use of ABs, CRBs and their auditors, for the assessment and certification/registration of supplier quality systems in accordance with the requirements of this document. The quality management system standard used by the CRB shall be 9100/9110/9120, as appropriate to the supplier’s activities. It shall be applied to the supplier’s complete Quality System that covers aerospace products. Sectors may use these requirements for other standards. IAQG members have committed to recognize the equivalence of certification/registration of a suppliers quality management system to either of the AS, EN or JISQ/SJAC standards. This AS provides the approval process for Auditor Authentication Bodies (AAB), training course providers, trainers and auditors who meet the requirements of AIR5493 and outlines the America’s sector specific process to implement AS9104. This document is created to be in conformance with AS9104
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
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
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Aerospace Standard (AS) further defines the requirements for a delegation process identified in Aerospace Quality Management System (AQMS) standards (i.e., AS9100, AS9110, AS9120). This standard establishes minimum requirements for the delegation of product verification to an organization's suppliers; outlining requirements for the initial delegation (qualification/selection), maintenance, and removal/withdrawal of delegations
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
The requirements of 9100 apply with the following clarification for software. This standard supplements the 9100 standard requirements for deliverable software and contains quality management system requirements for organizations that design, develop, and/or produce deliverable software and services for the aviation, space, and defense industry. This includes, as required, support software that is used in the development and maintenance of deliverable software and services. The deliverable software may be stand-alone, embedded, mobile application, or loadable into a target computer. This deliverable software may also be part of services (e.g., cloud environment, web hosted solutions or platforms). Where the use of Hardware Description Language (HDL) or high order language is utilized as the design source of electronic hardware [e.g., Application Specific Integrated Circuit (ASIC), Programmable Logic Device (PLD)]; the organization and customer, and/or supplier shall agree on the extent
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Standard provides test procedures, requirements, and guidelines for stop lamps intended for use on vehicles 2032 mm or more in overall width. Stop lamps conforming to the requirements of this document may be used on vehicles less than 2032 mm in overall width
Heavy Duty Lighting Standards Committee
This document surveys the systems used for thermal management of batteries in vehicles. Battery thermal management is important for battery performance and cycle life. The document also includes a summary of design considerations for battery thermal management and a glossary of terms
Battery Thermal Management Committee
This standard establishes requirements for performing and documenting APQP and PPAP. APQP begins with conceptual product needs and extends through product definition, production planning, product and process validation (i.e., PPAP), product use, and post-delivery service. This standard integrates and collaborates with the requirements of the 9100, 9102, 9103, and 9110 standards. 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
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Information Report provides test methods and determination options for evaluating the maximum wheel power and rated system power of vehicles with electrified vehicle powertrains. The scope of this document encompasses passenger car and light- and medium-duty (GVW <10000 pounds) hybrid-electric vehicles (HEVs), plug-in hybrid electric vehicles (PHEVs), battery electric vehicles (BEVs), and fuel-cell electric vehicles (FCEVs). These testing methods can also be applied to conventional ICE vehicles, especially when measuring and comparing wheel power among a range of vehicle types. This document version includes a definition and determination methodology for a rated system power that is comparable to traditional internal combustion engine power ratings (e.g., SAE J1349 and UN ECE R85). The general public is most accustomed to “engine power” and/or “motor power” as the rating metric for conventional and electrified vehicles, respectively. Wheel power will always be a lower-power
Hybrid - EV Committee
This SAE Standard establishes the test equipment, procedure, and acceptance criteria necessary to determine the location of power driven components that could—upon inadvertent contact by an operator, passenger, or bystander—inflict injury
Snowmobile Technical Committee
This standard establishes the common requirements for training of DPRV personnel for use at all levels of the aerospace engine supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to its suppliers (reference 9100 and 9110 standards) and to perform product acceptance on its behalf. It is intended that organizations specify their DPRV requirements through the application of AS9117. While the delegating organization will use the AS13001 standard as the baseline for establishing DPRV process and product training, it may include additional contractual training requirements to meet its specific needs. The DPRV training material was primarily developed for aerospace engine supply chain requirements. However, this standard may also be used in other aerospace industry sectors where a DPRV process requiring specific training can be of benefit
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This document describes requirements for standardized processes (and associated technologies) that ensure type design data are retrievable and usable for the life of a type certificate (50+ years). These processes are primarily concerned with, but not limited to, digital type design data retained in three-dimensional representations and associated data that is required for complete product definition, such as tolerances, specification call-outs, product structure and configuration control data, etc. This process standard includes process requirements for managing the evolution of technologies required to ensure the availability of the data for the life of the product. This data must be available to meet regulatory, legal, contractual and business requirements. This process standard is not intended to incorporate every company specific requirement and does not dictate specific organizational structures within a company. This process standard does not specify a design or an
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
To assure customer satisfaction, aerospace industry manufacturers must produce world class quality products at the lowest possible cost. This document standardizes, to the greatest extent possible, the quality system requirements of the aerospace industry. Standardization of compliance requirements results in cost savings due to the elimination or reduction of unique requirements developed for each different customer
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Aerospace Standard (AS) establishes documentation requirements for the First Article Inspection (FAI). The purpose of the First Article Inspection is to provide objective evidence the all engineering design and specification requirements are properly understood, accounted for, verified, and documented. The purpose of this document is to provide a consistent documentation requirement for aerospace components First Article Inspection. It is the intent that the documentation generated will be a quality record of the supplier and customer for review of accountability and planning, for performing periodic surveillance and audits to verify conformance, for evaluating root cause and corrective action for any non-conformance, and for problem ionvestigations
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Recommended Practice provides test methods and criteria for evaluating the internal cleanliness and air leakage for engine charge air coolers. This SAE Recommended Practice also provides nomenclature and terminology in common use for engine charge air coolers, related charge air cooling system components, and charge air cooling system operational performance parameters
Cooling Systems Standards Committee
This SAE Recommended Practice provides uniform definitions and classifications for motorcycles
Motorcycle Technical Steering Committee
This SAE Recommended Practice establishes air quality standards for the pressurized air in the brake system of vehicles with air brakes
Truck and Bus Brake Supply and Control Components Committee
This compliance assessment tool supports the summary of requirements applicable to AS6500A, including potential documentation to demonstrate compliance along with tailoring options and company policies. The standard is applicable to all phases of the system acquisition life cycle. It is intended for use on all programs with manufacturing content. It requires proven manufacturing management practices with the goal of delivering affordable and capable systems to the extent that it is invoked contractually
G-23 Manufacturing Management Committee
To define capabilities and limitations of Raman spectroscopy as it pertains to counterfeit detection of EEE parts and suggest possible applications to these ends. Additionally, this document outlines requirements associated with the application of Raman spectroscopy including: Operator training; Sample preparation; Data interpretation; Computerized spectral matching including pass/fail criteria; Equipment maintenance and; Reporting of data. If AS6171/8 is invoked in the contract, the base document, AS6171 General Requirements shall also apply
G-19A Test Laboratory Standards Development Committee
This information report provides definitions of acoustical terms relating to sound insulation materials. Appropriate methods of test are being developed by SAE and where applicable, ASTM methods will be referenced
Acoustical Materials Committee
This SAE Standard applies to off-road self-propelled construction, forestry and industrial machines as listed in categories 1, 2, and 4 of SAE J1116
Off-Road Machinery Technical Comm
This test standard covers the procedure for measuring the permeation of fuel or fuel surrogates through test samples of elastomeric, plastic or composite materials, up to about 3 mm thick. The method involves filling a test cup with the test fluid (fuel or fuel surrogate), sealing test sample over the open end of the cup, and then placing the sealed container into an oven at the desired test temperature and measuring the weight loss over time. Permeation rates are calculated from the rate of weight loss and the exposed area of the test sample. Standard permeation test temperatures are 40 °C and 60 °C. Standard test fluids are Fuel C, Fuel CE10 and Fuel CM15. Other fluids, such as Fuel CMTBE15, and other volatile liquids may be tested according to this procedure as desired (SAE J1681). The method is not applicable for measuring permeation of higher boiling materials that will not completely evaporate from the exterior surface of the sample at the test temperature
Fuel Systems Standards Committee
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
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This standard establishes supplemental requirements for 9100 and 9145 and applies to any organization receiving it as part of a Purchase Order or other contractual document from a customer. AS13100 also provides details of the Reference Materials (RM13xxx) developed by the SAE G-22 AESQ committee and listed in Section 2 - Applicable Documents, that can also be used by organizations in conjunction with this standard
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This SAE Standard covers ordering information for steel wire reinforced rubber hose assemblies using connectors specified in SAE Standard J516 or all parts of ISO 12151 for use in hydraulic systems using petroleum based hydraulic fluids with maximum working pressures of 1.7 to 42 MPa. See SAE J1754-2, Table 8 for hose operating temperature ranges and identification codes. NOTE: Working pressure is defined as maximum system pressure
Hydraulic Hose and Hose Fittings Committee
The task force was assigned responsibility for the following activities: 1 Formulate a recommendation for an acceptable ride meter including features, functional performance, and design specifications. 2 Conduct a survey to determine if there is a commercially available ride meter conforming to the recommendation. 3 If an acceptable ride meter is not commercially available, work with an electronics supplier to initiate a design and build a working prototype of a meter conforming to the recommendation
HFTC4, Operator Seating and Ride
Included herein are the detailed general and dimensional specifications applicable to hi-head finished hex bolts. All general specifications and dimensions not shown shall conform to those applicable to finished hex bolts in Table 4 of SAE J104. Hi-head finished hex bolts arc primarily intended for use in the heavy construction and industrial equipment industry. The increase in head height over that of the finished hex bolt assures good wrenchability where frequent servicing is necessary, where high torquing is a requirement, or where wear on the bolt head is a problem
Fasteners Committee
This SAE Recommended Practice is intended to establish guidelines for conducting passenger car roll-over tests so that data obtained by various test facilities may be more readily compared. A description is provided of the facilities and procedures for a curved rail-ramp technique, which has been found to be successful in producing roll-overs. Techniques and instrumentation for the study and evaluation of vehicle structure effects and occupant movement resulting from roll-overs produced by the curved rail-ramp system are also specified. The curved rail-ramp procedure has been evolved from laboratory and field studies and tests which have sought to establish procedures which would provide realistic simulations of roll-over accidents without collision, and which would be reproducible among laboratories and between different types of passenger cars. The original issue of SAE J857 described ground level and hill roll-over techniques. However, it was found that these procedures were not
Impact and Rollover Test Procedures Standards Committee
The aviation, space, and defense industries rely on the development and manufacture of complex products comprised of multiple systems, subsystems, and components each designed by individual designers (design activities) at various levels within the supply chain. Each design activity controls various aspects of the configuration and specifications related to the product. When a change to design information is requested or required, the change has to be evaluated against the impacts to the higher-level system. Proposed changes to design information that the design activity identifies to be minor and have no effect on their product requirements or specifications have the potential to be concurrently implemented and approved, where authorized to do so. Changes that affect customer mandated requirements or specifications must be approved prior to implementation. In many cases, the design activity is not the design approver or authority; ultimate approval may be several layers above the
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
The scope of this document is to: 1 Specify techniques to detect SC parts using electrical testing. 2 Provide various levels of electrical testing that can be used by the User to define test plans for detecting SC parts. 3 Provide minimum requirements for testing laboratories so that User/Requester can determine which test houses have the necessary capabilities. (For example: technical knowledge, equipment, procedures and protocols for performing electrical testing for verification analysis.) Note: User/Requester is defined in AS6171 General Requirements 4 Specify Burn-In and environmental tests. The environmental tests include Temperature Cycling for Active Devices and Thermal Shock for Passive Devices. Seal Tests are described and recommended for hermetic devices. The following terminology is used throughout this document: a Shall = is mandatory; b Should = is recommended; and c Will = is planned (is considered to be part of a standard process). If AS6171/7 is invoked in the contract
G-19A Test Laboratory Standards Development Committee
Limited to the commercial aerospace industry where a request is made for a PO to have Direct Delivery Authorization (DDA), which includes an Appropriate Arrangement (AA) between the PO and the Design Organization (DO). In this process the DO is responsible for ensuring the continuous updating of design and airworthiness data to the PO, whilst the PO is responsible for assurance that the manufactured article conforms to approved design and airworthiness data. The PO is responsible to provide airworthiness release documentation
G-14 Americas Aerospace Quality Standards Committee (AAQSC)
This SAE Standard standardizes practices to: a maximize availability of authentic materiel, b procure materiel from reliable sources, c assure authenticity and conformance of procured materiel, including methods such as certification, traceability, testing and inspection appropriate to the commodity/item in question, d control materiel identified as fraudulent/counterfeit, e and report suspect or confirmed fraudulent/counterfeit materiel to other potential users and Authority Having Jurisdiction
G-21 Counterfeit Materiel Committee
This SAE Aerospace Standard (AS) identifies the requirements for mitigating counterfeit products in the Authorized Distribution supply chain by the Authorized Distributor. If not performing Authorized Distribution, such as an Authorized Reseller, Broker, or Independent Distributor, refer to another applicable SAE standard
G-19 Counterfeit Electronic Parts Committee
The intent of this document is to define the methodology for suspect parts inspection using radiological inspection. The purpose of radiology for suspect counterfeit part inspection is to detect deliberate misrepresentation of a part, either at the part distributor or original equipment manufacturer (OEM) level. Radiological inspection can also potentially detect unintentional damage to the part resulting from improper removal of part from assemblies, which may include, but not limited to, prolonged elevated temperature exposure during desoldering operations or mechanical stresses during removal. Radiological inspection of electronics includes film radiography and filmless radiography such as digital radiography (DR), real time radiography (RTR), and computed tomography (CT). Radiology is an important tool used in part verification of microelectronic devices. Radiographic analysis is performed on parts to verify that the internal package or die construction is consistent with an
G-19A Test Laboratory Standards Development Committee
This SAE Recommended Practice contains a series of test methods for use in measuring the viscosity of automotive-type adhesives, sealers, and deadeners. The test methods which are contained in this document are as follows: 1.1 Brookfield® Method 1.2 Castor-Severs Rheometer or Pressure Flowmeter 1.3 Penetrometer 1.4 Capillary Rheometer 1.5 Plate Rheometers
Materials, Processes and Parts Council
This SAE Standard covers the flexible components of marine engine wet exhaust systems from the connection at the engine exhaust manifold to the hull or overboard discharge fittings
Marine Engine Fuel Systems Committee
This SAE Recommended Practice contains the reference information for SAE J1802
Truck and Bus Foundation Brake Committee
This document has been prepared and issued to provide information and guidance on the application of AQAP-2110 when the supplier adheres to the provisions of 9100. This document is published as AQAP-2110-SRD.2 and IA9137. It was jointly developed by NATO and industry representatives for use by NATO and industry to facilitate the use and understanding of the relationship between the AQAP-2110 and 9100. AQAPs may be required when an acquiring nation use Foreign Military Sales (FMS) as its procuring method
IAQG-1 Standards Committee
The content of ARP6328 contains guidance for implementing processes used for risk identification, mitigation, detection, avoidance, disposition, and reporting of counterfeit electrical, electronic, and electromechanical (EEE) parts and assemblies in accordance with AS5553 Revision D. This document may also be used in conjunction with other revisions of AS5553. This document retains guidance contained in the base document of AS5553, updated as appropriate to reflect current practices. This is not intended to stand alone, supersede, or cancel requirements found in other quality management system documents, requirements imposed by contracting authorities, or applicable laws and regulations unless an authorized exemption/variance has been obtained
G-19 Counterfeit Electronic Parts Committee
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