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This Standard is primarily intended to apply to new parts, but can also be applied to parts currently in production. The Standard shall be applicable to all production processes that influence the variation of Key Characteristics.

ARP9013/3 recommended practice specifies a product acceptance system using process control methods. Its purpose is to assure conformance for specified characteristics. Use of process control techniques for product acceptance requires maintaining process stability and capability. A stable and capable process is the best assurance of conforming hardware for the customer. There can be lower inspection costs associated with a process control acceptance approach.

ARP9013/3 recommended practice specifies a product acceptance system using process control methods. Its purpose is to assure conformance for specified characteristics. Use of process control techniques for product acceptance requires maintaining process stability and capability. A stable and capable process is the best assurance of conforming hardware for the customer. There can be lower inspection costs associated with a process control acceptance approach.

The purpose of ARP9013/4 is to ensure conformance for each product characteristic being verified under these methods. ARP9013/4 provides the requirements for continuous sampling, skip-lot sampling, and for statistical methods for product acceptance that do not derive from industry standard tables.

This SAE Aerospace Recommended Practice (ARP) establishes the general requirements when implementing any of the statistical product acceptance methods as defined in ARP9013/1, ARP9013/2, ARP9013/3, and ARP9013/4. This recommended practice also establishes the minimum content required to be covered in an organization’s documented procedures that govern their application of statistical product acceptance methods. These general requirements and documented procedures apply the requirements of AS9100 plus requirements for retrievability, safety/critical characteristics, quality parameters, and that these parameters protect the customer. This recommended practice is to be used in conjunction with the variety of sampling strategies, statistical techniques, and process control methods of the ARP9013/1 through ARP9013/4 recommended practices as chosen by the organization.

This procedure shall be applied by ANSI-RAB or other Accreditation Bodies to registrars that meet the criteria of 5.2 of this document, when specified by an aerospace company requiring assessment and/or registration of their quality system to the requirements of this procedure. The quality system standard shall be AS9000 or AS9100 and shall be applied to the supplier's complete Quality System that covers aerospace products.

The requirements established in this document are applicable to the IAQG and associated sectors for managing oversight to established requirements contained in 9104-series standards (i.e., 9104/1, 9104/2, 9104/3). The requirements are applicable to IAQG working groups for oversight.

This document provides the minimum requirements (Body of Knowledge) for AQMS auditors who will participate in AQMS certification/registration activities, including the auditor authentication process and requirements for a training organization. It is applicable to auditors seeking formal approval to conduct audits of the AQMS in support of the IAQG, and those who manage the competency element of an AQMS audit program and/or training organizations.

This standard includes ISO 9001:20152 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.

This standard includes selected quality system requirements from ISO 9001:2008[1] and AS9100:2009 applicable to noncomplex products and associated manufacturing processes. ISO 9001 text incorporated into this standard appears in standard font; while aviation, space, and defense industry additional requirements, definitions, and notes are presented in bold, italic text. The requirements of this standard are intended to be applied in whole, without any exclusions. Compliance with all corresponding AS9100 requirements is considered to meet/exceed compliance with the requirements of this standard. 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. The process approach described in ISO 9001 and AS9100 applies to this standard.

This standard includes selected quality system requirements from ISO 9001:2008[1] and AS9100:2009 applicable to noncomplex products and associated manufacturing processes. ISO 9001 text incorporated into this standard appears in standard font; while aviation, space, and defense industry additional requirements, definitions, and notes are presented in bold, italic text. The requirements of this standard are intended to be applied in whole, without any exclusions. Compliance with all corresponding AS9100 requirements is considered to meet/exceed compliance with the requirements of this standard. 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. The process approach described in ISO 9001 and AS9100 applies to this standard.

Limited to the Aerospace industry where an approved manufacturer requests a supplier to ship an article against the approved manufacturer’s quality system directly to a customer. The direct ship process is not required or applicable to standard parts or military parts. In this process the approved manufacturer is responsible for assurance that the article conforms to Type Design information.

This document is limited to the aerospace industry, where an approved manufacturer requests a supplier to ship an article against the approved manufacturer’s quality system directly to a customer. The direct ship process is not required or applicable to standard parts or military parts. In this process, the approved manufacturer is responsible for assurance that the article conforms to type design information.

Limited to the Aerospace industry where an approved manufacturer requests a supplier to ship an article against the approved manufacturer’s quality system directly to a customer. The direct ship process is not required or applicable to standard parts or military parts. In this process the approved manufacturer is responsible for assurance that the article conforms to Type Design information.

Limited to the Commercial Aerospace industry where a request is made for a Production Organization (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.

The basic requirements of AS9100A apply with the following clarifications. This document supplements the requirements of AS9100A for deliverable software. This supplement contains Quality System requirements for suppliers of products that contain deliverable embedded or loadable airborne, spaceborne or ground support software components that are part of an aircraft Type Design, weapon system, missile or spacecraft operational software and/or support software that is used in the development and maintenance of deliverable software. This includes the host operating system software including assemblers, compilers, linkers, loaders, editors, code generators, analyzers, ground simulators and trainers, flight test data reduction, etc., that directly support creation, test and maintenance of the deliverable software.

This standard specifies requirements for DPRV to establish common product/service requirements for use at all levels of the supply chain. This standard shall apply when an organization elects to delegate product release verification by contractual flow down to their supplier (reference 9100 and 9110 standards); to perform product acceptance on their behalf. The delegating organization shall use this standard as the baseline for establishing a DPRV process, although they may include additional contract requirements to meet their specific needs.

This standard defines uniform quality and technical requirements relative to metallic parts marking performed using "data matrix symbology" within the aviation, space, and defense industry. ISO/IEC 16022 specifies general requirements (e.g., data character encodation, error correction rules, decoding algorithm). In addition to ISO/IEC 16022 specification, part identification with such symbology is subject to the requirements in this standard to ensure electronic reading of the symbol. The marking processes covered by this standard are as follows: Dot Peening Laser Electro-Chemical Etching Further marking processes will be included, if required. Unless specified otherwise in the contractual business relationship, the company responsible for the design of the part shall determine the location of the data matrix marking. Symbol position should allow optimum illumination from all sides for readability. This standard does not specify information to be encoded.

This SAE Aerospace Standard (AS) defines uniform Quality and Technical requirements relative to metallic parts marking performed in using "Data Matrix symbology" used within the aerospace industry. The ISO/IEC 16022 specifies general requirements (data character encodation, error correction rules, decoding algorithm, etc.). In addition to ISO/IEC 16022 specification, part identification with such symbology is subject to the following requirements to ensure electronic reading of the symbol. The marking processes covered by this standard are as follows: Dot Peening Laser Electro-Chemical Etching Further marking processes will be included if required. This standard does not specify information to be encoded. Unless specified otherwise in the contractual business relationship, the company responsible for the design of the part shall determine the location of the Data Matrix Marking. Symbol position should allow optimum illumination from all sides for readability.

This Standard defines uniform Quality and Technical requirements relative to metallic parts marking performed in using "Data Matrix symbology" (2D) coding used within the aerospace industry. The ISO 16022 specifies general requirements (data characters encodation, error correction rules, decoding algorithm, etc.). In addition to this specification, part Identification with such coding is subject to the following requirements to ensure electronic reading (scanning) ability of the symbol. The marking processes covered by this standard are as follows: Dot Peening Laser Marking Electro-Chem Etching Further marking processes will be included if required. Unless specified otherwise in the contractual business relationship, the company responsible for the design of the part shall determine the location of the Data Matrix Marking. Symbol position should allow illumination from all sides for readability.