The purpose of this SAE Aerospace Recommended Practice (ARP) is to ensure conformance for each product characteristic being verified in a lot, without maintaining information from previous lots. ARP9013/1 specifies a product acceptance system for isolated lots. For example, isolated lot sampling avoids keeping track of the normal, tightened, and reduced levels of sampling formerly used in MIL-STD-105 and currently used in ANSI/ASQC Z1.4. Because those switching rules provided significant long-term protection for product quality, these isolated lot tables replace that protection in other ways.
These requirements are applicable to IAQG global sectors when utilizing Aerospace Industry Controlled Other Party (ICOP) schemes for the assessment and certification of supplier quality systems in accordance with the requirements contained in 9104. IAQG member companies have committed to perform sufficient oversight of the Aerospace accreditation/certification assessment processes in order to ensure conformance to established requirements contained in 9104. NOTE: The IAQG OPMT oversight structure is depicted graphically in Appendix A.
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.
This document defines to supplier/subcontractor common information and documentation required to inform Customers, when applicable about nonconformity (Customer-provider use). It does not apply to the reporting of a nonconformity to the product owner/operator. Reporting of Product Quality Escapes and use of Waiver/Concession is subject to the terms and conditions of the contractual requirements.
The purpose of this document is to define the content and the presentation of the Assessment Report of the section 1 of the AS/EN/JISQ 9100, based on ISO 9001-2000.
AS9131 - This standard defines the common nonconformance data definition and documentation that an internal or external supplier or sub-tier supplier must submit when informing a customer of a nonconformity. The requirements shall be are applicable for reporting a nonconforming product to the owner/operator (i.e., end item user), if specified by contract. Reporting of nonconformance data, either electronically or conventionally on paper, is subject to the terms and conditions of the contract. This also includes, where applicable, data access under export control regulations.
This document provides a basic uniform method for ensuring that aerospace standard parts (products) conform with the requirements of technical specifications referring to qualified parts and for a manufacturer of such parts to have a qualified management system at least equivalent to AS/EN/SJAC9100. These standards apply when called out in the aerospace standard part standard.
This document contains the minimum requirements for supplier Inspection and Test Quality System. It is emphasized that the quality system requirements specified in this standard are complementary (not alternative) to the contractual and applicable law and regulatory requirements.
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.
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.
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.
This standard is applicable to AQMS COs listed in the Online Aerospace Supplier Information System (OASIS) database. This standard is intended for the management and resolution of AQMS CO’s major QMS nonconformities. This standard is not intended to address QMS nonconformities classified as minor or nonconformities related to the products or services provided by the CO.
This standard is primarily intended to apply to new parts and products intended to be produced in an on-going production phase, but can also be applied to parts currently in production (e.g., manufacturing, maintenance). The standard is applicable to all production processes that influence the variation of KCs, as well as maintenance and service processes in which KCs are identified. It applies to organizations for assemblies and all levels of parts within an assembly, down to the basic materials including castings and forgings, and to organizations that are responsible for producing the design characteristics of the product. The variation control process begins with product definition, typically stated in the design documentation (e.g., digital model, engineering drawing, specification) which identifies KCs, and leads to a variation management process for those KCs. This process may also be used for producer-identified KCs (e.g., process KCs, additional/substitute product KCs).
This standard is primarily intended to apply to new parts and products, but can also be applied to parts currently in production. The standard shall be applicable to all production processes, that influence the variation of KCs, as well as maintenance processes in which KCs are identified. It applies to assemblies and all levels of parts within an assembly, down to the basic materials including castings and forgings, and to organizations that are responsible for producing the design characteristics of the product. It does not apply to lab-scale, pilot, or pre-production processes. However, particular management of some KCs might be required using other methods than those described in the standard, during these phases of a program, when required by the customer or deemed appropriate by the organization (e.g., Engineering department requirement).
This SAE Aerospace Standard (AS) provides a harmonized process and documentation requirements for the establishment of CoCs used to attest the conformity of aviation, space, and defense products (e.g., assemblies, sub-assemblies, equipment and systems, parts, material, software) or services. It includes a CoC template and supporting instructions on how to complete it. When quoted by the customer in a contractual requirement, application of this document is mandatory. In other cases, its use is recommended, but if there is a conflict between the requirements of this standard and customer or applicable statutory/regulatory requirements, the latter shall take precedence.