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This SAE Standard presents the minimum requirements for nonmetallic tubing with one or more layers manufactured for use in exhaust gas recirculation systems Requirements in this document apply to monowall tubing (one layer construction) and multilayer tubing. The tube construction can have a straight wall configuration, a wall that is convoluted or corrugated, or a combination of each.

This SAE Standard presents the minimum requirements for nonmetallic tubing with one or more layers manufactured for use as liquid carrying DEF lines for diesel engine selective catalyst reduction (SCR) after-treatment systems. Requirements in this document also apply to monowall tubing (one layer construction) and multi-layer constructions. Unless otherwise agreed to by suppliers and users this document applies to tubing for any portion of the DEF system that might operate continuously at temperatures above –40 °C and below 120 °C or for high temperature systems up to 160 °C. Maximum working pressure of 1140 kPa absolute. The tubing can be used at the peak intermittent exterior temperature up to 140 °C or 180 °C. Tubing systems supplied to this application are usually required to thaw from the frozen condition using various heating methods in operation complying with EPA requirements.

This SAE Standard presents the minimum requirements for nonmetallic tubing with one or more layers manufactured for use as pneumatic tubing in automotive air suspension lines. Requirements in this document also apply to monowall tubing (one layer construction) or multi-layer (MLT) constructions. Unless otherwise agreed to by suppliers and users this document applies to tubing for any portion of the fuel system that might operate continuously at temperatures above –40°C and below 90°C and up to a maximum working gage pressure of 1500 kPa. The tubing can be used at the peak intermittent temperature up to 115 °C with peak dynamic pressures of up to 2000 kPa. This document can apply to systems that operate at higher pressures and/or are exposed to higher temperatures with appropriate changes to the acceptance criteria within this document.

Standard covers material performance requirements for extruded thermoplastic tubes used in engine coolant/water applications.

This SAE Standard covers nonreinforced, extruded, plastic tubing intended primarily for use as fluid lines for automotive windshield washer systems which conform to the requirements of SAE J942.

The SAE Aerospace Information Report (AIR) is intended to be used as a process verification guide for evaluating implementation of key factors in bonded repair of fiber reinforced composite structure in a repair shop environment. The guide will be used in conjunction with a regulatory approved and substantiated repair, and is intended to promote consistency and reliability.

This guidebook will assist in the design and integration of composite commercial aircraft structures that exhibit improved durability, maintainability and repairability. For international use by composite aircraft component designers, this book identifies problems that have occurred with various composite components and provides potential problem-solving recommendations. Written primarily for composite design engineers, Design of Durable, Repairable, and Maintainable Aircraft Composites should also prove valuable to those in structural engineering, materials and processing, product support, advanced product development, systems engineering, technical services, and maintenance operations.

SAE CACRC has produced several standards, each representing the best-practice, recommended minimum training syllabus for the aforementioned target groups. The purpose of this document is to promote the use of these SAE standards, particularly for developing training programs for employee training, qualification in airlines and maintenance organizations, and as reference in regulatory guidance material. It summarizes, as a quick reference, the content of each training document and its relation to and interaction with other training documents. Thereby it allows users to select the appropriate training documents and syllabi to establish a comprehensive, sequential training program build-up customized to the specific needs of the aforementioned functions (see figure). This document does not intend to introduce new training content/syllabus.

To create Guidance on the essential information/data that is needed to correctly assess damage and document the damage. A guidance document is proposed as the initial step in which it is documented what essential information is required for a composite repair with the aim to reduce to number of back and forward communications, improve the documents to define damage such as mapping, damage descriptions, sketches, pictures. CACRC Procedures Task Group will be drafting the document.

Increased use of advanced composite structural materials on aircraft has resulted in the need to address the more demanding quality and non-destructive testing procedures. Accordingly, increased utilization of solid laminate composites is driving changes to airline NDT training requirements and greater emphasis on the application of accurate NDT methods. Modules, including an introduction to composite materials, composite NDI theory and practice, special cases and lessons learned, have been produced in addition to various hands-on NDT exercises. A set of proficiency specimens containing realistic composite structures and representative damage has been designed in order to reinforce teaching points of the course and “test” inspector’s proficiency. Extensive details of the course modules, hand-on exercises and the proficiency specimens are all presented in this report.

This document is intended to provide guidance towards setting up a composite repair workshop facility

Detail specification for T700S-12K-50C/#2511 Plain Weave Fabric

This standard establishes the requirements for the manufacturing of a Finished Goods Feedstock from receipt of Raw Feedstock Lot for continuous fiber-reinforced materials. It does not establish implementation.

This slash sheet establishes the requirements for the manufacturing of a Finished Goods Feedstock from receipt of Raw Feedstock Lot. It does not establish implementation. The Finished Goods Feedstock detailed in this document is Carbon Fiber FR-ATM (T300 1K tow), a Type 1 Form 1 PACF50FR05 filament. Carbon Fiber FR-A cannot be used on its own and is intended to be used with Onyx FR-A

This specification will establish the minimum requirements for Laser Sintering feedstock to be used in conjunction with the Laser Sintering process specification for fabricating LS parts. The Laser Sintering part (with/without subsequent processing) may be used for, but not limited to, aerospace applications. This specification outlines the minimum technical and documentation requirements for Laser Sintering materials.

This specification establishes the requirements for the production of reliable, repeatable, reproducible aerospace parts by fused filament fabrication with continuous fiber reinforcement. This specification establishes the requirements to approve new machines, processes, and materials. Specifically, this specification covers the constituent material, the configuration of the machine, operating software, machine calibration, build parameters, and acceptance criteria and testing methodology required to create aerospace parts. This specification also defines the user’s responsibility for following the specified requirements.

This specification establishes the requirements for the production of reliable, repeatable, reproducible aerospace parts by fused filament fabrication with continuous fiber reinforcement. This specification establishes the requirements to approve new machines, processes, and materials. Specifically, this specification covers the constituent material, the configuration of the machine, operating software, machine calibration, build parameters, and acceptance criteria and testing methodology required to create aerospace parts. This specification also defines the user’s responsibility for following the specified requirements.

This specification will establish the critical controls and requirements for the production of reliable, repeatable, reproducible aerospace parts by Laser Sintering fabrication but is not limited to such application. This procedure will establish guidelines that users shall follow to approve new machines, processes, and materials. Specifically, this specification covers the configuration of the machine, operating software, machine calibration, machine and build parameters, and testing methodology required to create high performance aerospace parts. This specification also outlines the user’s responsibility for following the established guidelines and documentation requirements

This specification establishes the requirements for the manufacturing of a Finished Goods Feedstock from receipt of Raw Feedstock Lot. The Finished Goods Feedstock detailed in this document is Onyx FR-A, a Type 1 Form 1 PACF15FR15 filament.

This slash sheet is used in conjunction with the AM Polymer base specification AMS 7100 and provides the unique and specific process information for the Onyx FR-A processes using the Markforged X7 Machine