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This specification covers a low-carbon steel in the form of wire up to 0.249 inch (6.32 mm), inclusive, supplied as coils of wire or, when specified, as straight lengths
AMS E Carbon and Low Alloy Steels Committee
This specification covers bonded honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered (see 8.5
AMS D Nonferrous Alloys Committee
This specification covers an aircraft-quality, corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate 1.000 inch (25.40 mm) and under in nominal thickness
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Information Report (AIR) has been compiled to provide information on: a The particularities of EHAs and their derivatives that make their implementation useful to meet some specific system requirements, solve some system architecture issues, or provide system optimization within the flight control actuation and hydraulic generation/distribution perimeter b System architecture drivers and basic schematic diagrams, actuator principle schematic diagrams, and basic characteristics, for various civil and military aircraft
A-6B2 Electrohydrostatic Actuation Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This SAE Recommended Practice is intended for use in testing and evaluating the approximate performance of engine-driven cooling fans. This performance would include flow, pressure, and power. This flow and pressure information is used to estimate the engine cooling performance. This power consumption is used to estimate net engine power per SAE J1349. The procedure also provides a general description of equipment necessary to measure the approximate fan performance. The test conditions in the procedure generally will not match those of the installation for which cooling and fuel consumption information is desired. The performance of a given fan depends on the geometric details of the installation, including the shroud and its clearance. These details should be duplicated in the test setup if accurate performance measurement is expected. The performance at a given air density and speed also depends on the volumetric flow rate, or the pressure rise across the fan, since these two
Cooling Systems Standards Committee
The supplier shall use the following process to respond to a customer request for corrective and preventive action
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This standard defines the minimum requirements for conducting Measurement Systems Analysis (MSA) for variable and attribute assessment on characteristics as defined on the drawing or specification. It does not define the detailed analytical methods for each type of study as these can be found in existing published texts (see Section 2 for guidance
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, and forging stock
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers the requirements for electrodeposition of tin on metals and the properties of the deposit
AMS B Finishes Processes and Fluids Committee
This set of criteria is intended for use by accredited Certification Bodies (CBs) to establish compliance and grant certification to AS6081A. It may also be used by others to assess compliance to AS6081A requirements
G-19 Counterfeit Electronic Parts Committee
This SAE Aerospace Recommended Practice (ARP) provides guidance to plan and perform validation and verification of IVHM systems. The intent of this ARP is to help the reader appreciate and understand additional objectives and activities of validation and verification processes, beyond validation and verification of the vehicle, that arise due to the nature of an IVHM System. This includes an end-to-end evaluation of the entire IVHM system, noting that IVHM is a “system of systems.” In order to perform validation and verification, the user must determine what they are using IVHM for, including the criticality of the application. The process should then determine appropriateness of the data corresponding to the application criticality. This document provides validation and verification guidance for IVHM as: (1) a system of systems, (2) a system, and (3) elements within a system. While this document is not intended to be prescriptive, it is a reference guide that highlights and discusses
HM-1 Integrated Vehicle Health Management Committee
This specification covers the requirements for an electrodeposit of cadmium diffused into an electrodeposit of nickel on carbon, low-alloy, and corrosion-resistant steels
AMS B Finishes Processes and Fluids Committee
The purpose of this SAE Recommended Practice is to establish reference standards for airflow measurements in the ranges required for testing automotive engine induction systems and to describe equipment that will facilitate the use of such standards to check the accuracy of various equipment and methods
Engine Power Test Code Committee
This standard establishes requirements for Process Control Methods to sustain product conformity. This includes training, selection of control methods, analysis and improvement of their effectiveness, and subsequent monitoring and control. It applies to all controls documented in the Control Plan. This will include but is not limited to Key Characteristics (KCs) and Critical Items (CIs). This standard aligns and collaborates with the requirements of AS9100, AS9103, AS9145, AS13000, AS13002, AS13003, and AS13004. Commercial-Off-The-Shelf (COTS) items and Standard Catalogue Items (that neither the customer nor supplier hold design authority for) are not included
G-22 Aerospace Engine Supplier Quality (AESQ) Committee
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
This specification covers a fluorocarbon (FKM) rubber in the form of O-rings, O-ring cord, compression seals, and molded-in-place gaskets for aeronautical and aerospace applications
AMS CE Elastomers Committee
Define a process enabling network devices to detect the baud rate of a CAN Classic network as specified by physical layers SAE J1939-11, SAE J1939-14, or SAE J1939-15. The intent is to minimize or eliminate communication disruption between existing network devices. These networks only support Classical Base Frame Format (CBFF) and Classical Extended Frame Format (CEFF) Data Frames, as defined in ISO 11898-1:2015. Baud rate detection on a SAE J1939 CAN FD network is not in scope, as SAE J1939-17 is currently the only SAE J1939 CAN FD physical layer option and specifies only one supported baud rate combination (500 kbit/s / 2000 kbit/s
Truck Bus Control and Communications Network Committee
This document establishes age limit and guidance for acceptance of hose and hose assemblies containing elastomeric materials for use in aircraft, space vehicles, missiles and component assemblies thereof at time of delivery to the contractor, procuring activity, or contracting officer. This document does not establish limitations on storage times for military/civil activities nor operating life
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This document specifically pertains to cybersecurity for road vehicles. This document encompasses the entire vehicle lifecycle of key management. It has been developed by SAE Committee TEVEES18F, Vehicle Security Credentials Interoperability (VSCI), a subcommittee of SAE Committee TEVEES18A, Vehicle Cybersecurity Systems Engineering Committee. This committee is authorized under the scope and authority fo the SAE Electronic Design Automation Steering Committee (also known as the Electronic Systems Group) that is directly under the scope and authority fo the SAE Motor Vehicle Council. The SAE Motor Vehicle Council’s stated scope of influence and authority, as defined by the SAE includes, passenger car and light truck in conjunction with ISO/SAE 21434
Vehicle Electrical System Security Committee
This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures
AMS K Non Destructive Methods and Processes Committee
This specification covers a precision cold-rolled corrosion- and heat-resistant nickel alloy in the form of sheet and strip over 0.005 to 0.015 inch (0.13 to 0.38 mm), inclusive, in nominal thickness and foil up to 0.005 inch (0.13 mm), inclusive, in nominal thickness (see 8.4
AMS F Corrosion and Heat Resistant Alloys Committee
This SAE Aerospace Information Report (AIR) provides information and guidelines on the selection and use of rotary lip seals for their expected duty cycle. Information on seal installation procedures is also included
A-6C2 Seals Committee
This SAE Standard specifies a message set, and its data frames and data elements, for use by applications that use vehicle-to-everything (V2X) communications systems
V2X Core Technical Committee
This SAE Standard was developed to provide a method for indicating the direction of engine rotation and numbering of engine cylinders. The document is intended for use in designing new engines to eliminate the differences which presently exist in industry
Engine Power Test Code Committee
This SAE Recommended Practice establishes uniform procedures for assuring the manufactured quality, installed utility, and service performance of manual automotive adaptive products, other than those provided by the OEM, intended to provide driving capability for persons with physical disabilities. These devices function as adaptive appliances to compensate for lost or reduced performance in the drivers’ arms or legs, or both. Some of the devices are designed to transfer foot functions to the hands, hand functions to the feet, or functions from one side of the body to the other. This document applies only to primary controls as defined in 3.4.1 and in the Foreword. In particular, this document is specifically concerned with those mechanical and hybrid products that are intended by the manufacturer of the adaptive product to: Be installed within the occupant space of the vehicle Be operated by a vehicle driver with a physical disability Be added to, or substituted for, the OEM vehicle
Adaptive Devices Standards Committee
This SAE Recommended Practice establishes procedure for the issuance and assignment of a World Manufacturer Identifier (WMI) on a uniform basis to vehicle manufacturers who may desire to incorporate it in their Vehicle Identification Numbers (VIN). This recommended practice is intended to be used in conjunction with the recommendations for VIN systems described in SAE J853, J187, J272, and other SAE reports for VIN systems. These procedures were developed to assist in identifying the vehicle as to its point of origin. It was felt that review and coordination of the WMI by a single organization would avoid duplication of manufacturer identifiers and assist in the identification of vehicles by agencies such as those concerned with motor vehicle titling and registration, law enforcement, and theft recovery
VIN - WMI Technical Committee
This document specifies the on-board system requirements for vehicle-to-vehicle (V2V) safety system for school buses, including functional requirements and performance requirements. The system can send the SAE J2735-defined basic safety message (BSM) over a wireless communications interface; the communications interface itself is outside the scope of this document. This document provides the specifications necessary to build interoperable systems that support V2V applications that rely on receiving BSMs from school buses
V2X Core Technical Committee
No scope available
Engine and Airframe Technical Standards Committee (TSC)
No scope available
Engine and Airframe Technical Standards Committee (TSC)
This SAE Standard covers unshielded cable, 22 gauge and larger, intended for use at a nominal system voltage up to 600 V or 1000 V (ACrms or DC). It is intended for use in surface vehicle electrical systems
Cable Standards Committee
This SAE Aerospace Recommended Practice (ARP) provides recommendations for the development of aircraft and systems, taking into account aircraft functions and operating environment. It provides practices for ensuring the safety of the overall aircraft design, showing compliance with regulations, and assisting a company in developing and meeting its own internal standards. These practices include validation of requirements and verification of the design implementation for safety, certification, and product assurance. The guidelines in this document were developed in the context of U.S. Title 14 Code of Federal Regulations (14 CFR) Part 25 and European Union Aviation Safety Agency (EASA) Certification Specification (CS) CS-25. They may be applicable in the context of other regulations, such as 14 CFR Parts 23, 27, 29, 33, and 35, and CS-23, CS-27, CS-29, CS-E, and CS-P. This document addresses the development cycle for aircraft and systems that implement aircraft and system functions. It
S-18 Aircraft and Sys Dev and Safety Assessment Committee
This SAE Aerospace Standard (AS) defines the overall requirements applicable to oxygen flow indication as required by Airworthiness Requirements of CS/FAR 25.1449 to show that oxygen is being delivered to the dispensing equipment. Requirements of this document shall be applicable to any type of oxygen system technology and encompass “traditional” pneumatic devices, as well electric/electronic indication
A-10 Aircraft Oxygen Equipment Committee
This document provides guidance for oxygen cylinder installation on commerical aircraft based on airworthiness requirements, and methods practiced within aerospace industry. It covers considerations for oxygen systems from beginning of project phase up to production, maintenance, and servicing. The document is related to requirements of DOT-approved oxygen cylinders, as well to those designed and manufactured to standards of ISO 11119. However, its basic rules may also be applicable to new development pertaining to use of such equipment in an oxygen environment. For information regarding oxygen cylinders itself, also refer to AIR825/12
A-10 Aircraft Oxygen Equipment Committee
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
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