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Items (206,858)

Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, 125 ksi (862 MPa) Tensile Strength

AMS6361H (Current)

05/09/2024

This specification covers aircraft-quality, low-alloy steel in the form of round, seamless tubing

AMS E Carbon and Low Alloy Steels Committee

Engine Oil Viscosity Classification

J300_202405 (Current)

05/09/2024

This SAE Standard defines the limits for a classification of engine lubricating oils in rheological terms only. Other oil characteristics are not considered or included

Fuels and Lubricants TC 1 Engine Lubrication

Combined Cornering and Braking Test for Truck and Bus Tires

J2675_202405 (Current)

05/09/2024

This SAE Recommended Practice describes a test method for determination of heavy truck (Class VI, VII, and VIII) tire force and moment properties under combined cornering and braking conditions. The properties are acquired as functions of slip angle, normal force, and slip ratio. Slip angle and normal force are changed incrementally using a sequence specified in this document. At each normal force and slip angle increment, the slip ratio is continually changed by application of a braking torque ramp. The data are suitable for use in vehicle dynamics modeling, comparative evaluations for research and development purposes, and manufacturing quality control. This document is intended to be a general guideline for testing on an ideal machine. Users of this recommended practice may modify the recommended protocols to satisfy the needs of specific use-cases, e.g., reducing the recommended number of test loads and/or pressures for benchmarking purposes. However, due care is necessary when

Truck and Bus Tire Committee

Nuts, Self-Locking, UNS N07001 730 °C, 1100 MPa, and 1210 MPa Procurement Specification for, Metric

MA1943C (Current)

05/09/2024

This procurement specification covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) types of nuts made from a corrosion and heat-resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Tension height nuts having overall length of threaded portion not less than 1.2 times the nominal thread diameter have 1210 MPa minimum tensile strength at room temperature. Shear height nuts having shorter threaded portion have 1100 MPa minimum tensile strength at room temperature. Maximum test temperature of parts is 730 °C

E-25 General Standards for Aerospace and Propulsion Systems

Machine Requalification Considerations for Fusion-Based Metal Additive Manufacturing

ARP7064 (Current)

05/09/2024

This document defines a recommended practice for addressing metal additive manufacturing (AM) machine requalification for all fusion-based metal AM machines. In general, this applies to powder bed fusion (PBF) and wire- or powder-fed directed energy deposition (DED) technologies. Plasma, electron beam, or lasers are applicable energy source(s

AMS AM Additive Manufacturing Metals

ARP5879A (Current)

05/09/2024

This SAE Aerospace Recommended Practice (ARP) provides recommended test requirements for electrohydrostatic actuators (EHAs

A-6B2 Electrohydrostatic Actuation Committee

J3350_202405 (Current)

05/09/2024

This SAE Standard describes the methods for testing flexible harness coverings for use on ground vehicle electrical distribution systems, specifically protection from severe mechanical impact. This SAE Standard shall apply to all tapes, extruded tubes, and textile sleeves used for this purpose

Harness Covering Standards Committee

Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form

AS7250E (Current)

05/09/2024

This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F

E-25 General Standards for Aerospace and Propulsion Systems

Aircraft Tire-to-Wheel Performance Characteristics

ARP5507A (Current)

05/09/2024

This SAE Aerospace Recommended Practice (ARP) defines the performance criteria and validation for tire circumferential movement on the rim, in the laboratory, by a static test, as well as a performance assessment in service. This document is applicable to braked wheel positions using both bias ply and radial aircraft tires

A-5C Aircraft Tires Committee

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance

ARP1947D (Current)

05/09/2024

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa

AMS D Nonferrous Alloys Committee

Nickel Alloy, Corrosion- and Heat-Resistant Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Solution Heat Treated, Precipitation Hardenable

AMS5582H (Current)

05/09/2024

This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness

AMS F Corrosion and Heat Resistant Alloys Committee

Cyber-Physical Systems Security Engineering Plan (CPSSEP

JA7496_202206 (Current)

06/02/2022

This SAE Standard establishes practices to: a Manage risk and ensure security of a cyber-physical system (CPS) throughout its life cycle by utilizing systems engineering principles; b Assess the impact of cyber-physical systems security (CPSS) objectives and requirements; c Assess the security risks to CPS technical effectiveness and functions, and address weaknesses and vulnerabilities; d Address various domains of consideration (see 3.1) that take into account operating conditions of the system, command and control, configuration management (refer to SAE EIA649), etc., that could negatively impact CPSS or CPS-designed purpose; e Perform design validation and verification to assess security and risk of the CPS

G-32 Cyber Physical Systems Security Committee

Laser Powder Bed Fusion Process

AMS7003A (Current)

08/05/2022

This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications

AMS AM Additive Manufacturing Metals

Opportunities, Challenges, and Requirements for Use of Blockchain in Unmanned Aircraft Systems Operating Below 400 Feet Above Ground Level for Commercial Use

AIR7356 (Current)

01/25/2023

This SAE Aerospace Information Report (AIR) focuses on opportunities, challenges, and requirements in use of blockchain for Unmanned Aircraft Systems (UAS) operating at and below 400 feet above ground level (AGL) for commercial use. UAS stakeholders like original equipment manufacturers (OEMs), suppliers, operators, owners, regulators, and maintenance repair and overhaul (MRO) providers face many challenges in certification, airspace management, operations, supply chain, and maintenance. Blockchain—defined as a distributed ledger technology that includes enterprise blockchain—can help address some of these challenges. Blockchain technology is evolving and also poses certain concerns in adoption. This AIR provides information on the current UAS challenges and how these challenges can be addressed by deploying blockchain technology along with identified areas of concern when using this technology. The scope of this AIR includes elicitation of key requirements for blockchain in UAS across

G-31 Digital Transactions for Aerospace

Unmanned Systems (UxS) Control Segment (UCS) Architecture: UCS Architecture Model

AS6518B (Current)

03/16/2022

This brief User Guide recaps the content of the AS6518B UCS Architectural Model. The purpose of the UCS Architecture Model is to provide the authoritative source for other models and products within the UCS Architecture as shown in the AS6512B UCS Architecture: Architecture Description

AS-4UCS Unmanned Systems Control Segment Architecture

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe Solution Heat Treated, Precipitation Hardenable to 155 ksi (1069 MPa) Tensile Strength

AMS5582G (Current)

01/18/2019

This specification covers a precipitation hardenable, corrosion and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness (see 8.5

AMS F Corrosion and Heat Resistant Alloys Committee

Titanium Alloy Bars, Forgings, and Flash-Welded Rings, 5Al - 2.5V - 4Sn - 1Co - 0.8Fe Annealed

AMS6903 (Current)

04/25/2024

This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up through 12.000 inches (304.80 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings. Bars, forgings, and flash-welded rings with a nominal thickness of 3.000 inches (79.20 mm) or greater shall have a maximum cross-sectional area of 113 square inches (729 cm2) (see 8.5

AMS G Titanium and Refractory Metals Committee

AGS3501 Connector 3/8" UNF. with Female Cone

AGS3501-2 (Current)

05/22/1970

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AS6598 Switch Body : Pilot's Control Wheel

AS6598-2 (Current)

08/03/1956

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AS3154 Insertion Tube - Switch Body Pilot's Control Wheel

AS3154-2 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

Heavy-Duty Circuit Breakers

J1625_201305 (Current)

05/03/2013

This SAE Recommended Practice defines the test conditions, procedures, and performance requirements for circuit breakers in ratings from 50 to 200 A. The document covers externally mounted automatic reset and manually reset types of circuit breakers for low voltage DC operation (typically 50 V or less

Truck and Bus Electrical Systems Committee

AS3132 Locking Plate - Switch Lever

AS3132-2 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

TS334 Test for Electrical Connectors Fluid Resistance Test

TS334-2 (Current)

10/01/1987

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AS3153 Insertion Tube Switch Body Pilot's Control Wheel

AS3153-2 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AGS1670 Cleat, Wiring, Aluminium, No. 9

AGS1670-3 (Current)

11/12/1940

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AS41092 Cable Assembly, Retaining

AS41092-9 (Current)

12/01/1996

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AS6593 Switch Contact Screw for Pilot's Control Wheel

AS6593-1 (Current)

08/03/1956

No scope available

Engine and Airframe Technical Standards Committee (TSC)

RS310 5.750" P.C. Dia. Starter Mounting Flange

RS310-1 (Current)

05/10/1948

No scope available

Engine and Airframe Technical Standards Committee (TSC)

FASTENER, ELECTRONIC EQUIPMENT, POSITIVE SELF-LOCKING

AS85731/1B (Current)

12/20/2015

SCOPE IS UNAVAILABLE

AE-8C2 Terminating Devices and Tooling Committee

AS3146 Switch Lever. Auto Pilot's Switch. Pilot's Control Wheel

AS3146-1 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

Software Life Cycle Processes – Implementation Considerations

IEEEEIA12207_2 (Current)

06/16/2016

This guide provides implementation consideration guidance for the normative clauses of IEEE/EIA 12207.0. The guidance is based on software industry experience with the life cycle processes presented in IEEE/EIA 12207.0

Systems Management Council

Automation Bulletin No. 3

EIAAB3D (Current)

06/16/2016

Systems Management Council

ESC53 Bush (Cable Support), Connector Accessory

ESC53-4 (Current)

11/01/1993

This drawing specifies parts ESC53-1, ESC53-10, ESC53-11, ESC53-12, ESC53-13, ESC53-14, ESC53-15, ESC53-2, ESC53-20, ESC53-21, ESC53-22, ESC53-23, ESC53-24, ESC53-25, ESC53-26, ESC53-27, ESC53-28, ESC53-29, ESC53-3, ESC53-30, ESC53-31, ESC53-32, ESC53-33, ESC53-34, ESC53-35, ESC53-36, ESC53-37, ESC53-38, ESC53-39, ESC53-4, ESC53-40, ESC53-41, ESC53-42, ESC53-43, ESC53-44, ESC53-45, ESC53-46, ESC53-5, ESC53-50, ESC53-51, ESC53-52, ESC53-53, ESC53-54, ESC53-55, ESC53-56, ESC53-57, ESC53-58, ESC53-59, ESC53-6, ESC53-60, ESC53-61, ESC53-62, ESC53-63, ESC53-64, ESC53-65, ESC53-66, ESC53-67, ESC53-68, ESC53-69, ESC53-7, ESC53-70, ESC53-71, ESC53-72, ESC53-73, ESC53-74, ESC53-75, ESC53-76, ESC53-77, ESC53-78, ESC53-8, and ESC53-9. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org

Engine and Airframe Technical Standards Committee (TSC)

Network End-to-End Data Link Evaluation System Transceiver Health Monitoring

AIR6552/3 (Current)

12/22/2020

This document establishes methods to obtain, store, and access data about the health of a fiber optic network using commercial sensors located in or near the transceiver. This document is intended for: Managers, Engineers, Contracting Officers, Third Party Maintenance Agencies, and Quality Assurance

AS-3 Fiber Optics and Applied Photonics Committee

AS6614 Base for Pitot Drain

AS6614-2 (Current)

08/03/1956

No scope available

Engine and Airframe Technical Standards Committee (TSC)

INSTALLING AND REMOVAL TOOLS, CONNECTOR, ELECTRICAL CONTACT, TYPE III, CLASS 1, COMPOSITION B

AS81969/16 (Current)

08/17/2020

AE-8C2 Terminating Devices and Tooling Committee

School Bus Stop Arm Lamp

J1133_201507 (Current)

07/08/2015

This document provides design guidelines, test procedure references, and performance requirements for stop arm lamp devices on school bus vehicles which are used to alert traffic to stop when passengers are loading and unloading

Emergency Warning Lights and Devices Standards Committee

CONNECTOR, RECEPTACLE, JAM NUT MOUNT, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, INDIVIDUAL RELEASE, CRIMP TYPE CONTACTS (CLASS A, F, AND W - SERIES 3

AS81511/49A (Current)

04/21/2020

AE-8C1 Connectors Committee

Starter Battery Identification and Classification

J2981_201605 (Current)

05/26/2016

To provide the industry with the means to apply a set of rules for identifying and providing a common numbering system for lead acid starting batteries

Starter Battery Standards Committee

ACCESSORY ENVELOPE FOR 8" NOMINAL DIAMETER GENERATORS

ARP551A (Current)

07/15/1958

AE-7 Aerospace Electrical Power and Equipment Committee

AS3306 Locking Plate - Switch Lever

AS3306-2 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

ESC66 Backshell, Assembly, 90° RFI / EMI Cone Grounding, Anti Decoupling. (MS 3155 Connector Interface MOD

ESC66-3 (Current)

09/01/1991

This drawing specifies parts ESC66-08, ESC66-10, ESC66-12, ESC66-14, ESC66-16, ESC66-18, ESC66-20, ESC66-22, ESC66-24, and ESC66-28. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org

Engine and Airframe Technical Standards Committee (TSC)

AS3061 Switch Assembly Pilot's Control Wheel

AS3061-1 (Current)

02/26/1951

No scope available

Engine and Airframe Technical Standards Committee (TSC)

Information on Brake-By-Wire (BBW) Brake Control Systems

AIR5372A (Current)

10/25/2019

This SAE Aerospace Information Report (AIR) describes the design approaches used for current applications of aircraft Brake-by-Wire (BBW) control systems. The document also discusses the experience gained during service, and covers system, ergonomic, hardware, and development aspects. The document includes the lessons that have been learned during application of the technology. Although there are a variety of approaches that have been used in the design of BBW systems, the main focus of this document is on the current state of the art systems

A-5A Wheels, Brakes and Skid Controls Committee

Electrical Propulsion Control - Off-Road Dumpers

J1299_201302 (Current)

02/21/2013

This SAE Information Report applies to the control circuits and devices associated with the electrical propulsion system used on electric drive dumpers. Dumper is defined in J/ISO 6165. The document does not apply to auxiliary equipment control systems such as: a Battery charging systems b Engine wiring and control c Monitoring and control circuits not directly affecting the operation of the electric propulsion and retarding system d Lighting e Accessory systems (heating, air conditioning, horns, radios, emergency steering, fire protection, and similar functions

CTTC C2, Electrical Components and Systems

ITS Data Bus—IDB-C Physical Layer

J2366/1_200111 (Current)

11/27/2001

This SAE Recommended Practice details the Physical Layer of the Intelligent Transportation Systems (ITS) Data Bus on CAN (IDB-C), which is generally intended for in-vehicle use. It has been developed by the ITS Data Bus (IDB) Physical Layer Subcommittee of the IDB Committee. The objectives of the subcommittee are to develop information reports, recommended practices and standards concerned with the requirements, design, and usage of devices that communicate electronic signals and control information among ITS related components within the vehicle environment. The IDB-C is a non-proprietary virtual-token passing bus, designed to allow disparate consumer, vehicle, and commercial electronic components to communicate and share information across a standard, open data bus. This document describes the Physical Layer of the IDB-C, as shown in Figure 1. The Physical Layer of the IDB-C incorporates the CAN 2.0B specification per SAE J2284-2, with modifications as noted in this document. The IDB

ITS Council

ESC74 Backshell, Assembly, 45° RFI / EMI Cone Grounding, Anti - Decoupling. (MS 3155 Connector Interface MOD

ESC74-1 (Current)

11/01/1991

This drawing specifies parts ESC74-08, ESC74-10, ESC74-12, ESC74-14, ESC74-16, ESC74-18, ESC74-20, ESC74-22, ESC74-24, and ESC74-28. To view suppliers qualified to manufacture this part, visit https://ts200.sae-itc.org

Engine and Airframe Technical Standards Committee (TSC)

TS355 Test for Electrical Connectors Contact Deformation after Crimping

TS355-1 (Current)

10/01/1987

No scope available

Engine and Airframe Technical Standards Committee (TSC)

AGS1663 Cleat, Wiring, Porcelain

AGS1663-3 (Current)

12/03/2015

No scope available

Engine and Airframe Technical Standards Committee (TSC)

INSERT ARRANGEMENTS, AS81582 CONNECTORS, UMBILICAL

AS16721 (Current)

11/07/2018

AE-8C1 Connectors Committee

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