Results

Items (212,032)

01/09/2025

This specification covers requirements for the superfinishing of High Velocity Oxygen/Fuel (HVOF) applied tungsten carbide thermal spray coatings

AMS B Finishes Processes and Fluids Committee

Aerospace - Evaluation of Particulate Contamination in Hydraulic Fluid - Membrane Procedure

ARP4285A (Current)

01/09/2025

This SAE Aerospace Recommended Practice (ARP) establishes a method for evaluating the particulate matter extracted from the working fluid of a hydraulic system or component using a membrane. The amount of particulate matter deposited on the membrane due to filtering a given quantity of fluid is visually compared against a standard membrane in order to provide an indication of the cleanliness level of the fluid

A-6C1 Fluids and Contamination Control Committee

Metallic Whiskers

AIR4129A (Current)

01/09/2025

This AIR presents an abbreviated review of the metallurgical phenomena known as whiskers. It is not all encompassing; rather, it is intended to introduce the design engineer to the technical issues of metallic whiskers, their formation, and the potentially dangerous problems they can cause

AMS B Finishes Processes and Fluids Committee

Air in Aircraft Hydraulic Systems

AIR5829 (Current)

01/09/2025

This SAE Aerospace Information Report (AIR) discusses the forms that air may take in aircraft hydraulic systems. Further, the effects of the various air forms on system operation are addressed. Recommended system design to prevent air effects and maintenance procedures to prevent and remove air are provided. Nitrogen leakage from accumulators is also a source of gas in hydraulic systems and may compose a portion of the “air” in the hydraulic system. The term “air” in this report does not differentiate between a gas composed strictly of normal atmospheric air or one that includes a mixture of additional nitrogen as well. The discussions of the report apply equally with any proportions of atmospheric air and nitrogen in the system

A-6C1 Fluids and Contamination Control Committee

Actuators, Linear Mechanical, General Specification Guide

ARP5812 (Current)

01/09/2025

This SAE Aerospace Recommended Practice (ARP) establishes design, manufacturing performance and test requirements for linear mechanical actuators intended to be used for linear motion applications in response to manual or automatic power control system inputs. It is applicable, but not confined to, ball screws, sliding contact screws, roller screws, helical splines, rack and pinion assemblies, and skewed roller actuators. It is a reference for preparing detail specifications for mechanical actuators compatible and applicable to military or commercial aircraft systems

A-6B3 Electro-Mechanical Actuation Committee

LEDs and Aircraft Applications

ARP6253A (Current)

01/09/2025

This document presents minimum criteria for the design and installation of LED assemblies in aircraft. The use of "shall" in this specification expresses provisions that are binding. Nonmandatory provisions use the term "should

A-20C Interior Lighting

INSERT, SCREW THREAD, HELICAL COIL, METRIC SERIES, FREE RUNNING, CRES, UNCOATED

MA3279D (Current)

01/09/2025

E-25 General Standards for Aerospace and Propulsion Systems

Method for Predicting Lateral Attenuation of Airplane Noise

AIR5662 (Current)

01/09/2025

This document describes analytical methods for calculating the attenuation of the level of the sound propagating from an airplane to locations on the ground and to the side of the flight path of an airplane during ground roll, climbout after liftoff, and landing operations. Both level and non-level ground scenarios may be modeled using these methods, however application is only directly applicable to terrain without significant undulations, which may cause multiple reflections and/or multiple shielding effects. This attenuation is termed lateral attenuation and is in excess of the attenuation from wave divergence and atmospheric absorption. The methods for calculating the lateral attenuation of the sound apply to: turbofan-powered transport-category airplanes with engines mounted at the rear of the fuselage (on the sides of the fuselage or in the center of the fuselage as well as on the sides) or under the wings propeller-driven transport-category or general-aviation airplanes

A-21 Aircraft Noise Measurement Aviation Emission Modeling

Test Slabs, Chloroprene (CR) 70 - 80

AMS3217/3D (Current)10/01/2021

This specification covers a standard chloroprene (CR) rubber stock in the form of molded test slabs

AMS CE Elastomers Committee

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, SPLIT, 90 DEGREE, CATEGORY 4C (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS

AS85049/65B (Current)10/06/2021

AE-8C1 Connectors Committee

CRIMPING TOOLS, TERMINAL, HAND, WIRE TERMINATION; IN-SERVICE INSPECTION GAGE FOR AS22520/41 CRIMP TOOLS

AS22520/42A (Current)12/27/2021

AE-8C2 Terminating Devices and Tooling Committee

Elastomer Compatibility Considerations Relative to Elastomer Selection

AIR786C (Current)

10/01/2021

This SAE Aerospace Information Report (AIR) contains data relative to the chemical nature of aerospace fluids and relates each to its empirical effect upon elastomeric components. Since the compatibilities of elastomers are determined by the compounding as well as the nature of the base polymer, the elastomers considered are limited to finished compounds for which material or performance specifications can be referenced

A-6C2 Seals Committee

REMOVAL TOOLS, CONNECTOR, ELECTRICAL CONTACT (TYPE CR CONNECTOR) TYPE II, CLASS 1, COMPOSITION

AS81969/6A (Current)10/06/2021

AE-8C2 Terminating Devices and Tooling Committee

BOLT, MACHINE - HEXAGON HEAD, PD SHANK, BLACK OXIDE, STEEL UNS G87400, 125 KSI MIN, .3750-24 UNJF-3A

AS9286C (Current)

10/01/2021

E-25 General Standards for Aerospace and Propulsion Systems

BEARING, ROLLER, NEEDLE, TRACK ROLLER INTEGRAL STUD, SEALED, TYPE VIII ANTIFRICTION, INCH

AS21440C (Current)

10/06/2021

ACBG Rolling Element Bearing Committee

Tungsten Carbide-Cobalt Chrome Powder Agglomerated and Sintered

AMS7882D (Current)

10/01/2021

This specification covers tungsten carbide-cobalt chrome in the form of powder

AMS F Corrosion and Heat Resistant Alloys Committee

Overview and History of Aircraft Inerting Systems

AIR1903A (Current)

10/08/2021

An airplane fuel tank inerting system provides an inert atmosphere in a fuel tank to minimize explosive ignition of fuel vapor. This SAE Aerospace Information Report (AIR) deals with the three methods of fuel tank inerting systems currently used in operational aircraft: (1) on-board inert gas generation systems (OBIGGS), (2) liquid/gaseous nitrogen systems, and (3) halon systems. The OBIGGS and nitrogen systems generally are designed to provide full-time fuel tank fire protection; the halon systems generally are designed to provide only on-demand or combat-specific protection. This document also addresses other design considerations that affect fuel tank flammability such as fuel tank pressure and other methods for reducing fuel tank flammability. This AIR does not treat the subject of explosion suppression foam (ESF) that has been used for fuel tank explosion protection on some military aircraft. ESF is also available for retrofit for commercial airplanes. The primary disadvantages of

AE-5D Fuel Tank Flammability Reduction Systems Committee

Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7651) Solution Heat Treated, Stress Relieved, and Overaged

AMS4364A (Current)

09/15/2021

This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6

AMS D Nonferrous Alloys Committee

Backup Lamp (Reversing Lamp

J593_202110 (Current)

10/06/2021

This SAE Standard provides installation requirements, test procedures, design guidelines, and performance requirements for backup/reversing lamps

Signaling and Marking Devices Stds Comm

Webbing Service Life for Occupant Restraints

ARP6073 (Current)

10/01/2021

This document applies to webbing used on occupant restraint systems in service on 14 CFR/CS part 23, part 25, part 27, and part 29 aircraft applications. The guidelines presented within this document are intended to be supplemental to the requirements supplied by the OEM in the CMM, ICA, or like document. In cases of conflict between this ARP and the OEM’s requirements, the requirements of the OEM shall be followed. The objective of this document is to establish practical guidelines to help operators in the determining if restraint webbing has reached the end of its service life. The recommendations contained herein are based on test data from in service restraint systems and the continued airworthiness guidelines recommended by restraint system OEMs

Aircraft Seat Committee

Beryllium Bars, Rods, Tubing, and Shapes, Instrument Grade

AMS7907E (Current)

12/10/2024

This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder

AMS G Titanium and Refractory Metals Committee

Lubrication Fittings

J534_202110 (Current)

10/06/2021

This SAE Standard covers complete general and dimensional specifications for the various types of lubrication fittings and related threaded components intended for general application in the automotive and allied fields

Hydraulic Tube Fittings Committee

Ferrule, Shield Terminating, Crimp Style

AS21608B (Current)

10/01/2021

This specification covers crimp style, insulated and uninsulated, shield terminating ferrules for RF cable and shielded cable

AE-8C2 Terminating Devices and Tooling Committee

Safety Alert Symbol for Agricultural, Construction, and Industrial Equipment

J284_202110 (Current)

10/01/2021

This SAE Recommended Practice covers the safety alert symbol intended for use on construction and industrial equipment as defined in SAE J1116 and on agricultural tractors and machinery as defined in ASABE S390

HFTC2, Machine Displays and Symbols

LIN Network for Vehicle Applications Conformance Test

J2602-2_202110 (Current)

10/01/2021

This document covers the tests to be performed on all SAE J2602-1 (2021 revision) devices. Tests described in this document will ensure a minimum standard level of performance to which all compatible electronic control units (ECUs) and media shall be designed. This will assure full serial data communication among all connected devices regardless of supplier. The goal of SAE J2602-2 is to improve the interoperability and interchangeability of LIN devices within a network by verifying the devices pass a minimum set of tests. To allow for easy cross-reference, this document is arranged such that the conformance test for a given section in SAE J2602-1 (2021 revision) is in the same section in SAE J2602-2. This document is to be referenced by the particular vehicle original equipment manufacturer (OEM) component technical specification that describes any given ECU in which the LIN data link controller and physical layer interface is located. Primarily, the performance of the physical layer

Vehicle Architecture For Data Communications Standards

File Structures for a Node Capability File (NCF) and LIN Description File (LDF

J2602-3_202110 (Current)

10/01/2021

This document covers the requirements for SAE implementations based on ISO 17987. Requirements stated in this document will provide a minimum standard level of performance to which all compatible systems, design and development tools, software, ECUs, and media shall be designed. This will assure consistent and unambiguous serial data communication among all connected devices regardless of supplier. This document may be referenced by any vehicle OEM component technical specification that describes any given ECU in which the single wire data link controller and physical layer interface is located. The intended audience includes, but is not limited to, ECU suppliers, LIN controller suppliers, LIN transceiver suppliers, component release engineers, and vehicle system engineers. The term “master” has been replaced by “commander” and term “slave” with “responder” in the following sections

Vehicle Architecture For Data Communications Standards

Cobalt Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 40Co - 22Cr - 22Ni - 14.5W - 0.07La Solution Heat Treated

AMS5772F (Current)

09/01/2021

This specification covers a corrosion and heat-resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings

AMS F Corrosion and Heat Resistant Alloys Committee

Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Foil 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) Cold Rolled and Annealed

AMS5879E (Current)

08/19/2021

This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and foil 0.100 inch (2.54 mm) and under in nominal thickness

AMS F Corrosion and Heat Resistant Alloys Committee

T-BOLT, A-286, 1000 °F

AS4108/1A (Current)09/01/2021

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Bolts and Screws, Steel, UNS S66286 Tensile Strength 160 ksi, Procurement Specification

AS4506C (Current)

09/01/2021

This document covers bolts and screws made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286

E-25 General Standards for Aerospace and Propulsion Systems

WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, LIGHTWEIGHT, 80 MICROINCH SILVER-COATED HIGH-STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHS

AS22759/47B (Current)08/26/2021

AE-8D Wire and Cable Committee

Silver Alloy Brazing Filler Metal 63Ag - 28.5Cu - 6.0Sn - 2.5Ni 1275 to 1475 °F (691 to 802 °C) Solidus-Liquidus Range

AMS4774H (Current)

09/01/2021

This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, and chips and a viscous mixture (paste) of powder in a suitable binder

AMS D Nonferrous Alloys Committee

Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Forging Stock, 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted, 1750 °F (954 °C) Solution Heat Treated, Welding Grade Precipitation Hardenable

AMS5895F (Current)

08/27/2021

This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings, or heading

AMS F Corrosion and Heat Resistant Alloys Committee

Gold-Palladium-Nickel Alloy, Brazing Filler Metal, High Temperature 30Au - 34Pd - 36Ni 2075 to 2130 °F (1135 to 1166 °C) Solidus-Liquidus Range

AMS4785K (Current)

08/26/2021

This specification covers a gold-palladium-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, preforms, and a viscous mixture (paste) of the powder in a suitable binder

AMS F Corrosion and Heat Resistant Alloys Committee

Steel Bars, Forgings, and Mechanical Tubing and Forging Stock 1.1Si - 1.45Cr - 1.0Mo - 0.08Al (0.16 - 0.22C) Double Vacuum Melted

AMS6255G (Current)

08/26/2021

This specification covers a premium aircraft quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock

AMS E Carbon and Low Alloy Steels Committee

Steel, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V 1800 °F (982 °C) Solution Heat Treated

AMS5525L (Current)

09/01/2021

This specification covers a corrosion and heat-resistant steel in the form of sheet, strip, and plate 0.0010 inch (0.025 mm) and above in nominal thickness (see 8.6

AMS F Corrosion and Heat Resistant Alloys Committee

688 Intersystem Network Integration

ARINC688 (Current)06/24/2021

The purpose of this document is to provide guidelines for integrating previously standalone cabin systems such as cabin management systems, In-Flight Entertainment (IFE) systems, In-Flight Connectivity (IFC) systems, galley systems, surveillance systems, etc. Resource sharing between systems can reduce airline costs and/or increase functionality. But, as systems expose their internal resources to external systems, the risk of an intrusion that could degrade function and/or negatively expose the supplier's or airline's brand increases. This document provides a recommended IP networking design framework between aircraft systems to reduce the operational security threats while still supporting the necessary intersystem routing

Airlines Electronic Engineering Committee

681 Timely Recovery of Flight Data (TRFD

ARINC681 (Current)08/06/2021

The difficulty in locating crash sites has prompted international efforts for alternatives to quickly recover flight data. This document describes the technical requirements and architectural options for the Timely Recovery of Flight Data (TRFD) in commercial aircraft. ICAO and individual Civil Aviation Authorities (CAAs) levy these requirements. The ICAO Standards and Recommended Practices (SARPs) and CAA regulations cover both aircraft-level and on-ground systems. This report also documents additional system-level requirements derived from the evaluation of ICAO, CAA, and relevant industry documents and potential TRFD system architectures. It describes two TRFD architectures in the context of a common architectural framework and identifies requirements. This report also discusses implementation recommendations from an airplane-level perspective

Airlines Electronic Engineering Committee

678 Guidance for Distributed Radio Architectures

ARINC678 (Current)07/15/2021

The purpose of this document is to evaluate Communication, Navigation, and Surveillance (CNS) Distributed Radio architectures and the feasibility of distributing the RF and systems processing sections to ensure the following: Reduce cost of equipment Reduce Size, Weight, and Power (SWaP) Ease of aircraft integration Growth capability built into the design Maintain or improve system availability, reliability, and maintainability It provides a framework to determine whether it is feasible to develop ARINC Standards that support CNS distributed radio architectures

Airlines Electronic Engineering Committee

Optical Warning Devices for Authorized Emergency, Maintenance, and Service Vehicles

J845_202108 (Current)

08/26/2021

This document provides design guidelines, test procedure references, and performance requirements for omnidirectional and selective coverage optical warning devices used on authorized emergency, maintenance, and service vehicles. It is intended to apply to, but is not limited to, surface land vehicles

Emergency Warning Lights and Devices Standards Committee

Chemical Check Analysis Limits, Titanium and Titanium Alloys

AMS2249K (Current)

12/10/2024

This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer

AMS G Titanium and Refractory Metals Committee

Tire Pressure Systems - Management (CTIS) Type for Medium- and Heavy-Duty Highway Vehicles

J2848/3_202108 (Current)08/26/2021

Truck and Bus Tire Committee

J2603_202109 (Current)

09/01/2021

This SAE Recommended Practice establishes a uniform procedure for assuring the manufactured quality, installed utility, and performance of automotive powered gas/brake controls other than those provided by the vehicle manufacturer (OEM). These products are intended to provide driving capability to persons with physical disabilities. These products function as adaptive modifications to compensate for lost or reduced function in the extremities of the driver. Powered gas/brake control systems are not only designed to transfer foot functions to the hands or from one side of the body to the other, but to supplement by power, other than by the driver’s own muscular efforts, the force output of the driver

Adaptive Devices Standards Committee

Application - Configurable Messaging

J1939/74_202108 (Current)08/26/2021

The SAE J1939 documents are intended for light, medium, and heavy-duty vehicles used on or off road as well as appropriate stationary applications which use vehicle derived components (e.g. generator sets). Vehicles of interest include, but are not limited to, on- and off-highway trucks and their trailers, construction equipment, and agricultural equipment and implements. The purpose of these documents is to provide an open interconnect system for electronic systems. It is the intention of these documents to allow Electronic Control Units to communicate with each other by providing a standard architecture. This particular document, SAE J1939-74, describes the message structure for a set of messages which enable the user to determine and announce to others on the network, the parameter placement within a particular message from the special set of messages defined within this document

Truck and Bus Control and Communications Network Committee

Performance Test for Air-Conditioned, Heated, and Ventilated Off-Road, Self-Propelled Work Machines

J1503_202109 (Current)

09/15/2021

This SAE Standard applies to off-road, self-propelled work machines used in earth moving, agriculture, and forestry as defined in SAE J1116, and establishes the following minimum performance levels in the operator's environment for the seated position

HFTC6, Operator Accommodation

Performance Standard for Passenger Smoke and Toxic Fumes Respiratory Protective Equipment

AS8048A (Current)

09/20/2021

This SAE Aerospace Standard (AS) defines the performance requirements for equipment to be used by untrained cabin occupants for protection from toxic and irritant atmospheres while on board and during evacuation of an aircraft

A-10 Aircraft Oxygen Equipment Committee

Minimum Operational and Maintenance Responsibilities for Aircraft Tire Usage

ARP5265C (Current)

09/20/2021

This SAE Aerospace Recommended Practice (ARP) sets forth criteria for the installation, inflation, inspection, and maintenance of aircraft tires and the maintenance of the operating environment to ensure the safety of support personnel and the safe operation of the aircraft

A-5C Aircraft Tires Committee

WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, NORMAL WEIGHT, 80 MICROINCH SILVER-COATED HIGH-STRENGTH COPPER ALLOY, 200 °C, 600 VOLT, ROHS

AS22759/49B (Current)09/20/2021

AE-8D Wire and Cable Committee

BOLT, MACHINE - HEXAGON HEAD, PD SHANK, BLACK OXIDE, STEEL UNS G87400, 125 KSI MIN, .2500-28 UNJF-3A

AS9284C (Current)

09/20/2021

E-25 General Standards for Aerospace and Propulsion Systems

Items per page:

1 – 50 of 212032