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Items (212,795)

02/07/2025

This SAE Recommended Practice establishes recommended procedures for the issuance, assignment, and structure of Identification Numbers on a uniform basis by states or provinces for use in an Assigned Identification Number (AIN).

VIN - WMI Technical Committee

ACCESSORY, COVER, PROTECTIVE, PLUG CONNECTOR, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING (SERIES 2)

AS81511/17A (Current)02/07/2025

AE-8C1 Connectors Committee

REPAIR SLEEVE, PRIMARY WIRE INSULATION DAMAGE, ELECTRIC, PERMANENT, ENVIRONMENT RESISTANT, 150 °C MAXIMUM OPERATING TEMPERATURE

AS6224/1A (Current)02/07/2025

AE-8C2 Terminating Devices and Tooling Committee

Guidance for Assessing the Damage Detection Capability of Structural Health Monitoring Systems

ARP6821 (Current)

02/07/2025

This document contains information and guidance necessary for the development of a representative, repeatable validation program that may be utilized to assess the capability of SHM systems. The nature of SHM data differs from that seen in traditional nondestructive evaluation (NDE) applications in that the position of SHM sensors is fixed and SHM data can be available much more frequently (if not continuously) over time. This document presents methodologies that can be used to arrive at SHM capability while considering the unique nature of SHM deployment. Each SHM system must be considered independently to determine the applicability and limitations of the guidance contained here for each SHM system being assessed.

Aerospace Industry Steering Committee on Structural Health

Design Considerations for Enclosed Turboshaft Engine Test Cells

AIR4989A (Current)

11/21/2018

This SAE Aerospace Information Report (AIR) developed by a broad cross section of personnel from the aviation industry and government agencies is offered to provide state-of-the-art information for the use of individuals and organizations designing new or upgraded turboshaft engine test facilities.

EG-1E Gas Turbine Test Facilities and Equipment

Electronic Propulsion Control/Aircraft Interface Control Documents

ARP4874A (Current)08/29/2013

This SAE Aerospace Recommended Practice (ARP) provides guidelines for the format and content of documents defining the interface between electronic propulsion control systems and aircraft systems. The scope includes civilian aircraft powered by turbofan, turboprop, and turboshaft engines equipped with electronic engine controls.

E-36 Electronic Engine Controls Committee

Design and Safety Criteria for Passenger Boarding Stairways

AIR6133 (Current)

09/21/2018

AGE-3 Aircraft Ground Support Equipment Committee

Gas Turbine Jet Exhaust Noise Prediction

ARP876F (Current)

01/05/2021

ARP876 is intended to provide specific recommended procedures for the prediction of gas turbine jet exhaust system noise sources. Procedures are issued as separate sections, to allow for future updating as additional methods, consistent with state-of-the-art, become available.

A-21 Aircraft Noise Measurement Aviation Emission Modeling

Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C)

AS83819 (Current)

08/23/2018

This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 1400 cpm (15 fpm). The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.

ACBG Plain Bearing Committee

Airline Tow Tractor - Baggage/Cargo Factors for Design Consideration

AIR1316B (Current)

09/27/2018

This document outlines the functional and design requirements for baggage/cargo tow tractors used for airline services.

AGE-3 Aircraft Ground Support Equipment Committee

Passageway Door Operation

ARP499C (Current)

09/19/2013

The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide recommendations which will lead to the standardization of passageway door operation in all transport aircraft, by providing in the design, features which will result in minimum exit passage blockage and jamming.

S-9B Cabin Interiors and Furnishings Committee

Aerospace - Impulse Testing of Hydraulic Components

ARP1383C (Current)

02/24/2020

This SAE Aerospace Recommended Practice (ARP) defines impulse test procedures that are recommended for hydraulic components.

A-6 Aerospace Actuation, Control and Fluid Power Systems

Aircraft Crash Axes

AIR5401A (Current)

09/19/2013

This SAE Aerospace Information Report (AIR) provides information demonstrating the need for establishing design and performance standards for aircraft crash axes.

S-9A Safety Equipment and Survival Systems Committee

CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-28748/9 CONNECTORS)

AS39029/36B (Current)07/24/2018

AE-8C1 Connectors Committee

SWITCH, TOGGLE, MAGNETIC HOLD-IN SPDT

AS55941/1A (Current)04/20/2013

AE-7P Protective and Control Devices

ADAPTER, ASSEMBLY - PORT CONNECTION RING LOCKED TO 60° FLARELESS TUBE END, METRIC

MA2119B (Current)

04/09/2013

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

BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 300 CPM (13 FPM) OSCILLATION, -65 TO +160 °F, LINERS LESS THAN .015 INCH THICK

AS82819/1 (Current)08/23/2018

ACBG Plain Bearing Committee

Safe Carriage of Impaired and Disabled Passengers

AIR1815A (Current)04/04/2013

This AIR defines the major groups of impairments and disabilities among passengers who use aircraft as a transportation mode, and the types of safety problems which might be associated with each impairment. These impairments, and their safety-related problems, should be considered when referring to ARP's related to the design of cabin furnishings and equipment.

S-9B Cabin Interiors and Furnishings Committee

SWITCH, TOGGLE, MAGNETIC HOLD-IN, DP3T

AS55941/3A (Current)04/20/2013

AE-7P Protective and Control Devices

Introduction to Pressure Suite Assemblies

AIR1103 (Current)09/01/1980

AC-9 Aircraft Environmental Systems Committee

Requirements for Alternative Coatings Used in Lieu of Nickel-Chromium Plating for Aerospace Hand Tools

ARP5130A (Current)02/03/2009

This SAE Aerospace Recommended Practice (ARP) covers the requirements for alternative coatings used in lieu of nickel-chromium plating and the surface finish requirements for aerospace hand tools. It is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances.

EG-1B Hand Tools Committee

Verification of Landing Gear Design Strength

AIR1494B (Current)04/13/2010

Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear. An industry survey was recently conducted to determine just what analysis and testing are currently being applied to landing gear. Timing in relation to first flight of new aircraft was also questioned. Opinions were solicited from designers of the following categories and/or types of aircraft: a. military - large land based (bomber); b. mililtary - small land based (fighter); c. military - carrier based (Navy); d. military - helicopter (large); e. military - helicopter (small-attack); f. commercial - large (airliner); g. commercial - small (business); and h. USAF (WPAFB) - recommendations. It is the objective of this AIR to present a summary of these responses. It is hoped that this summary will be useful to designers as a guide and/or check list in establishing criteria for landing gear analysis and

A-5B Gears, Struts and Couplings Committee

CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 3B (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)

AS85049/27B (Current)11/14/2019

AE-8C1 Connectors Committee

PUMPS, HYDRAULIC, POWER DRIVEN, VARIABLE DELIVERY COMPOSITE OUTLINE DRAWINGS

AIR45 (Current)

09/30/2000

Outline drawings from all known pump manufacturers for the various size pumps listed in MIL-P-7740 were requested and those received have been combined to make up the various outline drawings. There has been prepared a composite outline drawing enclosing all of the individual outline drawings. Since the pump manufacturers' drawings will change over a period of time and complete detail is not shown, it is not possible to make a detailed mockup of any specific pump. These drawings are intended to provide information concerning the general space requirement for variable delivery pumps, and could be used to manufacture a composite mockup to indicate roughly the space required on a new engine design.

A-6C4 Power Sources Committee

Aerospace Selected Diameter - Pitch Combinations of Metric 60° Screw Threads for Shaft or Bearing Retaining Screw Threads

AS1421A (Current)

11/16/2010

This Aerospace Standard establishes the diameter - pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module shaft or bearing retaining screw threads.

E-25 General Standards for Aerospace and Propulsion Systems

HOSE ASSEMBLY, METAL - MEDIUM PRESSURE, FLARELESS, WELDED, 45° TO 90°

AS140G (Current)

10/30/2014

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

HOSE ASSEMBLY, METAL - MEDIUM PRESSURE, FLARELESS, WELDED, STRAIGHT TO 45°

AS137G (Current)

10/29/2014

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

HOSE ASSEMBLY, LINED SILICONE, 125 PSI, FLARELESS, POTABLE WATER, STRAIGHT TO STRAIGHT

AS4469B (Current)

01/07/2013

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

Issues and Concerns Associated With Electronic Propulsion Control System Partitioning

AIR4366A (Current)08/23/2007

This SAE Aerospace Information Report (AIR) enumerates areas of concern which need to be addressed when the aircraft propulsion control system functions are distributed. Distributed items may include electronic control sensors, electrical or hydraulic power sources, computer hardware and software, etc. This report identifies many factors which should be considered to determine the best system architecture for any given application.

E-36 Electronic Engine Controls Committee

CONNECTOR ACCESSORIES, ELECTRICAL, BACKSHELL, NONENVIRONMENTAL, STRAIGHT, NON-SELF-LOCKING AND SELF-LOCKING, CATEGORY 3B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)

AS85049/31B (Current)11/14/2019

AE-8C1 Connectors Committee

Tire Pressure Monitoring Systems (TPMS) for Aircraft

ARP6137 (Current)

09/18/2020

A tire pressure monitoring system (TPMS) is a means to electronically measure and report the current tire pressure. Some systems are capable of transmitting the information to the flight deck while other systems are for use on the ground by maintenance personnel (only). This SAE Aerospace Recommended Practice (ARP) document is intended to establish overall component and system function guidelines and minimum performance levels for a TPMS. The system should visually indicate the tire inflation pressure status. These guidelines include, but are not limited to: a) Design recommendations for system components, which: 1 monitor tire inflation, and, 2 are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment. b) Recommended performance and safety guidelines for a TPMS.

A-5 Aerospace Landing Gear Systems Committee

The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing

AIR1706C (Current)01/08/2010

This document has been declared “CANCELLED” as of January 2010. By this action, this document will remain listed in the Numerical Section of the Aerospace Standards Index.

AC-9 Aircraft Environmental Systems Committee

FERRULE, COUPLING, RIGID, FIXED CAVITY THREADED, FERRULE TYPE TUBE ENDS

AS1737C (Current)

01/19/2015

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

Measurement Uncertainty and Consumer Risk

AIR6553 (Current)

02/03/2020

This document addresses measurement uncertainty and consumer risk as they relate to AS8879 thread inspection. It describes the rationale, theory and methodology used to generate the technical content of the AS5870. The document describes how to calculate measurement consumer risk. It documents all of the calculation methods which industry employs today to calculate what is commonly called measurement uncertainty (Appendices A, B, C, D, E and F). These, in turn, are used to calculate measurement uncertainty ratios which are required inputs to calculate measurement consumer risk. Users of this document can apply the information described herein for the evaluation of the capability of their measurements based on the measurement consumer risk. It involves the analysis of the measurement (product) distribution and biases of both the product and measurement system distributions. It protects the consumer from the worst case distribution results.

E-25 General Standards for Aerospace and Propulsion Systems

Accommodation for Passengers with Ambulatory Disabilities in Transport Category Aircraft Cabins with Seating Capacities Greater than 44

ARP4387B (Current)12/18/2009

The methods and designs presented herein shall not be construed as being the only means of accomplishing these accommodations. This document applies to all transport category aircraft using features required by Department of Transportation Regulations CFR382. Passengers with ambulatory disabilities for whom provisions shall be made on each airplane type and location(s) for their seating are defined in 14CFR382. The goal is to provide cabin service comparable to that available to other travelers without jeopardizing the safety of fellow passengers. This necessitates consideration of physical, neurological and sensory capabilities, and limitations of mobility impaired persons. With proper consideration and design implementation, it will be possible to serve the needs of the majority of the disabled population.

S-9B Cabin Interiors and Furnishings Committee

Modeling and Simulation Capabilities for Aerospace WDM LAN Applications

AIR6006 (Current)

10/08/2024

This document provides an overview of currently available and need to be developed modeling and simulation capabilities required for implementing robust and reliable Aerospace WDM LAN applications.

AS-3 Fiber Optics and Applied Photonics Committee

General Requirements for WDM Backbone Networks

AIR6005 (Current)

10/07/2024

This document (AIR6005) provides the framework for the specifications of a WDM OBN within the SAE AS5659 WDM LAN Specification document family, in particular, the Transparent Optical Backbone Network Specification. This framework includes potential requirements, technical background, investigation and context to support the writing of SAE’s WDM LAN specifications documents. The SAE’s AS6005 WDM OBN document describes a transparent optical network which contains optical components and optical interfaces to perform optical transport, optical add/drop, optical amplification, optical routing, and optical switching functions. The conforming optical signal interfaces for the data plane of the WDM OBN are defined. The conforming signal interfaces for the control and management planes of this network are also defined. The control and management plane signals may be either electrical or optical. If successful, a WDM LAN standard is anticipated to include multiple variants that may get created

AS-3 Fiber Optics and Applied Photonics Committee

HOSE ASSEMBLY, METAL - MEDIUM PRESSURE, FLARELESS, WELDED, 45° TO 45°

AS139G (Current)

10/30/2014

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

Flexure Fatigue Strength of Tube Fitting Joints

AIR1418B (Current)

05/06/2020

This SAE Aerospace Information Report (AIR) presents flexure fatigue strength of tube fitting joints in the form of graphs showing applied deflection D and total calculated axial stress S versus number of cycles to failure N. The graphs have been prepared from data obtained by actual testing conducted in accordance with ARP1185.

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