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Items (211,975)

Low Speed Thorax Impact Test Procedure for the HIII 50th Male Dummy

J2779_202206 (Current)

06/29/2022

Dummy Testing and Equipment Committee

Initiator Technical Requirements and Validation

06/06/2005

This specification establishes the design, performance, and validation requirements for the initiator assembly used in airbag modules, seatbelt pretensioners and/or any other Electro-Explosive Devices (EED

USCAR

450-1 Flight Simulator Design and Performance Data Requirements

ARINC450-1 (Current)09/10/2019

This document provides Flight Simulation Training Device (FSTD) operators, FSTD manufacturers, airplane manufacturers or other sources of approved data and vendors of airplane equipment, with a standard describing the scope and content of data required to build, test, and qualify FSTDs of adequate fidelity to meet flight crew training requirements

Flight Simulator Engineering and Maintenance Committee

434-2 Flight Simulation Training Device (FSTD) - Life Cycle Support

ARINC434-2 (Current)10/16/2019

This document will address measures pertaining to and directly associated with the maintainability and reliability of FSTDs throughout their entire life cycle, from initial specification and design to de-commissioning. Although the primary emphasis of this document is on full flight simulators (with motion and visual systems), it should be applicable in part or total to all FSTDs

Flight Simulator Engineering and Maintenance Committee

429P2-17 Digital Information Transfer System (DITS), Part 2, Discrete Word Data Standards

ARINC429P2-17 (Current)08/01/2019

This standard defines the air transport industry's standards for the transfer of digital data between avionics system elements. Part 2 provides the formats of data words with discrete bit encoding

Airlines Electronic Engineering Committee

Automated Gaseous Nitriding Controlled by Nitriding Potential

AMS2759/10D (Current)12/18/2024

This document specifies the procedure and requirements for nitriding steel parts in a process automatically controlled by the nitriding potential (see 2.3.6

AMS B Finishes Processes and Fluids Committee

Steel, Sheet and Strip, 0.25 Carbon, Maximum (SAE 1020), Hard Temper

AMS5045L (Current)12/18/2024

This specification covers a carbon steel in the form of sheet and strip

AMS E Carbon and Low Alloy Steels Committee

Ergonomic Guidelines for Small Lot Delivery Operations

USCAR42 (Current)

03/10/2015

This document describes the design, assessment methods and physical requirements associated with material handling systems. This would include, but not limited to manual dollies, small lot systems and kitting. All possible designs and applications could not be anticipated in creating these guidelines. Where there are questions of adherence to this document, such as use of an “off-the shelf” design, always consult the responsible Ergonomics Department

USCAR

807-4 Fiber Optic Training Requirements

ARINC807-4 (Current)01/10/2019

This document is based upon the SAE ARP5602 document, A Guideline for Aerospace Platform Fiber Optic Training and Awareness Education. ARINC Report 807: Fiber Optic Training Requirements is a subset of the SAE ARP5602 document designed to meet the requirements of the commercial air transport industry. Certification to the SAE ARP5602 document fulfills the requirements of ARINC Report 807. This document defines recommended general practices for training requirements of aerospace fiber optic systems. It is the intention of this document to outline proven training practices and general standards of workmanship for technicians engaged in aerospace fiber optic manufacturing, installation, maintenance, and repair for the air transport industry. It is also recommended that management and purchasing personnel receive fundamental training to familiarize themselves with the requirements of aerospace fiber optics

Airlines Electronic Engineering Committee

761-6 Second Generation Aviation Satellite Communication Systems, Aircraft Installation Provisions

ARINC761-6 (Current)12/23/2019

This ARINC Standard defines the installation characteristics of second generation L-band satellite communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included. Supplement 6 adds references to new Diplexer/Low Noise Amplifiers (DLNAs) defined in Supplement 8 to ARINC Characteristic 781: Mark 3 Aviation Satellite Communication Systems. The five new DLNAs are intended to protect Inmarsat Classic Aero and SwiftBroadband (SBB) satcom equipment from ground-based cellular sources, such as cellular Long Term Evolution (LTE) and Ancillary Terrestrial Component (ATCt). The DLNAs are categorized by desired features and service (e.g., new DLNA versus drop-in replacement, LTE and/or ATCt protection, Classic Aero and/or SBB service

Airlines Electronic Engineering Committee

SPECIFICATION FOR TESTING AUTOMOTIVE LAMP ASSEMBLIES

USCAR34 (Current)

03/15/2022

The procedures contained in this specification cover the laboratory testing of Exterior Lamps for use in automotive road illumination. The following tests are intended to be run under the following conditions. This document shall be applied to systems that meet the requirements for design, performance and validation established by government standards. If other manufacture’s components are intended to be approved for use in the lamp assembly, then those possible combinations of components shall be considered a new lamp assembly and shall also be tested

USCAR

424-22 Navigation System Database

ARINC424-22 (Current)07/23/2018

This standard provides a data base comprising standards used for the preparation of a navigation system data base. This data may be used with the operational flight software in a wide range of navigational equipment

Airlines Electronic Engineering Committee

Brake Rotor Thickness Variation and Lateral Run-Out Measurements

J3111_202412 (Current)12/12/2024

Brake NVH Standards Committee

Shipping Caps, Torque Caps, and Body Plugs Ergonomic Design Criteria

USCAR43 (Current)

03/30/2015

This document describes the design and assembly force guidelines for conventional shipping caps, torque caps, and body plugs. All possible design and applications could not be anticipated in creating these guidelines. Where there are questions of adherence to this document, such as use of an “off-the-shelf” design, always consult the responsible Ergonomics Department

USCAR

CLASSIFICATION SYSTEM FOR AUTOMOTIVE TOOLING, MACHINERY AND EQUIPMENT LOW VOC WATERBORNE PAINT SYSTEMS

USCAR9 (Current)

12/30/1998

The materials defined by this U.S. CAR / S.A.E Recommended Practice are low VOC water based coatings for automotive tooling and general maintenance

USCAR

648 Cabin Passenger Seat Production Testing

ARINC648 (Current)12/18/2019

This report defines the requirements and recommended practices for production testing of aircraft passenger seats and seat groups. Production testing is performed at the seat manufacturers' facilities prior to the shipment of the seats to the airframe manufacturers, Maintenance, Repair, and Overhaul (MRO), or airlines/operators for installation in the aircraft. Using this guidance, rework is minimized and schedules remain minimally affected

Airlines Electronic Engineering Committee

PERFORMANCE SPECIFICATION FOR CABLE-TO-TERMINAL ELECTRICAL CRIMPS

USCAR21-4 (Current)

01/22/2020

This specification defines test methods and requirements for validation of solderless crimped connections. The purpose of this test is to simulate in the lab the stress seen in a typical life (15 years and 150000 miles) for a crimp connection and assure the crimp is mechanically strong and electrically stable. This specification was developed for use with stranded automotive copper wire. Only where specifically mentioned are other constructions or other core materials (aluminum, clad, steel core, etc.) applicable. This specification does not apply to wire types not mentioned, such as coaxial cable crimps, unless a USCAR-21 test is specifically referenced in the test specification for that wire type. This specification is based on accepted levels of environmental exposure for automotive applications. In any intended vehicle application, if the products covered by this specification are or may be subjected to conditions beyond those described in this document, they must pass special

USCAR

PERFORMANCE SPECIFICATION FOR WELDED WIRE-TO-WIRE SPLICES

USCAR45 (Current)

06/14/2018

SAE/USCAR-45 defines test methods and performance requirements for ultrasonically-welded wire-to-wire splices for automotive applications. Face-to-face, butt splice, and center strip configurations per Figure 1 can be tested. The tests defined in this specification subject samples on test to stresses that simulate a lifetime of exposure for a road vehicle. Stresses called out in this specification include thermal shock, temperature/humidity cycling and mechanical stress from different directions

USCAR

741P1-15 Aviation Satellite Communication System, Part 1, Aircraft Installation Provisions

ARINC741P1-15 (Current)12/23/2019

This ARINC Standard defines the installation characteristics of first generation L-band satellite communication systems. It provides the traditional form, fit, function, and interfaces for the installation of satcom equipment for use in all types of aircraft. Description of avionics equipment (e.g., Satellite Data Unit (SDU), Antennas, etc.) are included. Supplement 15 adds references to new Diplexer/Low Noise Amplifiers (DLNAs) defined in Supplement 8 to ARINC Characteristic 781: Mark 3 Aviation Satellite Communication Systems. The five new DLNAs are intended to protect Inmarsat Classic Aero and SwiftBroadband (SBB) satcom equipment from ground-based cellular sources, such as cellular Long Term Evolution (LTE) and Ancillary Terrestrial Component (ATCt). The DLNAs are categorized by desired features and service (e.g., new DLNA versus drop-in replacement, LTE and/or ATCt protection, Classic Aero and/or SBB service

Airlines Electronic Engineering Committee

758-4 Communications Management Unit (CMU) Mark 2

ARINC758-4 (Current)11/26/2019

This ARINC Standard specifies the ARINC 758 Mark 2 Communications Management Unit (CMU) as an on-board message router capable of managing various datalink networks and services available to the aircraft. Supplement 4 adds Ethernet interfaces, per ARINC Specification 664 Part 2. This will allow the CMU to communicate with IP based radio transceivers (e.g., L-Band Satellite Communication Systems (Inmarsat SwiftBroadband (SBB) and Iridium Certus), ACARS over IP, AeroMACS, etc

Airlines Electronic Engineering Committee

Standard for Cigar Lighters & Power Outlets

USCAR4-1 (Current)

03/31/2014

This standard is intended to cover cigar or cigarette lighters as well as power outlets based on the form and dimensions of the cigar lighter. This standard is a full performance specification, it includes dimensional and operational parameters as well as performance characteristics which must be met when submitting a cigar lighter assembly or power outlet assembly for production approval. This standard constitutes an acceptance specification for a surface mounted, front-loaded cigar lighter or power outlet

USCAR

755-5 Multi-Mode Receiver (MMR) - Digital

ARINC755-5 (Current)01/25/2018

ARINC Characteristic 755 defines a multi-mode receiver capable of providing flight path deviation guidance (corrections) to the aircraft during the approach and landing phase. The data source may be from an Instrument Landing System (ILS), a Microwave Landing System (MLS) or an GNSS Landing System (GLS). Supplement 5 adds annunciations defined in RTCA/DO-253D - MOPS for GPS LAAS Airborne Equipment. GNSS Data and GLS Config Validity ARINC 429 Labels are also updated. The range for Selected Glide Path Angle is corrected

Airlines Electronic Engineering Committee

743B-1 GNSS Landing System Sensor Unit (GLSSU

ARINC743B-1 (Current)06/22/2018

This document sets forth the characteristics of the GNSS Landing System Sensor Unit (GLSSU) intended for installation in commercial aircraft. The intent of this document is to provide general and specific design guidance for the development of GLSSU for airline use. It describes the desired operational capability of the GLSSU and the standards necessary to ensure interchangeability

Airlines Electronic Engineering Committee

739-1 Multi-Purpose Control and Display Unit (MCDU

ARINC739-1 (Current)06/01/1990

MCDU consists of an alphanumeric keyboard and display unit capable of interfacing with a number of aircraft systems. Dedicated keys on the MCDU provide the means for system selection with programmable soft keys. ARINC 429 interfaces are used to communicate with participating systems

Airlines Electronic Engineering Committee

739A-1 Multi-Purpose Control and Display Unit (MCDU

ARINC739A-1 (Current)12/16/1998

This MCDU standard consists of the original ARINC 739 definition with enhancements to allow it to be logged on to up to two systems at one time. Alternate form factors are included to allow the MCDU to be introduced into a wide variety of airframes candidate for CNS/ATM upgrade

Airlines Electronic Engineering Committee

738-3 Air Data and Inertial Reference System (ADIRS

ARINC738-3 (Current)07/31/2001

This standard defines an integrated ADIRS that provides air data information and directional guidance information for cockpit display. The ADIRS consists of up to three Air Data/Inertial Reference Units (ADIRUs) located in the aircraft electronic rack, an associated Control and Display Unit (CDU) and remotely mounted Air Data Modules (ADMs

Airlines Electronic Engineering Committee

Plating, Cadmium, Low Hydrogen Embrittlement Process

AMS2401L (Current)12/05/2024

This specification covers the engineering requirements for cadmium deposited on ferrous and nonferrous metals using a low hydrogen embrittlement (LHE) electroplating process

AMS B Finishes Processes and Fluids 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

Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Forging Stock 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted, 1800 °F (982 °C) Solution Heat Treated, Precipitation Hardenable (X750

AMS5671J (Current)

12/05/2024

This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, and flash-welded rings up to 4.00 inches (101.6 mm), exclusive, in least distance between parallel sides (thickness) or diameter, and stock of any size for forging or flash-welded rings

AMS F Corrosion and Heat Resistant Alloys Committee

Magnetic Particles, Fluorescent, Wet Method, Oil Vehicle, Aerosol Packaged

AMS3046J (Current)12/05/2024

This specification covers one type of fluorescent magnetic particles in the form of a mixed, ready-to-use suspension in an odorless, inspection oil vehicle and packaged in aerosol cans

AMS K Non Destructive Methods and Processes Committee

Tolerances, Low-Alloy Steel Bars

AMS2251K (Current)12/10/2024

This specification covers established manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term “exclusive” is used to apply only to the higher figure of the specified range

AMS E Carbon and Low Alloy Steels Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Welded Tubing, 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 2.9Ti - 1.4Al - 0.006B - 0.08Zr (Waspaloy), Consumable Electrode Remelted or Vacuum Induction Melted, Annealed

AMS5586J (Current)12/05/2024

This specification covers a corrosion- and heat-resistant nickel alloy in the form of welded and drawn 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

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

Flareless Hydraulic Tube Fittings

J514/2_202404 (Current)04/23/2024

This SAE Standard covers complete general and dimensional specifications for flareless type of hydraulic tube fittings. These fittings are intended for general application in hydraulic systems on industrial equipment and commercial products. These fittings are capable of providing leakproof, full flow connections in hydraulic systems operating at working pressures as specified in Table 1. For any application, it is recommended that sufficient testing be conducted and reviewed by both the user and fitting manufacturer to assure that performance levels will be safe and satisfactory. Formerly, SAE J514 was organized as a single document with ten clauses, which included six sections. This revision of SAE J514 has been organized into three sections as follows: Part 1: 37-degree flared fittings Part 2: Flareless (bite type) fittings Part 3: NPTF pipe fittings and pipe unions It is important to note that this and all SAE J-documents are intended for ground vehicle use only and not intended

Hydraulic Tube Fittings Committee

Nickel - Copper Alloy, Corrosion-Resistant, Bars, Forgings and Forging Stock, 67Ni - 30Cu - 0.04S, Free Machining

AMS4674J (Current)12/05/2024

This specification covers a corrosion-resistant nickel-copper alloy in the form of bars up to 3.00 inches (76.2 mm), inclusive, in thickness and forgings and forging stock of any size

AMS F Corrosion and Heat Resistant Alloys Committee

Molybdenum Disulfide Coating, Thin Lubricating Film, Impingement Applied

AMS2526E (Current)12/18/2024

This specification covers requirements for a coating consisting of finely powdered molybdenum disulfide in a heat resistant inorganic binder applied to parts

AMS B Finishes Processes and Fluids Committee

Cold Spray Additive Manufacturing (CSAM) Process

AMS7057 (Current)

12/05/2024

This specification establishes process controls for the repeatable implementation of the CSAM process for the manufacturing of metallic and metal-nonmetal blend components

AMS AM Additive Manufacturing Metals

Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7451), Solution Heat Treated, Stress Relieved, and Overaged

AMS4354B (Current)12/10/2024

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

SPECIFICATION FOR TESTING AUTOMOTIVE LED MODULES

USCAR33-1 (Current)

08/03/2020

This specification is a general level subsystem light source specification that establishes test requirements of light emitting diode (LED) components and modules for use in automotive lighting systems. The completed test data from this test specification is intended to be provided to the OEM by the Tier 1 lamp set maker as part of the lamp assembly PPAP. Re-testing shall be required if any portion of the approved LED module experiences a design, manufacturing, or component change. This document shall be applied to systems that meet the requirements for design, performance, and validation established by government standards. The LED module is defined as the LED devices and any electronics required to properly energize the LEDs using a vehicle electrical power system along with any associated electrical wiring, connectors, and thermal management system. Samples shall be tested as a subsystem and considered one test sample for the entire test sequence. A failure of any component in the

USCAR

628P0-4 Cabin Equipment Interfaces, Part 0, Cabin Management and Entertainment System - Overview

ARINC628P0-4 (Current)08/28/2018

The purpose of this document is to provide an introduction and overview of the ARINC 628 series of Specifications. ARINC 628 defines equipment and installation standards for cabin equipment, which is generally defined as communication and entertainment equipment designed for passenger use. Part 0 provides the concepts and overview of ARINC 628 and descriptions of each individual part. Appendix B is written in briefing chart format to facilitate the understanding of high-level objectives. Supplement 4 represents a summary of recent changes to Parts 1 through 9 of ARINC Specification 628

Airlines Electronic Engineering Committee

AVIONICS APPLICATION SOFTWARE STANDARD INTERFACE PART 3A CONFORMITY TEST SPECIFICATIONS FOR ARINC 653 REQUIRED SERVICES

ARINC653P3A-1 (Current)09/07/2018

ARINC 653, Part 3A is the Compliance Test Specification for ARINC 653 Required Services presently defined in ARINC 653 Part 1. The document specifies a set of stimuli and the expected responses. Future work on the ARINC 653 document set includes an effort to define Operating System services for multi-core processor environments. The Compliance Test Specification is expected to be updated in step with ARINC 653, Part 1

Airlines Electronic Engineering Committee

820 Cabin Architecture for Wireless Distribution System

ARINC820 (Current)08/13/2019

This document defines a secure Wi-Fi distribution network installed in the aircraft passenger cabin for passenger and crew use. Carry-on Portable Electronic Devices (PEDs) such as smart phones, tablets, and laptops may use this network to access public internet services provided on the aircraft

Airlines Electronic Engineering Committee

846 Fiber Optic Ferrule, Mechanical Transfer

ARINC846 (Current)08/06/2018

This specification covers the dimensions, performance, and quality assurance criteria for fiber optic MT contacts, including performance test requirements and procedures, suitable for use on commercial aircraft

Airlines Electronic Engineering Committee

747-3 Flight Data Recorder

ARINC747-3 (Current)06/07/2011

This document provides design guidance for the development and installation of Flight Data Recorders (FDR) which may utilize solid state memory and which may employ some means of data compression. The Flight Data Recorder will be utilized with a Flight Data Acquisition Unit (FDAU) (ARINC Characteristic 573) or a Digital Flight Data Acquisition Unit (DFDAU) (ARINC Characteristic 717) to accommodate mandatory flight data recording and other flight data acquisition needs. The document provides guidance and information to ensure customer controlled interchangeability of equipment in a standard aircraft installation and in data retrieval. The system capability was expanded to accommodate a data bus speed of 1024 words per second

Airlines Electronic Engineering Committee

Engine Rotation and Cylinder Numbering

J824_202206 (Current)

06/29/2022

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