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J1939 Digital AnnexJ1939DA_202412 (Current)12/29/2024
This document is intended to supplement the J1939 documents by offering the J1939 information in a form that can be sorted and searched for easier use
Truck and Bus Control and Communications Network Committee
Supplement
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)06/29/2022
Dummy Testing and Equipment Committee
Recommended Practice
OBD-II Scan Tool - Second Generation ProtocolsJ1978-2_202412 (Current)12/03/2024
SAE J1978-2 specifies a complementary set of functions to be provided by an OBD-II scan tool. These functions provide complete, efficient access to all regulated OBD services on any vehicle that is compliant with SAE J1979-2 and SAE J1979-3 The content of this document is intended to satisfy the requirements of an OBD-II scan tool as required by current U.S. OBD regulations. This document specifies: A means of establishing communications between an OBD-equipped vehicle and an OBD-II scan tool. A set of diagnostic services to be provided by an OBD-II scan tool in order to exercise the services defined in SAE J1979-2. The presentation of the SAE J1978 document family, where SAE J1978-2 covers second generation protocol functionality defined in SAE J1979-2, and SAE J1978-1 covers first generation protocol functionality defined in SAE J1979 and protocol determination for both SAE J1979 and SAE J1979-2. The SAE J1978 document family does not preclude the inclusion of additional capabilities
Vehicle E E System Diagnostic Standards Committee
Recommended Practice
Test Cases for OBD-II Scan Tools and I/M Test EquipmentJ1699/2_202412 (Current)12/05/2024
To define test cases for the OBD-II interface on external test equipment (such as an OBD-II Scan Tool, Inspection/Maintenance Tester, etc.) which can be used to verify compliance with the applicable standards such as SAE J1978 and SAE J1979 for Passenger Cars, Light-Duty Trucks, and Medium-Duty Vehicles and Engines (OBD II
Vehicle E E System Diagnostic Standards Committee
Recommended Practice
Flareless Hydraulic Tube FittingsJ514/2_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
Technical Standard
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 (X750AMS5671J (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
Material Specification
Magnetic Particles, Fluorescent, Wet Method, Oil Vehicle, Aerosol PackagedAMS3046J (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
Material Specification
Tolerances, Low-Alloy Steel BarsAMS2251K (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
Material Specification
Cold Spray Additive Manufacturing (CSAM) ProcessAMS7057 (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
Material Specification
Automated Gaseous Nitriding Controlled by Nitriding PotentialAMS2759/10D (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
Material Specification
Plating, Cadmium, Low Hydrogen Embrittlement ProcessAMS2401L (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
Material Specification
Chemical Check Analysis Limits, Titanium and Titanium AlloysAMS2249K (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
Material Specification
Aluminum Alloy, Plate, 7.9Zn - 1.8Cu - 2.0Mg - 0.10Zr (7099-T7451), Solution Heat Treated, Stress Relieved, and OveragedAMS4354B (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
Material Specification
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, AnnealedAMS5586J (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
Material Specification
Beryllium Bars, Rods, Tubing, and Shapes, Instrument GradeAMS7907E (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
Material Specification
Nickel - Copper Alloy, Corrosion-Resistant, Bars, Forgings and Forging Stock, 67Ni - 30Cu - 0.04S, Free MachiningAMS4674J (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
Material Specification
Molybdenum Disulfide Coating, Thin Lubricating Film, Impingement AppliedAMS2526E (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
Material Specification
Steel, Sheet and Strip, 0.25 Carbon, Maximum (SAE 1020), Hard TemperAMS5045L (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
Material Specification
Measurement of the Total Ash Content of Aviation Piston Engine Oils by a Calculation MethodJ1787_202009 (Current)09/29/2020
This SAE Recommended Practice describes an empirical method for determining the theoretical ash content of aviation piston engine lubricating oils by calculating the equivalent weight of metallic oxides formed at 775 °C based on the metallic elemental concentration. The calculation method of ash determination may be used as an alternate to ASTM D 482 for application to the standards for aviation piston engine lubricating oils
E-38 Aviation Piston Engine Fuels and Lubricants
Recommended Practice
Electrical Charging Systems for Off-Road Work MachinesJ180_202410 (Current)10/21/2024
This SAE Standard describes alternator physical, performance, and application requirements for heavy-duty electrical charging systems for off-road work machines, including those defined in SAE J1116
CTTC C2, Electrical Components and Systems
Technical Standard
Evaluation Criteria for Reliability-Centered Maintenance (RCM) ProcessesJA1011_202411 (Current)11/06/2024
This SAE Standard for reliability-centered maintenance (RCM) is intended for use by any organization that has or makes use of physical assets or systems that it wishes to manage responsibly
G-11M, Maintainability, Supportability and Logistics
Recommended Practice
Plating, Silver, Nickel Strike, High BakeAMS2410M (Current)12/05/2024
This specification covers the requirements for electrodeposited silver on other metals, usually with a nickel strike between the basis metal and the silver
AMS B Finishes Processes and Fluids Committee
Material Specification
Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C), Aircraft QualityAMS6492C (Current)12/05/2024
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum-Beryllium Alloy, Sheet and Plate, 38Al - 62BeAMS7913E (Current)12/10/2024
This specification covers an aluminum-beryllium alloy in the form of sheet and plate consolidated from powder by extrusion and then rolled (see 8.5
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Sheet, Strip, and Plate, 6Al - 4V, Solution Heat TreatedAMS4903E (Current)12/10/2024
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 2.000 inches (50.80 mm), inclusive (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, Annealed, Heat TreatableAMS6947C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes 4.000 inches (101.60 mm) and under and stock for forging, heading, or flash-welded rings of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Beryllium Near-Net Preforms, Standard Grade, Cold Isostatic Pressed, SinteredAMS7910E (Current)12/10/2024
This specification covers beryllium in the form of bar, rod, tubing, and shapes fabricated from impact-ground beryllium powder consolidated by cold isostatic pressing (CIP) and sintering
AMS G Titanium and Refractory Metals Committee
Material Specification
Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 4Al - 2.5V -1.5 Fe, AnnealedAMS6948C (Current)12/10/2024
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, drawn shapes 5.000 inches (127.00 mm) and under, and stock for forging or flash-welded rings of any size (see 8.6
AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Flash-Welded Rings, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73), Solution and Precipitation Heat TreatedAMS4174F (Current)12/05/2024
This specification covers an aluminum alloy in the form of flash-welded rings 0.062 to 4.499 inches (1.57 to 114.27 mm), inclusive, in radial thickness with cross-sectional areas up to 32 square inches (206 cm2) (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Steel, Bars, and Forgings, Aircraft Quality, 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740), Heat Treated, 105 ksi (724 MPa) Tensile StrengthAMS6325M (Current)12/18/2024
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel Bars, 1.0Cr - 0.20Mo - 0.45Se (0.39 - 0.48C) (4142H Modified), Die-Drawn, 130 ksi (896 MPa) Yield Strength, Free MachiningAMS6378J (Current)12/18/2024
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter produced by a die-drawing process
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Iron-Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate, 44Fe - 18.5Cr - 35Ni - 1.15Si (Alloy 330), Solution Heat TreatedAMS5592H (Current)12/18/2024
This specification covers a corrosion- and heat-resistant iron-nickel alloy in the form of sheet, strip, and plate
AMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Steel Sheet, Strip, and Plate, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft QualityAMS6350R (Current)12/18/2024
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Steel Bars, Forgings, Tubing, and Forging Stock, 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C), Electroslag Remelted or Consumable Electrode Vacuum Remelted, Premium Aircraft QualityAMS6493C (Current)12/18/2024
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
Material Specification
INSERT, SCREW THREAD, NON-LOCKING, LOCKED IN, KEY LOCKED, HEAVY-DUTY, SELF-BROACHING KEYS, UNS S66286AS3572B (Current)12/18/2024
SCOPE IS UNAVAILABLE
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Aluminum Alloy, Extrusions, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73, 7075-T73511, 7075-T73510), Solution Heat Treated, Stress Relieved by Stretching when required, and OveragedAMS4617B (Current)12/10/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing 0.040 to 4.499 inches (1.01 to 114.27 mm), inclusive, in nominal diameter or least thickness and with areas up to 32 square inches (206 cm2), inclusive (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Steel, Sheet, Strip, and Plate, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, Normalized or Otherwise Heat TreatedAMS6345F (Current)12/10/2024
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate up to and including 1.500 inches (38.10 mm) in thickness
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy, Plate (7065-T7451), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and OveragedAMS4361B (Current)12/10/2024
This specification covers an aluminum alloy in the form of plate
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Plate (7065-T7651), 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr, Solution Heat Treated, Stress-Relieved, and OveragedAMS4351B (Current)12/10/2024
This specification covers an aluminum alloy in the form of plate
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Extruded Profiles (2043-T85), 2.8Cu - 1.65Li - 0.35Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and AgedAMS4450A (Current)12/10/2024
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thicknesses 0.040 to 2.500 inches (1.02 to 38.10 mm), inclusive, having a maximum cross-sectional area of 23 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 2.4.1 and 8.7
AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn; (2024-T81 Sheet, -T851 Plate), Solution Heat Treated, Cold Worked and Artificially AgedAMS4268B (Current)12/10/2024
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.500 inches (0.254 to 38.07 mm), inclusive, in thickness, supplied in the -T81/-T851 temper (see 8.5
AMS D Nonferrous Alloys Committee
Material Specification
HELICOPTER TURBINE ENGINE WASHAIR4416 (Current)12/18/2024
Engines subject to dust, industrial pollution, saltwater contamination or other chemically laden atmosphere (including pesticides and herbicides) lose performance due to deposits of contaminants on surfaces in the aidgas flow path. Engine wash and engine rinse procedures are utilized to restore turbine engine performance. These procedures are generated by the engine manufacturer and are included in the Engine Maintenance/Service Manuals. For most turbine engines these procedures are similar in concept and practice; however, application details, choice of solvents and many other service features can vary from engine manufacturer to engine manufacturer and may even vary within the range of engine models produced by any manufacturer. The intent of this SAE Aerospace Information Report (AIR) is to outline the general nature, considerations, and background of engine wash and engine rinse and is directed towards the needs of the entry level engineer, service engineer, and those involved in
S-12 Powered Lift Propulsion Committee
Information Report
Integrated Rudder and Brake Pedal Unit, General Requirements for Fly-By Wire Transport and Business AircraftARP6252 (Current)10/15/2018
This Aerospace Recommended Practice (ARP) provides general requirements for a generic, integrated rudder and brake pedal unit, incorporating a passive force-feel system that could be used for fixed-wing fly-by wire transport and business aircraft. This ARP addresses the following: The functions to be implemented The mechanical interconnection between captain and F/O station The geometric and mechanical characteristics The mechanical, electrical, and electronic interfaces The safety and certification requirements
A-6A3 Flight Control and Vehicle Management Systems Cmt
Recommended Practice
Steel, Sheet, Strip, and Plate, 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, SpheroidizedAMS6351M (Current)12/18/2024
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate
AMS E Carbon and Low Alloy Steels Committee
Material Specification
Aluminum Alloy, Alclad Sheet, 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (Alclad 7050-T76), Solution Heat Treated and OveragedAMS4243D (Current)12/18/2024
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm), inclusive, in nominal thickness (see 8.6
AMS D Nonferrous Alloys Committee
Material Specification
Portable Controlled Contamination Area (CCAAIR7522 (Current)12/18/2024
This SAE Aerospace Information Report (AIR) provides guidelines for the design of portable Controlled Contamination Areas (CCAs) that can provide localized environmental control when processing a repair at the airplane or in a hangar environment. The use of a portable CCA may result in a better quality repair. The use of a portable CCA may assist in achieving the environmental requirements for bonded repairs specified in an approved repair procedure. This provides an option to accomplish a repair on nonremovable structure or difficult to remove components
AMS CACRC Commercial Aircraft Composite Repair Committee
Information Report
Flight Control Actuators - Dynamic Seals, Collection of Duty Cycle DataARP4895B (Current)12/18/2024
This SAE Aerospace Recommended Practice (ARP) provides an algorithm aimed to analyze flight control surface actuator movements with the objective to generate duty cycle data applicable to hydraulic actuator dynamic seals
A-6A3 Flight Control and Vehicle Management Systems Cmt
Recommended Practice
Engine Rotation and Cylinder NumberingJ824_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
Technical Standard
747-3 Flight Data RecorderARINC747-3 (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
Characteristic
Standard for Cigar Lighters & Power OutletsUSCAR4-1 (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
Specification
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