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Aircraft Pressures and Temperatures – Resource DocumentAIR8471 (Current)
This SAE AIR covers Forced Air technology including: reference material, equipment, safety, operation, and methodology. It is intended to provide pressure and temperature (temps pages 26 & 31) information and minimum safety guidelines regarding use of equipment to remove frozen contaminants related to: i) Forced air ii) Forced air/fluid iii) Deicing fluid
G-12M Methods Committee
Aircraft Skin Pressures and TemperaturesAIR8469 (Current)
This information report covers all known aircraft with respect to deicing operations, especially with regard to OEM pressure and temperature limitations on the airframe. It provides data for airlines/operators on compliance with OEM limits and confirms that OEM limits are not exceeded during deicing operations.
G-12M Methods Committee
Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL SAE 8740, CADMIUM PLATED, 125 KSI MIN UTS, .4375-20 UNJF-3AAS9918C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON, EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS N07001, 165 KSI, .4375-20 UNJF-3AAS9727A (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
Driveline Parking Brake Test Procedure for Medium Duty VehiclesJ2690_202606 (Current)6/3/2026
This SAE Recommended Practice establishes uniform test procedures for friction based parking brake components used in conjunction with hydraulic service braked vehicles with a gross vehicle weight rating greater than 4500 kg (10 000 lb). The components covered in this document are the primary actuation and the foundation park brake. Various peripheral devices such as application dashboard switches or indicators are not included. These test procedures include the following: a Brake Related Tests 1 Brake Functional Performance 2 Brake Dynamic Torque Performance 3 Brake Corrosion Resistance 4 Brake Endurance with Torque 5 Brake Endurance without Torque 6 Vibration Resistance 7 Brake Ultimate Static Load 8 Brake Lining Wear Adjuster Function b Actuation Related Tests 1 Mechanical Actuator Functional Performance 2 Mechanical Actuator Endurance 3 Mechanical Actuator Quick Release 4 Mechanical Actuator Ultimate Load 5 Spring Apply Actuator Functional Performance 6 Spring Apply Actuator
Truck and Bus Hydraulic Brake Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3AAS9676C (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
WASHER, KEY - 90°, LOCKING, CRES, UNS S32100AS9581D (Current)6/3/2026
E-25 General Standards for Aerospace and Propulsion Systems
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings, and Stock for Forgings, Rings, or Heading 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V (A286) Consumable Electrode Remelted, 1800 °F (982 °C) Solution Heat Treated Precipitation HardenableAMS5731M (Current)9/5/2023
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, and flash welded rings up to 5.00 inches (127 mm), inclusive, in nominal diameter or least distance between parallel sides (thickness) and stock for forging, flash welded rings, or heading of any size.
AMS F Corrosion and Heat Resistant Alloys Committee
Piston Rings, Centrifugally-Case Alloyed Iron 0.50Mo - 0.50CuAMS7311H (Current)8/4/2017
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings.
AMS E Carbon and Low Alloy Steels Committee
Rings, Sealing, Synthetic Rubber Phosphate Ester Hydraulic Fluid Resistant, Butyl Type 70-85AMS7277C (Current)4/1/1991
AMS CE Elastomers Committee
STUDS, LOW-ALLOY HEAT-RESISTANT STEEL Normalized and Tempered, Roll Threaded 135,000 psi (931 MPa) Tensile StrengthAMS7458F (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
Powder, Plasma Spray 50 (88WC - 12Co) + 35 (70Ni - 16.5Cr - 4Fe - 4Si - 3.8B) + 15 (80Ni - 20Al) Three-Component MixtureAMS5792C (Current)4/1/2024
This specification covers a blend of tungsten carbide-cobalt aggregate, a nickel alloy, and a nickel aluminum aggregate in the form of powder.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 60.5Ni - 23Cr - 14Fe - 0.35Ti - 1.4Al (Alloy 601), Solution Heat TreatedAMS5870G (Current)3/27/2024
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.010 to 2.000 inches (0.25 to 50.80 mm), inclusive, in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe 1800 °F (982 °C) Solution Heat Treated, Precipitation HardenableAMS5747E (Current)11/18/2022
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, including (101.6 mm, including) in nominal diameter or least distance between parallel sides, and stock of any size for forging or flash welded rings (see 8.5).
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings, and Stock for Forgings, Rings, or Heading 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V (A286) Consumable Electrode Remelted 1800 °F (982 °C) Solution and Precipitation Heat TreatedAMS5732K (Current)11/15/2023
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, and flash welded rings up to 5.00 inches (127 mm), inclusive, in nominal diameter or least distance between parallel sides (thickness), and stock for forging, flash welded rings, or heading of any size.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion- and Heat-Resistant, Welding Wire 15Cr - 25.5Ni - 1.3Mo - 2.2Ti - 0.006B - 0.30V (A286)AMS5804J (Current)3/25/2025
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant 20cr 9ni 1.6mo 1.4w 0.6tiAMS5724A (Current)1/1/1991
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 AnnealedAMS5879E (Current)8/19/2021
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
Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 72Ni - 15.5Cr - 1.0Cb(Nb) - 2.4Ti - 0.70Al - 7.0FeAMS5778K (Current)10/18/2021
This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Tungsten Carbide-Cobalt Powder Sintered and CrushedAMS7880C (Current)3/13/2007
This specification covers tungsten carbide-cobalt in the form of powder.
AMS B Finishes Processes and Fluids Committee
Introduction to EDIF, Volume 1EIAEDIF1 (Current)7/1/2015
Systems Management Council
Detailed Specification for Aircraft Pressure Refueling NozzleAS5877C (Current)4/1/2024
This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for the refueling and defueling of aircraft fitted with pressure fuel servicing systems. It is to be used as a replacement for MIL-N-5877 and MS29520 and for all commercial applications.
AE-5C Aviation Ground Fueling Systems Committee
CDIF Integrated Meta-model Data Flow Model Subject AreaEIAIS115 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model defined for CASE also has applicability as the basis of standard definitions for use in repositories. The standards that form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This
Systems Management Council
CDIF Integrated Meta-model Presentation Location and Connectivity Subject AreaEIAIS118 (Current)7/1/2015
The CDIF Family of Standards is primarily designed to be used as a description of a mechanism for transferring information between CASE tools. It facilitates a successful transfer when the authors of the importing and exporting tools have nothing in common except an agreement to conform to CDIF. The language that is defined for the Transfer Format also has applicability as a general language for Import/Export from repositories. The CDIF Integrated Meta-model also has applicability as the basis of standard definitions for use in repositories. The standards that form the complete family of CDIF Standards are documented in EIA/IS-106 CDIF - CASE Data Interchange Format - Overview. These standards cover the overall framework, the transfer format and the CDIF Integrated Meta-model. The diagram in Figure 1 depicts the various standards that comprise the CDIF Family of Standards. The shaded box depicts this Standard and its position in the CDIF Family of Standards. This standard, EIA/IS-118
Systems Management Council
Specification Policy GuideEIAQAB7 (Current)7/1/2015
This document has been formulated as a suggested guide in assisting EIA Engineering Department Panels and JEDEC Councils in cooperating with the Defense Department and other Federal agencies in the preparation of suggested reliability requirements for various types of electronic products as part of a program designed to enhance the reliability of defense and related equipment. The document is to be followed merely as a guide and is not intended to limit technical groups in the consideration of the factors to be taken into account in the development of reliability specifications for recommendation to the Government. The document is prepared as a guide to the following EIA Engineering Department Panels and JEDEC Councils: This document is designed to implement the important specification features recommended by the PSMR-1 Report issued by DOD in 1960, and to guide specification writers toward the over-all objectives of making reliability information available in a consistent and orderly
Systems Management Council
Using EDIF 200 for Schematic TransferEIAEDIFAG1 (Current)7/1/2015
Systems Management Council
Historical Rationale for Military EMI LimitsEMCB1_1 (Current)7/1/2015
AE-4 Electromagnetic Compatibility (EMC) Committee
Industry Implementation of International Standard ISO/IEC 12207:1995 (ISO/IEC 12207) Standard for Information Technology Software Life Cycle ProcessesIEEEEIA12207_0 (Current)7/1/2015
This International Standard establishes a common framework for software life cycle processes, with well-defined terminology, that can be referenced by the software industry. It contains processes, activities, and tasks that are to be applied during the acquisition of a system that contains software, a stand-alone software product, and software service and during the supply, development, operation, and maintenance of software products. Software includes the software portion of firmware. This International Standard also provides a process that can be employed for defining, controlling, and improving software life cycle processes.
Systems Management Council
Aluminum Alloy, Extrusions and Rings, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr - (6061-T6), Solution and Precipitation Heat TreatedAMS4150P (Current)3/27/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing, flash-welded rings fabricated from extruded stock, and stock for flash-welded rings (see 8.6).
AMS D Nonferrous Alloys Committee
Steel, Nitriding, Bars, Forgings, Mechanical Tubing and Forging Stock Aircraft Quality 1.1Cr - 3.5Ni - 0.25Mo - 1.2Al (0.21 - 0.26C)AMS6475M (Current)10/28/2024
This specification covers an age-hardenable nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
J1939 Digital AnnexJ1939DA_202601 (Current)4/10/2026
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
HUB - WOOD PROPELLER - TAPER TYPE - NUMBER 0AS357 (Current)2/1/1958
CONNECTOR ACCESSORIES, ELECTRICAL BACKSHELL, 90 DEGREE, SELF LOCKING AND NON-SELF LOCKING, PRE-ATTACHED SHIELD TERMINATION (RFI/EMI), BOOT ACCOMODATION, CATEGORY 3B FOR MIL-DTL-38999 SERIES III AND IV CONNECTORSAS85049/117D (Current)7/1/2020
AE-8C1 Connectors Committee
Personal Watercraft - Display of Capacity InformationJ2566_202308 (Current)7/4/2023
This SAE Recommended Practice establishes uniform requirements and guidelines for the display of capacity information of personal watercraft.
Personal Watercraft Committee
Manual of Organization and ProcedureGEIAOP0001E (Current)7/1/2015
The TechAmerica Standards & Technology department is responsible for standardization activities, and provides other appropriate technical and engineering services within the scope of TechAmerica by-laws. Standardization activities shall include those associated with Business, Engineering, and Operations Management and Processes. All activities shall be conducted in accordance with appropriate legal guidance.
Systems Management Council
Systems EngineeringEIAIS632 (Current)7/1/2015
This standard defines a total system approach for the development of systems. The standard requires: establishing and implementing a structured, disciplined, and documented systems engineering effort incorporating the systems engineering process; multidisciplinary teamwork; and the simultaneous development of the products and processes needed to satisfy user needs. The systems engineering process is defined generically to facilitate broad application. This standard defines the requirements for technical reviews. The tasks in this standard provide a methodology for evaluating progress in achieving system objectives. This standard provides a comprehensive, structured, and disciplined approach for all life-cycle phases, including new system product and process developments, upgrades, modifications, and engineering efforts conducted to resolve problems in fielded systems. This standard is applicable to technical efforts in support of advancement and development of new technologies and
G-47 Systems Engineering
Assessment of Average Outgoing Quality Levels in Parts Per Million (PPM)EIA554_1 (Current)8/1/2015
This standard is intended to provide a uniform method of calculating an estimate of the proportion nonconforming in finished components and to provide a standardized definition of the quality index referred to as Average Outgoing Quality (AOQ). The method used here is primarily directed at components whose production or procured volume is large enough, during some predefined sampling period, to give statistically meaningful information.
Systems Management Council
Assessment of Nonconforming Levels In Parts Per Million (PPM)EIA554_2 (Current)8/1/2015
This standard is intended to provide a uniform method of determining proportion nonconforming in finished components and to provide a standardized definition of the quality index referred to as PPM. The method used here is primarily directed at components whose production or procured volume is large enough, during some predefined sampling period, to give statistically meaningful information.
Systems Management Council
National Electronic Process Certification StandardEIA599A (Current)8/1/2015
This Standard is applicable to suppliers of electronic components, assemblies, equipment and related materials. This standard establishes the general requirements to achieve a certified process. The use of this standard is intended for any manufacturing or service company whose goal is to achieve customer satisfaction through continuous improvement.
Systems Management Council
Reliability QuantificationRB4A (Current)7/1/2015
G-41 Reliability
Requirements for Road Weather ApplicationsJ2945/3_202201 (Current)12/1/2021
Inclement weather can have a significant impact on surface transportation systems. It can result in hazardous conditions for travelers due to poor visibility, or wet or icy roadways. Weather applications have the potential to provide additional data to surface transportation infrastructure owners and operators, allowing them to better assess the impacts of the weather environment on or around the roadway and to better manage the surface transportation system. Such weather applications can: Collect road weather data from connected vehicles and mobile devices, increasing the number of data sources available. Provide road weather related traveler information to travelers via connected vehicles and devices, such as when and where a hazardous condition exists. Provide the ability to manage road weather response on specific roadways. This SAE Standard specifies interface requirements between vehicles and infrastructure for weather applications, including detailed systems engineering
V2X Core Technical Committee
File Structures for a Node Capability File (NCF) and LIN Description File (LDF)J2602-3_202110 (Current)9/1/2021
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
CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, STRAIGHT SELF-LOCKING, NON-SELF-LOCKING, CATEGORY 4B (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)AS85049/118D (Current)5/21/2021
AE-8C1 Connectors Committee
Elastomer Compatibility Considerations Relative to Elastomer SelectionAIR786C (Current)9/1/2021
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
T-BOLT, A-286, 1000 °F BUSHING HEADAS4108/2B (Current)11/17/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
EYE BOLT, A-286 CRES, 1000 °FAS4108/3B (Current)11/18/2025
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Planetary Gears - TerminologyJ646_202310 (Current)11/1/2023
Figures 1 through 6 illustrate in simplified form some of the more common planetary gears, gearsets, and geartrain arrangements in order to establish applicable terminology. Figures 7 and 8 provide additional examples that use elements of those gear arrangements.
Automatic Transmission and Transaxle Committee
Test Procedures for Electric Vehicles to Determine Charging PerformanceISO/SAE 12906 (Current)3/1/2025
This document specifies test procedures to determine the charging performance of electric vehicles. This document facilitates clear and consistent comparisons of realistic charging capabilities of electrically propelled vehicles (EVs) via commercially available electric vehicle supply equipment. It provides details about test conditions, test methods, and test processes derived from typical use cases. Furthermore, it specifies requirements regarding the information for the vehicle operator. This document is applicable to EVs, including plug-in hybrid EVs. This document does not provide requirements for mopeds and motorcycles. Unless specified otherwise, all test procedures can be applied to AC, DC, or wireless charging methods.
Hybrid - EV Committee
International and National Quality Standards IndexEIA765A (Current)7/1/2015
G-33 Configuration Management
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