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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
SCREW, DRIVE, ROUND HEAD, TYPE U AMS5504 (UNS S41000)AS3568B (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Safety Considerations for Aircraft-Mounted Lasers Projected into the Navigable AirspaceARP5674A (Current)6/8/2026
This SAE Aerospace Recommended Practice (ARP) is intended to be used for laser systems mounted on aircraft and propagated into navigable airspace. This does not include lasers onboard aircraft where the beam is contained within an enclosure so that the beam cannot enter into airspace, nor does it include lasers from satellites and spacecraft in outer space. It may be used in conjunction with AS4970, ARP5535, ARP5572, ARP5293, and the ANSI Z136 laser safety standards.
G-10T Laser Safety Hazards Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, CORROSION AND HEAT RESISTANT STEEL, SIMILAR TO UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS9575F (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Guide to Certification of Aircraft in a High-Intensity Radiated Field (HIRF) EnvironmentARP5583B (Current)6/8/2026
This document and the EUROCAE equivalent, ED-107, provides detailed information, guidance, and methods in support of the Federal Aviation Administration (FAA) Advisory Circular (AC) 20-158 and to the European Union Aviation Safety Agency (EASA) AMC 20-158. AC 20-158 provides a means, but not the only means, for demonstrating compliance with Title 14 of the Code of Federal Regulations (14 CFR) 23.1308 (Amendment 57 and lower), 23.2520 (Amendment 64 and higher), 25.1317, 27.1317, 29.1317, and applicable FAA HIRF special conditions addressing HIRF Protection. AMC 20-158 is applicable to Certification Specifications CS 23.1308 (Amendment 4 and lower), 23.2520 (Amendment 5 and higher), 25.1317, 27.1317, and 29.1317. It should be noted that this document is neither mandatory nor regulatory in nature and does not constitute a regulation or legal interpretation of the regulation. Therefore, an applicant may elect to establish an alternative method of compliance that is acceptable to the
AE-4 Electromagnetic Compatibility (EMC) Committee
WASHER, KEY - SINGLE, BEARING RETAINING, AMS6350 (UNS G41300)AS172201C (Current)6/8/2026
SCOPE IS UNAVAILABLE.
E-25 General Standards for Aerospace and Propulsion Systems
Plating, GoldAMS2422G (Current)6/8/2026
This specification covers the requirements for electrodeposited gold plate.
AMS B Finishes Processes and Fluids Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Foil, 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) (Alloy 625), Consumable Electrode Remelted, Cold Rolled and AnnealedAMS5879F (Current)6/8/2026
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
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .5000-20 UNJF-3AAS3179C (Current)6/8/2026
E-25 General Standards for Aerospace and Propulsion Systems
Uphill Quenching of Aluminum Alloy ProductAMS2767B (Current)6/8/2026
This specification establishes the engineering requirements for the uphill quenching process of aluminum alloy product. Uphill quenching immerses product in liquid nitrogen followed by exposure to a high-pressure/high-velocity steam blast or boiling water.
AMS D Nonferrous Alloys Committee
Leaded Phosphor Bronze Strip, 88.5Cu - 4.0Sn - 4.0Pb - 3.0Zn - 0.26P, Cold Rolled, Half Hard (H02)AMS4520N (Current)6/8/2026
This specification covers a copper alloy in the form of strip (see 8.6).
AMS D Nonferrous Alloys Committee
Numerical Modeling Techniques for Jet Engine Test Cell AerodynamicsAIR6355 (Current)6/5/2026
This SAE Aerospace Information Report (AIR) has been written for individuals associated with ground level testing of turbofan and turbojet engines, and particularly for those who might be interested in investigating steady-state performance characteristics of a new test cell design or of proposed modifications to an existing test cell by means of numerical modeling and simulation. It is not the intent of this standard to provide specific test cell design recommendations, which are covered in the reference documentation.
EG-1E Gas Turbine Test Facilities and Equipment
J1930 Electrical/Electronic Systems Diagnostic Terms, Definitions, Abbreviations, and Acronyms Web Tool SpreadsheetJ1930DA_202301 (Current)1/17/2023
Continuation of the digital annex of terms and definitions for use by scantools and maintain alignment of terms with other committees such as J2012, J1979, J1939 etc. and with regulatory bodies.
Vehicle E E System Diagnostic Standards Committee
Alloy, Corrosion- and Heat-Resistant, Sheet, Strip, and Plate 29Fe - 22Cr - 21Ni - 18.5Co - 3.2Mo - 2.8W - 0.78Ta - 0.30Al - 0.05Zr - 0.05La - 0.20N (HS-556) Solution Heat TreatedAMS5874D (Current)10/16/2023
This specification covers a corrosion- and heat-resistant alloy in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Method for Evaluating the Cleavage Strength of Structurally Bonded Fiberglass Reinforced Plastic (Wedge Test)J1882_198708 (Current)10/1/1987
Materials, Processes and Parts Council
Functional, Performance, and Safety Guidelines for Tire Pressure Monitoring Systems (TPMS) for AircraftARP6137A (Current)6/1/2026
This SAE Aerospace Recommended Practice (ARP) establishes the overall component and system function guidelines and minimum performance levels for a TPMS. These guidelines include, but are not limited to: Design recommendations for system components, which: Monitor tire inflation Are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment Recommended performance and safety guidelines for a TPMS.
A-5 Aerospace Landing Gear Systems Committee
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
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
Low Speed Thorax Impact Test Procedure for the HIII 50th Male DummyJ2779_202206 (Current)6/29/2022
Dummy Testing and Equipment Committee
Steel, Corrosion and Heat Resistant, Welding Wire 15Cr - 7.1Ni - 2.4Mo - 1.0Al Vacuum Induction MeltedAMS5812G (Current)5/4/2021
This specification covers a corrosion and heat resistant steel in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Rubber: Fluorocarbon (FKM) High Temperature - Fluid Resistant Low Compression Set/70 to 80 Type A Hardness For Seals in Fuel Systems and Specific Engine Oil SystemsAMS7276J (Current)5/18/2020
This specification covers a fluorocarbon rubber in the form of molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications. For sheet, strip, tubing, extrusions, and molded shapes use AMS3216 specification which is intended for that use.
AMS CE Elastomers Committee
Perfluorocarbon (FFKM) Engine Oil, Fuel and Hydraulic Fluid Resistant 70 to 80 Hardness For High Temperature Seals in Engine Oil Systems, Fuel Systems and Hydraulic SystemsAMS7257E (Current)9/5/2014
This specification covers a Perfluorocarbon (FFKM) rubber in the form of molded rings, compression seals, o-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
AMS CE Elastomers Committee
Nickel-Iron Alloy Wire, Copper Clad, Round, 42Ni - 56.5Fe, Annealed DumetAMS7734D (Current)5/15/2006
This specification covers a nickel-iron alloy in the form of round wire clad with electrolytic copper.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, Rings and Stock for Rings and Forging 45.5Ni - 25.5Cr - 3.2Mo - 3.2W - 18.5Fe (Alloy 333) Solution Heat TreatedAMS5717K (Current)2/25/2025
This specification covers a corrosion- and heat-resistant nickel 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
Steel, Corrosion and Heat-Resistant, Bars and Forgings and Forging Stock, 15.5Cr - 4.5Ni - 2.9Mo - 0.10N (AM 355®), Consumable Electrode Remelted, Heat Treated, 170 ksi (1172 MPa) Tensile StrengthAMS5744G (Current)9/18/2024
This specification covers a corrosion- and heat-resistant steel in the form of bars, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Stock for Forgings and Rings 60.5Ni - 23Cr - 14Fe - 1.4Al (Alloy 601) AnnealedAMS5715H (Current)1/22/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, and flash-welded rings 4.00 inches (101.6 mm) and under in diameter or least nominal cross-sectional dimension and stock of any size for forging or flash-welded rings.
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 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
Tungsten Carbide Powder, Cobalt CoatedAMS7878C (Current)8/20/2002
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of March 1994. It is recommended, therefore, that this specification not be specified for new designs.
AMS F Corrosion and Heat Resistant Alloys Committee
Integration Engineering for System EffectivenessEQB2 (Current)7/1/2015
G-47 Systems Engineering
Style Manual for Standards and Other Publications of TechAmericaGEIAOP0002 (Current)7/1/2015
This style manual establishes requirements for the preparation of standards1) and certain other publications of TechAmerica. It also gives some indication with regard to presentation.
Systems Management Council
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
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
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
Powder, Plasma Spray 95Ni - 5AlAMS5793C (Current)4/1/2024
This specification covers a nickel-aluminum aggregate in the form of powder.
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
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
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
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
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
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