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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
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
J1979-DA, Digital Annex of E/E Diagnostic Test ModesJ1979DA_202508 (Current)5/27/2026
The SAE J1979 document set includes the communication between the vehicle's On-Board Diagnostic (OBD) systems and test equipment implemented across vehicles within the scope of regulated emissions and propulsion related OBD. The SAE J1979 Digital Annex supplements the J1979 base documents primarily by maintaining a global registry of regulated emissions and propulsion related data identifiers.
Vehicle E E System Diagnostic Standards Committee
Engine Rotation and Cylinder NumberingJ824_202206 (Current)6/29/2022
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
Signal and Marking Light SourcesJ573_202212 (Current)12/18/2022
Most signal and marking lighting devices have light sources (bulbs), which can be based on either filament or LED technology. To assure field replacement, it is important that light source types employed be readily available in normal service channels. This document defines the physical, electrical, and photometric characteristics necessary to achieve a proper replacement for popular types of signal and marking light sources. Some of the design characteristics in this document are listed solely for the sake of standardization and are not intended to describe the performance of lighting devices (lamp assemblies) on the vehicle. Halogen filament light sources suitable for signal and marking lighting are specified in SAE J2560.
Lighting Standard Practices Committee
Conical Spring WashersJ773_201608 (Current)8/31/2016
This SAE Standard covers dimensional, material, and general specifications and methods of test for two types of general purpose conical spring washers, designated type L and type H, for use as loose washers over screws and bolts, and also for use as pre-assembled washers in screw and washer assemblies.
Fasteners Committee
Dynamic Ozone Test Procedure--Hydraulic Brake HoseJ1914_198803 (Current)6/1/1988
The purpose of this recommended practice is to evaluate in the laboratory the effect of flexing on a brake hose when exposed to a high ozone concentration environment. This recommended practice is intended for all vehicle hydraulic brake hoses. It is an accelerated test which subjects the hose to dynamic ozone exposure.
Automotive Brake and Steering Hose Standards Comm
Hole Placement on Dozer End BitsJ63_199806 (Current)6/2/1998
The recommended practice applies to straight blade, angling blade, U blade, and semi-U blades used on earthmoving tractors per SAE J1057a up to a maximum weight of 100,000 lb (45,000 kg).
MTC1, Earthmoving Machinery
Manual Slack Adjuster Test ProcedureJ1461_201404 (Current)4/28/2014
This SAE Recommended Practice is intended for testing of manual slack adjusters as they are used in service, emergency, or parking brake systems for vehicles that can be licensed for on-road use.
Truck and Bus Foundation Brake Committee
Steel, Corrosion Resistant, Sheet, Strip, and Plate 15Cr - 6.5Ni - 0.75Mo - 0.60Cb - 1.5Cu Solution Heat Treated, Precipitation HardenableAMS5863F (Current)7/23/2021
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
Rings, Piston, Cast Iron As CastAMS7310M (Current)5/5/2026
This specification covers piston rings fabricated from cast iron.
AMS E Carbon and Low Alloy Steels Committee
Nickel, Corrosion and Heat Resistant, Sheet and Strip, Thoria Dispersion Strengthened, 2.2Th02AMS5865E (Current)11/30/2010
This specification covers thoria-dispersion-strengthened nickel powder metallurgy product in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 62Ni - 21.5Cr - 9.0Mo - 3.7Cb (Nb) (625)AMS5837H (Current)9/28/2023
This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
AMS F Corrosion and Heat Resistant Alloys Committee
Sheet and Strip, Flat-Rolled, Electrical, Non-Oriented, 2.65(Si+Al), Type 47S188 or Type 64S213, Semi-ProcessedAMS7711D (Current)9/1/2000
This specification covers two types of semi-processed silicon steel in the form of sheet and strip supplied in coils or cut lengths.
AMS E Carbon and Low Alloy Steels Committee
Rings, Flash Welded Corrosion and Heat-Resistant Austenitic Steels, Austenitic-Type Iron, Nickel or Cobalt Alloys, or Precipitation-Hardenable AlloysAMS7490R (Current)9/23/2025
This specification covers flash welded rings made of corrosion and heat-resistant austenitic steels and austenitic-type iron, nickel, or cobalt alloys, or precipitation-hardenable alloys.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion-Resistant, Investment Castings, 16Cr - 4.1Ni - 0.28Cb (Nb) - 3.2Cu (17-4), Homogenization, Solution, and Precipitation Heat Treated (H1000), 150 ksi (1034 MPa) Tensile StrengthAMS5343G (Current)10/1/2025
This specification covers a corrosion-resistant steel in the form of investment castings homogenized, solution, and precipitation heat treated to 150 ksi (1034 MPa) minimum tensile strength.
AMS F Corrosion and Heat Resistant Alloys Committee
Manufacturing Message Specification – Service Definition and ProtocolEIA511 (Current)7/1/2015
The Manufacturing Message Specification is an application layer Standard designed to support messaging communications to and from programmable devices in a Computer Integrated Manufacturing (CIM) environment. This environment is referred to in this Standard as the manufacturing environment. This Standard does not specify a complete set of services for remote programming of devices, although provision of such a set of services may be the subject of future standardization efforts. This Standard defines the Manufacturing Message Specification within the OSI application layer in terms of: a) an abstract model defining the interaction between users of the service; b) the externally visible functionality of implementations conforming to this Standard, in the form of procedural requirements associated with the execution of service requests; c) the primitive actions and events of the service; d) the parameter data associated with each primitive action and event; e) the relationship between
Systems Management Council
Software Life Cycle Processes – Implementation ConsiderationsIEEEEIA12207_2 (Current)7/1/2015
This guide provides implementation consideration guidance for the normative clauses of IEEE/EIA 12207.0. The guidance is based on software industry experience with the life cycle processes presented in IEEE/EIA 12207.0.
Systems Management Council
CDIF Integrated Meta-model - State/Event Model Subject AreaEIAIS116 (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.
Systems Management Council
Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion- and Heat-Resistant Procurement SpecificationAS7471K (Current)2/14/2023
This procurement specification covers bolts and screws made from a corrosion- and heat-resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered:
E-25 General Standards for Aerospace and Propulsion Systems
Tolerances Nickel, Nickel Alloy, and Cobalt Alloy Sheet, Strip, and PlateAMS2262J (Current)3/5/2025
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of nickel, nickel alloys, and cobalt alloys ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term “excl” is used to apply only to the higher figure of a specified range.
AMS F Corrosion and Heat Resistant Alloys Committee
Rework/Repair Handbook to Address the Implications of Lead-Free Electronics and Mixed Assemblies in Aerospace and High Performance Electronic SystemsGEIAHB0005_3 (Current)9/17/2015
This document provides technical background, procurement guidance, engineering procedures, and guidelines to assist organizations reworking/repairing aerospace and high performance electronic systems, whether they were assembled or previously reworked/repaired using traditional alloys such as SnPb or Pb-free alloys, or a combination of both solders and surface finishes. This document contains a review of known impacts and issues, processes for rework/repair, focused to provide the technical structure to allow the repair technician to execute the task. This document focuses on the removal and replacement of piece parts. For the purposes of this document, the term “Rework/Repair” is used as applicable. NOTE: The information contained within this document is based on the current knowledge of the industry at the time of publication. Due to the rapid changing knowledge base, this document should be used for guidance only.
G-24 Pb-free Risk Management Committee for ADHP
Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - Glass Fiber and Epoxy Resin, 7781 Weave FabricAMS3915B (Current)5/28/2026
The intent of this specification is for the procurement of 7781 glass fabric epoxy prepreg product with 250 °F (121 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (see 4.3).
AMS P17 Polymer Matrix Composites Committee
SPRING PINS, TUBULAR Corrosion and Moderate Heat Resistant SteelAMS7207G (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
BOLT, SHEAR - DOUBLE HEX HEAD, UNS N07718 - 185 KSIAS3574C (Current)5/4/2026
E-25 General Standards for Aerospace and Propulsion Systems
WIRE, RETAINER - TUBE COUPLING NUTAS1791E (Current)10/10/2023
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLTS AND SCREWS, LOW-ALLOY STEEL Heat Treated, Roll ThreadedAMS7452L (Current)5/1/1995
AMS E Carbon and Low Alloy Steels Committee
NUT ASSEMBLY COUPLING, RIGID, FIXED CAVITY, THREADED FERRULE TYPE TUBE ENDSAS1738C (Current)1/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
GASKET - 37° FLARED TUBE FITTING, NICKEL, AMS5553AS3074D (Current)9/5/2014
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
RIVET - 100 DEGREE COUNTERSUNK HEAD, ALUMINUM ALLOY (UNS A92117)AS125251C (Current)8/26/2022
E-25 General Standards for Aerospace and Propulsion Systems
Oil, Fluorescent Penetrant, Water WashableAMS3156E (Current)12/15/2008
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS2644. The requirements of the latest issue of AMS2644 shall be fulfilled whenever reference is made to the cancelled AMS3156. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS2644.
AMS K Non Destructive Methods and Processes Committee
Aerospace Fluid Systems and Components - Pressure and Temperature ClassificationsMA2001B (Current)8/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
RIVET - UNIVERSAL HEAD, ALUMINUM ALLOY (UNS A92117)AS125701C (Current)8/26/2022
E-25 General Standards for Aerospace and Propulsion Systems
FLANGE END, FEMALE, TYPE I STANDARD PROFILE DESIGN STANDARDAS1895/13E (Current)3/4/2018
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Tolerances Copper and Copper Alloy WireAMS2224H (Current)6/13/2023
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy wire ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted.
AMS D Nonferrous Alloys Committee
Polytetrafluoroethylene (PTFE) Sheet, Glass Cloth ReinforcedAMS3666E (Current)1/16/2012
This specification covers a glass-cloth-reinforced polytetrafluoroethylene (PTFE) resin in the form of sheet.
AMS P Polymeric Materials Committee
Aluminum Alloy, Extrusions, 4.4Cu - 1.5Mg - 0.60Mn (2024-O), AnnealedAMS4421A (Current)12/4/2024
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross-sectional area of 32 square inches (206 cm2), maximum (see 8.5).
AMS D Nonferrous Alloys Committee
COUPLING INSTALLATIONS, STANDARD CONDUIT, ELECTRICALAS10380B (Current)5/22/2023
AE-8A Elec Wiring and Fiber Optic Interconnect Sys Install
RETAINER, NUT AND BOLT, CUP LOCK, 5 MM AND 6 MM, AMS 5510, METRICMA3450A (Current)10/1/2018
E-25 General Standards for Aerospace and Propulsion Systems
MPR Micropitting Test MethodARP6991 (Current)6/1/2023
This method is designed to evaluate the micropitting performance of currently available and future aviation turbine oil formulations. Drawing on previously performed tests documented in AIR6989, the method comprises of three rings rotating against a rotating central roller configuration using the standard, commercially available PCS Instruments Micropitting Rig (MPR). A test profile has been developed between industry and academia that relies on standard, commercially available test specimens.
E-34 Propulsion Lubricants Committee
Automation Bulletin No. 3EIAAB3D (Current)7/1/2015
Systems Management Council
CDIF - Transfer Format General Rules for Syntaxes and EncodingsEIAIS108 (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 which 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
Beryllium Bars, Rods, Tubing, and Shapes, High Ductility GradeAMS7904F (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
CDIF - Transfer Format Syntax - SYNTAX.1EIAIS109 (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 which 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 the role that it plays in the CDIF Family of Standards
Systems Management Council
FITTING END, FLARELESS, BLUNT NOSE, DESIGN STANDARDAS4458B (Current)4/20/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD, METRICMA2023A (Current)4/24/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, CROSS, STANDARD AND REDUCER, FLAREDAS1036K (Current)8/25/2020
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FLANGE-ACCESSORY, 5” BOLT CIRCLEAS471C (Current)1/1/2001
AE-1 Engine Accessory Installations Committee
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