Search
Advanced Search
of the following are true
(
)

Results

Items (213,158)
Aluminum Alloy Castings, Permanent Mold, 5.0Si - 1.2Cu - 0.50Mg (355.0-T6), Solution and Precipitation Heat TreatedAMS4281H (Current)09/12/2025
This specification covers an aluminum alloy in the form of permanent mold castings (see 8.6).
AMS D Nonferrous Alloys Committee
Vehicle, Magnetic Particle Inspection Petroleum BaseAMS2641D (Current)09/12/2025
This specification covers two types of refined hydrocarbon compounds in the form of liquids. This specification only covers newly manufactured materials.
AMS K Non Destructive Methods and Processes Committee
Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings, 53.3Ni - 16.5Cr - 17Mo - 4.5W - 5.8Fe - 0.40V (CW-12MW), As-CastAMS5388L (Current)09/12/2025
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
Hardware Protected Security Environment - GlobalPlatform Technologies Information ReportJ3101-5_202509 (Current)09/12/2025
The scope of the analysis is on the GlobalPlatform Secure Element (SE) and Trusted Execution Environment (TEE) standard specifications correspondence to SAE J3101 recommended practices. This analysis includes focuses on the platform specifications but not the scope of any future security application/applets. Both of these GlobalPlatform specifications have associated protection profiles to validate compliance, although GlobalPlatform does not currently have any specific SAE J3101 protection profiles. GlobalPlatform has communicated that it is assessing whether or not to develop application-level protection profiles to more explicitly cover the remaining requirements of SAE J3101 in order to allow for standardized testing and certification of complete solutions.
Vehicle Electrical System Security Committee
Aluminum Alloy, Castings, 5.0Si - 1.2Cu - 0.50Mg (C355.0-T6), Solution and Precipitation Heat TreatedAMS4215K (Current)09/12/2025
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings (see 8.6).
AMS D Nonferrous Alloys Committee
AIRCRAFT FIRE PROTECTION FOR RECIPROCATING AND GAS TURBINE ENGINE INSTALLATIONSAIR1076 (Current)09/11/2025
This document is reissued for application to helicopters.
S-12 Powered Lift Propulsion Committee
FRONT-MOUNTED LINKAGE FOR AGRICULTURAL WHEELED TRACTORSJ2131_199210 (Current)10/17/1992
This SAE Standard describes the requirements of the linkage to attach implements or equipment to the front of agricultural wheeled tractors. This shall be a three-point linkage in association with a power lift. It applies to the categories defined in ISO 730/1.
Agricultural Tractor Standards Committee (ATSC)
Performance Levels and Methods of Measurement of Electromagnetic Radiation From Vehicles and Devices, Narrowband, 10 Khz to 1000 MhzJ1816_198710 (Current)10/01/1987
With the advent of computer based electronics being utilized in automobiles, the Electromagnetic Radiation Subcommittee has deemed it prudent that a new test method be written to provide a common test for the measurement of narrowband radiation from vehicles and devices. This SAE Standard covers methods of measuring incidental narrowband radiation from vehicles and devices. The standard also establishes performance levels intended to protect nearby communication and broadcast receivers. It is intended to serve as an alternate method of measuring electromagnetic radiation which is analogous to the FCC Part 15 methodology but adapted to measuring vehicles. The equivalent procedures for broadband emissions are set forth in SAE J551. This standard covers narrowband emissions in the frequency range of 10 kHz to 1000 MHz. An example of such radiation is the unintended emission from on-board logic and computer modules. In particular, the standard is intended to provide protection to adjacent
Electromagnetic Compatibility (EMC) Standards
Specifications and Standards for Marine Hydraulic Systems and ComponentsJ1784_200008 (Current)08/20/2000
This document lists military and industry specifications and standards that are considered to be of particular interest to designers of marine vehicle hydraulic systems. SAE AIR737 lists additional aerospace hydraulic documents which occasionally may have application in marine hydraulic systems. This report is intended to assist marine hydraulic system designers in identifying military and industry specifications and standards that are suitable for use in marine hydraulic systems. The documents are listed according to specific categories and components. Documents that can be identified with more than one category are listed accordingly. The user is cautioned to use the latest revision of each document and to review the document carefully to determine the suitability of the document for the particular applications.
Ship Fluid Systems Committee
Supplemental High Mounted Stop and Rear Turn Signal Lamps for Use on Vehicles Less Than 2032 Mm in Overall WidthJ186_198912 (Current)12/01/1989
CANCELLED JANUARY 1996 This document provides design parameters, performance requirements, and general installation recommendations for supplemental high mounted stop and/or rear turn signal lamps, intended to supplement stop and/or rear turn signal lamps described in SAE J586 and SAE J588, for use on vehicles less than 2032 mm in overall width. Lamps for vehicles more than 2032 mm in width are covered in SAE J1432. Reason for cancellation: J1957 provides requirements for CHMSLS for vehicles less 2032 mm overall width. J186a is referenced in FMVSS 108.
Signaling and Marking Devices Stds Comm
Molybdenum Alloy Forgings 0.5 Ti 0.08 Zr Arc Cast, Stress RelievedAMS7821 (Current)12/16/2002
AMS G Titanium and Refractory Metals Committee
Tungsten Sheet and StripAMS7899 (Current)12/16/2002
AMS G Titanium and Refractory Metals Committee
Retaining Rings, Steel Corrosion Resistant, Spiral WoundAMS7330B (Current)10/01/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Molybdenum Alloy Bars 0.5 Ti Arc Cast, Stress RelievedAMS7813 (Current)12/16/2002
AMS G Titanium and Refractory Metals Committee
Molybdenum Forgings Powder Metallurgy, Sintered, Stress RelievedAMS7806A (Current)10/01/1982
AMS G Titanium and Refractory Metals Committee
Rings, Sealing, Tubular Metal, Corrosion and Heat Resistant SteelAMS7325F (Current)10/01/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Crew Restraint SystemARP998B (Current)08/01/2000
This ARP is intended to make recommendations for flight crew and cabin attendant restraint systems in aircraft. A properly designed crew restraint system will avoid injury or debilitation during a survivable crash and enable post crash assistance to occupants and escape from the aircraft. Consideration is given to existing requirements of the FAA and to the recommendations of aircraft operators and those involved in the manufacture or use of restraining devices. Crew member safety is the primary objective, with appropriate provisions for crew comfort taken into consideration. The criteria established herein are designed to standardize restraining systems without hindering the development of new, improved systems.
Aircraft Seat Committee
Magnetos, Aircraft, Installation OfAS14 (Current)07/01/1991
This Aerospace Standard establishes the diameter - pitch combinations of ISO metric 60 screw threads recommended for use in the aerospace industry for metric module shaft of bearing retaining screw threads.
E-30 Propulsion Ignition Systems Committee
Screw Heads, Flat Fillister - Large Fillet Aircraft EngineAS135 (Current)12/16/2002
E-25 General Standards for Aerospace and Propulsion Systems
Magnetos, Aircraft, Mountings ForAS12 (Current)04/01/1997
This specification covers three types of flanges for magneto mountings as follows: 1. Two-bolt Flange, 2. Three-bolt Flange, and 3. Four-bolt Flange.
E-30 Propulsion Ignition Systems Committee
Alloy Bars and Forgings, Corrosion and Heat Resistant, 38fe 13.2cr 38ni 5.5mo 0.85cb 2.5ti 1.6al 0.009b, Consumable Electrode Melted, Solution and Precipitation Heat TreatedAMS5634C (Current)07/01/1993
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of July 1, 1993.
AMS F Corrosion and Heat Resistant Alloys Committee
Welding Electrodes, Covered, Steel, Corrosion and Heat Resistant, 19.5cr 10ni 0.60(Cb+Ta)AMS5681E (Current)09/01/1996
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996, and has been superseded by AWS A5.4 E347. Alloy: 30347 UNS Number: W34710
AMS F Corrosion and Heat Resistant Alloys Committee
STEEL WIRE, CORROSION RESISTANT 17Cr - 7.1Ni - 1.1Al Precipitation Hardenable, Spring TemperAMS5673D (Current)07/01/1982
AMS F Corrosion and Heat Resistant Alloys Committee
Shipping Containers - Aircraft Engines and ComponentsAS338 (Current)05/01/1995
E-25 General Standards for Aerospace and Propulsion Systems
Alloy Bars and Forgings, Corrosion and Heat Resistant 25fe 20.5cr 20ni 20co 4.0mo 4.0w 4.0(Cb + Ta) Solution and Precipitation Heat TreatedAMS5770D (Current)01/01/1990
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of Januray 1990.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars and Forgings, Corrosion and Heat Resistant 13.5cr 26ni 3mo 1.8tiAMS5733E (Current)01/01/1990
A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. Bars, forgings, and stock for forging or heading. Primarily for parts and assemblies, requiring high strength up to 1250 degrees F (677 degrees C).
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars, Corrosion and Heat Resistant 16cr 25.5ni 6.2mo 0.15nAMS5725C (Current)01/01/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Forgings, Corrosion and Heat Resistant 16cr 25ni 6moAMS5727B (Current)01/01/1982
AMS F Corrosion and Heat Resistant Alloys Committee
Bars, Forgings, and Rings, Iron Base, 20.5cr 32ni 1.1tiAMS5742B (Current)10/01/1991
This spedification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of March, 1991.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion and Heat Resistant 13.5Cr - 26Ni - 1.75Mo - 3Ti Consumable Electrode Vacuum MeltedAMS5741D (Current)10/01/1982
AMS F Corrosion and Heat Resistant Alloys Committee
Steel, Corrosion Resistant, Covered Welding Electrodes 12.5crAMS5777E (Current)04/01/2001
This specification covers a corrosion-resistant steel in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Bars and Forgings 54ni 19cr 10co 10mo 1al 2.6ti 0.006b, Vacuum Melted, Solution Heat TreatedAMS5756D (Current)07/01/1990
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of January 1990.
AMS F Corrosion and Heat Resistant Alloys Committee
HOSE ASSEMBLY, CONVOLUTED NONMETALLIC, TFE FLARELESS, STRAIGHT TO 45°MA2121 (Current)08/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Tolerances, Metric, Aluminum Alloy and Magnesium Alloy Sheet and PlateMAM2202C (Current)08/01/1996
This specification covers established manufacturing tolerances applicable to aluminum alloy and magnesium alloy sheet and plate ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. These tables are based on logical metric values and preferred metric sizes. Throughout this specification, the term 'metric' is intended to refer to the SI system.
AMS D Nonferrous Alloys Committee
HOSE ASSEMBLY, CONVOLUTED, NONMETALLIC, TFE, FLARELESS, 90° TO 90°MA2125 (Current)08/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, CONVOLUTED, NONMETALLIC, TFE, FLARELESS, STRAIGHT TO STRAIGHTMA2120 (Current)08/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Packaging and Marking of Packages of Welding Wire Premium QualityAMS2814G (Current)08/06/2021
This specification covers spooling and packaging of bare welding wire to ensure cleanliness and freedom from corrosion, spool sizes and weights of spooled wire, and package weights of cut lengths.
AMS B Finishes Processes and Fluids Committee
Hose Assembly, Convoluted Polytetrafluoroethylene, High Temperature, Medium Pressure, Aircraft, MetricMA2079 (Current)08/21/2015
This Aerospace Standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -55°C (-67°F) to +204°C (400°F). Operating pressures are listed in Table I.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
HOSE ASSEMBLY, CONVOLUTED, NONMETALLIC, TFE, FLARELESS, 45° TO 90°MA2124 (Current)08/21/2015
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Tin Bronze Castings, Sand and Centrifugal 86.5cu 11.2sn 2.0zn as CastAMS4846B (Current)02/01/2001
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of 10-1-83. It is recommended that this specification not be specified for new designs. See AMS 4845 for a recommended substitute casting alloy.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Forgings 7.5zn 1.6mg 0.7cu 0.55mn (76s - T6)AMS4137A (Current)07/01/1981
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Forgings 4.5Cu 0.85Si 0.8Mn 0.5MgAMS4135M (Current)04/01/1986
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and stock for forgings on rolled rings. Primarily for applications, such as aircraft structural members, requiring material with moderately high strength. Certain design and processing procedures may cause these forgings to become susceptible to stress corrosion cracking; ARP 823 recommends practices to minimize such conditions.
AMS D Nonferrous Alloys Committee
Alloy Sheet and Strip, Corrosion and Heat Resistant Cobalt Base 20Cr 20Ni 4Mo 4W 4CbAMS5534B (Current)10/01/1991
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of March, 1991
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Bars and Rogings Corrosion and Moderate Heat Resistant 12.5cr 1.9ni AnnealedAMS5615D (Current)01/01/1991
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad 4.5cu 1.5mg 0.60mn (Alclad 2024-T86) Width 30 In. and UnderAMS4072 (Current)07/01/1981
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Sheet and Plate, Alclad 4.5 Cu - 1.5 Mg - 0.60 Mn - (Alclad 2024-T86) Width Over 30 to 48 In., Incl.AMS4073 (Current)07/01/1981
AMS D Nonferrous Alloys Committee
Steel Sheet and Strip, Low Heat Resistant (UNS S50100)AMS5502B (Current)10/01/1991
This document was cancelled.
AMS F Corrosion and Heat Resistant Alloys Committee
Ground Electrical Power Unit Brushless, Synchronous, Electric Motor-Driven 400 Hertz, 3-Phase OutputARP1480A (Current)09/01/1998
AGE-3 Aircraft Ground Support Equipment Committee
Flight Management Computer SystemARP1570 (Current)12/16/2002
The purpose of this document is to describe the recommendations of SAE Committee S-7 for a Flight Management Computer System (FMCS) capable of providing the functions and displays listed below to permit completion of a desired flight plan in an energy efficient and/or cost effective manner while meeting the requirements of Air Traffic Control. The recommendations of this document apply to transport aircraft and describe the operational objectives of the FMCS and related controls and displays.
S-7 Flight Deck Handling Qualities Stds for Trans Aircraft
Steel, Corrosion and Heat Resistant, Covered Welding Electrodes 25cr 20niAMS5695G (Current)06/01/2000
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Items per page:
1 – 50 of 213158