Search
Advanced Search
of the following are true
(
)

Results

Items (215,930)
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
FITTING ASSEMBLY, RING LOCKED, ADAPTER, FLARELESS TO PORT, EXTRA FINE THREADS, 5080 PSIAS5550D (Current)3/27/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Safety and Cybersecurity Recommendations for the Use of the Rust Language in Critical SystemsJA1020_202603 (Current)3/26/2026
This document provides guidance to using Rust in critical and safety-related software. The document summarizes how the usage of Rust supports in arguing safety according to ISO 26262 or RTCA DO-178C combined with RTCA DO-332. Cybersecurity best practices are referenced as these requirements largely overlap with those implemented for safety. As the Rust language is still evolving, this document targets the 2021 and 2024 editions of the language. Older or newer editions might require additional or changed rules and guidelines. Generally, the newest available edition of the language should be selected as newer editions remove ambiguities and outdated parts from the language.
Functional Safety Committee
Truck and Bus Aerodynamic Device and Concept TerminologyJ2971_202603 (Current)3/26/2026
This SAE J2971 Recommended Practice describes a standard naming convention of aerodynamic devices and technologies used to control aerodynamic forces on trucks and buses weighing more than 10000 pounds (including trailers).
Truck and Bus Aerodynamics and Fuel Economy Committee
BEARING, BALL, AIRFRAME ANTIFRICTION, EXTRA LIGHT DUTY CORROSION-RESISTANT NITROGEN STEEL (CREN)AS27642/1A (Current)3/25/2026
ACBG Rolling Element Bearing Committee
Aluminum Alloy Castings, 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (A206.0-T4), Solution Heat Treated and Naturally AgedAMS4236E (Current)3/25/2026
This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings with nominal wall thicknesses of up to 1.0 inch (25.4 mm), inclusive (see 8.8).
AMS D Nonferrous Alloys Committee
Stepping Surface Test Method for Heavy VehiclesJ3351_202602 (Current)2/12/2026
Define the test equipment and test procedures for measuring slip resistance for stepping, walking, and standing surfaces commonly used on heavy vehicles.
Truck and Bus Human Factors Committee
Shaft Nut and Keywasher Installation Dimensions forAS1495B (Current)3/20/2026
The purpose of this Standard is to provide installation dimensions for shaft nuts and their companion keywasher. The Standard type typically shown on MS9951 and MS9952, but is also suitable for parts which are dimensionally equivalent.
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SPANNER, AERONAUTICAL, UNS G41400AS172321B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3125-24 UNJF-3A X .2500-28 UNJF-3AAS3140C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .375-24 UNJF-3AAS3117B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
FITTING ASSEMBLY, PLUG, RING LOCKED PORT CONNECTION, 4000 PSI AND 5000 PSIAS5103B (Current)2/6/2026
SCOPE IS UNAVAILABLE.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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
Sheet, Polychlorotrifluoroethylene (PCTFE), Molded, UnplasticizedAMS3646E (Current)3/25/2026
This specification covers a 100% homopolymer of polychlorotrifluoroethylene (PCTFE) in the form of molded sheet 0.250 inch (6.35 mm) and under in nominal thickness.
AMS P Polymeric Materials Committee
CONTACT, ELECTRICAL CONNECTOR, CONCENTRIC TWINAX, PIN, SIZE 8AS39029/90D (Current)3/25/2026
AE-8C1 Connectors Committee
Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 15Cr - 6.5Ni - 0.75Mo - 0.30Cb - 1.5Cu (Custom 450), Consumable Electrode Melted, Solution Heat Treated, Precipitation HardenableAMS5859G (Current)3/25/2026
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of sheet, strip, and plate.
AMS F Corrosion and Heat Resistant Alloys Committee
CONNECTORS, RECEPTACLE, ELECTRIC, JAM NUT MOUNTING, FRONT RELEASE, CRIMP CONTACT, AN TYPEAS34041C (Current)3/25/2026
AE-8C1 Connectors Committee
Chassis Dynamometer Test Procedure - Heavy-Duty Road VehiclesJ2177_202603 (Current)3/25/2026
This SAE Recommended Practice has been adopted by SAE to specify: a. A standard procedure for chassis dynamometer testing of heavy-duty road vehicles for the purpose of determining power delivered through the drive tires. b. A method of correcting observed power to reference test conditions. c. A method of analyzing the test data to determine if the test results are within expected power ranges.
Engine Power Test Code Committee
Copper-Zinc Alloy, Laminated Sheet, 70Cu - 30Zn, Surface BondedAMS4508K (Current)3/25/2026
This specification covers a copper-zinc alloy (brass) in the form of laminated sheet with nominal thickness 0.006 to 0.125 inch (0.15 to 3.18 mm) (see 8.5).
AMS D Nonferrous Alloys Committee
Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings and Stock for Forgings and Rings, 50Ni - 20Cr - 20Co - 5.8Mo - 2.2Ti - 0.45Al (Nimonic® Alloy 263), Consumable Electrode or Vacuum Induction Melted, 2100 °F (1149 °C) Solution Heat TreatedAMS5886E (Current)3/13/2026
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
STUD - STRAIGHT, DRILLED, .2500-20UNS X .2500-28UNF-3AAS128363B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .2500-28 UNJF-3A X .1900-32 UNJF-3AAS3139C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Battery Industrial, Lead-Acid Type, for Use in Electric Powered Ground Support EquipmentARP1817B (Current)3/25/2026
This SAE Aerospace Recommended Practice (ARP) describes an industrial battery, lead-acid type, for use in electric powered ground support equipment.
AGE-3 Aircraft Ground Support Equipment Committee
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, UNS S66286, .5625-18 UNJF-3AAS3120B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .4375-20 UNJF-3AAS3118B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES (UNS S66286), .5000-20 UNJF-3AAS3119B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Polychlorotrifluoroethylene (PCTFE), Compression Molded, Heavy Sections, UnplasticizedAMS3645E (Current)3/16/2026
This specification covers a 100% homopolymer of polychlorotrifluoroethylene (PCTFE) in the form of sheet 0.250 inch (6.35 mm) and over in thickness, rod, heavy wall tubing, and large molded and machined parts.
AMS P Polymeric Materials Committee
Steel Cleanliness, Premium Aircraft-Quality, Magnetic Particle Inspection ProcedureAMS2300N (Current)3/25/2026
This specification covers steel cleanliness requirements for premium aircraft-quality ferromagnetic steels, including hardenable, corrosion-resistant steels, by magnetic particle inspection methods. This specification contains sampling, sample preparation, inspection procedures, and cleanliness rating criteria (see 8.2).
AMS E Carbon and Low Alloy Steels 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)7/1/1993
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of July 1, 1993.
AMS F Corrosion and Heat Resistant Alloys Committee
Alloy Forgings, Corrosion and Heat Resistant, 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.15b 0.10zr (0.30-0.35c), Solution, Stabilized, and Precipitation Heat TreatedAMS5881B (Current)1/1/1993
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of August, 1992.
AMS F Corrosion and Heat Resistant Alloys Committee
Alloy Powder, Corrosion and Heat Resistant, 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.015b 0.10zr (0.30-0.35c), as FabricatedAMS5855B (Current)1/1/1993
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of August, 1992.
AMS F Corrosion and Heat Resistant Alloys Committee
Graphite Fiber Tape and Sheet, Epoxy Resin Impregnated, G 150,000 (1034) Tensile, 15,000,000 (103) Modulus, 350 (177)AMS3894/6B (Current)12/1/1994
This specification covers one type of epoxy-resin-impregnated graphite fibers in the form of tape and sheet.
AMS P17 Polymer Matrix Composites Committee
Bolts and Screws Steel, Low Alloy Heat Resistant 195,000 Psi Hardened & Tempered, Roll ThreadedAMS7459E (Current)10/1/1993
AMS E Carbon and Low Alloy Steels Committee
Gaskets, Type Xx Engine Accessory Drive Corrosion Resistant Steelscreen Reinforced Controlled PerforAMS7283C (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Primer, Adhesive, Corrosion-Inhibiting -55 to +95°C (-67 to +203°F)AMS3106A (Current)12/1/1994
AMS CE Elastomers Committee
Retaining Rings, Steel Corrosion Resistant, Spiral WoundAMS7330B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Rings, Sealing, Tubular Metal, Corrosion and Heat Resistant SteelAMS7325F (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Cotter Pins, Steel 18cr 10.5ni 0.40ti, Corrosion and Heat Resistant SteelAMS7211G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
POLYTETRAFLUOROETHYLENEAMS3651D (Current)12/1/1994
AMS P Polymeric Materials Committee
POTTING COMPOUND, EPOXY, FLEXIBLE Durometer 75 - 85AMS3750 (Current)12/1/1994
AMS P Polymeric Materials Committee
Bolts and Screws, Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Heat Treated, Roll Threaded, 1950°F Solution Heat Treatment (AMS 5708)AMS7471G (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Fatigue ResistantAMS7466B (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
PLASTIC ROD AND BAR, POLYIMIDE Unfilled, MoldedAMS3644/1 (Current)9/1/1994
This specification covers an unfilled polyimide plastic in the form of molded rod and bar.
AMS P Polymeric Materials Committee
Rods, Sheets, and Molded Shapes, Polychlorotrifluoroethylene (PCTFE), UnplasticizedAMS3650E (Current)3/16/2026
This specification covers a 100% homopolymer of polychlorotrifluoroethylene (PCTFE) in the form of rods, sheets, and molded shapes.
AMS P Polymeric Materials Committee
CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS, PLUG (SERIES B)AS29600/22B (Current)3/16/2026
AE-8C1 Connectors Committee
BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTRA WIDE, DOUBLE ROW, INTERMEDIATE DUTY, CORROSION-RESISTANT NITROGEN STEEL (CREN)AS27647/1A (Current)3/16/2026
ACBG Rolling Element Bearing Committee
Urea Compound, PowderAMS1731B (Current)3/1/1994
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Bolts and Screws, Corrosion and Heat Resistant, Nickel Alloy, Upset Headed, Heat Treated, Roll Threaded, 2050°F (1120°C) Solution, 1650°F (900°C) Precipitation Heat TreatedAMS7469D (Current)10/1/1993
AMS F Corrosion and Heat Resistant Alloys Committee
Plating, Chromium, Hard DepositAMS2406R (Current)12/3/2025
This specification covers the requirements for electrodeposited hard chromium plate.
AMS B Finishes Processes and Fluids Committee
Tolerances, Aluminum And Aluminum Alloy Bar, Rod, Wire, And Forging Stock Rolled Or Cold-FinishedAMS2201M (Current)9/1/1994
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1994. The requirements of this specification are embodied in the latest issue of ANSI H35.2, Dimensional Tolerances for Aluminum Mill Products.
AMS D Nonferrous Alloys Committee
Items per page:
1 – 50 of 215930