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Items (48,676)

Lubricant, Cetyl Alcohol, 1-Hexadecanol, Application to Fasteners

AS87132A (Current)

05/01/2024

This specification establishes the requirements for flake or granular cetyl alcohol, solvents for dissolving the cetyl alcohol, preparation and application requirements for use of cetyl alcohol as an installation lubricant on mechanical fasteners, such as pins, bolts, nuts, washers, threaded or nonthreaded fastening devices, and inspection criteria for coated parts

E-25 General Standards for Aerospace and Propulsion Systems

Emergency Evacuation Slides, Ramps, Ramp/Slides, and Slide/Rafts

AS8994 (Current)

05/01/2024

This AS provides the minimum performance requirements for the following types of inflatable emergency evacuation devices (hereinafter referred to as device[s]): 1 Type I - Inflatable Slide: A device suitable for assisting occupants in descending from a floor-level airplane exit or from an airplane wing to the ground. A Type I off-wing slide is a device that does not include a ramp. 2 Type II - Inflatable Slide/Raft: A device suitable for assisting occupants in descending from a floor-level airplane exit or an airplane wing to the ground that is also designed to be used as a life raft. A Type II off-wing slide/raft is a device that does not include a ramp. 3 Type III - Inflatable Exit Ramp: A device suitable for assisting occupants in descending from certain overwing exits to an airplane wing. 4 Type IV - Inflatable Ramp/Slide: A device suitable for assisting occupants from an overwing exit or airplane wing to the ground. It is a combination ramp and wing-to-ground device. 5 Type V

S-9A Safety Equipment and Survival Systems Committee

Architecture Framework for Unmanned Systems

AIR5665C (Current)

05/01/2024

This SAE Aerospace Information Report (AIR) describes the Architecture Framework for Unmanned Systems (AFUS). AFUS comprises a Conceptual View, a Capabilities View, and an Interoperability View. The Conceptual View provides definitions and background for key terms and concepts used in the unmanned systems domain. The Capabilities View uses terms and concepts from the Conceptual View to describe capabilities of unmanned systems and of other entities in the unmanned systems domain. The Interoperability View provides guidance on how to design and develop systems in a way that supports interoperability

AS-4JAUS Joint Architecture for Unmanned Systems Committee

Copper, Sheet, Strip, and Plate Soft Annealed

AMS4500L (Current)

05/01/2024

This specification covers unalloyed copper in the form of sheet, strip, and plate at least 0.015 inch (0.38 mm) in nominal thickness

AMS D Nonferrous Alloys Committee

Magnesium Alloy, Extrusions, 5.5Zn - 0.45Zr (ZK60A-T5), Precipitation Heat Treated

AMS4352K (Current)

05/01/2024

This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles up to 40 square inches (258 cm2) in cross-sectional area (solids) and up to 8.5 inches (216 mm) OD by 1.188 inches (30.18 mm) wall thickness (tubing) (see 8.5

AMS D Nonferrous Alloys Committee

Steel, Corrosion-Resistant, Bars, Wire, Forgings and Forging Stock 17Cr - 0.52Mo (0.95 - 1.20C) (SAE 51440C) for Bearing Applications

AMS5880F (Current)

05/01/2024

This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock

AMS F Corrosion and Heat Resistant Alloys Committee

Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized

AMS4375N (Current)

05/01/2024

This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.5

AMS D Nonferrous Alloys Committee

Lighting and Marking of Earthmoving Work Machines

J1029_202405 (Current)

05/01/2024

This SAE Standard establishes minimum requirements for lighting and marking earthmoving work machinery as defined in SAE J1116. It may be used as guidance for other types of machinery. Earthmoving work machines are normally operated off-highway. Therefore, this SAE document is not intended to be used as a basis for regulations by those having authority over on-highway motor vehicles

OPTC3, Lighting and Sound Committee

Aluminum Alloy, Extruded Profiles (2395-T84), 3.95Cu - 1.15Li - 0.3Ag - 0.5Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and Aged

AMS4359A (Current)

04/25/2024

This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 1.500 inches (1.02 to 38.10 mm), inclusive, in thickness, and produced with maximum cross-sectional area of 23.25 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 15.5 inches (394 mm) (see 2.4.1 and 8.6

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Alclad Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-O) Annealed, Fine Grained

AMS4278C (Current)

04/25/2024

This specification covers an aluminum alloy in the form of alclad sheet over 0.039 to 0.126 inches (0.99 to 3.20 mm), inclusive, in nominal thickness with a fine-grain core of ASTM No. 6 or finer (see 8.5

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Coiled Sheet, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024; -T4 Coiled Sheet), Solution Heat Treated

AMS4475C (Current)

04/25/2024

This specification covers an aluminum alloy in the form of alclad coiled sheet from 0.010 to 0.128 inch (0.25 to 3.25 mm), inclusive, in thickness supplied in the -T4 temper (see 8.5

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T861 Sheet and Plate), Solution Heat Treated, 6% Cold Worked and Artificially Aged

AMS4467C (Current)

04/25/2024

This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temper

AMS D Nonferrous Alloys Committee

Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °C

AMS3276H (Current)

04/25/2024

This specification covers fuel-resistant polysulfide (T) sealing compounds supplied as a two-component system

AMS G9 Aerospace Sealing Committee

Aluminum Alloy, Sheet and Plate, 2.5Mg - 0.25Cr (5052-H32), Strain Hardened, Quarter-Hard, and Stabilized

AMS4016N (Current)

04/25/2024

This specification covers an aluminum alloy in the form of sheet and plate 0.017 to 2.000 inches (0.43 to 50.80 mm), inclusive, in nominal thickness (see 8.6

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Plate (7160-T7651), 7.0Zn - 2.2Cu - 1.5Mg - 0.10Zr, Solution Heat Treated, Stress Relieved, and Overaged

AMS4378A (Current)

04/25/2024

This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inches (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.5

AMS D Nonferrous Alloys Committee

Tape for Organic Coatings Adhesion Testing

AMS3721A (Current)

04/25/2024

This specification establishes requirements for a tape that is used to perform organic coatings adhesion testing

AMS G8 Aerospace Organic Coatings Committee

Titanium Alloy Bars, Forgings, and Flash-Welded Rings, 5Al - 2.5V - 4Sn - 1Co - 0.8Fe Annealed

AMS6903 (Current)

04/25/2024

This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up through 12.000 inches (304.80 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings. Bars, forgings, and flash-welded rings with a nominal thickness of 3.000 inches (79.20 mm) or greater shall have a maximum cross-sectional area of 113 square inches (729 cm2) (see 8.5

AMS G Titanium and Refractory Metals Committee

Aluminum Alloy Sheet, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T4 Flat Sheet), Solution Heat Treated, High Formability

AMS4297C (Current)

04/25/2024

This specification covers an aluminum alloy in the form of sheet 0.020 to 0.128 inch (0.51 to 3.25 mm), inclusive, in nominal thickness (see 8.5

AMS D Nonferrous Alloys Committee

Elastomer: Silicone Rubber (MQ/VMQ), General Purpose, 35 - 45 Durometer Type ‘A’ Hardness

AMS3301K (Current)

04/25/2024

This specification covers a silicone (MQ/VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications

AMS CE Elastomers Committee

Titanium Alloy Bars, Forgings and Forging Stock, 6.0Al - 6.0V - 2.0Sn, Solution Heat Treated and Aged

AMS6935D (Current)

04/25/2024

This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 32 square inches (204.46 cm2), and stock for forging of any size (see 8.6

AMS G Titanium and Refractory Metals Committee

Titanium Alloy Welding Wire, 5Al - 2.5Sn

AMS4953J (Current)

04/25/2024

This specification covers a titanium alloy in the form of welding wire (see 8.5

AMS G Titanium and Refractory Metals Committee

Castings, Classification and Inspection

AMS2175B (Current)

04/25/2024

This specification establishes nondestructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castings

AMS B Finishes Processes and Fluids Committee

Plain Spherical Bearing Conformity Examination

ARP5448/6A (Current)

04/24/2024

This method outlines a standard procedure for performing conformity tests of bearings utilizing liners of bonded polytetrafluoroethylene (PTFE). The data from these tests shall be used to determine if the product meets the conformity requirements of the applicable specification

ACBG Plain Bearing Committee

BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), . 3750-24, UNJF-3A

AS3170B (Current)

04/24/2024

E-25 General Standards for Aerospace and Propulsion Systems

Clamp - Tube Support, Spring Clips and PTFE Cushion, Procurement Specification

MA3399A (Current)

04/24/2024

This procurement specification covers the requirements for metal tube support clamps comprising of two spring clips made of corrosion and heat resistant steel and the associated PTFE single split cushion that supports the tube. See Figure 1

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

BOLT, TEE HEAD - NICKEL ALLOY (UNS N07718), CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANT

AS3411E (Current)

04/24/2024

E-25 General Standards for Aerospace and Propulsion Systems

Flareless Hydraulic Tube Fittings

J514/2_202404 (Current)

04/23/2024

This SAE Standard covers complete general and dimensional specifications for flareless type of hydraulic tube fittings. These fittings are intended for general application in hydraulic systems on industrial equipment and commercial products. These fittings are capable of providing leakproof, full flow connections in hydraulic systems operating at working pressures as specified in Table 1. For any application, it is recommended that sufficient testing be conducted and reviewed by both the user and fitting manufacturer to assure that performance levels will be safe and satisfactory. Formerly, SAE J514 was organized as a single document with ten clauses, which included six sections. This revision of SAE J514 has been organized into three sections as follows: Part 1: 37-degree flared fittings Part 2: Flareless (bite type) fittings Part 3: NPTF pipe fittings and pipe unions It is important to note that this and all SAE J-documents are intended for ground vehicle use only and not intended

Hydraulic Tube Fittings Committee

PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800

AS9842B (Current)

04/23/2024

E-25 General Standards for Aerospace and Propulsion Systems

Aerospace Hydraulic and Pneumatic Specifications, Standards, Recommended Practices, and Information Reports

AIR737G (Current)

04/23/2024

This SAE Aerospace Information Report (AIR) lists military and industry specifications, standards, recommended practices, and information reports applicable to aerospace hydraulic and pneumatic systems and components

A-6 Aerospace Actuation, Control and Fluid Power Systems

Off-Road Self-Propelled Work Machines Operator Enclosure Environment Part 1: Terms and Definitions

J3078/1_202404 (Current)

04/23/2024

SAE J3078 provides test methods and criteria for the evaluation of the operator enclosure environment in earth-moving machinery as defined in ISO 6165. SAE J3078/1 gives the terms and definitions which are used in other parts of SAE J3078. It is applicable to Off-Road Self-Propelled Work Machines as defined in SAE J1116 and tractors and machinery for agriculture and forestry as defined in ANSI/ASAE S390

HFTC6, Operator Accommodation

Rivets, Solid, UNS N04400, Corrosion Resistant 67Ni - 31Cu Procurement Specification

AS7233A (Current)

04/23/2024

This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi minimum shear strength

E-25 General Standards for Aerospace and Propulsion Systems

Rivets, UNS S66286, Steel, Corrosion and Heat Resistant, 80 ksi Shear Strength, Procurement Specification

AS7235A (Current)

04/23/2024

This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 80 ksi single shear strength at room temperature

E-25 General Standards for Aerospace and Propulsion Systems

NUT, PLAIN, HEXAGON, CADMIUM PLATED, UNS G87400, 125 KSI MIN

AS9881C (Current)

04/23/2024

E-25 General Standards for Aerospace and Propulsion Systems

Liquid Leak Tightness Evaluation Methodology for EV Battery Packs Informational Report

J3277_202404 (Current)

04/23/2024

This technical information report (IR) presents a methodology to evaluate battery pack liquid leak tightness attributes to be used in a production line to satisfy the functional requirement for IPX7, water ingress requirement, and no sustainable coolant leakage for coolant circuits. The Equivalent Channel Method is used as a suggested production leak tightness requirement for a given battery pack design that will correlate and assure that the battery pack meets or exceeds its functional requirement. Obtaining the specific geometry of the Equivalent Channel (EC) for a given battery pack is done analytically and empirically in consideration of the product design limitations. This document is a precursor to J3277-1, which will present the practices to qualify that product leak tightness is equal or better than the maximum allowed EC for that product using applicable and commercially available leak test technologies. This document may be applied to EV and HEV battery packs as tested during

Battery Standards Testing Committee

Fuel Flow Rate Measurement System

AS407E (Current)

04/23/2024

This SAE Aerospace Standard (AS) defines minimum performance standards (MPS) for fuel flowmeters, fuel flow indicators, and fuel flow transmitters. The fuel flow indicators and transmitters are intended for use in 14 CFR Part 23, 25, 27, and 29 aircraft equipped with reciprocating and turbine engines. Multiple function displays are not within the scope of this SAE Aerospace Standard (refer to AS6296

A-4FLW Fuel Flowmeters

BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTRA LIGHT DUTY, CORROSION RESISTANT NITROGEN STEEL (CREN

AS27646/1B (Current)

04/23/2024

ACBG Rolling Element Bearing Committee

Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement Specification

AS7234A (Current)

04/23/2024

This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivets

E-25 General Standards for Aerospace and Propulsion Systems

Tire Burst Test Methodology

ARP6265 (Current)

04/17/2024

This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanes

A-5C Aircraft Tires Committee

Aircraft New Tire Standard - Bias and Radial

AS4833A (Current)

04/17/2024

This SAE Aerospace Standard (AS) sets forth criteria for the selection and verification processes to be followed in providing tires that will be suitable for intended use on civil aircraft. This document encompasses new and requalified radial and bias aircraft tires

A-5C Aircraft Tires Committee

Fuel and Lubricant Tanks for Motorcycles

J1241_202404 (Current)

04/15/2024

This SAE Recommended Practice is applicable to two- or three-wheel motorcycles intended for highway use. Unless noted, requirements apply to both metallic and nonmetallic tanks. Accessory or aftermarket tanks as well as original equipment tanks are covered

Motorcycle Technical Steering Committee

Aerospace - Accumulator, Hydraulic, Cylindrical, Piston Separated

ARP4379B (Current)

04/15/2024

This SAE Aerospace Recommended Practice (ARP) is a guide for defining the requirements for aerospace piston hydraulic accumulators, including details pertinent to the design, fabrication, performance and testing of the accumulator. This type of accumulator contains a piston which separates pressurized gas and fluid

A-6C4 Power Sources Committee

BOLT, SHEAR – DOUBLE HEX HEAD, DRILLED SHANK AMS5853 – 160 KSI

AS3529A (Current)

04/10/2024

E-25 General Standards for Aerospace and Propulsion Systems

Component Nomenclature - Skidder - Grapple

J1111_202404 (Current)

04/10/2024

This SAE Standard characterizes grapple skidders and identifies the major components and parts most commonly associated therewith. Illustrations used herein are not intended to include all existing commercial machines or to be exactly descriptive of any particular machine. They have been included to facilitate application of this document

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J1939 Digital Annex

J1939DA_202404 (Current)

04/10/2024

This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier use

Truck Bus Control and Communications Network Committee

CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR AS81659 SERIES 2 CONNECTORS

AS39029/11D (Current)

04/10/2024

AE-8C1 Connectors Committee

PIN, EXPANSION - ALUMINUM, 2024-T4 AND 2024-T351, SHORT, UNS A92024

AS3124B (Current)

04/10/2024

E-25 General Standards for Aerospace and Propulsion Systems

NUT, PLAIN, CASTELLATED, HEXAGON - UNS S66286, 130 KSI MIN

AS9358B (Current)

04/10/2024

E-25 General Standards for Aerospace and Propulsion Systems

Rings, Retaining – Spiral Wound, Uniform Section Corrosion and Heat Resistant, UNS S66286

AS4299B (Current)

04/10/2024

This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, work strengthened and heat treated to a tensile strength of 185 to 240 ksi at room temperature

E-25 General Standards for Aerospace and Propulsion Systems

INSERT - CRES HELICAL COIL FINE THREAD, STRAIGHT, STUD LOCKING, 2 DIA NOM LENGTH

AS3081A (Current)

04/10/2024

E-25 General Standards for Aerospace and Propulsion Systems

BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .1900-32 UNJF-3A

AS3250D (Current)

04/10/2024

E-25 General Standards for Aerospace and Propulsion Systems

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