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Items (48,665)

Nickel Alloy, Corrosion- and Heat-Resistant, Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Vacuum Melted, Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile Strength

AMS5583G (Current)

05/17/2024

This specification covers a precipitation hardenable corrosion- and heat-resistant nickel alloy in the form of seamless tubing

AMS F Corrosion and Heat Resistant Alloys Committee

Identification Carbon and Low-Alloy Steels, Corrosion- and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing

AMS2807C (Current)

05/17/2024

This specification covers procedures for identifying carbon and low-alloy steels, corrosion- and heat-resistant steels and alloys, maraging and other highly alloyed steels, and iron alloy sheet, strip, and plate, and aircraft tubing

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Corrosion-Resistant, Sheet, Strip, and Plate 17Cr - 7.1Ni - 1.1Al (Alloy 17-7) Solution Heat Treated, Precipitation Hardenable

AMS5528K (Current)

05/17/2024

This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 0.005 to 1.000 inches (0.13 to 25.40 mm) in nominal thickness in the solution heat-treated condition

AMS F Corrosion and Heat Resistant Alloys Committee

Vacuum Gauge Calibration

ARP7446A (Current)

05/17/2024

This SAE Aerospace Recommended Practice (ARP) addresses the general procedure for the best practices for minimizing uncertainty when calibrating thermal conductivity and cold cathode vacuum gauges, which includes the vacuum sensor(s) and accompanying electronics necessary for a pressure measurement to be made. It also includes the best practices for an in-process verification where limitations make it impossible to follow the best practices for minimizing uncertainty. Verifying the accuracy and operation of vacuum gauges is critical to ensure the maintenance of processes while under vacuum

AMS B Finishes Processes and Fluids Committee

Aerospace Series - Notice of Change (NOC

AS9116A (Current)

05/17/2024

The aviation, space, and defense industries rely on the development and manufacture of complex products comprised of multiple systems, subsystems, and components each designed by individual designers (design activities) at various levels within the supply chain. Each design or manufacturing activity controls various aspects of the configuration and specifications related to the product. When a change to design or process is requested or required, the change is typically required to be evaluated against the impacts to the entire system. Proposed changes to design data/information that the design activity identifies to be minor and have no effect on the product requirements or specifications, have the potential to be implemented and approved, where authorized to do so, but requires notification. Changes that affect customer mandated requirements or specifications shall be approved prior to implementation. In many cases, the design activity is not conducted by the DAH or design authority

G-14 Americas Aerospace Quality Standards Committee (AAQSC)

Brake Rotor Thermal Cracking Procedure for Vehicles Below 4 540 kg GVWR

J2928_202405 (Current)

05/17/2024

This recommended practice is derived from common test sequences used within the industry. This procedure applies to all on-road passenger cars and light trucks up to 4 540 kg of GVWR. This recommended practice does not address other aspects such as performance, NVH, and durability. Test results from this recommended practice should be combined with other measurements and dynamometer tests (or vehicle-level tests), and acceptance criteria to validate a given design or configuration

Brake Dynamometer Standards Committee

Magnesium Alloy Welding Wire, 9.0Al - 2.0Zn (AZ92A

AMS4395G (Current)

05/17/2024

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

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Plate (7140-T7651) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged

AMS4408B (Current)

05/17/2024

This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.6 to 254.0 mm), inclusive, in nominal thickness (see 8.5

AMS D Nonferrous Alloys Committee

Enhanced Ultrasonic Immersion Inspection for Titanium Alloy and other Metal Alloy Billets

AMS2628C (Current)

05/17/2024

This specification covers procedures for ultrasonic immersion inspection of premium-grade wrought titanium and titanium alloy round billet 5 inches (127 mm) and over in nominal diameter (see 2.6.1). Metal alloy billets other than titanium may be tested to this specification with the use of suitable reference standards

AMS K Non Destructive Methods and Processes Committee

Test Method for the Determination of Water Concentration in Polyol Ester and Diester Aerospace Lubricants by Coulometric Karl Fischer Titration

ARP5991B (Current)

05/17/2024

The test method describes the procedure for the direct determination of water concentration in polyol ester and diester based aerospace lubricants by commercially available automated coulometric Karl Fischer titration instruments. The method was validated to cover the water concentration range of 150 to 3500 µg/g. The method may also be suitable for the determination of water concentrations outside this range and for other classes of fluids; however, the precision statement shall not be applicable for such uses

E-34 Propulsion Lubricants Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.1Ti - 1.4Al - 0.006B Vacuum Induction Melted, Solution Heat Treated

AMS5828H (Current)

05/17/2024

This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire

AMS F Corrosion and Heat Resistant Alloys Committee

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged

AMS4340H (Current)

05/17/2024

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 5.000 inches (127.00 mm), inclusive, in nominal diameter or least thickness (see 8.5

AMS D Nonferrous Alloys Committee

Sheet and Strip Surface Finish Nomenclature

AS4194B (Current)

05/16/2024

This SAE Aerospace Standard (AS) defines the nomenclature for surface finishes commonly used for sheet and strip in aerospace material specifications. It is applicable to steel and to iron, nickel, cobalt, and titanium base alloys

AMS F Corrosion and Heat Resistant Alloys Committee

Hard Anodic Coating on Aluminum and Aluminum Alloys

AMS2469L (Current)

05/16/2024

This specification establishes the requirements for a hard anodic coating on aluminum and aluminum alloys

AMS B Finishes Processes and Fluids Committee

Standard Practice for Habitability

SAE1007A (Current)

05/16/2024

This SAE Systems Management Standard specifies the Habitability processes throughout planning, design, development, test, production, use and disposal of a system. Depending on contract phase and/or complexity of the program, tailoring of this standard may be applied. Appendix C provides guidance on tailoring standard requirements to fit the various DoD acquisition pathways. The primary goals of a contractor Habitability program include: Ensuring that the system design complies with the customer Habitability requirements and that discrepancies are reported to management and the customer. Identifying, coordinating, tracking, prioritizing, and resolving Habitability risks and issues and ensuring that they are: ◦ Reflected in the contractor proposal, budgets, and plans. ◦ Raised at design, management, and program reviews. ◦ Debated in working group meetings. ◦ Coordinated with Training, logistics, and the other HSI disciplines. ◦ Included appropriately in documentation and deliverable

G-45 Human Systems Integration

All-Wheel Drive Systems Classification

J1952_202405 (Current)

05/16/2024

This document seeks to classify all-wheel drive (AWD) architectures primarily based on the installed hardware and does not consider the implementation of the controls and software. For example, a power transfer unit (PTU) may be equipped with a clutch that is capable of torque management, but the control implementation only uses it for disconnection functions without torque management. In this SAE Recommended Practice, attention will be given to passenger cars and light trucks (through Class III). The definitions presented herein may also be applicable to heavy trucks (Class 4 through 8) and off-highway applications using more than two axles but are primarily focused on passenger cars and light trucks

Drivetrain Standards Committee

LED Light Sources Tests and Requirements Standard

J2938_202405 (Current)

05/16/2024

This SAE Recommended Practice provides the methods of measurements for electrical and photometric characteristics of LED packages. It provides procedures, requirements, and guidelines for the methods of the measurement of luminous flux and color maintenance of LED devices (packages, arrays, and modules) for ground vehicle lighting applications

Lighting Standard Practices Committee

Galley Lighting

ARP712C (Current)

05/14/2024

This SAE Aerospace Recommended Practice (ARP) provides minimum standards and environmental design requirement recommendations for lighting and control in galley areas. It also addresses electrical shock hazard in galley areas. The use of “shall” in this document expresses provisions that are binding. Non-mandatory provisions use the term “should

A-20C Interior Lighting

Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility

ARP1070E (Current)

05/14/2024

This document outlines the development process and makes recommendations for total antiskid/aircraft systems compatibility. These recommendations encompass all aircraft systems that may affect antiskid brake control and performance. It focuses on recommended practices specific to antiskid and its integration with the aircraft, as opposed to more generic practices recommended for all aircraft systems and components. It defers to the documents listed in Section 2 for generic aerospace best practices and requirements. The documents listed below are the major drivers in antiskid/aircraft integration: 1 ARP4754 2 ARP4761 3 RTCA DO-178 4 RTCA DO-254 5 RTCA DO-160 6 ARP490 7 ARP1383 8 ARP1598 In addition, it covers design and operational goals, general theory, and functions, which should be considered by the aircraft brake system engineer to attain the most effective skid control performance, as well as methods of determining and evaluating antiskid system performance. For definitions of

A-5A Wheels, Brakes and Skid Controls Committee

Information on Brake-By-Wire (BBW) Brake Control Systems

AIR5372A (Current)

05/14/2024

This SAE Aerospace Information Report (AIR) describes the design approaches used for current applications of aircraft Brake-by-Wire (BBW) control systems. The document also discusses the experience gained during service, and covers system, ergonomic, hardware, and development aspects. The document includes the lessons that have been learned during application of the technology. Although there are a variety of approaches that have been used in the design of BBW systems, the main focus of this document is on the current state of the art systems

A-5A Wheels, Brakes and Skid Controls Committee

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance

ARP1947D (Current)

05/09/2024

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa

AMS D Nonferrous Alloys Committee

Aircraft Tire-to-Wheel Performance Characteristics

ARP5507A (Current)

05/09/2024

This SAE Aerospace Recommended Practice (ARP) defines the performance criteria and validation for tire circumferential movement on the rim, in the laboratory, by a static test, as well as a performance assessment in service. This document is applicable to braked wheel positions using both bias ply and radial aircraft tires

A-5C Aircraft Tires Committee

ARP5879A (Current)

05/09/2024

This SAE Aerospace Recommended Practice (ARP) provides recommended test requirements for electrohydrostatic actuators (EHAs

A-6B2 Electrohydrostatic Actuation Committee

Machine Requalification Considerations for Fusion-Based Metal Additive Manufacturing

ARP7064 (Current)

05/09/2024

This document defines a recommended practice for addressing metal additive manufacturing (AM) machine requalification for all fusion-based metal AM machines. In general, this applies to powder bed fusion (PBF) and wire- or powder-fed directed energy deposition (DED) technologies. Plasma, electron beam, or lasers are applicable energy source(s

AMS AM Additive Manufacturing Metals

J3350_202405 (Current)

05/09/2024

This SAE Standard describes the methods for testing flexible harness coverings for use on ground vehicle electrical distribution systems, specifically protection from severe mechanical impact. This SAE Standard shall apply to all tapes, extruded tubes, and textile sleeves used for this purpose

Harness Covering Standards Committee

Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form

AS7250E (Current)

05/09/2024

This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F

E-25 General Standards for Aerospace and Propulsion Systems

Nickel Alloy, Corrosion- and Heat-Resistant Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Solution Heat Treated, Precipitation Hardenable

AMS5582H (Current)

05/09/2024

This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness

AMS F Corrosion and Heat Resistant Alloys Committee

Engine Oil Viscosity Classification

J300_202405 (Current)

05/09/2024

This SAE Standard defines the limits for a classification of engine lubricating oils in rheological terms only. Other oil characteristics are not considered or included

Fuels and Lubricants TC 1 Engine Lubrication

Combined Cornering and Braking Test for Truck and Bus Tires

J2675_202405 (Current)

05/09/2024

This SAE Recommended Practice describes a test method for determination of heavy truck (Class VI, VII, and VIII) tire force and moment properties under combined cornering and braking conditions. The properties are acquired as functions of slip angle, normal force, and slip ratio. Slip angle and normal force are changed incrementally using a sequence specified in this document. At each normal force and slip angle increment, the slip ratio is continually changed by application of a braking torque ramp. The data are suitable for use in vehicle dynamics modeling, comparative evaluations for research and development purposes, and manufacturing quality control. This document is intended to be a general guideline for testing on an ideal machine. Users of this recommended practice may modify the recommended protocols to satisfy the needs of specific use-cases, e.g., reducing the recommended number of test loads and/or pressures for benchmarking purposes. However, due care is necessary when

Truck and Bus Tire Committee

Nuts, Self-Locking, UNS N07001 730 °C, 1100 MPa, and 1210 MPa Procurement Specification for, Metric

MA1943C (Current)

05/09/2024

This procurement specification covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) types of nuts made from a corrosion and heat-resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Tension height nuts having overall length of threaded portion not less than 1.2 times the nominal thread diameter have 1210 MPa minimum tensile strength at room temperature. Shear height nuts having shorter threaded portion have 1100 MPa minimum tensile strength at room temperature. Maximum test temperature of parts is 730 °C

E-25 General Standards for Aerospace and Propulsion Systems

Steel Tubing, Seamless 0.95Cr - 0.20Mo (0.28 - 0.33C) (SAE 4130), Aircraft Quality, 125 ksi (862 MPa) Tensile Strength

AMS6361H (Current)

05/09/2024

This specification covers aircraft-quality, low-alloy steel in the form of round, seamless tubing

AMS E Carbon and Low Alloy Steels 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

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

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

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

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

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

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, 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

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, 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 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

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

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

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

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

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

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