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Items (212,033)

01/09/2025

This specification covers requirements for the superfinishing of High Velocity Oxygen/Fuel (HVOF) applied tungsten carbide thermal spray coatings

AMS B Finishes Processes and Fluids Committee

Metallic Whiskers

AIR4129A (Current)

01/09/2025

This AIR presents an abbreviated review of the metallurgical phenomena known as whiskers. It is not all encompassing; rather, it is intended to introduce the design engineer to the technical issues of metallic whiskers, their formation, and the potentially dangerous problems they can cause

AMS B Finishes Processes and Fluids Committee

Aerospace - Evaluation of Particulate Contamination in Hydraulic Fluid - Membrane Procedure

ARP4285A (Current)

01/09/2025

This SAE Aerospace Recommended Practice (ARP) establishes a method for evaluating the particulate matter extracted from the working fluid of a hydraulic system or component using a membrane. The amount of particulate matter deposited on the membrane due to filtering a given quantity of fluid is visually compared against a standard membrane in order to provide an indication of the cleanliness level of the fluid

A-6C1 Fluids and Contamination Control Committee

INSERT, SCREW THREAD, HELICAL COIL, METRIC SERIES, FREE RUNNING, CRES, UNCOATED

MA3279D (Current)

01/09/2025

E-25 General Standards for Aerospace and Propulsion Systems

LEDs and Aircraft Applications

ARP6253A (Current)

01/09/2025

This document presents minimum criteria for the design and installation of LED assemblies in aircraft. The use of "shall" in this specification expresses provisions that are binding. Nonmandatory provisions use the term "should

A-20C Interior Lighting

Air in Aircraft Hydraulic Systems

AIR5829 (Current)

01/09/2025

This SAE Aerospace Information Report (AIR) discusses the forms that air may take in aircraft hydraulic systems. Further, the effects of the various air forms on system operation are addressed. Recommended system design to prevent air effects and maintenance procedures to prevent and remove air are provided. Nitrogen leakage from accumulators is also a source of gas in hydraulic systems and may compose a portion of the “air” in the hydraulic system. The term “air” in this report does not differentiate between a gas composed strictly of normal atmospheric air or one that includes a mixture of additional nitrogen as well. The discussions of the report apply equally with any proportions of atmospheric air and nitrogen in the system

A-6C1 Fluids and Contamination Control Committee

Actuators, Linear Mechanical, General Specification Guide

ARP5812 (Current)

01/09/2025

This SAE Aerospace Recommended Practice (ARP) establishes design, manufacturing performance and test requirements for linear mechanical actuators intended to be used for linear motion applications in response to manual or automatic power control system inputs. It is applicable, but not confined to, ball screws, sliding contact screws, roller screws, helical splines, rack and pinion assemblies, and skewed roller actuators. It is a reference for preparing detail specifications for mechanical actuators compatible and applicable to military or commercial aircraft systems

A-6B3 Electro-Mechanical Actuation Committee

Method for Predicting Lateral Attenuation of Airplane Noise

AIR5662 (Current)

01/09/2025

This document describes analytical methods for calculating the attenuation of the level of the sound propagating from an airplane to locations on the ground and to the side of the flight path of an airplane during ground roll, climbout after liftoff, and landing operations. Both level and non-level ground scenarios may be modeled using these methods, however application is only directly applicable to terrain without significant undulations, which may cause multiple reflections and/or multiple shielding effects. This attenuation is termed lateral attenuation and is in excess of the attenuation from wave divergence and atmospheric absorption. The methods for calculating the lateral attenuation of the sound apply to: turbofan-powered transport-category airplanes with engines mounted at the rear of the fuselage (on the sides of the fuselage or in the center of the fuselage as well as on the sides) or under the wings propeller-driven transport-category or general-aviation airplanes

A-21 Aircraft Noise Measurement Aviation Emission Modeling

Flux, Aluminum Dip Brazing, 1090°F (588°C), Fusion Point

AMS3416B (Current)02/11/2005

This specification covers an aluminum brazing flux in granular form

AMS B Finishes Processes and Fluids Committee

Aluminum Silicon Bronze Bars, Rods, and Forgings, 90cu 7.0al 1.9si, Drawn and Stress Relieved

AMS4263A (Current)01/01/1993

This specification has been declared 'Superseded' by the Aerospace Materials Division, SAE, as of September, 1992. The requirements of this specification are embodied in the latest issue of AMS 4633. UNS Number: C64200 Alloy: HR50

AMS D Nonferrous Alloys Committee

Magnesium Alloy, Sand Castings 4.0Y - 2.3Nd - 0.7Zr (WE43B - T6) Solution and Precipitation Heat Treated

AMS4427D (Current)08/28/2019

This specification covers a magnesium alloy in the form of sand castings

AMS D Nonferrous Alloys Committee

STEEL WELDING ELECTRODES, COVERED, CORROSION RESISTANT 16.4Cr - 4.8Ni - 0.22(Cb + Ta) - 3.6Cu

AMS5827C (Current)08/15/2011

This specification covers a corrosion-resistant steel in the form of covered welding electrodes

AMS F Corrosion and Heat Resistant Alloys Committee

Magnesium Alloy Castings, Sand, 3.3Th - 2.1Zn - 0.75Zr (HZ32A-T5), Precipitation Heat Treated

AMS4447F (Current)06/21/2006

This specification covers a magnesium alloy in the form of sand castings

AMS D Nonferrous Alloys Committee

Steel, Corrosion and Moderate Heat Resistant, Bars, Forgings, and Rings, 14.5Cr - 6.5Ni - 0.72Ti, Solution Heat Treated and Maraged, 180,000 psi (1240 MPa) Tensile Strength

AMS5739E (Current)05/15/2006

This specification covers a corrosion and moderate heat resistant steel in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings

AMS F Corrosion and Heat Resistant Alloys Committee

Magnesium Alloy, Sheet and Plate, 3.2Th - 0.70Zr, Cold Rolled and Partially Annealed

AMS4385K (Current)10/30/2006

This specification covers a magnesium alloy in the form of sheet and plate

AMS D Nonferrous Alloys Committee

Forgings, Magnesium Alloy, 2.0Th - 0.78Mn (HM21A - T5), Precipitation Heat Treated

AMS4363G (Current)06/21/2006

This specification covers a magnesium alloy in the form of die forgings, hand forgings, rolled rings, and forging stock

AMS D Nonferrous Alloys Committee

Magnesium Alloy Castings, Sand, 3.5Ce - 0.7Zr (EK41A-T6), Solution and Precipitation Heat Treated

AMS4441E (Current)06/21/2006

This specification covers a magnesium alloy in the form of sand castings

AMS D Nonferrous Alloys Committee

Magnesium Alloy Castings, Sand, 5.7Zn - 1.8Th (ZH62A-T5), Precipitation Heat Treated

AMS4438E (Current)06/21/2006

This specification covers a magnesium alloy in the form of sand castings

AMS D Nonferrous Alloys Committee

STUDS, LOW-ALLOY HEAT-RESISTANT STEEL Normalized and Tempered, Roll Threaded 135,000 psi (931 MPa) Tensile Strength

AMS7458F (Current)08/15/2011

AMS E Carbon and Low Alloy Steels Committee

Shims, Molded, Filled Resin Compound and Sheet Prepeg

AMSS83474B (Current)

07/06/2016

This specification covers the requirements for filled, resinous thermosetting compound and sheet pre-preg to fabricate shims for use during assembly of aircraft and marine components and parts

AMS P Polymeric Materials Committee

Tape and Sheet, Adhesive, Rubber and Cork Composition

AMST6841A (Current)07/06/2016

This specification covers one type of tape and sheet for use in the installation of windshields, panels, and windows in cabins and cockpits of aircraft

AMS P Polymeric Materials Committee

Paper, Recording, Heat Sensitive

AMSP22968A (Current)

07/06/2016

This specification presents the requirements for one type of a heat-sensitive recording paper, in roll form, that furnishes permanent marking or tracing on one side

AMS P Polymeric Materials Committee

Tolerances, Metric, Nickel, Nickel Alloy, and Cobalt Alloy Tubing

MAM2263B (Current)09/13/2007

This specification covers established metric manufacturing tolerances applicable to seamless and welded thin-walls aircraft tubing of nickel, nickel alloys, and cobalt alloys ordered to metric dimensions. These tolerances apply to all conditions and are based on individual measurements, 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

Tolerances, Metric, Corrosion and Heat Resistant Steel Tubing

MAM2243D (Current)09/13/2007

This specification covers manufacturing tolerances applicable to seamless and welded tubing of corrosion and heat resistant steel ordered to metric dimension. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. Tubing may be specified by two dimensions only (OD and wall thickness, ID and wall thickness, or OD and ID

AMS F Corrosion and Heat Resistant Alloys Committee

Steel Cleanliness, Aircraft Quality, Martensitic Corrosion-Resistant Steels, Magnetic Particle Inspection Procedure, Metric (SI) Measurement

MAM2303E (Current)07/19/2007

This specification covers steel cleanliness requirements in SI (Metric) units for aircraft-quality, ferromagnetic, hardenable, corrosion-resistant steels as determined by magnetic particle inspection methods. This specification contains sampling, specimen preparation, and inspection procedures and cleanliness rating criteria

AMS F Corrosion and Heat Resistant Alloys Committee

Wire - Steel, Corrosion and Heat Resistant, Safety, 1800°F

AMS9226A (Current)01/26/2006

No Scope available

AMS F Corrosion and Heat Resistant Alloys Committee

Silicone Resin, Elastomeric, Opaque, Room Temperature Cure

AMS3371A (Current)06/16/2009

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED". Cancelled specifications are available from SAE

AMS G9 Aerospace Sealing Committee

Aluminum Alloy, Drawn Seamless Tubing, 1.2Mn - 0.12Cu (3003-O), Annealed

AMS4065K (Current)07/13/2007

This specification covers an aluminum alloy in the form of drawn seamless tubing

AMS D Nonferrous Alloys Committee

Aluminum Alloy, Drawn Seamless Round Tubing, (1100-H14), Strain Hardened

AMS4062J (Current)07/13/2007

This specification covers an aluminum alloy in the form of drawn seamless round tubing

AMS D Nonferrous Alloys Committee

Sealing Compound, Thread and Gasket, Fuel, Oil, and Water Resistant

AMSS7916B (Current)07/08/2009

This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of July 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED

AMS G9 Aerospace Sealing Committee

Aluminum Alloy Castings, Sand, 4.0Cu - 2.1Ni - 2.0Mg - 0.30Cr - 0.30Mn - 0.13T - 0.13V (243.0), Stabilized

AMS4224C (Current)01/05/2010

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of January 2010 and no superseding specification is identified. By this taction, this document will remain listed in the Numercial Section of the Index of Aerospace Material Specifications, noting that it has been cancelled. This specification covers an aluminum alloy in the form of sand castings. Primarily for components operating up to 600 °F (315 °C

AMS D Nonferrous Alloys Committee

Tolerances, Metric, Low-Alloy Steel Sheet, Strip, and Plate

MAM2252C (Current)07/13/2007

This specification covers established metric manufacturing tolerances applicable to low-alloy steel sheet, strip, and plate ordered to metric dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range

AMS E Carbon and Low Alloy Steels Committee

Cloth, Aramid Intermediate Modulus

AMS3909B (Current)

10/04/2022

This specification and its supplementary detail specifications cover an intermediate modulus aramid yarn in the form of cloth

AMS P17 Polymer Matrix Composites Committee

Spring Pins, Tubular, Carbon Steel

AMS7205G (Current)02/15/2008

This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole

AMS E Carbon and Low Alloy Steels Committee

Compound, Alkaline Degreaser Aircraft Turbine Engine Components

AMS1741 (Current)

04/15/2015

This specification covers an alkaline degreaser compound in the form of a liquid concentrate or a water-soluble powder for dilution with water

AMS J Aircraft Maintenance Chemicals and Materials Committee

Compound, Alkaline Solvent Cleaner Aircraft Turbine Engine Components Room Temperature Application

AMS1742 (Current)

04/15/2015

This specification covers a solvent cleaning compound in the form of a liquid

AMS J Aircraft Maintenance Chemicals and Materials Committee

BOLTS AND SCREWS, CARBON STEELS, ALLOY STEELS OR CORROSION AND HEAT RESISTANT STEELS OR ALLOYS Roll Threaded

AMS7473E (Current)05/01/1995

AMS E Carbon and Low Alloy Steels Committee

Steel Bars Free-Machining Cold Drawn (SAE 1212 or SAE 1215

AMS5010L (Current)

12/23/2014

This specification covers a free-machining carbon steel in the form of bars

AMS E Carbon and Low Alloy Steels Committee

BOLTS AND SCREWS, CORROSION HEAT RESISTANT NICKEL ALLOY Upset Headed, Heat Treated, Roll Threaded 2050°F (1121°C) Solution and 1650°F (899°C) Precipitation Heat Treated

AMS7469C (Current)05/01/1995

AMS F Corrosion and Heat Resistant Alloys Committee

BOLTS AND SCREWS, CORROSION AND HEAT RESISTANT STEEL Heat Treated, Roll Threaded 1650°F (899°C) Solution and Precipitation Heat Treated

AMS7479D (Current)05/01/1995

AMS F Corrosion and Heat Resistant Alloys Committee

BOLTS AND SCREWS, CORROSION AND HEAT RESISTANT STEEL Upset Headed, Heat Treated, Roll Threaded 1800°F (982°C) Solution and Precipitation Heat Treated

AMS7477C (Current)

05/01/1995

AMS F Corrosion and Heat Resistant Alloys Committee

Deodorant, Aircraft Toilet

AMS1476C (Current)01/12/2016

This specification covers a biodegradable deodorant in the form of a liquid concentrate, solid, or gel

AMS J Aircraft Maintenance Chemicals and Materials Committee

IRON BAR, SHEET, STRIP, AND PLATE, COMMERCIALLY PURE Hot Rolled, Annealed

AMS7706A (Current)10/01/1991

AMS E Carbon and Low Alloy Steels Committee

Inspection Process, Magnetic Rubber

AMSI83387B (Current)

01/06/2016

This specification covers both the material and the examination process of an inspection material in the form of a dispersion of magnetic particles in a controlled viscosity rubber base that cures at room temperature by addition of one or more curing agents. The test object is magnetized with the uncured rubber covering the area of interest. The magnetic particles then migrate to the leakage field caused by the discontinuity. As the rubber cures, discontinuity indications remain in place on the rubber. The product may be supplied in a variety of viscosities and colors

AMS K Non Destructive Methods and Processes Committee

Balls, Steel, Low-Chromium, High Carbon Hardened and Tempered

AMS7440E (Current)

01/04/2016

This specification covers balls made of a low-chromium, high-carbon steel

AMS E Carbon and Low Alloy Steels Committee

Tube, Aluminum, Drawn, Seamless, 1100

AMSWWT700/1A (Current)04/13/2007

This specification covers the specific requirements for seamless tube drawn from aluminum 1100

AMS D Nonferrous Alloys Committee

Aluminum 1100, Plate and Sheet

AMSQQA250/1A (Current)04/13/2007

AMS D Nonferrous Alloys Committee

Sealing Compound, Low Adhesion, Corrosion Inhibiting, 200 to 600 Poises (20 to 60 Pa⋅s), 2 Hour Application Time (A-2

AMS3267/3B (Current)02/18/2011

This specification covers accelerated curing synthetic rubber compounds with corrosion inhibitors and low adhesive strength supplied as a two-component system. This product has been used typically for sealing aircraft access doors and accessories where gaskets are required, but usage is not limited to such applications. Compound is classified as an A-2 sealing compound; the compound being suitable for brush application with a minimum of two hours application time after mixing

AMS G9 Aerospace Sealing Committee

Nickel Alloy, Corrosion and Heat Resistant, Forgings 57Ni - 19.5Cr - 13.5Co - 4.6Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F (996 to 1038 °C) Solution, Stabilization, and Precipitation Heat Treated

AMS5704L (Current)

08/03/2020

This specification covers a corrosion and heat-resistant nickel alloy in the form of forgings 3.25 inches (82.6 mm) and under, and forging stock of any size (see 8.6

AMS F Corrosion and Heat Resistant Alloys Committee

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