Results

This SAE Aerospace Standard (AS) provides a harmonized process and documentation requirements for the establishment of CoCs used to attest the conformity of aviation, space, and defense products (e.g., assemblies, sub-assemblies, equipment and systems, parts, material, software) or services. It includes a CoC template and supporting instructions on how to complete it. When quoted by the customer in a contractual requirement, application of this document is mandatory. In other cases, its use is recommended, but if there is a conflict between the requirements of this standard and customer or applicable statutory/regulatory requirements, the latter shall take precedence. Requirements for the establishment of Authorized Release Certificates (ARCs)—e.g., European Union Aviation Safety Agency (EASA) Form 1, Federal Aviation Administration (FAA) 8130-3 tag, Civil Aviation Administration of China (CAAC) Form 038—by an external provider holding a production approval (for new aviation products

G-14 Americas Aerospace Quality Standards Committee (AAQSC)

HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 °F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 45 TO 90 DEGREES

AS1913D (Current)

12/07/2022

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

Micropitting of Bearings and Gears in Aviation

AIR6989 (Current)

12/07/2022

The intent of this SAE Aerospace Information Report (AIR) is to summarize and review the E34 committee’s efforts to educate the aerospace propulsion lubrication community on the science of micropitting, its consequences, and the various tribology evaluation methods that can be employed under aviation related conditions to differentiate formulation related aggravating factors

E-34 Propulsion Lubricants Committee

Application Guideline for Use of Hydrogen Quality Specification

J2719/1_202211 (Current)11/02/2022

This SAE Information Report is intended to be used for routine (or periodic) monitoring of filling station performance. It is not intended to provide process quality control requirements for any portion of the product delivery cycle

Fuel Cell Standards Committee

Bolts and Screws, Aerospace Engine - Materials, Procurement Specifications, and Properties

AIR4923B (Current)

11/02/2022

This SAE Aerospace Information Report (AIR) includes general design information on materials, procurement specifications, and mechanical properties for bolts and screws developed for use on aerospace propulsion systems. Both inch and metric (SI) designs are included

E-25 General Standards for Aerospace and Propulsion Systems

Ice Melting Test Method for Runways and Taxiways Deicing/Anti-Icing Chemicals

AIR6170B (Current)10/27/2022

This test method provides stakeholders (runway deicing chemical manufacturers, users, regulators, and airport authorities) with relative ice melting capacity of runway deicing chemicals, by measuring the amount of ice melted as a function of time. Such runway deicing chemicals are often also used on taxiways and other paved areas. This test method does not quantitatively measure the theoretical or extended time ice melting capability of ready-to-use runway deicing/anti-icing chemicals in liquid or solid form

G-12RDP Runway Deicing Product Committee

Steel, Mechanical Tubing 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140

AMS6381K (Current)

11/02/2022

This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing

AMS E Carbon and Low Alloy Steels Committee

Titanium Alloy, Bars and Rods 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Centerless Ground or Peeled and Polished

AMS4958F (Current)

11/02/2022

This specification covers a titanium alloy in the form of bars and rods 1.00 inch (25.4 mm) and under in nominal diameter

AMS G Titanium and Refractory Metals Committee

Steel, Sheet, Strip, and Plate 0.75Cr - 9.0Ni - 4.5Co - 1.0Mo - 0.09V (0.17 - 0.23C) Vacuum Consumable Electrode Melted, Annealed

AMS6523J (Current)

11/02/2022

This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate

AMS E Carbon and Low Alloy Steels Committee

Class A Multiplexing Architecture Strategies

J2057/4_202212 (Current)12/20/2022

The subject matter contained within this SAE Information Report is set forth by the Class A Task Force of the Vehicle Network for Multiplexing and Data Communications (Multiplex) Committee as information the network system designer should consider. The Task Force realizes that the information contained in this report may be somewhat controversial and a consensus throughout the industry does not exist at this time. The Task Force also intends that the analysis set forth in this document is for sharing information and encouraging debate on the benefits of utilizing a multiple network architecture

Vehicle Architecture For Data Communications Standards

Requirements for Conducting Audits of Aviation, Space, and Defense Quality Management Systems

AS9101G (Current)

11/29/2022

This standard defines requirements for the preparation and execution of the audit process. In addition, it defines the content and composition for the audit reporting of conformity and process effectiveness to the 9100-series standards, the organization's QMS documentation, and customer and statutory/regulatory requirements. The requirements in this standard are additions or represent changes to the requirements and guidelines in the standards for conformity assessment, auditing, and certification as published by ISO/IEC (i.e., ISO/IEC 17000, ISO/IEC 17021-1). When there is conflict with these standards, the requirements of the 9101 standard shall take precedence

G-14 Americas Aerospace Quality Standards Committee (AAQSC)

AS60400-499AR Amendment Record for Aerospace Standard No. AS60400-499

AS60400AR-4 (Current)10/26/2022

No scope available

Engine and Airframe Technical Standards Committee (TSC)

Class A Application/Definition

J2057/1_202212 (Current)12/20/2022

This SAE Information Report will explain the differences between Class A, B, and C networks and clarify through examples, the differences in applications. Special attention will be given to a listing of functions that could be attached to a Class A communications network

Vehicle Architecture For Data Communications Standards

Selection of Transmission Media

J2056/3_202212 (Current)12/20/2022

This SAE Information Report studies the present transmission media axioms and takes a fresh look at the Class C transmission medium requirements and also the possibilities and limitations of using a twisted pair as the transmission medium. The choice of transmission medium is a large determining factor in choosing a Class C scheme

Vehicle Architecture For Data Communications Standards

FITTING, TEE, FLARED TUBE, INTERNAL THREAD ON RUN, FOR SEAL RING

AS4310B (Current)

11/02/2022

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

Sealing Compound, Polythioether Elastomeric Two-Part Electrically Conductive

AMS3266B (Current)

11/02/2022

This specification covers two types of electrically conductive, elastomeric polythioether sealing compounds that cure at room temperature. The sealing compound is supplied as either a two-component system or as premixed and frozen

AMS G9 Aerospace Sealing Committee

J2777_202211 (Current)

11/14/2022

With many corporations and suppliers conducting development and validation tests at different climatic wind tunnel sites, there is an increasing need for a recommended best practice that defines a process by which climatic wind tunnels can be correlated. This document addresses the test methods and metrics used to correlate results from different facilities, independent of location, for heating ventilation and air conditioning (HVAC) and powertrain cooling (PTC) development. This document should be used as a guideline to make sure key aspects of tunnel testing are covered when comparing various climatic wind tunnel facilities. The depth of the correlation program is ultimately influenced by program objectives; therefore, a correlation program, for the intent and purposes of this document, can range from just a few tests to a full analysis that involves multiple vehicle tests identifying limitations and statistical boundaries. Using recommendations in this document will eliminate most

Interior Climate Control Vehicle OEM Committee

Steel, Bars 0.95Cr - 0.20Mo (0.38 - 0.43C) (SAE 4140) Special Aircraft-Quality Cleanliness Normalized

AMS6529E (Current)

11/02/2022

This specification covers a special aircraft-quality, low-alloy steel in the form of bars

AMS E Carbon and Low Alloy Steels Committee

Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340) Normalized and Tempered

AMS6484F (Current)

11/02/2022

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock

AMS E Carbon and Low Alloy Steels Committee

Steel, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Forging Stock 13.5Cr - 13.5Ni - 0.35Mo - 2.2W Annealed

AMS5700H (Current)

11/02/2022

This specification covers a corrosion- and heat-resistant steel 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

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings and Forging and Ring Stock 19Cr - 10Ni Solution Heat Treated

AMS5639K (Current)

11/02/2022

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

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Spring Wire 0.95Cr - 0.22V (0.48 - 0.53C) (SAE 6150) Annealed and Cold Drawn

AMS6450L (Current)

11/02/2022

This specification covers a low-alloy steel in the form of wire supplied as coils, spools, and straight lengths

AMS E Carbon and Low Alloy Steels Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, and Rings 53Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti - 1.6Al - 0.006B Vacuum Melted, Solution Heat Treated Precipitation Hardenable

AMS5712L (Current)

08/17/2022

This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars 3.00 inches (76.2 mm) and under in nominal diameter, thickness or for hexagons least distance between parallel sides, forgings, flash welded rings 3.00 inches (76.2 mm) and under in nominal radial thickness, and stock of any size for forging, flash welded rings, or heading (see 8.5

AMS F Corrosion and Heat Resistant Alloys Committee

Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or, When Specified, “As Fabricated” (2219-F

AMS4031K (Current)

08/17/2022

This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in nominal thickness, supplied in the annealed (-O) condition (see 8.3). When specified, product shall be supplied in the “as fabricated” (-F) temper

AMS D Nonferrous Alloys Committee

Titanium Alloy Extrusions and Flash Welded Rings 6Al - 4V Annealed Beta Processed

AMS4935M (Current)

08/17/2022

This specification covers a titanium alloy in the form of extruded bars and shapes, flash welded rings 3.000 inches (76.20 mm) and under in nominal diameter or least distance between parallel sides, and stock for flash welded rings

AMS G Titanium and Refractory Metals Committee

Aluminum Alloy, Welding Wire 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti for Welding A206.0 Type Alloys

AMS4244D (Current)

08/09/2022

This specification covers an aluminum alloy in the form of two types of welding wire

AMS D Nonferrous Alloys Committee

Steel Bars and Forgings 1.8Ni - 0.25Mo (0.38 - 0.43C) (4640) Heat Treated, 125 ksi (862 MPa) Tensile Strength

AMS6317L (Current)

08/09/2022

This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings 1.00 inches (25.4 mm) and under in nominal cross section or diameter and for hexagonal shapes, least distance between parallel sides

AMS E Carbon and Low Alloy Steels Committee

Copper-Nickel-Tin Alloy, Mechanical Tube 77Cu - 15Ni - 8Sn Solution Annealed and Spinodal Hardened (TX02, formerly TX00

AMS4598B (Current)

08/05/2022

This specification covers a copper-nickel-tin alloy in the form of mechanical tube 1.100 to 13.6 inches (28 to 346 mm) in outer diameter (see 8.11

AMS D Nonferrous Alloys Committee

Sealing of Integral Fuel Tanks

AIR4069D (Current)

07/26/2022

This SAE Aerospace Information Report (AIR) presents preferred design, assembly, and repair practices for sealing of aircraft integral fuel tanks, including rework of applied fuel tank seals. It addresses engineering designs for integral fuel tanks as they are currently found in practice and discusses the most practical and conservative methods for producing a reliable, sealed system. Although this AIR presents practices for sealing of integral fuel tanks, the practices presented within this report are practices that are carried throughout sealing that include both pressure and environmental aircraft sealing. Design preferences for optimum sealing are not within the scope of this document. Such discussions can be found in the United States Air Force (USAF) sponsored report AFWAL-TR-87-3078, “Aircraft Integral Fuel Tank Design Handbook.” Key objectives of the fuel tank sealing process are to produce a sealing plane that is leak-free and corrosion resistant, especially at fastener

AMS G9 Aerospace Sealing Committee

Steel, Corrosion-Resistant, Flat Wire 18Cr - 9.0Ni (302) Spring Temper

AMS5866F (Current)

07/19/2022

This specification covers a corrosion-resistant steel in the form of flat wire 0.005 to 0.095 inch (0.13 to 2.41 mm) thick, inclusive

AMS F Corrosion and Heat Resistant Alloys Committee

Nomenclature and Definitions for Electrified Propulsion Aircraft

ARP8676 (Current)

08/01/2022

Create and publish a list of terms relevant to electrified propulsion aircraft with summary text descriptions. The terms and descriptions will not provide full explanations, diagrams, and other detailed technical descriptions. These deeper descriptions will be addressed in other documents. This document defines the relevant terms and abbreviations related to the design, development, and use of electrified propulsion in aircraft. This definition is provided to enable a consistent use of technical language throughout the standards developed by the E-40 committee

E-40 Electrified Propulsion Committee

Class A Multiplexing Sensors

J2057/3_202212 (Current)12/20/2022

The Class A Task Force of the Vehicle Network for Multiplexing and Data Communications Subcommittee is providing information on sensors that could be applicable for a Class A Bus application. Sensors are generally defined as any device that inputs information onto the bus. Sensors can be an input controlled by the operator or an input that provides the feedback or status of a monitored vehicle function. Although there is a list of sensors provided, this list is not all-inclusive. This SAE Information Report is intended to help the network system engineer and is meant to stimulate the design thought process

Vehicle Architecture For Data Communications Standards

Sealing and Coating Compound, Polyurethane (PUR) Fuel Resistant, High Tensile Strength/Elongation for Integral Fuel Tanks/Fuel Cavities/General Purpose

AMS3278C (Current)

11/22/2022

This specification covers polyurethane (PUR) in the form of two-component sealing compounds

AMS G9 Aerospace Sealing Committee

Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock 0.80Cr - 1.8Ni - 0.25Mo (0.38 - 0.43C) (SAE 4340

AMS6415V (Current)

11/22/2022

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock

AMS E Carbon and Low Alloy Steels Committee

Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T361 Sheet and Plate) Solution Heat Treated, 6% Cold Worked, and Naturally Aged

AMS4466B (Current)

11/22/2022

This specification covers an aluminum alloy in the form of alclad sheet and plate 0.020 to 0.500 inch (0.508 to 12.70 mm), inclusive, in thickness, supplied in the -T361 temper (see 8.5

AMS D Nonferrous Alloys Committee

Titanium Alloy, Cold Rolled Sheet and Strip 15V - 3Al - 3Cr - 3Sn Solution Heat Treated

AMS4914H (Current)

11/22/2022

This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inch (3.18 mm) in nominal thickness

AMS G Titanium and Refractory Metals Committee

Powder History Metric and Labeling Schema

ARP7044 (Current)

11/22/2022

This SAE Aerospace Recommended Practice (ARP) describes a method to measure, track, and characterize the history of powder feedstock when consumed in the production of parts via additive manufacturing (AM). The history captured as part of this ARP includes AM process exposure, feedstock consumption, blending, and losses associated with the totality of the AM workflow. This document also outlines a two-part metric schema for used powder feedstock consequential of its process exposure history. This metric schema also enables aligning risk determination and usage practices for used powder when based on a correlation between tabulated values in the scheme and user-identified metrics. These correlated metrics with schema values may also be used when establishing powder blending workflows or identifying end-of-life for feedstock

AMS AM Additive Manufacturing Metals

Electron Beam-Powder Bed Fusion (EB-PBF) Produced Preforms and Parts Titanium Alloy, 6Al - 4V Hot Isostatically Pressed

AMS7011 (Current)

11/22/2022

This specification covers a titanium alloy in the form of preforms and parts produced by electron beam-powder bed fusion (EB-PBF) that are subjected to post-deposition hot isostatic press (HIP). Preforms may require subsequent machining or surface finishing to meet requirements for their intended final part application

AMS AM Additive Manufacturing Metals