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Titanium Alloy Bars, Forgings, and Rings 6Al - 4V Extra Low Interstitial (ELI) Duplex Annealed, Fracture Toughness

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4931G
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a titanium alloy in the form of bars 6.000 inches (152.40 mm) and under in nominal diameter or least distance between parallel sides, forgings and flash welded rings 6.000 inches (152.40 mm) and under in thickness, and stock for forging and stock for flash welded rings of any size.
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Plating, Nickel Low-Stressed Deposit

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2424F
  • Current
Published 2019-11-04 by SAE International in United States
This specification covers the requirements for electrodeposited low-stressed nickel.
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Coating, Titanium Nitride Physical Vapor Deposition

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2444A
  • Current
Published 2019-11-04 by SAE International in United States
This specification covers the requirements for the application and properties of a titanium nitride coating on metal parts applied by physical vapor deposition (PVD).
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Magnesium Alloys in Aircraft Seats - Engineering Design and Fabrication Recommended Practices

Aircraft SEAT Committee
  • Aerospace Standard
  • ARP6256
  • Current
Published 2019-10-31 by SAE International in United States
This document is a guide to the application of magnesium alloys to aircraft interior components including but not limited to aircraft seats. It provides background information on magnesium, its alloys and readily available forms such as extrusions and plate. It also contains guidelines for “enabling technologies” for the application of magnesium to engineering solutions including: machining, joining, forming, cutting, surface treatment, flammability issues, and designing from aluminum to magnesium.
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Additively Manufactured Component Substantiation

AMS AM Additive Manufacturing
  • Aerospace Standard
  • AIR7352
  • Current
Published 2019-10-31 by SAE International in United States
This AIR is applicable to components fabricated using additive manufacturing (AM) processes. The discussion is generic with respect to specific additive processes as much as possible. Each additive process has unique considerations that should be addressed in any effort to substantiate additively manufactured components, This specification is written for metallics but conceptually could be applied to non-metallics.
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BEARING, ROLLER, NEEDLE, TRACK ROLLER, CROWN RADIUSED OD INTEGRAL STUD, TYPE VII ANTIFRICTION, INCH

ACBG Rolling Element Bearing Committee
  • Aerospace Standard
  • AS21447C
  • Current
Published 2019-10-22 by SAE International in United States
No Abstract Available.
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Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 4V, Extra Low Interstitial Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4930K
  • Current
Published 2019-10-10 by SAE International in United States
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or distance between parallel sides, and stock for forging or flash welded rings of any size.
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Numbering System for Single Diameter and Taper Reamers

Motor Vehicle Council
  • Ground Vehicle Standard
  • J2124_201910
  • Current
Published 2019-10-09 by SAE International in United States
This SAE Recommended Practice provides a systematic method for the identification of single diameter and taper reamers. It is intended to assist in the cataloging and supplying of these tools. NOTE 1— Caution must be taken when assigning codes for designators to prevent specifying reamers that cannot be physically or economically manufactured. NOTE 2— The Code Number coming from the manufacturer MUST reflect the actual tool construction. NOTE 3— In particular without limitation, SAE disclaims all responsibility for the accuracy or completeness of information contained within this report if the standards of this report are retrieved, combined, or used in connection with any software.
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Protective Coatings for Fasteners

Fasteners Committee
  • Ground Vehicle Standard
  • J1648_201910
  • Current
Published 2019-10-07 by SAE International in United States
This SAE Information Report is provided as an advisory guide. Careful discretion as to application is recommended. The content has been presented as accurately as possible, but responsibility for its application lies with the user. It covers finishes applied to fasteners and related topics, corrosion resistance, lubricity, electrical grounding, ultraviolet light, and embrittlement. Table 1 lists these coatings and their properties so that finish selection can be reasonably made in accordance with known and anticipated fastener assembly applications. Application of protective coatings will affect fastener dimensions. This is especially critical for the thread fit of mating parts because the pitch diameter increases by four times the coating thickness. Explanation is covered in Section 5.
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Performance Engine Building Recommended Practices

Motor Vehicle Council
  • Ground Vehicle Standard
  • J2379_201910
  • Current
Published 2019-10-03 by SAE International in United States
This SAE Recommended Practice applies to the function of building reciprocating spark-ignition engines which are used in conjunction with standard and high-performance ancillary components in applications intended to achieve a minimum of 1 hp/in3. This document does not apply to rebuilt engines which may only be partially repaired with little or no machining, nor does it apply to second-hand or used engines.
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