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High Temperature Materials Bundle

  • Professional Development
  • PD281946
Published 2019-04-25

Metals and alloys all have different melting ranges depending on their chemistry. High temperature metals are much harder at room temperature, have exceptionally high melting points (usually above 2000 degree Celsius), and are resistant to wear, corrosion and deformation. The following five on-demand courses are included in the High Temperature Materials bundle.  Each course is approximately one-hour in duration. See Topics/Outline for additional details.

 

Steel Strip 0.68 - 0.80C (SAE 1074)

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS5120N
  • Current
Published 2019-04-25 by SAE International in United States
This specification covers a carbon steel in the form of strip.
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Ultrasonic Inspection Thin Wall Metal Tubing

AMS K Non Destructive Methods and Processes Committee
  • Aerospace Material Specification
  • AMS2634B
  • Current
Published 2019-04-24 by SAE International in United States
This specification covers procedures for ultrasonic inspection of thin wall metal tubing of titanium, titanium alloy, and corrosion and heat resistant steels and alloys having nominal OD over 0.1875 inch (4.762 mm) with OD to wall thickness ratio of 8 or greater and wall thickness variation not exceeding ±10% of nominal.
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STUD, LOCKED IN - RING, STRAIGHT, HOLE PREPARATION FOR

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS1620A
  • Current
Published 2019-04-11 by SAE International in United States
No Abstract Available.
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BOLT, TEE HEAD – CHAMFERED, AMS5708 (UNS N07001), 165 KSI MIN UTS, .1900-32UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3232C
  • Current
Published 2019-04-11 by SAE International in United States
No Abstract Available.
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BOLT, TEE HEAD - CHAMFERED, PD SHANK NICKEL ALLOY (UNS N07001), 165 KSI MIN UTS .3125-24 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3234B
  • Current
Published 2019-04-11 by SAE International in United States
No Abstract Available.
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Nuts, Self-Locking, Alloy, Corrosion and Heat Resistant, High Strength, All Metal, Solid Film Lubricated, 1400 °F, Procurement Specification

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS4417A
  • Current
Published 2019-04-10 by SAE International in United States
This document covers all-metal, self-locking nuts, plate nuts, and gang channel nuts made of a corrosion and heat resistant nickel alloy.
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Insert - Screw Thread, Thin Wall, Self-Locking, UNS N07718, Silver Plated, Class: 185 ksi/1025 °F, Procurement Specification

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3506B
  • Current
Published 2019-04-09 by SAE International in United States
This SAE Aerospace Standard (AS) establishes the requirements for AS3504 and AS3505 thin wall self-locking inserts made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718.
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Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Foil 52.5Ni - 19Cr - 3.0Mo - 5.0Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted Precision Cold Rolled, Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5914B
  • Current
Published 2019-02-21 by SAE International in United States
This specification covers a precision cold rolled corrosion and heat resistant nickel alloy in the form of sheet and strip over 0.005 up to 0.015, inclusive, inch in nominal thickness and foil up to 0.005 inch, inclusive, in nominal thickness (see 8.5).
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Inserts, Screw Thread, Helical Coil 19Cr-9.2Ni, Corrosion Resistant Steel, Procurement Specification for

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS7245B
  • Current
Published 2019-02-13 by SAE International in United States
This specification covers closely-wound helical coil, screw thread inserts made of a corrosion resistant steel formed wire with a chemical composition in accordance with Table 1 and identified under the Unified Numbering System as UNS S30200 or UNS S30400 that can be formed by an insert manufacturer to achieve the requirements of this procurement specification. The inner surface of the insert coil, after assembly into a screw thread tapped hole, provides internal threads of standard 60° Unified form.
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