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NUT, SELF-LOCKING, CASTELLATED, PREVAILING TORQUE, UNS G41300 OR UNS G43400, UNJ 16 PITCH THREAD FORM

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3566A
  • Current
Published 2018-11-21 by SAE International in United States
No Abstract Available.
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Tantalum Alloy, Bars and Rods 90Ta - 10W

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS7848D
  • Current
Published 2018-11-21 by SAE International in United States
This specification covers a tantalum alloy in the form of bars and rods up through 3.5 inches (88.9 mm), inclusive.
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CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SHIELDED (FOR MIL-DTL-26482 SERIES 1 CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS39029/26B
  • Current
Published 2018-11-21 by SAE International in United States
No Abstract Available.
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Test Method for Evaluating the Electrochemical Resistance of Coolant System Hoses and Materials

Non-Hydraulic Hose Committee
  • Ground Vehicle Standard
  • J1684_201811
  • Current
Published 2018-11-21 by SAE International in United States
This test method provides a standardized procedure for evaluating the electrochemical resistance of automotive coolant hose and materials. Electrochemical degradation has been determined to be a major cause of EPDM coolant system hose failures. The test method consists of a procedure which induces voltage to a test specimen while it is exposed to a water/coolant solution. Method #1, referred to as a “Brabolyzer” test, is a whole hose test. Method #2, referred to as a “U” tube test, uses cured plate samples or plates prepared from tube material removed from hose (Method No. 2 is intended as a screening test only). Any test parameters other than those specified in this SAE Recommended Practice, are to be agreed to by the tester and the requester.
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NUT, SPLINE DRIVE - EXTENDED WASHER, CUPWASHER LOCK, UNS S66286, SILVER PLATE, MJ THREAD, METRIC

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • MA3351
  • Current
Published 2018-11-21 by SAE International in United States
No Abstract Available.
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Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS7250D
  • Current
Published 2018-11-21 by SAE International in United States
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.
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Tantalum Alloy Sheet, Strip, and Plate 90Ta - 10W

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS7847D
  • Current
Published 2018-11-21 by SAE International in United States
This specification covers a tantalum alloy in the form of sheet, strip, and plate from 0.010 through 0.250 inch (0.25 through 6.35 mm), inclusive.
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BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS 5643, .4375-20, UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3171
  • Current
Published 2018-11-21 by SAE International in United States
No Abstract Available.
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Design Considerations for Enclosed Turboshaft Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR4989A
  • Current
Published 2018-11-21 by SAE International in United States
This SAE Aerospace Information Report (AIR) developed by a broad cross section of personnel from the aviation industry and government agencies is offered to provide state-of-the-art information for the use of individuals and organizations designing new or upgraded turboshaft engine test facilities.
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Titanium Alloy Powdered Metal Products 6Al - 4V Hot Isostatically Pressed, Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4994A
  • Current
Published 2018-11-21 by SAE International in United States
This specification covers powdered metal products consolidated by hot isostatic pressing (HIP) of titanium alloy powder compacts.
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