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NUT, SPANNER BEARING RETAINING, PHOSPHATE TREATED AERONAUTICAL, UNS G41400
- Aerospace Standard
Published August 21, 2015 by SAE International in United States
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THIS DOCUMENT HAS BEEN DETERMINED TO CONTAIN BASIC AND STABLE TECHNOLOGY WHICH IS NOT DYNAMIC IN NATURE.
THERE WERE VERY MINOR ERRORS NOTED ON THE STABILIZATION BALLOT.
AS6140A: PAGE 2; TABLE 1A
PART NUMBER: AS6140-01; THREAD T; MINOR DIAMETER .3606-.3649 DECIMAL POINT MISSING ON .3649 DIMENSION.
PART NUMBER: AS6140-02; THREAD T; MINOR DIAMETER .4386 - .4429 DECIMAL POINT MISSING ON .4429 DIMENSION.
PART NUMBER: AS6140-02; THREAD T; PITCH DIAMETER .4487 - .4513 DECIMAL POINT MISSING ON .4513 DIMENSION.
|Aerospace Material Specification||Cobalt Alloy, Corrosion and Heat Resistant, Bars 62Co-28Cr-6Mo Warm-Worked|
|Ground Vehicle Standard||Metric Ball Joints|
|Aerospace Material Specification||Tow or Yarn, Carbon Fibers For Structural Composites GF 300 (2068) Tensile Strength, 75 (517) Tensile Modulus|
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Data Sets - Support Documents
|TABLE 1A||PARTNUMBERS AND DIMENSIONS|
|TABLE 1B||PART NUMBERS AND DIMENSIONS (CONTINUED)|
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
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