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Insert, Screw Thread, Helical Coil Metric Series, Standard Assembly Dimensions for

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • MA1567C
  • Current
Published 2019-07-01 by SAE International in United States
This SAE Metric Aerospace Standard (MA) provides for helical coil screw thread inserts, both free running and self-locking, installation screw thread dimensional data and guidance on insert length selection. The document also provides formulas for determining requirements when non standard insert lengths are necessary.
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Undercuts for Straight Screw Threads - Metric

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS1508A
  • Current
Published 2019-06-19 by SAE International in United States

This standard provides recommended dimensional data for screw thread undercuts for straight 'MJ' metric screw threads in accordance with AS1370.

 

Wrenches, Twelve Spline, Metric

EG-1B Hand Tools Committee
  • Aerospace Standard
  • MA1547A
  • Current
Published 2019-05-10 by SAE International in United States
This standard covers the design, performance, and test requirements for high strength, thin wall, commercial sockets, universal sockets, and box wrenches used for the attachment and detachment of metric spline drive, high strength, and high temperature aircraft fasteners. Inclusion of dimensional data in this standard is not intended to imply that all of the products described herein are stock production sizes. Consumers are requested to consult with manufacturers concerning lists of stock production sizes. This standard is based on, but not limited to, the following external spline wrenching system:
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Fasteners - Part Standard - Cap Screws, Hex Bolts, and Hex Nuts (Metric)

Ship Systems - Fasteners Committee
  • Ground Vehicle Standard
  • J2295M_201905
  • Current
Published 2019-05-10 by SAE International in United States
This SAE Part Standard covers selected metric screws, hex bolts, and nuts manufactured in accordance with American Society for Testing and Materials (ASTM) and SAE fastener standards. This document covers fastener materials often used in ship systems and equipment but its use may be applied wherever fasteners of the covered materials are used. This document permits the fasteners to be identified and ordered by a part or identifying number (PIN) as defined in this document.
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CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, NONENVIRONMENTAL, 90°, SELF-LOCKING AND NON-SELF-LOCKING CATEGORY 4B (FOR AS50151 CRIMP, AS95234, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/51F
  • Current
Published 2019-05-03 by SAE International in United States
No Abstract Available.
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High Strength Elevated Temperature Bolting Practice

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • ARP700C
  • Current
Published 2019-05-03 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides general information on the design and installation of threaded fasteners in high strength and high temperature applications in propulsion systems. Some of the more common definitions of fastener terminology are also provided.
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Bolts, Screws, and Nuts - External Wrenching, Metric Threads - Design Parameters for

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • MA1518C
  • Current
Published 2019-05-03 by SAE International in United States
To fully define the following requirements for bolts with spline and hexagon heads of strength class up to but not including 1250 MPa: a Head dimensions (see 3.1) b Shank dimensions (see 3.2) c Geometric control (see 3.3) d Surface texture (see 3.4) This document is based on one class of thread after all processing, including coating or plating, has been completed as follows: tolerance class 4h6h. For particulars of thread, see AS1370. For thread runout and lead threads, see AS3062. To fully define the following requirements for nuts with spline, plain hexagon and castellated configurations of strength class up to and including 1100 MPa: a Nut dimensions (see 4.1) b Geometric control (see 4.2) c Surface texture (see 4.3) For particulars of threads, see AS1370. This document is based on the following classes of internal threads after all processing, including coating or plating, has been completed: Tolerance class 4H6H for sizes up to and including 5 mm Tolerance class 4H5H for size 6 mm and larger For particulars of thread, see AS1370.
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Areas for Calculating Stress or Load Values for Metric MJ Internally Threaded Fasteners

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • MA4284A
  • Current
Published 2019-05-03 by SAE International in United States
Areas for the standard metric series of threaded diameter-pitch combinations for aerospace internally threaded fasteners are established for the following conditions: a Area for shear stress or load in fastener thread b Area for ultimate tensile stress or load in thread
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CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, STRAIGHT SELF-LOCKING, AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES I AND II CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/121C
  • Current
Published 2019-04-22 by SAE International in United States
No Abstract Available.
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CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90°, CATEGORY 4C (FOR MIL-DTL-24308 CONNECTORS)

AE-8C1 Connectors Committee
  • Aerospace Standard
  • AS85049/50E
  • Current
Published 2019-04-22 by SAE International in United States
No Abstract Available.
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