Your Selections

TEAE25
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Publishers

Committees

Committee Codes

 
new

Nut, Spanner, Aeronautical, UNS G41400

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS172321B
  • Current
Published 2019-07-12 by SAE International in United States

Scope is unavailable.

 
new

Nut, Self-Locking, Double Hexagon, Silver Plated, Counterbored 180 ksi, 1400 °F, UNS N07001

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3553B
  • Current
Published 2019-07-02 by SAE International in United States

Scope is unavailable.

 
new

Plug, Expansion - CRES, 303, Long, Std and .010 Oversize Diameters, UNS S30300

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3129C
  • Current
Published 2019-07-01 by SAE International in United States

Scope is unavailable.

 
new

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.

 
new

Nut, Floating, Attached Retention Element (A.R.E.) - Hole Dimensions and Installation Requirements

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS5133A
  • Current
Published 2019-07-01 by SAE International in United States

This specification establishes the procedure for installing self-locking, floating, attached retention element (A.R.E.) nut assemblies and defines the necessary hole preparation.

 
new

Nut - Self-Locking Clinch, Serrated Shank, Hole Preparation, Installation and Removal Procedures

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS4389A
  • Current
Published 2019-07-01 by SAE International in United States

This SAE Aerospace Standard (AS) provides minimum design, hole preparation, installation and removal requirements for AS3272, AS3273, MA3274, and MA3275 serrated shank self-locking clinch nuts. This standard is applicable when specified on engineering drawings or in procurement documents.

 
new

Insert, Screw Thread, Self-Locking, UNS S66286, Locked in, Key Locked, Procurement Specification for

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS4892B
  • Current
Published 2019-07-01 by SAE International in United States

This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286 which have self-locking internal threads and integrated locking keys to positively secure the insert against rotation when properly installed in threaded holes.

 
new

Insert - Thin Wall, Self-Locking, Short and Long Length, Installation and Removal of

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3507C
  • Current
Published 2019-07-01 by SAE International in United States

This SAE Aerospace Standard (AS) provides minimum design, installation (by manual and power methods) and removal requirements for AS3504 and AS3505 thin wall inserts and is applicable when specified on engineering drawings or in procurement documents.

 
new

Nut, Slotted, Hexagon, Shear - Silver Plated, UNS S66286, 130 ksi Min

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS9364B
  • Current
Published 2019-06-20 by SAE International in United States

Scope is unavailable.

 
new

Nut, Self-Locking, Double Hexagon, Silver Plated, Extended Wrench Pad, 180 ksi, 1400 °F, UNS N07001

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3552B
  • Current
Published 2019-06-20 by SAE International in United States

Scope is unavailable.