• ARP674
• Revision: A

• 1988-06-20

• Historical. Access the latest revision: ARP674C

• E-25 General Standards For Aerospace And Propulsion Systems

Groove designs presented herein are applicable for use with the following MS metal O-ring gaskets, or to dimensionally equivalent gaskets of other materials:a. AMS 5570 or AMS 5576 Plain1. MS9141 - 0.035 tube x 0.006 wall2. MS9142 - 0.062 tube x 0.006 wall3. MS9202 - 0.062 tube x 0.010 wall4. MS9203 - 0.094 tube x 0.006 wall5. MS9204 - 0.094 tube x 0.010 wall6. MS9205 - 0.125 tube x 0.010 wallb. AMS 5570 or AMS 5576 Silver Pl.1. MS9371 - 0.035 tube x 0.006 wall2. MS9372 - 0.062 tube x 0.006 wall3. MS9373 - 0.062 tube x 0.010 wall4. MS9374 - 0.094 tube x 0.006 wall5. MS9375 - 0.094 tube x 0.010 wall6. MS9376 - 0.125 tube x 0.010 wall

• SAE ARP 674

• Aerospace

• Parts
• Seals and Gaskets
• Gas turbines
• Hybrid engines
• Jet engines