SAE ARP1631A-2007 PDF

Scope: This document establishes the requirements for sequencing processes relating to parts fabricated from 300M or 4340 modified steel heat treated to, or to be heat treated to 270,000 psi (1860 MPa) minimum ultimate tensile strength (UTS) and higher.

SAE ARP1631A-2007 Referenced Document

ASTM E1444-05 Standard Practice for Magnetic Particle Testing
ASTM E1742-06 Standard Practice for Radiographic Examination
ASTM E18-07 Standard Test Methods for Rockwell Hardness of Metallic Materials
SAE AMS-C-8837-1999 Coating, Cadmium (Vacuum Deposited) AREA MFFP; Should Be Used Instead of MIL-C-8837B, Which Was Cancelled on 10 September 1999
SAE AMS-QQ-C-320-2000 Chromium Plating (Electrodeposited)
SAE AMS-S-13165-1997 Shot Peening of Metal Parts
SAE AMS-STD-2154-1998 Inspection, Ultrasonic, Wrought Metals, Process for
SAE AMS2300K-2003 Steel Cleanliness, Premium Aircraft-Quality Magnetic Particle Inspection Procedure
SAE AMS2401 CADMIUM PLATING Low Hydrogen Content Deposit
SAE AMS2403L-2004 Plating, Nickel General Purpose [Superseded: SAE AMS-QQ-N-290A, SAE AMS-QQ-N-290]
SAE AMS2406 CHROMIUM PLATING, HARD
SAE AMS2419 CADMIUM-TITANIUM ALLOY PLATING

2018 SAE ARP1631A-2018 Manufacturing Sequence for Fabrication of High-Strength Steel Parts 300M or 4340 Modified Low-Alloy Steels 270,000 psi (1860 MPa) Tensile Strength and Higher
2007 SAE ARP1631A-2007 Manufacturing Sequence for Fabrication of High-Strength Steel Parts 300M or 4340 Modified Low-Alloy Steels 270,000 psi (1860 MPa) Tensile Strength and Higher
1984 SAE ARP1631-1984 Manufacturing Sequence for Fabrication of High- Strength Steel Parts 300M or 4340 Modified Low-Alloy Steels 270@000 psi (1860 MPa) Tensile Strength and Higher