Standard STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized) 1942-06-01 HISTORICAL AMS6510
Standard Forgings, Hardenable Steels and Corrosion-Resistant Steels Heat-Treated, Finished-Part Properties Short-Transverse Tensile Strength and Fracture Toughness 2012-10-03 HISTORICAL AMS6474A This specification establishes requirements for steel forgings of any shape or form that finished parts are to be made (See 8.4, 8.5, 8.8.4 and 8.10).
Standard Forgings, Hardenable Steels and Corrosion-Resistant Steels Heat-Treated, Finished-Part Properties Short-Transverse Tensile Strength and Fracture Toughness 2002-06-19 HISTORICAL AMS6474 This specification establishes requirements for steel forgings of any shape or form from which finished parts are to be made (See 8.2, 8.3.4, 8.5, and 8.6).
Standard DUCTILE (NODULAR) IRON CASTINGS, SAND 60,000 psi (415 MPa) Tensile Strength Ferritize Annealed 2011-08-10 HISTORICAL AMS5315C This specification covers a ductile (nodular) iron in the form of sand castings.
Standard Ductile (Nodular) Iron Castings, Sand 60,000 psi (415 MPa) Tensile Strength Ferritize Annealed 2013-04-03 HISTORICAL AMS5315D This specification covers a ductile (nodular) iron in the form of sand castings.
Standard DUCTILE (NODULAR) IRON CASTINGS, SAND 60,000 psi (414 MPa) Tensile Strength 1981-07-01 HISTORICAL AMS5315B This specification covers a ductile (nodular) iron in the form of sand castings.
Standard Steel Plate, Sheet, and Strip, Alloy 4130 Aircraft Quality 1998-12-01 HISTORICAL AMSS18729 This specification covers chrome-molybdenum alloy 4130, steel sheet, strip, and plate of thickness to and including 1.50 inches.
Standard Steel, Bars, Forgings, and Tubing 1.0Cr (0.98 - 1.10C) (SAE 51100) For Bearing Applications 2001-03-01 HISTORICAL AMS6449D This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard STEEL BARS, FORGINGS, AND TUBING 1.0Cr (0.98 - 1.10C) (SAE 51100) Electroslag Remelted 1994-11-01 HISTORICAL AMS6446C This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard Steel, Bars, Forgings, and Tubing 1.0Cr (0.98 - 1.10C) (SAE 51100) Electroslag Remelted 2001-05-01 HISTORICAL AMS6446D This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard STEEL BARS, FORGINGS, AND TUBING 1.0Cr (0.98 - 1.10C) (SAE 51100) For Bearing Applications 1994-11-01 HISTORICAL AMS6449C This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard STEEL BARS, FORGINGS, AND TUBING 1.0Cr (0.98 - 1.10C) (SAE 51100) Consumable Electrode Vacuum Melted 1988-10-01 HISTORICAL AMS6443E This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard Steel Bars, Forgings, and Tubing 1.0Cr (0.98 - 1.10C) (SAE 51100) Consumable Electrode Vacuum Melted 2000-10-01 HISTORICAL AMS6443F This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard Steel Bars and Forgings 5.0Cr - 1.3Mo - 0.5V (0.38 - 0.43C) 2001-11-05 HISTORICAL AMS6485G This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
Standard STEEL BARS AND FORGINGS 5.0Cr - 1.3Mo - 0.50V (0.38 - 0.43C) 1989-07-01 HISTORICAL AMS6485F This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
Standard STEEL TUBING, WELDED 0.50Cr - 0.55Ni - 0.20Mo (0.28 - 0.33C) (SAE 8630) 1982-01-01 HISTORICAL AMS6550G This specification covers an aircraft-quality, low-alloy steel in the form of welded tubing.
Standard STEEL WIRE, COPPER CLAD, ROUND 99Fe - 0.45Mn (0.13C max) Annealed 1987-04-01 HISTORICAL AMS7733B This specification covers a low-carbon steel in the form of round wire clad with phosphorus-deoxidized copper.