Inconel® 718 AMS 5663

Inconel® 718 AMS 5663 available at Rockwell Industries (also known as Inconel alloy 718, inco718, inc718, alloy718) is a nickel-chromium-molybdenum alloy designed to resist a wide range of corrosive environments, pitting and crevice corrosion. Rockwell Industries Inconel 718 nickel alloy also displays high tensile and creep-rupture properties at elevated temperatures.

Stock sizes: 0.500”dia to 3.000” diameter

Common Specifications:

  • AMS 5663
  • PWA-S-5663, CPW-A-5663
  • B50TF15 Classes B/C/E/F
  • ASTM-B637
  • ASME-SB637
  • Pratt & Whitney LCS F-17
  • General Electric S-400 / S-SPEC-35
  • SPS-M-275

Industry Trade Names:

  • Inconel 718
  • Pyromet 718
  • VDM 718
  • ATI 718
  • Nickel 718

Common Applications:

  • Jet engines
  • Aerospace fasteners
  • Rocket motors
  • Oil and gas shafts and wellhead components
Rockwell-Industries-AMS-5663-Inconel-718-Annealed-Aged webP image

Composition

Element Min. Max.
Carbon 0.8
Manganese 0.35
Silicon 0.35
Phosphorus 0.010
Sulfur 0.015
Chromium 17.00 21.00
Nickel 50.00 55.00
Molybdenum 2.80 3.30
Copper 0.30
Columbium (Niobium) 4.75 5.50
Titanium 0.65 1.15
Aluminum 0.20 0.80
Cobalt 1.00
Boron 0.006
Lead 0.0005 (5 ppm)
Bismuth 0.00003 (0.3 ppm)
Selenium 0.0003 (3ppm)
Iron remainder

Melt practice: VIM-VAR or VIM-ESR.

Minimum room temperature tensile properties:
Specimen Orientation Diameter or Least Distance Between Parallel Sides, inch Tensile Strength ksi Yield Strength at 002% Offset ksi Elongation in 4D% Reduction of Area %
Longitudinal Up to 10.00, incl. 185 150 12 15
Long-Transverse (Forgings) Up to 5.00, incl
——————-
Over 5.00 to 10.00, incl
180
——
180
150
——
145
10
——
10
12
——
12
Transverse (Bars) Up to 5.00, incl
——————-
Over 5.00 to 10.00, incl
180
——
180
150
——
145
6
——
6
8
——
8

Hardness shall not be lower than 331 HB or equivalent.