Steels, stainless and nickel alloys
Where to buy| Material | What it is for |
|---|---|
| Inconel 625 | Inconel 625 sheet for aircraft: annealed 120 ksi Ftu design values, AMS 5599, corrosion and oxidation to 1,800 |
| Inconel 718 | Inconel 718 for aircraft: 180 ksi solution-treated-and-aged sheet, AMS 5596, 5597 and 5589, welding, forming, |
| 15-5PH Stainless Steel | 15-5PH stainless for aircraft: H900 to H1150M, AMS 5659 bar and AMS 5862 plate, transverse toughness, welding |
| 17-4PH Stainless Steel | 17-4PH stainless for aircraft: H900 to H1150 conditions, strength 135–190 ksi, AMS 5604 sheet and 5643 bar, we |
| 17-7PH Stainless Steel | 17-7PH semiaustenitic stainless sheet for aircraft: form in Condition A, harden to TH1050, AMS 5528, 177 ksi d |
| 301 Stainless Steel | 301 stainless steel sheet for aircraft: strength by temper from annealed to full hard, AMS 5901-5519, firewall |
| 302 Stainless Steel | 302 (18-8) stainless steel for aircraft: composition, AMS 5516 and 5903–5906 by temper, welding, corrosion, an |
| 304 Stainless Steel | 304 stainless steel for aircraft: AMS 5513 and 5910–5913 by temper, strength from the 301 table, 308L filler, |
| 316 Stainless Steel | 316 stainless steel for aircraft: molybdenum-bearing austenitic, AMS 5524 and 5907, 316L filler, strength from |
| 321 Stainless Steel | 321 titanium-stabilized stainless steel for aircraft: composition, AMS 5510 sheet, exhaust-heat use, welding a |
| 347 Stainless Steel | 347 niobium-stabilized stainless steel for aircraft: composition, AMS 5512 sheet, high-temperature use, weld f |
| 4140 Steel | 4140 chromium-molybdenum steel for aircraft: how it differs from 4130, AMS specs, forms, why it is harder to w |
| 4340 Steel | 4340 nickel-chromium-molybdenum steel: 260 ksi vacuum-melted design values, AMS 6414, temper embrittlement, an |
| 8740 Steel | 8740 nickel-chromium-molybdenum steel for aircraft: the alternate to 4140, AMS 6322 and 6323 specs, 125 ksi ba |
| A-286 Alloy | A-286 iron-base alloy for aircraft: AMS 5525 sheet, solution treated and aged, 140 ksi, strength to 1,300 °F, |
| H-11 Tool Steel (5Cr-Mo-V) | H-11 / 5Cr-Mo-V aircraft steel: strength to 1,000 °F, AMS 6437 sheet and AMS 6487/6488 bar, 240–280 ksi design |
| 4130 Steel | 4130 chromium-molybdenum steel for aircraft: composition, density, tubing specs, TIG welding rules for thin wa |
Where to buy
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Educational reference only. not approved data. Always consult the applicable SRM, AMM, or AC 43.13-1B and your certifying authority.