{"id":3549,"date":"2026-09-16T10:58:58","date_gmt":"2026-09-16T07:58:58","guid":{"rendered":"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8620\/"},"modified":"2026-09-25T16:31:06","modified_gmt":"2026-09-25T13:31:06","slug":"aisi-8620","status":"publish","type":"page","link":"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8620\/","title":{"rendered":"AISI 8620 \/ AMS 6274"},"content":{"rendered":"<p><!-- dm-hap --><\/p>\n<h1 class=\"dm-ust-baslik\" style=\"font-family:-apple-system,BlinkMacSystemFont,'Segoe UI',Helvetica,Arial,sans-serif !important;text-transform:none !important;font-size:27px;line-height:1.3;font-weight:800;color:#12303f;margin:0 0 10px;letter-spacing:-.01em;\">AISI 8620 \/ (1.6523) \/ UNS G86200 \/ AMS 6274<\/h1>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"background:#12303f;padding:14px 16px 12px;position:relative;z-index:2;\">\n<div style=\"font-size:22px;font-weight:700;color:#fff;line-height:1.25;\">AISI 8620<\/div>\n<div style=\"font-family:ui-monospace,Menlo,Consolas,monospace;font-size:12.5px;color:#b9cfdb;line-height:1.5;margin-top:5px;word-wrap:break-word;\">UNS G86200 (hardenability-band grade 8620H = H86200) \u00b7 W.Nr. 1.6523 \u00b7 EN 10084 name 20NiCrMo2-2 (FORMER DIN NAME 21NiCrMo2; resulphurised free-machining variant 20NiCrMoS2-2 = 1.6526) \u00b7 SAE J404 \/ ASTM A29 band: C 0.18-0.23% &#8211; Mn 0.70-0.90% &#8211; Si 0.15-0.35% &#8211; Ni 0.40-0.70% &#8211; Cr 0.40-0.60% &#8211; Mo 0.15-0.25% &#8211; P 0.035% max &#8211; S 0.040% max &#8211; balance Fe. The nominal form used in the AMS titles is 0.50Cr &#8211; 0.55Ni &#8211; 0.20Mo (0.18-0.23C). THE EN 10084 20NiCrMo2-2 BAND IS NOT THE SAME: C 0.17-0.23% &#8211; Si 0.40% max &#8211; Mn 0.65-0.95% &#8211; Cr 0.35-0.70% &#8211; Mo 0.15-0.25% &#8211; Ni 0.40-0.70% &#8211; P 0.025% max &#8211; S 0.020-0.040%. The EN band is WIDER on chromium and manganese, and EN also sets a LOWER limit on sulphur (0.020%) where SAE sets none. Material delivered against a 20NiCrMo2-2 certificate therefore does not automatically satisfy an 8620 order; acceptance depends on the heat analysis meeting both bands. IT IS A CARBURIZING (CASE-HARDENING) STEEL: its carbon is low and it does not harden usefully by direct quenching; carbon is diffused into the surface to give a hard case over a tough core. IT IS NOT STAINLESS. IT DOES NOT PRECIPITATION HARDEN; there is no H900 \/ H1025 \/ H1150 type ageing step.<\/div>\n<div data-dmkars-blok=\"1\" style=\"border-top:1px solid rgba(255,255,255,.16);margin-top:13px;padding-top:11px;\">\n<div style=\"font-size:10px;letter-spacing:.09em;text-transform:uppercase;color:#7f9fb0;font-weight:700;margin-bottom:8px;\">Not to be confused with<\/div>\n<p><a href=\"https:\/\/www.defencemetal.com\/index.php\/2026\/09\/15\/aisi-8620-aisi-9310-difference\/\" data-dmkars=\"1\" style=\"display:inline-block;padding:4px 11px;border:1px solid rgba(36,190,229,.45);background:rgba(36,190,229,.12);border-radius:99px;margin:0 6px 6px 0;font-size:12.5px;font-weight:600;color:#9fe2f7;text-decoration:none;\">AISI 9310<\/a><\/div>\n<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">For what<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Bought for parts whose surface must resist wear while the body underneath takes impact: gears and ring-and-pinion sets, pinions, shafts and spindles, pins and bushings, chains and sprockets, hydraulic pump bodies, drilling and earth-moving components, plastic moulds.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Forms<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">Supplied as bar, flat bar, plate, sheet, tube and forgings.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Standards<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">AMS (verified, 0.50Cr &#8211; 0.55Ni &#8211; 0.20Mo, C 0.18-0.23% chemistry): 6274 (BARS, FORGINGS, MECHANICAL TUBING AND FORGING STOCK; AIRCRAFT QUALITY; latest revision S\/2021) \u00b7 6276 (same product forms; CONSUMABLE ELECTRODE VACUUM REMELTED &#8211; VAR) \u00b7 6277 (same product forms; VACUUM ARC OR ELECTROSLAG REMELTED &#8211; VAR or ESR) \u00b7 6375 (WELDING WIRE; vacuum melted; environment-controlled packaging). Heat treatment procedure: <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2759<\/b>\/7 (Carburizing and Heat Treatment of Carburizing Grade Steel Parts). Cleanliness: <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2300<\/b> \/ 2301 \/ 2304. ASTM: A29 \/ A29M (general requirements, hot-wrought alloy bars) \u00b7 A322 (alloy steel bars, standard grades) \u00b7 A331 (cold-finished bars) \u00b7 A506 (hot-rolled sheet and strip) \u00b7 A507 (cold-rolled sheet and strip) \u00b7 A513 (ERW mechanical tubing) \u00b7 A519 (seamless mechanical tubing) \u00b7 A534 (carburizing steels for anti-friction bearings) \u00b7 A646 (premium quality blooms and billets for aerospace forgings) \u00b7 A711 (stock for forgings) \u00b7 A752 (alloy steel wire rod) \u00b7 A829 (alloy structural steel plate). SAE: J404 (chemistry) \u00b7 J1268 (hardenability bands for H grades) \u00b7 J1397. EN and others: EN 10084 20NiCrMo2-2 (1.6523) and 20NiCrMoS2-2 (1.6526) \u00b7 BS 970 805M20 \u00b7 AFNOR 20NCD2 \u00b7 JIS SNCM220 \u00b7 SS 2506. Military: MIL-S-8690 (8620 bars, aircraft quality).<br \/><span style=\"font-size:12.5px;color:#7b8f9b;line-height:1.6;display:inline-block;margin-top:6px;\">AMS 6274, 6276 AND 6277 ARE NOT INTERCHANGEABLE. All three share one chemistry and all three cover the same product forms (bars, forgings, tubing); THE DIFFERENCE IS THE MELTING METHOD.<\/span><\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Advantage<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">That one chemistry is covered on both the general-industrial and the aerospace side, and can be tied to numbers on both. On the industrial side the EN 10084 core table as printed by Saarstahl guarantees tensile strength by diameter after carburizing and tempering at 200 C: at least 1100 N\/mm2 up to\u2026<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#F7FAFB;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;line-height:1.5;\">Welding<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;\">WELDABLE IN THE UNCARBURIZED (as-delivered) CONDITION. Its carbon is 0.18-0.23%, which makes it more amenable to welding than quench-and-temper grades such as 4140 or 8740.<\/div>\n<\/div>\n<div style=\"display:flex;flex-wrap:wrap;border-top:1px solid #eceff1;\">\n<div style=\"flex:0 0 118px;padding:11px 14px;background:#fdeceb;font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#c0392b;font-weight:600;line-height:1.5;\">Limits<\/div>\n<div style=\"flex:1 1 230px;min-width:0;padding:11px 14px;font-size:14.5px;line-height:1.7;color:#3d5260;word-wrap:break-word;overflow-wrap:break-word;background:#fdeceb;\">1) IT IS NOT STAINLESS. Chromium is 0.40-0.60% and no passive layer forms. Without plating, phosphating, oil or paint it rusts in damp conditions; it is not suitable for marine or chloride-bearing environments.<br \/>\n2) IT DOES NOT HARDEN ON ITS OWN. Its carbon is 0.18-0.23%.<\/div>\n<\/div>\n<div style=\"padding:14px;border-top:1px solid #eceff1;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;background:#dd3333;color:#ffffff;\">REQUEST A QUOTE<\/a><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/alloy-steels\/\" style=\"display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;font-weight:600;border:1px solid #12303f;color:#12303f;\">All alloy steels &rarr;<\/a><span data-dm=\"dm-teknik\" style=\"cursor:pointer;display:inline-block;padding:11px 20px;font-size:14px;font-weight:700;text-decoration:none;margin:0 8px 6px 0;border:1px solid #dd3333;color:#dd3333;\">TECHNICAL DETAILS &darr;<\/span><\/div>\n<div style=\"padding:9px 14px;border-top:1px solid #eceff1;font-size:11.5px;color:#8a9aa4;line-height:1.5;\">Compiled from manufacturer data sheets \u00b7 confirm against the current specification before ordering<\/div>\n<\/div>\n<\/div>\n<p><!-- \/dm-hap --><!-- dm-nav --><\/p>\n<style>h4[id^=\"dm-b\"]{scroll-margin-top:120px}#dm-teknik{scroll-margin-top:120px}<\/style>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:0 0 22px;padding:12px 14px;\">\n<div style=\"font-size:10.5px;letter-spacing:.09em;text-transform:uppercase;color:#6b8091;font-weight:600;margin-bottom:9px;\">On this page &middot; click to jump<\/div>\n<div><span data-dm=\"dm-b0\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">What AISI 8620 Is<\/span><span data-dm=\"dm-b1\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Standards by Product Form<\/span><span data-dm=\"dm-b2\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Specification Gaps<\/span><span data-dm=\"dm-b3\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Chemical Composition<\/span><span data-dm=\"dm-b4\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">CARBURIZING<\/span><span data-dm=\"dm-b5\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">RETAINED AUSTENITE and DIMENSIONAL INSTABILITY<\/span><span data-dm=\"dm-b6\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Hardenability and Core Properties<\/span><span data-dm=\"dm-b7\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Mechanical Properties<\/span><span data-dm=\"dm-b8\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Physical Properties<\/span><span data-dm=\"dm-b9\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Welding<\/span><span data-dm=\"dm-b10\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Machining<\/span><span data-dm=\"dm-b11\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Corrosion<\/span><span data-dm=\"dm-b12\" style=\"cursor:pointer;display:inline-block;padding:5px 11px;border:1px solid #dfe6ea;background:#F7FAFB;margin:0 6px 7px 0;font-size:13px;color:#12303f;\">Frequently Asked Questions<\/span><\/div>\n<\/div>\n<p><script>(function(){function go(id){var e=document.getElementById(id);if(e){var s=document.scrollingElement||document.documentElement;var y=e.getBoundingClientRect().top+s.scrollTop-118;if(y-0-0-0-0!==y){y=0;}window.scrollTo(0,y);}}function bind(el){el.addEventListener(\"click\",function(ev){ev.preventDefault();go(el.getAttribute(\"data-dm\"));});}function init(){var l=document.querySelectorAll(\"[data-dm]\");Array.prototype.forEach.call(l,bind);if(location.hash){if(location.hash.indexOf(\"#dm-\")===0){try{history.replaceState(null,\"\",location.pathname+location.search);}catch(e){}window.scrollTo(0,0);setTimeout(function(){window.scrollTo(0,0);},80);}}}if(document.readyState===\"loading\"){document.addEventListener(\"DOMContentLoaded\",init);}else{init();}})();<\/script><!-- \/dm-nav --><br \/>\n<span id=\"dm-teknik\" style=\"display:block;height:0;overflow:hidden;\"><\/span><br \/>\nAISI 8620 is a low-carbon nickel-chromium-molybdenum alloyed case hardening (carburising) steel. What separates it from through-hardening grades such as 4140 and 4340 in the alloy steel group is that it gains its hardness not through its bulk but by carbon being diffused into its surface.<\/p>\n<p>Keeping the carbon content low allows the core to remain tough and impact resistant. After the part has been machined, carbon is diffused into its surface in a carburising furnace, then it is quenched and tempered. The result is a hard, wear resistant outer layer over a tough core able to absorb impact \u2014 exactly the structure sought for gears and rolling contact surfaces.<\/p>\n<p>Nickel raises core toughness, while chromium and molybdenum increase hardenability and the strength of the carburised case. This composition makes 8620 the most widely used and most readily available grade among the case hardening steels.<\/p>\n<p>It is used in aerospace and defence for gearbox components, transmission gears, cams, pins and bushings, and in general machine building for shafts, sprockets and bearing housing parts. It can be supplied as round bar and forgings.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Chemical Composition \u00b7 AISI 8620<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">C \u2014 Carbon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.18 \u2013 0.23%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Ni \u2014 Nickel<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">0.40 \u2013 0.70%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Cr \u2014 Chromium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.40 \u2013 0.60%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Mo \u2014 Molybdenum<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">0.15 \u2013 0.25%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Mn \u2014 Manganese<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.70 \u2013 0.90%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Fe \u2014 Iron<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Balance<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Heat Treatment \u00b7 AISI 8620<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Carburising<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">900 \u2013 925 \u00b0C, in carburising atmosphere<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Hardening<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">~830 \u00b0C, oil quench<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Tempering<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">150 \u2013 200 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Result<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Hard case + tough core<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<div class=\"dm-std\" style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards and Equivalents \u00b7 AISI 8620<\/div>\n<div data-dmtw=\"1\" style=\"position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;overflow-x:auto;\">\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Trade name<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">AISI 8620<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">UNS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">G86200<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">W.Nr (DIN\/EN)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">1.6523<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">AMS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">6274<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Available forms<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Round bar \u00b7 Flat bar \u00b7 Plate \u00b7 Sheet \u00b7 Tube \u00b7 Forgings<br \/><span style=\"font-size:13px;color:#6b7a84;\">All forms are supplied to order.<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"margin:28px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;font-size:15px;line-height:1.7;\">\n<p style=\"margin:0 0 10px;\"><span style=\"color:#DD3333;font-weight:700;\">\u2192<\/span> Contact us for AISI 8620 stock availability, sizes and AMS 6274 certified supply.<\/p>\n<p style=\"margin:0;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/contact\/\" style=\"display:inline-block;background:#DD3333;color:#ffffff;font-weight:700;font-size:14px;padding:9px 16px;text-decoration:none;\">Request a quote<\/a><\/p>\n<\/div>\n<div style=\"margin:22px 0 0;padding:14px 16px;border:1px solid #e0e0e0;background:#FBFCFD;\">\n<p style=\"font-size:11px;font-weight:700;letter-spacing:.08em;text-transform:uppercase;color:#9aa3a8;margin:0 0 8px;line-height:1.4;\">Related grades<\/p>\n<p style=\"margin:0;font-size:15px;line-height:2;color:#333;\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-9310\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AISI 9310<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8740\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AISI 8740<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AISI 4140<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4340\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AISI 4340<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/alloy-steels\/\" style=\"color:#666;font-weight:600;text-decoration:none;\">All alloy steels \u2192<\/a><\/p>\n<\/div>\n<p><!-- dm-zengin --><\/p>\n<h4 id=\"dm-b0\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">What AISI 8620 Is \u2014 and Why You Cannot Order a Hardness Number<\/h4>\n<p><!-- dm-diy-sert --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STRENGTH VALUES<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 10px 0;\"><svg viewBox=\"0 0 740 300\" style=\"width:100%;height:auto;display:block;\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\" role=\"img\"><rect x=\"16\" y=\"6\" width=\"12\" height=\"12\" fill=\"#12303f\"\/><text x=\"34\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Yield (MPa)<\/text><rect x=\"146\" y=\"6\" width=\"12\" height=\"12\" fill=\"#7fa8bd\"\/><text x=\"164\" y=\"16\" font-size=\"11.5\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">Tensile (MPa)<\/text><text x=\"16\" y=\"44\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">CORE \u00b7 hardened and tempered at 200 C \u00b7 up to 16 mm diameter<\/text><rect x=\"16\" y=\"50\" width=\"607.8\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"630.8\" y=\"62\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">1100<\/text><text x=\"16\" y=\"90\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">CORE \u00b7 hardened and tempered at 200 C \u00b7 16 to 40 mm diameter<\/text><rect x=\"16\" y=\"96\" width=\"442.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"465.0\" y=\"108\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">800<\/text><text x=\"16\" y=\"136\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">CORE \u00b7 hardened and tempered at 200 C \u00b7 40 to 100 mm diameter<\/text><rect x=\"16\" y=\"142\" width=\"386.8\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"409.8\" y=\"154\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">700<\/text><text x=\"16\" y=\"182\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">CORE \u00b7 11 mm reference specimen (core hardening plus stress relief)<\/text><rect x=\"16\" y=\"188\" width=\"652.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"675.0\" y=\"200\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">1180<\/text><rect x=\"16\" y=\"206\" width=\"513.9\" height=\"15\" fill=\"#12303f\"\/><text x=\"536.9\" y=\"218\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">930<\/text><text x=\"16\" y=\"246\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">CORE \u00b7 30 mm reference specimen (core hardening plus stress relief)<\/text><rect x=\"16\" y=\"252\" width=\"458.6\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"481.6\" y=\"264\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">830<\/text><rect x=\"16\" y=\"270\" width=\"326.0\" height=\"15\" fill=\"#12303f\"\/><text x=\"349.0\" y=\"282\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">590<\/text><\/svg><\/div>\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Condition<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Hardness<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Yield MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Tensile MPa<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Elongation<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">EN 10084 \u00b7 20NiCrMo2-2 \u00b7 +A (soft-annealed delivery condition)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">212 HBW max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Saarstahl \u00b7 delivery condition +S (cold shearable)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">161-212 HB<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">CORE \u00b7 hardened and tempered at 200 C \u00b7 up to 16 mm diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1100 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">CORE \u00b7 hardened and tempered at 200 C \u00b7 16 to 40 mm diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">800 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">CORE \u00b7 hardened and tempered at 200 C \u00b7 40 to 100 mm diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">700 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">CORE \u00b7 11 mm reference specimen (core hardening plus stress relief)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">354-438 HB<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">930 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1180-1570<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">7% min<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">CORE \u00b7 30 mm reference specimen (core hardening plus stress relief)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">249-339 HB<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">590 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">830-1130<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">10% min<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">CASE \u00b7 carburized surface, 0.25 mm depth<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">64 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">CASE \u00b7 carburized surface, 0.50 mm depth<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">60.5 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">CASE \u00b7 carburized surface, 0.65 mm depth<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">57.5 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">JOMINY \u00b7 8620H hardenability band \u00b7 1.5 mm from the quenched end<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">41-49 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">JOMINY \u00b7 8620H hardenability band \u00b7 9 mm from the quenched end<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">22-36 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">JOMINY \u00b7 8620H hardenability band \u00b7 40 mm from the quenched end<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">about 20-24 HRC<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">&#8211;<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\"><b style=\"color:#12303f;\">THE TABLE CONTAINS THREE DIFFERENT MEASUREMENT LOCATIONS AND THEY ARE NOT INTERCHANGEABLE: the CASE rows come from the carburized surface, the CORE rows from the middle of the part, and the JOMINY rows from the end-quench test. The akma_mpa and cekme_mpa columns carry ONLY the MPa value; the ksi equivalents are in separate columns. The core rows depend on DIAMETER: the same material gives a lower tensile strength in a heavy section because hardenability is limited. The case rows are NOT A SPECIFICATION MINIMUM but Lucefin&#8217;s measured curve; on a real part the case hardness depends on carbon potential, case depth and tempering temperature.<\/b> In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. THE CASE, CORE AND JOMINY ROWS CANNOT BE COMPARED WITH ONE ANOTHER: all three are measured in different places under different test rules. The core tensile rows are SPECIFICATION MINIMA; they are the guaranteed floor, not typical values. The case rows come from a SINGLE SOURCE (Lucefin) and are given here under that source&#8217;s name. As a matter of rule they are not presented as specification values; the actual case hardness of a part depends on the carburizing cycle. NO SINGLE FIGURE IS STATED for the 40 mm Jominy row: the value is read off a curve and the small difference between the Rodacciai and Ovako curves has not been papered over with an average. Typical tensile and yield figures for uncarburized (quenched only) 8620 ARE NOT IN THE TABLE; every source found derives from the same ASM database, so the four-independent-source requirement is not met.<\/div>\n<\/div>\n<p><!-- \/dm-diy-sert --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">AISI\/SAE <b>8620<\/b> (UNS <b>G86200<\/b> \/ W.Nr. <b>1.6523<\/b> \/ EN <b>20NiCrMo2-2<\/b> \/ former DIN designation <b>21NiCrMo2<\/b> \/ BS <b>805M20<\/b> \/ AFNOR <b>20NCD2<\/b> \/ JIS <b>SNCM220<\/b>) is a <b>low-carbon, triple-alloyed (Ni-Cr-Mo) CASE-HARDENING \u2014 that is, carburizing \u2014 steel<\/b>. Its single distinguishing sentence is this: <b>it is the most widely used carburizing steel in the world, because it carries small amounts of all three alloying elements, and those small amounts buy a core toughness that single-element budget grades cannot deliver at the same price.<\/b><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>And the first thing that has to be said: when you buy 8620, you are NOT buying a hardness.<\/b> Carbon is nominally <b>0.20 %<\/b>. The maximum martensitic hardness achievable with that carbon is roughly <b>45 HRC<\/b> \u2014 so 8620 <b>can never reach 60 HRC on its own<\/b>. The <b>58\u201362 HRC<\/b> figure you see on datasheets is not the hardness of the steel; it is the hardness of <b>carbon that a carburizing furnace loaded into the surface afterwards<\/b>. <b>The steel is only a carrier; the hardness is produced by the heat treater.<\/b> That is the single most important sentence on this page, and everything below is built on it.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The engineering sits in <b>three elements present together in small amounts<\/b>. <b>Chromium (0.40\u20130.60 %)<\/b> and <b>molybdenum (0.15\u20130.25 %)<\/b> delay the pearlite and bainite transformations \u2014 that is, they provide <b>hardenability<\/b>. <b>Nickel (0.40\u20130.70 %)<\/b> contributes to hardenability too, but does its real work elsewhere: it <b>solid-solution strengthens the ferrite matrix and pushes the ductile-to-brittle transition temperature DOWN<\/b> \u2014 it keeps the core tough in the cold. Chromium-manganese carburizing steels (16MnCr5, 20MnCr5) have no nickel, and <b>that is exactly where the difference shows up<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Honest Position in the Family \u2014 Which Steel for Which Job<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Versus <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-9310\/\">AISI 9310<\/a> (E9310)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">9310 is nominally <b>0.10 C \u00b7 3.25 Ni \u00b7 1.20 Cr \u00b7 0.12 Mo<\/b>. Nickel is roughly <b>six times<\/b> higher, chromium <b>twice<\/b>. The result: <b>far higher hardenability, far higher core strength and markedly better low-temperature toughness<\/b>. 9310 is sold under <b>AMS 6260 \/ 6265 \/ 6267<\/b> and typically <b>vacuum melted (VAR\/CEVM)<\/b> \u2014 helicopter transmission gears and aero-engine gears are its territory. <b>The price: several times the cost, long lead times, worse machinability.<\/b> <b>Rule:<\/b> flight-critical parts, or cores that must absorb impact at \u221250 \u00b0C, take 9310; automotive and industrial gears, pins and bushings take 8620<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Versus AISI 4320<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Same carbon (<b>0.17\u20130.22 %<\/b>) and the same chromium band, but <b>1.65\u20132.00 % Ni<\/b> (8620 has 0.40\u20130.70) and <b>0.20\u20130.30 % Mo<\/b>. 4320 sits <b>exactly between 8620 and 9310<\/b>: it is the right answer where 8620 runs out and 9310 is overkill. <b>Rule:<\/b> once the section exceeds \u230075 mm, or the core yield required is above what 8620 delivers, <b>try 4320 first<\/b> and go to 9310 only afterwards<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Versus 16MnCr5 (1.7131) and 20MnCr5 (1.7147)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">These are Europe&#8217;s volume carburizing steels and they run on the <b>Mn-Cr system: there is NO nickel and NO molybdenum<\/b>. Two consequences. <b>In their favour:<\/b> markedly cheaper, and in thin sections they give comparable surface hardness. <b>Against them:<\/b> without nickel the <b>core toughness, and especially low-temperature toughness, is lower<\/b>; without molybdenum the <b>hardenability is shallower<\/b>. <b>Rule:<\/b> small parts, room temperature, hard cost pressure \u2192 16MnCr5\/20MnCr5; heavy sections, impact, or cold service \u2192 8620<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Versus 18CrNiMo7-6 (1.6587)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">This is Europe&#8217;s heavy-section carburizing steel; <b>chromium and nickel are well above 8620<\/b>. In wind-turbine gearing, large reducers and rail gears \u2014 <b>big module, thick section<\/b> \u2014 8620 simply does not have the hardenability and the core stays bainitic or ferritic. <b>Above module 8, question whether 8620 is the right steel.<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Versus <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/\">AISI 4140<\/a> and <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8740\/\">AISI 8740<\/a> \u2014 A CATEGORY ERROR<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Those are <b>quenched-and-tempered (through-hardening) steels<\/b> at <b>0.38\u20130.43 % C<\/b>. Their job is to produce <b>one uniform structure throughout<\/b>. 8620&#8217;s job is to produce <b>a hard case over a tough core<\/b>. &#8220;Which is harder, 8620 or 4140?&#8221; is <b>the wrong question<\/b>; the right one is <b>&#8220;is the surface loaded, or the bulk?&#8221;<\/b> Surface wear and root bending fatigue \u2192 8620; a shaft body in torsion or bending \u2192 4140 or 8740<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Versus nitriding steels (e.g. 31CrMoV9, 41CrAlMo7)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Nitriding runs at about <b>500\u2013530 \u00b0C<\/b> \u2014 <b>no phase transformation, no quench, minimal distortion<\/b>. Carburizing 8620 means <b>900\u2013955 \u00b0C plus a quench<\/b>: the part <b>will distort<\/b>. <b>Rule:<\/b> if dimensional stability is critical and a shallow 0.3 mm hard layer suffices, nitride; if you need a load-bearing case 1\u20132 mm deep, carburize \u2014 accept the distortion and leave grinding stock<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Versus stainless grades (<a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/17-4ph-1-4542-aisi-630\/\">17-4 PH<\/a> etc.)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>The comparison ends the moment corrosion resistance is required.<\/b> 8620 is <b>not stainless<\/b>, and carburizing does not make it stainless \u2014 if anything, high-carbon martensite <b>rusts more readily<\/b>. A carburized part working wet or in chemicals <b>must be plated or kept under an oil film<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">8620, 8620H, 8620RH and &#8220;carburized 8620&#8221; \u2014 four different purchase-order lines<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>8620<\/b> is a chemistry specification (ASTM A29 \/ A322, SAE J404). <b>8620H<\/b> is a <b>hardenability specification<\/b>: the chemistry band widens slightly (C <b>0.17\u20130.23 %<\/b>, Mn <b>0.60\u20130.95 %<\/b>, Cr <b>0.35\u20130.65 %<\/b>, Ni <b>0.35\u20130.75 %<\/b>, Mo <b>0.15\u20130.25 %<\/b>) but the mill <b>guarantees the Jominy end-quench band<\/b>. <b>8620RH<\/b> (restricted hardenability, SAE J1868) narrows the band further. <b>&#8220;Carburized 8620&#8221;<\/b> is neither a chemistry nor a standard \u2014 it is a <b>process outcome<\/b>, and what defines that outcome is not the steel&#8217;s chemistry but <b>the recipe the heat treater writes<\/b>. Do not put all four on the same purchase-order line.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The practical rule:<\/b> if you or your subcontractor will do the heat treatment and you want batch-to-batch repeatability, <b>buy 8620H, not 8620<\/b>. A plain &#8220;8620&#8221; order does not guarantee hardenability; two heats that both meet the specification can come out of the same furnace on the same cycle <b>several HRC apart in the core<\/b>.<\/p>\n<h4 id=\"dm-b1\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Standards by Product Form<\/h4>\n<p><!-- dm-diy-std --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">STANDARDS BY PRODUCT FORM<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Product form<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Standards<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Round bar \u00b7 flat bar (shapes)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6274<\/b> (bars, forgings, mechanical tubing and forging stock; AIRCRAFT QUALITY) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6276<\/b> (same forms; VAR) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6277<\/b> (same forms; VAR or ESR) \u00b7 ASTM A29 \/ A29M (general requirements) \u00b7 ASTM A322 (alloy steel bars, standard grades) \u00b7 ASTM A331 (cold-finished bars) \u00b7 EN 10084 20NiCrMo2-2 \/ 20NiCrMoS2-2 \u00b7 BS 970 805M20 \u00b7 MIL-S-8690 (aircraft-quality bars)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Mechanical tubing<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6274<\/b> \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6276<\/b> \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6277<\/b> (all three cover mechanical tubing) \u00b7 ASTM A519 (seamless mechanical tubing) \u00b7 ASTM A513 (ERW mechanical tubing)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Plate \u00b7 sheet \u00b7 strip<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">ASTM A506 (hot-rolled sheet and strip) \u00b7 ASTM A507 (cold-rolled sheet and strip) \u00b7 ASTM A829 (alloy structural steel plate). NO AMS number covering flat product for 8620 could be verified across four sources.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Forgings \u00b7 rings \u00b7 forging stock<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6274<\/b> (forgings and forging stock; aircraft quality) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6276<\/b> (VAR) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6277<\/b> (VAR or ESR) \u00b7 ASTM A711 (stock for forgings) \u00b7 ASTM A646 (premium quality blooms and billets for aerospace forgings)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Wire \u00b7 wire rod<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">ASTM A752 (alloy steel wire rod). Apart from welding wire, no AMS WIRE number specific to 8620 could be verified across four sources.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Welding filler metal<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6375<\/b> (welding wire, 0.50Cr &#8211; 0.55Ni &#8211; 0.20Mo, C 0.18-0.23%, vacuum melted, environment-controlled packaging)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Bearing components<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">ASTM A534 (Standard Specification for Carburizing Steels for Anti-Friction Bearings)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Carburizing and heat treatment procedure<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2759<\/b>\/7 (Carburizing and Heat Treatment of Carburizing Grade Steel Parts) \u00b7 EN 10084 annex (heat treatment temperatures) \u00b7 SAE J1268 (hardenability bands for H grades)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">Cleanliness \/ internal quality<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2300<\/b> \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2301<\/b> \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2304<\/b> (magnetic particle cleanliness classes, invoked from within the AMS numbers)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">Welding procedure group<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">NO ASME SECTION IX P-NUMBER IS STATED: 8620 is not listed as an ASME BPVC base metal and no P-Number could be verified across four independent sources.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">AMS numbers come FIRST in every row, with ASTM and EN after them. Three AMS numbers covering one product form IS NOT A CHOICE: 6274 carries no remelting requirement, 6276 requires VAR, and 6277 permits VAR or ESR. No AMS number specific to 8620 was found for flat product (sheet, strip, plate); that gap is stated explicitly. AMS 2759\/7 is not a material specification but a PROCEDURE specification; the carburizing cycle is tied to it.<\/div>\n<\/div>\n<p><!-- \/dm-diy-std --><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Standards by Product Form \u00b7 AISI 8620 (G86200 \/ 1.6523 \/ 20NiCrMo2-2)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>General requirements<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A29 \/ A29M<\/b> \u2014 general requirements for hot-wrought steel bars. <b>This is the companion document for 8620<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Alloy steel bar (hot wrought)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A322<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Cold-finished bar<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A331<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Hot-rolled sheet and strip<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A506<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Cold-rolled sheet and strip<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A507<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Seamless mechanical tubing<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A519<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">ERW (electric-resistance-welded) mechanical tubing<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A513<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Aircraft-quality billet \u00b7 bloom \u00b7 slab<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A646<\/b> \u2014 8620 is listed in the premium quality class as <b>A646 grade 8620-4<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Wire rod<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A752<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Structural plate<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A829<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Bearing-quality carburizing steel<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A534<\/b> \u2014 &#8220;Carburizing Steels for Anti-Friction Bearings&#8221;. <b>8620 falls within its scope<\/b>, and here the <b>cleanliness and sulphur\/phosphorus limits tighten<\/b>. If you are having bearing races or tapered roller components made, this is the standard to cite<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>SAE<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>J404<\/b> (chemical compositions) \u00b7 <b>J1397<\/b> (estimated mechanical properties) \u00b7 <b>J1268<\/b> (hardenability bands for H steels) \u00b7 <b>J1868<\/b> (restricted hardenability bands \u2014 RH grades)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Aerospace (AMS) \u2014 these three are NOT the same thing<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6274<\/b>: bars, forgings and mechanical tubing, <b>vacuum degassed (VD)<\/b>, quality level <b>AMS 2301<\/b>. <b>AMS 6276<\/b>: <b>consumable-electrode vacuum melted (CEVM\/VAR)<\/b>, quality <b>AMS 2300<\/b>. <b>AMS 6277<\/b>: <b>consumable-electrode melted (CEM)<\/b>, quality <b>AMS 2300<\/b>. <b>The difference is melting practice and cleanliness, not chemistry<\/b> \u2014 though 6276 and 6277 also tighten the chemistry: <b>Mn 0.70\u20131.00 % \u00b7 P \u22640.012 % \u00b7 S \u22640.010 %<\/b>. <b>They are not interchangeable<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Military<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>MIL-S-8690<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Europe \u2014 case-hardening steel<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>EN 10084<\/b>, grade <b>20NiCrMo2-2 (1.6523)<\/b> and its resulphurised variant <b>20NiCrMoS2-2 (1.6526)<\/b>. The old DIN 17210 designation was <b>21NiCrMo2<\/b>; <b>same material number, obsolete name<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Other national equivalents<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">BS 970 <b>805M20<\/b> (and <b>806M20<\/b>) \u00b7 AFNOR <b>20NCD2<\/b> \/ <b>22NCD2<\/b> \u00b7 JIS G4053 <b>SNCM220<\/b> \u00b7 GB\/T 3077 <b>20CrNiMo<\/b> \u00b7 SS <b>2506<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b2\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Specification Gaps \u2014 What &#8220;8620&#8221; Does Not Buy You<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>In 8620 the gap is not in the chemistry, it is in the PROCESS OUTCOME.<\/b> And that gap is the source of nearly every commercial dispute around this alloy: <b>you buy the chemistry, but what does the work is the case<\/b> \u2014 and the case is usually nowhere on the purchase order.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Gaps and Traps<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>&#8220;8620&#8221; alone commits to NO hardness and NO strength<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM A29 and A322 give <b>chemistry and general requirements<\/b>; they commit to <b>no<\/b> surface hardness, <b>no<\/b> case depth and <b>no<\/b> core yield. The same 8620 bar can sit anywhere between <b>149 HB (annealed)<\/b> and <b>62 HRC at the surface (carburized)<\/b>. <b>If your order line does not state case depth and core hardness, you have ordered nothing<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Case depth has THREE different definitions and they get confused<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Effective case depth<\/b>: distance from the surface to <b>50 HRC<\/b> (the most common definition). <b>Total case depth<\/b>: distance to the core structure \u2014 typically <b>1.5\u20132\u00d7 the effective<\/b>. <b>Chemical case depth<\/b>: where the carbon profile falls to a stated level. <b>&#8220;0.8 mm case&#8221; without naming the definition is meaningless<\/b> and can put the two parties 100 % apart<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The hardness measurement method belongs in the specification<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">On a thin case, <b>an HRC indentation reaches into the core and reads low<\/b>. The correct method is <b>superficial Rockwell (HR15N \/ HR30N)<\/b> or a <b>microhardness (HV0.3 \/ HV1)<\/b> traverse on a section. <b>Below about 0.4 mm of case, do not write HRC.<\/b> If you see a value like &#8220;Rc 90&#8221; on a distributor page, that is an <b>HR15N<\/b> number with the wrong unit<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Retained austenite is not specified \u2014 but it should be<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Retained austenite in a carburized case is unavoidable<\/b>, and how much you get depends on <b>surface carbon, quench route and whether a cryogenic step is used<\/b>. No base ASTM specification sets an upper limit. <b>If dimensional stability matters, make a retained austenite ceiling (typically 20 % or 15 % by volume) a purchase requirement<\/b> and state the measurement method (X-ray diffraction, ASTM E975)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Cast equivalent<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>There is no standardised cast counterpart to 8620.<\/b> Casting specifications (ASTM A148, A487) are written by <b>mechanical class<\/b>, not chemistry. And a cast structure carburizes differently from wrought product because of <b>segregation and porosity<\/b>. The honest answer to &#8220;cast 8620&#8221;: <b>choose an equivalent casting class<\/b> and define the case with a <b>separate heat-treatment specification<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Welding consumable equivalent<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>There is no such product as &#8220;8620 welding wire&#8221;.<\/b> Welding is done by <b>strength matching<\/b>: for the un-carburized \/ core strength level, <b>ER90S-G<\/b> or <b>E9018-G \/ E9018-M<\/b>. See the welding section below<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Wire and fasteners<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>ASTM A752<\/b> covers wire rod, but <b>there is no separate property-class standard for a carburized 8620 fastener<\/b>. If you want one, you must write <b>case depth, core hardness and whether the thread roots are to be carburized<\/b> line by line<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b3\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Chemical Composition<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The table below puts <b>three specification families side by side<\/b>. They are close but <b>not identical<\/b>, and the sentence &#8220;8620 = 20NiCrMo2-2&#8221; <b>should not be said without reading the mill certificate<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Chemical Composition \u2014 Weight %<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Element<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>SAE 8620 (ASTM A29\/A322)<\/b> \u00b7 <b>8620H<\/b> \u00b7 <b>EN 20NiCrMo2-2 (1.6523)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Carbon (C)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.18\u20130.23<\/b> \u00b7 <b>0.17\u20130.23<\/b> \u00b7 <b>0.17\u20130.23<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Manganese (Mn)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.70\u20130.90<\/b> \u00b7 <b>0.60\u20130.95<\/b> \u00b7 <b>0.65\u20130.95<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Silicon (Si)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.15\u20130.35<\/b> \u00b7 <b>0.15\u20130.35<\/b> \u00b7 <b>0.15\u20130.40<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Chromium (Cr)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.40\u20130.60<\/b> \u00b7 <b>0.35\u20130.65<\/b> \u00b7 <b>0.35\u20130.70<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Nickel (Ni)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.40\u20130.70<\/b> \u00b7 <b>0.35\u20130.75<\/b> \u00b7 <b>0.40\u20130.70<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Molybdenum (Mo)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.15\u20130.25<\/b> \u00b7 <b>0.15\u20130.25<\/b> \u00b7 <b>0.15\u20130.25<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Phosphorus (P)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u22640.035<\/b> \u00b7 <b>\u22640.035<\/b> \u00b7 <b>\u22640.025<\/b> \u2014 <b>Europe is tighter<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Sulphur (S)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22640.040<\/b> \u00b7 <b>\u22640.040<\/b> \u00b7 <b>\u22640.035<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Copper (Cu)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Not specified on the SAE side \u00b7 <b>\u22640.40<\/b> on the EN side<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Aluminium (Al)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Not specified on the SAE side \u00b7 <b>0.020\u20130.050<\/b> on the EN side \u2014 <b>this is a serious difference<\/b>: at carburizing temperature, AlN precipitates are what hold grain growth in check<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Iron (Fe)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Balance \u2014 roughly <b>96.9\u201398.0 %<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Three weak points in the sentence &#8220;8620 = 20NiCrMo2-2&#8221;<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>First: manganese.<\/b> SAE asks for <b>0.70\u20130.90 %<\/b>, EN for <b>0.65\u20130.95 %<\/b>. The common band is <b>0.70\u20130.90 %<\/b> \u2014 here EN is the wider one, so <b>a European heat at Mn = 0.93 % meets EN but fails SAE 8620<\/b>. (It does fit the 8620<b>H<\/b> band: 0.60\u20130.95 %.)<br \/><b>Second: chromium.<\/b> SAE <b>0.40\u20130.60 %<\/b>, EN <b>0.35\u20130.70 %<\/b>. Again EN is wider; a heat at Cr = 0.66 % fails SAE 8620.<br \/><b>Third, and most important: aluminium and cleanliness.<\/b> EN 10084 <b>requires Al 0.020\u20130.050 %<\/b> and a cleaner steel at <b>P \u22640.025 %<\/b>; on the SAE side there is <b>no<\/b> aluminium requirement and P runs to <b>0.035 %<\/b>. Aluminium is not decorative here: <b>in a steel held for hours at 900\u2013955 \u00b0C, AlN precipitation is the principal brake on grain growth<\/b>. A heat without aluminium carries a real risk of <b>abnormal grain growth<\/b>, and with it <b>distortion and loss of case toughness<\/b>.<br \/><b>What to do:<\/b> before issuing a dual certificate, compare the <b>Mn, Cr, P and especially Al lines<\/b> of the mill certificate one by one. If the Al line is blank, EN 10084 compliance cannot be claimed.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The resulphurised variant: 20NiCrMoS2-2 (1.6526)<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">EN 10084 also lists the same chemistry with sulphur <b>forced into the 0.020\u20130.040 % band<\/b>. Sulphur precipitates as manganese sulphide, breaks the chip and <b>markedly improves machinability<\/b>. <b>The price:<\/b> MnS inclusions elongate in the rolling direction and <b>reduce transverse ductility and impact toughness<\/b>. <b>Rule:<\/b> high-volume small parts on screw machines \u2192 1.6526; parts loaded transversely or subject to impact \u2192 <b>stay with 1.6523<\/b>.<\/p>\n<h4 id=\"dm-b4\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">CARBURIZING \u2014 the Heart of This Page<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">Carburizing means holding the steel <b>in the austenite range (above Ac3)<\/b> in a carbon-donating atmosphere so that <b>carbon diffuses into the surface<\/b>. 8620 was designed for exactly this: <b>the core stays at 0.20 % C and stays tough; the surface rises to 0.80\u20131.00 % C and, when quenched, transforms to high-carbon martensite and gets hard<\/b>. You end up with <b>two different steels in one part<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Carburizing Parameters \u00b7 AISI 8620<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Carburizing temperature (atmosphere)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>900\u2013955 \u00b0C (1650\u20131750 \u00b0F)<\/b>. The common operating point is <b>925 \u00b0C (1700 \u00b0F)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Carburizing temperature (vacuum \/ low pressure)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>900\u2013980 \u00b0C (1650\u20131800 \u00b0F)<\/b>. Because vacuum carburizing can run hotter, it reaches <b>the same depth in less time<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Carbon potential<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.9\u20131.1 %<\/b> during boost; reduced during the diffusion step<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Surface carbon after carburizing<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.80\u20131.00 %<\/b>. <b>Going above 1.00 % is not wanted<\/b>: carbide networks and excessive retained austenite<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Time \u2192 effective case depth (at 925 \u00b0C)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>0.5 mm (0.020\u2033) \u2248 2 h<\/b> \u00b7 <b>1.0 mm (0.040\u2033) \u2248 8 h<\/b> \u00b7 <b>1.5 mm (0.060\u2033) \u2248 18 h<\/b> \u00b7 <b>2.0 mm (0.080\u2033) \u2248 32 h<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>A second published set (same temperature, boost + diffuse)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.75 mm (0.030\u2033) \u2248 4 h<\/b> \u00b7 <b>1.5 mm (0.060\u2033) \u2248 16 h<\/b> \u00b7 <b>2.5 mm (0.100\u2033) &gt; 30 h<\/b>. <b>[conflict]<\/b> The two sets give different times for the same depths, because one is pure boost and the other a boost + diffusion cycle. <b>Do not make either an acceptance criterion; calibrate with a test coupon in your own furnace<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>The governing law<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Depth grows with the <b>SQUARE ROOT of time<\/b>. So <b>doubling the depth quadruples the time<\/b>. Both sets above are consistent with it: 0.5 \u2192 1.0 mm costs 2 \u2192 8 h<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Direct quench<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Straight from carburizing temperature into oil.<\/b> <b>The cheapest and fastest route<\/b> \u2014 it removes one heating from the cycle. <b>The price:<\/b> the grain size is the grain size of the carburizing temperature \u2014 <b>coarser grain, more retained austenite, more distortion<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Reheat quench<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">After carburizing the part is <b>slow cooled<\/b>, then re-austenitised in the <b>800\u2013855 \u00b0C<\/b> band and quenched in oil. European practice splits this into two targets: <b>860\u2013900 \u00b0C for the core<\/b>, <b>780\u2013820 \u00b0C for the case<\/b>. <b>Finer grain, less retained austenite, better toughness<\/b> \u2014 at the cost of an <b>extra cycle<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Quench medium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Agitated oil<\/b> is standard. Water quenching is avoided outside special cases because of <b>cracking and excessive distortion<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Tempering<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>150\u2013190 \u00b0C (300\u2013375 \u00b0F) for 2 h<\/b> is the most common recipe. Published ranges spread over <b>120\u2013200 \u00b0C (250\u2013400 \u00b0F)<\/b>. <b>The purpose is not to reduce hardness but to relieve quench stresses<\/b> \u2014 skip it and the part cracks in grinding or on first load<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Resulting surface hardness<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>58\u201362 HRC<\/b> (if the case is thick enough; on a thin case measure with HR15N or HV)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Resulting core hardness<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>25\u201340 HRC<\/b>, depending on section: <b>36\u201340 HRC in thin sections<\/b>, <b>28\u201332 HRC in heavy sections<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Effective case definition<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Distance from the surface to <b>50 HRC<\/b>. Typical commercial range <b>0.5\u20132.0 mm<\/b>. <b>Total case = 1.5\u20132\u00d7 the effective case<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Before and after carburizing \u2014 the complete cycle<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. Normalize (BEFORE machining).<\/b> <b>870\u2013925 \u00b0C (1600\u20131700 \u00b0F)<\/b>, <b>1 h per 25 mm<\/b> of section, <b>still air cool<\/b>. Result <b>149\u2013179 HB<\/b>. The purpose is not hardness but <b>erasing the banded structure and residual stresses left by rolling or forging<\/b>. Skip it and post-carburizing distortion becomes unpredictable.<br \/><b>2. Rough machining.<\/b> The part is at its most machinable here (149\u2013183 HB).<br \/><b>3. Stress relief (optional, but strongly advised after heavy cuts).<\/b> <b>595\u2013650 \u00b0C (1100\u20131200 \u00b0F)<\/b>. It removes the stresses roughing left behind, before the part goes into the carburizing furnace.<br \/><b>4. Masking.<\/b> Surfaces that must not carburize (areas to be threaded, bearing seats, surfaces that will not be ground) are protected with <b>copper plating or stop-off paint<\/b>. <b>The alternative: leave extra stock and machine the case away afterwards.<\/b><br \/><b>5. Carburize + quench + temper.<\/b> The table above.<br \/><b>6. Cryogenic treatment (if needed).<\/b> <b>BEFORE tempering<\/b> \u2014 see the next section.<br \/><b>7. Grinding \/ honing.<\/b> This is where distortion is taken out. <b>The stock left must not exceed half the case<\/b>; otherwise you grind away the hardest, highest-carbon layer.<\/p>\n<h4 id=\"dm-b5\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">RETAINED AUSTENITE and DIMENSIONAL INSTABILITY \u2014 the Section Usually Left Out<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Retained austenite in a carburized case is UNAVOIDABLE, and it is not a defect \u2014 it is physics.<\/b> Here is why: carbon lowers the martensite start temperature (<b>Ms<\/b>). In the core, carbon is <b>0.20 %<\/b> and Ms is far above room temperature \u2014 the core transforms completely. At the surface, carbon has risen to <b>0.80\u20131.00 %<\/b> and <b>Ms has fallen to near or below room temperature<\/b>. Because the quench stops at room temperature, <b>the transformation cannot finish<\/b> and some austenite <b>remains<\/b> in the case.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">The Three Consequences of Retained Austenite<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>1. Hardness comes out low<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Austenite is <b>soft and ductile<\/b>. With 25\u201330 % retained austenite by volume in the case, the measured surface hardness sits <b>several HRC below target<\/b>. &#8220;We carburized but could not make 58 HRC&#8221; has <b>this single cause more often than any other<\/b> \u2014 not case depth<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>2. The part changes size OVER TIME<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">This is the insidious one. <b>Austenite and martensite have different specific volumes.<\/b> In service, <b>stress, cold and time<\/b> gradually convert retained austenite to martensite, and that conversion means a <b>volume increase<\/b>. The result: <b>the part grows over months<\/b>, dimensions drift, bearing clearance closes, gear backlash disappears. The part <b>leaves the factory in tolerance<\/b> and <b>goes out of tolerance in the field<\/b> \u2014 your inspection cannot catch it<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>3. The case chips<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Soft austenite pockets<\/b> between hard martensite islands act as local yield sites under heavy Hertzian contact. That shows up as <b>edge chipping of the case<\/b> and early pitting<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The remedy: cryogenic (deep-freeze) treatment<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The logic is simple:<\/b> if the transformation stopped at room temperature, <b>go colder and let it continue<\/b>. In practice:<br \/><b>Temperature.<\/b> The published range is wide: cryogenic chambers reach <b>\u2212185 \u00b0C (\u2212300 \u00b0F)<\/b>, but for carburized 8620 the <b>\u221268 to \u221279 \u00b0C (\u221290 to \u2212110 \u00b0F)<\/b> band is often reported as <b>sufficient<\/b>. <b>Going to liquid-nitrogen temperature is not always necessary and brings thermal-shock risk.<\/b><br \/><b>Sequence \u2014 this is critical.<\/b> The cryogenic step goes <b>immediately after the quench and BEFORE tempering<\/b>. The reason: tempering redistributes carbon in the retained austenite and <b>stabilises it<\/b>. Once stabilised, that austenite <b>no longer transforms readily<\/b> on subsequent cooling. <b>Delay between quench and freeze starts the same stabilisation<\/b>, so keep the wait short.<br \/><b>And you must still temper.<\/b> The cryogenic step produces fresh martensite, and fresh martensite is <b>stressed and brittle<\/b>. <b>Tempering after the freeze is not optional.<\/b> On critical work a <b>temper\u2013freeze\u2013temper<\/b> double cycle is used.<br \/><b>When it is needed:<\/b> close-tolerance gears, bearing races, hydraulic valve bodies, long-life transmission parts. <b>When it is not:<\/b> loose-tolerance wear bushings and pins.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Is retained austenite always the enemy?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>No \u2014 and this is the honest side of the topic.<\/b> A measured amount (roughly 15\u201320 % by volume) <b>yields plastically under Hertzian contact and spreads the contact stress<\/b>, and in some rolling-contact fatigue (RCF) applications it <b>extends life<\/b>. The effect is well known in the bearing and gear literature. <b>The distinction is this:<\/b> if the loading is rolling contact, measured retained austenite <b>can help<\/b>; if the governing requirement is dimensional stability or edge strength, it <b>hurts<\/b>. <b>So &#8220;eliminate retained austenite&#8221; is not a universal rule<\/b>; write an application-specific <b>ceiling<\/b> instead.<\/p>\n<h4 id=\"dm-b6\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Hardenability and Core Properties<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">A carburized part raises <b>two separate hardenability questions<\/b>. The first is whether the <b>case<\/b> hardens \u2014 with carbon at 0.80 % that is nearly guaranteed. The second is whether the <b>core<\/b> hardens, and <b>that is the real engineering question<\/b>: if the core does not harden, the case sits on a <b>soft foundation<\/b> and <b>collapses like an eggshell<\/b>.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Jominy End-Quench Band \u2014 EN 10084, 20NiCrMo2-2 (HRC)<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Distance from quenched end<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>+H (standard)<\/b> \u00b7 <b>+HH (upper half)<\/b> \u00b7 <b>+HL (lower half)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">1.5 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>41\u201349<\/b> \u00b7 <b>44\u201349<\/b> \u00b7 <b>41\u201346<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">3 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>37\u201348<\/b> \u00b7 <b>41\u201348<\/b> \u00b7 <b>37\u201344<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">5 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>31\u201345<\/b> \u00b7 <b>36\u201345<\/b> \u00b7 <b>31\u201340<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">7 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>25\u201342<\/b> \u00b7 <b>31\u201342<\/b> \u00b7 <b>25\u201336<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">9 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>22\u201336<\/b> \u00b7 <b>27\u201336<\/b> \u00b7 <b>22\u201331<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">11 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>20\u201333<\/b> \u00b7 <b>24\u201333<\/b> \u00b7 <b>20\u201329<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Three things can be read from that table.<\/b><br \/><b>First \u2014 the band is WIDE.<\/b> At 7 mm the standard +H band is <b>25\u201342 HRC<\/b>: a <b>17 HRC spread<\/b>, and <b>both ends fully meet the specification<\/b>. So two heats both stamped &#8220;8620&#8221; can genuinely come out of the same furnace on the same cycle <b>with different cores<\/b>. The batch-to-batch scatter you are seeing is usually not a furnace fault but <b>a scatter the standard permits<\/b>.<br \/><b>Second \u2014 the fix is to order +HH or +HL.<\/b> These grades <b>split the band in two<\/b>. At the same distance, +HH gives you <b>31\u201342<\/b> and +HL <b>25\u201336<\/b>. Narrowing the band is <b>buying repeatability<\/b>. The US-side equivalent is the <b>8620RH<\/b> grades (SAE J1868).<br \/><b>Third \u2014 8620 hardens SHALLOW.<\/b> At 11 mm, hardness can fall to <b>20 HRC<\/b>. That means that a few millimetres inside the centre of an oil-quenched bar, the core will already be ferritic-bainitic. <b>If you need core strength in a heavy section, 8620 is the wrong steel<\/b> \u2014 look at 4320, 18CrNiMo7-6 or 9310.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>A single-source US figure:<\/b> one distributor quotes 8620H at <b>48 HRC maximum at 1\/16\u2033 (1.6 mm)<\/b> and <b>32 HRC minimum at 3\/16\u2033 (4.8 mm)<\/b>. Those values are <b>consistent<\/b> with the EN band above but have <b>not been independently verified<\/b>; check the current SAE J1268 table before making them an acceptance criterion.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">CORE Mechanical Properties After Case Hardening \u2014 EN practice, 200 \u00b0C temper<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Ruling section \u2300 \u226416 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>\u22651100 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>\u2300 16\u201340 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rm <b>\u2265800 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>\u2300 40\u2013100 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>\u2265700 MPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>General published band<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rm <b>660\u20131160 MPa<\/b> \u00b7 Re <b>470\u2013560 MPa<\/b> \u00b7 A <b>9\u201311 %<\/b> \u00b7 KU <b>25\u201330 J<\/b> \u00b7 hardness <b>229 HB max<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>How to read it<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Core strength COLLAPSES with section.<\/b> The same steel that gives 1100 MPa at \u230016 mm gives <b>700 MPa<\/b> at \u2300100 mm \u2014 a <b>36 % drop<\/b>. <b>Any core figure quoted without a section size is meaningless<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b7\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Mechanical Properties<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Read the first two rows of the table below carefully: they are the properties of UN-CARBURIZED 8620<\/b>, and many datasheets publish them on their own as &#8220;the mechanical properties of 8620&#8221;. <b>They do not describe the behaviour of a carburized part.<\/b><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Mechanical Properties \u00b7 AISI 8620 \u2014 Not Readable Without a Condition<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Condition<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Rm \u00b7 Rp0.2 \u00b7 A \u00b7 Z \u00b7 Hardness \u00b7 Impact<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Annealed (870 \u00b0C, furnace cool)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rm <b>530\u2013536 MPa<\/b> \u00b7 Rp0.2 <b>385 MPa<\/b> \u00b7 A <b>31.3 %<\/b> \u00b7 hardness <b>149 HB (\u224880 HRB)<\/b> \u00b7 Izod <b>\u2248115 J<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Normalized (915 \u00b0C, air)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>633\u2013635 MPa<\/b> \u00b7 Rp0.2 <b>357\u2013360 MPa<\/b> \u00b7 A <b>26\u201326.3 %<\/b> \u00b7 Z <b>60 %<\/b> \u00b7 hardness <b>183 HB<\/b> \u00b7 Izod <b>\u224898 J<\/b> <i>(\u230013 mm specimen)<\/i><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Normalized \u2014 section effect<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Hardness falls from <b>197 HB<\/b> at \u230013 mm to <b>179 HB<\/b> at \u230050\u2013100 mm<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>As-rolled<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm min <b>530 MPa<\/b> \u00b7 Rp0.2 min <b>385 MPa<\/b> \u00b7 A min <b>26 %<\/b> \u00b7 Z min <b>60 %<\/b> \u00b7 hardness max <b>149 HB<\/b> \u2014 <b>[conflict]<\/b> the same page also states <b>255 HB max<\/b>; the two cannot both be right, so read the certificate<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Delivery-condition hardness (EN practice)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Soft annealed <b>+A<\/b>, turned: <b>\u2264212 HB<\/b> \u00b7 <b>+A+C<\/b> cold drawn: <b>\u2264255 HB<\/b> \u00b7 ferrite-pearlite <b>+FP<\/b>, turned: <b>149\u2013194 HB<\/b> \u00b7 as-rolled: <b>\u2264212 HB<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>CARBURIZED \u2014 surface<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>58\u201362 HRC<\/b>. This belongs to <b>the case, not the steel<\/b>, and <b>must not be confused with the core<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>CARBURIZED \u2014 core<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>25\u201340 HRC<\/b> (thin sections <b>36\u201340<\/b>, heavy sections <b>28\u201332<\/b>); for core Rm see the section-size table above<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Through hardening without carburizing (alternative route)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Austenitize <b>830\u2013855 \u00b0C<\/b>, 1 h per 25 mm, oil; temper <b>205\u2013315 \u00b0C<\/b> for 2 h. Result <b>\u224840 HRC at the surface, \u224825 HRC in the core<\/b>. <b>Single source<\/b> \u2014 and in any case this is not what 8620 was designed to do<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Modulus of elasticity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>190\u2013212 GPa<\/b> (published values scatter). Shear modulus <b>73\u201380 GPa<\/b>, Poisson&#8217;s ratio <b>0.27\u20130.30<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Fatigue strength (un-carburized)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Reported in the <b>270\u2013360 MPa<\/b> band \u2014 <b>single source and wide<\/b>; do not use it as a design value<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>One oddity in the table needs explaining:<\/b> the annealed yield (<b>385 MPa<\/b>) appears <b>higher<\/b> than the normalized yield (<b>357\u2013360 MPa<\/b>), even though normalized tensile strength is higher. This is a known inconsistency in the published ASM-derived data and most likely comes from <b>different specimen diameters and mixed yield definitions<\/b> (lower yield point versus 0.2 % offset). <b>Do not use either value for design<\/b>; work from the certificate of your own delivery condition.<\/p>\n<h4 id=\"dm-b8\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Physical Properties<\/h4>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Physical Properties \u00b7 AISI 8620 \/ 20NiCrMo2-2<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Density<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>7.84\u20137.85 g\/cm\u00b3<\/b> (0.284 lb\/in\u00b3)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Modulus of elasticity (20 \u00b0C)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>205\u2013212 GPa<\/b>, falling to <b>164 GPa at 600 \u00b0C<\/b>. Some US sources quote <b>190 GPa<\/b> \u2014 the scatter is real<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Shear modulus<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>73\u201380 GPa<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Poisson&#8217;s ratio<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.29<\/b> (0.27\u20130.30 reported)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Thermal conductivity (20 \u00b0C)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>44\u201346.6 W\/m\u00b7K<\/b>, falling to <b>35.9 W\/m\u00b7K at 600 \u00b0C<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Specific heat (20 \u00b0C)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>460\u2013475 J\/kg\u00b7K<\/b>, rising to <b>587 J\/kg\u00b7K at 600 \u00b0C<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Coefficient of thermal expansion<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>10.5 \u00d710\u207b\u2076 \/K at \u2212100 \u00b0C<\/b> \u00b7 <b>14.4 \u00d710\u207b\u2076 \/K at 600 \u00b0C<\/b>. The single figure usually quoted near room temperature is <b>\u224813 \u00d710\u207b\u2076 \/K<\/b> \u2014 <b>using one number produces errors in shrink-fit calculations<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Electrical resistivity<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>1.6\u20132.25 \u00d710\u207b\u2077 \u03a9\u00b7m<\/b> (0.16\u20130.225 \u00b5\u03a9\u00b7m)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Melting range<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22481416\u20131460 \u00b0C<\/b> (2580\u20132660 \u00b0F)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Magnetic behaviour<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>FERROMAGNETIC.<\/b> Carburizing does not change that. It cannot be used anywhere a non-magnetic material is required<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\">Maximum service temperature<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Reported as <b>\u2248410 \u00b0C<\/b> \u2014 <b>single source<\/b>. But the real limit lies elsewhere: <b>the carburized case begins to soften above its tempering temperature (150\u2013190 \u00b0C)<\/b>. <b>Do not run a carburized part continuously above 200 \u00b0C<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b9\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Welding \u2014 When and Why<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Because its carbon is low (0.18\u20130.23 %), 8620 welds MORE EASILY than 4140 or 8740<\/b> \u2014 but that does not mean &#8220;without trouble&#8221;. The alloying raises hardenability, so <b>the HAZ turns to martensite if it cools fast<\/b>. <b>Preheat is mandatory.<\/b><\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Welding Parameters \u00b7 AISI 8620<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Preheat (un-carburized)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>175\u2013205 \u00b0C (350\u2013400 \u00b0F)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Preheat (carburized \/ hardened)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">raised to <b>\u2248260 \u00b0C (500 \u00b0F)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Maximum interpass temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>315 \u00b0C (600 \u00b0F)<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Covered electrode (SMAW)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>E9018-G<\/b> or <b>E9018-M<\/b> (AWS A5.5). Must be <b>low hydrogen<\/b> and <b>fully baked before use<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>TIG \/ MIG (GTAW \/ GMAW)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>ER90S-G<\/b> type wire<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Joining to carbon steel<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>E7018<\/b> is acceptable. And if E9018-G cracks, moving deliberately to a <b>softer<\/b> E7018 deposit is a published fix<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Post-weld heat treatment (PWHT)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>620\u2013650 \u00b0C (1150\u20131200 \u00b0F)<\/b>, <b>1 h per 25 mm<\/b> of thickness<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Cooling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">On carburized sections, cool the part <b>slowly under ceramic wool<\/b> after welding<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Hydrogen control<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Low-hydrogen consumables + dry surfaces + baked electrodes. <b>Hydrogen is the governing variable for delayed (cold) cracking<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The critical question: weld BEFORE or AFTER carburizing?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The answer is almost always &#8220;before&#8221;.<\/b> In order:<br \/><b>1. A carburized surface cannot be welded.<\/b> Surface carbon is <b>0.80\u20131.00 %<\/b>. At that carbon level the HAZ transforms to <b>very hard, very brittle<\/b> martensite and the weld cracks. The carbon equivalent jumps into <b>through-hardening steel territory<\/b>.<br \/><b>2. Welding heat destroys the case.<\/b> Welding takes the adjacent region far above the tempering temperature and <b>locally softens the case<\/b>. Your hardness map is no longer known.<br \/><b>3. The required PWHT kills the case.<\/b> PWHT runs at <b>620\u2013650 \u00b0C<\/b>, which is <b>far above<\/b> the case tempering temperature of 150\u2013190 \u00b0C. Do the PWHT and you lose most of the case hardness; skip it and you accept the cracking risk. <b>There is no way out of that dilemma.<\/b><br \/><b>The correct order:<\/b> weld \u2192 stress relieve \u2192 machine \u2192 carburize \u2192 quench \u2192 temper \u2192 grind. <b>If you are forced to weld in the hardened condition<\/b>: <b>grind the case off completely<\/b> in the weld zone, raise the preheat to <b>260 \u00b0C<\/b>, use a soft filler, cool slowly under ceramic wool, and <b>accept that the zone will no longer be hard<\/b>.<\/p>\n<h4 id=\"dm-b10\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Machining<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>8620 machines better than 4140 or 8740 thanks to its low carbon<\/b> \u2014 but that same low carbon creates the alloy&#8217;s <b>one machining problem<\/b>: <b>a tendency to built-up edge (BUE)<\/b>. A soft, ductile steel welds itself to the tool nose at low cutting speed and ruins the finish.<\/p>\n<div style=\"border:1px solid #d7dfe4;background:#ffffff;margin:24px 0 18px;position:relative;overflow:hidden;\">\n<div style=\"background:#DD3333;color:#ffffff;font-size:13px;font-weight:700;letter-spacing:.04em;text-transform:uppercase;padding:10px 12px;line-height:1.35;\">Machinability and Starting Cutting Parameters \u00b7 AISI 8620<\/div>\n<p><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<table style=\"border-collapse:collapse;width:100%;font-size:15px;line-height:1.5;\">\n<tbody>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Machinability index<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>65\u201366 %<\/b> (AISI 1212 = 100 %)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>ISO material group<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>P<\/b> \u2014 low-alloy steel<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Reference strength range<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>510\u2013710 N\/mm\u00b2<\/b> (annealed \/ normalized)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Turning<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>245\u2013335 m\/min<\/b> (800\u20131100 SFM)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Milling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>155\u2013205 m\/min<\/b> (510\u2013670 SFM)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Drilling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>100\u2013135 m\/min<\/b> (330\u2013440 SFM)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Parting<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>120\u2013160 m\/min<\/b> (390\u2013520 SFM)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Grooving<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>140\u2013185 m\/min<\/b> (460\u2013610 SFM)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Tooling \u2014 turning (stable conditions)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Hard substrate + CVD coating<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Tooling \u2014 low speed (&lt;150 m\/min)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Hard substrate + PVD coating<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>Tooling \u2014 milling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Semi-hard substrate + PVD coating<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>The golden rule<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>If the finish is poor, do not REDUCE the speed \u2014 INCREASE it.<\/b> Poor finish on 8620 is usually built-up edge; the cure is a sharp tool and higher speed. This is <b>the exact opposite<\/b> of the instinct that works on many alloy steels<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;background:#F7FAFB;\"><b>When to machine<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>In the normalized condition (149\u2013183 HB) and BEFORE carburizing.<\/b> After carburizing, a 58\u201362 HRC case <b>can only be ground<\/b><\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Resulphurised variant<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">For high-volume screw-machine work, <b>20NiCrMoS2-2 (1.6526)<\/b> improves chip breaking markedly \u2014 <b>at the cost of transverse ductility<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Planning the grinding stock \u2014 the step most often skipped.<\/b> Carburizing plus quenching <b>inevitably produces distortion<\/b>, so critical surfaces need grinding stock. <b>But that stock must not exceed half the case.<\/b> If you target a 1.0 mm effective case and leave 0.6 mm of grinding stock, you <b>grind away the hardest, highest-carbon layer<\/b> and what remains is no longer at the target hardness. <b>Write the case depth into the specification as a value to be measured AFTER grinding.<\/b><\/p>\n<h4 id=\"dm-b11\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Corrosion \u2014 the &#8220;NOT Stainless&#8221; Section<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>AISI 8620 is NOT stainless, and carburizing does not make it stainless.<\/b> It contains about <b>0.50 % chromium<\/b>. The threshold for a steel to behave <b>passively<\/b> \u2014 to build a self-repairing chromium oxide film \u2014 is <b>roughly 10.5 % chromium<\/b>. 8620 has about <b>one twentieth<\/b> of that. The chromium is there <b>for hardenability, not corrosion resistance<\/b>.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it does well<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>It does well in dry, closed systems running under an oil film.<\/b> Gearbox internals, sealed reducers, gears and bearing components in an oil bath \u2014 in all of these 8620 <b>causes no corrosion trouble at all<\/b>, because the surface is permanently wetted with oil. Much of the alloy&#8217;s industrial success comes from <b>exactly this environment<\/b>.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where it FAILS<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. Unprotected in the atmosphere.<\/b> Left unpainted, unplated and unoiled, an 8620 part <b>shows surface rust within days<\/b> \u2014 like plain carbon steel.<br \/><b>2. A carburized surface rusts FASTER.<\/b> Counter-intuitive but true: high-carbon martensite and its carbides are <b>galvanically more active<\/b> than low-carbon ferrite-pearlite. &#8220;We hardened it, so it is more durable&#8221; is <b>wrong<\/b>.<br \/><b>3. After grinding.<\/b> A freshly ground case surface is <b>stripped of protective oxide and may be micro-cracked<\/b>. Oil or passivate <b>immediately after grinding<\/b>; a ground gear left overnight on the bench <b>comes back with rust staining<\/b>.<br \/><b>4. Seawater, salt spray, road salt.<\/b> Not usable. Plating is mandatory (zinc, zinc-nickel, phosphate + oil, cadmium in aerospace).<br \/><b>5. Sour (H\u2082S) service.<\/b> Under <b>NACE MR0175 \/ ISO 15156<\/b>, the typical limit for carbon and low-alloy steels is <b>22 HRC<\/b>. <b>A carburized 8620 surface is 58\u201362 HRC<\/b> \u2014 far above it. <b>Carburized 8620 is not suitable for sour service.<\/b> This is almost never stated on datasheets and causes real failures in oilfield equipment.<br \/><b>6. Hydrogen from electroplating.<\/b> A carburized surface is <b>very hard and very high strength<\/b>, and therefore <b>susceptible<\/b> to hydrogen charged in during electroplating or acid pickling. <b>Post-plate baking must be a purchase requirement.<\/b><br \/><b>7. Oxidising acids, chloride-bearing aqueous media, food and pharmaceutical cleaning cycles.<\/b> Unusable in all of them.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">If you need corrosion resistance as well as a hard case<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>There are three routes, and none of them is 8620.<\/b> First, <b>nitriding<\/b> \u2014 it adds some corrosion resistance (especially nitrocarburizing + oxidation cycles) but the layer is shallow. Second, a <b>martensitic stainless<\/b> (440C, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/17-4ph-1-4542-aisi-630\/\">17-4 PH<\/a>): corrosion resistance and hardness together, at a cost in fracture toughness and price. Third, <b>stainless carburizing grades<\/b> (e.g. high-nickel aerospace gear steels): expensive and long lead time. <b>The fourth &#8220;route&#8221; \u2014 plate 8620 and manage it \u2014 is often the cheapest<\/b>, but decide on the basis of plating life and hydrogen risk, not first cost.<\/p>\n<h4 id=\"dm-b12\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Frequently Asked Questions<\/h4>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The datasheet says &#8220;8620 hardness 58\u201362 HRC&#8221; but the bar we received measured 180 HB. Did we get the wrong material?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Most likely the material is right and the datasheet is wrong \u2014 or at least badly written.<\/b><br \/><b>To be clear:<\/b> the as-delivered hardness of 8620 bar is typically <b>149\u2013212 HB<\/b>, depending on whether it is annealed, normalized or as-rolled. <b>180 HB is entirely normal<\/b> and is <b>exactly what a normalized 8620 is expected to be<\/b> (the published typical value is <b>183 HB<\/b>).<br \/><b>58\u201362 HRC is NOT a delivery condition; it is a PROCESS RESULT.<\/b> To reach it, the part must be <b>held for hours at 900\u2013955 \u00b0C in a carbon-donating atmosphere<\/b>, then oil quenched and tempered \u2014 that is, <b>carbon has to be loaded into the surface afterwards<\/b>. The steel&#8217;s own carbon is <b>0.20 %<\/b>, and <b>58 HRC is physically impossible<\/b> with it.<br \/><b>The confusion is so common<\/b> that many distributor pages publish the line &#8220;Hardness: 58\u201362 HRC&#8221; <b>with no qualification at all<\/b>. The result: the buyer expects hard bar, receives soft bar, and a return process begins.<br \/><b>What to do:<\/b> write two things separately on the order \u2014 <b>(a)<\/b> the delivery condition and hardness band of the bar, and <b>(b)<\/b> if carburizing is to follow, the target effective case depth, surface hardness and core hardness. <b>They cannot go on the same line because they are not the same thing.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Our gears come out in tolerance after carburizing but seize in the field within months. What causes that?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Your first suspect should be RETAINED AUSTENITE. What you describe is its classic signature.<\/b><br \/><b>The mechanism:<\/b> in the carburized surface, carbon rises to 0.80\u20131.00 % and that carbon drives the martensite start temperature (Ms) <b>to or below room temperature<\/b>. Because the oil quench stops at room temperature, <b>the transformation does not complete<\/b> and some austenite remains in the case. In service, <b>stress, cold and time<\/b> gradually convert it to martensite \u2014 and <b>martensite occupies more volume than austenite<\/b>. So <b>the part GROWS OVER TIME<\/b>. Backlash closes, bearing clearance shrinks, the part seizes.<br \/><b>Why your inspection does not catch it:<\/b> the part is in tolerance when it leaves the factory. The transformation takes months. <b>Hardness testing will not show it either<\/b> \u2014 in fact hardness creeps slightly <b>upward<\/b>.<br \/><b>Confirmation:<\/b> <b>measure retained austenite by X-ray diffraction<\/b> (ASTM E975). Test one failed part and one new part. High in the new part and low in the returned one and <b>the diagnosis is certain<\/b>.<br \/><b>The fix has three steps.<\/b> <b>First and most effective: add a cryogenic step<\/b> \u2014 <b>immediately after the quench, BEFORE tempering<\/b>, in the <b>\u221268 to \u221279 \u00b0C<\/b> band. The sequence matters: tempering <b>stabilises<\/b> retained austenite, and freezing afterwards achieves much less. <b>Second: lower the surface carbon<\/b> \u2014 pull the carbon potential back from 1.1 % to the 0.85\u20130.90 % band; the higher the surface carbon, the more retained austenite. <b>Third: move from direct quenching to reheat quenching<\/b> \u2014 finer grain, less retained austenite. <b>And write a ceiling into your specification<\/b> (typically 15\u201320 % by volume), together with the measurement method.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">We carburized a heavy shaft; the case is hard but the teeth collapsed under load. Is the case too thin?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Most likely the case is fine and the CORE is inadequate. This is 8620&#8217;s most typical application error.<\/b><br \/><b>The physics:<\/b> a hard case carries load only if <b>there is a hard foundation beneath it to support it<\/b>. If the core did not harden, the case <b>collapses like an eggshell<\/b> \u2014 no matter how hard the case itself is.<br \/><b>And 8620 is a shallow-hardening steel.<\/b> Look at the Jominy band: at <b>11 mm<\/b> from the quenched end the standard +H band has fallen to <b>20\u201333 HRC<\/b>. The centre of a heavy oil-quenched bar cools even more slowly than that. In heavy sections the core stays <b>ferritic-bainitic<\/b> and <b>has no load-carrying capacity<\/b>.<br \/><b>The numerical check:<\/b> in EN practice the minimum core Rm after case hardening is <b>1100 MPa at \u2300\u226416 mm<\/b>, <b>800 MPa at \u230016\u201340 mm<\/b> and <b>700 MPa at \u230040\u2013100 mm<\/b>. The same steel loses <b>a third of its core strength<\/b> when the section quadruples. Which number was your design based on?<br \/><b>The fix, in order:<\/b> <b>(1)<\/b> Buy a restricted-hardenability grade \u2014 <b>+HH<\/b> (or <b>8620RH<\/b> on the US side). That guarantees the upper half of the band and is essentially a free gain. <b>(2)<\/b> If that is not enough, <b>move to AISI 4320<\/b>: same carbon, but nickel at <b>1.65\u20132.00 %<\/b> hardens markedly deeper. <b>(3)<\/b> Still not enough \u2014 <b>18CrNiMo7-6<\/b> in Europe, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-9310\/\">AISI 9310<\/a> in aerospace. <b>(4)<\/b> Increase quench severity (more agitation, faster oil) \u2014 but know that <b>distortion and cracking risk rise with it<\/b>.<br \/><b>Making the case thicker does NOT fix this<\/b>, and can make it worse: a thicker case means more retained austenite and more distortion.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">A customer wants &#8220;carburized 8620, 60 HRC, NACE compliant&#8221;. Can we supply it?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>No. That specification contradicts itself and should be rejected.<\/b><br \/><b>NACE MR0175 \/ ISO 15156-2<\/b> typically imposes a <b>22 HRC maximum<\/b> and a <b>quenched-and-tempered<\/b> condition on carbon and low-alloy steels in sour (H\u2082S) service. The reason is <b>sulphide stress cracking (SSC)<\/b>: hard martensite, charged with hydrogen in an H\u2082S environment, <b>cracks without warning under stress<\/b>.<br \/><b>A carburized 8620 surface is 58\u201362 HRC<\/b> \u2014 nearly <b>three times<\/b> the limit. And that hardness is <b>exactly at the outer surface<\/b>, the part in contact with the environment. <b>These two requirements cannot be met on the same part.<\/b><br \/><b>The NACE limit is also LOCAL, not an average.<\/b> &#8220;The core is 30 HRC, so the average is acceptable&#8221; is not a defence: weld metal, HAZ, rolled thread roots and the carburized surface must <b>each individually<\/b> sit below the limit.<br \/><b>The honest answer to the customer has three options.<\/b> <b>(1)<\/b> If sour service is real: <b>drop the carburizing<\/b> and use a steel quenched and tempered below 22 HRC (the logic of <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/\">4140<\/a> \/ A193 B7M) \u2014 and obtain wear resistance <b>by another route<\/b>. <b>(2)<\/b> If wear resistance is non-negotiable: <b>isolate the hard surface from the environment<\/b> (closed oil-filled system, coating, sleeve) and describe that in writing. <b>(3)<\/b> If both are genuinely required: <b>the material class has to change<\/b> \u2014 nickel-base alloys or purpose-built duplex\/stainless solutions. <b>Under no circumstances issue a written statement that a carburized part is NACE compliant.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">We hold bar certified to 20NiCrMo2-2 and the customer wants SAE 8620. Can we ship it?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Not without reading the certificate line by line \u2014 and the trap here is DIFFERENT from the 4140\/42CrMo4 case.<\/b><br \/><b>On chemistry, the EN band is WIDER than the SAE band.<\/b> On manganese, EN asks for <b>0.65\u20130.95 %<\/b> and SAE for <b>0.70\u20130.90 %<\/b>. On chromium, EN <b>0.35\u20130.70 %<\/b> and SAE <b>0.40\u20130.60 %<\/b>. So <b>not every heat that meets EN meets SAE 8620<\/b>: a European heat at Mn = 0.93 % or Cr = 0.66 % <b>satisfies EN 10084 perfectly but falls outside the SAE 8620 band<\/b>. (Interestingly it does largely fit the <b>8620H<\/b> band \u2014 Mn 0.60\u20130.95 %, Cr 0.35\u20130.65 %.)<br \/><b>In the other direction, EN demands a CLEANER steel:<\/b> P \u22640.025 % (SAE \u22640.035 %) and, crucially, <b>Al 0.020\u20130.050 % is mandatory<\/b>. So <b>a US heat certified to SAE 8620 cannot claim EN 10084 compliance if the aluminium line is blank<\/b>. And that line is not decorative: in a steel held for hours at carburizing temperature, <b>AlN precipitation is the principal brake on grain growth<\/b>.<br \/><b>What to do:<\/b> compare the <b>Mn, Cr, P and Al<\/b> lines of the mill certificate against the target bands <b>one by one<\/b>. If they all fit, a dual certificate can be issued \u2014 and many mills deliberately produce <b>narrow heats that satisfy both bands<\/b>. <b>But that is a choice, not a rule.<\/b> If they do not fit, <b>supply the customer material to the specification they asked for<\/b>; &#8220;same steel&#8221; is not a defensible sentence in a third-party audit.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Common datasheet errors \u2014 check these before you order<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. &#8220;8620 hardness: 58\u201362 HRC&#8221; \u2014 THE MOST COMMON ERROR.<\/b> That is the hardness of the <b>carburized case, not the steel<\/b>. As-delivered 8620 bar is <b>149\u2013212 HB<\/b>. <b>58 HRC is physically impossible at 0.20 % carbon.<\/b><br \/><b>2. Case hardness quoted as if it were core hardness.<\/b> A carburized part has <b>two hardnesses<\/b>: surface <b>58\u201362 HRC<\/b>, core <b>25\u201340 HRC<\/b>. Any line that does not say which one will be measured generates a dispute.<br \/><b>3. Case depth quoted with no definition.<\/b> <b>Effective<\/b> (to 50 HRC) and <b>total<\/b> (to the core structure) differ by <b>1.5\u20132\u00d7<\/b>. &#8220;0.8 mm case&#8221; \u2014 by which definition?<br \/><b>4. Time-versus-depth tables conflict.<\/b> One source gives <b>18 h<\/b> for 1.5 mm at 925 \u00b0C, another <b>16 h<\/b>; one gives <b>4 h<\/b> for 0.75 mm while another gives <b>2 h<\/b> for 0.5 mm. The difference comes from <b>how the boost\/diffusion cycle is built<\/b>. <b>Make none of them an acceptance criterion.<\/b><br \/><b>5. Values like &#8220;Rc 90&#8221; get published \u2014 A UNIT ERROR.<\/b> The Rockwell C scale <b>does not go above about 70<\/b>. That number is almost certainly <b>HR15N<\/b>. The same pages print thermal conductivity as <b>&#8220;26&#8221;<\/b> and modulus as <b>&#8220;31&#8221;<\/b> with <b>no units at all<\/b> (Btu and 10\u2076 psi).<br \/><b>6. Retained austenite is never mentioned.<\/b> It is the most common cause of dimensional instability and <b>no base specification sets a ceiling<\/b>. <b>You have to write one.<\/b><br \/><b>7. The SEQUENCE of the cryogenic step is described wrongly.<\/b> The correct order is <b>quench \u2192 cryogenic \u2192 temper<\/b>. Freezing after tempering is <b>far less effective<\/b>, because tempering stabilises the austenite.<br \/><b>8. A single &#8220;core strength&#8221; number is published.<\/b> The same steel has a minimum core Rm of <b>1100 MPa at \u230016 mm and 700 MPa at \u2300100 mm<\/b>. <b>Any value quoted without a section size is meaningless.<\/b><br \/><b>9. Jominy values are given as single numbers.<\/b> The EN +H band at 7 mm is <b>25\u201342 HRC<\/b> \u2014 a <b>17 HRC spread<\/b>, both ends compliant. The batch-to-batch scatter you see is <b>scatter the standard permits<\/b>. The cure: order <b>+HH \/ +HL or 8620RH<\/b>.<br \/><b>10. &#8220;8620 = 20NiCrMo2-2&#8221; \u2014 INCOMPLETE.<\/b> The EN band is <b>wider<\/b> on Mn and Cr, but <b>tighter<\/b> on P, and <b>Al 0.020\u20130.050 % is MANDATORY<\/b>. EN compliance cannot be claimed from a certificate with a blank aluminium line.<br \/><b>11. Nobody questions why annealed yield exceeds normalized yield.<\/b> The published data give <b>385 MPa<\/b> annealed against <b>357\u2013360 MPa<\/b> normalized. That inconsistency comes from different specimen diameters and yield definitions; <b>neither is a design value<\/b>.<br \/><b>12. AMS 6274, 6276 and 6277 are used interchangeably.<\/b> The difference is <b>melting practice<\/b>: 6274 vacuum degassed (VD), 6276 <b>CEVM\/VAR<\/b>, 6277 <b>CEM<\/b>. And 6276\/6277 tighten the chemistry to <b>P \u22640.012 %, S \u22640.010 %<\/b>. <b>Get the number right on aerospace orders.<\/b><br \/><b>13. &#8220;Carburizing makes 8620 corrosion resistant&#8221; \u2014 WRONG, AND THE OPPOSITE IS TRUE.<\/b> High-carbon martensite is <b>more active<\/b> and rusts <b>faster<\/b> than the low-carbon structure.<br \/><b>14. NACE compliance is claimed for carburized parts.<\/b> The limit is <b>22 HRC<\/b>; a carburized surface is <b>58\u201362 HRC<\/b>. <b>It cannot be met.<\/b><br \/><b>15. Welding AFTER carburizing is recommended.<\/b> Surface carbon is 0.80\u20131.00 %; the HAZ cracks. And the required PWHT (<b>620\u2013650 \u00b0C<\/b>) is <b>far above<\/b> the case tempering temperature and destroys the case. <b>Correct order: weld FIRST.<\/b><br \/><b>16. Grinding stock is planned independently of case depth.<\/b> If the stock exceeds <b>half the case<\/b>, you grind off the hardest layer. <b>Specify case depth as measured AFTER grinding.<\/b><br \/><b>17. &#8220;Poor finish \u2014 slow down&#8221; \u2014 BACKWARDS on 8620.<\/b> Poor finish is usually <b>built-up edge<\/b>; the cure is a sharp tool and a <b>HIGHER<\/b> speed.<br \/><b>18. 8620 is compared with 4140\/8740 on the &#8220;hardness&#8221; axis.<\/b> 8620 is a <b>carburizing steel<\/b> (0.18\u20130.23 % C); the others are <b>through-hardening steels<\/b> (0.38\u20130.43 % C). <b>They answer different questions.<\/b><br \/><b>19. Thermal expansion is given as a single number.<\/b> It runs from <b>10.5 \u00d710\u207b\u2076 \/K (\u2212100 \u00b0C)<\/b> to <b>14.4 \u00d710\u207b\u2076 \/K (600 \u00b0C)<\/b>. A single figure produces errors in shrink-fit calculations. Likewise modulus falls from <b>212 GPa to 164 GPa<\/b>.<br \/><b>20. &#8220;8620 was made for carburizing, so it suits every carburizing job&#8221; \u2014 INCOMPLETE.<\/b> 8620 <b>hardens shallow<\/b>. Large-module gears, heavy sections and low-temperature impact call for <b>4320, 18CrNiMo7-6 or 9310<\/b>.<br \/><b>21. The normalizing step is skipped.<\/b> An 8620 that was not normalized before machining <b>distorts unpredictably<\/b> after carburizing. That step is not a cost, it is insurance.<br \/><b>22. Resulphurised 20NiCrMoS2-2 is offered in place of 20NiCrMo2-2.<\/b> Sulphur improves machinability but <b>reduces transverse ductility and impact toughness<\/b>.<\/p>\n<p><!-- dm-diy-isil --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">HEAT TREATMENT \u2014 SCHEMATIC<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">1 \u00b7 HOT WORKING \/ FORGING<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1 \u00b7 HOT WORKING \/ FORGING<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Not a heat treatment but a precondition: the finish forging temperature and the cooling that follows determine whether normalizing is needed.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1100-850 C (Saarstahl). Ellwood gives the same operation in Fahrenheit as running down from 2200 F to 1800 F (about 1205-982 C); THE UPPER LIMIT DIVERGES between these two sources and NO AVERAGE HAS BEEN TAKEN.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Until the whole section is at temperature. No numerical time was found in four independent sources, so none is stated.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Not forged below 850 C. After forging, slow cooling, or transfer to a furnace near the finishing temperature followed by air cooling.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Hardness after forging depends on section and cooling rate; no binding hardness is stated for this stage.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">2 \u00b7 NORMALIZING<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">2 \u00b7 NORMALIZING<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Refines the grain and evens out the structure after forging or rolling. Recommended before carburizing: because carburizing is long and hot, the uniformity of the entering structure governs the uniformity of the case.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">850-900 C. Saarstahl 850-880 C \u00b7 Ovako 860-890 C \u00b7 Virgamet 860-900 C \u00b7 Lucefin 880-900 C.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Until the whole section is at temperature. The same numerical time could not be verified in four independent sources, so no binding time is stated.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">AIR cooling (Saarstahl, Ovako, Lucefin, Virgamet &#8211; four sources agree).<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Normalized hardness depends on section; no single figure could be verified in four independent sources, so none is stated.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">3 \u00b7 SOFT ANNEALING (for machinability)<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">3 \u00b7 SOFT ANNEALING (for machinability)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Carried out BELOW the critical temperature to lower hardness before machining. It is not part of the carburizing cycle.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">650-700 C. Saarstahl 650-700 C \u00b7 Virgamet 650-700 C \u00b7 Lucefin 700 C \u00b7 Ovako 600-670 C (2 hours).<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Ovako gives 2 hours. The same numerical time could not be verified in four independent sources, so no binding time is stated.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">SLOW FURNACE COOLING. Saarstahl says furnace cool; Lucefin gives furnace cooling from 700 C to 600 C and then air; Ovako also accepts air cooling.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">In the soft-annealed (+A) condition, 212 HBW MAXIMUM. This ceiling is the same in the BS EN 10084:2008 text, in Saarstahl and in Rodacciai. Saarstahl additionally gives 161-212 HB for the cold-shearable delivery condition (+S) and 212 HB maximum as rolled. Virgamet gives 229 HB maximum for the annealed condition; THIS VALUE DIVERGES and has been recorded.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">4 \u00b7 CARBURIZING (CASE CARBON DIFFUSION)<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">4 \u00b7 CARBURIZING (CASE CARBON DIFFUSION)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">THE CASE IS FORMED HERE. The part is held in a carbon-donating atmosphere and the surface carbon rises to roughly 0.7-0.9%. Case depth is a function of time and temperature and MUST BE STATED SEPARATELY ON THE ORDER.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">880-980 C. This band is IDENTICAL in the heat-treatment annex of BS EN 10084:2008, in Saarstahl, in Rodacciai and in Lucefin (four sources). DIVERGING SOURCES: Virgamet 880-950 C \u00b7 Ovako 850-930 C. NO AVERAGE HAS BEEN TAKEN.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Hours, depending on the case depth required. No numerical time-versus-depth table was found in four independent sources, so no time is stated. In aerospace work the cycle is tied to AMS 2759\/7.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Two routes follow carburizing: (a) DIRECT QUENCHING &#8211; the part goes straight from the carburizing temperature into oil; (b) SLOW COOL AND REHARDEN &#8211; the part is cooled slowly to room temperature and then requenched from the temperature given in stage 5 or 6. Ellwood specifies oil quenching for thin sections and furnace cooling for heavy sections.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">At the end of this stage the part IS NOT YET HARD; only the surface carbon has been raised. Hardness appears at the quenching stage.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">5 \u00b7 CORE HARDENING (quench from the higher temperature)<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">5 \u00b7 CORE HARDENING (quench from the higher temperature)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">The stage that sets core strength. The carburized part is heated above the critical temperature of the core and quenched. This route is chosen where core strength rather than core toughness is to be favoured.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">860-900 C. This band is IDENTICAL in the BS EN 10084:2008 annex, in Saarstahl, in Rodacciai, in Lucefin and in Virgamet (five sources).<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Until the whole section is at temperature. No numerical time could be verified in four independent sources, so none is stated.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">OIL. Saarstahl and Rodacciai also list WATER for heavy sections; Lucefin gives oil-polymer solution or a salt bath. Water quenching raises the risk of cracking and distortion.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Core: Lucefin gives 354-438 HB at 11 mm diameter and 249-339 HB at 30 mm. The case hardens at this stage as well.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">6 \u00b7 CASE HARDENING (quench from the lower temperature) + TEMPERING<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Step<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6 \u00b7 CASE HARDENING (quench from the lower temperature) + TEMPERING<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Summary<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Refines the grain of the case. The quench is made from a LOWER temperature than core hardening; the aim is case toughness. Tempering after quenching is MANDATORY and is carried out at LOW temperature &#8211; completely unlike the 540-680 C tempering band of quench-and-temper steels.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Temperature<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">CASE HARDENING: 780-820 C. This band is the same in the BS EN 10084:2008 annex, in Saarstahl and in Rodacciai. DIVERGING SOURCES: Virgamet 810-830 C \u00b7 Ovako 780-830 C for the carburized part. TEMPERING: 150-200 C. This band is IDENTICAL in the BS EN 10084:2008 annex, in Saarstahl, in Rodacciai, in Lucefin and in Virgamet (five sources). DIVERGING SOURCE: Ovako 160-250 C. Saarstahl additionally gives a 630-650 C intermediate anneal between the two quenches.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Time<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">At least one hour at temperature is common practice for tempering; no numerical time could be verified in four independent sources, so no binding time is stated.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Cooling<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Oil for case hardening (Saarstahl and Rodacciai also list water). Air cooling after tempering.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Resulting hardness<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">CASE: in the Lucefin measured curve, 64 HRC at 0.25 mm depth, 63.5 HRC at 0.30 mm, 62 HRC at 0.40 mm, 60.5 HRC at 0.50 mm, 59 HRC at 0.60 mm and 57.5 HRC at 0.65 mm. CORE: 354-438 HB at 11 mm diameter, 249-339 HB at 30 mm (Lucefin).<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">The diagram is SCHEMATIC; the time axis is NOT TO SCALE. No TTT\/CCT curve published in four independent sources was used, so no curve is drawn. THIS ALLOY IS A CARBURIZING (CASE-HARDENING) STEEL: it gains its hardness through carburizing, quenching and LOW-temperature tempering. IT DOES NOT PRECIPITATION HARDEN; there is no H900 \/ H1025 \/ H1150 type AGEING STEP. The six stages below were each verified separately, and the core of the temperature values comes from the heat-treatment annex of BS EN 10084:2008. The core of the temperatures is taken directly from the heat-treatment annex of the BS EN 10084:2008 standard text; the producer data sheets (Saarstahl, Rodacciai, Lucefin, Ovako, Virgamet) confirm these bands independently. STAGES 5 AND 6 ARE ALTERNATIVES; BOTH ARE NOT MANDATORY. For single hardening, either the core or the case temperature is chosen; for double hardening, 860-900 C is applied first and 780-820 C second, with an optional 630-650 C intermediate anneal in between (Saarstahl). THE TEMPERING TEMPERATURE IS 150-200 C AND MUST NOT BE CONFUSED WITH THE BAND USED FOR QUENCH-AND-TEMPER STEELS. The 540-680 C band quoted for 4140 or 8740 DOES NOT APPLY to this steel; at that temperature the case softens completely. Case depth is not given as a number in this diagram: depth is a function of carburizing time and is stated separately on the order. In aerospace work the cycle is tied to AMS 2759\/7. Times are not stated: the same numerical time could not be verified across four independent sources. THE CASE AND THE CORE ARE MEASURED SEPARATELY AND SPECIFIED SEPARATELY. CASE: in the Lucefin measured curve, 64 HRC at 0.25 mm depth, 60.5 HRC at 0.50 mm and 57.5 HRC at 0.65 mm. CORE: Lucefin gives 354-438 HB at 11 mm diameter and 249-339 HB at 30 mm; in the Saarstahl EN 10084 table the core tensile strength is at least 1100 N\/mm2 up to 16 mm, at least 800 N\/mm2 from 16 to 40 mm and at least 700 N\/mm2 from 40 to 100 mm. These two lines are taken from two different places in the same part and neither can stand in for the other. NO TEMPER-EMBRITTLEMENT FORBIDDEN BAND IS STATED FOR 8620. Carburizing tempering is at 150-200 C, entirely below the classical embrittlement bands (Total Materia: irreversible 250-400 C, reversible 450-650 C; Thermal Processing: 375-575 C), so a normal cycle never enters them. No band specific to 8620 could be verified across four independent sources, so none is stated. Practical rule: a carburized part is not tempered above 200 C and is not put into service above 200 C.<\/div>\n<\/div>\n<p><!-- \/dm-diy-isil --><!-- dm-diy-kars --><\/p>\n<div style=\"border:1px solid #e3e9ec;margin:22px 0 26px;background:#fff;position:relative;overflow:hidden;\">\n<div style=\"background:#12303f;color:#fff;padding:9px 14px;font-size:14px;font-weight:700;letter-spacing:.3px;position:relative;z-index:2;\">COMPARISON<\/div>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"padding:10px 14px 0;font-size:12.5px;color:#5b7180;line-height:1.7;\">TWO CRITERIA, EACH READ FROM A SINGLE SOURCE FAMILY. (1) NICKEL AND CARBON: all three bands are taken from the same place, the bar producers&#8217; handbooks that reprint the SAE J404 \/ ASTM A29 chemistry (Steel Dynamics Bar Data Handbook, TimkenSteel Practical Data for Metallurgists), so the nickel difference is compared under one specification logic. (2) DEPTH OF HARDENING: for each grade a SPECIFICATION or PRODUCER table is used that shows, within that grade&#8217;s own heat-treatment logic, what remains in the core as the section grows. Hardness and tensile figures collected from different sources are NOT placed side by side; every row states where its number comes from. 8740 DOES NOT SHARE THE HEAT-TREATMENT LOGIC of the other two, and this table deliberately shows it under a separate logic.<\/div>\n<div style=\"padding:12px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"overflow-x:auto;position:relative;z-index:2;\">\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;min-width:430px;background:transparent;\">\n<tr>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Grade<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">UNS<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">W.-Nr.<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Alloy type<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Carbon<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Nickel<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Chromium<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Molybdenum<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Hardenability<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Resulting hardness<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">AMS coverage<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Typical use<\/th>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">AISI 8620<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">G86200 (hardenability-band grade 8620H = H86200)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1.6523 \u00b7 EN 10084 20NiCrMo2-2 (former DIN name 21NiCrMo2) &#8211; close equivalent, bands not identical<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">CARBURIZING (case hardening). Low-carbon core plus a carbon-enriched hard case.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.18-0.23%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.40-0.70% (nominal 0.55% in the AMS titles)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.40-0.60% (AMS nominal 0.50%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.15-0.25% (AMS nominal 0.20%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">SHALLOW. In the EN 10084 core table as printed by Saarstahl the requirement falls quickly with section: at least 1100 N\/mm2 tensile up to 16 mm diameter, at least 800 N\/mm2 from 16 to 40 mm, at least 700 N\/mm2 from 40 to 100 mm. The Jominy end-quench curve runs from 41-49 HRC at 1.5 mm down to roughly 20-24 HRC at 40 mm (Rodacciai, Lucefin and Ovako all print the 8620H band).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Case: in the Lucefin measured curve 64 HRC at 0.25 mm depth and 57.5 HRC at 0.65 mm. Core: Lucefin gives 354-438 HB for 11 mm diameter and 249-339 HB for 30 mm.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6274 (bars, forgings, mechanical tubing, forging stock; aircraft quality) \u00b7 6276 (same forms; VAR) \u00b7 6277 (same forms; VAR or ESR) \u00b7 6375 (welding wire; vacuum melted).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">General industrial gears, ring and pinion sets, shafts, pins and bushings, chain parts, hydraulic pump bodies, plastic moulds.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;\">AISI 9310<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">G93100 (G93106 for vacuum-remelted product)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">NO W.Nr. EQUIVALENT VERIFIED ACROSS FOUR SOURCES. Two independent international cross-reference tables contain no row for 9310 at all. The widely quoted 1.6657 \/ 14NiCrMo13-4 match does not hold chemically; see the contradictions list.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">CARBURIZING (case hardening). Low-carbon but HIGH-NICKEL core plus a carbon-enriched hard case.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.07-0.13%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">3.00-3.50% (nominal 3.25% in the AMS titles)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1.00-1.40% (AMS nominal 1.2%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.08-0.15% (AMS nominal 0.12%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">DEEP. Although its carbon is about half that of 8620, its core hardness is far higher: Carpenter gives 331-363 HBW in the core of the carburized part, NASA measured 38 HRC in the core of carburized 9310 spur gears and a second NASA report gives a nominal 40 HRC. This is the effect of NICKEL, not of carbon.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Case: 60-62 HRC (Carpenter); 60 HRC with a 0.97 mm (0.038 in.) case on the NASA test gears and a nominal 58 HRC in the second NASA report. Core: 331-363 HBW (Carpenter) \u00b7 38-40 HRC (NASA).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">6260 (bars, forgings, tubing; air melting accepted) \u00b7 6265 (same forms; VACUUM CONSUMABLE ELECTRODE REMELTING &#8211; VAR REQUIRED) \u00b7 6267 (same forms; ESR OR VAR REQUIRED). Cleanliness is called out through AMS 2300 \/ 2301 \/ 2304.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Aircraft and helicopter engine gears and pinions, transmission gears, heavy-duty shafts, clutch parts, piston pins.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;\">AISI 8740<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">G87400<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1.6546 \u00b7 40NiCrMo2-2 (cross-reference tables give DIN name 40NiCrMo22, UNI 40NiCrMo2, JIS SNCM240) &#8211; found in three sources, band not verified element by element<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">QUENCH AND TEMPER. NOT A CARBURIZING STEEL; its carbon is too high for case hardening.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.38-0.43%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.40-0.70% (nominal 0.55% in the AMS titles)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.40-0.60% (AMS nominal 0.50%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.20-0.30% (AMS nominal 0.25%)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">INTERMEDIATE. In the ASTM A320 table Grade L7C is guaranteed at 125 ksi (860 MPa) tensile and 105 ksi (725 MPa) yield for diameters of 65 mm (2 1\/2 in.) and under, while in the same standard the 4340-based Grade L43 carries the same band up to 100 mm (4 in.). The section-strength figure is read from these two rows; no second independent diameter table was found.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">THERE IS NO CASE-CORE DISTINCTION. One structure is aimed at through the section. The ASTM A320 L7C hardness CEILING is 321 HBW \/ 35 HRC.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6322 (bars, forgings, rings and stock for forging or flash-welded rings; aircraft quality) \u00b7 6323 (mechanical tubing) \u00b7 6325 (bars and forgings; heat treated to 105 ksi \/ 724 MPa tensile) \u00b7 6327 (bars and forgings; heat treated to 125 ksi \/ 862 MPa tensile) \u00b7 6358 (sheet, strip and plate; aircraft quality). THERE IS NO AMS NUMBER CARRYING A REMELTING (VAR \/ ESR) REQUIREMENT.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Aircraft engine bolts and fasteners, axles, drill tool joints, drill and reamer bodies, piston rods, ASTM A320 Grade L7C low-temperature bolting.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<div style=\"padding:10px 12px 2px;position:relative;overflow:hidden;\"><span aria-hidden=\"true\" data-dmwm=\"1\" style=\"position:absolute;top:50%;left:50%;transform:translate(-50%,-50%) rotate(-18deg);font-size:72px;font-weight:800;letter-spacing:.12em;color:#12303f;opacity:.05;white-space:nowrap;pointer-events:none;user-select:none;z-index:3;\">DEFENCE METAL<\/span><\/p>\n<div style=\"position:relative;z-index:2;\">\n<div style=\"font-size:13.5px;font-weight:700;color:#12303f;margin:6px 0 6px;\">Additional information<\/div>\n<table style=\"width:100%;border-collapse:collapse;font-size:13.5px;background:transparent;\">\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Nickel difference<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">THE DECIDING DIFFERENCE IS NICKEL. In 8620 and 8740 nickel sits in the 0.40-0.70% band; in 9310 it is 3.00-3.50%, roughly SIX TIMES as much. Nickel forms no carbide; it strengthens the ferrite in solid solution and lowers the transformation temperature of austenite, so martensite and bainite still form in slowly cooling heavy sections. The practical consequence is this: 9310 has the LOWEST CARBON OF THE THREE (0.07-0.13%) and still holds 331-363 HBW (about 35-39 HRC) in the CORE of the carburized part, while 8620 at 30 mm diameter sits in the 249-339 HB band. THE DIFFERENCE IS NOT IN SURFACE HARDNESS: both carburizing grades reach a case of roughly 58-62 HRC, because case hardness is set by the carbon DIFFUSED IN DURING CARBURIZING, not by the steel&#8217;s own carbon. The difference is how deep into the section the core that carries that hard case stays strong.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">AMS difference<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">THE SECOND DIFFERENCE THAT DECIDES AN ORDER IS THE MELTING REQUIREMENT. For 9310, AMS 6265 REQUIRES VACUUM CONSUMABLE ELECTRODE REMELTING (VAR) and AMS 6267 permits ESR or VAR, while AMS 6260 accepts air melting. On the 8620 side remelted numbers also EXIST: AMS 6276 (VAR) and AMS 6277 (VAR or ESR). For 8740 THERE IS NO AMS NUMBER WITH A REMELTING REQUIREMENT; the highest level is the &#8216;aircraft quality&#8217; wording of AMS 6322, and that is NOT a remelting requirement. A specification calling for remelted material cannot be met with 8740.<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);font-weight:700;color:#12303f;width:34%;vertical-align:top;\">Ortak sinir<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">NONE OF THE THREE IS STAINLESS. Chromium runs from 0.40 to 1.40% and no passive layer forms; protection comes from plating, phosphating, oil or paint. All three are low-alloy steels, so post-plating hydrogen relief baking and the risk of hydrogen embrittlement at high hardness apply to all three. Choosing between the grades does not solve a corrosion problem.<\/td>\n<\/tr>\n<\/table>\n<\/div>\n<\/div>\n<\/div>\n<div style=\"padding:6px 14px 12px;font-size:12px;color:#5b7180;line-height:1.7;border-top:1px solid #f0f3f5;position:relative;z-index:2;\">The table is built WITHOUT INVENTED NUMBERS: every hardenability row states which table its figure was read from, and hardness values from different sources are not equated with one another. 8740 IS NOT SHOWN AS A CARBURIZING GRADE here. Its carbon is 0.38-0.43%; carburizing it would over-carburize the surface and leave no toughness, because the core is already hard. 8740 is quenched and tempered. The effect of nickel is not &#8216;harder&#8217; but &#8216;hard deeper&#8217;. The case hardness of the two carburizing grades is of the same order; the two grades separate in the core. 9310 and 8620 have AMS numbers carrying a remelting requirement; 8740 does not. In an aerospace order this is the most concrete discriminator between the grades. This is a comparative summary. For all three grades the order must be tied to the AMS or ASTM number that matches the product form.<\/div>\n<\/div>\n<p><!-- \/dm-diy-kars --><\/p>\n<p><!-- \/dm-zengin --><\/p>\n<p><!-- dm-ld --><script type=\"application\/ld+json\">{\"@context\":\"https:\/\/schema.org\",\"@type\":\"WebPage\",\"name\":\"AISI 8620\",\"url\":\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8620\/\",\"inLanguage\":\"en\",\"description\":\"AISI\/SAE 8620 (UNS G86200 \/ W.Nr. 1.6523 \/ EN 20NiCrMo2-2 \/ former DIN designation 21NiCrMo2 \/ BS 805M20 \/ AFNOR 20NCD2 \/ JIS SNCM220) is a low-carbon, triple-alloyed (Ni-Cr-Mo) CASE-HARDENING \u2014 that is, carburizing \u2014 steel.\",\"isPartOf\":{\"@type\":\"WebSite\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"publisher\":{\"@type\":\"Organization\",\"name\":\"Defence Metal\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"mainEntity\":{\"@type\":\"DefinedTerm\",\"name\":\"AISI 8620\",\"description\":\"AISI\/SAE 8620 (UNS G86200 \/ W.Nr. 1.6523 \/ EN 20NiCrMo2-2 \/ former DIN designation 21NiCrMo2 \/ BS 805M20 \/ AFNOR 20NCD2 \/ JIS SNCM220) is a low-carbon, triple-alloyed (Ni-Cr-Mo) CASE-HARDENING \u2014 that is, carburizing \u2014 steel.\",\"inDefinedTermSet\":{\"@type\":\"DefinedTermSet\",\"name\":\"Defence Metal - metals and alloys\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"alternateName\":[\"UNS G86200\",\"W.Nr. 1.6523\"],\"identifier\":[{\"@type\":\"PropertyValue\",\"propertyID\":\"UNS\",\"value\":\"G86200\"},{\"@type\":\"PropertyValue\",\"propertyID\":\"Werkstoffnummer\",\"value\":\"1.6523\"}]}}<\/script><!-- \/dm-ld --><\/p>\n","protected":false},"excerpt":{"rendered":"<p>AISI 8620 \/ (1.6523) \/ UNS G86200 \/ AMS 6274 DEFENCE METAL AISI 8620 UNS G86200 (hardenability-band grade 8620H = H86200) \u00b7 W.Nr. 1.6523 \u00b7 EN 10084 name 20NiCrMo2-2 (FORMER DIN NAME 21NiCrMo2; resulphurised free-machining variant 20NiCrMoS2-2 = 1.6526) \u00b7 SAE J404 \/ ASTM A29 band: C 0.18-0.23% &#8211; Mn 0.70-0.90% &#8211; Si 0.15-0.35% &#8211; &hellip; <\/p>\n<p class=\"link-more\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-8620\/\" class=\"more-link\"><span class=\"screen-reader-text\"> &#8220;AISI 8620 \/ AMS 6274&#8221;<\/span>devam\u0131n\u0131 oku<\/a><\/p>\n","protected":false},"author":1,"featured_media":0,"parent":3526,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_yoast_wpseo_title":"AISI 8620 \/ (1.6523) \/ UNS G86200 \/ AMS 6274 | Defence Metal","_yoast_wpseo_metadesc":"AISI 8620 (UNS G86200, 1.6523) \u2014 AMS 6274. Nickel-chromium-molybdenum carburising steel giving a hard case over a tough core.","inspiro_hide_title":false,"inspiro_hide_featured_image":false,"footnotes":""},"dm_sektor":[10,13,9,14,15],"class_list":["post-3549","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.5 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>AISI 8620 \/ (1.6523) \/ UNS G86200 \/ AMS 6274 | Defence Metal<\/title>\n<meta name=\"description\" content=\"AISI 8620 (UNS G86200, 1.6523) \u2014 AMS 6274. 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