{"id":3529,"date":"2026-09-16T10:51:31","date_gmt":"2026-09-16T07:51:31","guid":{"rendered":"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/"},"modified":"2026-09-25T16:30:32","modified_gmt":"2026-09-25T13:30:32","slug":"aisi-4140","status":"publish","type":"page","link":"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/","title":{"rendered":"AISI 4140"},"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 4140 \/ UNS G41400 \/ AMS 6349 \/ AMS 6382<\/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 4140<\/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 G41400 (aircraft quality E4140 = G41406) \u00b7 W.Nr. 1.7225 \u00b7 EN 42CrMo4 (free-machining variant 42CrMoS4 = 1.7227) \u00b7 ASTM A29 \/ SAE J404 band: C 0.38-0.43% &#8211; Mn 0.75-1.00% &#8211; Si 0.15-0.35% &#8211; Cr 0.80-1.10% &#8211; Mo 0.15-0.25% &#8211; P 0.035% max &#8211; S 0.040% max &#8211; balance Fe. NICKEL IS NOT A SPECIFIED ELEMENT; in 4140 nickel is a residual. The EN 10083-3 42CrMo4 band is NOT THE SAME: C 0.38-0.45% &#8211; Si 0.40% max &#8211; Mn 0.60-0.90% &#8211; Cr 0.90-1.20% &#8211; Mo 0.15-0.30% &#8211; P 0.025% max &#8211; S 0.035% max. The two bands do not fully overlap on chromium (ASTM floor 0.80%, EN floor 0.90%; ASTM ceiling 1.10%, EN ceiling 1.20%) and are offset on manganese. Material certified to 42CrMo4 is therefore not automatically acceptable against a 4140 order; acceptance depends on the heat analysis meeting both bands. THIS IS A MARTENSITIC QUENCHED-AND-TEMPERED STEEL: it transforms to martensite on austenitising and oil quenching, and is then TEMPERED. 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-4140-aisi-4340-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 4340<\/a><a href=\"https:\/\/www.defencemetal.com\/index.php\/2026\/09\/15\/aisi-4140-h11-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;\">H11<\/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 machine and structural parts that are hardened by heat treatment and need medium-to-high strength together with toughness: shafts and spindles, gears, pins and bushings, hydraulic cylinder rods, die holders and plates, drilling and earth-moving components, and secondary structure and\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;\">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;\">Round bar, flat bar, plate, sheet, pipe\/tube, forging. All forms are supplied to order.<\/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, plain 4140 chemistry 0.95Cr &#8211; 0.20Mo &#8211; C 0.38-0.43%): 6382 (bars, forgings, rings and stock for forging or flash welded rings; AIRCRAFT QUALITY; ANNEALED) \u00b7 6349 (BARS only; NORMALIZED) \u00b7 6529 (BARS only; SPECIAL AIRCRAFT-QUALITY CLEANLINESS; NORMALIZED) \u00b7 6381 (MECHANICAL TUBING; first issued 1942, current revision K\/2022) \u00b7 6395 (SHEET, STRIP, PLATE) \u00b7 6452 (WELDING WIRE; vacuum melted; environment-controlled packaging) \u00b7 6390 (mechanical tubing &#8211; listed in the SAE catalogue with 4140 chemistry, but its current status could not be verified; see the standards note). ASTM: A29 \/ A29M (general requirements for hot-wrought alloy steel bars) \u00b7 A322 (alloy steel bars, standard grades) \u00b7 A331 (cold-finished bars) \u00b7 A519 (seamless mechanical tubing) \u00b7 A513 (ERW mechanical tubing) \u00b7 A506 (hot-rolled sheet and strip) \u00b7 A711 (stock for forgings) \u00b7 A646 (premium quality blooms and billets for aerospace forgings) \u00b7 A752 (wire rod) \u00b7 A829 (alloy structural steel plate) \u00b7 A193 B7 and B7M with A194 2H \/ 2HM (bolting and nuts) \u00b7 A320 L7 and L7M (low-temperature bolting). EN \/ ISO: EN 10083-3 42CrMo4 (1.7225) and 42CrMoS4 (1.7227) \u00b7 ISO 683-2. SAE: J404 \u00b7 J412 \u00b7 J1397.<br \/><span style=\"font-size:12.5px;color:#7b8f9b;line-height:1.6;display:inline-block;margin-top:6px;\">THE AMS NUMBERS ARE NOT INTERCHANGEABLE. All six carry the same chemical band (0.95Cr &#8211; 0.20Mo &#8211; C 0.38-0.43%), but they differ in PRODUCT FORM, DELIVERY CONDITION and CLEANLINESS LEVEL: 6382 is ANNEALED bar, forging and ring material and carries the\u2026<\/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;\">Its single most important practical advantage is that the same material is the base of both a structural quench-and-temper table and a bolting specification, and both guarantee numbers.<\/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;\">IT IS WELDABLE, BUT PREHEAT IS MANDATORY, and the delivery condition of the material governs the welding decision. PREHEAT: citing the Procedure Handbook of Arc Welding, Welding Answers gives 205-260 \u00b0C (400-500 \u00b0F) up to 13 mm (\u00bd in) and 316-371 \u00b0C (600-700 \u00b0F) for 13-50 mm (\u00bd-2 in);<\/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 0.80-1.10% and no passive layer forms. Without oil, paint, phosphating, plating or another protective measure it rusts in damp air; it is not suitable for marine or chloride-bearing environments.<br \/>\n2) CHOICE OF TEMPERING BAND: the 250-450 \u00b0C band is not used for structural quench and temper.<\/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 4140 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;\">Heat Treatment<\/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;\">TEMPER EMBRITTLEMENT<\/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 Section Size Effect<\/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;\">Physical 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;\">Welding<\/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;\">Machining<\/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;\">Corrosion, Hydrogen and Sour Service<\/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;\">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 4140 is a low-alloy steel, alloyed with chromium and molybdenum, that can be hardened by heat treatment. One of the most widely used grades in the <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/alloy-steels\/\">alloy steel<\/a> family, it stands out for combining strength, toughness and wear resistance in a single material. Its UNS designation is G41400.<\/p>\n<p>The approximately 1% chromium in the composition raises hardenability and wear resistance, while the 0.25% molybdenum increases strength at elevated temperature and reduces the risk of temper embrittlement. Together, the two make 4140 a steel that hardens through the depth of the section, so uniform mechanical properties can be achieved even in heavy cross-sections.<\/p>\n<p>AISI 4140 is normally supplied hardened and tempered (T condition). The heat treatment temperatures are: forging 1150 \u00b0C, annealing 830-850 \u00b0C, normalising 870-900 \u00b0C, hardening 800-830 \u00b0C (oil or polymer quench), tempering 450-700 \u00b0C. Tempering in the 200-420 \u00b0C range is avoided in order to prevent temper embrittlement.<\/p>\n<p>The grade is widely used in axles, gears, shafts, sprockets, pinions, studs and similar heavily loaded machine components. It can be supplied in round, flat, square and hexagonal bar form.<\/p>\n<div class=\"dm-tablo\" 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;\">Chemical Composition \u00b7 AISI 4140 (G41400)<\/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;\">C \u2014 Carbon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">0.40%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Si \u2014 Silicon<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">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;\">0.85%<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Cr \u2014 Chromium<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">1.00%<\/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;\">Mo \u2014 Molybdenum<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">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%;\">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>\n<\/div>\n<div class=\"dm-mekanik\" 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;\">Mechanical Properties \u00b7 AISI 4140 \u00b7 Hardened + Tempered<\/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;\">Section 50 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">R<sub>m<\/sub> 930 MPa \u00b7 R<sub>p0.2<\/sub> 770 MPa \u00b7 Elongation 17% \u00b7 275 HB<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Section 100 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">R<sub>m<\/sub> 920 MPa \u00b7 R<sub>p0.2<\/sub> 710 MPa \u00b7 Elongation 15% \u00b7 270 HB<\/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;\">Section 200 mm<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">R<sub>m<\/sub> 850 MPa \u00b7 R<sub>p0.2<\/sub> 570 MPa \u00b7 Elongation 14% \u00b7 250 HB<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Izod impact<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">90 J (50 mm) \u00b7 70 J (100 mm) \u00b7 60 J (200 mm)<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<\/div>\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 4140<\/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 4140<\/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;\">G41400<\/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;\">AMS<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">6349 \u00b7 6382<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">Available forms<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">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 class=\"dm-ic-baglanti\" 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 4140 stock availability, sizes and AMS 6349 \/ AMS 6382 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<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 4140 Is \u2014 and Why It Is Not \u201cAlmost Stainless\u201d<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">AISI\/SAE <b>4140<\/b> (UNS <b>G41400<\/b> \/ W.Nr. <b>1.7225<\/b> \/ EN <b>42CrMo4<\/b> \/ JIS <b>SCM440<\/b>) is a <b>medium-carbon, through-hardening chromium-molybdenum alloy structural steel<\/b>. Its one distinguishing sentence: <b>it is the most widely used quenched-and-tempered steel in the world because, instead of being excellent at one thing, it is good enough at everything<\/b> \u2014 acceptable hardenability, acceptable toughness, acceptable machinability, and a low price.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>And this has to be said at the outset: 4140 IS NOT STAINLESS.<\/b> It contains about <b>1 % chromium<\/b>. The threshold for forming a passive chromium oxide film is about <b>10.5 %<\/b> \u2014 so 4140 carries roughly <b>one tenth<\/b> of what is required. The chromium is there for <b>hardenability<\/b>, not for corrosion. <b>4140 rusts like plain carbon steel<\/b> and, left unpainted, unplated and unoiled, will show surface rust in the atmosphere within days.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The whole engineering of the alloy sits in <b>two elements<\/b>. <b>Chromium (0.80\u20131.10 %)<\/b> delays the pearlite and bainite transformations, which at a given cooling rate means <b>martensite deeper into the section<\/b> \u2014 that is hardenability. <b>Molybdenum (0.15\u20130.25 %)<\/b> does two jobs: it adds hardenability <b>and it provides resistance to temper embrittlement<\/b>. That second job is the subject of the most critical section on this page, and almost no distributor sheet mentions it.<\/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 4130<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Same Cr-Mo system, but nominal carbon <b>0.30 %<\/b> (0.40 % in 4140). The result: <b>4130 reaches lower maximum hardness and lower strength, but is far easier to weld<\/b> \u2014 its carbon equivalent is markedly lower. <b>For welded tubular structures (aircraft frames, roll cages, chassis) 4130 is the right answer, not 4140.<\/b> Choose 4130 for any job where post-weld heat treatment is impossible<\/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 4340<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Same carbon (0.38\u20130.43 %) and similar Cr-Mo, but <b>Ni 1.65\u20132.00 % is added<\/b> (4140 contains NO nickel) and Mn is lower (0.60\u20130.80 % against 0.75\u20131.00 %). What the nickel buys is <b>far greater hardenability<\/b>: 4340 hardens much larger sections to the core and gives <b>better toughness at a given strength<\/b>. The cost is price and machinability. <b>Rule:<\/b> if the section exceeds \u2300100 mm, or if impact \/ fracture toughness is critical, <b>move to 4340<\/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 8620 \u2014 A CATEGORY ERROR<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">At <b>C 0.18\u20130.23 %<\/b>, 8620 is a <b>CARBURISING (case hardening) steel<\/b>. It is not a through-hardening grade. Its job is to produce <b>a hard case over a tough core<\/b>; 4140\u2019s job is to produce <b>a uniform quenched-and-tempered structure throughout<\/b>. \u201cWhich is harder, 4140 or 8620?\u201d is the wrong question \u2014 the right question is <b>surface or core<\/b>. Use 8620 for gears, pins and bushings with surface wear and core toughness; 4140 for shafts, bars and forged bodies loaded through their volume<\/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 4142 \u00b7 4145<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Same alloy system, <b>only the carbon step differs<\/b>: 4140 C 0.38\u20130.43 %, <b>4142 C 0.40\u20130.45 %<\/b>, <b>4145 C 0.43\u20130.48 %<\/b>. Higher carbon means higher attainable hardness and worse weldability. <b>The ASTM A193 B7 bolting specification gives a C band of 0.38\u20130.48 %<\/b> \u2014 so a B7 stud may actually be 4140, 4142 or 4145. You cannot know which without reading 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%;background:#F7FAFB;\"><b>Versus ultra-high-strength steels<\/b> (<a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/300m\/\">300M<\/a>, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aermet-100\/\">AerMet 100<\/a>, <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-250\/\">Maraging 250<\/a>)<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">These work in the <b>1900\u20132000 MPa<\/b> band; 4140\u2019s practical quenched-and-tempered band is <b>750\u20131200 MPa<\/b>. <b>They are not in the same league<\/b> and the price gap exceeds a factor of ten. Maraging steels are also <b>carbon-free<\/b> and take their strength from precipitation hardening \u2014 no quench distortion, no temper embrittlement. <b>If dimensional stability is critical, maraging; if cost is critical, 4140<\/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>Versus <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/17-4ph-1-4542-aisi-630\/\">17-4 PH<\/a><\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>The comparison ends the moment corrosion resistance is required.<\/b> 17-4 PH is a martensitic <b>stainless<\/b> working in strength bands close to 4140. If the part is wet, outdoors or in a chemical environment, the choice between <b>4140 + coating<\/b> and <b>17-4 PH<\/b> should be made on coating life and hydrogen embrittlement risk \u2014 not on first cost<\/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;\">4140, 4140H and \u201c4140 HT\u201d \u2014 three different orders<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>4140<\/b> is a chemistry specification. <b>4140H<\/b> means an <b>H band<\/b>: the chemistry widens slightly but the mill <b>guarantees the Jominy hardenability band<\/b>. If you will do the heat treatment yourself and you want repeatability, <b>ask for 4140H<\/b> \u2014 asking for \u201c4140\u201d guarantees no hardenability at all. <b>\u201c4140 HT\u201d or \u201cpre-hardened 4140\u201d<\/b> is neither a chemistry nor a standard but a <b>delivery condition<\/b>: bar quenched and tempered at the mill, typically shipped in the <b>28\u201332 HRC (\u2248285\u2013321 HB)<\/b> band. Do not put all three on one purchase line.<\/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 6382<\/b> (annealed, aircraft quality) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6349<\/b> (normalized) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6529<\/b> (normalized, special aircraft-quality cleanliness) \u00b7 ASTM A29 \/ A29M (general requirements) \u00b7 ASTM A322 (alloy steel bars, standard grades) \u00b7 ASTM A331 (cold-finished bars) \u00b7 EN 10083-3 42CrMo4 \/ 42CrMoS4 \u00b7 ISO 683-2<\/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 6381<\/b> (mechanical tubing; revision K\/2022 verified) \u00b7 <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6390<\/b> (mechanical tubing; STATUS NOT VERIFIED) \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;\"><b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6395<\/b> (sheet, strip and plate) \u00b7 ASTM A506 (hot-rolled sheet and strip) \u00b7 ASTM A829 (alloy structural steel plate)<\/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 6382<\/b> (forgings, rings and stock for forging or flash welded rings; annealed) \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). No AMS WIRE number (other than welding wire) verified across four sources was found for 4140.<\/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 6452<\/b> (welding wire, 0.95Cr &#8211; 0.20Mo, C 0.38-0.43%, vacuum melted, environment-controlled packaging) \u00b7 AWS A5.28 ER80S-D2 (general fabrication). <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 6457<\/b> DOES NOT BELONG TO THIS MATERIAL: it is 4130 welding wire (C 0.28-0.33%).<\/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;\">Bolts \u00b7 studs \u00b7 nuts<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">ASTM A193 Grade B7 and B7M (studs and bolts) \u00b7 ASTM A194 Grade 2H and 2HM (nuts) \u00b7 ASTM A320 Grade L7 and L7M (low-temperature bolting, 593 \u00b0C minimum temper plus a Charpy requirement)<\/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;\">Sour service<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">NACE MR0175 \/ ISO 15156-2 &#8211; carbon and low alloy steels are acceptable without further testing when hardness does not exceed 22 HRC; the higher steps (26 and 30 HRC for tubulars) require SSC testing and the quenched-and-tempered condition. On the bolting side the equivalent is A193 B7M \/ A194 2HM.<\/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;\">Post-plating hydrogen embrittlement relief<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">SAE <b style=\"font-size:16.5px;font-weight:800;color:#12303f;\">AMS 2759<\/b>\/9 (Hydrogen Embrittlement Relief \/ Baking of Steel Parts) &#8211; typically 190-218 \u00b0C for 2 to 24 hours, started within 1 to 4 hours of exposure.<\/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: 4140 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;\">In every row the AMS numbers come FIRST and ASTM and EN follow; the customer asked for the AMS numbers to be prominent. Where a product form has more than one AMS number, those are NOT alternatives: the delivery condition (annealed \/ normalized) and the cleanliness level differ. The AMS 6390 row is deliberately left with its caution: the number belongs to 4140 chemistry, but its current revision could not be verified. For wire (other than welding wire) and for pipe, no AMS number specific to 4140 and verified across four sources was found; that gap is stated openly.<\/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 4140 (G41400 \/ 1.7225 \/ 42CrMo4)<\/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 4140<\/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 bars (standard grades)<\/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 bars<\/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%;\">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;\">Electric-resistance-welded (ERW) 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%;\">Other forms<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Hot-rolled sheet and strip <b>A506<\/b> \u00b7 forging stock <b>A711<\/b> \u00b7 aerospace blooms and billets <b>A646<\/b> (premium quality) \u00b7 wire rod <b>A752<\/b> \u00b7 structural plate <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>Bolts \u00b7 studs<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A193 Grade B7<\/b> (standard) and <b>B7M<\/b> (sour service, \u226422 HRC). <b>Note the B7 chemistry is a C 0.38\u20130.48 % band<\/b> \u2014 so it may be 4140, 4142 or 4145<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Nuts<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">ASTM <b>A194 Grade 7<\/b> \/ <b>7M<\/b>. <b>[conflict]<\/b> One publisher gives the matching nut for B7 studs as <b>A194 Grade 2H<\/b> (248\u2013352 HB). <b>Both are used in practice<\/b>; <b>write which nut you want on the order<\/b> rather than assuming<\/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>Low-temperature bolting<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">ASTM <b>A320 Grade L7<\/b>, <b>L7M<\/b>, <b>L7D<\/b> \u2014 the same material with added Charpy impact requirements<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\">SAE<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>SAE J404<\/b> (chemical compositions) \u00b7 <b>J412<\/b> \u00b7 <b>J1397<\/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>Aerospace (AMS)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>AMS 6349, 6381, 6382, 6390, 6395, 6529<\/b>. These numbers cover <b>different product forms and different quality \/ cleanliness levels<\/b> (bar, tubing, forging, premium melt) \u2014 <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-5626<\/b> \u00b7 <b>MIL-S-16974<\/b> \u00b7 <b>MIL-S-46059<\/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 Q&amp;T steel<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>EN 10083-3<\/b>, grade <b>42CrMo4 (1.7225)<\/b> and its sulphur-bearing variant <b>42CrMoS4 (1.7227)<\/b>. The international equivalent is <b>ISO 683-2<\/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>Europe \u2014 bolting<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>EN 10269<\/b> \u2014 steels for fasteners with specified elevated and\/or low temperature properties; <b>42CrMo4 appears there together with elevated-temperature proof strength values<\/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>NACE<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>MR0175 \/ ISO 15156-2<\/b> \u2014 for carbon and low alloy steels, a maximum of <b>22 HRC<\/b> and a mandatory <b>quenched-and-tempered<\/b> condition. This is the single most restrictive rule on this page<\/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 \u201c4140\u201d Does Not Buy You<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>In 4140 the gap is not in the chemistry, it is in the HEAT TREATMENT CONDITION.<\/b> This is the alloy\u2019s most trouble-prone commercial property: <b>you buy the chemistry, but what determines the part\u2019s properties is not the chemistry \u2014 it is the heat treatment<\/b>, and the heat treatment is usually missing from the order line.<\/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>\u201c4140\u201d alone is NOT a mechanical property commitment<\/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> Rp0.2 or Rm. The same 4140 bar may, depending on delivery condition, sit anywhere between <b>655 MPa (annealed) and 2000 MPa (quenched, low tempered)<\/b>. <b>If your order line does not state the heat treatment condition and a target hardness, you have not specified anything<\/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 European route CLOSES this gap<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">EN 10083-3 defines the <b>+QT<\/b> (quenched and tempered) delivery condition <b>with mechanical minimums per ruling section<\/b> \u2014 and, beyond that, it also sets an <b>UPPER LIMIT on Rm<\/b>. Nothing of the kind exists on the ASTM side. <b>If you want repeatability, the European ordering language is the safer one<\/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>Cast equivalent<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>4140 has no standardised cast counterpart.<\/b> Casting specifications such as ASTM A148 and A487 are written <b>by mechanical class<\/b>, not by chemistry. The honest answer to a customer asking for \u201ccast 4140\u201d is: <b>choose an equivalent CASTING CLASS<\/b> and state in writing that it is not 4140<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Weld metal equivalent<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>There is no common filler wire that reproduces 4140 chemistry, and that is deliberate.<\/b> In practice <b>ER80S-D2<\/b> is used (and undermatching <b>ER70S-2<\/b> for toughness). Matching chemistry only makes sense on parts that will be <b>fully re-quenched and tempered after welding<\/b>. The reason is in the Welding section<\/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;\"><b>SAE 4140 \/ UNS G41400 (ASTM A29 \u00b7 A322 \u00b7 SAE J404), weight %:<\/b> <b>C 0.38\u20130.43<\/b> \u00b7 <b>Mn 0.75\u20131.00<\/b> \u00b7 <b>Si 0.15\u20130.35<\/b> \u00b7 <b>P \u22640.035<\/b> \u00b7 <b>S \u22640.040<\/b> \u00b7 <b>Cr 0.80\u20131.10<\/b> \u00b7 <b>Mo 0.15\u20130.25<\/b> \u00b7 Fe balance.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>EN 42CrMo4 \/ 1.7225 (EN 10083-3 \u00b7 ISO 683-2), weight %:<\/b> <b>C 0.38\u20130.45<\/b> \u00b7 <b>Si 0.10\u20130.40<\/b> \u00b7 <b>Mn 0.60\u20130.90<\/b> \u00b7 <b>P \u22640.025<\/b> \u00b7 <b>S \u22640.035<\/b> \u00b7 <b>Cr 0.90\u20131.20<\/b> \u00b7 <b>Mo 0.15\u20130.30<\/b> \u00b7 <b>Cu \u22640.40<\/b> \u00b7 Fe balance.<br \/><b>42CrMoS4 \/ 1.7227:<\/b> identical, with the single difference <b>S 0.020\u20130.040 (with a MINIMUM)<\/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;\">SAE 4140 versus EN 42CrMo4 \u2014 NOT \u201cthe Same Steel\u201d<\/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>Manganese \u2014 the biggest divergence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">SAE <b>0.75\u20131.00<\/b> \u00b7 EN <b>0.60\u20130.90<\/b>. <b>The common band is only 0.75\u20130.90.<\/b> A heat at Mn = 0.95 % that conforms perfectly to SAE 4140 <b>DOES NOT conform to EN 42CrMo4<\/b>; a heat at Mn = 0.65 % <b>does not conform to SAE 4140<\/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>Chromium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">SAE <b>0.80\u20131.10<\/b> \u00b7 EN <b>0.90\u20131.20<\/b>. <b>Common band 0.90\u20131.10.<\/b> Again, non-conformance is possible in both directions<\/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<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">SAE <b>0.38\u20130.43<\/b> \u00b7 EN <b>0.38\u20130.45<\/b>. <b>EN is wider<\/b>: a European heat at C = 0.44 % does not meet SAE 4140 (but does meet SAE <b>4142<\/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>Molybdenum<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">SAE <b>0.15\u20130.25<\/b> \u00b7 EN <b>0.15\u20130.30<\/b>. EN is wider<\/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>Phosphorus and sulphur<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">SAE P \u22640.035 \/ S \u22640.040 \u00b7 EN P \u2264<b>0.025<\/b> \/ S \u2264<b>0.035<\/b>. <b>EN demands a cleaner steel.<\/b> This matters directly in the temper embrittlement section \u2014 <b>phosphorus is the embrittling element<\/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>Copper<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">The SAE specification sets <b>no<\/b> Cu limit; EN sets <b>\u22640.40<\/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;\"><b>Practical consequence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Heats that satisfy BOTH specifications exist and are common<\/b> \u2014 many mills deliberately produce dual-certified material. <b>But that is a choice, not a rule.<\/b> A page that writes \u201c4140 = 42CrMo4\u201d is describing the <b>intersection<\/b> of the two specifications and presenting it <b>as an identity<\/b>. <b>If the customer asks for 42CrMo4, check the certificate against the 42CrMo4 bands LINE BY LINE<\/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>And the A193 B7 band is wider still<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">B7 allows <b>C 0.38\u20130.48 %<\/b> \u2014 i.e. it covers <b>4140, 4142 and 4145 together<\/b>. Saying \u201ca B7 stud is a 4140 stud\u201d is wrong; <b>B7 is a performance class, not a chemistry grade<\/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;\">42CrMoS4 \u2014 the sulphur-bearing variant and its hidden cost<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>42CrMoS4 (1.7227) is the same steel as 42CrMo4; its only difference is that sulphur carries a MINIMUM (0.020\u20130.040 %).<\/b> Sulphur forms <b>manganese sulphide (MnS) inclusions<\/b>, which break the chip, lubricate the tool and <b>improve machinability markedly<\/b>. For a shop running automatic lathes, that is a real gain.<br \/><b>Here is the cost.<\/b> MnS inclusions <b>elongate<\/b> in the rolling direction and make the material anisotropic. <b>Transverse ductility and impact toughness drop.<\/b> Longitudinal Charpy may look unchanged while the transverse value has fallen significantly. <b>So do not use 42CrMoS4 for:<\/b> transversely loaded forgings, shafts under multiaxial stress, impact-loaded connections, and any part that will run at low temperature. <b>The equation \u201cbetter machinability, therefore better steel\u201d is false for this grade<\/b>, and distributor sheets routinely offer the two interchangeably.<\/p>\n<h4 id=\"dm-b4\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Heat Treatment \u2014 the Heart of This Page<\/h4>\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 forging finish temperature and the cooling that follows decide whether a normalize 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;\">The sources diverge at the upper limit. Saarstahl and Lucefin 1100-850 \u00b0C \u00b7 Rodacciai 850-1150 \u00b0C \u00b7 Flame Hardening 850-1050 \u00b0C. AZoM (ASM-derived) gives 926-1205 \u00b0C, which sits above the others; 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 confirmed across 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;\">Do not forge below 850 \u00b0C. Flame Hardening says furnace cool; Saarstahl and Lucefin say cool in still air.<\/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;\">As-forged hardness depends on section and cooling rate; no binding hardness is stated for this step.<\/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 and homogenises the grain structure after forging or rolling. Recommended before hardening.<\/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;\">840-900 \u00b0C. Saarstahl 850-880 \u00b0C \u00b7 Doerrenberg 850-880 \u00b0C \u00b7 Lucefin 870 \u00b0C \u00b7 Flame Hardening 840-880 \u00b0C \u00b7 Vulcan 870-900 \u00b0C \u00b7 Nifty Alloys 870-900 \u00b0C. DIVERGING SOURCE: AZoM gives a single value of 913 \u00b0C (1675 \u00b0F).<\/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;\">Vulcan gives 10-15 minutes per 25 mm of section. No single numerical time was confirmed across 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 cool (Saarstahl, Doerrenberg, Lucefin, Flame Hardening, Vulcan and Nifty Alloys all 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 value was confirmed across 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 (SPHEROIDISING) ANNEAL AND FULL ANNEAL &#8211; THESE ARE NOT THE SAME THING<\/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 (SPHEROIDISING) ANNEAL AND FULL ANNEAL &#8211; THESE ARE NOT THE SAME THING<\/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 soft anneal stays BELOW the critical temperature and is for machinability. The full anneal goes ABOVE it.<\/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;\">SOFT ANNEAL (subcritical): 680-720 \u00b0C. Saarstahl 680-720 \u00b0C \u00b7 Doerrenberg 680-720 \u00b0C \u00b7 Ovako 680-720 \u00b0C \u00b7 Flame Hardening 680-720 \u00b0C \u00b7 Lucefin 720 \u00b0C \u00b7 Rodacciai 650 \u00b0C. FULL ANNEAL (supercritical): 800-872 \u00b0C. AZoM 872 \u00b0C (1600 \u00b0F) \u00b7 Ellwood 871 \u00b0C (1600 \u00b0F) \u00b7 Vulcan 800-850 \u00b0C \u00b7 Nifty Alloys 840-870 \u00b0C \u00b7 Rodacciai gives 830-860 \u00b0C for an isothermal anneal.<\/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 confirmed across 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;\">SLOW FURNACE COOLING. Lucefin and Ovako give 15 \u00b0C per hour down to 600 \u00b0C; Saarstahl, Doerrenberg, Vulcan and AZoM say furnace cool.<\/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, 241 HBW MAXIMUM (Saarstahl and Doerrenberg). Lucefin gives separate figures for the as-rolled condition: +AR 301 HB max, controlled-cooled +ARc 279 HB max &#8211; these are NOT the annealed condition and must not be confused with it.<\/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 AUSTENITISING + QUENCH (hardening)<\/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 AUSTENITISING + QUENCH (hardening)<\/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;\">This is the step that produces the hardness. Carbon goes into solid solution and the quench turns the structure to martensite.<\/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;\">820-880 \u00b0C. Saarstahl 820-860 \u00b0C \u00b7 Doerrenberg 820-860 \u00b0C \u00b7 Rodacciai 830-850 \u00b0C \u00b7 Flame Hardening 830-860 \u00b0C \u00b7 Ovako 840-880 \u00b0C \u00b7 Lucefin 860 \u00b0C \u00b7 AZoM and Ellwood 845 \u00b0C (1550 \u00b0F) \u00b7 Nifty Alloys 845-870 \u00b0C \u00b7 Industeel about 850 \u00b0C. DIVERGING SOURCE: West Yorkshire Steel 860-890 \u00b0C. 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;\">Industeel gives one hour per 25 mm (1 in) of section. No single numerical time was confirmed across 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. In all ten sources listed, oil is the first choice (Saarstahl, Doerrenberg, Ovako, Rodacciai, Lucefin, Flame Hardening, AZoM, Ellwood, West Yorkshire, Nifty Alloys). Saarstahl, Doerrenberg, Ovako and Rodacciai also list WATER for heavy sections; Lucefin adds a polymer solution. A water quench raises the risk of cracking.<\/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;\">The as-quenched (untempered) hardness differs between sources: Lucefin measures 57 HRC at a 100 \u00b0C temper (so the as-quenched value is just above that), Nifty Alloys gives 55-60 HRC, and the Doerrenberg TTT diagram shows about 48 HRC for an oil quench from 850 \u00b0C. NO SINGLE VALUE IS STATED. In this condition the material is brittle and IS NOT USED WITHOUT TEMPERING.<\/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 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;\">5 \u00b7 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;\">MANDATORY after quenching. The temperature is chosen for the target strength and toughness.<\/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;\">STRUCTURAL QUENCH-AND-TEMPER BAND (European producer consensus): 540-680 \u00b0C. Saarstahl 540-680 \u00b0C \u00b7 Lucefin 540-680 \u00b0C \u00b7 Ovako 540-680 \u00b0C \u00b7 Flame Hardening 540-680 \u00b0C \u00b7 Rodacciai 550-650 \u00b0C \u00b7 Industeel 520-640 \u00b0C. WIDE US BAND (by hardness target): 205-650 \u00b0C (400-1200 \u00b0F) &#8211; AZoM, Ellwood and Nifty Alloys. For 250-450 \u00b0C see the FORBIDDEN BAND box.<\/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;\">Flame Hardening and Vulcan: soak at heat for AT LEAST 1 hour. Industeel recommends double tempering with a full cool to room temperature after each temper.<\/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 cool (Saarstahl, Lucefin, Flame Hardening). Total Materia gives ACCELERATED cooling from above 600 \u00b0C as the countermeasure against reversible temper embrittlement.<\/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;\">See the tempering table.<\/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;\">Tempering table<\/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;\">Note<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The table shows the relationship between tempering temperature and hardness\/strength. EVERY ROW IS GIVEN WITH ITS SOURCE. The Lucefin rows are a MEASURED curve: a \u00d810 mm specimen oil quenched from 850 \u00b0C. In a heavy section the same tempering temperature gives LOWER hardness, because full martensite does not form at the centre. This table is not an ordering specification; an order must be tied to an EN 10083-3 +QT diameter row or to a specification such as ASTM A193 B7.<\/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;\">FORBIDDEN TEMPERING BAND &#8211; 250-450 \u00b0C (for structural quench and temper)<\/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;\">FORBIDDEN TEMPERING BAND &#8211; 250-450 \u00b0C (for structural quench and temper)<\/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;\">What happens<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Impact toughness drops. Two separate mechanisms cover this band: tempered martensite embrittlement (TME, irreversible) and temper embrittlement (TE, reversible).<\/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;\">As named in the source<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The Industeel 4340 data sheet states plainly &#8216;avoid temperature between 250-450 \u00b0C&#8217;; the same producer&#8217;s 4140 sheet gives the tempering band as 520-640 \u00b0C. Herring (The Heat Treat Doctor): TME at 250-400 \u00b0C (480-750 \u00b0F), the mechanism being cementite precipitation on prior-austenite and interlath boundaries together with impurity segregation, IRREVERSIBLE; TE at 375-575 \u00b0C (705-1070 \u00b0F), the mechanism being segregation of P, Sn, As and Sb to grain boundaries, REVERSIBLE by re-tempering above 575 \u00b0C with rapid cooling. Thermal Processing Magazine: TE 375-575 \u00b0C. Total Materia: the irreversible form at 250-400 \u00b0C, the reversible form at 450-650 \u00b0C, countered by accelerated cooling from above 600 \u00b0C and by 0.2-0.3% molybdenum.<\/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;\">Contrary evidence<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">THE SOURCES ARE NOT UNANIMOUS ON THIS BAND, and the counter-evidence is recorded too: Carpenter describes 4140 as &#8216;a through hardening Chromium-Molybdenum medium Carbon steel which is not subject to temper embrittlement&#8217;. Flame Hardening and Vulcan state that molybdenum keeps the steel from being susceptible to temper brittleness. Herring and Total Materia also confirm that molybdenum (0.2-0.3%) reduces the effect &#8211; the molybdenum band of 4140 is 0.15-0.25%, which reduces the effect but does not remove it. PRACTICAL CONCLUSION: the band the European producers (Saarstahl, Lucefin, Ovako, Flame Hardening) give for structural quench and temper is 540-680 \u00b0C, entirely outside the disputed region. 250-450 \u00b0C is used only where high hardness is the target and there is no impact toughness requirement.<\/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;\">Servis uyarisi<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">This band is not only a HEAT TREATMENT question: long SERVICE inside 250-450 \u00b0C runs the same mechanism.<\/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 published TTT\/CCT curve confirmed across four independent sources was used, so no curve is drawn. THIS ALLOY IS A MARTENSITIC QUENCH-AND-TEMPER STEEL: it hardens by austenitising, oil quenching and tempering. It does NOT precipitation harden; there is NO ageing step of the H900 \/ H1025 \/ H1075 \/ H1150 type. The five steps below were each verified separately. 4140 DOES NOT PRECIPITATION HARDEN. There is NO &#8216;H900 \/ H1025&#8217; type step for this material; those steps belong to precipitation hardening stainless steels such as 17-4 PH. A soft anneal (680-720 \u00b0C) and a full anneal (800-872 \u00b0C) are NOT the same thing and do not give the same result. The order must state which one is required. The quench medium is oil. Some producers allow water for heavy sections, but it raises the risk of cracking; the design must account for that. Quenched but untempered 4140 is NOT used. Tempering is the mandatory final step of the cycle. The tempering table is for a \u00d810 mm specimen. In a heavy section the same temperature gives lower hardness; this is not a quality problem but a consequence of the hardenability limit. Normalized and annealed delivery conditions map to different AMS numbers: AMS 6349 and 6529 are normalized, AMS 6382 is annealed. The sources diverge on the 250-450 \u00b0C band; whoever reads this card should see that the counter-evidence is recorded too. The point of agreement is the 540-680 \u00b0C band for structural quench and temper.<\/div>\n<\/div>\n<p><!-- \/dm-diy-isil --><\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>With 4140 you do not buy the material, you buy the heat treatment.<\/b> The same chemistry can sit anywhere between <b>27 HRC and 57 HRC<\/b> depending on the tempering temperature. The tables below are the most-used part of this page.<\/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;\">Transformation Temperatures and Core Heat Treatment Parameters<\/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>Critical points<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Ac1 745 \u00b0C<\/b> \u00b7 <b>Ac3 790 \u00b0C<\/b> \u00b7 <b>Ms 335 \u00b0C<\/b> \u00b7 <b>Mf 80 \u00b0C<\/b>. <b>Mf at 80 \u00b0C matters:<\/b> if you finish the quench at room temperature the transformation is <b>complete<\/b>; 4140 generally has no significant retained austenite problem<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Normalising<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>870 \u00b0C<\/b>, still air. <b>[CONFLICT \u2014 important]<\/b> One US source gives the result as <b>302 HB<\/b>; a European source gives <b>\u2248190 HB<\/b> for the same 870 \u00b0C. <b>The difference comes from section thickness and the real air-cooling rate<\/b> \u2014 a thin specimen can partly martensite in air. <b>Do not promise a normalised hardness; ask for the section<\/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>Soft annealing<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>US practice:<\/b> heat to 845 \u00b0C, cool from <b>755 \u00b0C to 665 \u00b0C at 14 \u00b0C\/h<\/b>, then in air \u2192 <b>\u2248197 HB<\/b> (alternative: cool rapidly to 675 \u00b0C and hold <b>5 h isothermally<\/b>). <b>Europe (+A):<\/b> <b>720 \u00b0C<\/b>, furnace cool to 600 \u00b0C, then air \u2192 <b>\u2264241 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%;\"><b>Hardening (austenitising)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>845\u2013870 \u00b0C<\/b> (1550\u20131600 \u00b0F). European practice <b>860 \u00b0C<\/b>. Soak: <b>1 hour per 25 mm of section, minimum 1 hour<\/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>Quench medium<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Agitated OIL<\/b> is the standard medium; polymer is also used. <b>Do not water quench<\/b> \u2014 4140 is prone to quench cracking in water and its hardenability is already adequate for oil<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>As-quenched maximum hardness<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>54\u201358 HRC<\/b> (fully martensitic structure; the spread follows the 0.38\u20130.43 % carbon band). <b>This is NOT a delivery condition<\/b> \u2014 untempered martensite is unusable<\/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 range<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>204\u2013649 \u00b0C<\/b> (400\u20131200 \u00b0F). European +T practice <b>540\u2013680 \u00b0C<\/b>. <b>Minimum soak: 2 hours after the load is at temperature throughout<\/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>Stress relief<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">At least <b>28 \u00b0C (50 \u00b0F) below<\/b> the tempering temperature (European +SR: <b>50 \u00b0C below<\/b>). <b>Removes 60\u201370 % of residual stress<\/b>, at a cost of <b>2\u20133 HRC<\/b> over a two-hour soak<\/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>Forging temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22481232 \u00b0C<\/b> (2250 \u00b0F). Another publisher gives the working band as <b>1204 \u2192 927 \u00b0C<\/b> (2200 \u2192 1700 \u00b0F)<\/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 tempering curve \u2014 all the numbers, and which section they came from<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>The table below is a complete European tempering curve.<\/b> The test condition must be stated explicitly: <b>\u230010 mm specimen, oil quenched from 850 \u00b0C<\/b>. <b>That is a small specimen and the values are an UPPER BOUND.<\/b> A \u2300100 mm bar will reach none of these rows at its core.<\/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;\">Tempering Temperature \u2192 Hardness and Strength (\u230010 mm, oil from 850 \u00b0C)<\/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>100 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 595 \u00b7 <b>HRC 57<\/b> \u00b7 Rm <b>2200<\/b> \u00b7 Rp0.2 <b>1520 MPa<\/b> \u00b7 A \u2014 \u00b7 <b>KV 24 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%;\"><b>150 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 586 \u00b7 <b>HRC 56.5<\/b> \u00b7 Rm 2180 \u00b7 Rp0.2 1600 MPa \u00b7 A 7.0 % \u00b7 KV 27 J<\/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>200 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 550 \u00b7 <b>HRC 54.5<\/b> \u00b7 Rm 2030 \u00b7 Rp0.2 <b>1620 MPa (PEAK)<\/b> \u00b7 A 9.5 % \u00b7 KV 28 J<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>250 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 518 \u00b7 HRC 52.5 \u00b7 Rm 1910 \u00b7 Rp0.2 1590 MPa \u00b7 A 10.0 % \u00b7 KV 27 J<\/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>300 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 496 \u00b7 HRC 51 \u00b7 Rm 1800 \u00b7 Rp0.2 1560 MPa \u00b7 A 10.0 % \u00b7 KV 26 J<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>350 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 468 \u00b7 HRC 49 \u00b7 Rm 1700 \u00b7 Rp0.2 1510 MPa \u00b7 A 10.0 % \u00b7 <b>KV 26 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>400 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 442 \u00b7 HRC 47 \u00b7 Rm 1590 \u00b7 Rp0.2 1440 MPa \u00b7 A 10.4 % \u00b7 <b>KV 26 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%;\"><b>450 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 421 \u00b7 HRC 45 \u00b7 Rm 1480 \u00b7 Rp0.2 1340 MPa \u00b7 A 11.0 % \u00b7 <b>KV 27 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>500 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 390 \u00b7 HRC 42 \u00b7 Rm 1350 \u00b7 Rp0.2 1230 MPa \u00b7 A 12.0 % \u00b7 KV 31 J<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>550 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 362 \u00b7 HRC 39 \u00b7 Rm 1220 \u00b7 Rp0.2 1110 MPa \u00b7 A 13.5 % \u00b7 <b>KV 42 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>600 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 336 \u00b7 HRC 36 \u00b7 Rm 1100 \u00b7 Rp0.2 1000 MPa \u00b7 A 15.8 % \u00b7 <b>KV 75 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%;\"><b>650 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">HB 294 \u00b7 HRC 31 \u00b7 Rm 980 \u00b7 Rp0.2 870 MPa \u00b7 A 19.0 % \u00b7 <b>KV 114 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>700 \u00b0C<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">HB 264 \u00b7 HRC 27 \u00b7 Rm 880 \u00b7 Rp0.2 710 MPa \u00b7 A 21.5 % \u00b7 <b>KV 135 J<\/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>There are THREE conclusions to draw from this table and none of them appear on distributor sheets.<\/b><br \/><b>1) Yield strength PEAKS at 200 \u00b0C (1620 MPa) and then falls.<\/b> As-quenched (HRC 57) the yield is <b>1520 MPa<\/b> \u2014 i.e. <b>lower than tempered<\/b>. The reason is the relief of internal stresses in the martensite and fine carbide precipitation during low-temperature tempering. <b>\u201cTempering always weakens the steel\u201d is false.<\/b><br \/><b>2) Charpy energy is FLAT between 150 \u00b0C and 450 \u00b0C (26\u201328 J).<\/b> Across a three-hundred-degree tempering range <b>toughness does not improve at all<\/b>, only strength falls. So <b>tempering at 350\u2013450 \u00b0C gives up 500 MPa of strength and buys NOTHING in return<\/b>. Toughness only opens up <b>above 500 \u00b0C<\/b>: 31 J at 500 \u00b0C, 42 J at 550 \u00b0C, <b>75 J at 600 \u00b0C, 114 J at 650 \u00b0C<\/b>.<br \/><b>3) That gives the real rule for choosing a tempering temperature.<\/b> If impact or fracture toughness matters, temper at <b>at least 550 \u00b0C, preferably 600 \u00b0C and above<\/b>. If you want only hardness and wear resistance, stay in the <b>200\u2013250 \u00b0C<\/b> band. <b>The intermediate 300\u2013500 \u00b0C band is the worst of both worlds<\/b> \u2014 and, as the next section shows, the embrittlement hazards sit exactly there.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">The second and third tempering tables \u2014 why they do not agree<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Source B (US, secondary):<\/b> 204 \u00b0C <b>52\u201354 HRC<\/b> \u00b7 316 \u00b0C <b>48\u201351<\/b> \u00b7 427 \u00b0C <b>43\u201346<\/b> \u00b7 482 \u00b0C <b>38\u201342<\/b> \u00b7 538 \u00b0C <b>34\u201338 HRC<\/b>.<br \/><b>Source C (secondary):<\/b> 200 \u00b0C <b>50\u201352 HRC<\/b> \u00b7 300 \u00b0C <b>45\u201348<\/b> \u00b7 400 \u00b0C <b>40\u201344<\/b> \u00b7 500 \u00b0C <b>35\u201338<\/b> \u00b7 600 \u00b0C <b>28\u201332<\/b> \u00b7 650 \u00b0C <b>25\u201328 HRC<\/b>.<br \/><b>The full curve above (Source A):<\/b> 200 \u00b0C <b>54.5<\/b> \u00b7 300 \u00b0C <b>51<\/b> \u00b7 400 \u00b0C <b>47<\/b> \u00b7 500 \u00b0C <b>42<\/b> \u00b7 600 \u00b0C <b>36<\/b> \u00b7 650 \u00b0C <b>31 HRC<\/b>.<br \/><b>At 400 \u00b0C the three sources say 40\u201344, 43\u201346 and 47 HRC \u2014 a 7 HRC spread; at 600 \u00b0C the gap is 8 HRC.<\/b> The causes are section size, soak time, actual carbon content and quench severity; none of the three is wrong, all three come from different specimens. <b>Never make a published tempering table an acceptance criterion<\/b> \u2014 the real temperature is established with your own section, in your own furnace, on a trial piece.<\/p>\n<h4 id=\"dm-b5\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">TEMPER EMBRITTLEMENT \u2014 the Most Critical Section on This Page<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>There are THREE distinct phenomena that must be named separately. Data sheets routinely confuse them, and that confusion causes real failures.<\/b> All three have a different temperature band, a different mechanism and \u2014 most importantly \u2014 <b>a different reversibility<\/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;\">Three Separate Embrittlement Phenomena<\/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) TEMPERED MARTENSITE EMBRITTLEMENT (TME)<\/b><br \/>\u201c500 \u00b0F embrittlement\u201d, \u201cone-step\u201d<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Band: 260\u2013370 \u00b0C<\/b> (500\u2013700 \u00b0F). Some sources give <b>250\u2013400 \u00b0C<\/b>. <b>IRREVERSIBLE.<\/b> Mechanism: (a) <b>coarse cementite films<\/b> form at prior austenite grain boundaries and between laths and act as stress concentrators; (b) <b>retained austenite becomes mechanically unstable<\/b> and transforms to untempered martensite under load; (c) phosphorus and nitrogen segregate to the boundaries. <b>Silicon and molybdenum reduce TME by retarding cementite precipitation.<\/b> Oil-quenched structures (less retained austenite) are less affected than air-cooled ones<\/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) TEMPER EMBRITTLEMENT (TE)<\/b><br \/>\u201creversible\u201d, \u201ctwo-step\u201d<\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Band: 375\u2013575 \u00b0C<\/b> (707\u20131070 \u00b0F). <b>REVERSIBLE:<\/b> it can be undone by heating <b>above 575 \u00b0C for MINUTES<\/b> \u2014 but <b>only if the part is then cooled rapidly<\/b>. Mechanism: <b>phosphorus, antimony, tin and arsenic diffuse to and segregate at prior austenite grain boundaries<\/b>. The result: <b>the ductile-to-brittle transition temperature (DBTT) RISES and fracture toughness FALLS<\/b> \u2014 while room-temperature hardness and tensile strength <b>barely change at all<\/b>. <b>Which is why hardness testing WILL NOT CATCH IT<\/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>3) BLUE BRITTLENESS<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Occurs in a low-temperature band by a <b>strain aging<\/b> mechanism. It affects plain carbon and alloy steels; <b>high tin or phosphorus<\/b> increases susceptibility. Practical avoidance: <b>temper above 595 \u00b0C (1100 \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>4) A fourth that must not be confused with these<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u201c475 \u00b0C embrittlement\u201d<\/b> concerns only steels with <b>15 % chromium and above<\/b> (ferritic stainless steels, the ferrite phase of duplex). <b>It has nothing to do with 4140\u2019s 1 % chromium.<\/b> If a 4140 sheet mentions 475 \u00b0C embrittlement, that sheet is copy-paste<\/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;\">Two formulas that predict susceptibility in advance<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Susceptibility to temper embrittlement (TE) can be predicted FROM THE CHEMISTRY, and that is a real tool you can use at the ordering stage.<\/b> Two established indices exist:<br \/><b>Watanabe J factor<\/b> \u2014 compositions entered in weight %; <b>keep J &lt; 180<\/b>.<br \/><b>Bruscato X factor<\/b> \u2014 compositions entered in ppm; <b>keep X &lt; 20<\/b>.<br \/>As a broader criterion, a <b>PE value below 2.8\u20133.0<\/b> is considered adequate.<br \/><b>The harmful elements are phosphorus, antimony, tin and arsenic.<\/b> <b>Even trace amounts below 0.01 % can trigger embrittlement.<\/b> <b>Manganese and silicon MULTIPLY their effect<\/b> \u2014 which is why the J factor carries an (Si+Mn) multiplier.<br \/><b>The role of molybdenum:<\/b> <b>small molybdenum additions reduce TE susceptibility<\/b>, because they form <b>(Mo,Fe)\u2083P clusters that block phosphorus from reaching the grain boundary<\/b>. <b>The \u201cMo\u201d in 4140 is there for exactly this job.<\/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;\">And Now the Big Contradiction in the Literature<\/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>Claim A (one producer)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">4140 \u201c<b>is NOT subject to temper embrittlement<\/b>\u201d \u2014 a direct quotation from a producer\u2019s alloy description<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Claim B (literature)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">An independent technical report exists titled <b>\u201cTemper Embrittlement in 4140 Seamless Tubing\u201d<\/b>. A trade association also writes that <b>\u201cmost common low alloy steels\u201d<\/b> are affected in the 375\u2013575 \u00b0C band and recommends using <b>no tempering cycle below 1100 \u00b0F (593 \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;\"><b>How to resolve it<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Both are partly right, and the difference is one of DEGREE.<\/b> Molybdenum genuinely <b>reduces<\/b> TE susceptibility \u2014 4140 is far less susceptible than a Mo-free Cr-Mn steel. But <b>\u201creduced\u201d and \u201cimmune\u201d are not the same thing<\/b>: 0.15\u20130.25 % Mo does not tie up phosphorus <b>completely<\/b>, and a heat carrying high P\/Sn\/Sb\/As will still embrittle<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>And the key point<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>TME (260\u2013370 \u00b0C) is an entirely SEPARATE phenomenon and molybdenum does not remove it.<\/b> Even if \u201c4140 is not subject to TE\u201d were true, it <b>would not remove the danger of tempering at 260\u2013370 \u00b0C<\/b>. Any advice that does not separate the two phenomena is incomplete<\/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 SAFE RULE<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>For any 4140 part that is impact-loaded, notched, welded or will run at low temperature: do not temper in the 260\u2013575 \u00b0C band.<\/b> Choose either <b>\u2264250 \u00b0C<\/b> (if you want hardness only) or <b>\u2265595 \u00b0C<\/b> (if you want toughness). One source gives an even narrower warning: \u201c<b>avoid tempering in the 232\u2013299 \u00b0C (450\u2013570 \u00b0F) range for impact-loaded applications<\/b>\u201d<\/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 single most-omitted practical detail: COOLING AFTER TEMPERING<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Tempering a part at 620 \u00b0C and then furnace-cooling it takes that part STRAIGHT THROUGH the temper embrittlement band.<\/b> TE is reversible \u2014 it dissolves above 575 \u00b0C \u2014 but <b>it re-forms during slow cooling between 575 and 375 \u00b0C<\/b>. Phosphorus needs time to reach the grain boundary, and a heavy section cooling in a furnace gives it exactly that.<br \/><b>Correct practice:<\/b> cool from the tempering temperature <b>fast enough to pass quickly through 575\u2013375 \u00b0C<\/b> \u2014 in oil or water for heavy sections. <b>This one sentence explains a large share of the \u201cthe heat treatment was correct but the part still came out brittle\u201d cases<\/b>, and it appears on almost no product page.<\/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 Section Size Effect<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>4140 is not a \u201cdeep hardening\u201d steel; it is a \u201cdeep enough hardening\u201d steel.<\/b> That distinction becomes concrete around \u2300100 mm.<\/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 Hardenability (ISO 683-2, grain size \u22655) \u2014 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;\">From the quenched end <b>1.5 \u00b7 3 \u00b7 5 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>53\u201361<\/b> \u00b7 <b>53\u201361<\/b> \u00b7 <b>52\u201361<\/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>7 \u00b7 9 \u00b7 11 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>51\u201360<\/b> \u00b7 <b>49\u201360<\/b> \u00b7 <b>43\u201359<\/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>13 \u00b7 15 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>40\u201359<\/b> \u00b7 <b>37\u201358<\/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>20 \u00b7 25 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>34\u201356<\/b> \u00b7 <b>32\u201353<\/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>30 \u00b7 35 \u00b7 40 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>31\u201351<\/b> \u00b7 <b>30\u201348<\/b> \u00b7 <b>30\u201347<\/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>45 \u00b7 50 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>29\u201346<\/b> \u00b7 <b>29\u201345<\/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 REAL MESSAGE OF THIS TABLE<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Look at the band widths.<\/b> At 15 mm the accepted range is <b>37\u201358 HRC<\/b> \u2014 a <b>21 HRC spread<\/b>. So <b>two heats that both fully conform to the specification<\/b> can come out <b>21 HRC apart<\/b> at the same point after the same heat treatment. <b>That is not an error, that is the standard<\/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>Commercial consequence<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>If you want repeatable heat treatment, buy \u201c4140H\u201d, not \u201c4140\u201d<\/b> \u2014 H grades <b>narrow and guarantee the Jominy band<\/b>. If your production sees hardness drift between lots, this is most likely why<\/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;\">Section Size Effect \u2014 EN 10083-3 \/ ISO 683-2 +QT Minimums<\/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>\u230016\u201340 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>1000\u20131200 MPa<\/b> \u00b7 Rp0.2 <b>\u2265750 MPa<\/b> \u00b7 A <b>\u226511 %<\/b> \u00b7 Z <b>\u226545 %<\/b> \u00b7 KV <b>\u226535 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%;\"><b>\u230040\u2013100 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rm <b>900\u20131100 MPa<\/b> \u00b7 Rp0.2 <b>\u2265650 MPa<\/b> \u00b7 A <b>\u226512 %<\/b> \u00b7 Z <b>\u226550 %<\/b> \u00b7 KV <b>\u226535 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>\u2300100\u2013160 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>800\u2013950 MPa<\/b> \u00b7 Rp0.2 <b>\u2265550 MPa<\/b> \u00b7 A <b>\u226513 %<\/b> \u00b7 Z <b>\u226550 %<\/b> \u00b7 KV <b>\u226535 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%;\"><b>\u2300160\u2013250 mm<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rm <b>750\u2013900 MPa<\/b> \u00b7 Rp0.2 <b>\u2265500 MPa<\/b> \u00b7 A <b>\u226514 %<\/b> \u00b7 Z <b>\u226555 %<\/b> \u00b7 KV <b>\u226535 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>The yield falls by 33 %<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>750 MPa at \u230016 mm, 500 MPa at \u2300250 mm.<\/b> <b>Same steel, same heat treatment, same standard.<\/b> This is the section size effect quantified, and it is the proof that <b>publishing a single \u201c4140 yield strength\u201d figure is wrong<\/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>Rm is a BAND<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">EN sets not only a floor but <b>a ceiling<\/b> (e.g. 1000\u20131200 MPa for \u230016\u201340 mm). <b>An over-hard part can clear ASTM and still fail EN.<\/b> No such upper bound exists on the ASTM 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;\"><b>Quench depth<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Oil quenching produces martensite in sections up to about <b>\u2300100 mm (4 in)<\/b>. Above that <b>the core does not fully harden<\/b> and the design must account for it \u2014 or move to <b>nickel-bearing 4340<\/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 and normalised hardness<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">European route: <b>+AR \u2264301 HB<\/b> (natural cooling) \u00b7 <b>+ARc \u2264279 HB<\/b> (controlled cooling) \u00b7 <b>+A \u2264241 HB<\/b> (soft annealed) \u00b7 <b>+N \u2248190 HB<\/b> (normalised)<\/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;\">Typical US-route values \u2014 SINGLE SOURCE, small specimen<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Normalised at 870 \u00b0C:<\/b> Rm 1020 MPa \u00b7 Rp0.2 655 MPa \u00b7 A 17.7 % \u00b7 Z 46.8 % \u00b7 <b>302 HB<\/b>.<br \/><b>Annealed at 815 \u00b0C:<\/b> Rm 655 MPa \u00b7 Rp0.2 425 MPa \u00b7 A 25.7 % \u00b7 Z 56.9 % \u00b7 <b>197 HB<\/b>.<br \/><b>Quenched from 845 \u00b0C + tempered at 540 \u00b0C:<\/b> Rm 1075 MPa \u00b7 Rp0.2 986 MPa \u00b7 A 15.5 % \u00b7 Z 56.9 % \u00b7 <b>311 HB<\/b>.<br \/><b>These are NOT specification minimums but typical measurements<\/b> on small specimens. The <b>302 HB<\/b> normalised figure in particular <b>directly contradicts<\/b> the European source\u2019s <b>\u2248190 HB<\/b> for the same temperature \u2014 the cause is section size and real cooling rate.<\/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;\">EN 10269 \u2014 Elevated-Temperature Proof Strength for Bolting (d \u226460 mm)<\/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>Room temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rm <b>860\u20131060 MPa<\/b> \u00b7 Rp0.2 <b>\u2265730 MPa<\/b> \u00b7 A <b>\u226514 %<\/b> \u00b7 KV at +20 \u00b0C <b>\u226550 J<\/b> \u00b7 at \u221240 \u00b0C <b>\u226540 J<\/b> \u00b7 at 100 \u00b0C <b>\u226527 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%;\"><b>Rp0.2 versus temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">50 \u00b0C <b>720<\/b> \u00b7 100 \u00b0C <b>702<\/b> \u00b7 150 \u00b0C <b>677<\/b> \u00b7 200 \u00b0C <b>640<\/b> \u00b7 250 \u00b0C <b>602<\/b> \u00b7 300 \u00b0C <b>562<\/b> \u00b7 350 \u00b0C <b>518<\/b> \u00b7 400 \u00b0C <b>475<\/b> \u00b7 450 \u00b0C <b>420<\/b> \u00b7 500 \u00b0C <b>375 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>How to read it<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>At 400 \u00b0C the yield is 65 % of its room-temperature value, and at 500 \u00b0C only 51 %.<\/b> These are the numbers used in design calculation, and they explain why a bolt loses its preload when hot<\/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 ASTM counterpart<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">For ASTM <b>A193 B7<\/b> the commonly quoted limit is <b>450 \u00b0C (840 \u00b0F) continuous service<\/b>; above that, <b>A193 B16<\/b> (Cr-Mo-V) is recommended. Lower bound: no impact testing required down to <b>\u221229 \u00b0C (\u221220 \u00b0F)<\/b>; colder than that, use <b>A320 L7<\/b><\/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;\">ASTM A193 B7 \u2014 Mechanical Minimums by Diameter<\/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>\u226464 mm (2\u00bd in)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp0.2 <b>\u2265725 MPa (105 ksi)<\/b> \u00b7 Rm <b>\u2265860 MPa (125 ksi)<\/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>64\u2013100 mm (2\u00bd\u20134 in)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Rp0.2 <b>\u2265655 MPa (95 ksi)<\/b> \u00b7 Rm <b>\u2265795 MPa (115 ksi)<\/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>100\u2013180 mm (4\u20137 in)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Rp0.2 <b>\u2265515 MPa (75 ksi)<\/b> \u00b7 Rm <b>\u2265690 MPa (100 ksi)<\/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>Ductility<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Elongation <b>\u226516\u201318 %<\/b> \u00b7 reduction of area <b>\u226550 %<\/b> (the source gives this as a range)<\/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>Hardness<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">The source gives a <b>235\u2013331 HB<\/b> band \u2014 <b>single-sourced<\/b>. <b>Confirm from the current edition<\/b>; we publish no single ceiling figure on this page<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Heat treatment requirement<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Quenched in oil (or water) and tempered at a MINIMUM of 593 \u00b0C (1100 \u00b0F).<\/b> <b>That minimum tempering temperature is no accident<\/b> \u2014 it is set precisely to stay above the temper embrittlement band (375\u2013575 \u00b0C)<\/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>What B7M changes<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Maximum 22 HRC<\/b>, for NACE MR0175 sour service compliance. The price is <b>lower strength<\/b>: the same bolt, softer. Saying \u201clet us substitute B7M for B7, it is the same steel anyway\u201d <b>means reducing the design load<\/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;\">Physical Properties<\/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 0 740 674\" 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\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 up to 16 mm diameter<\/text><rect x=\"16\" y=\"50\" width=\"652.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"675.0\" y=\"62\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">1100<\/text><rect x=\"16\" y=\"68\" width=\"533.5\" height=\"15\" fill=\"#12303f\"\/><text x=\"556.5\" y=\"80\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">900<\/text><text x=\"16\" y=\"108\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 16-40 mm diameter<\/text><rect x=\"16\" y=\"114\" width=\"592.7\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"615.7\" y=\"126\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">1000<\/text><rect x=\"16\" y=\"132\" width=\"444.5\" height=\"15\" fill=\"#12303f\"\/><text x=\"467.5\" y=\"144\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">750<\/text><text x=\"16\" y=\"172\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 40-100 mm diameter<\/text><rect x=\"16\" y=\"178\" width=\"533.5\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"556.5\" y=\"190\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">900<\/text><rect x=\"16\" y=\"196\" width=\"385.3\" height=\"15\" fill=\"#12303f\"\/><text x=\"408.3\" y=\"208\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">650<\/text><text x=\"16\" y=\"236\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 100-160 mm diameter<\/text><rect x=\"16\" y=\"242\" width=\"474.2\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"497.2\" y=\"254\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">800<\/text><rect x=\"16\" y=\"260\" width=\"326.0\" height=\"15\" fill=\"#12303f\"\/><text x=\"349.0\" y=\"272\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">550<\/text><text x=\"16\" y=\"300\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 160-250 mm diameter<\/text><rect x=\"16\" y=\"306\" width=\"444.5\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"467.5\" y=\"318\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">750<\/text><rect x=\"16\" y=\"324\" width=\"296.4\" height=\"15\" fill=\"#12303f\"\/><text x=\"319.4\" y=\"336\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">500<\/text><text x=\"16\" y=\"364\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM A193 Grade B7 \u00b7 bolting, up to 63.5 mm (2\u00bd in) diameter<\/text><rect x=\"16\" y=\"370\" width=\"509.7\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"532.7\" y=\"382\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">860<\/text><rect x=\"16\" y=\"388\" width=\"429.7\" height=\"15\" fill=\"#12303f\"\/><text x=\"452.7\" y=\"400\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">725<\/text><text x=\"16\" y=\"428\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM A193 Grade B7 \u00b7 bolting, 66.7-101.6 mm (2\u215d-4 in) diameter<\/text><rect x=\"16\" y=\"434\" width=\"471.2\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"494.2\" y=\"446\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">795<\/text><rect x=\"16\" y=\"452\" width=\"388.2\" height=\"15\" fill=\"#12303f\"\/><text x=\"411.2\" y=\"464\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">655<\/text><text x=\"16\" y=\"492\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM A193 Grade B7 \u00b7 bolting, 104.8-177.8 mm (4\u215b-7 in) diameter<\/text><rect x=\"16\" y=\"498\" width=\"409.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"432.0\" y=\"510\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">690<\/text><rect x=\"16\" y=\"516\" width=\"305.3\" height=\"15\" fill=\"#12303f\"\/><text x=\"328.3\" y=\"528\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">515<\/text><text x=\"16\" y=\"556\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM A193 Grade B7M \u00b7 low-hardness bolting for sour service, up to 101.6 mm (4 in)<\/text><rect x=\"16\" y=\"562\" width=\"409.0\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"432.0\" y=\"574\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">690<\/text><rect x=\"16\" y=\"580\" width=\"326.0\" height=\"15\" fill=\"#12303f\"\/><text x=\"349.0\" y=\"592\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">550<\/text><text x=\"16\" y=\"620\" font-size=\"12.5\" font-weight=\"bold\" fill=\"#12303f\" font-family=\"Arial,Helvetica,sans-serif\">ASTM A320 Grade L7 \u00b7 low-temperature bolting, up to 63.5 mm (2\u00bd in) diameter<\/text><rect x=\"16\" y=\"626\" width=\"509.7\" height=\"15\" fill=\"#7fa8bd\"\/><text x=\"532.7\" y=\"638\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">860<\/text><rect x=\"16\" y=\"644\" width=\"429.7\" height=\"15\" fill=\"#12303f\"\/><text x=\"452.7\" y=\"656\" font-size=\"11.5\" fill=\"#5b7180\" font-family=\"Arial,Helvetica,sans-serif\">725<\/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 10083-3 \u00b7 42CrMo4 \u00b7 +QT \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;\">900 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1100-1300<\/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;\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 16-40 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;\">750 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1000-1200<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">11% 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;\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 40-100 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;\">650 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">900-1100<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">12% 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;\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 100-160 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;\">550 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">800-950<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">13% 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;\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +QT \u00b7 160-250 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;\">500 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">750-900<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">14% 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;\">EN 10083-3 \u00b7 42CrMo4 \u00b7 +A (soft annealed)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">241 HBW max<\/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;\">ASTM A193 Grade B7 \u00b7 bolting, up to 63.5 mm (2\u00bd in) diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">321 HBW \/ 35 HRC max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">725 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">860 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">16% 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;\">ASTM A193 Grade B7 \u00b7 bolting, 66.7-101.6 mm (2\u215d-4 in) diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">321 HBW \/ 35 HRC max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">655 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">795 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">16% 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;\">ASTM A193 Grade B7 \u00b7 bolting, 104.8-177.8 mm (4\u215b-7 in) diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">321 HBW \/ 35 HRC max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">515 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">690 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">18% 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;\">ASTM A193 Grade B7M \u00b7 low-hardness bolting for sour service, up to 101.6 mm (4 in)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">235 HBW \/ 99 HRB max \u00b7 100% of the batch is hardness tested<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">550 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">690 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">16-18% min (by size)<\/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;\">ASTM A320 Grade L7 \u00b7 low-temperature bolting, up to 63.5 mm (2\u00bd in) diameter<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">321 HBW \/ 35 HRC max<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">725 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">860 min<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">16% min<\/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;\">EVERY ROW IS A SPECIFICATION MINIMUM &#8211; a guaranteed floor, not a typical value. The akma_mpa and cekme_mpa columns carry ONLY the MPa value; the ksi equivalents are in the akma_ksi and cekme_ksi columns. The EN rows depend on DIAMETER: the same material gives a lower yield in a heavy section because hardenability is limited. The ASTM A193 \/ A320 rows are BOLTING specifications and include a hardness CEILING; the EN rows have no hardness ceiling.<\/b> In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. The EN 10083-3 rows and the ASTM A193 rows CANNOT be compared with each other: one is a structural quench-and-temper table, the other a bolting specification, and they carry different test-piece and measurement rules. B7 and B7M are made from the same material; the difference is the heat treatment target and the hardness ceiling. Sour service requires B7M. In the EN +QT rows the yield falls as the diameter grows: 900 MPa at 16 mm, 500 MPa at 250 mm. That is the numerical expression of the hardenability limit of 4140. Typical annealed tensile\/yield values have NOT been put in the table: every source found for them derives from the same ASM database, so the four-independent-source requirement is not met (see the omissions list).<\/div>\n<\/div>\n<p><!-- \/dm-diy-sert --><\/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;\">Physical Properties \u00b7 AISI 4140 \/ 42CrMo4<\/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>Density<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>7.85 g\/cm\u00b3<\/b> (European source) \u00b7 <b>7.83 g\/cm\u00b3<\/b> (US source, as specific gravity). <b>The difference is negligible; use 7.85<\/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>Modulus of elasticity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>\u2248217 GPa<\/b> at room temperature, falling to <b>164 GPa<\/b> with temperature. <b>[conflict]<\/b> A US source gives <b>33 Mpsi (\u2248228 GPa)<\/b>. <b>Do not treat the modulus as constant<\/b> \u2014 the drop must be accounted for in hot service calculations<\/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>Thermal expansion<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">European source <b>10.5 \u2192 14.4 \u00d7 10\u207b\u2076\/K<\/b> (\u2212100 to 600 \u00b0C). US source <b>12.2 \u00d7 10\u207b\u2076\/K<\/b> (20\u2013100 \u00b0C, oil hardened and tempered). <b>The two sources are consistent<\/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>Thermal conductivity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>45.1 \u2192 34.4 W\/m\u00b7K<\/b> (falling with temperature). US source <b>42.7 W\/m\u00b7K<\/b> at 100 \u00b0C. <b>About three times that of stainless<\/b> \u2014 which means heat escapes into the workpiece instead of burning the tool<\/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>Specific heat<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>423 \u2192 587 J\/kg\u00b7K<\/b> (rising with temperature). US source <b>473 J\/kg\u00b7K<\/b> for 20\u2013200 \u00b0C<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Electrical resistivity<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>0.231 \u2192 0.806 \u03a9\u00b7mm\u00b2\/m<\/b>, i.e. <b>23.1 \u2192 80.6 \u00b5\u03a9\u00b7cm<\/b> (strongly rising with temperature). US source <b>22 \u00b5\u03a9\u00b7cm<\/b> at 20 \u00b0C<\/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>Melting point<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>\u22481416 \u00b0C<\/b> (2580 \u00b0F) \u2014 single source<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>MAGNETIC BEHAVIOUR<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Ferromagnetic.<\/b> Magnetic in every heat treatment condition. It cannot be used in any application requiring non-magnetic material \u2014 the absolute dividing line between this steel and austenitic stainless<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b8\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Welding \u2014 Preheat Is MANDATORY<\/h4>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>4140 is a difficult steel to weld, and that is the material\u2019s single biggest practical limitation.<\/b> The reason can be given in one word: <b>hardenability<\/b>. The heat-affected zone (HAZ) is austenitised and then cooled by the surrounding cold mass <b>at quenching rates<\/b>. The result is <b>untempered, hard, brittle martensite<\/b> \u2014 and combined with the hydrogen present, it produces <b>cold (delayed) cracking<\/b>.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Carbon equivalent \u2014 calculate it yourself<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\">The measure of weldability is the <b>IIW carbon equivalent<\/b>:<br \/><b>CE = C + Mn\/6 + (Cr + Mo + V)\/5 + (Ni + Cu)\/15<\/b><br \/><b>Applying that formula to 4140\u2019s specification chemistry gives (this is a CALCULATED value, not taken from a published source):<\/b> lower corner (C 0.38 \u00b7 Mn 0.75 \u00b7 Cr 0.80 \u00b7 Mo 0.15) <b>\u22480.70<\/b>; nominal (C 0.40 \u00b7 Mn 0.88 \u00b7 Cr 0.95 \u00b7 Mo 0.20) <b>\u22480.78<\/b>; upper corner (C 0.43 \u00b7 Mn 1.00 \u00b7 Cr 1.10 \u00b7 Mo 0.25) <b>\u22480.87<\/b>.<br \/><b>The common engineering threshold is CE = 0.45<\/b>, above which preheat is considered necessary. <b>4140 sits at nearly twice that.<\/b> Which is why preheat is not a recommendation but <b>a requirement<\/b>. For comparison, <b>4130<\/b> carries about 0.30 % carbon and its CE is markedly lower \u2014 <b>if a welded structure is required, that is the right steel<\/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 4140 \u2014 THE PUBLISHED RANGES CONFLICT; WE GIVE THEM ALL<\/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 \u2014 four separate published ranges<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Source A:<\/b> \u226412.7 mm <b>205\u2013260 \u00b0C<\/b>, 12.7\u201350 mm <b>316\u2013371 \u00b0C<\/b> \u00b7 <b>Source A\u2019s lower alternative:<\/b> \u226412.7 mm <b>177 \u00b0C<\/b>, 12.7\u201325 mm <b>232 \u00b0C<\/b>, 25\u201350 mm <b>260 \u00b0C<\/b> \u00b7 <b>Source B:<\/b> <b>288\u2013427 \u00b0C<\/b> for thick components \u00b7 <b>Source C (general):<\/b> <b>170\u2013350 \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%;\"><b>Honest summary<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>The published range spans 175 \u00b0C to 425 \u00b0C in total.<\/b> Publishing a single number would be misleading. <b>The correct value depends on thickness, degree of restraint, hydrogen level and filler choice<\/b> and is established in weld procedure qualification<\/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 apply preheat<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>The heat must pass through the ENTIRE section<\/b> and extend <b>at least 75 mm (3 in) in every direction<\/b> from the joint. Heating only the top of the bead is not preheat<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Interpass temperature<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Must be held at or above the preheat temperature.<\/b> Do not let it fall \u2014 every drop is a quenching cycle<\/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>Filler metal<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">Primary: <b>ER80S-D2<\/b>. Undermatching (for toughness): <b>ER70S-2<\/b>. <b>If the part will be fully re-quenched and tempered after welding<\/b>, a filler matching the base metal chemistry is required. <b>WARNING: do not use a filler that OVERMATCHES the tensile strength<\/b> \u2014 ductility falls and cracking risk in the weld metal rises<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Hydrogen control (DHT)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Immediately after welding, <b>hold the part at preheat temperature<\/b> and wrap it in ceramic insulation: <b>30 minutes to 1 hour per 25 mm of thickness<\/b>. This lets hydrogen diffuse out and is <b>the single most effective measure against delayed cracking<\/b>. Also <b>use low-hydrogen electrodes and respect the baking and storage discipline<\/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>PWHT (stress relief)<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>566\u2013677 \u00b0C<\/b> (1050\u20131250 \u00b0F), <b>\u22481 hour per 25 mm<\/b>. Recommended for thicknesses above 3 mm (\u215b in)<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>PWHT on ALREADY heat-treated (4140 HT) parts<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Must stay BELOW the original tempering temperature<\/b>, otherwise the part loses hardness. <b>[UNIT ERROR WARNING]<\/b> One publication writes this as \u201c<b>60 \u00b0F (15 \u00b0C) below<\/b>\u201d \u2014 <b>a 60 \u00b0F DIFFERENCE is 33 \u00b0C, not 15 \u00b0C<\/b>. The source\u2019s own conversion is wrong. <b>In practice, stay 30\u201355 \u00b0C below<\/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>Cooling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>Cool slowly using heating blankets.<\/b> Rapid cooling means embrittlement and hydrogen-induced cracking. <b>But after PWHT, pass quickly through 575\u2013375 \u00b0C<\/b> \u2014 remember the temper embrittlement section. These two look contradictory; <b>they are not, they describe different temperature bands<\/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;\">What actually goes wrong<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. No preheat, or insufficient preheat.<\/b> Single most common cause of failure in 4140. The part looks hot at the moment of welding, but <b>the rest of the mass is cold<\/b> and quenches the HAZ within seconds. The result is a <b>delayed crack<\/b> appearing days later \u2014 in transit, at assembly, or on first loading.<br \/><b>2. Hydrogen.<\/b> Damp electrodes, oily surfaces, rust, paint residue and humid air are all hydrogen sources. Hard HAZ + hydrogen + residual stress is <b>precisely the recipe for cold cracking<\/b>. <b>Bake the electrodes, clean the joint, apply the post-weld hold (DHT).<\/b><br \/><b>3. Skipping post-weld heat treatment.<\/b> Without PWHT the HAZ remains <b>untempered martensite<\/b>. Test its hardness and you will read 50+ HRC \u2014 and on a NACE-scope part that is a direct non-conformance (limit 22 HRC).<br \/><b>4. Overmatching filler.<\/b> Weld metal significantly stronger than the base metal <b>reduces ductility<\/b> and moves the crack into the weld metal.<br \/><b>5. Fabricating welded parts from pre-hardened bar.<\/b> If you bought 28\u201332 HRC \u201c4140 HT\u201d bar, welding <b>destroys the heat treatment condition<\/b> locally. <b>A welded 4140 part must be re-quenched and tempered as a whole after welding<\/b> \u2014 or the design must be based on the weakest region.<\/p>\n<h4 id=\"dm-b9\" 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>4140 is one of the better-machining quenched-and-tempered steels \u2014 but that depends entirely on the delivery condition.<\/b> Annealed (\u2248195 HB) it is a comfortable material; quenched and tempered (300+ HB) it is a different job altogether.<\/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<\/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 rating<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>61 %<\/b> general \u00b7 <b>70 %<\/b> in the annealed condition (against B1112 free-machining steel = 100 %) \u2014 <b>single source<\/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>Hardness by delivery condition<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Annealed <b>\u2248195 HB<\/b> \u00b7 Normalised <b>240\u2013300 HB<\/b> \u00b7 Quenched and tempered <b>230\u2013340 HB<\/b>. <b>The speeds below are for nominal (annealed \/ normalised) hardness and must be reduced substantially above 300 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>Turning<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>225\u2013305 m\/min<\/b> (740\u20131000 sfm) \u2014 carbide. <b>Thick CVD coating, medium-toughness grade<\/b> recommended<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>Milling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>140\u2013190 m\/min<\/b> (460\u2013620 sfm) \u2014 a general-purpose carbide grade is adequate<\/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>Drilling<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>90\u2013120 m\/min<\/b> (300\u2013390 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>Parting and grooving<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Parting <b>105\u2013145 m\/min<\/b> (340\u2013480 sfm) \u00b7 grooving <b>125\u2013170 m\/min<\/b> (410\u2013560 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>Assumptions<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\">These speeds assume <b>stable clamping, quality material, short tool overhang and nominal hardness<\/b>. <b>If those conditions are not met, reduce the speed<\/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 thermal advantage<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\">Thermal conductivity is <b>\u224843\u201345 W\/m\u00b7K<\/b> \u2014 about three times that of stainless. <b>Heat escapes into the part instead of accumulating in the tool.<\/b> This is largely the physical reason 4140 machines comfortably compared with stainless<\/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 sulphur-bearing variant<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;background:#F7FAFB;\"><b>42CrMoS4<\/b> machines noticeably better (chip breaking and tool life). <b>The price is transverse toughness<\/b> \u2014 see the chemistry section<\/td>\n<\/tr>\n<tr>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;font-weight:700;color:#12303f;width:42%;\"><b>After hardening<\/b><\/td>\n<td style=\"padding:7px 12px;border-top:1px solid #eceff1;\"><b>Finishing operations are required after hardening<\/b> (grinding, hard turning). If tolerances are critical, <b>add heat treatment distortion to your machining allowance<\/b><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/div>\n<h4 id=\"dm-b10\" style=\"font-size:19px;font-weight:700;color:#12303f;margin:30px 0 10px;line-height:1.35;\">Corrosion, Hydrogen and Sour Service \u2014 the \u201cNOT Stainless\u201d Section<\/h4>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Atmospheric and aqueous corrosion<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>4140\u2019s corrosion resistance is, in practice, that of plain carbon steel.<\/b> Its 0.80\u20131.10 % chromium is <b>not enough<\/b> to form a passive film \u2014 the threshold is around <b>10.5 %<\/b>. Molybdenum contributes nothing meaningful to corrosion either; both are <b>hardenability elements<\/b>.<br \/><b>Consequence:<\/b> 4140 parts <b>must be protected<\/b> \u2014 paint, zinc or zinc-nickel plating, phosphating plus oil, cadmium (in aerospace), nitriding or chrome plating. <b>And the protection itself brings the risk described in the next section.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">HYDROGEN EMBRITTLEMENT \u2014 the number one failure mode of high-strength 4140<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>As a steel\u2019s strength rises, its susceptibility to hydrogen embrittlement increases SHARPLY.<\/b> The practical threshold is taken as roughly <b>1000\u20131100 MPa tensile strength<\/b> or <b>32\u201335 HRC<\/b> \u2014 and 4140 works right at and above that band.<br \/><b>Where the hydrogen comes from:<\/b> <b>acid pickling<\/b>, <b>electroplating<\/b> (zinc, cadmium, chromium), <b>phosphating<\/b>, <b>electrolytic cleaning<\/b>, <b>cathodic protection<\/b>, and in service <b>the corrosion reaction itself<\/b>.<br \/><b>The mechanism is insidious for this reason:<\/b> the part looks normal coming out of the plating line, its hardness is correct, it passes a tensile test. <b>Fracture arrives days later, under static load, without warning<\/b> \u2014 which is why it is called <b>delayed fracture<\/b>.<br \/><b>The countermeasure \u2014 post-plating bake-out:<\/b> a long, low-temperature bake carried out <b>immediately after<\/b> plating lets trapped hydrogen diffuse out. <b>The governing specifications are ASTM B850, ASTM F1940 and ISO 4042.<\/b> <b>The bake temperature and duration could NOT be independently verified in this research<\/b> \u2014 we publish no numbers. <b>The temperature, the duration and the maximum permissible delay after plating must be taken from the applicable specification according to the part\u2019s strength class.<\/b> <b>What you must not do is take a random temperature\/time pair from a distributor sheet and apply it.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Sulphide stress cracking and NACE MR0175<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>In environments containing hydrogen sulphide (H\u2082S), 4140 suffers sulphide stress cracking (SSC).<\/b> The mechanism is a sibling of hydrogen embrittlement: the corrosion reaction generates hydrogen, the sulphide ion <b>prevents<\/b> that hydrogen from recombining into molecules and escaping, and the hydrogen enters the steel.<br \/><b>The NACE MR0175 \/ ISO 15156-2 rule is unambiguous: for carbon and low alloy steels, a maximum of 22 HRC (approximately 250 HV \/ 237 HBW), and the material must be in the QUENCHED AND TEMPERED condition.<\/b><br \/><b>That single rule governs the whole design of 4140 in sour service.<\/b> Reaching 22 HRC means, per the tempering curve above, tempering roughly in the <b>620\u2013650 \u00b0C<\/b> band, which brings Rm down to around <b>900\u20131000 MPa<\/b>. In other words <b>none of 4140\u2019s high-strength conditions can be used in sour service<\/b>.<br \/><b>And the 22 HRC limit is a LOCAL limit:<\/b> weld metal, HAZ, cold-formed threads, rolled thread roots and any non-decarburised surface layer must each <b>individually<\/b> be below it. <b>A part whose average hardness is 20 HRC can have a 45 HRC HAZ and be non-conforming.<\/b> The ASTM <b>A193 B7M<\/b> and <b>A320 L7M<\/b> grades exist precisely to meet this limit.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Where not to use it<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. Wet or outdoor service without protection.<\/b> It rusts. Coating, paint or oil is mandatory. <b>2. Sour service above 22 HRC.<\/b> A NACE violation and a real cracking risk. <b>3. Welded structures where heat treatment is impossible.<\/b> CE \u22480.78; if preheat and PWHT cannot be applied, <b>choose 4130<\/b>. <b>4. Impact-loaded parts tempered in the 260\u2013575 \u00b0C band.<\/b> The embrittlement bands. <b>5. Sections above \u2300100 mm requiring full through-hardening.<\/b> The core will not harden; <b>4340<\/b> is needed. <b>6. Anywhere non-magnetic material is required.<\/b> It is ferromagnetic. <b>7. High-strength parts electroplated without a bake-out.<\/b> Delayed fracture. <b>8. Continuous service above 500 \u00b0C.<\/b> The yield falls to half its room-temperature value at 500 \u00b0C; 4140 is not a creep steel.<\/p>\n<h4 id=\"dm-b11\" 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 customer wants material certified to 42CrMo4 and we have SAE 4140 in stock. 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. The two specifications overlap but are NOT IDENTICAL, and non-conformance is possible in both directions.<\/b><br \/><b>The most critical divergence is manganese.<\/b> SAE 4140 requires <b>0.75\u20131.00 %<\/b>, EN 42CrMo4 requires <b>0.60\u20130.90 %<\/b>. <b>The common band is only 0.75\u20130.90 %.<\/b> So a heat at Mn = 0.96 % that conforms perfectly to SAE 4140 <b>does not conform to 42CrMo4<\/b>. The second divergence is chromium: SAE <b>0.80\u20131.10 %<\/b>, EN <b>0.90\u20131.20 %<\/b> \u2014 common band <b>0.90\u20131.10 %<\/b>. A SAE heat at Cr = 0.85 % again <b>fails 42CrMo4<\/b>.<br \/><b>It also works in reverse:<\/b> the EN carbon band is <b>0.38\u20130.45 %<\/b>, SAE\u2019s is <b>0.38\u20130.43 %<\/b>. A European heat at C = 0.44 % meets 42CrMo4 but <b>fails SAE 4140<\/b> (it meets SAE <b>4142<\/b>). And <b>EN demands a cleaner steel<\/b>: P \u22640.025 % and S \u22640.035 %, against SAE\u2019s \u22640.035 % and \u22640.040 %.<br \/><b>The good news is that<\/b> many mills know this and deliberately produce narrow-band heats that <b>satisfy both specifications at once<\/b> \u2014 \u201cdual certified 4140\/42CrMo4\u201d is a common product. <b>But that is a choice, not a rule<\/b>, and it does not hold for every heat.<br \/><b>What to do:<\/b> pull the mill certificate for the heat you hold and <b>compare the Mn, Cr, C, P and S lines against the 42CrMo4 bands ONE BY ONE<\/b>. If all conform, dual certification can be issued. If not, <b>supply the customer with 42CrMo4<\/b>. \u201cIt is the same steel\u201d 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;\">The shaft must carry 600 MPa yield and will take impact loads. What tempering temperature? The supplier suggests 400 \u00b0C.<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>400 \u00b0C is definitely wrong, and for two compounding reasons. The supplier\u2019s recommendation was read off a hardness table without looking at the toughness data.<\/b><br \/><b>First reason \u2014 toughness does not improve at all.<\/b> Look at the full tempering curve: Charpy energy is <b>27 J at 150 \u00b0C, 26 J at 350 \u00b0C, 26 J at 400 \u00b0C, 27 J at 450 \u00b0C<\/b>. Across a three-hundred-degree range <b>toughness is effectively CONSTANT<\/b>. So tempering at 400 \u00b0C drops the yield from 1620 to 1440 MPa and <b>buys no toughness whatsoever<\/b>. Toughness only opens up <b>above 500 \u00b0C<\/b>: <b>31 J at 500 \u00b0C, 42 J at 550 \u00b0C, 75 J at 600 \u00b0C, 114 J at 650 \u00b0C<\/b> \u2014 roughly a <b>fourfold<\/b> difference.<br \/><b>Second reason \u2014 400 \u00b0C sits squarely inside the embrittlement band.<\/b> The reversible <b>temper embrittlement band is 375\u2013575 \u00b0C<\/b>. In that band phosphorus, tin, antimony and arsenic diffuse to and segregate at prior austenite grain boundaries; <b>the ductile-to-brittle transition temperature rises and fracture toughness falls<\/b>. And the most dangerous aspect of this damage is that <b>it barely changes hardness or tensile strength at all<\/b> \u2014 so it passes your routine quality control without a flag and reveals itself only <b>in the field, under impact loading<\/b>.<br \/><b>The right answer:<\/b> for 600 MPa yield with impact loading, <b>temper in the 620\u2013650 \u00b0C band<\/b>. Per the curve, 650 \u00b0C gives you <b>Rp0.2 \u2248870 MPa, Rm \u2248980 MPa and KV \u2248114 J<\/b> \u2014 well above the target yield with four times the toughness.<br \/><b>And do one more thing:<\/b> after tempering, <b>cool rapidly through 575 \u2192 375 \u00b0C<\/b> (in oil for heavy sections). Furnace cooling <b>re-creates on the way down<\/b> the embrittlement you dissolved at 650 \u00b0C. This one sentence explains a large share of \u201cthe heat treatment was correct but the part came out brittle\u201d cases. <b>Remember the curve above comes from a \u230010 mm specimen<\/b>; validate on a trial piece for your own section.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Is it true that \u201c4140 already contains chromium, so it behaves almost like stainless in mildly corrosive service\u201d?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>No, and this misunderstanding generates real costs.<\/b> 4140 contains <b>0.80\u20131.10 %<\/b> chromium. For a steel to behave <b>passively<\/b> \u2014 to build a self-repairing chromium oxide film \u2014 the threshold is about <b>10.5 % chromium<\/b>. 4140 sits at <b>one tenth<\/b> of that. The chromium here is present <b>for hardenability, not for corrosion<\/b>: it delays the pearlite transformation so that an oil quench produces martensite deeper into the section. The same applies to molybdenum.<br \/><b>In practice 4140 rusts like plain carbon steel.<\/b> Protection is <b>mandatory<\/b>: paint, zinc or zinc-nickel plating, phosphate and oil, cadmium in aerospace, or nitriding.<br \/><b>And here the real trap begins.<\/b> Most of those protections are <b>electrolytic<\/b>, which means they <b>charge the steel with hydrogen<\/b> \u2014 as does acid pickling. A high-strength 4140 part (roughly <b>above 1000\u20131100 MPa<\/b> or <b>above 32\u201335 HRC<\/b>) is <b>sharply susceptible<\/b> to that hydrogen. The part leaves the plating line sound, its hardness is correct, it passes test \u2014 and <b>days later it fractures under static load without warning<\/b>. This is called <b>delayed fracture<\/b> and it is the number one field failure of high-strength 4140.<br \/><b>So frame the decision this way:<\/b> if the part is wet, outdoors or in a chemical environment, choose between \u201c4140 + coating\u201d and a stainless (for example <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/17-4ph-1-4542-aisi-630\/\">17-4 PH<\/a>) <b>not on first cost<\/b> but on coating life, bake-out discipline and hydrogen risk. If you settle on 4140, <b>make post-plating bake-out an order requirement<\/b> and state which specification governs it (ASTM B850, F1940 or ISO 4042). <b>Do not let anyone apply an arbitrary temperature and time.<\/b><\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">We use the same heat treatment recipe but hardness drifts 6\u20138 HRC from lot to lot. Is the furnace faulty?<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>Most likely it is not the furnace \u2014 it is THE STEEL ITSELF. And it is a drift the standard permits.<\/b><br \/><b>Look at the Jominy table.<\/b> The hardenability band ISO 683-2 accepts for 42CrMo4 at <b>15 mm<\/b> from the quenched end is <b>37\u201358 HRC<\/b>. That is a <b>21 HRC spread<\/b>, and both 37 and 58 are <b>fully conforming<\/b>. At 20 mm the band is <b>34\u201356<\/b>, at 25 mm <b>32\u201353 HRC<\/b>. So <b>two conforming heats can come out more than 20 HRC apart at the same point after the same cycle in the same furnace<\/b>. The 6\u20138 HRC you are seeing is a perfectly ordinary slice of that band.<br \/><b>The cause is the freedom inside the chemistry:<\/b> C 0.38\u20130.45 %, Mn 0.60\u20130.90 %, Cr 0.90\u20131.20 %, Mo 0.15\u20130.30 %. A heat at the top corner of those bands genuinely hardens differently from one at the bottom. Add <b>grain size<\/b> variation on top (the table assumes grain size \u22655).<br \/><b>The fix has three steps.<\/b> First and most important: <b>buy \u201c4140H\u201d, not \u201c4140\u201d.<\/b> H grades widen the chemistry slightly but <b>narrow and GUARANTEE the Jominy band<\/b>. If you do your own heat treatment, this is the product you should be buying, and most buyers do not know it. Second: <b>run a trial piece from every lot<\/b> and set the tempering temperature from it, rather than using one fixed recipe. Third: <b>record the actual C, Mn, Cr and Mo from each mill certificate<\/b>; after a few lots you will have your own hardenability correlation.<br \/><b>And check two more things:<\/b> the austenitising soak should be <b>1 hour per 25 mm of section<\/b>, and the tempering soak <b>at least 2 hours AFTER the load reaches temperature<\/b>. The difference between \u201cthe furnace is at temperature\u201d and \u201cthe part is at temperature\u201d is worth several HRC on its own in heavy sections.<\/p>\n<p style=\"margin:18px 0 6px;font-size:15px;font-weight:700;color:#12303f;line-height:1.5;\">Common data sheet errors \u2014 check before you order<\/p>\n<p style=\"margin:0 0 12px;font-size:15px;line-height:1.75;\"><b>1. \u201c4140 = 42CrMo4\u201d \u2014 INCOMPLETE.<\/b> The Mn bands overlap only between 0.75 and 0.90 %; the Cr bands only between 0.90 and 1.10 %; EN carbon reaches 0.45 % while SAE stops at 0.43 %; EN P and S limits are tighter. <b>Dual-certified heats are common but not guaranteed.<\/b><br \/><b>2. A single \u201c4140 yield strength\u201d figure is published.<\/b> Per EN 10083-3 the same steel yields <b>750 MPa at \u230016 mm and 500 MPa at \u2300250 mm<\/b> \u2014 a <b>33 % difference<\/b>. Any mechanical value without a stated section is <b>meaningless<\/b>.<br \/><b>3. Tempering tables published without a section size.<\/b> The full curve above comes from a <b>\u230010 mm specimen<\/b>. <b>The Rm 2200 MPa \/ 57 HRC row can NEVER be reached at the core of a \u2300100 mm bar.<\/b><br \/><b>4. \u201cAs-quenched 4140: Rm 2200 MPa\u201d written as a product property.<\/b> Untempered martensite is <b>not a usable delivery condition<\/b> \u2014 it cracks. Note also that this row carries the lowest Charpy value in the table, <b>24 J<\/b>.<br \/><b>5. \u201c4140 is not subject to temper embrittlement\u201d \u2014 CONTRADICTED.<\/b> One producer writes this; against it stands an independent technical report titled <b>\u201cTemper Embrittlement in 4140 Seamless Tubing\u201d<\/b>, and a trade association recommending <b>no tempering cycle below 1100 \u00b0F (593 \u00b0C)<\/b>. <b>The truth: molybdenum REDUCES susceptibility but does not confer IMMUNITY.<\/b><br \/><b>6. Two different embrittlement phenomena conflated.<\/b> <b>Tempered martensite embrittlement is at 260\u2013370 \u00b0C and IRREVERSIBLE<\/b>; <b>temper embrittlement is at 375\u2013575 \u00b0C and REVERSIBLE<\/b> (dissolved above 575 \u00b0C in minutes). <b>Different mechanism, different remedy.<\/b><br \/><b>7. If a 4140 sheet mentions \u201c475 \u00b0C embrittlement\u201d, that sheet is copy-paste.<\/b> 475 \u00b0C embrittlement concerns steels with <b>15 % chromium and above<\/b>; it has nothing to do with 4140\u2019s 1 %.<br \/><b>8. \u201cTemper at 400 \u00b0C for a good balance\u201d \u2014 WRONG.<\/b> The Charpy data is <b>flat at 26\u201328 J between 150 and 450 \u00b0C<\/b>. In that band you sacrifice strength and <b>gain no toughness at all<\/b>. Toughness only opens up above 500 \u00b0C.<br \/><b>9. Stress relief given as \u201c60 \u00b0F (15 \u00b0C) below the original tempering temperature\u201d \u2014 UNIT ERROR.<\/b> <b>A 60 \u00b0F DIFFERENCE is 33 \u00b0C.<\/b> A published source\u2019s own conversion is wrong.<br \/><b>10. Normalised hardness given as a single number.<\/b> For the same 870 \u00b0C one source writes <b>302 HB<\/b> and another <b>\u2248190 HB<\/b> \u2014 the difference comes from section and real cooling rate. Likewise <b>the modulus of elasticity is given as constant<\/b>: it falls from <b>217 GPa to 164 GPa<\/b>, and a US source writes <b>\u2248228 GPa<\/b>.<br \/><b>11. Tempering tables diverge by 6\u20138 HRC between publishers<\/b>, and Jominy values are given as single numbers \u2014 the standard\u2019s band at 15 mm is <b>37\u201358 HRC<\/b>. <b>Make none of them an acceptance criterion.<\/b><br \/><b>12. \u201c4140 contains chromium, therefore it resists corrosion\u201d \u2014 WRONG.<\/b> The passivity threshold is <b>10.5 % Cr<\/b>; 4140 has <b>0.80\u20131.10 %<\/b>. <b>It rusts.<\/b><br \/><b>13. Preheat given as a single number.<\/b> The published range spans <b>175\u2013425 \u00b0C<\/b> and depends on thickness, restraint, hydrogen level and filler.<br \/><b>14. The post-weld hydrogen hold (DHT) step is omitted.<\/b> Holding the part at preheat temperature for <b>30 minutes to 1 hour per 25 mm<\/b> after welding is the single most effective step against delayed cracking.<br \/><b>15. \u201cA B7 stud is a 4140 stud\u201d \u2014 INCOMPLETE.<\/b> The A193 B7 chemistry is a <b>C 0.38\u20130.48 %<\/b> band covering <b>4140, 4142 and 4145 together<\/b>. B7 is a <b>performance class<\/b>.<br \/><b>16. Comparison with 8620 made on the wrong axis.<\/b> 8620 is a <b>carburising steel<\/b> (C 0.18\u20130.23 %); 4140 is a <b>through-hardening steel<\/b>.<br \/><b>17. The NACE 22 HRC limit read as an \u201caverage hardness\u201d.<\/b> The limit is <b>LOCAL<\/b>: weld metal, HAZ, rolled thread roots and cold-formed regions must <b>each<\/b> be below 22 HRC.<br \/><b>18. 42CrMoS4 offered as a drop-in for 42CrMo4.<\/b> Sulphur improves machinability but <b>reduces transverse ductility and impact toughness<\/b>.<br \/><b>19. \u201c4140\u201d assumed to be the same as \u201c4140H\u201d.<\/b> <b>H grades guarantee the Jominy band<\/b>; plain 4140 does not. If you do your own heat treatment, the difference shows up as <b>6\u20138 HRC of lot-to-lot drift<\/b>.<\/p>\n<p><!-- 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;\">THREE SEPARATE CRITERIA, EACH READ FROM ONE SOURCE FAMILY. (1) CHEMISTRY: the band for all three grades is taken from ASTM A29 \/ SAE J404, so nickel, chromium and molybdenum are compared under the same specification logic. (2) DEPTH OF HARDENABILITY: for 4140 and 4340 the condition letter &#8211; section &#8211; tensile band mapping of THE SAME STANDARD (AS 1444-1996) is used; the criterion is the question &#8216;up to what section can the same tensile band be reached&#8217;, because that mapping holds the section and the test rule constant. (3) AMS COVERAGE: for each grade, the numbers verified from SAE title records together with their melting and cleanliness requirements. Hardness or tensile figures from DIFFERENT sources have NOT been placed side by side.<\/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;\">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;\">Toughness<\/th>\n<th style=\"padding:7px 9px;text-align:left;font-size:12px;color:#12303f;background:#F2F6F8;border:1px solid #eceff1;\">Ams kapsami<\/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 4140<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">G41400 (aircraft quality E4140 = G41406)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">1.7225 \/ 42CrMo4 (close equivalent, the bands are not identical)<\/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;\">NOT SPECIFIED (residual element)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.80-1.10%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.15-0.25%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">In the AS 1444 condition table only the R\/S conditions (700-930 MPa tensile) hold at a 250 mm section; the highest condition, W, is limited to 20-30 mm (1000-1230 MPa).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Izod 27-54 J in the AS 1444 table; KV 35 J minimum in EN 10083-3 +QT (16-250 mm).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6349 \u00b7 6381 \u00b7 6382 \u00b7 6395 \u00b7 6529 \u00b7 6452. There is NO VAR (vacuum arc remelted) AMS number; the highest cleanliness requirement is the &#8216;special aircraft-quality cleanliness&#8217; wording of 6529.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Shafts and spindles, gears, hydraulic cylinder rods, die holders, ASTM A193 B7 studs and A320 L7 bolting, drilling components.<\/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 4340<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">G43400 (aircraft quality E4340 = G43406)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">The W.Nr. assignment is CONTRADICTORY between sources (1.6565 \/ 40NiCrMo8-4 is given by some, 1.6511 \/ 36CrNiMo4 and 1.6582 \/ 34CrNiMo6 by others)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.38-0.43%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">1.65-2.00%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.70-0.90%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">0.20-0.30%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">In the AS 1444 condition table condition T (850-1000 MPa tensile) holds at a 250 mm section and the range extends up to condition X (1150-1300 MPa at 30 mm). In tables where THE SAME PUBLISHER applies THE SAME STANDARD in THE SAME FORMAT, 4340 stays one condition above 4140. (The sources are not fully unanimous on this point; see the contradictions list.)<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Izod 21-54 J in the AS 1444 table; nickel raises low-temperature toughness, which is why the ASTM A320 class with a -101 \u00b0C Charpy requirement, L43, is based on 4340.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">6359 \u00b7 6409 \u00b7 6414 \u00b7 6415 \u00b7 6454 \u00b7 6484 (plus 6456 welding wire, 4340Mod). THERE ARE VAR-REQUIRED AMS NUMBERS (6414 and 6454) and 6409 carries a &#8216;special aircraft quality cleanliness&#8217; requirement.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">Aircraft landing gear, transmission and drive shafts, heavy-section crankshafts and gears, high-strength fasteners, ASTM A320 L43 low-temperature bolting.<\/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;\">No W.Nr. equivalent verified across four sources was found<\/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%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.40-0.60%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">0.20-0.30%<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Its nickel and chromium levels sit between 4140 and 4340. No numerical section-versus-strength table could be verified across four independent sources, so NO NUMBER IS GIVEN in this row.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Izod 41 J in the annealed condition (AZoM, ASM-derived). No four-source figure was found for the quenched-and-tempered condition.<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">6322 (bars, forgings, rings) \u00b7 6323 (mechanical tubing) \u00b7 6325 \u00b7 6327 (bars, forgings) \u00b7 6358 (sheet, strip, plate) \u00b7 7452 (bolts and screws) \u00b7 7456 (studs) \u00b7 7496 (flash welded rings).<\/td>\n<td style=\"padding:7px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">Axles, tool joints, bits and reamer bodies, aircraft engine bolts, piston rods.<\/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;\">Nikel farki<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(255,255,255,.72);color:#3d5260;\">The one decisive chemical difference is NICKEL. In 4140 nickel is NOT specified; in 8740 it is 0.40-0.70%; in 4340 it is 1.65-2.00%. Nickel forms no carbide, strengthens the ferrite in solid solution and lowers the transformation temperature of austenite; the practical consequences are two: deeper hardening at the same carbon level, and higher low-temperature toughness. Carbon is 0.38-0.43% in all three grades, so the MAXIMUM ATTAINABLE HARDNESS is similar in all three. THE DIFFERENCE IS NOT IN THE HARDNESS BUT IN HOW DEEP INTO THE SECTION THAT HARDNESS REACHES.<\/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 farki<\/td>\n<td style=\"padding:6px 9px;border:1px solid #eceff1;background:rgba(247,250,251,.78);color:#3d5260;\">The difference that decides the order in practice: 4340 has AMS numbers with a VAR (vacuum arc remelted) requirement (6414 for bars\/forgings\/tubing, 6454 for sheet\/strip\/plate) and also 6409 with a &#8216;special aircraft quality cleanliness&#8217; requirement. 4140 HAS NO VAR-REQUIRED AMS NUMBER; its highest cleanliness requirement is the &#8216;special aircraft-quality cleanliness&#8217; wording that AMS 6529 places on normalized bar. A specification that calls for remelted material cannot be met with 4140.<\/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;\">ALL THREE ARE QUENCH-AND-TEMPER STEELS AND NONE OF THEM IS STAINLESS. Corrosion protection, hydrogen embrittlement measures (the AMS 2759\/9 bake after plating) and the 22 HRC limit of NACE MR0175 \/ ISO 15156-2 apply to all three alike. 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 comparison is made WITHOUT INVENTING NUMBERS: no hardenability figure is given in the 8740 row, because no section-versus-strength table could be found across four independent sources. The hardenability difference between 4140 and 4340 is read from the section assignments that one publisher gives for the two grades in the AS 1444 condition tables. One publisher (Vulcan) gives the SAME table for both grades; that contradiction is recorded. The consequence of the nickel difference is not &#8216;harder&#8217; but &#8216;hard deeper in&#8217;. All three grades have carbon in the same band. The difference in AMS coverage (a VAR-required number exists or does not) is the most concrete discriminator in practice.<\/div>\n<\/div>\n<p><!-- \/dm-diy-kars --><\/p>\n<p><!-- \/dm-zengin --><\/p>\n<div class=\"dm-benzer\" 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-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\/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\/aermet-100\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">AerMet 100<\/a> &nbsp;\u00b7&nbsp; <a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/maraging-300\/\" style=\"color:#24BEE5;font-weight:600;text-decoration:none;\">Maraging 300<\/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-ld --><script type=\"application\/ld+json\">{\"@context\":\"https:\/\/schema.org\",\"@type\":\"WebPage\",\"name\":\"AISI 4140\",\"url\":\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/\",\"inLanguage\":\"en\",\"description\":\"AISI\/SAE 4140 (UNS G41400 \/ W.Nr. 1.7225 \/ EN 42CrMo4 \/ JIS SCM440) is a medium-carbon, through-hardening chromium-molybdenum alloy structural 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 4140\",\"description\":\"AISI\/SAE 4140 (UNS G41400 \/ W.Nr. 1.7225 \/ EN 42CrMo4 \/ JIS SCM440) is a medium-carbon, through-hardening chromium-molybdenum alloy structural steel.\",\"inDefinedTermSet\":{\"@type\":\"DefinedTermSet\",\"name\":\"Defence Metal - metals and alloys\",\"url\":\"https:\/\/www.defencemetal.com\/\"},\"alternateName\":[\"UNS G41400\",\"W.Nr. 1.7225\"],\"identifier\":[{\"@type\":\"PropertyValue\",\"propertyID\":\"UNS\",\"value\":\"G41400\"},{\"@type\":\"PropertyValue\",\"propertyID\":\"Werkstoffnummer\",\"value\":\"1.7225\"}]}}<\/script><!-- \/dm-ld --><\/p>\n","protected":false},"excerpt":{"rendered":"<p>AISI 4140 \/ UNS G41400 \/ AMS 6349 \/ AMS 6382 DEFENCE METAL AISI 4140 UNS G41400 (aircraft quality E4140 = G41406) \u00b7 W.Nr. 1.7225 \u00b7 EN 42CrMo4 (free-machining variant 42CrMoS4 = 1.7227) \u00b7 ASTM A29 \/ SAE J404 band: C 0.38-0.43% &#8211; Mn 0.75-1.00% &#8211; Si 0.15-0.35% &#8211; Cr 0.80-1.10% &#8211; Mo 0.15-0.25% &#8211; &hellip; <\/p>\n<p class=\"link-more\"><a href=\"https:\/\/www.defencemetal.com\/index.php\/en\/aisi-4140\/\" class=\"more-link\"><span class=\"screen-reader-text\"> &#8220;AISI 4140&#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 4140 \/ UNS G41400 \/ AMS 6349 \/ AMS 6382 | Defence Metal","_yoast_wpseo_metadesc":"AISI 4140 (UNS G41400) \u2014 AMS 6349 and AMS 6382 equivalents. Chromium-molybdenum alloy steel supplied as bar, flat, plate, sheet, tube and forgings.","inspiro_hide_title":false,"inspiro_hide_featured_image":false,"footnotes":""},"dm_sektor":[10,9,14,15],"class_list":["post-3529","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 4140 \/ UNS G41400 \/ AMS 6349 \/ AMS 6382 | Defence Metal<\/title>\n<meta name=\"description\" content=\"AISI 4140 (UNS G41400) \u2014 AMS 6349 and AMS 6382 equivalents. 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