High Strength
Quenched-and-tempered conditions can provide high tensile and yield strength for loaded engineering components.
A practical commercial and technical guide to EN19 standards, properties, supply conditions, heat treatment, applications, testing and purchase requirements.
Reviewed for grade-designation accuracy, condition-dependent mechanical properties, heat-treatment context, testing requirements and responsible equivalent-grade guidance.
EN19 round bar is a chromium-molybdenum engineering alloy steel commonly selected for transmission shafts, gears, spindles, axles, pins, crankshafts, heavy-duty fasteners and other components exposed to high stress, shock or torsional loading. The grade is valued for its combination of strength, toughness, fatigue resistance and response to quenching and tempering.
The name EN19 is widely used in Indian engineering and purchasing discussions, but it is a legacy British designation. A technically complete enquiry should state the required standard, delivery condition, bar diameter, mechanical-property level, heat-treatment route, testing scope and component application. For product-specific supply information, visit the EN19 Round Bars page.
EN19 is commonly associated with 709M40 under later British specifications. 42CrMo4 / 1.7225 and SAE 4140 are frequently used as close international cross-references, but no substitution should be approved from the grade name alone. The controlling chemistry, condition, size, mechanical properties and inspection requirements must match the purchase specification.
EN19 originated as a British alloy-steel designation under BS 970:1955. Later supplier data commonly associates it with 709M40. European 42CrMo4 and American SAE/AISI 4140 belong to a similar chromium-molybdenum alloy family and are often used as comparison grades, but their chemistry limits and standard rules are not identical in every edition.
| System | Common Designation | Buyer Guidance |
|---|---|---|
| Legacy British designation | EN19 | State the applicable BS 970 edition or customer specification. |
| Later British designation | 709M40 / 709M40T | The suffix or condition matters because properties depend on heat treatment and ruling section. |
| European comparison | 42CrMo4 / material number 1.7225 | Confirm EN/EN ISO chemistry, condition and dimensional product standard. |
| American comparison | SAE/AISI 4140 | Use only after reviewing the specified chemistry, hardenability and property requirements. |
| French comparison | 42CD4 | Treat as a technical cross-reference, not an automatic substitute. |
| Swedish comparison | SS 2244 | Verify the current standard and supply condition before ordering. |
Purchasing rule: Write the exact standard, grade, condition and required properties on the purchase order. A general “EN19 equivalent” instruction can lead to differences in chemistry, hardness, impact performance or heat-treatment response.
The following composition is a BS 970: Part 1:1983 reference for 709M40 / EN19. Other standards and supplier data sheets may publish slightly different ranges, so the approved standard and Material Test Certificate must control the order.
| Element | Reference Range | Engineering Relevance |
|---|---|---|
| Carbon (C) | 0.36–0.44% | Supports strength, hardness and heat-treatment response. |
| Silicon (Si) | 0.10–0.35% | Acts as a deoxidiser and contributes to strength. |
| Manganese (Mn) | 0.70–1.00% | Contributes to hardenability and strength. |
| Chromium (Cr) | 0.90–1.20% | Improves hardenability, wear response and strength. |
| Molybdenum (Mo) | 0.20–0.35% | Supports hardenability, high-temperature tempering response and resistance to temper embrittlement. |
| Nickel (Ni) | 0.40% maximum | Residual or controlled limit in the cited specification. |
| Phosphorus (P) | 0.035% maximum | Controlled because excessive phosphorus may reduce toughness. |
| Sulphur (S) | 0.040% maximum | Controlled for cleanliness, toughness and fatigue-sensitive applications. |
EN19 properties cannot be represented by one universal strength or hardness value. The result depends on bar diameter, ruling section, delivery condition, prior processing, austenitising, quenching and tempering. The table below shows representative published values for S, T and U conditions.
| Condition | Tensile Strength | Yield Strength | Elongation | Impact | Hardness |
|---|---|---|---|---|---|
| S | 775–925 MPa | 555 MPa minimum | 13% minimum | 22 J | 223–277 HB |
| T | 850–1000 MPa | 680 MPa minimum | 13% minimum | 50 J | 248–302 HB |
| U | 925–1000 MPa | 755 MPa minimum | 12% minimum | 42 J | 269–331 HB |
These rows are condition- and ruling-section-dependent supplier references, not guaranteed values for every EN19 bar. The purchase specification and certified test results determine acceptance.
Quenched-and-tempered conditions can provide high tensile and yield strength for loaded engineering components.
Chromium-molybdenum alloying supports a practical balance of strength, shock resistance and toughness when processed correctly.
EN19 is widely investigated for rotating and cyclically loaded components, subject to cleanliness, surface finish and design.
The grade has better through-hardening capability than plain medium-carbon steels, although larger sections still require ruling-section review.
The selected condition should match the buyer’s machining, forging and final heat-treatment sequence. Depending on availability and the approved specification, EN19 round bar may be discussed in the following conditions:
Jain Steels Group publishes a general round-bar diameter range of 25 mm to 66 mm. Final EN19 grade-size-condition availability is confirmed for each enquiry through the EN19 Round Bars product page.
EN19 is commonly heat treated by austenitising, quenching and tempering. Published supplier guidance for 709M40 lists hardening by reheating to approximately 860–890°C followed by oil quenching, with tempering generally in the 550–700°C range. 42CrMo4 references publish similar but not identical process windows.
These temperatures are reference windows, not a production instruction for every component. Section size, furnace uniformity, prior microstructure, quench severity, distortion allowance, target strength, impact toughness and final machining must be reviewed by a qualified metallurgist or heat-treatment specialist.
Used to reduce hardness, improve machinability and prepare material for extensive machining or further processing.
May be used to refine and equalise the structure before machining or final heat treatment, subject to the specification.
Develops the high-strength and toughness combination commonly associated with EN19 engineering components.
Can be considered for selected surfaces where a hard wear-resistant layer and tougher core are required.
May be considered for wear and fatigue-critical surfaces after appropriate core heat treatment and process approval.
May be used after rough machining or selected processes to reduce residual stress and improve dimensional stability.
EN19 is generally selected where a plain carbon-steel grade may not provide sufficient hardenability, strength or fatigue performance. Common applications include:
For rotating components exposed to torsion, bending and cyclic loading.
For through-hardened, induction-hardened or otherwise specified drive components subject to engineering approval.
For automotive, machinery and heavy-engineering components requiring strength and toughness.
For selected components exposed to repeated dynamic loading, where the drawing and heat-treatment plan specify EN19.
For bolts, studs, tie rods and pins requiring controlled strength and traceability.
For forged and machined parts used in machinery, oil and gas equipment and industrial assemblies.
Application suitability should be approved from the component design, required fatigue life, stress concentration, surface finish, heat-treatment response and inspection class. EN19 should not be selected only because it is described as “high tensile.”
Testing requirements should be agreed before order confirmation. Jain Steels Group’s Quality Assurance page describes chemistry verification, mechanical testing, hardness, microstructure, ultrasonic testing, magnetic-particle inspection and traceability controls.
| Test or Document | Purpose | What the Buyer Should Specify |
|---|---|---|
| Material Test Certificate | Provides heat identity, chemistry and agreed mechanical results. | Required certificate type, traceability and document language. |
| Chemical analysis | Confirms compliance with the ordered grade and standard. | Heat analysis, product analysis and permitted variation where applicable. |
| Tensile testing | Verifies tensile strength, yield strength and elongation. | Condition, ruling section, specimen location and acceptance values. |
| Hardness testing | Confirms supply condition or heat-treatment response. | HB, HRC or HV scale, sampling frequency and acceptance range. |
| Impact testing | Assesses toughness at the specified temperature. | Test temperature, specimen orientation, method and minimum energy. |
| Ultrasonic testing | Checks internal soundness against an agreed standard. | Applicable UT standard, quality class and reporting requirement. |
| MPI or surface inspection | Detects relevant surface and near-surface discontinuities. | Inspection stage, acceptance standard and finished surface condition. |
| Dimensional inspection | Checks diameter, length, ovality and straightness. | Tolerance standard, machining allowance and cut-length requirement. |
Use this checklist when requesting availability or comparing quotations:
State EN19, 709M40 or the exact approved equivalent together with the standard edition.
Provide raw-bar size, required length, cut tolerance, straightness and machining allowance.
Specify as rolled, annealed, normalized, quenched and tempered, peeled, turned or ground.
List tensile, yield, elongation, hardness, impact and applicable ruling-section requirements.
Explain whether the material will be forged, rough-machined, Q&T, induction hardened, nitrided or stress relieved.
Define MTC, UT, MPI, hardness, third-party inspection, marking and traceability requirements.
Share the drawing or identify whether the bar is for a shaft, gear, axle, spindle, fastener or forged component.
Provide quantity, delivery destination, required schedule, packaging and any phased delivery plan.
EN19 is a legacy British designation commonly associated with 709M40 chromium-molybdenum alloy steel. It is used for high-strength shafts, gears, pins and other engineering components, subject to the specified condition and heat treatment.
They are commonly used as close cross-references, but they are not automatic substitutes. Compare the governing chemistry, standard, product form, delivery condition, mechanical properties and inspection requirements.
Yes. EN19 is commonly processed or supplied in quenched-and-tempered conditions. The final cycle must be qualified for component geometry, section size, target strength, toughness and distortion limits.
Common uses include transmission shafts, gears, axles, spindles, crankshafts, high-tensile fasteners, pins and heavy engineering components.
Share the exact grade and standard, diameter, length, quantity, supply condition, application, mechanical requirements, heat-treatment plan, testing scope and delivery destination.
Continue to the EN19 product, round-bar, quality and enquiry pages required for a complete sourcing review.