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title: "1.7254 — Special steels for aviation and aerospace"
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Material number · Europe · 1 designation

# 1.7254

1.7254 is the material number of the grade also listed as J24056. It is a material in the category Special steels for aviation and aerospace. We list 1 designations recorded for this grade, in the standards UNS.

- ***Material no.* **1.7254****
- [*Category* **Special steels for aviation and aerospace · 39 grades**](/categories/special-steels-for-aviation-and-aerospace "Category: Special steels for aviation and aerospace · 39 grades")
- *Designations* **1**

[Search](/search "Steel grade search")[Inquiry](/inquiry?material=b0a43b6c-cfae-445c-b3bc-1d1866fd4e0b "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/material-no/1.7254.pdf "Datasheet as PDF")

## About Special steels for aviation and aerospace

Special steels for aviation and aerospace are engineered steels designed to provide controlled mechanical properties and reliable performance in demanding service. Their alloying and heat-treatment capabilities support components that require a combination of strength, toughness and fatigue resistance, including aircraft structures and engine parts.

This describes the material class as a whole. Always confirm the individual grade against the standard before ordering.

## Also known as

 1 designations · 1 standards · nothing hidden

This grade’s own name recorded in our sources as this grade’s own designation under that standard.

Indicative taken from a published cross-reference table; a close match, not a guarantee of interchangeability. Verify against the mill certificate before ordering.

Withdrawn designation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.

UNS United States · 1

- [J24056 Indicative](/materials/uns/j24056 "UNS J24056")

Every designation on file is listed — no truncation, no “+ n more”. Each one is itself a route that leads back here.

## Chemical composition

 8 elements on file · weight %

What this alloy is

Fe Cr Mn Si

Iron — the balance, never listed by a standard — 97.2 % Cr — 1 % Mn — 0.6 % Si — 0.4 % Traces & impurities · 0.8 %

Logarithmic scale, 0.01 % to 100 % — every value here compares directly, decade by decade.

| Element | % by weight |
|---|---|
| C | 0.23–0.28 |
| Si | 0.3–0.5 |
| Mn | 0.5–0.7 |
| P | 0.02 |
| S | 0.015 |
| Cr | 0.8–1.1 |
| Mo | 0.2–0.3 |
| Ni | 0.3 |

Carbon Silicon Manganese Phosphorus Sulfur Chromium Molybdenum Nickel

0.01 % 0.1 % 1 % 10 % 100 %

The scale is logarithmic, not the element’s raw share of the alloy — the only honest way to fit 0.01 % and 100 % in one picture, and it means every value here can be compared with every other.

| Element | As published source text, verbatim | Min% by weight | Max% by weight | Bound |
|---|---|---|---|---|
| C | 0,23-0,28 | 0.230 | 0.280 | Range |
| Si | 0,30-0,50 | 0.300 | 0.500 | Range |
| P | 0,02 | 0.020 | 0.020 | Exact |
| S | 0,015 | 0.015 | 0.015 | Exact |
| Cr | 0,80-1,10 | 0.800 | 1.100 | Range |
| Mn | 0,50-0,70 | 0.500 | 0.700 | Range |
| Ni | 0,3 | 0.300 | 0.300 | Exact |
| Mo | 0,20-0,30 | 0.200 | 0.300 | Range |

The published column is the source string byte-for-byte, decimal comma and all; Min and Max are the parsed bounds. Elements not listed have no value on file — they are omitted, never inferred.

## Predicted transformation temperatures

 computed from composition · °C

Predicted Ae3 810 °C

Predicted Ae1 746 °C

Predicted Acm 527 °C

Predicted Bs 542 °C

These four temperatures are a CALCULATION from this grade's own composition, using the published Li, Niebuhr, Meekisho & Atteridge (1998) model — never a measurement, and computed from the UPPER BOUND of each element's specified range, not a mid-range figure. Where this grade also has a measured transformation point (Ac1, Ac3, Ar1, Ar3) on file, it is shown separately, in Physical & mechanical properties, and is never replaced by the predicted figures here — Ae (predicted, equilibrium) and Ac/Ar (measured, on heating or cooling) are different physical quantities and can differ by tens of degrees; a mismatch between the two is not an error in either.

## Physical & mechanical properties

Density 7,85 g/cm³ Exact

An absent property means we hold no value for it — it is left out rather than estimated, interpolated from a neighbouring grade, or filled from a handbook. It does not mean the property is undefined for the material.

## Similar grades — and why

Selection rule, stated so you can disagree with it: same number class 1.7, a shared category, and a published range for Cr / Mn that overlaps this grade’s. These are neighbours in composition space — they are not equivalents, and none is claimed to be interchangeable with this grade.

[25CrMo4 1.7214

Cr 0,90-1,20 · Mn 0,50-0,80

- ΔCr 0.10
- ΔMn 0.05
- 29 designations](/materials/din-en/25crmo4 "25CrMo4")

## Looking for this grade under another name?

Search the catalogue by designation, material number or composition — every name on this page is itself a way in.

[Search](/search "Steel grade search")[Inquiry](/inquiry?material=b0a43b6c-cfae-445c-b3bc-1d1866fd4e0b "Inquiry")[**Datasheet as PDF** Print-ready A4 document **Generating …** **Download started** **Try again**](/materials/material-no/1.7254.pdf "Datasheet as PDF")
