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AISI / SAE · United States · 40 designations

9310RH

9310RH is a designation in AISI / SAE for the material held under material number 1.6657, also listed as 14NiCrMo13-4. It is a material in the category Special steels for aviation and aerospace. We list 40 designations recorded for this grade, in the standards DIN / EN, UNS, AISI / SAE, ASTM, BS, AFNOR, UNE, SAE AMS, JIS, GOST, UNI, ČSN, PN, MSZ, BDS and ÖNORM.

If you came for one of these

The most-used names for this grade.

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

40 designations · 16 standards · nothing hidden
This grade’s own namerecorded in our sources as this grade’s own designation under that standard.
Indicativetaken from a published cross-reference table; a close match, not a guarantee of interchangeability. Verify against the mill certificate before ordering.
Withdrawndesignation no longer current — a separate column from the two above, so a name can be same grade and withdrawn at once.

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

Iron — the balance, never listed by a standard — 94.5 %Ni — 3.3 %Cr — 1 %Mn — 0.4 %Traces & impurities · 0.8 %

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

Element% by weight
0.11–0.17
≤ 0.4
0.3–0.6
0.025
0.035
0.8–1.1
0.2–0.3
3–3.5
CarbonSiliconManganesePhosphorusSulfurChromiumMolybdenumNickel
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.

ElementAs publishedsource text, verbatimMin% by weightMax% by weightBound
C0,11-0,170.1100.170Range
Si≤0,400.400Max
P0,0250.0250.025Exact
S0,0350.0350.035Exact
Cr0,80-1,100.8001.100Range
Mn0,30-0,600.3000.600Range
Ni3,00-3,503.0003.500Range
Mo0,20-0,300.2000.300Range

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

This grade's composition falls outside the published model's validated range (a low-alloy composition window), so no transformation temperature is predicted here.

Physical & mechanical properties

Density7,85g/cm³Exact
Transformation point Ac1700°CExact
Transformation point Ac3810°CExact · Ac3(Acm)
Transformation point Ar3400°CExact · Ar3(Arcm)
Transformation point Ar1350°CExact
Weldabilitydifficult to weldAs published: hard weldability.
Flake sensitivitysusceptibleAs published: predisposed
Temper brittlenessnot susceptibleAs published: not predisposed

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.

Properties by condition

8 conditions · 36 values
By delivery stateTreated to improve shearabilitysource steelnumber
Delivery stateHB
Treated to improve shearability255
By delivery stateSoft annealedsource steelnumber
Delivery stateHB
Soft annealed241
By delivery stateTreated to hardness rangesource steelnumber
Delivery stateHB
Treated to hardness range187 – 241
By delivery stateTreated to ferrite-pearlite structure and hardness rangesource steelnumber
Delivery stateHB
Treated to ferrite-pearlite structure and hardness range166 – 217
By dimensionQuenching and drawingsource splav
DimensionmmRmN/mm²ReN/mm²A5%Z%KCUkJ/m²
Ø 1511308351250980
By delivery stateno delivery state statedsource splav
Delivery stateHB
(annealing) , GOST 4543-71269
At temperatureno delivery state statedsource splav
Temperature°CDensityg/cm³Elastic modulusGPaThermal expansion coefficient10^-6/KThermal conductivityW/(m·K)
207.95200
1007.9316511.736
2007.914112.236
3007.8612.735
4007.8313913.135
5007.813.534
6007.7613.933
70032
80030
At temperatureno delivery state statedsource steelnumber
Temperature°CRmN/mm²
2001200

Every figure holds only for the condition on its own row. Values are never merged across conditions or across sources, never averaged, and never interpolated between two rows. An em dash means no value on file — never zero. Figures are converted to the unit in the column header; the source’s own wording is kept and shown where the two differ.

Heat treatment

Supply condition

  • Soft annealingSteel product

Conditions the standard permits on delivery. No temperature or medium is published for these, so no order and no alternation is implied.

Source: www.caishuku.com

Similar grades — and why

Selection rule, stated so you can disagree with it: same number class 1.6, a shared category, and a published range for Ni / Cr 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.

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.