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Steel C55E +A (Annealed)

Heat-treated state

EN C55E · AISI/SAE 1055 · GB 55

Softest supply condition; choose for heavy machining, cold forming or as a pre-condition before hardening.

Budget cost $

Values for the +A condition

Other C55E tempers and conditions

C55E is listed in 10 conditions; see the grade overview at C55E.

Compare all 10 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
+AThis page
Annealed
Softest supply condition; choose for heavy machining, cold forming or as a pre-condition before hardening.34062020190 HB—
Normalized
Uniform fine pearlitic structure for good machinability and predictable strength without quenching distortion.39076014225 HB—
Hot rolled
Cheapest bar/plate condition for parts that will be re-heat-treated after machining or for low-duty use.40072015210 HB—
Normalized and tempered
Pick when normalized strength is sufficient but residual stress and hardness scatter must be reduced before precision machining.40074015215 HB—
+QTDefault
Quenched and tempered
Standard engineering condition: best strength/toughness balance for shafts, keyed drive parts and wear plates up to ~40 mm section.5508501424 HRC—
+QT + induction surface hardened
Tough Q&T core with a hard wear-resistant skin — the classic choice for journal areas of shafts, pins and rollers.5608701258 HRC—
Stress relieved
Cold-drawn bar with residual stress removed to minimize bending/distortion during asymmetric machining.6007801020 HRC9.5 % IACS
Cold drawn
Close-tolerance bright bar with raised strength and good surface finish; use for shafts machined without further heat treatment.660820822 HRC—
Q&T to 28–32 HRC
Ordered when a specified through-hardness is required for gear blanks, spline shafts and moderately loaded wear parts.7409501230 HRC—
Q&T to 40–45 HRC
High-hardness condition for blades, wear strips, hand-tool bodies and springs in sections under ~25 mm; toughness drops sharply.1,1301,350942 HRC44 W/m·K

What is C55E +A?

C55E +A is C55E heat treated to +A — softest supply condition; choose for heavy machining, cold forming or as a pre-condition before hardening. C55E +A has a yield strength of 340 MPa (49.3 ksi) and a tensile strength of 620 MPa (89.9 ksi) — weaker than 76% of steel grades. Elongation at break is 20% and the elastic modulus is 210 GPa (30.5 Msi). C55E +A has a density of 7.84 g/cm³ (0.283 lb/in³), lighter than 78% of steel grades. It melts at 1,420°C (2,588 °F). +QT is the default condition FabDigit quotes; +A is available on request or by drawing note.

Limitations

  • Low fracture toughness — 50 MPa·√m (45.5 ksi·√in), worse than 86% of steel grades
  • Low strength — 340 MPa (49.3 ksi), worse than 76% of steel grades

C55E +A properties

Typical room-temperature values for C55E +A; 15 are specific to this condition. Other listed values are C55E reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

C55E +A has a density of 7.84 g/cm³ (0.283 lb/in³), lighter than 78% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.84 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,480°C2,696 °F

Mechanical16

C55E +A has a yield strength of 340 MPa (49.3 ksi) and a tensile strength of 620 MPa (89.9 ksi) — weaker than 76% of steel grades. Elongation at break is 20% and the elastic modulus is 210 GPa (30.5 Msi).

Elastic (Young's) Modulus210 GPa30.5 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)620 MPa89.9 ksi
Yield Strength (0.2% offset)340 MPa49.3 ksi
Elongation at Break20%
Reduction in Area45%
Compressive Strength850 MPa123 ksi
Shear Strength380 MPa55.1 ksi
Fatigue Strength (Endurance Limit)280 MPa40.6 ksi
Fracture Toughness (K_IC)50 MPa·√m45.5 ksi·√in
Charpy V-Notch Impact (RT)28 J20.7 ft·lbf
Hardness, Brinell190 HB
Hardness, Rockwell C24 HRC
Hardness, Vickers200 HV

Thermal6

C55E +A is rated for continuous service to 400°C (752 °F). It conducts heat at 46 W/m·K (26.6 BTU/hr·ft·°F), better than 71% of steel grades. Thermal expansion is 11.5 µm/m·K (6.39 µin/in·°F).

Thermal Conductivity46 W/m·K26.6 BTU/hr·ft·°F
Specific Heat Capacity470 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.5 µm/m·K6.4 µin/in·°F
Latent Heat of Fusion250 J/g107 BTU/lb
Max Service Temperature (continuous)400°C752 °F
Min Service Temperature-20°C-4 °F

Electrical3

C55E +A conducts electricity at 9 % IACS, better than 71% of steel grades.

Electrical Conductivity9 % IACS
Electrical Resistivity1.9×10⁻⁷ Ω·m7.48 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is not recommended (10/100), worse than 86% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.61 V
Corrosion ResistanceNot recommended10/100
Chemical Resistance SummaryRusts freely in humid air, water and chlorides; attacked by all acids; acceptable in dry oils, greases and neutral non-aqueous media. Requires oiling, phosphating, plating or paint for storage and service.

Sustainability4

Producing a kilogram of C55E +A takes about 25 MJ of energy and emits 2 kg of CO₂ — less than 82% of steel grades. Typical recycled content is 30%.

Embodied Energy (primary production)25 MJ/kg10,748 BTU/lb
Embodied Carbon (primary production)2 kg CO₂/kg
Embodied Water40 L/kg4.8 gal/lb
Typical Recycled Content30%

Manufacturability7

C55E +A's machinability is good (55/100, better than 62% of steel grades); weldability poor (30/100); formability fair (45/100).

MachinabilityGood55/100
Machinability Rating (AISI 1212 = 100 %)65%
WeldabilityPoor30/100
Formability (cold)Fair45/100
Brazeability / SolderabilityGood55/100
PolishabilityGood55/100
Anodizing Responsen/a — ferrous alloy; use blackening (oxide), phosphating, zinc plating or nitriding instead

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with C55E +A

Is C55E easy to machine?

Machine in +A or +N (≈55–65 % of 1212); above 30 HRC use coated carbide, rigid setups and reduced feeds — grind above 45 HRC.

Can C55E be welded?

Poor weldability (CE ≈ 0.7): preheat 250–350 °C, low-hydrogen consumables, slow cooling and post-weld tempering to avoid HAZ martensite cracking.

Can C55E be formed, bent or molded?

Cold forming limited to gentle bends in the annealed condition (r ≥ 2–3 t); hot forge at 1100–850 °C then normalize.

What surface finishes work on C55E?

No natural corrosion resistance — protect with black oxide, phosphate + oil, zinc/nickel plating or paint; hardened surfaces polish and hard-chrome plate well.

C55E chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
C0.52 – 0.60.55
Si≤ 0.40.25
Mn0.6 – 0.90.75
PE-quality: controlled P≤ 0.03—
SE-quality: controlled S≤ 0.04—
Crresidual≤ 0.4—
Niresidual≤ 0.4—
Moresidual≤ 0.1—
Cr+Mo+Nisum of residuals per EN 10083-2≤ 0.63—
Febalance—

C55E +A — frequently asked

What is C55E +A used for?

C55E +A is typically used for machine shafts, gears, springs and wear parts. In short: higher strength than C45; spring and wear grade; poor weldability at 0.55 % C.

What is the yield strength of C55E +A?

C55E +A has a typical yield strength of 340 MPa (49.3 ksi) and a tensile strength of 620 MPa (89.9 ksi) — weaker than 76% of steel grades. Strength varies by condition: see the 10 listed tempers.

Is C55E +A easy to machine?

Reasonably — machinability is rated good (55/100, better than 62% of steel grades). Machine in +A or +N (≈55–65 % of 1212); above 30 HRC use coated carbide, rigid setups and reduced feeds — grind above 45 HRC.

Can C55E +A be welded?

Not readily — weldability is rated poor (30/100). Poor weldability (CE ≈ 0.7): preheat 250–350 °C, low-hydrogen consumables, slow cooling and post-weld tempering to avoid HAZ martensite cracking.

What surface finishes work on C55E +A?

No natural corrosion resistance — protect with black oxide, phosphate + oil, zinc/nickel plating or paint; hardened surfaces polish and hard-chrome plate well.

Can C55E +A be formed, bent or molded?

Cold forming limited to gentle bends in the annealed condition (r ≥ 2–3 t); hot forge at 1100–850 °C then normalize.

What is the maximum service temperature of C55E +A?

C55E +A is rated for continuous use to about 400°C (752 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Sources

  1. EN 10083-2: Steels for quenching and tempering — Non-alloy steels — CEN (2006)
  2. EN 10277 / EN 10025 bright and hot-rolled product conditions — CEN (2018)
  3. ASM Handbook Vol.1: Properties and Selection — Irons, Steels and High-Performance Alloys (AISI 1055) — ASM International (1990)
  4. Machinery's Handbook, machinability ratings — Industrial Press (2020)
  5. ISO 18265 hardness conversion tables — ISO (2013)
  6. Mysteel / carbon bar price series and 1688 — Mysteel, SMM (2026)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.