JIANGSU LIANGYI Co., Ltd

AMS 6512 vs 6514 vs 6515 vs 6520 The complete 18Ni maraging steel specification map

Six SAE specifications. Four alloys. Two axes. The specification number tells you almost nothing on its own — and the most common substitution error in maraging procurement comes from assuming it does.

Published Last reviewed Reading time 15 minutes Author Jiangsu Liangyi engineering team
The 30-second answer

AMS 6511 is the 18Ni 200 grade. AMS 6512 is the 250. AMS 6514 is the 300. AMS 6515 is the 350. Those four cover bars, forgings, mechanical tubing and rings.

AMS 6520 and AMS 6521 are not new grades at all. They are the 250 and 300 alloys in sheet, strip and plate form. Same chemistry, different product form, different specification number.

So this family is not six materials. It is four alloys on a strength ladder, crossed with two product-form routes. Choose the rung first, then choose the form. Reversing that order is what produces the errors described below.

Key facts

  • AMS 6512 is the 18Ni 250 grade, UNS K92890, nominal 18Ni-7.8Co-4.9Mo-0.40Ti-0.10Al.
  • AMS 6514 is the 18Ni 300 grade, UNS K93120, nominal 18.5Ni-9.0Co-4.9Mo-0.65Ti-0.10Al.
  • AMS 6515 is the 18Ni 350 grade, UNS K93540, nominal 18.5Ni-12.0Co-4.9Mo-1.40Ti-0.10Al. It is the strongest, not an intermediate grade.
  • AMS 6511 is the 18Ni 200 grade, UNS K92810, nominal 18Ni-8.5Co-3.2Mo-0.20Ti-0.10Al.
  • AMS 6520 is the same alloy as AMS 6512, supplied as sheet, strip and plate.
  • AMS 6521 is the same alloy as AMS 6514, supplied as sheet, strip and plate.
  • Titanium content is what sets the grade: 0.20% at 200, 0.40% at 250, 0.65% at 300, 1.40% at 350.
  • All six specifications deliver material in a soft condition. None delivers a hardened part.
  • Standard aging cycle for the 200, 250 and 300 grades is approximately 480 °C for three to six hours, air cooled.
  • Fracture toughness falls roughly four-fold from the 200 grade to the 350 grade.

1. Why the specification number quietly misleads you

Line up the four wrought specifications in numerical order and something convenient happens. AMS 6511 is the 200 grade, 6512 is the 250, 6514 is the 300, 6515 is the 350. Ascending number, ascending strength. Engineers notice this within about ten minutes of working with the family, and it quietly becomes a mental shortcut.

The pattern is a coincidence, and it fails in three places.

It fails at AMS 6520 and 6521, which carry higher numbers than every wrought specification but sit back at the 250 and 300 chemistry. It fails at 6513, which is not a maraging bar specification at all, so the sequence is not continuous. And it fails hardest in the direction people actually use it — reading a number off a legacy drawing and inferring a grade instead of looking it up.

A check worth running

Secondary sources sometimes describe AMS 6515 as a lower grade than AMS 6514, or describe AMS 6512 as the 200 grade. Neither is correct. AMS 6515 was introduced to cover UNS K93540 — the 350 grade, the strongest and least tough member of the family, and AMS 6512 covers the 250 grade under UNS K92890.

Before relying on any comparison table, including this one, check the grade against the UNS number in the specification itself. UNS numbers identify the alloy unambiguously; specification numbers only identify the document.

2. Two axes, not one list

The useful mental model is a grid, not a ranking.

18Ni maraging AMS specification grid by strength grade and product form A four-by-two grid. Rows are strength grades 350, 300, 250 and 200. Columns are product form. In the wrought column, from top: AMS 6515 at 350, AMS 6514 at 300, AMS 6512 at 250, AMS 6511 at 200. In the flat product column only two cells are filled: AMS 6521 at 300 and AMS 6520 at 250. No specification exists for flat product at the 350 or 200 grades. PRODUCT FORM Bar · Forging · Tubing · Ring Sheet · Strip · Plate STRENGTH GRADE 350 AMS 6515 UNS K93540 · 1.40 Ti no specification 300 AMS 6514 UNS K93120 · 0.65 Ti AMS 6521 same alloy as 6514 250 AMS 6512 UNS K92890 · 0.40 Ti AMS 6520 same alloy as 6512 200 AMS 6511 UNS K92810 · 0.20 Ti no specification Titanium content rises up the grid. Product form changes across it. Nothing else moves.
Figure 1. The 18Ni maraging AMS family plotted on its two real axes. AMS 6520 and 6521 are not additional grades — they are the flat-product route to rungs already occupied by AMS 6512 and AMS 6514.

The vertical axis is the strength grade, set by cobalt, molybdenum and above all titanium. Titanium drives Ni3Ti precipitation during aging, so it is the element that moves you up the ladder: 0.20% at the 200 grade, 0.40% at 250, 0.65% at 300, and 1.40% at 350. Nickel barely changes across the whole family. Titanium changes by a factor of seven.

The horizontal axis is the product form, and it determines which specification number you are permitted to write. Bars, forgings, mechanical tubing, flash welded rings and forging stock live under 6511, 6512, 6514 and 6515. Sheet, strip and plate live under 6520 and 6521. No specification covers both. The delivery condition differs across that axis too: the wrought specifications are supplied annealed, the flat-product specifications are supplied solution heat treated.

Once the grid is in your head, most of the confusion in this family dissolves. A drawing that says AMS 6520 beside a forging callout is not a tolerance question — it is a specification that does not cover the part.

3. The six specifications

Nominal compositions and product-form scopes below follow the published SAE International specification titles and scope statements. These are nominal values, not the permitted ranges inside the purchased document.

AMS 651118Ni 200

AMS 6511 is the SAE specification for 18Ni maraging steel, 200 grade, in bar, forging, mechanical tubing, flash welded ring and forging stock form.

UNS
K92810
Nominal
18Ni · 8.5Co · 3.2Mo · 0.20Ti · 0.10Al
Melt
Double vacuum melted
Condition
Annealed
Aged UTS
≈1450 MPa / 210 ksi

The toughness grade. Lowest strength, by far the highest fracture toughness. Its 2023 revision added an explicit stress corrosion cracking precaution and pyrometry requirements — a signal worth reading.

AMS 651218Ni 250

AMS 6512 is the SAE specification for 18Ni maraging steel, 250 grade, in bar, forging, mechanical tubing, flash welded ring and forging stock form.

UNS
K92890
Nominal
18Ni · 7.8Co · 4.9Mo · 0.40Ti · 0.10Al
Melt
Consumable electrode vacuum melted
Condition
Annealed
Aged UTS
≈1760 MPa / 255 ksi

The workhorse. Premium aircraft quality, through-hardening without quenching. The best strength-to-toughness balance in the family and the default for damage-tolerant structure. For available forging forms, size ranges and lead times, see our AMS 6512 open die forgings and seamless rolled rings page.

AMS 651418Ni 300

AMS 6514 is the SAE specification for 18Ni maraging steel, 300 grade, in bar, forging, mechanical tubing, ring and forging stock form.

UNS
K93120
Nominal
18.5Ni · 9.0Co · 4.9Mo · 0.65Ti · 0.10Al
Melt
Consumable electrode vacuum melted
Condition
Annealed
Aged UTS
≈2000 MPa / 290 ksi

Strength-led selection. Titanium rises to 0.65%, which lifts tensile strength and costs toughness. Correct where the design is strength-critical rather than crack-growth-critical. See our AMS 6514 forging page.

AMS 651518Ni 350

AMS 6515 is the SAE specification for 18Ni maraging steel, 350 grade — the highest-strength wrought grade in the family, introduced to cover UNS K93540.

UNS
K93540
Nominal
18.5Ni · 12.0Co · 4.9Mo · 1.40Ti · 0.10Al
Melt
Double vacuum melted
Condition
Annealed
Aged UTS
≈2400 MPa / 348 ksi

The ceiling. 12% cobalt and 1.40% titanium make this a genuinely different alloy, not a hotter version of the 300. Narrow processing window, low toughness, unforgiving of aging error.

AMS 6520250 · flat

AMS 6520 is the SAE specification for the 250-grade alloy in sheet, strip and plate form — the same chemistry as AMS 6512.

Alloy
Same as AMS 6512 (250)
Nominal
18Ni · 7.8Co · 4.9Mo · 0.40Ti · 0.10Al
Melt
Consumable electrode melted
Condition
Solution heat treated
Typical use
Booster cases, pressure vessels

Check status before use. Written for large booster rocket cases and pressure vessels that through-harden without quenching. Its current revision carries SAE stabilized status — maintained for legacy use, not intended for new design.

AMS 6521300 · flat

AMS 6521 is the SAE specification for the 300-grade alloy in sheet, strip and plate form — the same chemistry as AMS 6514.

Alloy
Same as AMS 6514 (300)
Nominal
18.5Ni · 9.0Co · 4.9Mo · 0.65Ti · 0.10Al
Melt
Consumable electrode melted
Condition
Solution heat treated
Typical use
Flat-product structure

Flat product, 300 grade. An old specification with a long reaffirmation history. Check its current status before invoking it on a new programme.

4. Master comparison matrix

Table 1 — 18Ni maraging AMS specifications by grade, product form, melt route and delivery condition. Compositions are nominal values taken from published SAE specification titles. The two highlighted rows are the same alloy under two specification numbers.
SpecGradeUNS TiCo Product formDelivery condition
AMS 6511200K928100.20%8.5%Bar / forging / tube / ringAnnealed
AMS 6512250K928900.40%7.8%Bar / forging / tube / ringAnnealed
AMS 6514300K931200.65%9.0%Bar / forging / tube / ringAnnealed
AMS 6515350K935401.40%12.0%Bar / forging / tube / ringAnnealed
AMS 6520250K928900.40%7.8%Sheet / strip / plateSolution heat treated
AMS 6521300K931200.65%9.0%Sheet / strip / plateSolution heat treated

Read the two highlighted rows together. Identical grade, identical UNS number, identical chemistry — and two specification numbers that are not interchangeable, because the product form differs. That single pair explains most of the misrouted enquiries we receive on this family.

5. What each rung on the ladder costs you

Strength in this family is bought with titanium, and paid for in fracture toughness. The exchange rate is steep, and it is not linear.

Typical aged properties by grade

Indicative values after a standard aging cycle. Not specification minima — verify against the revision your contract invokes.

AMS 6511 — 18Ni 200

Strength1450 MPa
Toughness~150 MPa·m0.5

Extremely tough. Chosen when thick sections, SCC exposure or weld-heavy fabrication dominate the design.

AMS 6512 — 18Ni 250

Strength1760 MPa
Toughness~100 MPa·m0.5

The balance point — and the reason this grade dominates landing gear, shafting, actuators and sour-service valve internals. See how we produce AMS 6512 forgings to meet these application requirements.

AMS 6514 — 18Ni 300

Strength2000 MPa
Toughness~70 MPa·m0.5

Roughly 14% more strength than the 250 grade, for about 30% less toughness. Justified only when the stress analysis genuinely needs it.

AMS 6515 — 18Ni 350

Strength2400 MPa
Toughness~40 MPa·m0.5

65% stronger than the 200 grade, with roughly a quarter of its toughness. A specialist choice, not a general upgrade.

AMS 6520 and AMS 6521 do not appear on this ladder. They occupy the same two rungs as 6512 and 6514 — they are simply the flat-product route to those rungs. Nothing about the ladder changes when you cross the product-form axis.

Look at what toughness does between the 300 and the 350 grade. The strength gain is real, but the crack length a component tolerates before unstable fracture scales with the square of KIc. Halving toughness cuts the tolerable defect size to a quarter — and with it, the inspection interval. In damage-tolerant design, climbing the ladder often makes a part more expensive to own, not less.

6. Three different melt-route phrases in one family

This one costs people money, and it stays invisible unless you read the specification titles side by side.

Three phrasings, one alloy family. If your quality plan contains a blanket statement such as "all maraging material shall be VIM + VAR", the specification titles alone will not enforce it consistently across all six. The fix takes one line: state the melt route explicitly on the purchase order rather than inferring it from the specification you invoked.

Why it matters metallurgically

Titanium is the strengthening element, and it reacts aggressively with oxygen, nitrogen and sulphur. Every 0.01% of titanium consumed forming TiN or TiO2 is titanium unavailable for Ni3Ti precipitation — and each of those inclusions is a fatigue initiation site.

At 1.40% nominal titanium, the 350 grade is the most exposed of the four. That is consistent with its specification calling out double vacuum melting explicitly.

7. Flash welded ring ceilings are not the same across specifications

All four wrought specifications cover flash welded rings, but they do not cover them to the same size. AMS 6511 extends to flash welded rings through 6.000 inches (152.40 mm). AMS 6515 caps at 5.000 inches (127.00 mm) inclusive.

That is a small clause with a large consequence. A ring above the ceiling falls outside the flash-welded-ring scope of the specification, and the compliant route is a seamless rolled ring produced from forging stock under the same specification — not a flash welded ring with a concession attached. Discovering this at first article inspection rather than at design release is an expensive way to learn it.

8. None of these specifications delivers a hardened part

Every specification in this family is a soft-condition specification. The wrought specifications deliver annealed material; the flat-product specifications deliver solution heat treated material. In practice that means roughly 28–34 HRC arriving at your dock, machinable with coated carbide, and nowhere near the strength the grade is named after.

The 250 in "250 grade" is a capability — the tensile strength in ksi the material will reach after a correctly executed aging cycle, typically around 480 °C for three to six hours, air cooled. Until that cycle runs, the part is soft.

The consequence people miss

Buying to AMS 6512 does not buy a 250 ksi component. It buys certified material capable of 250 ksi, in a condition suitable for machining. Whoever performs the aging owns the final properties — and owns the failure if the furnace overshoots.

Above roughly 510 °C, austenite reversion begins and the strength loss cannot be recovered by re-aging. Only a full re-solution-anneal and a fresh cycle will restore it. Decide contractually, before the purchase order, whether the mill, the machinist or your own plant carries that risk.

This is also why the machine-then-age sequence is standard practice with maraging steels. Dimensional change through aging is on the order of 0.05% linear, so parts can be finish machined soft and hardened afterwards without a grinding operation. It is one of the few genuine process advantages this family holds over quenched-and-tempered ultra-high-strength steels — and it only works if the delivery condition on the purchase order is correct.

9. Writing a callout that survives first article

A complete 18Ni maraging callout has five parts. Missing any one of them creates an ambiguity a supplier is entitled to resolve in the cheapest direction.

// Wrought forging, 250 grade — complete callout MATERIAL .... SAE AMS 6512, latest revision at PO date ALLOY ....... UNS K92890 (18Ni maraging, 250 grade) FORM ........ Open die forging / seamless rolled ring per drawing MELT ........ VIM + VAR minimum; VIM + ESR + VAR preferred CONDITION ... Supply ANNEALED. Aging by purchaser. CERTIFICATE . EN 10204 3.1 with heat number traceability

The five-step selection procedure

  1. Fix the product form first. Wrought part, or flat product? That decision eliminates four of the six specifications immediately.
  2. Choose the grade from a damage tolerance calculation, not from a strength table. The required critical crack length and inspection interval should drive the rung, not the peak tensile number.
  3. State the melt route explicitly. The title language is not uniform across the family, so write the requirement rather than inferring it.
  4. State the delivery condition and name who ages the part. This is the single most common dispute on maraging orders.
  5. Pin the revision and add the UNS number. Specifications in this family are actively revised — AMS 6511 reached revision C in 2023, adding a stress corrosion cracking precaution, pyrometry requirements and clarified transverse testing. A supplier can misread 6514 for 6512; nobody misreads K93120 for K92890.

If you are ready to source, our AMS 6512 forging parts page covers the full range of available product forms — open die forgings, seamless rolled rings and machined blanks — with the exact callout we recommend for each form.

One more line worth adding

For rotating or fatigue-critical parts, add an inclusion cleanliness requirement and a UT acceptance class. Without a stated class, a supplier may default to the least stringent one available and remain fully compliant with your drawing.

10. Glossary

18Ni maraging steel
A family of ultra-high-strength, low-carbon iron–nickel alloys that develop strength by precipitating intermetallic compounds during a low-temperature aging treatment, rather than by the martensite-plus-carbon mechanism used in quenched-and-tempered steels.
Aging
The low-temperature heat treatment, typically around 480 °C, that precipitates Ni3Ti and Ni3Mo and develops the grade's rated strength. Performed after machining, and followed by air cooling.
Annealed condition
The soft, as-delivered state of wrought maraging material, roughly 28–34 HRC. Sometimes called the solution annealed condition. Machinable, and not yet at rated strength.
Austenite reversion
The transformation of martensite back to austenite when aging temperature is too high, generally above roughly 510 °C. It causes a permanent strength loss that re-aging alone cannot recover.
CEVM
Consumable electrode vacuum melted. A remelting route in which a solid electrode is progressively melted under vacuum, refining cleanliness and solidification structure.
Double vacuum melted
Vacuum induction melting followed by vacuum arc remelting, commonly written VIM + VAR. The melt route called out in the titles of AMS 6511 and AMS 6515.
Flash welded ring
A ring formed by bending bar stock and joining the ends by flash welding. Covered by the wrought specifications only up to stated diameter limits, which differ between specifications.
Fracture toughness (KIc)
The resistance of a material to crack propagation, expressed in MPa·m0.5. It governs the critical crack length a component can tolerate, and it falls sharply as maraging grade rises.
Stabilized specification
An SAE status indicating a document that is no longer actively developed but remains available for existing programmes. Generally unsuitable for new design work.
UNS number
Unified Numbering System designation. It identifies the alloy itself, independently of which specification, product form or country's standard invokes it.

11. Frequently asked questions

What is the difference between AMS 6512 and AMS 6514?

AMS 6512 covers the 18Ni 250 grade, UNS K92890, nominally 18Ni-7.8Co-4.9Mo-0.40Ti-0.10Al. AMS 6514 covers the 18Ni 300 grade, UNS K93120, nominally 18.5Ni-9.0Co-4.9Mo-0.65Ti-0.10Al.

Both cover bars, forgings, mechanical tubing and rings, and both are supplied annealed. After aging, the 300 grade reaches roughly 2000 MPa against roughly 1760 MPa for the 250 grade — but its fracture toughness is around 30% lower.

Is AMS 6515 a stronger grade than AMS 6514?

Yes. AMS 6515 covers the 350 grade (UNS K93540, nominally 18.5Ni-12.0Co-4.9Mo-1.40Ti-0.10Al). AMS 6514 covers the 300 grade (UNS K93120). AMS 6515 is the strongest wrought specification in the family.

It is also the least tough, with the narrowest hot-working window and the least tolerance for aging error. It is a specialist selection, not an upgrade path from 6514.

Are AMS 6512 and AMS 6520 the same material?

Same alloy, different specification. Both carry the 250-grade chemistry, UNS K92890. AMS 6512 covers bars, forgings, mechanical tubing, flash welded rings and forging stock. AMS 6520 covers sheet, strip and plate.

You cannot buy a forging to AMS 6520, or a sheet to AMS 6512, identical chemistry notwithstanding. Note also that the current revision of AMS 6520 carries SAE stabilized status, which makes it a poor choice for a new programme even where the product form fits.

Does material supplied to AMS 6512 arrive at 250 ksi strength?

No. It arrives annealed, at roughly 28–34 HRC, ready to machine. The 250 ksi class is reached only after an aging cycle, typically around 480 °C for three to six hours followed by air cooling.

The specification governs chemistry, melt practice, cleanliness and the properties the material must be capable of achieving. It does not govern the condition of your finished part unless your purchase order says the supplier performs the aging.

Which specification should be used for landing gear components?

Normally AMS 6512, the 250 grade. It holds fracture toughness around 100 MPa·m0.5 at roughly 1760 MPa tensile strength, which is what damage-tolerant design on airframe structure needs.

Moving to AMS 6514 or 6515 raises allowable stress but shortens the critical crack length, which tightens inspection intervals and can raise lifecycle cost above the value of the weight saved. The grade should come out of a damage tolerance calculation, not a strength table.

Can AMS 6514 be substituted for AMS 6512 to gain margin?

Not as a paperwork change. It is a different alloy with different titanium and cobalt levels, a different aging response, lower toughness and reduced elongation, under a different UNS number.

The substitution changes the material of record on the certificate. On aerospace and nuclear programmes it will normally require a formal deviation, heat treatment requalification and a new first article inspection — often more schedule than designing to the correct grade in the first place.

What are the UNS numbers for the 18Ni maraging specifications?

AMS 6511 covers the 200 grade, UNS K92810. AMS 6512 covers the 250 grade, UNS K92890. AMS 6514 covers the 300 grade, UNS K93120. AMS 6515 covers the 350 grade, UNS K93540.

AMS 6520 covers the same 250 alloy as 6512, and AMS 6521 the same 300 alloy as 6514, both in sheet, strip and plate form. Quoting the UNS number alongside the AMS number is the fastest way to remove ambiguity from a purchase order.

What is the aging temperature for 18Ni maraging steel?

Approximately 480 °C (900 °F) for three to six hours, followed by air cooling, is the standard cycle for the 200, 250 and 300 grades. The 350 grade generally requires a longer hold.

Above roughly 510 °C, austenite reversion begins and strength is lost. That loss cannot be recovered by re-aging alone — it requires a full re-solution anneal followed by a fresh aging cycle.

Which grade is right for sour service and thick sections?

Generally the lower rungs. Toughness and resistance to environmentally assisted cracking both fall as titanium rises, and thick sections magnify the penalty because through-section aging uniformity becomes harder to guarantee.

The 250 grade is the usual ceiling for H2S-exposed components, with hardness controlled against the applicable NACE MR0175 / ISO 15156 limits. Where section thickness is extreme or weldment toughness governs, the 200 grade is worth evaluating — its recent revision added a specific stress corrosion cracking precaution for good reason.

Why does the melt route wording differ between these specifications?

The titles use three different phrases. AMS 6512 and AMS 6514 say consumable electrode vacuum melted. AMS 6511 and AMS 6515 say double vacuum melted. AMS 6520 and AMS 6521 say consumable electrode melted, with no mention of vacuum.

Because the wording is not uniform, the melt route should be written explicitly on the purchase order rather than inferred from the specification number.

Forging to AMS 6512, in the condition your drawing actually specifies

Jiangsu Liangyi Co., Limited is an open die forging and seamless ring rolling manufacturer in Jiangyin, Jiangsu, operating a quality management system certified to ISO 9001:2015. Material certification to EN 10204 3.1 is issued with supply; EN 10204 3.2 can be arranged where a third-party inspection body is appointed.

Send a drawing and a specification and our engineering team will review the callout before quoting, including any of the ambiguities described above.

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Sources and verification

  1. SAE International — published specification titles, scopes and revision records for AMS6511, AMS6512, AMS6514, AMS6515, AMS6520 and AMS6521.
  2. Nominal compositions are taken from specification titles and are not substitutes for the permitted ranges in the purchased document.
  3. Aged mechanical properties are indicative values typical of each grade after a standard aging cycle. They are not specification minima. Confirm against the revision invoked by your contract.