Reference Guide · Specifications

AMS vs ASTM vs SAE: How to Read a Material Specification

Author: C&W Engineering Team
Reading time: 11 min
Audience: Design Engineers · Buyers · Quality
"6061-T651 per AMS 4027," "4140 per ASTM A29," "17-4 PH per AMS 5643 Condition H900." Every one of those callouts has two halves: a grade that says what the metal is, and a specification that says who guarantees it and how. Shops buy to the spec, mills certify to the spec, and inspectors accept to the spec, so a drawing that names the grade without the spec is only half specified. This guide explains what SAE, ASTM, AMS, ANSI, and AWS each govern, how the numbering systems work, and then indexes every specification cited elsewhere in this library so a link on "AMS 5662" lands on a plain-English answer.

Grade vs Specification: Two Halves of a Callout

A grade (6061, 4140, 304, Ti-6Al-4V, Inconel 718) is a chemistry and, loosely, a family of properties. A specification is a published document that says, for a particular product form, exactly what chemistry range, mechanical properties, condition, tolerances, testing, and certification a supplier must deliver. The same grade usually lives under several specs: 4140 bar can be bought to ASTM A29 (commercial), ASTM A322 (alloy bar), AMS 6349 (aircraft quality, normalized), or AMS 6382 (aircraft quality, annealed), and those differ in cleanliness, testing, and price even though the chemistry overlaps.
Why it matters to the quote: the spec decides which mill product we can buy, what paperwork comes with it, and sometimes what extra testing (ultrasonic, macro-etch, grain size) the mill must perform. Aerospace specs cost more and take longer to source. If your application does not need them, do not call them out; if it does, the callout is the only thing that makes them happen. The RFQ guide has a before/after table of incomplete vs complete callouts.
The four-part callout
Alloy + temper / condition + specification + product form. "7075-T7351 plate per AMS 4078" is complete. "7075" is a chemistry, not a purchase order.

SAE / AISI: The Four-Digit Steel Grades

The SAE four-digit numbering system (historically shared with AISI, which no longer maintains it) is the naming scheme for carbon and alloy steels. The first digit is the alloy family, the second the major modifier, and the last two the nominal carbon content in hundredths of a percent:
SeriesFamilyExamples in this library
10xxPlain carbon steel (Mn ≤ 1.00%)1018 (0.18% C), 1045 (0.45% C)
11xx / 12xxResulfurized / resulfurized-rephosphorized free-machining12L14 (leaded), 1215
41xxChromium-molybdenum4130, 4140
43xxNickel-chromium-molybdenum4340
86xx / 93xxNi-Cr-Mo carburizing grades8620, 9310 (gears, case-hardened parts)
So "4140" means: 4 = chromium-molybdenum family, 1 = the ~1% Cr / 0.2% Mo variant, 40 = 0.40% carbon. The "L" in 12L14 is lead; an "H" suffix (4140H) means the grade is sold to a guaranteed hardenability band. This is the SAE designation logic the alloy-steel article refers to.
SAE J403 (Chemical Compositions of SAE Carbon Steels) and SAE J404 (SAE Alloy Steels) are the documents that actually define the chemistry ranges for each number. They are composition standards only: they say what 1018 is, not what properties a given bar must have. That is why a drawing that says "SAE 1018" still needs a product specification (ASTM A108 for cold-finished bar, ASTM A29 general requirements, and so on) before a mill can certify it.

ASTM: Commercial and Structural Material Standards

ASTM International (formerly the American Society for Testing and Materials) publishes the specifications most commercial, structural, and industrial material is bought to. An ASTM material spec is identified by a letter (A = ferrous metals, B = nonferrous metals, F = specific applications such as medical devices, E = test methods) and a number, and it covers a product form: A36 is structural carbon steel plate and shapes, A108 is cold-finished carbon steel bar, B209 is aluminum sheet and plate, B211 is aluminum bar. Properties, tolerances, testing, and marking are all inside. ASTM specs are what a steel service center stocks by default, so they are the fastest and cheapest material to source. When you don't need aerospace pedigree, ASTM is the right callout.

AMS: Aerospace Material Specifications

AMS specifications are published by SAE International's Aerospace Materials Division and are the language of aerospace and defense drawings. They are numbered by family: AMS 2xxx are process specs (AMS 2700 passivation, AMS 2759 heat treatment of steel, AMS 2770 heat treatment of aluminum, AMS 2774 heat treatment of nickel alloys), AMS 4xxx aluminum and other nonferrous wrought products, AMS 5xxx steels, stainless steels, and nickel/cobalt superalloys, AMS 6xxx low-alloy steels, and AMS 4900–4999 titanium. Compared with the ASTM equivalent, an AMS material spec usually tightens chemistry, requires more testing (ultrasonic inspection, macro-etch, grain size, hydrogen limits), demands full heat-lot traceability, and sometimes fixes the condition (AMS 5662 is 718 annealed; AMS 5663 is 718 direct-aged; AMS 5664 is 718 solution-and-aged). That is why one grade appears under several AMS numbers: the number encodes the form and condition, not just the alloy. The Inconel AMS specs article walks through the 625/718 family; AMS 4050 is covered on its own page.
When to call out AMS
When the part is flight, defense, or safety-critical, when your customer's drawing or purchase order flows it down, or when you need the testing it mandates (for example ultrasonic-tested thick aluminum plate). Otherwise ASTM saves money and lead time with no loss of chemistry.

ANSI, AWS, MIL/DTL, OSHA, UNS

ANSI H35.1 is the American National Standard for aluminum alloy and temper designations: it defines what the four-digit aluminum numbers (6061, 7075, 2024, 7050) and the temper suffixes (O, H14, T4, T6, T651, T73, T7451) mean. It does not specify products; the ASTM B-series and AMS 4xxx specs do that using H35.1's vocabulary. See the temper note in the aluminum guide.
AWS D1.1 (Structural Welding Code — Steel) from the American Welding Society governs the welding of structural carbon and low-alloy steel: prequalified joints, procedure and welder qualification, inspection. It is the code most fabricated steel weldments are built to, and why 4130, with its low carbon and weldability, is the alloy steel of choice for welded structures.
MIL-, MIL-DTL-, MIL-PRF- specs are U.S. military specifications. In a machine shop they show up mostly as finish and hardware callouts: MIL-A-8625 (anodizing), MIL-DTL-5541 (chem film), MIL-DTL-13924 (black oxide), MS and NAS hardware part numbers. Our finishes and coatings guide covers the finish specs.
29 CFR 1910.1025 is OSHA's occupational lead standard. It is why leaded free-machining steels such as 12L14 carry handling requirements in the shop, and why lead-free alternatives (1215, 1117) are sometimes specified instead.
UNS (Unified Numbering System) numbers, such as N07718 for Inconel 718 or S17400 for 17-4 PH, are a cross-reference index that gives each alloy one unambiguous identifier across all the naming systems. A UNS number is not a specification either; it just tells you which alloy everyone is talking about.

What "Per Spec" Buys You: Certs and Traceability

When material is bought to a specification, the mill or distributor issues a material test report (MTR, "mill cert") stating the heat number, the actual chemistry, the measured mechanical properties, and the spec(s) the heat conforms to. That document is what lets a shop issue a certificate of conformance, lets an FAI package trace the part back to the melt, and lets a customer's quality system accept the lot. Commercial stock from a service center may carry a cert or may not; aerospace stock always does. If your part needs the paperwork, say so in the RFQ (see quality documentation) because certified stock is a different purchase than commercial stock, and because specs like AMS 4050 mandate testing (ultrasonic inspection) that must be done at the mill, not after the fact.
"Equivalent" is not a spec
Drawings that say "6061-T6 or equivalent" or "4140 or equal" leave the decision to the supplier and the argument to inspection. If a substitute is genuinely acceptable, list it ("6061-T6 per AMS 4027 or ASTM B209"). Otherwise name one spec.

Specification Index (Every Spec in This Library)

Plain-English entries for each specification referenced in the resource library. Numbers are current designations; always work from the revision on your drawing.

Carbon & alloy steel

SpecWhat it coversSee also
SAE J403Chemical compositions of SAE carbon steels (10xx, 11xx, 12xx, 15xx). Composition only; pair with a product spec.A36 vs 1018 vs 12L14
ASTM A29General requirements for carbon and alloy steel bars, hot-wrought. The umbrella spec bars like 4140 and 1045 are sold under; sets chemistry and general delivery rules.4140 vs 4340 vs 4130
ASTM A36Carbon structural steel plate, shapes, and bars: 36 ksi minimum yield, weldable. The default hot-rolled plate grade.A36 vs 1018
ASTM A108Cold-finished carbon and alloy steel bars (1018, 1045, 12L14 cold drawn, turned-and-polished, ground). Sets size tolerances and surface finish for cold-finished bar.1018 vs 1045 TG&P
SAE 1215Lead-free free-machining carbon steel (resulfurized, rephosphorized): the usual substitute when 12L14's lead is unacceptable.A36 vs 1018 vs 12L14
AMS 63494140 alloy steel bars, forgings, and tubing, aircraft quality, normalized (or normalized and tempered). Aerospace-grade 4140 stock.4140
AMS 63704130 alloy steel bars, forgings, and tubing, aircraft quality, normalized. The weldable chrome-moly grade in aerospace form.4130
AMS 64144340 alloy steel bars, forgings, and tubing, vacuum consumable-electrode remelted, aircraft quality. Premium-cleanliness 4340 for high-strength parts (often heat treated to 260–280 ksi).4340
AMS 2759 (/1–/12)Heat treatment of steel parts. Slash sheets cover specific processes: /1 carbon and low-alloy (Q&T), /3 precipitation-hardening stainless (H-conditions), /6 gas nitriding, /7 carburizing, /11 stress relief, and so on.Heat treatment glossary
AWS D1.1Structural welding code for steel: joint design, qualification, inspection of welded carbon and low-alloy steel structures.4130 (weldable)

Stainless steel & nickel superalloys

SpecWhat it coversSee also
AMS 564317-4 PH (UNS S17400) bars, wire, forgings, rings: solution treated, precipitation hardenable. The standard 17-4 bar spec; H-condition is called out separately.Stainless grades
ASTM A564Hot-rolled and cold-finished age-hardening stainless steel bars and shapes: the commercial spec for 17-4 PH (Type 630) and 15-5 PH bar.Stainless grades
ASTM A276Stainless steel bars and shapes (303, 304, 316, 17-4 and others), hot- or cold-finished. The commercial stainless bar spec.Stainless grades
AMS 2700Passivation of corrosion-resistant steels: the citric or nitric acid process that removes free iron from a machined stainless surface.Finishes & coatings
AMS 5596Inconel 625 (UNS N06625) sheet, strip, and plate, solution annealed.Inconel 625 vs 718
AMS 5666Inconel 625 bars, forgings, and rings, solution annealed.Inconel 625 vs 718
AMS 5662Inconel 718 (UNS N07718) bars, forgings, and rings, solution annealed (not aged): the machinable starting condition, ~38 HRC max.Inconel AMS specs
AMS 5663Inconel 718 bars, forgings, rings: solution annealed and precipitation heat treated by the mill (direct-aged stock). Arrives hard.Inconel AMS specs
AMS 5664Inconel 718 bars, forgings, rings: solution treated and aged (double aging per AMS 2774) to full properties, ~180 ksi UTS, ~40–45 HRC. The finished-part condition most aerospace drawings call out.Inconel AMS specs
AMS 2774Heat treatment of wrought nickel alloy and cobalt alloy parts: the process spec that defines the 718 solution-and-double-age cycle.Double aging cycle
AMS 5536Hastelloy X (UNS N06002) sheet, strip, and plate, solution heat treated.Hastelloy X vs C-276 vs 282
AMS 5754Hastelloy X bars, forgings, and rings, solution heat treated.Hastelloy X
AMS 5750Hastelloy C-276 (UNS N10276) bars, forgings, and rings, solution heat treated.Hastelloy C-276
ASTM B575Low-carbon nickel-chromium-molybdenum alloy plate, sheet, and strip (C-276, C-22, C-2000, 59 and others). The commercial spec for Hastelloy C-276 flat products.Hastelloy C-276
AMS 5951Haynes 282 (UNS N07208) sheet, strip, and plate, solution heat treated.Haynes 282
AMS 5952Haynes 282 bars, forgings, and rings, solution heat treated.Haynes 282

Aluminum & titanium

SpecWhat it coversSee also
ANSI H35.1Alloy and temper designation systems for aluminum: defines the 6061 / 7075 / 2024 / 7050 numbers and the O, H, T tempers.Temper designations
ASTM B209Aluminum and aluminum-alloy sheet and plate: the commercial spec for 6061, 7075, 2024 plate. (B211 is bar, B221 is extrusions.)6061 vs 7075 vs 2024
AMS 40276061-T6 / T651 sheet and plate, aerospace quality.6061
AMS 40787075-T7351 plate, aerospace quality: the overaged, stress-corrosion-resistant 7075 plate temper.7075
AMS 40507050-T7451 plate, aerospace quality, with mandatory ultrasonic inspection per AMS-STD-2154. The thick-section aerospace plate spec.AMS 4050 guide · 7050
AMS 2770Heat treatment of wrought aluminum alloy parts (solution treatment, quench, aging to T-tempers). AMS 2772 is the raw-material counterpart.Aluminum tempers
AMS 4911Ti-6Al-4V sheet, strip, and plate, annealed.Titanium grades
AMS 4928Ti-6Al-4V bars, wire, forgings, and rings, annealed. The standard aerospace Ti-6-4 bar spec.Titanium grades
AMS 4902Commercially pure titanium Grade 2 sheet, strip, and plate, annealed.Titanium grades
ASTM B265Titanium and titanium alloy strip, sheet, and plate (Grades 1–38): the commercial flat-product titanium spec.Titanium grades
AMS 4965Ti-6Al-4V bars, wire, forgings, and rings, solution treated and aged (STA): the higher-strength heat-treated condition.Titanium grades
AMS 4930Ti-6Al-4V ELI (extra-low interstitial) bars, wire, forgings, rings, annealed: aerospace-form Grade 23.Titanium grades
ASTM F136Ti-6Al-4V ELI (extra-low interstitial, Grade 23) wrought alloy for surgical implant applications. The medical-implant titanium spec.Titanium grades

Engineering plastics & food contact

SpecWhat it coversSee also
ASTM D4020Ultra-high-molecular-weight polyethylene (UHMW-PE) molding and extrusion materials: defines the molecular-weight classes and properties.UHMW vs Delrin
ASTM D4181Acetal (POM) molding and extrusion materials, homopolymer (Delrin) and copolymer grades.UHMW vs Delrin
FDA 21 CFR 177.1520Olefin polymers (including UHMW-PE) permitted for food-contact use.UHMW vs Delrin
FDA 21 CFR 177.2480Polyoxymethylene (acetal) homopolymer permitted for food-contact use.UHMW vs Delrin

Finishes, quality & other

SpecWhat it coversSee also
MIL-A-8625Anodic coatings for aluminum: Type I/IB chromic, Type II sulfuric, Type III hard coat; Class 1 undyed, Class 2 dyed.Finishes & coatings
MIL-DTL-5541Chemical conversion coatings (chem film, "Alodine") on aluminum: Type I hexavalent, Type II trivalent; Class 1A corrosion protection, Class 3 electrical contact.Finishes & coatings
ASTM B633Electrodeposited zinc coatings on iron and steel: service-condition (SC) thickness classes and chromate types.Finishes & coatings
AS9102Aerospace first article inspection requirement: the FAI forms and content that accompany a new part number or revision.RFQ guide
AS478Identification marking methods for aerospace parts (laser, ink stamp, bag-and-tag, and so on).RFQ guide
AMS-STD-2154Ultrasonic inspection of wrought metals: the acceptance classes (AAA, AA, A, B, C) cited by AMS 4050 and similar plate specs.Ultrasonic testing
ASME Y14.5Dimensioning and tolerancing: the GD&T standard on U.S. drawings.DFM guide
ISO 2768General tolerances for dimensions without individual tolerance indication (f/m/c/v classes): the common metric title-block default.RFQ guide
29 CFR 1910.1025OSHA lead standard: exposure limits and handling rules that apply when machining leaded steels such as 12L14.12L14

Quick Reference Card

SAE / AISI
Names the steel grade (four digits: family + modifier + carbon). Composition only; not a purchase spec.
4140 = Cr-Mo, 0.40% C
ASTM
Commercial / structural product specs by form: A = ferrous, B = nonferrous, F = applications. Cheapest, fastest to source.
A36 plate · A108 bar · B209 plate
AMS
Aerospace specs: tighter chemistry, more testing, traceability, condition fixed by the number. 2xxx = process specs.
AMS 5662 annealed · 5664 aged
ANSI / UNS
ANSI H35.1 defines aluminum alloy + temper names; UNS gives every alloy one cross-reference number.
N07718 = Inconel 718
MIL / AWS / OSHA
MIL specs for finishes and hardware; AWS D1.1 for structural welding; 29 CFR 1910.1025 for leaded steels.
MIL-A-8625 Type II Class 2
The callout
Alloy + temper/condition + spec + form. "Or equivalent" is not a spec.
7075-T7351 plate / AMS 4078

Not sure which spec your part needs?

Send the drawing through the contact page and an engineer will suggest the right specification for the application before it is quoted.

Sources & References
[1]SAE International, J403 Chemical Compositions of SAE Carbon Steels; J404 Chemical Compositions of SAE Alloy Steels; J1086 Numbering Metals and Alloys (UNS).
[2]ASTM International, Annual Book of ASTM Standards, Vol. 01.03 (steel bar), 01.04 (structural steel), 02.02 (aluminum), 02.04 (nonferrous nickel alloys), 13.01 (medical devices).
[3]SAE Aerospace Material Specifications, AMS 2xxx–6xxx series as cited; AMS-STD-2154.
[4]The Aluminum Association / ANSI H35.1, Alloy and Temper Designation Systems for Aluminum.
[5]American Welding Society, AWS D1.1/D1.1M Structural Welding Code — Steel. OSHA 29 CFR 1910.1025, Lead.