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GuidePublished 11 Jul 2026Updated 13 Aug 202611 min readBy Kevin Jogin
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KEVOS® Knowledge Library · Engineering → Mechanical Engineering

Engineering / Mechanical Engineering

Metric Threaded Fasteners

The ISO metric system states a thread’s pitch outright and prints a bolt’s strength on its head as two numbers separated by a dot. Learn to read 8.8 and you can compute what the bolt will carry before you pick up a spanner.

  • Reading time · 6 min
  • 7 sections
  • Property class decoded
  • Stress area validated
8.8 8 × 100 = 800 N/mm² tensile × 0.8 → 640 N/mm² yield × stress area 58 mm² → 37.1 kN two numbers give the whole strength of the bolt
Doc №KL-ENG-MECH-128
SectionEngineering → Mechanical Engineering
Sheet1 of 1
DrawnKEVOS®
Date2026-07-11

In this reference

  1. The ISO metric system
  2. Reading a designation
  3. Coarse and fine
  4. The tensile stress area
  5. The property class
  6. Choosing a class
  7. Quick reference

§1The ISO metric system

The ISO metric thread is the world’s standard fastener thread — a 60° form, sized in millimetres, with the pitch stated directly rather than counted per inch.

It shares the unified inch thread’s 60° flank angle and general geometry, so the two are near-identical in form and differ chiefly in units and in how they are specified. Where the inch system counts threads per inch, metric names the pitch — the millimetres between adjacent threads — which is more direct and reads the intuitive way round: a bigger pitch number means a coarser thread, the opposite of the inch system’s reciprocal count. Two other things make the metric system pleasant to work with: the strength is stamped on the head as a two-number property class that decodes arithmetically (§5), and the stress area follows a formula that reproduces the standard tables exactly (§4). Between them, a metric bolt’s capacity can be worked out from its markings alone.

Contents

§2Reading a designation

A metric thread is written M, then the nominal diameter, then — if it is not the standard coarse pitch — a multiplication sign and the pitch.

M10 × 1.5 means a nominal major diameter of 10 mm with 1.5 mm between threads. Because 1.5 mm is the standard coarse pitch for a 10 mm thread, the same fastener is usually written simply M10 — the pitch being implied. A fine thread must always be stated, so M10 × 1.25 is unambiguous: 10 mm diameter, fine 1.25 mm pitch. A fuller designation can carry the tolerance class too (M10 × 1.5 – 6g, where 6g is the common external-thread class, the metric counterpart of the inch system’s 2A). The habit to build is to read the second number as a distance, not a count: M10 × 1.5 has threads 1.5 mm apart, so a single turn of the nut advances it 1.5 mm — which is exactly the quantity that drives the torque relation and the angle-control method on the torque-and-tension page.

Contents

§3Coarse and fine

Each metric size has one standard coarse pitch and one or more finer options, and the choice follows the same logic as the inch system’s UNC and UNF.

Coarse — M10 × 1.5, M8 × 1.25, M12 × 1.75 — is the default: quicker to assemble, more forgiving of dirt and damage, deeper-threaded so it strips less readily in soft materials, and the pitch you get if none is named. Fine — M10 × 1.25, M12 × 1.5 — has a larger stress area and so more tensile strength (§4), holds adjustment more precisely because each turn advances less, and resists vibration slightly better; against that it is slower to run down, easier to cross-thread, and its shallow threads are poorer in soft metal. The rule is unchanged from the inch page: coarse for general work and soft materials; fine for strength, fine adjustment and thin sections. Because coarse is the unstated default, a fine thread must always be written out in full — and mixing the two in one assembly is a classic and expensive mistake, since an M10 × 1.25 nut will start onto an M10 × 1.5 bolt and then jam.

Contents

§4The tensile stress area

A bolt’s strength is reckoned not on its nominal diameter but on a tensile stress area that allows for the metal the threads cut away — and the formula reproduces the standard tables exactly.

As = π4 (d − 0.9382 p)²  — d nominal diameter, p pitch (mm)
Example 1 — the area that carries the load

The bracketed term is an effective diameter lying between the thread’s root and pitch diameters, which is where a bolt in tension actually fails. For M10 × 1.5: As = (π/4) × (10 − 0.9382 × 1.5)² = (π/4) × 8.593² = 58.0 mm² — appreciably less than the 78.5 mm² of a plain 10 mm bar, which is why a bolt is weaker than its nominal size suggests. Run the same formula across the range and it lands on the standard values every time: M6 → 20.1 mm², M8 → 36.6 mm², M12 → 84.3 mm², M16 → 157 mm². That agreement is worth noticing: the tabulated stress areas are not arbitrary, and one formula and a pocket calculator will reproduce them for any size — which, combined with the property class of §5, means any metric bolt’s capacity can be computed from first principles.

Contents

§5The property class

The two numbers stamped on a metric bolt head are not a part code — they are an arithmetic statement of its strength, and they decode in one step.

Example 2 — decoding 8.8

The first number × 100 is the ultimate tensile strength in N/mm²; the second number ÷ 10 is the ratio of yield to tensile. So 8.8 (the hero) means 8 × 100 = 800 N/mm² tensile, yielding at 0.8 of that = 640 N/mm². Multiply by the stress area and the bolt is fully characterised: an M10 8.8 yields at 640 × 58.0 = 37.1 kN and finally breaks at 800 × 58.0 = 46.4 kN. The same arithmetic runs up the range: 10.9 → 1000 N/mm² tensile, 900 N/mm² yield; 12.9 → 1200 N/mm² tensile, 1080 N/mm² yield. This is the system’s real elegance — where the inch system asks you to count lines and look up a grade, metric prints the numbers themselves, and two multiplications give the load. It is also the figure the torque-and-tension page’s 75%-of-proof preload target is taken from.

Contents

§6Choosing a class

Higher classes are stronger but not automatically better — hardness brings brittleness and notch sensitivity, so the class is chosen for the duty.

The common property classes and their place
ClassTensile / yield (N/mm²)Where it belongs
4.6400 / 240low-carbon commercial bolts; light, non-critical work
8.8800 / 640the general engineering standard — structural and machine work
10.91000 / 900highly loaded joints where 8.8 will not do
12.91200 / 1080socket head cap screws, high-duty machine assembly
Classes 8.8 and above are quenched-and-tempered alloy steels — the very heat treatment of the materials section — and as it warns, the strength is bought with toughness. A 12.9 bolt yields at 1080 N/mm² but is harder, more brittle, more sensitive to notches and thread damage, and more prone to hydrogen embrittlement if plated. So 8.8 is the sensible default for general work, 10.9 and 12.9 are reached for when the load genuinely demands them, and stainless classes (A2-70, A4-80) trade strength for corrosion resistance. Choose the class the joint needs, not the strongest available.
Contents

§7Quick reference

The working core of the page on one card rack.

Designation

M10 × 1.5 = Ø10, pitch 1.5

coarse pitch implied if omitted

Stress area

As = (π/4)(d − 0.9382p)²

M10 → 58.0 mm²

Class

first × 100 = tensile

× second/10 = yield

M10 8.8

640 × 58 = 37.1 kN yield

800 × 58 = 46.4 kN ultimate

Choosing

8.8 the default

12.9 strong but brittle

Contents

Handbook application: from concept to controlled practice

Purpose. This expanded section turns the original page into a practical handbook. It preserves the supplied material and adds a repeatable way to apply, check and review Metric Threaded Fasteners. It does not replace a contract, legislation, a controlled standard, competent engineering judgement or specialist advice.

The operating aim is to carry the subject from function and assumptions through design evidence, verification and controlled release. Read the original explanation first, then use the workflow and checks below to convert knowledge into evidence.

Apply Metric Threaded Fasteners by beginning with the duty, not the component or software command. Convert the key ideas—metric, system, reading, designation, coarse—into measurable requirements and interfaces. Record operating and non-operating environments, duty cycle, expected life, loads, energy sources, human interaction and reasonably foreseeable abnormal conditions. When a value is not a project requirement or verified supplier datum, identify it as an assumption or illustrative value.

Create a calculation and evidence trail that another competent person can audit. Every input should carry a source, unit, revision and uncertainty or tolerance where relevant. Every model should state its boundary conditions and limitations. Keep nominal capacity separate from design capacity, and keep verification margin separate from an arbitrary safety factor. If a code or standard governs the work, confirm the applicable edition and contractual status rather than copying a number from a secondary summary.

Design for manufacture, assembly, inspection, operation and maintenance at the same time. A technically valid geometry can still fail because it cannot be fixtured, measured, cleaned, guarded, reached or replaced. Review process capability, datum or reference strategy, tolerance accumulation, access, error-proofing and changeover. Where people interact with plant, apply the hierarchy of controls and consult those who will operate, clean, maintain and recover the equipment.

Plan verification before release. Define the characteristic, method, equipment, sample or test condition, acceptance criterion, record and responsible person. Validation then asks a different question: whether the resulting system is effective and suitable in the intended use context. A passed drawing check or analysis does not by itself validate usability, maintainability or production performance.

Step-by-step operating method

  1. Define the duty. Capture the required function, interfaces, operating environment, life, loads and unacceptable outcomes.
  2. Establish the model. Identify governing principles, units, material or process data, assumptions and uncertainty.
  3. Develop alternatives. Compare feasible concepts against performance, manufacturability, safety, maintainability and cost.
  4. Verify the design. Use analysis, test, inspection or demonstration with acceptance criteria defined before execution.
  5. Release and learn. Baseline the design, control changes, retain evidence and feed operating results into the next revision.

Illustrative design review record

Illustrative values only. Build a one-page record with the required function, input sources, assumptions, governing load or process condition, failure consequences, selected concept, verification method and acceptance criterion. Mark every numerical input as project requirement, verified supplier data, measured value, calculation output or assumption. Review the weakest evidence first. If an assumption can change safety, compliance, interchangeability or capacity, it must be resolved before release rather than buried in a calculation note.

Evidence classQuestionRelease expectation
RequirementWhat must the design do and under which conditions?Approved and traceable
InputWhere did the load, property, tolerance or process limit come from?Source, unit and revision recorded
AnalysisWhich model and assumptions connect input to result?Checkable calculation or simulation
VerificationHow will conformity be demonstrated?Method and acceptance criterion agreed
ValidationWill the solution work for intended users and conditions?Representative use evidence

Common failure modes and recovery actions

1. Watch for

Starting detailed design before interfaces and operating limits are agreed.

Recovery: Return to the governing definition or requirement and restate the decision in one sentence.

2. Watch for

Using catalogue or typical values as though they were certified project inputs.

Recovery: Separate evidence from assumption, assign an owner and set a date for validation.

3. Watch for

Checking nominal performance while ignoring tolerances, degradation and foreseeable misuse.

Recovery: Run a small counterexample, boundary test, pilot or independent check before proceeding.

4. Watch for

Confusing verification of requirements with validation of user need.

Recovery: Record the consequence, decision and rationale, then update the controlled baseline.

5. Watch for

Releasing drawings or procedures without configuration, inspection and change controls.

Recovery: Escalate when the issue affects safety, compliance, acceptance, material value or an agreed tolerance.

Review checklist

  • What function and failure consequence govern this decision?
  • Which inputs are measured, specified, assumed or illustrative?
  • How will conformity be demonstrated and recorded?
  • What change would invalidate the current evidence?
  • Are mandatory requirements distinguished from recommendations and illustrative values?
  • Are sources, assumptions, units, dates and versions recorded closely enough to reproduce the decision?
  • Have safety, legal, ethical, stakeholder and operational consequences been considered at the appropriate level?
  • Is there a named owner and a trigger for review, escalation, change or retirement?

Questions for deeper application

What is the most important distinction a practitioner must preserve when applying Metric Threaded Fasteners?

Answer with a fact or cited source where available. Where evidence is incomplete, record the assumption, consequence, responsible owner and next validation action.

Which assumption about metric would change the result most if it proved false?

Answer with a fact or cited source where available. Where evidence is incomplete, record the assumption, consequence, responsible owner and next validation action.

What evidence would allow an independent reviewer to reproduce or challenge the conclusion?

Answer with a fact or cited source where available. Where evidence is incomplete, record the assumption, consequence, responsible owner and next validation action.

Which boundary, exception or failure case has not yet been tested?

Answer with a fact or cited source where available. Where evidence is incomplete, record the assumption, consequence, responsible owner and next validation action.

What must be handed over, monitored or reviewed after the immediate work is complete?

Answer with a fact or cited source where available. Where evidence is incomplete, record the assumption, consequence, responsible owner and next validation action.

Authoritative references and use notes

The sources below were selected as institutional or primary guidance for the broader practice. They support the handbook method; they do not imply that every statement or clause in a source applies to every project. Confirm the current edition, jurisdiction, contract and application before treating any requirement as mandatory.

  • NASA Systems Engineering Handbook — NASA. Used for requirements, design, verification, validation and technical management. Accessed 2026-08-13.
  • Identify, assess and control hazards — Safe Work Australia. Used for hazard identification, risk assessment, controls and review. Accessed 2026-08-13.

KEVOS® Knowledge Library · Engineering → Mechanical Engineering · Original KEVOS® synthesis — written, computed and drawn for this page. Built 11 July 2026.

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