Testing standard

ASTM F382

Standard Specification and Test Method for Metallic Bone Plates

Written and technically reviewed by Dak System Inc. engineeringLast reviewed

ASTM F382 tests metallic bone plates in four-point bending. Two inner rollers load the plate so at least two screw holes lie in a region of constant bending moment and zero shear. Annex A1 bends once and records load against deflection; Annex A2 repeats it as a sinusoid until the plate cracks or reaches run-out.

At a glance

Test type
Fatiguea load is applied over and over until something fails
Published by
ASTM
Edition
F382-24

What the test does

A finished bone plate is laid across four cylindrical rollers: two outer rollers support it, two inner rollers load it near mid-span. The inner pair sits so at least two screw holes lie between them, placing the holes in a region of constant bending moment and zero shear. The crosshead drives the inner rollers down and the plate bends. Annex A1 does this once, in displacement control, recording load against deflection; Annex A2 repeats it as a sinusoid at a load ratio of 0.1 until the plate cracks or reaches run-out.

What it measures, and why it matters

The single-cycle test yields bending stiffness, bending structural stiffness and bending strength. The two stiffness figures answer different questions — how the section resists bending, and how the plate as a whole deflects in the fixture it was tested in — so neither is usable without the roller spans alongside it. Stiffness governs how load is shared between plate and healing bone: too stiff and the bone is shielded from the stimulus it needs, too compliant and the fracture gap moves. Bending strength sets the margin against a single overload, such as a fall during rehabilitation. The fatigue annex reports cycles to failure at a given load, and testing at descending loads brackets a run-out level; that figure decides whether a plate survives the months to union under repeated gait loading. F382 sets no fatigue strength a plate must achieve, and cautions that four-point bending is not the in situ loading configuration, so the numbers rank designs rather than predicting clinical life.

The plate and the roller spacing

Specimen
A finished bone plateTested as manufactured — the holes, the contours and the surface finish are all part of it.
Loading
Four-point, two outer supports and two inner rollers
Inner roller spacing
At least two screw holes between themTHE defining requirement. It puts the holes in constant bending moment and zero shear, so they are loaded the way they fail clinically.
Annex A1
Single bend, displacement control
Annex A2
Sinusoid at a load ratio of 0.1
Record which holes were spanned
Every specimenDakPlates are not uniform along their length, and a result depends on which part of the plate was in the constant-moment region.

Static and dynamic

Annex A1 rate
Displacement control, constant
Annex A2 load ratio
0.1Minimum load is a tenth of the maximum — always in the same direction.
Run-out
Declared in advance
Frequency
Chosen so heating and inertia stay negligible

What comes out

Bending structural stiffness

From the slope of the load–displacement curve and the roller geometry

A structural property of the plate as a whole, not a material modulus — the holes and the contour are included, which is the point.

Bending strength

The bending moment at the proof or ultimate condition

Reported as a moment rather than a stress, because a plate with holes has no single meaningful section.

Fatigue run-out moment

The highest bending moment reaching run-out without cracking

How the test runs

  1. 01Select the plate and record which screw holes will lie between the inner rollers.
  2. 02Set the outer supports and inner rollers to the specified spans.
  3. 03Confirm at least two holes lie in the constant-moment region.
  4. 04Seat the plate so it does not rock and the contour does not preload it.
  5. 05For Annex A1, bend once in displacement control and record load against deflection.
  6. 06For Annex A2, cycle sinusoidally at a load ratio of 0.1.
  7. 07Continue to cracking or to the declared run-out.
  8. 08Record where the crack initiated — almost always at a hole.
  9. 09Repeat at several moment levels to establish the run-out moment.

Watch the test

Our dynamic fatigue frame, which is what the Annex A2 cycling requires. A general introduction to the machine rather than a run of this method.

The fixture this method needs

Four point bending fixture with two inner and two outer supports
Uniform momentTJ-165

Four Point Bend Fixture

Four-point loading with adjustable inner and outer spans, so the inner rollers can be set to span at least two screw holes as the method requires.

Specifications

What the report has to contain

  • Reference to ASTM F382 and which annex
  • Plate identification, material, size and hole pattern
  • WHICH HOLES lay between the inner rollers
  • Outer and inner span dimensions
  • Loading rate or cycling frequency and load ratio
  • Bending structural stiffness
  • Bending strength as a moment
  • Fatigue run-out moment, with run-outs identified
  • Crack initiation site for every specimen
  • Number of plates tested

What the machine must be capable of

The requirement splits. Annex A1 runs on an ordinary static frame in displacement control, with the rate left to the user; laboratories commonly work at around 5 mm/min. Annex A2 needs a dynamic frame able to hold a load-controlled sinusoid for a million cycles — 5 Hz and a 1,000,000-cycle run-out are the standard's suggested figures rather than absolute mandates, and R = 0.1 is near-universal practice.

No capacity is prescribed. Small-fragment plates run out at a couple of hundred newtons while heavy femoral plates go well past a kilonewton; one published study performed to F382 identified a run-out load of 1,200 N. A dynamic frame of 5 to 10 kN covers the range with headroom. The reported quantity, though, is bending moment, which follows from applied load and roller spacing together — two laboratories quoting the same newtons can be reporting quite different moments, so fixture geometry must be recorded alongside the load.

No extensometer is used; deflection is taken from the crosshead or a deflectometer. Rollers are cylindrical and commonly 6 to 12 mm in diameter — a figure that reflects fixture practice rather than a dimension the standard fixes. Which force-verification practice F382-24 names could not be confirmed from public sources, so no accuracy class is quoted here.

What goes wrong in practice

Contoured plates are the usual nuisance. A curved or tubular plate wants to roll or creep on the support rollers, quietly changing the span and therefore the moment, and the result still looks reasonable on the plot. Roller contact marking is the next trap: a worn or undersized roller indents the plate and starts a crack at the contact line rather than at a screw hole — a fixture artefact, not a device property.

In fatigue the costliest failure is the false run-out. As the plate accumulates damage its compliance rises, and if the machine is not holding amplitude cleanly in load control the specimen sees less load than the report says. Check the recorded amplitude at the end of a run-out, not only at the start. Alignment errors that put the plate out of plane add a torsional component, and the crack then initiates on one side of a hole rather than symmetrically — a visible clue worth acting on.

Why four-point rather than three

Four-point (F382)Three-point
Between the inner loadsConstant moment, zero shearMoment peaks under one nose
Where failure occursAt the weakest hole in that regionUnder the loading nose
RepresentsA plate bridging a fracture gapA point load on the plate
Screw holesLoaded as they fail clinicallyOnly if one lies under the nose

The geometry is chosen so the screw holes are loaded the way they actually fail. A three-point arrangement would concentrate stress under the nose and might miss the hole entirely, testing the plate section instead of the feature that governs its life.

Questions we are asked about this test

What is ASTM F382?

It is the ASTM standard for the flexural properties of metallic bone plates. A finished plate is bent in four-point loading, with Annex A1 covering a single static bend and Annex A2 covering fatigue cycling at a load ratio of 0.1 until the plate cracks or reaches run-out.

Why must screw holes lie between the inner rollers?

Because that region carries constant bending moment and zero shear, so the holes are loaded uniformly and the weakest one governs. Screw holes are stress concentrations and they are where plates crack clinically — putting them anywhere else in the test would measure the plate section rather than the feature that decides its life.

Why four-point rather than three-point bending?

Three-point loading peaks the moment under a single nose, so failure occurs there whether or not a hole is present. Four-point spreads a constant moment across a length, letting the plate fail at its genuinely weakest section within that length — which for a bone plate is a hole.

Why is bending strength reported as a moment rather than a stress?

Because a plate with holes and a contoured profile has no single meaningful cross-section to divide by. A moment is a structural property of the plate as tested, which is what a surgeon or designer actually needs — how much bending this plate withstands, not what stress an idealised section reached.

Why record which holes were spanned?

Because plates are not uniform along their length — hole spacing, contour and thickness vary. A result therefore belongs to the part of the plate that lay in the constant-moment region, and without that record two laboratories testing the same plate can legitimately disagree.

What is bending stiffness used for, as distinct from strength?

For predicting how the plate shares load with the bone it is fixed to. A very stiff plate carries most of the load itself and shields the bone from stress, which can delay healing; too flexible and the fracture site moves more than it should. The equivalent bending stiffness from F382 is the number that lets a designer place a plate sensibly between those two failures.

Does F382 tell you how a plate will behave in a patient?

Only in part, and it is not intended to. It is a bench comparison of plate designs under a defined, repeatable four-point bend, with no bone, no screws loading the holes and no cyclic loading. Its value is that two plates tested this way can be compared honestly. Fatigue behaviour, which is what usually limits a plate in service, is covered by the cyclic annex rather than the static test.

Running ASTM F382 on the Fatigue Tester

A fatigue frame is judged on whether it holds amplitude at frequency, not on peak load, so the figures that matter here are the cycling ones.

The method asks forDak supplies
Load & frequencyNo capacity is prescribed. Bone plates run out anywhere from a couple of hundred newtons for small-fragment plates to well over a kilonewton for heavy femoral plates — one published study working to F382 identified a run-out load of 1,200 N. A 5–10 kN dynamic frame covers the range comfortably. The useful output is the bending moment, which follows from the applied load and the roller spacing rather than from the load figure alone, so two laboratories quoting the same newtons can be reporting different moments.Load up to 500 kN at up to 100 Hz, 60 mm actuator stroke with travel resolution up to 0.1 µm
Load accuracyunknown±0.5% of reading
GrippingFour-point bend rig with two inner loading rollers and two outer support rollersGrips built to the specimen, with alignment held through the cycle
EnvironmentAmbient laboratory conditions; the standard defines no conditioning atmosphere or test temperature3009 series chambers, −150 °C to +400 °C — temperature only

This page describes the method as practised. The governing text is the current edition from the issuing body. Tell us what you are testing and we will answer with the machine, the fixture and a quotation.

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