01
Two different arguments for the same conclusion
Both end with a device you may use. They get there by reasoning about completely different things, and knowing which one you are in changes what you optimise.
The American argument is about material. Take the steel's strength, divide by a design factor that follows from a design category, and check every member and connection against the result. The conservatism lives in one number, that number is traceable to a duty decision about how well the loads are known, and everything downstream is an ordinary structural check.
The European argument is about the device. Require the whole assembly to satisfy stated conditions under multiples of its rated load: elastic behaviour at one multiple, no collapse at a higher one. Then, separately, check the members against a structural code with its own partial factors. The conservatism lives in the multiples, and the multiples are about the device as an object rather than about any member in it.
Three practical consequences follow.
They can disagree about which check governs. A member check and a whole-device condition are different questions, and on the worked beam below the European route's governing check is not a member at all.
They optimise differently. Under the American scheme you improve a device by improving its worst member. Under the European one you may have to improve the device's overall behaviour under overload, which is not always the same intervention.
Neither is generally more conservative. Anybody who tells you one is has not run enough devices through both.
01What question is the scheme asking?
- American: can each member carry the design load?
- Allowable stress from a design factor, tied to a design category. Plus a service class governing the fatigue side. Both are declarations somebody makes and owns.
- European: does the whole device survive multiples of its rated load?
- Proof conditions on the assembly, plus member resistances from the structural code. Two documents doing two jobs. Neither is complete alone.
02What decides the margin?
- American
- The design category, from how well the loads are known. One number, traceable, and it moves every check by the same ratio.
- European
- The load multiples in the proof conditions, plus the national partial factors. The multiples are fixed by the standard; the partial factors are a national decision.
03What happens with a lot of load cycles?
- American
- A service class, and a fatigue check inside the same standard.
- European
- Above a stated cycle threshold, the proof moves to a different standard family entirely. Not a harder version of the same calculation - a different set of documents, and the point at which a tool should stop rather than guess.
02
The same lifting beam, both ways
A 6 t lifting beam on a 4 m span, one top lug, two pick points. Bending-governed, which is where the two schemes diverge most.
Spreader Beam Design Calculator · computed at page render
The American route, Design Category B
Allowable stresses from the design factor tied to the category.
| Major-axis bending including lateral-torsional bucklinggoverns | 63.9% |
|---|---|
| Combined axial and bending | 63.9% |
| Combined normal and shear | 42.7% |
| Shear | 9.3% |
| Padeye pin bearing | 52.7% |
| Checks that computed | 13 |
A member check governs, as it always does on this route. The beam is bending-governed and the answer is a bending utilisation.
Open this example in the calculatorSpreader Beam Design Calculator · computed at page render
The European route, 16 000 declared cycles
The harmonised standard's proof conditions alongside the structural code's member resistances. Identical section, identical load, identical restraint.
| Elastic condition at 2 x rated loada whole-device condition | 61.4% |
|---|---|
| Yielded condition at 3 x rated loadgoverns | 86.1% |
| Bending and lateral-torsional bucklingagainst 63.9% on the American route | 85.4% |
| Combined axial and bending | 86.1% |
| Padeye pin connection | 62.6% |
| Checks that computed | 11 |
The governing check is the yielded condition - the device under three times its rated load - and it is not a member check at all. Read the third row against the American route's first: the same beam's bending utilisation is 64 percent under one scheme and 85 under the other, on identical steel and an identical restraint declaration.
Open this example in the calculator03
What a proof condition is, and why it is not a load factor
It is a statement about the device's behaviour at an overload, not a demand you design members against. That difference decides how you fix a device that fails one.
It is tempting to read "the device shall behave elastically at twice its rated load" as "apply a factor of two to the load and check the members". It is not the same thing, for three reasons.
It is about the device, not a member. The condition is on the assembly's behaviour. A device that yields locally somewhere harmless at twice load may still fail the condition if that yielding matters to the whole.
There is more than one multiple. Elastic behaviour at one, no collapse at a higher one. Those two conditions can be governed by different mechanisms in the same device, which a single load factor cannot express.
It can be satisfied by test. Where the standard allows verification by static test rather than by calculation, the device is proved rather than argued for. That is a different kind of evidence and it is available where a calculation is awkward.
The practical consequence is about how you fix a failure. A member check that fails is fixed by making that member stronger. A proof condition that fails may be fixed that way, and it may instead need a change to how the device redistributes load at overload, or to a detail whose behaviour under yield is the problem.
04
The European route's cliff
Declare more than the low-cycle threshold and the static proof moves to a different standard family. That is not a harder version of the same calculation.
Spreader Beam Design Calculator · computed at page render
The same beam declared for 200 000 cycles
Identical steel, identical load, identical everything except the declared number of load cycles.
| Declared load cyclesagainst 16 000 | 200 000 |
|---|---|
| Checks that computedagainst 11 at the lower cycle count | 2 |
| Member resistance checks that computedthe route has moved to a standard family this pack does not implement | 0 |
| Equilibrium and sling anglegeometry does not need a standard | still computed |
The rigging still solves, because geometry is geometry. Everything about the device stops, and the report says why: above the threshold the static and fatigue proof route through a different standard chain, and reporting EN 1993 fatigue mathematics in its place would be pretending one document is another.
Open this example in the calculatorTwo things to take from that.
The threshold is a design input, not a formality. Declaring the cycle count honestly can change which standard family your device is proved under, and that is a schedule and scope question rather than a calculation one.
A tool that stops is telling you something. An engine that produced a number here would be substituting a calculation it can perform for the one the standard requires. The refusal is the correct output, and it is the same behaviour as declining to invent a load factor for a jurisdiction that has none.
05
Which scheme, and what it means for your design
Usually decided by where the lift is. What is worth deciding deliberately is what you do once you know.
If you are on the American route. Get the design category and service class right first, because they move everything by a constant ratio and the whole margin traces to them. Then improve the worst member, and expect the worst member to be the answer.
If you are on the European route. Expect two families of check and expect the proof conditions to be competitive with the member checks. Decide early whether you are verifying by calculation or by test, because that decision changes what evidence has to exist and when.
If you are designing for both markets. Do not average them. Run both, take the worse of each check, and state that the device satisfies both schemes with the governing check named under each. A device sized to the maximum of two schemes is heavier than either requires, and that is an honest cost of selling into two markets.
If somebody asks which is more conservative. The correct answer is that it depends on the device, and the worked example is a fair illustration: the American route gave 64 percent and the European one 86 on the same beam, and swapping the section for a stockier one would move both, not necessarily in the same direction.
06
Six ways this comparison goes wrong
Four are about treating one scheme's parts as interchangeable with the other's.
1. A proof condition read as a load factor. The condition is on the device's behaviour, and fixing a failure may not be a member change.
2. The harmonised standard cited alone. It carries no member resistances. A calculation citing it alone has checked nothing against a capacity.
3. A design factor carried across. It is tied to a design category defined in its own standard, and it means nothing outside it.
4. Partial factors assumed. They are a national decision, and the same beam can be accepted differently in two countries.
5. The cycle count declared casually. On the European route it can move the whole proof to a different standard family.
6. The two schemes averaged. A device for both markets satisfies both, with the governing check named under each. There is no midpoint that means anything.
Common questions
- What is the difference between EN 13155 and ASME BTH-1?
- The argument each makes. The American standard sets an allowable stress by dividing the material's strength by a design factor that follows from a declared design category, then checks every member against it. The European standard requires the whole device to satisfy stated conditions under multiples of its rated load, and leaves member resistances to EN 1993. One reasons about material and one reasons about the device, and they can disagree about which check governs.
- Is EN 13155 more conservative than ASME BTH-1?
- Not in general, and anybody who says otherwise has not run enough devices through both. On this article's worked lifting beam the American route gives a governing bending utilisation of 64 percent and the European route gives 86 percent on its yielded proof condition, on identical steel and identical restraint. Change the section for a stockier one and both move, not necessarily in the same direction, because the two schemes put their conservatism in different places.
- What is a proof condition and how is it different from a load factor?
- It is a statement about how the whole device behaves at an overload, not a demand to check members against. Three things follow. It applies to the assembly rather than to a member, so local yielding somewhere harmless may still fail it. There is more than one multiple, and different mechanisms can govern each. And it can often be satisfied by static test rather than by calculation, which is a different kind of evidence. Fixing a failed proof condition may therefore not be a member change.
- What happens on the European route above the low-cycle threshold?
- The static and fatigue proof move to a different standard family entirely, which is a change of scope rather than a harder version of the same calculation. In this article's worked example, declaring 200 000 cycles instead of 16 000 stops every device check: the rigging geometry still solves because geometry does not need a standard, and everything about the device reports that the route has moved elsewhere. A tool producing a number there would be substituting the calculation it can do for the one required.
- How do I design a lifting device for both markets?
- Run both schemes, take the worse of each check, and state that the device satisfies both with the governing check named under each. Do not average them, because there is no midpoint that means anything. A device sized to the maximum of two schemes is heavier than either alone requires, and that is an honest cost of selling into two markets rather than an error.
Sources
Every document below is linked at its publisher or regulator. Xarpis reproduces no standard text; where a clause is named, the identifier is given so you can find it in your own copy.
EN 13155Cranes. Safety. Non-fixed load lifting attachments
BSI (national adoption of the CEN standard) · paid document
The harmonised European standard for non-fixed load lifting attachments - the family a spreader beam or lifting beam belongs to. It carries the load basis and the proof requirements, not member resistances, which is why an EN route needs EN 1993 alongside it. Now published as EN 13155:2020+A1:2025.
ASME BTH-1Design of Below-the-Hook Lifting Devices
ASME · paid document
Structural, mechanical and electrical design criteria for below-the-hook lifting devices, used alongside ASME B30.20 which carries the safety requirements. The current edition is BTH-1-2023; Xarpis implements the 2020 edition and says so on every result.
EN EurocodesEurocodes: Building the future
European Commission, Joint Research Centre · free portal
The Commission's own Eurocodes portal: the structure of EN 1990 to EN 1999, the database of Nationally Determined Parameters, and the second-generation timetable. The standards themselves are sold by the national bodies, but the NDP database is free and is what decides which partial factors apply in your country.
ASME B30.20Below-the-Hook Lifting Devices
ASME · paid document
The safety half of the US below-the-hook pair: marking, construction, installation, inspection, testing, maintenance and operation. It requires the device to have been designed to BTH-1 and then governs everything that happens afterwards, which is why citing BTH-1 alone leaves half the obligation unstated.
Run the check properly
Reading about a calculation is not the same as being able to hand one over. These tools produce the traceable record.
Something here wrong, or thinner than it should be? Tell us which paragraph and it gets rewritten. Articles carry the date they were last revised for exactly this reason.