Deck checking: formulas and assumptions

This sheet documents the method behind the TG20 Platform Checker. Every formula is shown and every assumption stated, in the same order as the calculator: Inputs (sections 1–7), Analysis (sections 8–11), Results (sections 12–16) and Component data (sections 17–20).

Part A — Inputs

1. Notation

Symbol

Meaning

Unit

Default

q₁

Uniform service load on the main boards

kN/m²

2.0 (class 3)

F₁, F₂

Concentrated loads on 500 × 500 mm and 200 × 200 mm

kN

1.5, 1.0

q₂, aₚ

Partial area load and its area factor (classes 4–6)

kN/m², –

not used

qᵢₙ

Imposed load on the inside boards

kN/m²

0.75

g

Deck self-weight (boards + layers + other dead load)

kN/m²

0.245

nb

Number of main boards

–

5

nᵢₙ

Number of inside boards

–

2

b

Board width

mm

225

D

Tube outside diameter

mm

48.3

W

Ledger spacing, outer to inner (centres)

mm

1,173

c

Transom cantilever beyond the inner ledger

mm

524

nL

Ledgers under the main boards

–

2

nᵤₚ

Uprights along each ledger

–

3 (2 bays)

Lb

Bay length (upright spacing)

m

2.0

sₘ

Board span m (distance between adjacent transoms)

m

1.0

nₜ, nₗ

Transoms at one position; tubes in one ledger

–

1, 1

Mₐ, Vₐ

Safe working moment and shear of one member

kNm, kN

1.12, 29.10 (steel tube)

Fₛ

Safe working slip load of one right-angle coupler

kN

9.1 (class B)

M, V, δ, R

Bending moment, shear, deflection, reaction

kNm, kN, mm, kN

–

u

Utilisation = load effect ÷ safe working value

%

–

  • x runs along the ledgers from upright U1; y runs across the platform from ledger 1 (outer).

  • Loads are positive downward; reactions positive upward; sagging moment positive.

  • All loads are working (unfactored) loads compared with safe working values. No partial safety factors are applied.

2. Load class

The class buttons fill in the BS EN 12811-1 service loads used by TG20:21. Any value can be overwritten.

Class

TG20 duty

q₁ kN/m²

F₁ kN

F₂ kN

q₂ kN/m²

aₚ

1

Inspection / very light duty

0.75

1.5

1.0

–

–

2

Light duty

1.50

1.5

1.0

–

–

3

General purpose (default)

2.00

1.5

1.0

–

–

4

Heavy duty

3.00

3.0

1.0

5.0

0.4

5

Masonry

4.50

3.0

1.0

7.5

0.4

6

Special duty

6.00

3.0

1.0

10.0

0.5

F₁ as a pressure

F₁ as a pressure

q = F₁ ÷ (0.5 × 0.5)

q = F₁ ÷ (0.5 × 0.5)

F₂ as a pressure

F₂ as a pressure

q = F₂ ÷ (0.2 × 0.2)

q = F₂ ÷ (0.2 × 0.2)

Partial loaded area

Partial loaded area

Aₚ = aₚ × Lb × z (z = width of the loaded zone)

Aₚ = aₚ × Lb × z (z = width of the loaded zone)

Other dead load

Other dead load

added to g over every board (kN/m²)

added to g over every board (kN/m²)

  • q₁, F₁, F₂ and q₂ are separate load cases; they are never added together.

  • Choosing a class resets q₁ to aₚ. Loads tagged “class” in the load cases follow these values until edited.

Example, class 3: F₂ = 1.0 kN ÷ (0.2 × 0.2)

Example, class 3: F₂ = 1.0 kN ÷ (0.2 × 0.2)

25.0 kN/m² over 200 × 200 mm

25.0 kN/m² over 200 × 200 mm

3. Section: boards, inside boards and ledgers

Ledger spacing

Ledger spacing

W = nb × b + D

W = nb × b + D

Main boards zone

Main boards zone

y = D/2 to W − D/2

y = D/2 to W − D/2

Inside boards zone

Inside boards zone

y = W + D/2 to W + D/2 + nᵢₙ × b

y = W + D/2 to W + D/2 + nᵢₙ × b

Transom length, cantilever

Transom length, cantilever

Yend = W + D/2 + nᵢₙ × b + 50 mm; c = Yend − W

Yend = W + D/2 + nᵢₙ × b + 50 mm; c = Yend − W

Extra inside ledger

Extra inside ledger

y = W + D + nᵢₙ × b

y = W + D + nᵢₙ × b

Intermediate ledgers

Intermediate ledgers

yⱼ = j × W ÷ (nL − 1), j = 0 … nL − 1

yⱼ = j × W ÷ (nL − 1), j = 0 … nL − 1

  • Main boards fit between the outer and inner standards, which stand on the ledger lines.

  • Inside boards start at the face of the inner standard and sit on the transom cantilever, or on an extra ledger at their inside edge.

  • Each board is a strip b wide. Load is only taken where there are boards; nothing is counted over the standards.

  • The inside board load qᵢₙ is a user value applied separately from the main platform load. 0.75 kN/m² is a default, not a TG20 value.

  • Intermediate ledgers are equally spaced and every ledger has an upright at every upright line.

Example: W = 5 × 225 + 48.3

Example: W = 5 × 225 + 48.3

1,173 mm

1,173 mm

Inside zone = 1,197 to 1,197 + 2 × 225

Inside zone = 1,197 to 1,197 + 2 × 225

1,197 – 1,647 mm

1,197 – 1,647 mm

c = 1,647 + 50 − 1,173

c = 1,647 + 50 − 1,173

524 mm

524 mm

4. Deck layers

Extra board or plywood layers can be laid on the main boards, and optionally on the inside boards. Layers are not fixed together: each bends on its own and they share load in proportion to their stiffness. For each layer i, per metre width: eᵢ = EI, mᵢ = Mₐ, vᵢ = Vₐ.

Stiffness of a board strip

Stiffness of a board strip

EIₛₜᵣᵢₚ = b × Σ eᵢ

EIₛₜᵣᵢₚ = b × Σ eᵢ

Moment taken by layer i

Moment taken by layer i

Mᵢ = M × eᵢ ÷ Σ eᵢ

Mᵢ = M × eᵢ ÷ Σ eᵢ

Moment factor

Moment factor

kM = max(eᵢ ÷ mᵢ) ÷ Σ eᵢ

kM = max(eᵢ ÷ mᵢ) ÷ Σ eᵢ

Shear factor

Shear factor

kV = max(eᵢ ÷ vᵢ) ÷ Σ eᵢ

kV = max(eᵢ ÷ vᵢ) ÷ Σ eᵢ

Safe moment of the deck per board

Safe moment of the deck per board

Ma,deck = b ÷ kM

Ma,deck = b ÷ kM

Deck self-weight

Deck self-weight

g = (25 + Σ layer kg/m²) × 9.81 ÷ 1000 + other dead load

g = (25 + Σ layer kg/m²) × 9.81 ÷ 1000 + other dead load

Spread of concentrated loads

Spread of concentrated loads

ly = max(ly, sₛₚ); sₛₚ = user value, or 450 mm with plywood, otherwise 0

ly = max(ly, sₛₚ); sₛₚ = user value, or 450 mm with plywood, otherwise 0

  • The layer that reaches its own safe value first governs the deck, so a thin sheet can add little capacity.

  • The spread acts across the boards only (y direction), only on concentrated and point loads, and only where layers are present.

  • Layers change the transoms and ledgers only through their self-weight.

Example, 18 mm plywood on boards: Σe = 29.0 + 2.916

Example, 18 mm plywood on boards: Σe = 29.0 + 2.916

31.916 kNm²/m

31.916 kNm²/m

e ÷ m: board 29.0 ÷ 2.111 = 13.74; plywood 2.916 ÷ 0.432 = 6.75 → kM = 13.74 ÷ 31.916

e ÷ m: board 29.0 ÷ 2.111 = 13.74; plywood 2.916 ÷ 0.432 = 6.75 → kM = 13.74 ÷ 31.916

0.4304

0.4304

Ma,deck = 0.225 ÷ 0.4304

Ma,deck = 0.225 ÷ 0.4304

0.523 kNm per board

0.523 kNm per board

g = (25 + 10.8) × 9.81 ÷ 1000

g = (25 + 10.8) × 9.81 ÷ 1000

0.351 kN/m²

0.351 kN/m²

5. Bays and transoms

Uprights

Uprights

xᵢ = i × Lb

xᵢ = i × Lb

Equal per bay, n intermediate

Equal per bay, n intermediate

x = xᵢ + Lb × k ÷ (n + 1), k = 1 … n

x = xᵢ + Lb × k ÷ (n + 1), k = 1 … n

Maximum spacing sₘₐₓ

Maximum spacing sₘₐₓ

n = ⌈Lb ÷ sₘₐₓ⌉ − 1 per bay, then equal spacing

n = ⌈Lb ÷ sₘₐₓ⌉ − 1 per bay, then equal spacing

Custom positions

Custom positions

50 mm ≤ x ≤ L − 50 mm and ≥ 50 mm from any other transom

50 mm ≤ x ≤ L − 50 mm and ≥ 50 mm from any other transom

Board spans

Board spans

sₘ = xₘ₊₁ − xₘ

sₘ = xₘ₊₁ − xₘ

Doubled / tripled transoms

Doubled / tripled transoms

EI, w, Mₐ, Vₐ × nₜ (nₜ = 1, 2 or 3)

EI, w, Mₐ, Vₐ × nₜ (nₜ = 1, 2 or 3)

  • A transom is always present at every upright line and cannot be moved.

  • Dragging a transom on the plan snaps it to 25 mm.

  • Transoms at one position share load equally and deflect together.

Example, sₘₐₓ = 800 mm: n = ⌈2.0 ÷ 0.8⌉ − 1 = 2 per bay

Example, sₘₐₓ = 800 mm: n = ⌈2.0 ÷ 0.8⌉ − 1 = 2 per bay

spans 667 mm

spans 667 mm

Example, double transoms (default job): transom M = 0.522 kNm ÷ (2 × 1.12)

Example, double transoms (default job): transom M = 0.522 kNm ÷ (2 × 1.12)

23% (was 46%)

23% (was 46%)

6. Members and couplers

Transoms and ledgers can each be any member in the library (section 17). The defaults are 48.3 mm steel tube for both.

Member self-weight

Member self-weight

wₜ = kg/m × 9.81 ÷ 1000 (steel tube: 0.0429 kN/m)

wₜ = kg/m × 9.81 ÷ 1000 (steel tube: 0.0429 kN/m)

Tubes in one ledger (1 or 2)

Tubes in one ledger (1 or 2)

EI, w, Mₐ, Vₐ, Fₛ × nₗ

EI, w, Mₐ, Vₐ, Fₛ × nₗ

Coupler slip load

Coupler slip load

Fₛ = 6.1 kN (class A) or 9.1 kN (class B)

Fₛ = 6.1 kN (class A) or 9.1 kN (class B)

  • Each tube of a doubled ledger is assumed to have its own coupler at every upright.

  • Galvanised tubes in good condition are taken as new.

7. Load cases

A load case is a list of loads acting together. Each load can be ticked, edited or removed, and new cases added.

Load

How it is applied

Deck self-weight

g on the main boards, gᵢₙ on the inside boards, every bay

Member self-weight

wₜ × nₜ along every transom; wₜ × nₗ along every ledger

Uniform load

q on one zone (main or inside boards); every bay or pattern-loaded

Concentrated load

q = F ÷ (lₓ × ly) over its area; fixed x, y or worst position

Partial area load

q₂ over Aₚ at the worst position; with “replaces uniform load” the added intensity is q₂ − q₁

Point load

q = P ÷ (0.1 × ly) over 100 mm along the span and 100 mm (or sₛₚ) across

Default case

Loads acting together

LC1 Uniform load q₁

Self-weights + q₁ on main boards (pattern) + qᵢₙ on inside boards (pattern)

LC2 Concentrated F₁

Self-weights + F₁ on 500 × 500, worst position + qᵢₙ

LC3 Concentrated F₂

Self-weights + F₂ on 200 × 200, worst position + qᵢₙ

LC4 Partial area q₂

Self-weights + q₁ + q₂ on Aₚ replacing q₁ below it + qᵢₙ (classes 4–6 only)

LC5 Point loads

Self-weights + 1.5 kN at x 1.0, y 0.6 m + 1.0 kN at x 0.5, y 0.3 m + qᵢₙ

Pattern arrangements

Pattern arrangements

N = (2ⁿbays − 1) × (2ⁿregions − 1)

N = (2ⁿbays − 1) × (2ⁿregions − 1)

Pattern regions

Pattern regions

each span between ledgers under the main boards, plus the inside boards

each span between ledgers under the main boards, plus the inside boards

Worst position, candidate x

Worst position, candidate x

every transom and every board mid-span

every transom and every board mid-span

Worst position, candidate y

Worst position, candidate y

every ledger, board centre, mid-span between ledgers and a 100 mm grid

every ledger, board centre, mid-span between ledgers and a 100 mm grid

Refinement around each member’s worst

Refinement around each member’s worst

x ± 4 × sₘᵢₙ/8, y ± 4 × 30 mm

x ± 4 × sₘᵢₙ/8, y ± 4 × 30 mm

q₂ patch shapes

q₂ patch shapes

Aₚ/z × z, s × Aₚ/s, √Aₚ × √Aₚ, Lb × Aₚ/Lb

Aₚ/z × z, s × Aₚ/s, √Aₚ × √Aₚ, Lb × Aₚ/Lb

  • Load cases are independent. Each member’s result is its worst over all active cases.

  • Pattern loading finds the largest sagging, hogging and reactions, including an unloaded inside cantilever, which gives the largest sagging in the main transom span.

  • Only one load per case can move to its worst position; pattern loading is not combined with a moving load (uniform loads then act on every bay).

  • Each member keeps its own worst position. The search was checked against a brute-force scan on a 20 × 12.5 mm grid and is within 1%.

  • Loads that fall outside the boards are ignored and flagged; concentrated loads are clipped to their zone.

  • All loads are static and vertical. Wind, impact, dynamic and horizontal loads are not included.

Example, LC1: N = (2² − 1) × (2² − 1)

Example, LC1: N = (2² − 1) × (2² − 1)

9 arrangements

9 arrangements

LC2 and LC3 worst-position search

LC2 and LC3 worst-position search

319 and 402 positions

319 and 402 positions

Part B — Analysis

8. Load path

Loads go from the boards to the transoms, from the transoms to the ledgers, and from the ledgers into the uprights through the right-angle couplers.

Board line load

Board line load

w = q × (overlap of the load with the board in y)

w = q × (overlap of the load with the board in y)

Lever-rule share to transom k

Lever-rule share to transom k

φₖ(x) = (x − xₖ₋₁) ÷ sₖ₋₁ or (xₖ₊₁ − x) ÷ sₖ, 0 elsewhere

φₖ(x) = (x − xₖ₋₁) ÷ sₖ₋₁ or (xₖ₊₁ − x) ÷ sₖ, 0 elsewhere

Transom line load from an area load

Transom line load from an area load

wₖ = q × ∫ φₖ(x) dx

wₖ = q × ∫ φₖ(x) dx

Tributary width, load on every bay

Tributary width, load on every bay

fₖ = (sₖ₋₁ + sₖ) ÷ 2 (half at the end transoms)

fₖ = (sₖ₋₁ + sₖ) ÷ 2 (half at the end transoms)

Point load share

Point load share

Pₖ = P × φₖ(xP)

Pₖ = P × φₖ(xP)

Ledger loads

Ledger loads

transom reactions Rk,j at xₖ + ledger self-weight

transom reactions Rk,j at xₖ + ledger self-weight

Upright reaction

Upright reaction

Ri,j = reaction of ledger j at upright i

Ri,j = reaction of ledger j at upright i

  • The lever rule is exact for boards simply supported between adjacent transoms.

  • The transom at an upright passes its load straight into the coupler at that upright.

Example, LC1, transom T2: f = (1.0 + 1.0) ÷ 2 = 1.0 m; main boards (2.0 + 0.245) × 1.0

Example, LC1, transom T2: f = (1.0 + 1.0) ÷ 2 = 1.0 m; main boards (2.0 + 0.245) × 1.0

2.245 kN/m

2.245 kN/m

9. Boards

Each board strip is checked span by span, simply supported between two adjacent transoms.

Uniform load

Uniform load

M = w s² ÷ 8, V = w s ÷ 2, δ = 5 w s⁴ ÷ (384 EI)

M = w s² ÷ 8, V = w s ÷ 2, δ = 5 w s⁴ ÷ (384 EI)

Central patch, total P over length l

Central patch, total P over length l

M = P s ÷ 4 − P l ÷ 8, δ = P (8s³ − 4s l² + l³) ÷ (384 EI)

M = P s ÷ 4 − P l ÷ 8, δ = P (8s³ − 4s l² + l³) ÷ (384 EI)

Any other loading

Any other loading

solved with the beam method of section 10

solved with the beam method of section 10

  • Boards are not taken as continuous over transoms. This is conservative for sagging and ignores staggered board ends.

  • Every board and every span is checked; the worst is reported.

10. Transoms and ledgers

Transoms are continuous over the ledgers, with the inside cantilever where there is no extra ledger. Ledgers are continuous over the uprights. Both are solved with the three-moment equation.

Cantilever end moment

Cantilever end moment

Mend = −Σ P a − Σ w (b − a)(a + b) ÷ 2

Mend = −Σ P a − Σ w (b − a)(a + b) ÷ 2

Three-moment equation

Three-moment equation

Mᵢ₋₁Lᵢ + 2Mᵢ(Lᵢ + Lᵢ₊₁) + Mᵢ₊₁Lᵢ₊₁ = −Tᵢ − Tᵢ₊₁

Mᵢ₋₁Lᵢ + 2Mᵢ(Lᵢ + Lᵢ₊₁) + Mᵢ₊₁Lᵢ₊₁ = −Tᵢ − Tᵢ₊₁

Load term, point load

Load term, point load

T = P a (L² − a²) ÷ L

T = P a (L² − a²) ÷ L

Load term, part uniform load a₁ to a₂

Load term, part uniform load a₁ to a₂

T = (w ÷ L) [L² a²/2 − a⁴/4] from a₁ to a₂

T = (w ÷ L) [L² a²/2 − a⁴/4] from a₁ to a₂

Moment in a span

Moment in a span

M(x) = M₀(x) + Mₗ(1 − x/L) + Mᵣ x/L

M(x) = M₀(x) + Mₗ(1 − x/L) + Mᵣ x/L

Shear in a span

Shear in a span

V(x) = V₀(x) + (Mᵣ − Mₗ) ÷ L

V(x) = V₀(x) + (Mᵣ − Mₗ) ÷ L

Reactions

Reactions

R = R₀ ± (Mᵣ − Mₗ) ÷ L + cantilever loads at the end support

R = R₀ ± (Mᵣ − Mₗ) ÷ L + cantilever loads at the end support

Deflection

Deflection

EI y″ = M(x), y = 0 at supports, slope continuous into cantilevers

EI y″ = M(x), y = 0 at supports, slope continuous into cantilevers

M₀, V₀, R₀ are the simply supported values of each span. The support moments are solved directly (tridiagonal system).

  • Moment and shear are exact. Deflection is integrated numerically at 96 points per span.

  • Supports are rigid and joints are pins: coupler rotational stiffness, slip and eccentricity are ignored.

  • Shear deformation is ignored for all members.

11. Superposition

One arrangement

One arrangement

M = Mevery bay + Mmoving or patterned (V, δ, R likewise)

M = Mevery bay + Mmoving or patterned (V, δ, R likewise)

  • The analysis is linear elastic, so loads acting on every bay are solved once and added to each moving or patterned arrangement.

  • Supports never lift off. A negative reaction is reported as uplift but the support stays in the model.

Part C — Results

12. Utilisation and result

Board, moment

Board, moment

uM = (M ÷ b) × kM (one board, no layers: M ÷ 0.475)

uM = (M ÷ b) × kM (one board, no layers: M ÷ 0.475)

Board, shear

Board, shear

uV = (V ÷ b) × kV (one board: V ÷ 4.60)

uV = (V ÷ b) × kV (one board: V ÷ 4.60)

Board, deflection

Board, deflection

uδ = δ ÷ (sₘ ÷ 100)

uδ = δ ÷ (sₘ ÷ 100)

Transom or ledger

Transom or ledger

u = max(|M| ÷ (n Mₐ), |V| ÷ (n Vₐ))

u = max(|M| ÷ (n Mₐ), |V| ÷ (n Vₐ))

Ledger coupler

Ledger coupler

u = |Ri,j| ÷ (nₗ × Fₛ)

u = |Ri,j| ÷ (nₗ × Fₛ)

Overall

Overall

u = max(uboards, uₜᵣₐₙₛₒₘₛ, uledgers, ucouplers)

u = max(uboards, uₜᵣₐₙₛₒₘₛ, uledgers, ucouplers)

Utilisation u

Result shown

u ≤ 90%

PASS

90% < u ≤ 100%

PASS · CLOSE

u > 100%

FAIL

  • span/100 is the BS EN 12811-1 deflection limit for platform units. Each board span uses its own length.

  • n = nₜ for transoms and nₗ for ledgers; |M| is the larger of sagging and hogging.

  • Transom and ledger deflections are shown but not checked against a limit.

  • The 90% band is a visual warning only; it is not a code limit.

13. Plan and upright reactions

Selected load case

Selected load case

Ri,j = largest over all its arrangements

Ri,j = largest over all its arrangements

All load cases

All load cases

Ri,j = largest over all active cases

Ri,j = largest over all active cases

Equilibrium (fixed loads only)

Equilibrium (fixed loads only)

Σ Ri,j = total load on the platform

Σ Ri,j = total load on the platform

  • The plan shows the load arrangement that governs the selected member, including where a moving load or q₂ area sits.

  • With pattern or moving loads each upright shows its own largest value, so the values do not add up to one arrangement.

  • Reactions are from this lift’s platform only. Other lifts, ties, bracing and wind are not included.

14. Section and member diagrams

Transom load band

Transom load band

w = q × fₖ (e.g. 2.00 kN/m² × 1.000 m = 2.00 kN/m)

w = q × fₖ (e.g. 2.00 kN/m² × 1.000 m = 2.00 kN/m)

Board load band

Board load band

w = q × b (e.g. 2.00 kN/m² × 0.225 m = 0.45 kN/m)

w = q × b (e.g. 2.00 kN/m² × 0.225 m = 0.45 kN/m)

Ledger loads

Ledger loads

transom reactions Tₖ in kN + ledger self-weight

transom reactions Tₖ in kN + ledger self-weight

Check line

Check line

total load = Σ R

total load = Σ R

  • Diagrams show the governing arrangement for the chosen member: loads and reactions, moment, shear and deflection.

  • A region left unloaded by pattern loading is drawn dashed and labelled “not loaded in this arrangement”.

  • Concentrated loads show the part that reaches the member, e.g. 1.5 kN → 1.31 kN on this transom.

15. Load case and combination tables

  • Utilisation by load case lists each member’s worst result in each case, and the largest upright reaction.

  • Ledgers and couplers lists each ledger’s worst moment and coupler load.

  • The combinations table repeats the full check for 2, 3 and 4 ledgers with 2, 3 and 4 uprights, using the same deck, members and loads.

16. Worked example (default inputs)

Class 3, 5 main boards + 2 inside boards on a cantilever (qᵢₙ = 0.75 kN/m²), 2 ledgers, 3 uprights, Lb = 2.0 m, one intermediate transom per bay (s = 1.0 m), steel tubes (Mₐ = 1.12 kNm), class B couplers (Fₛ = 9.1 kN), one board layer.

Board — LC5, 1.0 kN point load at x 0.5 m (mid-span of span 1, board 2):

Self-weight on one board w = 0.245 × 0.225

0.0552 kN/m

M = 0.0552 × 1.0² ÷ 8 + 1.0 × 1.0 ÷ 4 − 1.0 × 0.1 ÷ 8

0.244 kNm

u = 0.244 ÷ 0.475

51%

Transom T2 — LC1, bay 1 loaded on the main boards, inside boards unloaded:

wₘₐᵢₙ = 2.245 kN/m over 1.125 m; wᵢₙ = 0.245 kN/m over 0.450 m; tube 0.0429 kN/m

total 2.709 kN

Cantilever moment at L2 = −0.245 × 0.45 × 0.2492 − 0.0429 × 0.524² ÷ 2

−0.033 kNm

RL1 = (2.526 × 0.5867 + 0.0429 × 1.1733² ÷ 2 − 0.033) ÷ 1.1733

1.260 kN

M at zero shear (x = 0.574 m) = 1.260 × 0.574 − 0.0429 × 0.574² ÷ 2 − 2.245 × 0.550² ÷ 2

0.377 kNm

u = 0.377 ÷ 1.12

34%

Ledger 2 (inner) — LC1, bay 2 loaded: transom loads T2 = 0.33 kN, T4 = 1.86 kN.

Support moment at U2: 8 MB = −(0.33 × 1.5 + 1.86 × 1.5 + 2 × 0.0429 × 2)

−0.432 kNm

M under T4 = 1.86 ÷ 2 × 1.0 + 0.0429 × 1.0 − 0.0429 ÷ 2 − 0.432 ÷ 2

0.735 kNm

u = 0.735 ÷ 1.12

66%

Coupler L2 at U2 (all bays loaded): 4.52 ÷ 9.1

50%

Load case

Arrangements

Boards

Transoms

Ledgers

Couplers

LC1 Uniform load q₁

9

13%

34%

66%

50%

LC2 Concentrated F₁

319

28%

26%

58%

32%

LC3 Concentrated F₂

402

49%

22%

52%

30%

LC5 Point loads

3

51%

46%

57%

27%

Worst

–

51%

46%

66% — governs

50%

Ledgers

Uprights

Boards

Transoms

Ledgers

Couplers

Max R kN

2

2

51%

42%

85%

21%

1.93

2

3

51%

46%

66%

50%

4.52

2

4

51%

46%

70%

47%

4.32

3

2

51%

10%

79%

18%

1.64

3

3

51%

10%

72%

43%

3.88

3

4

51%

10%

71%

41%

3.73

4

2

51%

10%

69%


1.54

4

3

51%

10%

54%

32%

2.95

4

4

51%

10%

54%

31%

2.80

All values agree with the calculator’s output for the default inputs. Upright reactions, LC1: L1 1.17 / 3.10 / 1.17 kN and L2 1.71 / 4.52 / 1.71 kN at U1 / U2 / U3. With 18 mm plywood added, the boards drop from 51% to 26%.

Part D — Component data

17. Scaffold beams, tubes and boards

Member

Mₐ kNm

Vₐ kN

kg/m

I cm⁴

A cm²

EI kNm²

Ladder Beam

13.50

12.00

11.9

2,600

11.10

5,271

Unit Beam

27.70

18.50

14.5

10,572

–

21,320

Haki 750

41.30

30.60

7.5

17,182

16.90

11,856

Haki 450

15.70

12.70

4.2

4,481

11.10

3,087

Apollo X 750

42.90

45.40

8.0

17,097

12.14

11,796

ASP 750

36.50

30.70

6.5

16,563

12.32

11,594

Layher 450

13.94

12.32

5.0

4,481

–

3,137

Layher 750

33.50

25.60

6.0

15,195

–

10,637

Dessa D78

38.87

31.66

5.5

16,520

12.30

11,399*

Triangle Rail

11.20

21.60

10.68*

281

13.60

576*

Steel tube 48.3 Ø (default)

1.12

29.10

4.37

13.77

5.57

28.22*

Aluminium tube 48.3 Ø

1.33

25.52

1.65

–

6.15

10.45

Scaffold board 38 × 225

0.475 per board

4.60 per board

25 kg/m²

–

–

29.0 per m width

Values marked * are derived, not taken from a datasheet:

Steel tube 48.3 × 4.0

EI = 205 GPa × 13.77 cm⁴ = 28.2 kNm²

Dessa D78 (aluminium)

EI = 69 GPa × 16,520 cm⁴ = 11,399 kNm²

Triangle Rail (steel assumed)

EI = 205 GPa × 281 cm⁴ = 576 kNm²; 13.6 cm² × 7,850 kg/m³ = 10.68 kg/m

Board EI read per metre width


Board values per metre width

m = 0.475 ÷ 0.225 = 2.111 kNm/m; v = 4.60 ÷ 0.225 = 20.44 kN/m

  • Safe working values are from manufacturers’ datasheets and must be checked against current manufacturer information. All values are editable on the Component data tab.

  • The board EI is taken per metre width because per board it would need E ≈ 28,000 N/mm², which is not possible for timber.

18. Plywood

Per metre width, face grain along the span, from typical values over the full thickness t:

Safe moment, σ = 8 N/mm²

Safe moment, σ = 8 N/mm²

Mₐ = 8 × 1000 t² ÷ 6 ÷ 10⁶ = 8 t² ÷ 6000 (kNm/m)

Mₐ = 8 × 1000 t² ÷ 6 ÷ 10⁶ = 8 t² ÷ 6000 (kNm/m)

Safe shear, τ = 0.5 N/mm²

Safe shear, τ = 0.5 N/mm²

Vₐ = 0.5 × (2/3) × 1000 t ÷ 1000 = t ÷ 3 (kN/m)

Vₐ = 0.5 × (2/3) × 1000 t ÷ 1000 = t ÷ 3 (kN/m)

Stiffness, E = 6,000 N/mm²

Stiffness, E = 6,000 N/mm²

EI = 6000 × 1000 t³ ÷ 12 ÷ 10⁹ = 0.0005 t³ (kNm²/m)

EI = 6000 × 1000 t³ ÷ 12 ÷ 10⁹ = 0.0005 t³ (kNm²/m)

Self-weight, 600 kg/m³

Self-weight, 600 kg/m³

0.6 t (kg/m²)

0.6 t (kg/m²)

Thickness

Mₐ kNm/m

Vₐ kN/m

EI kNm²/m

kg/m²

6 mm

0.048

2.00

0.108

3.6

9 mm

0.108

3.00

0.364

5.4

12 mm

0.192

4.00

0.864

7.2

15 mm

0.300

5.00

1.688

9.0

18 mm (default layer)

0.432

6.00

2.916

10.8

22 mm

0.645

7.33

5.324

13.2

25 mm

0.833

8.33

7.813

15.0

  • These are typical figures, not a supplier’s data. Replace them with the supplier’s declared values.

19. Right-angle couplers

Coupler

Slipping force kN

Cruciform stiffness kNm/rad

Cruciform bending kNm

Class A

6.1

10.0

0.32

Class B (default)

9.1

15.0

0.48

  • Only the slipping force is used in the checks. Cruciform values are for reference; joints are analysed as pins.

20. Not checked

  • Uprights (standards), base plates, sole boards and ground bearing.

  • Ties, bracing, wind, lateral and dynamic loads.

  • Transom-to-ledger fixings, check couplers and hop-up brackets.

  • System scaffold components; use the manufacturer’s data.

  • Loads from other lifts. The checker covers one boarded lift.

Guidance only. Imposed loads are the BS EN 12811-1 service classes used by TG20:21; the 0.75 kN/m² inside board load is a default, not a TG20 value. Safe working values are from manufacturers’ datasheets; board EI is taken per metre width and plywood properties are typical values, so replace them with your supplier’s data. Boards are simply supported between transoms and checked to span/100; transoms and ledgers are continuous beams with pinned joints and rigid supports; layers share load by stiffness; g = 9.81 m/s². Uprights, ties, bracing, wind and fittings other than ledger couplers are not checked. Designs should be checked by a competent temporary works engineer. Results are for preliminary estimation and educational purposes only. They do not replace professional engineering judgement, applicable codes and standards, or design verification by a qualified engineer. Use at your own risk.

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Results are for preliminary estimation and educational purposes only. They do not replace professional engineering judgement, applicable codes and standards, or design verification by a qualified engineer. Use at your own risk. Product names are trademarks of their respective owners and are used only to identify the product; this site is not affiliated with or endorsed by any manufacturer.

© 2026 ScaffoldCalculators.com. All rights reserved.

Built with AI assistance · reviewed by an engineer

Portrait of P. G. Kosatko

No sign-up, no paywall. If a calculator saved you time, a coffee helps keep it free and growing. Thank you!

Results are for preliminary estimation and educational purposes only. They do not replace professional engineering judgement, applicable codes and standards, or design verification by a qualified engineer. Use at your own risk. Product names are trademarks of their respective owners and are used only to identify the product; this site is not affiliated with or endorsed by any manufacturer.

© 2026 ScaffoldCalculators.com. All rights reserved.

Built with AI assistance · reviewed by an engineer

No sign-up, no paywall. If a calculator saved you time, a coffee helps keep it free and growing. Thank you!

Results are for preliminary estimation and educational purposes only. They do not replace professional engineering judgement, applicable codes and standards, or design verification by a qualified engineer. Use at your own risk. Product names are trademarks of their respective owners and are used only to identify the product; this site is not affiliated with or endorsed by any manufacturer.

© 2026 ScaffoldCalculators.com. All rights reserved.

Built with AI assistance · reviewed by an engineer