Sheet Metal Stamping & Press Lines worked example
Die Changeover Cost at 92% cost capture factor: a worked example in sheet metal stamping & press lines
What does the result look like when cost capture factor reaches 92%? The full calculation is worked below with real intermediate numbers. Use it when die changeover cost in sheet metal stamping and press lines is being put through a sheet metal stamping and press lines weighted-cost review.
The inputs for this scenario
- Parts run before the changeover: 100 units (unchanged)
- Machine cost rate: 45 $ / unit (unchanged)
- Cost capture factor: 92 % (raised for this scenario; the documented default is 80)
- Fixed setup cost: 250 $ (unchanged)
Working through the calculation
- Applying the documented formula (Die Changeover Cost cost = quantity × rate × capture factor + fixed cost) to the inputs above produces each figure below.
- At this operating point the engine returns 4,390 $ for weighted cost, the number this scenario is built around.
- At this operating point the engine returns 43.9 $ / piece for per piece value.
- At this operating point the engine returns 4,140 $ for captured value.
- At this operating point the engine returns 250 $ for fixed adjustment.
How this compares with the baseline
- Against the tool's baseline example, where cost capture factor sits at 80% and the headline result is 3,850 $, this scenario comes in 14.03% above the baseline at 4,390 $.
- A figure at this level is achievable when cost capture factor is genuinely sustained, not just peaked for a shift. It assumes a linear per-unit rate and a single fixed cost, so it will not model a changeover whose crew size or downtime scales nonlinearly with the die.
Results at a glance
- Weighted cost: 4,390 $ (headline result)
- Per piece value: 43.9 $ / piece
- Captured value: 4,140 $
- Fixed adjustment: 250 $
Run it with your numbers
- Every input above is editable in the live Die Changeover Cost calculator, which recalculates instantly and can be shared with the inputs intact.
Last reviewed 2026-05-12.