The exhaust manifold tooling lead time runs 5–7 weeks for a four-cavity wax tool plus the first poured article. Three to four weeks go into design and cavity cutting, and one to two into the first wax, shell and pour. The clock starts at design freeze, not at the first email.
The tool phase is four steps that cannot be compressed by adding people. Design review fixes the shrinkage compensation at 2.2 %, the three parting lines and the eight ejector positions, then issues the tool drawing for approval. Cavity cutting runs on a three-axis machining centre with EDM for the corners, and the cavity is held to ±0.05 mm with Ra 0.8 on the sealing faces. Bench fitting closes the tool and checks the parting gap before any wax is injected.
Most of the 3–4 weeks sits in cutting and fitting, not in design. A four-cavity tool for this manifold has two cores and three parting surfaces, and each one is fitted by hand before the first close. That is the step where a schedule is won or lost: an approved drawing cuts faster than a drawing that changes at the bench.
One to two weeks covers first wax to first casting. The first pattern is injected at 75 °C and 0.3 MPa with an 8 s hold and 60 s cooling, then measured on a CMM against the compensated CAD.
The shell takes 7 layers with 8 h of drying per layer, which is about 2.5 days of calendar time, followed by dewax at 165 °C and 7 bar, burnout at 1000 °C, and the pour. The first casting is then checked to CT6 under ISO 8062-3.
The pour itself is one shift. What takes the week is the sequence around it: the first pattern has to be right before the shell is built, because a shell around a wrong pattern wastes 2.5 days. That is why the first-article plan puts the four wax measurements ahead of the shell, and why a tool correction found at that point saves a week rather than costing one.
Preparation can overlap with cutting; the sequence after the first pattern cannot. The wax lot, the shell material and the CMM program can all be ready while the cavity is still on the machine. The gating design can be reviewed on CAD, and the press parameters can be pre-set from the tool card.
The hard sequence is short and fixed: cavity, first wax, shell, pour. An automatic wax press shortens the production cycle later, but it cannot shorten this first loop, because the first pattern is a measurement rather than a production run.
Four things move the date, and all four are decisions rather than capacity.
Each one is listed below with the delay it adds.
A design change after the tool drawing is released. A parting-line change means re-cutting two faces and re-fitting, which adds about a week.
A compensation decision without a reference. If the first article lands outside 0.2 mm, the tool goes back for correction and the first loop restarts.
Shell trials on an unproven wax lot. Seven layers at 8 h each cannot be compressed below about 2.5 days without risking the shell.
A booked furnace or CMM queue. The pour and the first measurement each need a slot, and a full week adds days at both ends.
None of these is solved by asking for a shorter date. Each is solved by fixing the input before the step starts: a frozen drawing, a reference part, a proven wax lot and a booked slot.
The 5–7 weeks starts at design freeze. It does not include drawing changes after release, procurement of an unusual stainless grade, or shipping. It also does not scale linearly with cavity count: a second four-cavity tool adds cutting and fitting time, but the design and the first-article sequence stay the same.
The number is also not a promise for a different part. A manifold with internal cores and a cored turbo inlet needs more tool work than this one, and a production case on lost wax casting production shows how the sequence behaves across a full project rather than a single tool.
Send the drawing, the annual volume and the alloy, and we will return a tool build and first-article schedule with the four decision points marked, priced together with the vacuum investment casting route before the tool is ordered.