Case study · Aerospace tooling

Aerospace Drill Jig Fixture — Precision Hole-Pattern Tooling

An aluminum drill jig with hardened bushings and tight positional tolerances, hardcoat anodized and documented for repeatable aerospace hole patterns on the assembly line.

  • Drill bushings
  • ±0.02 mm position
  • Documented FAI
Machined aluminum aerospace drill jig fixture with hardened drill bushings
Representative project image — replace with the production photo when available.
Project overview

Project overview

This project is an aluminum drill jig — a fixture whose whole job is to transfer a precise hole pattern into an aerospace assembly, part after part, without a CNC machine at the point of use. Hole position drives fit and fastener integrity on the assembly, so the jig has to place every hole in exactly the same spot over its production life.

Two things make that possible. First, the bushing bores are held to ±0.02 mm true position off hard tooling datums, so the pattern is accurate and repeatable at setup. Second, hardened, replaceable drill bushings carry the drilling wear — drills chew through aluminum quickly, so the wear lives in a swappable insert instead of the jig body. The body itself is stress-relieved and hardcoat anodized so it holds its geometry through handling and use.

Every tool ships with a documented CMM inspection report tying the bushing positions back to the tooling datums. Material, fixture size, and program quantities are placeholders — the datum strategy, hardened bushings, and documented inspection are representative of the aerospace tooling we machine, with no confidential program details fabricated.

Technical specification

Part specification

Key manufacturing parameters for this project. Values marked as placeholders stand in for confidential production data.

ParameterSpecification
Fixture sizePlaceholder — sized to the assembly footprint
Bushing hole position±0.02 mm true position off tooling datums
Bushing bore fitPress / slip fit per bushing spec
Datum schemeHard tooling datums for repeatable setup
Flatness0.05 mm across the locating face
General tolerance±0.05 mm (ISO 2768-f unless noted)
Engineering challenges

What made this part difficult

The manufacturability risks we planned around before cutting metal.

Positional accuracy of the hole pattern

The jig exists to transfer a hole pattern accurately, part after part. Bushing bores were held to ±0.02 mm true position off hard tooling datums so every drilled hole lands in the same place.

Wear at the drill bushings

Drills wear aluminum bores quickly, so hardened, replaceable drill bushings carry the wear and can be swapped without scrapping the jig.

Stability over the tool's life

A jig that moves is worse than no jig. The body was stress-relieved and hardcoat anodized so it holds its geometry through production use.

Manufacturing process

How the part was made

The routing from raw stock to finished, inspected components.

  1. Step 1: Engineering review
    Confirmed datum scheme, bushing fits, and positional tolerances before quoting.
  2. Step 2: Body machining
    Fixture body machined from tooling-grade aluminum plate with a stress-relief step.
  3. Step 3: Datum finishing
    Hard tooling datums and locating face finished to establish the reference.
  4. Step 4: Bushing bore machining
    Bushing bores machined to fit and ±0.02 mm position off the datums.
  5. Step 5: Masking and hardcoat
    Bushing bores masked, then hardcoat anodize on the body wear surfaces.
  6. Step 6: Bushing fit and documented inspection
    Hardened bushings fitted, then full CMM inspection with a documented report.
Inspection methods

How quality was verified

Dimensional and process controls used to sign off the part. See our full aluminum part inspection process.

CMM positional report

Bushing positions mapped on a CMM against the tooling datums, with a documented report supplied for the program.

Bushing fit verification

Bushing bore fits confirmed before and after finishing.

First article inspection

Full FAI on the tool with documentation. Placeholder for the program's specific quality requirements.

Surface finishing

Finishing and post-processing

Finishing decided alongside the machining plan. Compare options in the aluminum surface finishes hub.

Hardcoat anodize (Type III)

Wear-resistant surface on the jig body so handling and contact don't degrade the tool over its life.

Masked bushing bores

Bushing bores masked so hardcoat growth does not disturb the press/slip fits.

Chem-film option

Chem film available where conductivity or a thinner coating is preferred on specific features.

Typical application

Where this drill jig is used

Drill jigs let an assembly line transfer a precise hole pattern into structure repeatedly, without a CNC machine at the point of use — critical for aerospace assemblies where hole position drives fit and fastener integrity.

Aluminum with hardened bushings gives a light, handleable tool that still resists drill wear, and hardcoat anodize keeps the body stable through production.

  • Manufacturability review
    Every project starts with an engineering review of tolerances, wall thickness, and finish before we quote.
  • Prototype to production
    The same routing scales from a first article to recurring production batches.
  • Documentation
    Material certificates and first article inspection reports are available on request.
Explore the engineering

Related capabilities, materials, and pages

This project connects to our wider aluminum machining program. Start with our engineering capabilities, then dive into the specific products, materials, industries, and finishes involved.

Have a similar part? Get it quoted by an engineer

Upload your CAD model and drawing with alloy, finish, and tolerance notes. We review manufacturability before quoting — not after the parts are on the machine.

  • Engineering review within one business day
  • Prototype to production
  • Material certificates available
  • ISO 9001 quality management