Clips and Retainers
Thin-gauge attachment and retention parts with controlled spring geometry and edge condition.
Build-to-print formed clips, shims, brackets, covers and retention parts for aerospace equipment programs. DRAmetal controls released material, tooling, first articles and production records; the design authority owns stress, fatigue, airworthiness and final part approval.
Stamping is appropriate when the released geometry, material behavior and demand justify controlled tooling. Low-volume soft tools and production dies can follow different qualification routes.
Thin-gauge attachment and retention parts with controlled spring geometry and edge condition.
Repeat brackets with ribs, offsets, joggles and drawing-defined hole-to-form relationships.
Flat and lightly formed parts with material, thickness and profile traceability.
Stamped covers, guards and lightweight shields for released equipment assemblies.
DRAmetal manufactures to the approved drawing, tooling and quality plan. The aerospace design authority owns loads, fatigue, airworthiness, qualification and final part release.
Tooling level is selected from annual volume, geometry stability, material and qualification requirements.
Retention Thin-gauge stamped hardware for released attachment and retention functions.
Structural Repeat formed brackets with offsets, ribs and localized features.
Precision Profiled shims, spacers and thin plates with controlled thickness and burr direction.
Protection Lightweight formed metal covers for equipment and subsystem protection.
| Materials | Drawing-defined aluminum, stainless steel, titanium, nickel alloys and specialty strip with lot traceability |
|---|---|
| Tooling | Laser and brake prototypes, soft tooling, compound dies or progressive tooling according to released production plan |
| Processes | Blanking, forming, drawing, piercing, restrike, deburring, cleaning, finishing and secondary machining where specified |
| Critical controls | Material grain, thickness, form angle, springback, hole-to-form position, burr direction and surface condition |
| Documentation | Material records, tool revision, first-article report, inspection plan and nonconformance control as contractually required |
| Supply boundary | Build-to-print stamped hardware; the aerospace design authority owns stress, fatigue, material allowables, airworthiness and final approval |
Confirm drawing, material, volume, qualification and record-retention requirements.
Review grain, radii, springback, draw depth, burr direction and finish allowance.
Use laser and forming or soft tooling to validate geometry before production-tool release.
Control die datums, stations, restrike features and tool revision.
Inspect released characteristics and document results through the agreed approval route.
Maintain material lot, tool condition, in-process checks and protected packout.
A stable die cannot compensate for uncontrolled strip direction, material temper or tool revision.
Alloy, temper, grain and tool geometry interact at every formed feature.
Burrs and feature drift require defined in-process checks and maintenance triggers.
Strip and sheet identity must remain connected to released part records.
Drawing and tool changes require coordinated approval before production.
Materials, fabrication decisions and results for an anonymous customer project.

Component reference image
Wrinkling, springback and surface damage made thin-sheet dimensions inconsistent.
Results apply to the project configuration described on the linked page.
Read the Customer Project →Early formed parts can inform a controlled production tooling release.
Grain, temper and lot identity are carried through fabrication and inspection.
Released characteristics are mapped to the agreed inspection record.
Part, tool and process revisions remain linked through production.
We manufacture build-to-print clips, retainers, formed brackets, shims, plates, covers and shields.
Yes. Laser blanks, press-brake forming and soft tools can support development or lower volumes before production dies are justified.
We can provide the contractually defined first-article and dimensional records against the released drawing and revision.
No. The aerospace design authority owns design, stress, fatigue, qualification and airworthiness. We manufacture released parts.
Send drawings, models, material specifications, grain direction, annual volume, tooling ownership, inspection and record requirements, finish and quantities.
Send drawings, material and grain requirements, volumes, tooling plan, first-article requirements, finish and quantities for review.