Finishing and Painting a Composite Repair

A composite repair is not finished when the cure ends. The resin needs a top coating against ultraviolet light, leading edges and panel edges need protection from erosion, and on many parts the conductive coating that carries lightning current has to be put back. The finish system, its layer order and thickness come from the SRM or the paint maker; the FAA Handbook gives the steps around it.

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Finish removed and restored over a scarf repair

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Section through a scarf repair with the old finish removed one inch beyond the taper and primer, conductive coating and topcoat restored; detail of the lightly sanded patch surface with uncut fibres and primer; tables of primers for composite and paint stripping methods; parts list
Section, detail of the patch surface, primers, stripping methods and parts list, after FAA-H-8083-31B chapters 7 and 8. Not to scale; the finish system comes from the SRM or the paint maker.

Why the finish matters on composite

Ultraviolet light. UV light affects the strength of composite materials, so composite structures are protected by a top coating; special UV primers and paints have been developed for them (H-31B p. 7-15).

Erosion. Composites erode more easily than aluminium, so leading edges generally carry an erosion coating, and the edges of doors and panels exposed to the air stream can erode too (p. 7-14).

Lightning. A repair removes the exterior finish including the conductive coating over an area at least 1 inch larger than the border of the taper; the last step of the repair applies the top finish and the conductive coating again (pp. 7-35, 7-37).

Preparing the surface

1. Remove the finish far enough. At least 1 inch (about 25 mm, not the official figure) beyond the border of the taper, conductive coating included (p. 7-35).

2. Strip with care. Plastic media blasting has been used on composite surfaces because it leaves less visual damage than sanding the paint off; laser stripping has been developed to remove coatings from composites (p. 8-20). Check the method against the SRM before use.

3. Sand the patch lightly. After the cure, lightly sand the repair patch to a smooth finish without damaging the fibres; the patch should be free of pits, blisters, resin-rich and resin-starved areas (p. 7-37).

4. Seal before paint. Composite cowlings and plastic fairings must be properly sanded and sealed before painting, or sanding scratches show through the finish (p. 8-14).

5. Clean. Improper cleaning and preparation is the first cause of poor adhesion (p. 8-12). Use the cleaner the SRM names; acetone is a strong solvent for most plastics (p. 8-1).

Primers over composite

PrimerUseSource
Epoxy sanding primerExcellent base over composites; finish sanded with 320 grit on a dual action orbital sander; compatible with two-part epoxy primers and polyurethane topcoatsH 8-9
Gray enamel undercoatSingle-component, non-sanding; a good primer for composite substratesH 8-3
UV primers and paintsProtect composite structure from UV lightH 7-15

Priming and painting

Composite surfaces that need priming range from the whole aircraft to fairings, radomes, antennas and control surface tips (p. 8-9). Prime, restore the conductive coating and apply the topcoat in the order and to the thickness the SRM or the paint maker gives. Zinc chromate is not used under polyurethane paints (p. 8-9).

Wear a charcoal-filtered, double-cartridge organic vapour respirator for spraying and sanding (p. 8-8).

What to check when the finish is done

CheckHowSource
Patch surface smooth, fibres intactVisual, before primerH 7-37
Conductive coating restored over the whole stripped areaVisual against the SRM; electrical check if the SRM asksH 7-35, 7-37
No sanding scratches, fisheyes or blushingVisual, in good lightH 8-12 to 8-14
Repair inspected after finishingVisual, tap and/or ultrasonicH 7-37

Defects and fixes

DefectCauseFixSource
Sanding scratches show throughComposite not sanded and sealed before the finishSand and seal before the finish coatsH 8-14
Poor adhesionPoor cleaning, wrong primer, topcoat not compatible with the primerRemove the finish completely, correct the cause, refinishH 8-12
Fibres cut on the patchSanding too hard after the cureSand lightly; disposition of cut fibres by the SRMH 7-37
Lightning protection lostConductive coating not restoredApply the conductive coating as the SRM saysH 7-37
Edges erodingEdges exposed to the air stream without protectionErosion coating as the SRM saysH 7-14

Questions people actually ask

How far beyond the repair does the paint come off?

At least 1 inch beyond the border of the taper, conductive coating included, per the Handbook. The SRM may ask for more.

Can composite be sanded to bare fibre before painting?

No. The Handbook says to lightly sand the patch to a smooth finish without damaging the fibres.

Which primer goes on composite?

Epoxy sanding primers are described as an excellent base over composites, and gray enamel undercoat as a good primer for composite substrates. The SRM or the paint maker names the system.

Why put the conductive coating back on a small repair?

It is part of the lightning protection; the Handbook's repair steps end with the top finish and the conductive coating.

Limits of this guide

What the sources support, and no further.

  • The manual governs. Finish system, layer order, film thickness and conductive coating come from the SRM or the paint maker.
  • Stripping. Chemical strippers are not covered here; use only what the SRM allows on composite.
  • Radomes. Radome finishes have their own limits in the SRM.

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Sources

  • FAA-H-8083-31B, Aviation Maintenance Technician Handbook: Airframe, Chapters 7 and 8 — p. 7-14, erosion and erosion coatings; p. 7-15, UV light and top coatings; p. 7-35, finish and conductive coating removed 1 inch beyond the taper; p. 7-37, light sanding, top finish and conductive coating, post-repair inspection; p. 8-1, acetone; p. 8-3, gray enamel undercoat; p. 8-8, respirators; p. 8-9, primers over composite surfaces; pp. 8-12 to 8-14, finish defects; p. 8-20, plastic media blasting and laser stripping.
Educational reference only. not approved data. Always consult the applicable SRM, AMM, or AC 43.13-1B and your certifying authority.
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