E-Glass (Electrical Glass) Fiberglass

E-glass is the everyday aircraft fiberglass: low cost, white, non-conductive and corrosion-free. It is used on fairings, radomes, wing tips and rotor blades, not on the main load path.

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Fiberglass, aramid and carbon fiber cloth side by side
Fiberglass is white, aramid yellow and carbon black. FAA-H-8083-31B, Fig. 7-7

E-glass at a glance

Where to buy
ItemWhat the sources saySource
NameElectrical glass: identified as such for electrical applications; high resistance to current flowFAA-H-8083-31B, p. 7-5
CompositionBorosilicate glassFAA-H-8083-31B, p. 7-5
AdvantagesLower cost than other composites; chemical and galvanic corrosion resistance; does not conduct electricityFAA-H-8083-31B, p. 7-5
Colour and formsWhite; dry fabric or prepregFAA-H-8083-31B, p. 7-5
Typical usesSecondary structure such as fairings, radomes and wing tips; helicopter rotor bladesFAA-H-8083-31B, p. 7-5
Fabric weights1.4 oz/yd² (48 g/m², styles 108 and 1080) to 19.7 oz/yd² (668 g/m², style 7587); dry thickness 2.2 to 27.2 milHexcel HexForce data sheets
Breaking strength of fabric80 to 750 lbf/in (warp) across those styles; 7781 is 570 / 450 lbf/in warp / fillHexcel HexForce data sheets
Service temperatureNot set by the glass; set by the resin and cure (see the resin pages)—

Fabric figures come from the Hexcel HexForce sheets for styles 108, 1080, 120, 1581, 7500, 7580, 7587 and 7781, all E-type yarn. Full table on the glass fabric styles page.

Using E-glass in a repair

AC 43.13-1B paragraph 3-2 covers repairs to fiberglass laminate used for non-structural fairings, covers, cowlings and honeycomb panel facings. It says these repairs are not to be used on radomes or on advanced composite parts such as carbon or Kevlar.

The material rule comes first: the repair material must preserve the strength, weight, aerodynamic and electrical properties of the part, best done with the same chemical composition or a manufacturer-approved substitute (paragraph 3-1a). Moisture left on the surface inhibits the cure of the resin, so the laminate is dried thoroughly before bonding.

For a carbon part, fiberglass is not a free substitute. Where glass touches carbon under aluminium, or is used as the isolating ply, the SRM says how. See repair materials by part.

Light fiberglass facing repair (AC 43.13-1B 3-2)

StepActionWhat to do
1CheckTap test for voids and delamination. Remove paint by dry sanding; no chemical strippers.
2CleanWash with detergent and water, then an acceptable cleaner.
3Sand and re-cleanSand with 280-grit paper, clean off residue and moisture, and dry the laminate.
4Resin or pliesMix resin per the maker. Surface scars: one or two coats. Deeper: contoured glass cloth soaked in resin.
5Peel plyCover with peel ply, work out bubbles and excess resin, let it cure.
6FinishSand to contour, seal all edges against water, refinish.

Questions people actually ask

Is E-glass the same as fiberglass?

It is the most common type. S-glass and S2-glass are the higher-strength structural types (FAA-H-8083-31B, p. 7-5).

Does E-glass corrode against aluminium?

The FAA lists corrosion resistance, chemical and galvanic, as an advantage of fiberglass. Carbon is the one that is cathodic against aluminium.

Limits — when NOT to use this

  • Not primary structure. The sources place it in secondary structure.
  • Not for radomes or advanced composites by AC 43.13-1B 3-2 methods. Those need the manufacturer’s data.
  • No strength allowable here. Laminate strength depends on resin and ply schedule, which the SRM gives.

Where to buy

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Distributors coming soon.

Sources

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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