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| General purpose liner constructed from woven E-glass cloth with a polyester resin system. Qualified to Boeing specifications BMS8-2, Class 1 Grade A. |
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| High wear resistant liner constructed from woven E-glass cloth with a polyester resin system. Qualified to Boeing specifications BMS8-2, Class 3 Grade A. |
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| High impact resistant grade liners constructed of woven E- and S-glass cloth with a polyester resin system to optimize strength, weight and cost.
Qualified to Boeing specifications BMS8-2, Class 2 Grade A and Grade B. |
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| Woven fiberglass reinforced phenolic "h" profile used for the installation of cargo decompression panels. Qualified to Airbus technical specification 2550 M1M 0004 00. |
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| Unidirectional S-2 glass® reinforced phenolic facings meta-aramid honeycomb core floor panel. Qualified to BAe specification BAER 3232. |
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| Unidirectional S-2 glass reinforced phenolic facings meta-aramid honeycomb core floor panel. Qualified to BAe specification MAT 006. |
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| Unidirectional graphite reinforced epoxy facings meta-aramid honeycomb core floor panel. Qualified to Embraer specification MEP 15-030. |
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| Unidirectional S-2 glass reinforced epoxy facings meta-aramid honeycomb core floor panel. Qualified to McDonnell Douglas specification BZZ 7002 Types 1 thru 3, Embraer MEP 15-031 and BAe MAT 003. |
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| Woven fiberglass reinforced phenolic facings/ honeycomb core sandwich panel. Qualified to McDonnell Douglas specifications 9100059, S3933941, S3933942. |
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| Aluminum facings/aluminum honeycomb core sandwich panel. Qualified to Lockheed specification LAC-C-28-1145 Ty 5, 7, 9 and 10. |
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| Gillfab® 4034 panel is a high performance sandwich panel with epoxy resin pre-impregnated carbon facings and aluminum core. |
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| Unidirectional carbon reinforced phenolicmeta-aramid honeycomb core, low smoke floor panel. Qualified to McDonnell Douglas specification 9D0207 Ty 1 and 2, BAER 3231, Gr M & L. |
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| Gillfab® 4117 is a sandwich panel made with facings of fiberglass cloth reinforced epoxy laminate and aramid honeycomb core. |
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| Woven fiberglass cloth reinforced phenolic facings/ honeycomb core floor panel. |
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| Woven fiberglass reinforced phenolic facings meta-aramid honeycomb core, lightweight and low smoke sandwich panel. Qualified to McDonnel Douglass specifications 3962952, Embraer MEP 15-029 and Lockheed LAC-LS60204. |
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| Woven fiberglass cloth reinforced phenolic facings meta-aramid honeycomb core floor panel. Qualified to Airbus technical specification 5360 M1B 000500, (BCC2). |
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| Type 1 - Woven fiberglass cloth reinforced epoxy facings honeycomb core floor panel. Type 2 identical except for a sheet of aluminum foil bonded to the bottom facing. Qualified to Airbus technical specification TL53/5000/79, Annex A Types 1 and 2. |
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| Unidirectional fiberglass reinforced epoxy facings meta-aramid honeycomb core floor panel. 4417 is qualified to Boeing specification BMS 4-17, Ty I thru V, IX and Drawing 69B15779 (Ty V). Unidirectional fiberglass reinforced epoxy facings meta-aramid honeycomb core floor panel. 4417A is qualified to Boeing specification BMS 4-17, Ty VI. |
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| Woven fiberglass cloth reinforced phenolic laminate with 1 mil overlay meta-aramid honeycomb core, high-impact resistant cargo liner panel. Qualified to Airbus technical specification 2550 M1M 0008 00. |
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| Unidirectional carbon/woven glass reinforced phenolic facings meta-aramid honeycomb core floor panel. |
