HIGH-PERFORMANCE COMPOSITE PRODUCTS SINCE 1945
Product Description
Gillcore® HD is an aramid fiber reinforced honeycomb which is coated with phenolic resin.
Gillcore® HK is a reinforced honeycomb. It offers a significant 25% weight savings over honeycomb.
Woven fiberglass cloth reinforced phenolic laminate. Service temperature range: 350 degrees F continuous, intermittent to 500 degrees F. Qualified to McDonnell Douglas specification DMS 1556.
Woven fiberglass cloth reinforced phenolic laminate. Service temperature range: Up to 300 degrees F. Qualified to McDonnell Douglas specification DMS 1558, Type 2.
Woven fiberglass cloth reinforced phenolic, very high impact resistant, low smoke and toxicity cargo liner with white on the face side for reflectivity. Qualified to Boeing specification BMS 8-223 Cl 2 Gr B, all types, McDonnell Douglas specification DMS 2419 Ty 50-90 and LAC-C-22-1249 Cl 3.
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and toxicity cargo liner with white on the face side. Qualified to Boeing specification BMS 8-223 Cl 2 Gr B Types 13 thru 40, McDonnell Douglas DMS 2419 Cl 1 (Ty 13-40), and Airbus 2550 M1M 000800.
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and toxicity cargo liner with white on the face side. 20-25% lighter in weight than 1367A with no sacrifice to mechanical properties.
1367B Qualified to Boeing Specification BMS 8-223 Cl 4 Gr B Type 13, 20, 30, 40 and 50.

1367M Meets Requirements Of (MRO) BMS 8-223 Cl 4 Gr B Type 13, 20, 30 and 40.
Woven fiberglass reinforced phenolic facings/ honeycomb core sandwich panel. Qualified to McDonnell Douglas specifications 9100059, S3933941, S3933942.
Unidirectional fiberglass reinforced epoxy facings/aluminum honeycomb core floor panel. Qualified to McDonnell Douglas specification BZZ 7002 Ty IV and V.
An aircraft grade sandwich panel made from aluminum alloy facings bonded to end grain balsa wood core. McDonnell Douglas Drawing S4929905.
Woven fiberglass cloth reinforced polyester with white overlay face side, high impact resistant cargo liner. Qualified to McDonnell Douglas specification DMS 1946 Type 1.
Woven fiberglass cloth reinforced phenolic, very high impact resistant, low smoke and toxicity cargo liner with white on the face side. Qualified to McDonnell Douglas specification DMS 2226 Ty 1 Cl 1.
Gillfab® 1367G is a high impact resistant, low smoke and toxicity, fiberglass reinforced phenolic laminate. For technical and product performance data please contact The Gill Corporation.
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke, and toxicity cargo liner with white on the face side or on both sides. Qualified to Boeing specification BMS 8-223 Cl 2 Gr A and B, all types, and McDonnell Douglas specification DMS 2419 Ty 13-90.
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and toxicity cargo liner with white on the face side. Qualified to Boeing specification BMS 8-223 Cl 4 Gr B, all types.
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and toxicity cargo liner with white on the face side. Qualified to Boeing specification BMS 8-223 Cl 5 Gr B, all types.
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.
Woven fiberglass reinforced phenolic facings meta-aramid honeycomb core, lightweight and low smoke sandwich panel. Qualified to McDonnel Douglass specifications 3962952 and Embraer MEP 15-029.
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.
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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