The Gill Corporation
HIGH-PERFORMANCE COMPOSITE PRODUCTS SINCE 1945
The Gill Product Description
Blanket Application, Edge Fill, Edge Seal, Inserts, Panel Routing, Subassembly Attachment, and Tape Application
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 polyester, general purpose cargo liner. M.C. Gill proprietary product.
Gilliner 1076C is a general purpose fiberglass cloth reinforced polyester laminate.
Wear resistant fiberglass cloth reinforced polyester laminate. Aircraft cargo compartment liner; designed for lower sidewalls where in-service conditions may result in wear through over frame sections, impact damage and/or fastener hole tear out at attach points
Woven fiberglass cloth reinforced polyester with white Tedlar® overlay face side, high impact resistant cargo liner.   Qualified to McDonnell Douglas specification DMS 1946 Type 1.
Nylon cloth reinforced nylon fuel cell liner.
Woven fiberglass cloth reinforced phenolic, very high impact resistant, low smoke and toxicity cargo liner with white Tedlar® on the face side. Qualified to McDonnell Douglas specification DMS 2226 Ty 1 Cl 1.
Woven fiberglass cloth reinforced polyester, high impact resistant cargo liner. Qualified to Boeing specification BMS 8-2 Cl 2 Gr A, De Havilland DHMS P1.42 Cl B, Lockheed LAC-C-22-1249 Cl 3, and Airbus 2550 M1M 0014 01. 1366T is same as 1366 but with a 1 mil white Tedlar® face side. Qualified to Boeing specification BMS 8-2 Cl 2 Gr B.
Woven fiberglass cloth reinforced phenolic, very high impact resistant, low smoke and toxicity cargo liner with white Tedlar® 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 Tedlar® 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 Tedlar® 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.
Gillfab 1367G is a high impact resistant, low smoke and toxicity, fiberglass reinforced phenolic laminate
Gillpatch™ 1367P System is a low smoke and toxicity, fiberglass reinforced, phenolic laminate patch for repair of limited damage to cargo liner sandwich panels in Airbus aircraft – refer to specific Airbus AMM for application and limitations.
Gillfab 1694 is a high performance laminate made from e–glass woven roving reinforced phenolic resin.
Woven fiberglass reinforced phenolic "h" profile used for the installation of cargo decompression panels. Qualified to Airbus technical specification 2550 M1M 0004 00.
Unidirectional S-2 glass® reinforced phenolic facings/Nomex® honeycomb core floor panel.  Qualified to BAe specification BAER 3232.
Unidirectional S-2 glass reinforced phenolic facings/Nomex® honeycomb core floor panel.   Qualified to BAe specification MAT 006.
Unidirectional graphite reinforced epoxy facings/Nomex® honeycomb core floor panel. Qualified to Embraer specification MEP 15-030.

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