The Gill Corporation
HIGH-PERFORMANCE COMPOSITE PRODUCTS SINCE 1945
The Gill Product Description
Unidirectional S-2 glass reinforced epoxy facings/Nomex® honeycomb core floor panel.  Qualified to McDonnell Douglas specification BZZ 7002 Types 1 thru 3,  Embraer MEP 15-031 and BAe MAT 003.
Woven fiberglass reinforced phenolic facings/ Nomex® honeycomb core sandwich panel. Qualified to McDonnell Douglas specifications 9100059, S3933941, S3933942.
Aluminum facings/aluminum honeycomb core sandwich panel. Qualified to Lockheed specification LAC-C-28-1145 Ty 5, 7, 9 and 10.
Gillfab™ 4034 panel is a high performance sandwich panel with epoxy resin pre-impregnated carbon facings and aluminum core.
Unidirectional carbon reinforced phenolic/Nomex® honeycomb core, low smoke floor panel. Qualified to McDonnell Douglas specification 9D0207 Ty 1 and 2,
Gillfab 4117 is a sandwich panel made with facings of fiberglass cloth reinforced epoxy laminate and aramid honeycomb core.
Gillfab™ 4122A/B is a light weight and low smoke emission sandwich panel made from woven glass reinforced phenolic facings bonded to Nomex® honeycomb core. 1 mil white Tedlar® can be added on the face side or both sides of the panel.
Woven fiberglass cloth reinforced phenolic facings/ Nomex® honeycomb core floor panel.
Data on this product is available by contacting M.C. Gill Corporation.Phone: 626-443-4022; Fax: 626-350-5880; Email:info@mcgillcorp.com
Woven fiberglass cloth reinforced phenolic facings/Nomex® honeycomb core floor panel.   Qualified to Airbus technical specification 5360 M1B 000500, (BCC2).
Type 1 - Woven fiberglass cloth reinforced epoxy facings/Nomex® 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.
Unidirectional fiberglass reinforced epoxy facings/Nomex® 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/Nomex® honeycomb core floor panel. 4417A is qualified to Boeing specification BMS 4-17, Ty VI.
Woven fiberglass cloth reinforced phenolic laminate with 1 mil Tedlar® overlay/Nomex® honeycomb core, high-impact resistant cargo liner panel. Qualified to Airbus technical specification 2550 M1M 0008 00.
Unidirectional carbon/woven glass reinforced phenolic facings/Nomex® honeycomb core floor panel.
Unidirectional carbon reinforced phenolic facings/Nomex® honeycomb core, low smoke and toxicity, light-weight floor panel. Qualified to McDonnell Douglas drawing 7954400, all types.
Gillfloor 4518 is a light weight aircraft flooring panel made from unidirectional fiberglass & woven glass cloth reinforced epoxy facings bonded to Kevlar honeycomb core.
Woven fiberglass cloth reinforced phenolic facings/Nomex® honeycomb core floor panel.  Qualified to Airbus technical specification 5360 M1M 000500, (CCC1).
Fiberglass reinforced phenolic facings/Nomex honeycomb core floor panel. Qualified to Airbus Technical Specification 5360 M1M 000500, (BCC3).
Unidirectional carbon/woven fiberglass reinforced phenolic facings/Nomex® honeycomb core, low smoke and toxicity floor panel.  Qualified to Airbus technical specification 5360 M1M 000600, (PC1).
Unidirectional carbon reinforced phenolic facings/Nomex® honeycomb core, low smoke and toxicity, light-weight floor panel.  Qualified to BAe specification AVN 3-005.

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