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Commercial grade aramid paper reinforced phenolic (Nomex®) honeycomb core. |
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Gillcore HA Honeycomb |
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Gillcore HD Honeycomb |
Aramid paper reinforced phenolic (Nomex®) honeycomb core. Qualified to Boeing |
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BMS 8-124 Cl IV, McDonnell Douglas DMS 1974 Gr A, Lockheed STM 28-105/C28- |
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105/LCM 28-1041, Northrop Grumman GC101 and Mil C 81986. |
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Gillcore HK Honeycomb |
Kevlar® N636 reinforced phenolic honeycomb core. High strength characteristics |
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offer weight savings over Nomex. Qualified to BMS 8-124 Cl VI. |
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Gillcore OXHD Honeycomb |
Aramid paper reinforced phenolic (Nomex®) honeycomb core whose cells are |
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overexpanded to a rectangular shape to provide flexibility in curving or forming the |
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honeycomb in the "W" direction. |
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Gillab 990C Table Top |
Fiberglass mat reinforced, chemical resistant polyester lab table top overlay. |
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Gillfab 1000 Laminate |
Woven fiberglass cloth reinforced acrylic laminate for aircraft windshield edge. |
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Gillfab 1002 Laminate |
Woven fiberglass cloth reinforced phenolic laminate. Service temperature range: |
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350 degrees F continuous, intermittent to 500 degrees F. Qualified to McDonnell |
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Douglas specification DMS 1556. |
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Gillfab 1042 Laminate |
Woven fiberglass cloth reinforced phenolic laminate. Service temperature range: |
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Up to 300 degrees F. Qualified to McDonnell Douglas specification DMS 1558, Type |
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2. |
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Gilliner 1066 Laminate |
Woven fiberglass cloth reinforced polyester, general purpose cargo liner. M.C. Gill |
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proprietary product. |
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Gilliner 1076A Laminate |
Woven fiberglass cloth reinforced polyester, general purpose cargo liner. Qualified |
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to Boeing specification BMS 8-2 Class 1. |
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Woven fiberglass cloth reinforced polyester, high abrasion/wear resistant cargo |
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Gilliner 1076B Laminate |
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liner. Qualified to Boeing specification BMS 8-2 Class 3. |
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Gillfab 1094 Laminate |
Woven fiberglass roving reinforced polyester general purpose ballistic laminate. |
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Gillfab 1100 Laminate |
Woven fiberglass cloth reinforced polyester with white Tedlar® overlay face side, |
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high impact resistant cargo liner. Qualified to McDonnell Douglas specification |
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DMS 1946 Type 1. |
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Gillfab 1100G Laminate |
Same as Gillfab 1100 Laminate, but no Tedlar® and green in color. Qualified to |
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McDonnell Douglas specification DMS 1946 Type 2. |
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Gillfab 1102 Laminate |
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and |
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toxicity cargo liner with gray Tedlar® face side. Meets Fokker specification FON 1- |
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4621. |
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Gillfab 1108 Laminate |
Unidirectional fiberglass reinforced epoxy with White Tedlar® both sides, high |
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impact resistant cargo liner. Qualified to Boeing specification BMS 8-100 Gr A. |
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Gillfab 1137 Laminate |
Nylon cloth reinforced nylon fuel cell liner. |
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Gilliner 1166/1266 Laminate |
Woven fiberglass cloth reinforced polyester cargo liner with glossy white .004" thick |
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resin coating of Gillcoat on the face side for improved wear resistance, rigidity. |
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M.C. Gill proprietary product. |
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Gillfab 1167 Laminate |
Woven fiberglass cloth reinforced phenolic, very high impact resistant, low smoke |
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and toxicity cargo liner with white Tedlar® on the face side. Qualified to McDonnell |
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Douglas specification DMS 2226 Ty 1 Cl 1. |
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Gilliner 1266/1166 Laminate |
Woven fiberglass cloth reinforced polyester cargo liner with glossy white .004" thick |
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resin coating of Gillcoat on the face side for improved wear resistance, rigidity. |
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M.C. Gill proprietary product. |
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Gillfab 1342 Laminate |
Gillfab 1042 Laminate with removable peel ply for bondability. Qualified to |
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McDonnell Douglas specification DMS 1558, Type 4. |
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Gillfab 1360A Laminate |
Woven Kevlar® 29 fabric reinforced phenolic, high performance ballistic laminate. |
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Woven aramid fabric reinforced phenolic, high performance ballistic laminate. |
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Gillfab 1360B Laminate |
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Gilliner 1366/1366T LaminateWoven 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.
Gillfab 1367 Laminate 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
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specification DMS 2419 Ty 50-90 and LAC-C-22-1249 Cl 3. |
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Gillfab 1367A Laminate |
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and |
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toxicity cargo liner with white Tedlar® on the face side. Qualified to Boeing |
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specification BMS 8-223 Cl 2 Gr B Types 13 thru 40, McDonnell Douglas DMS 2419 |
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Cl 1 (Ty 13-40), and Airbus 2550 M1M 000800. |
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Gillfab 1367B Laminate |
Woven fiberglass cloth reinforced phenolic, high impact resistant, low smoke and |
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toxicity cargo liner with white Tedlar® on the face side. 20-25% lighter in weight |
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than 1367A with no sacrifice to mechanical properties. Qualified to Boeing |
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specification BMS 8-223 Cl 4 Gr B, all types. |
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Gillfab 1367G Laminate |
Gillfab 1367G is a high impact resistant, low smoke and toxicity, fiberglass |
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reinforced phenolic laminate |
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Gillfab 1367M Laminate |
Product designation for Gillfab 1367B Laminate manufactured in roll stock form. |
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Gillpatch 1367P Laminate |
Gillpatch™ 1367P System is a low smoke and toxicity, fiberglass reinforced, |
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phenolic laminate patch for repair of limited damage to cargo liner sandwich panels |
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in Airbus aircraft – refer to specific Airbus AMM for application and limitations. |
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Gillfab 1394 Laminate |
S-2 Glass® roving reinforced phenolic, high performance ballistic laminate. |
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Gillite 1401 Laminate |
Gillite™ 1401 Transparent Laminate is a fiberglass cloth reinforced polyester sheet. |
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It is designed for use in any applications, where transparency combined with high |
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strength and flammability characteristics are of primary concern. |
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Gillfab 1566 Laminate |
Aramid (Kevlar®) cloth reinforced polyester lightweight cargo liner with white |
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Tedlar® on the face side. Qualified to de Haviland specification DHMS P1.42 Cl A. |
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Gillfab 1694 Laminate |
Gillfab 1694 is a high performance laminate made from e–glass woven roving |
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reinforced phenolic resin. |
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Gillfab 3072 Profile |
Woven fiberglass reinforced phenolic "h" profile used for the installation of cargo |
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decompression panels. Qualified to Airbus technical specification 2550 M1M 0004 |
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00. |
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Unidirectional S-2 Glass® reinforced phenolic facings/aramid honeycomb core floor |
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Gillfab 4004 Panel |
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panel. Qualified to McDonnell Douglas specification 7954401, Ty 1. |
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Gillfab 4004A Panel |
Unidirectional S-2 glass® reinforced phenolic facings/Nomex® honeycomb core |
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floor panel. Qualified to BAe specification BAER 3232. |
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Gillfab 4004B Panel |
Unidirectional S-2 glass reinforced phenolic facings/Nomex® honeycomb core floor |
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Gillfab 4009 Panel
Gillfab 4014 Panel
Gillfloor 4017T Panel
Gillfab 4018/S/T Panel
Gillfab 4019 Panel
Gillfab 4022A/B Panel
Gillfab 4030 Panel
Gillfab 4034 Panel
Gillfab 4088 Panel
Gillfab 4101 Panel
Gillfab 4105A/B Panel
Gillfab 4105C Panel
Gillfab 4106A/B Panel
panel. Qualified to BAe specification MAT 006.
Unidirectional graphite reinforced epoxy facings/Nomex® honeycomb core floor panel. Qualified to Embraer specification MEP 15-030.
Aluminum facings/aluminum honeycomb core sandwich panel.
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.
Unidirectional fiberglass reinforced phenolic facings/Nomex® honeycomb core floor panel. Qualified to Fokker specification FoN 1.4350.
Unidirectional graphite/ woven fiberglass reinforced phenolic facings/Nomex® honeycomb core floor panel. Qualified to Fokker specification FoN 1.4354.
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 glass reinforced epoxy facings/aluminum honeycomb, high strength sandwich panel. Qualified to Lockheed specification LAC-C-28-1147 Ty 11A.
Aluminum facings/aluminum honeycomb core semi structural sandwich panel. Qualified to Learjet specification LES 1247.
Woven fiberglass cloth reinforced epoxy facings/Nomex® honeycomb core floor panel. Qualified to Airbus technical specification TL53/500/79 Ty 1 and 2.
Woven fiberglass cloth reinforced epoxy facings/Nomex® honeycomb core floor panel.
Aluminum facings/Nomex® honeycomb core floor panel. Qualified to McDonnell Douglas specification no. S3932194.
Gillfab 4109 Panel |
Unidirectional carbon reinforced phenolic/Nomex® honeycomb core, low smoke |
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floor panel. Qualified to McDonnell Douglas specification 9D0207 Ty 1 and 2, and |
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BAe specification BAeR 3247. |
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Gillfab 4122A Panel |
Woven fiberglass cloth reinforced phenolic facings/Nomex® honeycomb core, low |
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smoke and toxicity, sandwich panel. Qualified to McDonnell Douglas specification |
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3962952 and Embraer specification MEP15-029. |
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Gillfab 4122B |
A light weight sandwich panel constructed of woven glass reinforced phenolic |
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facings bonded to Nomex® honeycomb core. Face side features a 2 mil white |
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Tedlar® overlay. |
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Gillfab 4123 Panel |
Woven fiberglass cloth reinforced phenolic facings/ Nomex® honeycomb core floor |
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panel. |
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Gillfab 4201 Panel |
Data on this product is available by contacting M.C. Gill Corporation. |
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Phone: 626-443-4022; Fax: 626-350-5880; Email: This email address is being protected from spambots. You need JavaScript enabled to view it. |
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Gillfab 4205 Panel |
Unidirectional carbon reinforced phenolic facings/Nomex® honeycomb core floor |
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panel. Qualified to Airbus technical specification no. 5360 M1B 000100. |
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Gillfab 4223 Panel |
Woven fiberglass cloth reinforced phenolic facings/Nomex® honeycomb core floor |
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panel. Qualified to Airbus technical specification 5360 M1B 000500, (BCC2). |
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Gillfab 4230 Panel |
Gillfab 4230 is an aircraft structural sandwich panel composed of aluminum skins |
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bonded to an aluminum honeycomb core, and qualified to Raytheon Specification |
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TMS 11-903. |
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Gillfab 4322 Panel |
S-2 glass reinforced phenolic facings//Nomex® honeycomb core floor panel. |
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Qualified to Airbus technical specification 5360 M1B 000100. |
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Gillfab 4323 Panel |
S-2 glass reinforced phenolic facings/Nomex® honeycomb core floor panel. |
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Qualified to Airbus technical specification 5360 M1B 000100. |
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Type 1 - Woven fiberglass cloth reinforced epoxy facings/Nomex® honeycomb core |
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Gillfab 4405A/B Panel |
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floor panel. Type 2 identical except for a sheet of aluminum foil bonded to the |
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bottom facing. Qualified to Airbus technical specification TL53/5000/79, Annex A |
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Types 1 and 2. |
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Gillfloor 4417 Panel |
Unidirectional fiberglass reinforced epoxy facings/Nomex® honeycomb core floor |
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panel. Qualified to Boeing specification BMS 4-17, Ty I thru V, IX and Drawing |
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69B15779 (Ty V). |
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Gillfloor 4417A Panel |
Unidirectional fiberglass reinforced epoxy facings/Nomex® honeycomb core floor |
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panel. Qualified to Boeing specification BMS 4-17, Ty VI. |
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Gillfab 4422 Panel |
Woven fiberglass cloth reinforced phenolic laminate with 1 mil Tedlar® |
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overlay/Nomex® honeycomb core, high-impact resistant cargo liner panel. |
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Qualified to Airbus technical specification 2550 M1M 0008 00. |
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Gillfab 4505 Panel |
Unidirectional carbon/woven glass reinforced phenolic facings/Nomex® honeycomb |
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core floor panel. |
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Gillfloor 4509 Panel |
Unidirectional carbon reinforced phenolic facings/Nomex® honeycomb core, low |
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smoke and toxicity, light-weight floor panel. Qualified to McDonnell Douglas |
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drawing 7954400, all types. |
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Gillfab 4522 Panel |
Woven fiberglass cloth reinforced phenolic facings/Nomex® honeycomb core floor |
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panel. Qualified to Airbus technical specification 5360 M1M 000500, (CCC1). |
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Gillfab 4605 Panel |
Unidirectional carbon/woven fiberglass reinforced phenolic facings/Nomex® |
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honeycomb core, low smoke and toxicity floor panel. Qualified to Airbus technical |
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specification 5360 M1M 000600, (PC1). |
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Gillfloor 4609 Panel |
Unidirectional carbon reinforced phenolic facings/Nomex® honeycomb core, low |
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smoke and toxicity, light-weight floor panel. Qualified to BAe specification AVN 3- |
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005. |
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Gillfloor 4709 Panel |
Unidirectional carbon reinforced epoxy facings/Nomex® honeycomb core floor |
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panel. Qualified to Boeing specification BMS 4-20, Types II and III. |
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Gillfloor 4809 Panel |
Unidirectional carbon reinforced epoxy facings/Kevlar® N636 honeycomb core floor |
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panel. Qualified to Boeing specification BMS 4-20, Types VI, VII, VIII and IX. |
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Gillfab 4909 Panel |
Gillfab™ 4909 is a family of low smoke aircraft sandwich panels with facings made |
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from epoxy resin reinforced with cross-plied unidirectional carbon and woven |
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fiberglass fabric bonded to Kevlar® honeycomb core. |
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Gillfloor 5007A Panel |
Woven fiberglass cloth reinforced polyester facings/9.0 pcf avg.end grain balsa |
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wood core floor panel. M.C. Gill proprietary. |
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Gillfloor 5007B Panel |
Similar to Gillfloor 5007A Panel, but with higher climbing drum peel strength. M.C. |
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Gill proprietary. |
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Gillfloor 5007C Panel |
Same as Gillfloor 5007B Panel, but with mat overlay for enhanced abrasion/wear |
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resistance and increased durability. M.C. Gill proprietary. |
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Gillfloor 5007D Panel |
The Gillfloor 5007D cargo floor panel was developed in response to freight carriers’ |
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requests for a more durable, impact resistant panel for use in areas subjected to |
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high abuse. It is constructed of heavy, uni-directional fiberglass reinforced, vinyl |
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ester facings bonded to an end-grain balsawood core. An abrasion resistant top |
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surface is integrally bonded to the panel. |
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Gillfab 5017 Panel |
Woven fiberglass cloth reinforced epoxy facings/Nomex® honeycomb core |
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sandwich panel. Qualified to Lockheed specification LAC-C-28-1247. |
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Gillfab 5019 Panel |
Woven fiberglass reinforced epoxy facings/fire retardant urethane foam sandwich |
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panel. |
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Gillfab 5020 Panel |
Aluminum facings/crushed aluminum honeycomb core, thin, lightweight sandwich |
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panel. It is as rigid as sheet aluminum, but weighs half as much. Qualified to |
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Lockheed specification LCM 28-1033, and Learjet specification LES 1070. |
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Gillfab 5030 Panel |
Aluminum facings/aluminum honeycomb commercial grade sandwich panel. |
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Gillfab 5040 Panel |
Aluminum facings/9.0 pcf avg. end grain balsa wood core sandwich panel. |
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Gillfab 5042 Panel |
Aluminum facings/9.0 pcf avg. end grain balsa wood core floor panel. Qualified to |
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Boeing specification BMS 4-10, Type 1, Grades A thru G. |
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Gillfab 5042B Panel |
Aluminum facings/9.0 pcf avg. end grain balsa wood core floor panel. Qualified to |
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McDonnell Douglas specifications S3932193, S3932195 and S4931863. |
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Gillfloor 5065 Panel |
Unidirectional fiberglass reinforced epoxy facings/aluminum honeycomb core floor |
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panel. Qualified to McDonnell Douglas specification BZZ 7002 Ty IV and V. |
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Gillfab 5071A/5072A Panel |
Woven fiberglass reinforced phenolic facings/Nomex® honeycomb core, |
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lightweight, high performance, low smoke and toxicity sandwich panel. |
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Gillfab 5075 is a family of lightweight, high performance sandwich panels designed |
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Gillfab 5075 Panel |
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for use in aircraft cabin interior structures such as galleys, lavatories, bulkheads, |
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partitions, stowage compartments and crew rests. |
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Gillfab 5101 Panel |
Aluminum facings/aluminum honeycomb core, with corrosion inhibiting primer on |
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the bonding side. Qualified to Learjet specification LES 1277. |
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Gillfab 5120 Panel |
Gillfab 5120 Panel is a very thin sandwich panel made with aluminum skins and |
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aluminum honeycomb. |
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Gillfab 5142 Panel |
An aircraft grade sandwich panel made from aluminum alloy facings bonded to end |
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grain balsa wood core. McDonnell Douglas Drawing S4929905. |
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Gillfab 5142A Panel |
An aircraft grade sandwich panel made from aluminum alloy facings bonded to end |
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grain balsa wood core. McDonnell Douglas Drawing S4929962. |
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Gillfab 5202 Panel |
Data on this product is available by contacting M.C. Gill Corporation. |
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Phone: 626-443-4022; Fax: 626-350-5880; Email: This email address is being protected from spambots. You need JavaScript enabled to view it. |
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Gillfab 5242 Panel |
Aluminum facings, 9.0 pcf avg end grain balsa wood core with a .020 fiberglass |
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reinforced epoxy overlay face side, floor panel. Qualified to McDonnell Douglas |
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specification S00096. |
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Gillfloor 5424 Panel |
Unidirectional fiberglass reinforced epoxy facings/aluminum honeycomb core floor |
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panel. Qualified to Boeing specification BMS 4-23 Types I and II. |
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Gillfab 5433C Panel |
Aluminum facings/ woven fiberglass reinforced epoxy core floor panel. Qualified to |
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Boeing specification BMS 7-326, Type VII, Class 2/1. |
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Gillfab 5433E Panel |
Gillfab 5433E sandwich panel is made from aluminum facings bonded to a woven |
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fiberglass reinforced epoxy core. |
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Gillfab 5509 Panel |
Gillfab™ 5509 panel is a low smoke aircraft sandwich panel with facings made from |
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phenolic resin reinforced with crossplied unidirectional carbon and Kevlar™ |
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honeycomb core. |
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Gillpatch III Repair System |
Woven fiberglass reinforced phenolic laminate with an intumescent barrier front |
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side, pressure sensitive adhesive back side, cargo liner repair patch. |
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