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| Blanket Application, Edge Fill, Edge Seal, Inserts, Panel Routing, Subassembly Attachment, and Tape Application |
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| IMPORTANT -- READ THIS INSTRUCTION SHEET BEFORE PROCEEDING
First, decide if the damage can be patched. If not, the cargo liner must be replaced.
The patch must extend at least 2 inches beyond all sides of a puncture. Straight tears of any length can be repaired, but the damage must not be closer than 3 inches from any seam, screws, or trim strips; and the patch must extend at least 3 inches from all edges of the damage. The margin for L-shaped tears can be 2 inches, and a single square or rectangular patch must be used to cover this type of damage. |
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| 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. |
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| Woven fiberglass cloth reinforced phenolic laminate.? Service temperature range: Up to 300 degrees F. Qualified to McDonnell Douglas specification DMS 1558, Type 2. |
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| Woven fiberglass cloth reinforced polyester, general purpose cargo liner. M.C. Gill proprietary product. |
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| Gilliner®1076C is a general purpose fiberglass cloth reinforced polyester laminate. |
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| 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 |
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| 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. |
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| Nylon cloth reinforced nylon fuel cell liner. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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| 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. |
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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/Nomex® honeycomb core floor panel.? Qualified to BAe specification BAER 3232. |
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| Unidirectional S-2 glass reinforced phenolic facings/Nomex® honeycomb core floor panel. Qualified to BAe specification MAT 006. |
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| Unidirectional graphite reinforced epoxy facings/Nomex® honeycomb core floor panel. Qualified to Embraer specification MEP 15-030. |
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| 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. |
