HIGH-PERFORMANCE COMPOSITE PRODUCTS SINCE 1945
Product Description
Unidirectional carbon fiber reinforced epoxy facings bonded to GillVANA® honeycomb core panel. Provides excellent acoustic benefits while still meeting physical, mechanical and flammability requirements. Qualified to Boeing specifications BMS 4-20.
Woven fiberglass cloth reinforced, high impact resistant cargo liner. Qualified to De Havilland DHMS P1.42 Cl B. 1366T is same as 1366 but with a 1 mil white face side.
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
Gilliner®1076C is a general purpose fiberglass cloth reinforced polyester laminate.
Unidirectional fiberglass reinforced epoxy facings/aluminum honeycomb core floor panel. Qualified to Boeing specification BMS 4-23 Types I and II.
Unidirectional carbon reinforced epoxy facings/ N636 honeycomb core floor panel. Qualified to Boeing specification BMS 4-20, Types VI, VII, VIII and IX.
Unidirectional carbon reinforced epoxy facings meta-aramid honeycomb core floor panel. Qualified to Boeing specification BMS 4-20, Types II and III.
Unidirectional carbon reinforced phenolic facings meta-aramid honeycomb core, low smoke and toxicity, light-weight floor panel. Qualified to McDonnell Douglas drawing 7954400, all types.
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.
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.
Woven fiberglass reinforced phenolic facings meta-aramid honeycomb core, lightweight and low smoke sandwich panel. Qualified to McDonnel Douglass specifications 3962952, Embraer MEP 15-029 and Lockheed LAC-LS60204.
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 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.
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 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.
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, 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.
Woven fiberglass cloth reinforced polyester with white overlay face side, high impact resistant cargo liner. Qualified to McDonnell Douglas specification DMS 1946 Type 1.
An aircraft grade sandwich panel made from aluminum alloy facings bonded to end grain balsa wood core. McDonnell Douglas Drawing S4929905.
Unidirectional fiberglass reinforced epoxy facings/aluminum honeycomb core floor panel. Qualified to McDonnell Douglas specification BZZ 7002 Ty IV and V.

Result Pages:  1  2  [Next >>]  Displaying 1 to 20 (of 28 products)