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Master Bond adhesives

Hexcel® Fibrelam® Grade 12 Panels for Aircraft Flooring
Categories: Other Engineering Material

Material Notes: Fibrelam® structural sandwich panels have been in service since 1973 and are currently approved for flooring by major aircraft manufacturers and airlines worldwide. These extensively flight-proven panels offer outstanding mechanical and physical properties, can be easily cut and machined on equipment normally found in airline maintenance shops, and are easy to install.

Information provided by Hexcel

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Descriptive Properties
Burn Length (mm)56BSS 7230; Flammability: 60 Second Vertical Ignition
Drip Extinguish Time (sec)0BSS 7230; Flammability: 60 Second Vertical Ignition
Glow Time (sec)0BSS 7230; Flammability: 45 Degree Test
Impact Resistance (N-m)9.9BMS 4-17
In-Plane Shear (N/mm)175BMS 4-17
Insert Shear (N)5350BMS 4-17
Long Beam Bending Deflection (mm)8.9MIL-STD-401B; At 445N (100lb)
Long Beam Bending Load (N)3070BSS 7250 Humidity; Humidity Resistance Load (100% at 60°C (140°F) for 30 days)
 3540MIL-STD-401B; Core Ribbon, Transverse
Panel Shear Strength (N)5060MIL-STD-401B 3 point loading; Core Ribbon, Transverse
Sandwich Peel (N/76 mm)420MIL-STD-401B; Core Ribbon, Transverse
Self-Extinguish Time (sec)1BSS 7230; Flammability: 45 Degree Test
 8BSS 7230; Flammability: 60 Second Vertical Ignition
Stabilized Core Compression (N/mm2)25.8MIL-STD-401B
Warpage (mm/m), max0.8

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to view all the property values for this datasheet as they were originally entered into MatWeb.

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PHEXC687 / 101306

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