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Hexcel® Fibrelam® Grade 11 Panels for Aircraft Flooring

Category Other Engineering Material
Manufacturer Hexcel
Trade Name Fibrelam®
Port Shanghai port,China
Trade Terms FOB, CFR, CIF
Payment Terms L/C, T/T, Western Union
Download PDF Hexcel® Fibrelam® Grade 11 Panels for Aircraft Flooring.pdf
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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
Descriptive Properties Value Comments
Burn Length (mm) 71
BSS 7230; Flammability: 60 Second Vertical Ignition
Drip Extinguish Time (sec) 0
BSS 7230; Flammability: 60 Second Vertical Ignition
Glow Time (sec) 0
BSS 7230; Flammability: 45 Degree Test
Impact Resistance (N-m) 5.6
BMS 4-17
In-Plane Shear (N/mm) 110
BMS 4-17
Insert Shear (N) 4600
BMS 4-17
Long Beam Bending Deflection (mm) 11.7
MIL-STD-401B; At 445N (100lb)
Long Beam Bending Load (N) 1450
BSS 7250 Humidity; Humidity Resistance Load (100% at 60°C (140°F) for 30 days)
2000
MIL-STD-401B; Core Ribbon, Transverse
Panel Shear Strength (N) 4900
MIL-STD-401B 3 point loading; Core Ribbon, Transverse
Sandwich Peel (N/76 mm) 400
MIL-STD-401B; Core Ribbon, Transverse
Self-Extinguish Time (sec) 3
BSS 7230; Flammability: 45 Degree Test
6
BSS 7230; Flammability: 60 Second Vertical Ignition
Stabilized Core Compression (N/mm2) 21.1
MIL-STD-401B
Warpage (mm/m), max 0.8
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