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Features & Benefits
High compressive strength provides strong structural reinforcement
Flame retardant enhances fire safety of bonded components
Fast heat cure accelerates manufacturing and repair processes
Excellent adhesion ensures reliable bonding to composite materials
Wide application range suitable for various aerospace composite structures
Specifications
Series: 1618 D/B
Container Size: 5 gal
Container Type: Pallet
Color: Amber/Off-White (Part B/A)
Composition: 25 to 30% Bisphenol-A Epoxy Resin, 10 to 20% O-Cresyl Glycidyl Ether, 5 to 10% Epoxy Phenol Novolac Resin, 5 to 10% 2,2-Bis(Acryloyloxyethyl)Butyl Acrylate, 2.5 to 5% Dimethyl Methylphosphonate, 1 to 2.5% Siloxanes and Silicones, Di-Me, 3-Hydroxypropyl Me, Ethoxylated, 0.1 to 0.25% Ethylbenzene (Part D), 3 to 7% Monoethanolamine, 30 to 60% 4,4'-Isopropylidene Diphenol, 30 to 60% Diethylenetriamine, 13 to 30% 2,2'-Dimethyl-4,4'-Methylenebis(Cyclohexylamine) (Part B)
Mixing Ratio: 100:14
Boiling Point: >200 deg C (Part D)
Form: Liquid (Part D), Paste (Part B)
Curing Time: 5 hr at 125 deg F
Odor/Scent: Slight (Part A), Amine-Like (Part B)
Flash Point: >100 deg C (Part D and B)
Viscosity: 400 mPa-s at 25 deg C (Part B)
Shelf Life: 180 days
Specific Gravity: 1 (Part B)
Density: 0.63 to 0.66 g/cc at 25 deg C (Part D), 1 g/cc at 25 deg C (Part B)
Compressive Strength: 5000 psi at 77 deg F
Flame Retardant: Yes
Application
For manufacturing and repair of composite radomes fairings flight control surfaces and cargo/cabin panels
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Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
