JetFlex Aircraft Interior Finish - Delta EMIS Jump flex PI sheet... · • Low energy curing system...

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PRODUCT I NFORMATION S HEET Revision 3, 03/29/2004 Page 1 of 2 JetFlex ® Aircraft Interior Finish Solvent-based Polyurethane Enamel 981300 Series (L and E Colors) DESCRIPTION JetFlex ® Aircraft Interior Finish is a two-component polyurethane coating formulated for the finishing and re- finishing of plastic and metal components within the cabin and cockpit of aircraft. JetFlex ® finishes meet the performance criteria set forth in the Boeing BMS 10-83D Type II and Type III specification and FAA FAR 25.853 regulation. Advantages: Meets the flammability, yellowing resistance and smoke stain resistance performance requirements of the Boeing BMS 10-83D specification. Fast drying. Low energy curing system for heat sensitive substrates. Very good physical and chemical resistance. Excellent adhesion to plastic and metal substrates and to recommended primer. Excellent film flexibility. Full color range available through intermix system. Easy to handle and use. Versatile application properties. Non-photochemically reactive. Excellent hardness, mar and abrasion resistance. Texturable. Meets the performance criteria of the FAA FAR 25.853 regulation for burn, smoke and heat release. COATING PROPERTIES Gloss: Low Gloss (20-30 units) Type II Flat (8-12 Units) Type III Volume Solids : 16-28%, varies by color Catalyzed and reduced: 16-23.5%, varies by color VOC: As packaged, maximum <6.1 lb/gal, (730 g/L) Catalyzed and reduced: <6.1 lb/gal, (730 g/L) Flash Point: 23°F (-5°C) Pensky-Martens Closed Cup Recommended Film Thickness 4.0-6.0 Mils Wet 0.8-1.2 Mils Dry Spreading Rate: (Catalyzed and Reduced) 1 mil DFT 260-375 sq. ft./gal. No application loss, varies by color. Drying: (77°F [25°C], 50% RH) To Touch 10-15 minutes To Handle: 30-60 minutes Dry Through: 2 hours Force Dry: 30 minutes at 140°F (60°C) Pot Life: 16 hours at room temperature SURFACE PREPARATION General : Surface should be free of grease, dirt, fingerprints, rust and other foreign matter to insure optimum adhesion. Plastic : Clean thoroughly to remove contaminants and mold release agents. Use isopropyl alcohol or other suitable solvent cleaner. If necessary, prime with JetFlex Primer CM0480930 to obtain adhesion. JetFlex ® WR Spray Fil CM0481505 may be used for adhesion and filling on plastic substrates. Test system integrity before use or consult your Sherwin-Williams aerospace representative for additional information. Steel and Aluminum: Chemical treatment on conversion coating is recommended. Prime with JetFlex ® Primer CM0480930 if required. MIXING I NSTRUCTIONS Mix by volume: 7 parts JetFlex ® Color CM09813XX or LXXXXX or EXXXXX 1 part JetFlex ® Catalyst CM0981520 2-4 parts (25-50%) JetFlex ® Reducer CM0110845 APPLICATION Catalyze 7 parts paint to 1 part JetFlex ® Catalyst CM0981520 and reduce 25-50% using Reducer CM0110845. Spray with conventional, HVLP or air assisted airless spray equipment. Texturing: Catalyze and reduce as needed (0-50%). Adjust air and fluid pressures as needed. Flattening : To lower the gloss, use CM0571096 Flattening Additive. Safety Cautions : This product must be mixed with a JetFlex ® Catalyst containing isocyanates. PRODUCT LIMITATIONS JetFlex ® Enamels must be catalyzed at 7:1 ratio with CM0981520. Do not use interior primer catalyst CM0120930. Do not spray hot.

Transcript of JetFlex Aircraft Interior Finish - Delta EMIS Jump flex PI sheet... · • Low energy curing system...

Page 1: JetFlex Aircraft Interior Finish - Delta EMIS Jump flex PI sheet... · • Low energy curing system for heat sensitive substrates. • Very good physical and chemical resistance.

PRODUCT INFORMATION SHEET

Revision 3, 03/29/2004 Page 1 of 2

JetFlex® Aircraft Interior Finish Solvent-based Polyurethane Enamel

981300 Series (L and E Colors)

DESCRIPTION JetFlex® Aircraft Interior Finish is a two-component polyurethane coating formulated for the finishing and re-finishing of plastic and metal components within the cabin and cockpit of aircraft. JetFlex® finishes meet the performance criteria set forth in the Boeing BMS 10-83D Type II and Type III specification and FAA FAR 25.853 regulation. Advantages: • Meets the flammability, yellowing resistance and smoke

stain resistance performance requirements of the Boeing BMS 10-83D specification.

• Fast drying. • Low energy curing system for heat sensitive substrates. • Very good physical and chemical resistance. • Excellent adhesion to plastic and metal substrates and to

recommended primer. • Excellent film flexibility. • Full color range available through intermix system. • Easy to handle and use. • Versatile application properties. • Non-photochemically reactive. • Excellent hardness, mar and abrasion resistance. • Texturable. • Meets the performance criteria of the FAA FAR 25.853

regulation for burn, smoke and heat release.

COATING PROPERTIES

Gloss: Low Gloss (20-30 units) Type II Flat (8-12 Units) Type III

Volume Solids: 16-28%, varies by color Catalyzed and reduced: 16-23.5%, varies by color VOC: As packaged, maximum <6.1 lb/gal, (730 g/L) Catalyzed and reduced: <6.1 lb/gal, (730 g/L) Flash Point: 23°F (-5°C) Pensky-Martens

Closed Cup

Recommended Film Thickness

4.0-6.0 Mils Wet

0.8-1.2 Mils Dry Spreading Rate: (Catalyzed and Reduced) 1 mil DFT 260-375 sq. ft./gal. No application loss, varies by color. Drying: (77°F [25°C], 50% RH) To Touch 10-15 minutes To Handle: 30-60 minutes Dry Through: 2 hours

Force Dry: 30 minutes at 140°F (60°C) Pot Life: 16 hours at room temperature

SURFACE PREPARATION General: Surface should be free of grease, dirt, fingerprints, rust and other foreign matter to insure optimum adhesion. Plastic: Clean thoroughly to remove contaminants and mold release agents. Use isopropyl alcohol or other suitable solvent cleaner. If necessary, prime with JetFlex™ Primer CM0480930 to obtain adhesion. JetFlex® WR Spray Fil CM0481505 may be used for adhesion and filling on plastic substrates. Test system integrity before use or consult your Sherwin-Williams aerospace representative for additional information. Steel and Aluminum: Chemical treatment on conversion coating is recommended. Prime with JetFlex® Primer CM0480930 if required.

MIXING INSTRUCTIONS Mix by volume: 7 parts JetFlex® Color CM09813XX or LXXXXX or EXXXXX

1 part JetFlex® Catalyst CM0981520

2-4 parts (25-50%) JetFlex® Reducer CM0110845

APPLICATION Catalyze 7 parts paint to 1 part JetFlex® Catalyst CM0981520 and reduce 25-50% using Reducer CM0110845. Spray with conventional, HVLP or air assisted airless spray equipment. Texturing: Catalyze and reduce as needed (0-50%). Adjust air and fluid pressures as needed. Flattening: To lower the gloss, use CM0571096 Flattening Additive. Safety Cautions: This product must be mixed with a JetFlex® Catalyst containing isocyanates.

PRODUCT LIMITATIONS • JetFlex® Enamels must be catalyzed at 7:1 ratio with

CM0981520.

• Do not use interior primer catalyst CM0120930.

• Do not spray hot.

Page 2: JetFlex Aircraft Interior Finish - Delta EMIS Jump flex PI sheet... · • Low energy curing system for heat sensitive substrates. • Very good physical and chemical resistance.

981300 SERIES (L AND E COLORS) PRODUCT INFORMATION SHEET

Revision 3, 03/29/2004 Page 2 of 2

• Do not vary catalyst ratio. The catalyst ratio has been established for optimum hardness, flexibility, gloss, and chemical and solvent resistance. Slight over or under catalyzation will not seriously affect performance

• Because of many types and compositions of plastic available, each user should test the coating on each substrate before production use. Consult your Sherwin-Williams aerospace representative for additional information.

• Curing temperature must not exceed the heat distortion temperature of the plastic substrate.

• Protect JetFlex® Enamels, Catalyst and Reducer from moisture as water affects pot life and properties. Store indoors.

• Do not package products coated with JetFlex® Enamels in airtight plastic bags unless completely cured. Since JetFlex® Enamels continue to cure for several weeks. The build up of organic solvents and reaction by-products could cause improper cure and adhesion failure in use.

• Do not blend with any other polyurethane.

• Do not use lacquer thinners and alcohol containing solvent blends because they will neutralize the curing mechanism and destroy performance properties.

• Customers must verify FAA FAR 25.853 regulation compliance on their substrate and system.

EQUIPMENT CLEANUP

Use JetFlex® Reducer CM0110845.

SHELF LIFE

Shelf Life is applicable only for material stored in unopened and undamaged original factory filled containers. Minimum Storage Temp. 40ºF / 4ºC Maximum Storage Temp. 90ºF / 32ºC

CM09813XX (L and E-colors) Base Component: 2 years CM0981520: 2 years

Pint Touch-up Kit (includes 10.5 oz. Color, 1.5 oz CM0981520 Hardener, and 4 oz. CM0110845 Thinner): 1 year Aerosol Touch –up Kits: 1 year Cool, Dry Storage Required.

USE OF SYSTEMS STATEMENT Sherwin-Williams Aerospace coatings have been developed and evaluated for use as complete systems. The Aerospace interior primers have been developed to be compatible with the JetFlex® coatings. Use of products not manufactured by Sherwin-Williams Aerospace as primer replacements is not recommended and could negatively affect coating appearance, inter-coat adhesion, chemical resistance, and durability of the finish. Use a complete Sherwin-Williams Aerospace system to ensure the long-term integrity of the coating.

HEALTH AND SAFETY INFORMATION Consult the Material Safety Data Sheets for product information regarding health, physical and environmental hazards, handling precautions and “First Responder” first-aid recommendations.

PRODUCT INFORMATION Please contact your Sherwin-Williams Aerospace Distributor or Representative for more information. NOTE: Product Information Sheets are periodically updated to reflect new information relating to the product. It is important that the customer obtain the most recent Product Information Sheet for the product being used. The information, rating, and opinions stated here pertain to the material currently offered and represent the results of tests believed to be reliable. However, due to variations in customer handling and methods of application which are not known or under our control, The Sherwin-Williams Company cannot make any warranties as to the end result.