FORD WSS-M1H1077-A2-2014 FABRIC PULSE SOUTH AFRICA WOVEN DOBBY UNLAMINATED TO BE USED WITH FORD WSS-M99P1111-A (Shown On FORD WSS-M1H1077-A1).pdf

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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev. 1 2014 07 01 Editorial Corrected back coating and total weight of A2 R. Kyle, EU 2012 11 26 Released R.Kyle Controlled document at www.MATS Copyright 2014, Ford Global Technologies, LLC Page 1 of 2 FABRIC, PULSE, AAT (THAILAND), WOVEN DO

2、BBY, UNLAMINATED WSS-M1H1077-A1 FABRIC, PULSE, SOUTH AFRICA, WOVEN DOBBY, UNLAMINATED WSS-M1H1077-A2 FABRIC, PULSE, ARGENTINA, WOVEN DOBBY, UNLAMINATED WSS-M1H1077-A3 1. SCOPE The material defined by this specification is a polyester woven dobby face fabric. 2. APPLICATION This specification was rel

3、eased originally for material used as an interior trim bolster fabric for use in the T6 program. Fabric was developed as a Tri-Laminate. The fabric is used back coated and unlaminated in seat back applications only. A1 is for AAT (Thailand) A2 is for South Africa A3 is for Argentina 3. REQUIREMENTS

4、In addition to the requirements listed herein, the fabric shall meet all requirements of WSS-M8P18-A1/A2/A3/A4 as applicable. 3.1 STANDARD REQUIREMENTS FOR PRODUCTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements for Production Materials (WSS-M99P

5、1111-A). 3.2 FABRIC CONSTRUCTION 3.2.1 Fabric Count, +/- 10% (ASTM D3775) A1 (AAT) A2 (South Africa) A3 (Argentina) Warp 330 ends/10 cm 330 ends/10 cm 330 ends/10 cm Weft 165 picks/10 cm 165 picks/10 cm 165 picks/10 cm 3.2.2 Fabric Weight, +/- 10% (FLTM BN 106-01) A1 (AAT) A2 (South Africa) A3 (Arge

6、ntina) Face Fabric 315 g/m2 315 g/m2 315 g/m2 Back coat 60 g/m2 60 g/m2 60 g/m2 Total Weight 375 g/m2 375 g/m2 375 g/m2 ENGINEERING MATERIAL SPECIFICATION WSS-M1H1077-A1 WSS-M1H1077-A2 WSS-M1H1077-A3 Copyright 2014, Ford Global Technologies, LLC Page 2 of 2 3.3 COMPOSITION (ASTM D629) Fabric 100% po

7、lyester 3.4 YARN CONSTRUCTION (ASTM D1244) Warp 470dtex, f288 (Air Jet Texturised) Weft 850dtex, f408 (Air Jet Texturised) 3.5 METHOD OF DYEING Solution dyed or as approved by Materials Engineering 3.6 FINISHED OPERATIONS Washing Drying Back coating Or as approved by Materials Engineering 4. GENERAL

8、 INFORMATION The information given below is provided for clarification and assistance in meeting the requirements of this specification. Contact for questions concerning Engineering Material Specifications. 4.1 Purchase departments will ensure that the material defined in this specification and shi

9、pped to any one assembly plant will be produced by one supplier only. 4.2 Global Strategy is to use Tri-Laminate construction in all regions. 4.3 If yarn is locally sourced it must meet the above Fabric Construction, Composition and Yarn construction requirements. The fabric must also meet the requirements of WSS-M8P18-A1/A2/A3/A4.

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