FORD WSS-M15P32-D-2016 TRIM ASSEMBLY ENCLOSED LUGGAGE COMPARTMENT COVERING TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、ENGINEERING MATERIAL SPECIFICATIONTRIM ASSEMBLY, ENCLOSED LUGGAGE WSS-M15P32-D COMPARTMENT COVERING 1. SCOPE The material defined by this specification is the minimum durability and performance requirements of all enclosed carpeted luggage or load compartment trim components where various materials
2、are combined to provide a trim assembly having decorative and/or functional features. This includes: rear seat back trim in enclosed luggage compartment applications, deck lid trim and spare tire covers (not for exposed load compartment applications). 2. APPLICATION This specification was released o
3、riginally for material used as enclosed luggage compartment trim parts. 3. REQUIREMENTS 3.1 APPROVED SOURCES This specification is performance based and does not have approved sources. 3.2 CONDITIONING AND TEST CONDITIONS All test values are based on material conditioned for not less than 24 h prior
4、 to testing in a controlled environment of 23 +/- 2 C and 50 +/- 5% relative humidity. Testing of the material should occur in the conditioning environment or soon after removal. 3.3 PERFORMANCE CRITERIA 3.3.1 In addition to the requirements listed herein, the individual carpet assembly components s
5、hall meet all the requirements of the applicable material specifications for the carpet, padding, adhesive, barrier, or trim application as well as any functional/SDS requirements as outlined by Engineering. Material specification requirements are to be used mainly for initial qualification of mater
6、ials. 3.3.2 Mold in Color plastic components shall meet the requirements of WSS-M15P4-G/latest. 3.3.3 Painted components shall meet the requirements of WSS-M2P188-B1/latest for paint over plastic or WSS-M2P190-A / latest if paint over metal. 3.3.4 Labels must meet the appropriate suffix of WSS-M99P4
7、1-A10-A72/latest. 3.4 SAMPLE SELECTION See Table 1 and 2 for sample size and testing requirements. When production test specimens are taken from an area in the carpet with padding, the padding should be stripped away as much as possible before evaluation, unless otherwise specified. 3.5 COMPOSITION
8、AND CONSTRUCTION Date Action Revisions Rev. 3 2016 07 08 Revised See Summary of Revisions L. Sinclair, NA 2014 07 24 Revised See Summary of Revisions L. Sinclair, NA 2011 10 17 Activated Replaces WSS-M15P32-C L. Sinclair NA, J. Williams, Eu Controlled document at www.MATS Copyright 2016, Ford Global
9、 Technologies, LLC Page 1 of 11 ENGINEERING MATERIAL SPECIFICATIONPage 2 of 11Copyright 2016, Ford Global Technologies, LLCWSS-M15P32-D Shall be as specified on the Material Specification The Carpet Supplement Form shall be completed and submitted to Materials Engineering with the construction packa
10、ge. Backcoating: The backcoating shall form a continuous and uniform coating over the back of the carpet so that all pile fibers are covered. Also, the backcoat shall show no evidence of cracking or crumbling during any of the evaluations required within the specification and during normal field con
11、ditions. The backcoat shall thoroughly saturate the base of the pile fiber bundles to ensure adequate fiber lock. Penetration of the backcoat through to the face of the carpet shall be controlled to provide the required resistance to abrasion and fiber loss, but backcoat shall not be visible on the
12、face of the pile fiber. If the carpet does not have a back coating it shall be a fused backed carpet. 3.6 APPEARANCE The color, pattern, and finish shall match the approved Design Center master sample. 3.7 PHYSICAL PROPERTIES 3.7.1 Short Term Environmental Cycling (FLTM BO 040-01, Procedure A, 80 C,
13、 except run evaluation on rolled goods 300 x 300 +/- 2 mm) Rating 4 min 2% max Shrinkage/Expansion 3.7.2 Long Term Environmental Cycling (FLTM BO 040-01, Procedure B, 80 C, except run evaluation on rolled goods 300 x 300 +/- 2 mm) Rating 4 min 2% max Shrinkage/Expansion 3.7.3 Resistance to Mildew (7
14、 days at 98 +/- 2% relative humidity and 38 +/- 2 C, Specimen size 100 mm x 100 mm) Remove the part from the cabinet and evaluate (smell the sample) immediately. The part shall exhibit no visible evidence of mildew growth and / or objectionable odor after the 7 day exposure. 3.7.4 Stretch and Set (f
15、or cut and sew seat back applications only) (SAE J855) WMD & AMD Stretch WMD & AMD Set 18% max5% max3.8 APPEARANCE PROPERTIES 3.8.1 Resistance to Fade (FLTM BO 116-01, ISO 105-A02/ AATCC Evaluation Procedure 1) 225.6 kJ/m2Rating 4 min3.8.2 Fiber Deterioration after UV Exposure (SAE J1530-A, 500 g lo
16、ad, H-10 wheels) 900 cycles No deterioration of fibers or yarns after testing to the applicable exposure levels in section 3.5.1 on molded production components. See Appendix 1 for failure criteria. ENGINEERING MATERIAL SPECIFICATIONPage 3 of 11Copyright 2016, Ford Global Technologies, LLCWSS-M15P32
17、-D 3.8.3 Heat Aging Rating 4 min (7 days at 80 +/- 2 C, ISO 105-A02/ AATCC Evaluation Procedure 1 Use a sample size of 100 x 100 mm.) No individual yarn or combination of yarns shall exhibit fiber deterioration or color tone change in excess of the above rating. There shall be no visual deterioratio
18、n of the backcoating. 3.8.4 Resistance to Rubbing (Crocking) (FLTM BN 107-01, ISO 105-A02/ AATCC Evaluation Procedure 2) Rating 4 min3.8.5 Soiling and Cleanability (FLTM BN 112-08, ISO 105-A02/ AATCC Evaluation Procedure 2) Rating 4 min3.9 WEAR PROPERTIES 3.9.1 Resistance to Abrasion 1200 cycles (SA
19、E J1530A, 500 g load, H-10 wheel) The carpet shall exhibit no visual evidence of wear through to the foundation of the pile fibers in the abraded area. See Appendix 1 for acceptance criteria. No roping or pilling allowed. 3.9.2 Resistance to Snagging 50 cycles (SAE J1530A, 500 g load, H-18 wheels) N
20、o evidence of fiber pullout allowed. See Appendix 2 for acceptance criteria. 3.10 COMPOSITE TESTING 3.10.1 Short Term Environmental Cycling Rating 4 min (FLTM BO 040-01, Procedure A, 80 C) 3.10.2 Long Term Environmental Cycling Rating 4 min (FLTM BO 040-01, Procedure B, 80 C) 3.10.3 Cold Impact (Flo
21、or Components Only) (Age 24 h at 80 +/- 2 C, then condition for 5 h at - 30 C) Rubber Ball 4.5 kg weight, 127 mm dia 60 +/- 5, Durometer “A“, (ISO 686/ASTM D 2240) Mount the portion of the assembly to be tested on an actual or simulated production support foundation with the approved retention metho
22、ds. Condition the sample then remove from the cold box and immediately (within 10 seconds), drop the rubber ball from a height indicated below in the most adverse locations as noted on the Engineering Drawing. Within the next 110 seconds, remove the trim from the actual or ENGINEERING MATERIAL SPECI
23、FICATIONPage 4 of 11Copyright 2016, Ford Global Technologies, LLCWSS-M15P32-D simulated production support foundation and evaluate. (See section 4 for rubber ball supplier contact information). Drop Height 610 mm The assembly shall show no evidence of cracking or breaking on either side of the part
24、after the ball drop test or removal from the support foundation and shall fully recover from indentation caused by the ball drop test in the time required for the assembly to return to 23 +/- 2 C. Evaluation should be performed on the substrate avoiding any mold in color handles, etc. Breakage of mo
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