FORD WSS-M99P43-D-2015 PERFORMANCE GENUINE LEATHER TO BE USED WITH FORD WSS-M99P1111-A .pdf
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1、 ENGINEERING MATERIAL SPECIFICATION Date Action Revisions Rev. 6 2015 12 15 Editorial See Summary of Revisions M. Montgomery, EU 2015 10 16 Editorial See Summary of Revisions L. Schmalz, NA 2015 02 27 Released L. Schmalz, NA Controlled document at www.MATS Copyright 2015, Ford Global Technologies, L
2、LC Page 1 of 8 PERFORMANCE, GENUINE LEATHER WSS-M99P43-D 1. SCOPE This specification defines the performance requirements for interior trim and seating leather. 2. APPLICATION This specification was released to outline the performance of interior trim and seating leather, the requirements are applic
3、able to chrome or chrome free tanned leather. 2.1 LIMITATIONS Do not use this specification for steering wheel, gearshift or handbrake leather. (See WSS-M1F21- C/latest or WSS-M1F22-C/latest) and instrument panel (WSS-M15P45-B/latest) applications. 3. REQUIREMENTS 3.1 STANDARD REQUIREMENTS FOR PRODU
4、CTION MATERIALS Material suppliers and part producers must conform to the Companys Standard Requirements For Production Materials (WSS-M99P1111-A). Materials used in interior applications must meet the requirements outlined in WSS-M99P2222-D1 or latest, Performance, Vehicle Interior Environment Qual
5、ity Material/Component Requirements. Data must be included in the material submission package. No buffing, stuccoing, filling or other repair is permitted unless otherwise stated on individual Material Specifications. It is the Leather suppliers responsibility to inform the JIT supplier that subject
6、ing leather to steam or radiant heat or organic solvents during any manufacturing process will adversely affect the hand and appearance characteristics. Perforated leather must also meet requirements for Fully Perforated Leather, achieved by using a sealer known as flesh coating, to bind any loose f
7、ibers and to ensure flesh side fibers will not be visible through perforation holes on the A surface. Note: All leather is expected to meet these requirements except when noted in the individual WSS-M1FXXX range of material specifications For all test methods, no individual specimen shall fall below
8、 the minimum values specified. 3.2 SAMPLE SELECTION LOCATIONS The location of the test samples is described in ISO 2418 or ASTM D2813 for physical testing of leather samples. Samples to be taken for the belly and backbone areas as noted in Table 1. ENGINEERING MATERIAL SPECIFICATION WSS-M99P43-D Cop
9、yright 2015, Ford Global Technologies, LLC Page 2 of 8 3.3 APPEARANCE The color, grain, gloss and hand shall match the approved Corporate Design master sample. 3.4 FOGGING (SAE J1756, Method B: Gravimetric Procedure 16 h at 100 C heating, 21 C cooling plate, post test conditioning, 4 h) Weight of Co
10、ndensate 4.0 mg max Samples shall be predried by storing in a desiccator over silica gel or equivalent for a period of 2 days. 3.5 ODOR Rating 3 max (FLTM BO 131-03) 3.6 FLAMMABILITY (ISO 3795/SAE J369) Burn Rate 100mm/minute max 3.7 CONSTRUCTION PROPERTIES 3.7.1 Cold Flexibility -30 C or below (SAE
11、 J323, Method A) The material must remain flexible and after bending at 180 it must not exhibit cracks. 3.7.2 Bally Flex Test (FLTM BN 162-01) 3.7.2.1 Original 100,000 cycles 3.7.2.2 After Heat Aging per 3.8.2 30,000 cycles 3.7.2.3 After Humidity Aging per 3.8.3 30,000 cycles No cracking of the surf
12、ace finish with a 6X microscope when the sample is bent over a 12 +/- 2 mm mandrel in the direction of the test area. 3.7.3 Finish Adhesion after Bally Flex/W Flex 3.5 N min (100,000 cycles of FLTM BN 162-01 / FLTM BN 102-02 followed by ISO 11644, Adhesive: Cyanoacrylate- Sicomet 8400, Supplier: Hen
13、kel, or equivalent. Condition bonded test specimens for 1 hour min.) 3.7.4 Breaking Strength 400 N min (ASTM D2208, Grab Method, Any direction) 3.7.5 Elongation at 100 N 40% max (ASTM D2211, Grab Method, use 152 x 76 mm sample per breaking strength and distance between grips 76 +/- 3.2 mm ) 3.7.6 Te
14、ar Strength (Trapezoid) 70 N min (ASTM D5587) ENGINEERING MATERIAL SPECIFICATION WSS-M99P43-D Copyright 2015, Ford Global Technologies, LLC Page 3 of 8 3.7.7 Seam Fatigue Resistance (FLTM BN 106-02) Needle hole elongation after test 2 mm max 3.7.8 Resistance to Scuffing. 200 cycles min. (SAE J365, S
15、cuff head A) No breakthrough or cracking of coating. No permanent parallel deformation to the surface, no break of the finish. Color change must be reviewed and approved by the responsible Materials Engineer. 3.7.9 Simulated Seat Wear No wear through the (FMVSS 209, S5.1 (d), 10,000 cycles, finish t
16、o russet except replace the hexagonal steel rod with a 40 mm dia. round steel rod covered with 2 mm thick rubber sheet, and abrade with No 8 cotton duck, 60 cycles/min, 250 mm stroke length). 3.7.10 Resistance to Top Coat Wear 5 minutes min (FLTM BN 108-14, 89 N Load) Also, report time to wear throu
17、gh to the russet (check every 3 minutes, max time-30 minutes) 3.7.11 Adhesion of Surface Coating, (ISO 11644, Adhesive Sicomet 8400 or equivalent Supplier: Henkel, or equivalent Condition bonded test specimens for 1 hour min.) As received 4N/10mm min After humidity (para 3.9.3) 4N/10mm min 3.7.12 Re
18、sistance to Mildew (7 days at 98 +/- 2 % relative humidity and 38 +/-2C, Specimen size is 200 x 200 mm unless part size is smaller.) 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 aft
19、er the 7 day exposure. 3.7.13 Thickness Range (ASTM D 1813) Report only (reference the Material Specification) 3.7.14 Stiffness Report only (reference (FLTM BN 157-02) the Material Specification) 3.8 COLOR PROPERTIES The material shall not exhibit any change in appearance such as color change, tone
20、change, fading or gloss change in excess of the required AATCC rating. In addition, the material shall not exhibit staining, blistering, loss of coating adhesion, peeling, chalking, cracking, splits, or tackiness. ENGINEERING MATERIAL SPECIFICATION WSS-M99P43-D Copyright 2015, Ford Global Technologi
21、es, LLC Page 4 of 8 3.8.1 Resistance to Fade (FLTM BO 116-01, ISO 105-A02/ AATCC Evaluation Procedure 1) 977.6 kJ/m2 Rating 4 min In addition, the material must remain flexible and exhibit no cracking when bent around a 12 +/-2 mm mandrel. 3.8.2 Resistance to Heat Aging Rating 4 min (7 days at 100 +
22、/- 2 C, ISO 105-A02/AATCC Evaluation Procedure 1) (Expose three samples, one for Visual Evaluation, one for Bally Flex and one for Xenon if needed) After exposure, the material shall no evidence of excessive loss of grain or exhibit staining, color tone change, or change in hue in excess of required
23、 AATCC rating (See Note). Any “spotty” or non-uniform staining or discoloration shall be cause for rejection. Note: If rating is less than 4, then the material must be subjected to Xenon Arc weathering to determine if the observed color change is temporary or permanent. Use one sample exposed in 3.8
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