NAVISTAR TMS 7109-2001 Molded Fiberglass Headliner (Revision A-1).pdf
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1、 This document is restricted and may not be sent outside International Truck and Engine Corporation or reproduced without permission from Corporate Technical Standards. Suppliers are required to assume all patent liability. Ge32001 by International Truck and Engine Corporation. AUGUST 2001 Page 1 of
2、 4 INTERNATIONAL TRUCK AND ENGINE CORPORATION TMS (TRUCK MATERIAL SPECIFICATION) NUMBER: TMS-7109 TITLE: Molded Fiberglass Headliner REVISION: A-1 WRITTEN/EDITED BY: Materials Engineering APPROVED BY: Materials Engineering DATE ISSUED: August 2001 PRINTED COPIES OF THIS DOCUMENT MUST BE VERIFIED FOR
3、 CURRENT REVISION This specification may involve hazardous materials, equipment, and procedures. This specification does not purport to address all of the safety issues associated with its use. The user is responsible to consult appropriate safety and health practices and to determine the applicabil
4、ity of regulatory limits prior to use. Change Notice: Reformatted and Editorial Changes Reference: File 30-14D Keywords: Fiberglass; Molded Headliner 1.0 APPLICATION This specification covers a composite headliner consisting of a molded fiberglass core with a non-woven backing material and a bonded
5、decorative fabric facing. 2.0 SCOPE This specification covers the general requirements for the molded fiberglass headliner core and performance requirements of the finished headliner. 3.0 REFERENCE DOCUMENTS Unless otherwise specified, the latest issue of all referenced standards shall apply. The fo
6、llowing standards, specifications and regulations are referenced in this specification. Quality System Standard QS-9000 (ISO 9001) ASTM D 903 INTERNATIONAL IQR Quality Standard FMVSS INTERNATIONAL Manufacturing Std. D-13 INTERNATIONAL Test Procedure NV-2C1 CFR Title 29, Part 1910 ASTM C 384 4.0 GENE
7、RAL REQUIREMENTS 4.1 The molded fiberglass headliner core shall consist of: 4.1.1 Glass fibers .0043-.0061 mm (.00017-.00024 in) in diameter and up to 50 mm (2 in) in length. 4.1.2 A suitable non-toxic and non-malodorous phenolic resin binder with a total resin content of 15-19 percent and a surface
8、 resin content of 20-24 percent. 4.1.3 A suitable non-woven backing material that will protect the part until it has been installed in the vehicle. 4.1.4 The fiberglass core shall have a density of 256 25 kg/m (16 1.6 lbs/ft) for nominal 5 mm (.2 in) thick sections and 64 6 kg/m (4 .4 lbs/ft) for no
9、minal 25 mm (1 in) thick sections. 4.1.5 Reinforcement may be required as designated on the part drawing. When reinforcement is required, the method and placement of the reinforcement shall be fully detailed on the part drawing. NUMBER: TMS-7109 TITLE: Molded Fiberglass Headliner REVISION: A-1 This
10、document is restricted and may not be sent outside International Truck and Engine Corporation or reproduced without permission from Corporate Technical Standards. Suppliers are required to assume all patent liability. Ge32001 by International Truck and Engine Corporation. AUGUST 2001 Page 2 of 4 4.2
11、 The bonded fabric facing shall consist of: 4.2.1 An adhesive that will bond securely, such that a peel test, per ASTM D-903, will result in the destruction of the glass fiber surface or a minimum peel strength of 800 N/m (4.6 lbf/in) width. No adhesive bleed-thru shall be permitted. 4.2.2 A fabric
12、covering that meets the requirements of the International specification as indicated on the part drawing. 4.3 All materials and the composite assembly must conform with Federal regulations concerning materials of this type, such as the flammability requirements of FMVSS 302 and TMS-9544. 4.4 PERFORM
13、ANCE REQUIREMENTS 4.4.1 Cyclic Aging 4.4.1.1 Sample Preparation: Seven (7) boards 200 x 300 x 5 mm (8 x 12 x 0.2 in) and seven (7) boards 200 x 300 x 25 mm (8 x 12 x 1 in) shall be prepared by cutting sections from production headliners or suitable samples representative of a production part. All bo
14、ards must include the decorative fabric facing on one of the 200 x 300 mm (8 x 12 in) faces. 4.4.1.2 Method: All fourteen (14) boards are subjected to the seven-step aging test shown in the table below. One board of each thickness 5 and 25 mm (0.2 and 1 in) is subjected to 180 peel tests per ASTM D9
15、03 after each step in the aging cycle, except as indicated below. Three peel test samples measuring 25 x 200 mm (1 x 8 in) are cut from each board for this testing. The peel test samples shall be cut immediately before the peel test and shall not be closer than 25 mm (1 in) to an edge or any other p
16、eel test sample. After cutting the peel test samples, the test chamber and all samples shall be returned to the conditions of the particular step before performing the peel test. 4.1.1.3 Required: There shall be no loss of adhesion between the fabric facing and the fiberglass core or delamination of
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