Technical Report. Product testing of 6 mm Graniti Fiandre Maximum panels with support system and fabrication by Telling Architectural

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Technical Report Title: Product testing of 6 mm panels with support system and fabrication by Telling Architectural Report No: N950-14-16799

CONTENTS 1 INTRODUCTION...4 2 CLASSIFICATION OF TEST RESULTS...5 3 DESCRIPTION OF TEST SAMPLE...6 4 TEST RIG GENERAL ARRANGEMENT...9 5 TEST SEQUENCE...10 6 AIR PERMEABILITY TESTING...11 7 WATERTIGHTNESS TESTING...14 8 WIND RESISTANCE TESTING...17 9 IMPACT TESTING...27 10 APPENDIX - DRAWINGS...40 Page 3 of 40

1 INTRODUCTION This report describes tests carried out at VINCI Technology Centre UK Limited at the request of Telling Architectural Ltd. The test sample consisted of 6 mm panels with support system and fabrication by Telling Architectural. The tests were carried out in on 26 February 2014 and were to determine the weathertightness and impact resistance of the test sample. The test methods were in accordance with the CWCT Standard Test Methods for building envelopes, 2005, for: Dynamic pressure. Wind resistance serviceability & safety. Impact resistance. Note: The backing wall used for the test sample had been tested in December 2013 and the results are included in this report. The testing was carried out in accordance with Technology Centre Method Statement C4777/MS/rev 0. This test report relates only to the actual sample as tested and described herein. The results are valid only for sample(s) tested and the conditions under which the tests were conducted. VINCI Technology Centre UK Limited is accredited to ISO/IEC 17025:2008 by the United Kingdom Accreditation Service as UKAS Testing Laboratory No.0057. VINCI Technology Centre UK Limited is certified by BSI for: ISO 9001:2008 Quality Management System, ISO 14001:2004 Environmental Management System, BS OHSAS 18001:2007 Occupational Health and Safety Management System. The tests were witnessed by David Adams of Telling Architectural Ltd. Page 4 of 40

2 CLASSIFICATION OF TEST RESULTS The following summarises the results of the tests carried out. Sections 6, 7, 8 and 9. For full details refer to 2.1 CLASSIFICATION TABLE 1 Test Standard Classification / Declared value Air permeability CWCT A4 ± 600 pascals (Backing wall only) Watertightness CWCT Dynamic + 600 pascals Wind resistance CWCT Serviceability ± 2400 pascals Safety ± 3600 pascals Impact resistance CWCT TN75 Soft body serviceability Class 1 Soft body safety Low risk Hard body serviceability Class 4 Hard body safety Low risk Page 5 of 40

3 DESCRIPTION OF TEST SAMPLE 3.1 GENERAL ARRANGEMENT The sample was as shown in the photo below and the drawings included as an appendix to this report. The sample measured 3.0 m high by 4.4 m wide and comprised eight 6 mm thick Graniti Fiandre porcelain panels supported on an aluminium framework. The panels had a backing support mesh to prevent fragment fallout if damaged. The framework was mounted on a backing wall comprising a stud framework, cement particle boards and Tyvek sheeting. TEST SAMPLE ELEVATION PHOTO 3512 3.2 CONTROLLED DISMANTLING During the dismantling of the sample no water penetration or discrepancies from the drawings were found. Page 6 of 40

PHOTO 3537 PANEL REMOVED FROM TEST RIG PHOTO 3539 SAMPLE DURING CONTROLLED DISMANTLE Page 7 of 40

PHOTO 3541 PANEL SUPPORT CLIP Page 8 of 40

4 TEST RIG GENERAL ARRANGEMENT The test sample was mounted on a rigid test rig with support steelwork designed to simulate the on-site/project conditions. The test rig comprised a well sealed chamber, fabricated from steel and plywood. A door was provided to allow access to the chamber. Representatives of Telling Architectural installed the sample on the test rig. See Figure 1. TEST RIG SCHEMATIC ARRANGEMENT FIGURE 1 SEALED TEST CHAMBER TEST RIG SUPPORT STEELWORK, TO SIMULATE ON-SITE CONDITIONS WATER SPRAY GANTRY TEST SAMPLE RAINSCREEN TEST SAMPLE BACKING WALL PRESSURE TRANSDUCER CONTROLLED AND METERED AIR SUPPLY GENERATING POSITIVE AND NEGATIVE PRESSURES FAN COMPUTER CONTROLLED DATA LOGGER SECTION THROUGH TEST RIG Page 9 of 40

5 TEST SEQUENCE The test sequence was as follows: (1) Air permeability (2) Watertightness static (3) Wind resistance serviceability (4) Air permeability (5) Watertightness static (6) Watertightness dynamic (7) Wind resistance safety (8) Impact resistance Page 10 of 40

6 AIR PERMEABILITY TESTING 6.1 INSTRUMENTATION 6.1.1 Pressure One static pressure tapping was provided to measure the chamber pressure and was located so that the readings were unaffected by the velocity of the air supply into or out of the chamber. A pressure transducer, capable of measuring rapid changes in pressure to within 2% was used to measure the differential pressure across the sample. 6.1.2 Air Flow A laminar flow element mounted in the air system ductwork was used with a pressure transducer to measure the air flow into the chamber. This device was capable of measuring airflow through the sample to within 2%. 6.1.3 Temperature Platinum resistance thermometers (PRT) were used to measure air temperatures to within 1 C. 6.1.4 General Electronic instrument measurements were scanned by a computer controlled data logger, which also processed and stored the results. All measuring instruments and relevant test equipment were calibrated and traceable to national standards. 6.2 FAN The air supply system comprised a variable speed centrifugal fan and associated ducting and control valves to create positive and negative static pressure differentials. The fan provided essentially constant air flow at the fixed pressure for the period required by the tests and was capable of pressurising at a rate of approximately 600 pascals in one second. 6.3 PROCEDURE Three positive pressure pulses of 1200 pascals were applied to prepare the test sample. The average air permeability was determined by measuring the rate of air flow through the chamber whilst subjecting the sample to positive pressure differentials of 50, 100, 150, 200, 300, 450 and 600 pascals. Each pressure increment was held for at least 10 seconds. Extraneous leakage through the test chamber and the joints between the chamber and the test sample was determined by sealing the sample with adhesive tape (polythene sheet as mentioned in CWCT clause 5.10.3.1 was not used on this occasion) and measuring the air flow at the pressures given above. The test was then repeated with the sample unsealed; the difference between the readings being the rate of air flow through the backing wall. The test was then repeated using negative pressure differentials. Page 11 of 40

6.4 PASS/FAIL CRITERIA The permissible air flow rate, Q o, at peak test pressure, p o, could not exceed: 1.5 m 3 per hour per m 2. At intermediate pressures, p n, flow rates, Q n, were calculated using Q n = Q o ( p n/p o ) 2/3 The area of the sample was 13.2 m 2. 6.5 RESULTS TABLE 2 Pressure differential Measured air flow through backing wall (m 3 /hour/m 2 ) Test 1 Date: 12 December 2013 Test 4 Date: 13 December 2013 (pascals) Infiltration Exfiltration Infiltration Exfiltration 50 0.07 0.01 0.06 0.01 100 0.08 0.02 0.05 0.04 150 0.00 0.02 0.00 0.01 200 0.03 0.07 0.02 0.11 300 0.09 0.13 0.07 0.14 450 0.13 0.07 0.11 0.07 600 0.17 0.17 0.13 0.18 Temperatures Ambient = 7 C Chamber = 8 C Ambient = 9 C Chamber = 9 C The results are shown graphically in Figures 2 and 3. Page 12 of 40

FIGURE 2 Air infiltration test results Air flow / m3/hour/m2 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 Test 1 Test 4 Permissible 0 100 200 300 400 500 600 Pressure differential / pascals Air exfiltration test results FIGURE 3 Air flow / m3/hour/m2 1.6 1.4 1.2 1.0 0.8 0.6 0.4 0.2 0.0 Test 1 Test 4 Permissible 0 100 200 300 400 500 600 Pressure differential / pascals Page 13 of 40

7 WATERTIGHTNESS TESTING 7.1 INSTRUMENTATION 7.1.1 Pressure One static pressure tapping was provided to measure the chamber pressure and was located so that the readings were unaffected by the velocity of the air supply into or out of the chamber. A pressure transducer, capable of measuring rapid changes in pressure to within 2% was used to measure the differential pressure across the sample. 7.1.2 Water Flow An in-line water flow meter was used to measure water supplied to the spray gantry to within 5%. 7.1.3 Temperature Platinum resistance thermometers (PRT) were used to measure air and water temperatures to within 1 C. 7.1.4 General Electronic instrument measurements were scanned by a computer controlled data logger, which also processed and stored the results. All measuring instruments and relevant test equipment were calibrated and traceable to national standards. 7.2 FAN 7.2.1 Static Pressure Testing The air supply system comprised a variable speed centrifugal fan and associated ducting and control valves to create positive and negative static pressure differentials. The fan provided essentially constant air flow at the fixed pressure for the period required by the tests and was capable of pressurising at a rate of approximately 600 pascals in one second. 7.2.2 Dynamic Pressure Testing A wind generator was mounted adjacent to the external face of the sample and used to create positive pressure differentials during dynamic testing. The wind generator comprised a piston type aero-engine fitted with 4 m diameter contra-rotating propellers. 7.3 WATER SPRAY The water spray system comprised nozzles spaced on a uniform grid not more than 700 mm apart and mounted approximately 400 mm from the face of the sample. The nozzles provided a full-cone pattern with a spray angle between 90 and 120. The spray system delivered water uniformly against the exterior surface of the sample. Page 14 of 40

7.4 PROCEDURE 7.4.1 Watertightness static Three positive pressure pulses of 1200 pascals were applied to prepare the test sample. Water was sprayed onto the sample using the method described above at a rate of at least 3.4 litres/m 2 /minute for 15 minutes at zero pressure differential. With the water spray continuing the pressure differential across the sample was then increased in increments of: 50, 100, 150, 200, 300, 450 and 600 pascals, each held for 5 minutes. Throughout the test the interior face of the sample was examined for water penetration. 7.4.2 Watertightness dynamic Water was sprayed onto the sample using the method described above at a flow rate of at least 3.4 litres/m 2 /minute. The aero-engine was used to subject the sample to wind of sufficient velocity to produce by a static pressure differential of 600 pascals. These conditions were maintained for 15 minutes. Throughout the test the inside of the sample was examined for water penetration. DYNAMIC WIND GENERATOR PHOTO 3514 Page 15 of 40

7.5 PASS/FAIL CRITERIA There shall be no water penetration to the internal face of the backing wall throughout testing. At the completion of the test there shall be no standing water in locations intended to remain dry. 7.6 RESULTS Test 2 (Static pressure) Date: 12 December 2013 No water penetration through the backing wall was observed throughout the test. Chamber temperature= 9 C Ambient temperature = 7 C Water temperature = 8 C Test 5 (Static pressure) Date: 13 December 2013 No water penetration through the backing wall was observed throughout the test. Chamber temperature= 10 C Ambient temperature = 9 C Water temperature = 9 C Test 6 (Dynamic pressure) Date: 26 February 2014 No water penetration through the backing wall was observed throughout the test. Chamber temperature= 8 C Ambient temperature = 6 C Water temperature = 8 C Page 16 of 40

8 WIND RESISTANCE TESTING 8.1 INSTRUMENTATION 8.1.1 Pressure One static pressure tapping was provided to measure the chamber pressure and was located so that the readings were unaffected by the velocity of the air supply into or out of the chamber. A pressure transducer, capable of measuring rapid changes in pressure to within 2% was used to measure the differential pressure across the sample. 8.1.2 Deflection Displacement transducers were used to measure the deflection of principle framing members to an accuracy of 0.1 mm. The gauges were set normal to the sample framework at midspan and as near to the supports of the members as possible and installed in such a way that the measurements were not influenced by the application of pressure or other loading to the sample. The gauges were located at the positions shown in Figure 4. 8.1.3 Temperature Platinum resistance thermometers (PRT) were used to measure air temperatures to within 1 C. 8.1.4 General Electronic instrument measurements were scanned by a computer controlled data logger, which also processed and stored the results. All measuring instruments and relevant test equipment were calibrated and traceable to national standards. 8.2 FAN The air supply system comprised a variable speed centrifugal fan and associated ducting and control valves to create positive and negative static pressure differentials. The fan provided essentially constant air flow at the fixed pressure for the period required by the tests and was capable of pressurising at a rate of approximately 600 pascals in one second. 8.3 PROCEDURE 8.3.1 Wind Resistance serviceability on backing wall Three positive pressure differential pulses of 1200 pascals were applied to prepare the sample. The displacement transducers were then zeroed. The sample was subjected to one positive pressure differential pulse from 0 to 2400 pascals to 0. The pressure was increased in four equal increments each maintained for 15 ±5 seconds. Displacement readings were taken at each increment. Residual deformations were measured on the pressure returning to zero. Any damage or functional defects were recorded. The test was then repeated using a negative pressure of -2400 pascals. Page 17 of 40

8.3.2 Wind Resistance safety on backing Three positive pressure differential pulses of 1200 pascals were applied to prepare the sample. The displacement transducers were then zeroed. The sample was subjected to one positive pressure differential pulse from 0 to 3600 pascals to 0. The pressure was increased as rapidly as possible but not in less than 1 second and maintained for 15 ±5 seconds. Displacement readings were taken at peak pressure. Residual deformations were measured on the pressure returning to zero. Any damage or functional defects were recorded. The test was then repeated using a negative pressure of 3600 pascals. 8.3.3 Wind Resistance serviceability on rainscreen Note: For this test the joints between the rainscreen panels were sealed over and the pressure applied to the cavity between the backing wall and panels, via holes in the plywood sides. Three positive pressure differential pulses of 1200 pascals were applied to prepare the sample. The displacement transducers were then zeroed. The sample was subjected to one positive pressure differential pulse from 0 to 2400 pascals to 0. The pressure was increased in four equal increments each maintained for 15 ±5 seconds. Displacement readings were taken at each increment. Residual deformations were measured on the pressure returning to zero. Any damage or functional defects were recorded. The test was then repeated using a negative pressure of -2400 pascals. 8.3.4 Wind Resistance safety on rainscreen Note: For this test the joints between the rainscreen panels were sealed over and the pressure applied to the cavity between the backing wall and panels. Three positive pressure differential pulses of 1200 pascals were applied to prepare the sample. The displacement transducers were then zeroed. The sample was subjected to one positive pressure differential pulse from 0 to 3600 pascals to 0. The pressure was increased as rapidly as possible but not in less than 1 second and maintained for 15 ±5 seconds. Displacement readings were taken at peak pressure. Residual deformations were measured on the pressure returning to zero. Any damage or functional defects were recorded. The test was then repeated using a negative pressure of 3600 pascals. Page 18 of 40

FIGURE 4 DEFLECTION GAUGE LOCATIONS External and Internal Views 1 2 3 5 4 Deflection gauge 6 3 5 2 4 1 Deflection gauge Page 19 of 40

8.4 PASS/FAIL CRITERIA 8.4.1 Calculation of permissible deflection for backing wall Gauge number Member Span (L) (mm) Permissible deflection (mm) Permissible residual deformation 2, 5 Vertical span 3000 L/200= 15.0 1 mm 8.4.2 Calculation of permissible deflection for rainscreen panels Gauge number Member Span (L) (mm) Permissible deflection (mm) 2 Panel width 3000 L/90 = 33.3 8.5 RESULTS Test 3 (serviceability) Date: 26 February 2014 The deflections measured during the wind resistance test, at the positions shown in Figure 4, are shown in Tables 3 and 4 for the backing wall and 6 and 7 for the rainscreen panels. Summary Table for backing: Gauge number Member Pressure differential (Pa) Measured deflection (mm) Residual deformation (mm) 2 Stud rail 2397-2410 6.3 4.6 0.3-0.4 5 Backing wall panel 2397-2410 6.7 5.7 0.3-0.3 No damage to the test sample was observed. Page 20 of 40

Summary Table for rainscreen: Gauge number Member Pressure differential (Pa) Measured deflection (mm) Residual deformation (mm) 2 Horizontal span of panel 2396-2392 8.8-2.5 0.0 0.0 No damage to the test sample was observed. Ambient temperature = 4 C Chamber temperature = 6 C Test 7 (safety) Date: 26 February 2014 The deflections measured during the structural safety test, at the positions shown in Figure 4, are shown in Table 5 for the backing wall and Table 8 for the rainscreen panels. No damage to the sample was observed. Ambient temperature = 5 C Chamber temperature = 7 C Page 21 of 40

TABLE 3 WIND RESISTANCE POSITIVE SERVICEABILITY TEST RESULTS BACKING WALL Position Pressure (pascals) / Deflection (mm) 606 1195 1822 2397 Residual 1 0.1 0.1 0.3 0.4 0.0 2 1.5 3.0 5.1 7.2 0.4 3 0.4 0.7 1.0 1.3 0.1 4 0.5 1.0 1.8 2.5 0.2 5 1.8 3.7 6.3 8.8 0.5 6 0.4 0.7 1.2 1.6 0.2 2 * 1.2 2.6 4.5 6.3 0.3 5 * 1.4 2.8 4.8 6.7 0.3 * Mid-span reading adjusted between end support readings Page 22 of 40

TABLE 4 WIND RESISTANCE NEGATIVE SERVICEABILITY TEST RESULTS BACKING WALL Position Pressure (pascals) / Deflection (mm) -604-1193 -1798-2410 Residual 1-0.1-0.2-0.3-0.4-0.1 2-1.4-2.5-3.8-5.4-0.5 3-0.3-0.5-0.8-1.1-0.1 4-0.6-1.0-1.5-2.2-0.2 5-1.9-3.5-5.3-7.5-0.4 6-0.4-0.6-0.9-1.3-0.1 2 * -1.2-2.2-3.3-4.6-0.4 5 * -1.4-2.6-4.1-5.7-0.3 * Mid-span reading adjusted between end support readings Page 23 of 40

TABLE 5 WIND RESISTANCE - SAFETY TEST RESULTS BACKING WALL Position Pressure (pascals) / Deflection (mm) 3599 Residual -3599 Residual 1 0.7 0.1-0.9-0.3 2 10.9 0.0-10.8-1.0 3 1.8 0.2-2.2-0.4 4 3.8 0.2-4.0-0.6 5 13.3 0.4-14.2-0.9 6 2.3 0.2-2.5-0.3 2 * 9.6-0.1-9.5-0.7 5 * 10.2 0.2-11.0-0.5 * Mid-span reading adjusted between end support readings Page 24 of 40

TABLE 6 WIND RESISTANCE POSITIVE SERVICEABILITY TEST RESULTS RAINSCREEN PANELS Position Pressure (pascals) / Deflection (mm) 601 1217 1805 2396 Residual 1 1.7 2.9 4.6 6.3 0.3 2 4.5 8.6 12.6 17.0 0.3 3 2.4 4.9 7.4 10.1 0.3 4 2.1 3.6 5.0 6.8 0.3 5 5.1 9.9 14.5 19.7 0.3 2 * 2.4 4.7 6.6 8.8 0.0 * Mid-span reading adjusted between end support readings TABLE 7 WIND RESISTANCE NEGATIVE SERVICEABILITY TEST RESULTS RAINSCREEN PANELS Position Pressure (pascals) / Deflection (mm) -609-1207 -1820-2392 Residual 1-1.4-2.7-4.0-5.3 0.0 2-2.4-4.7-7.1-9.3 0.0 3-1.9-3.9-6.1-8.2 0.1 4-1.2-2.3-3.3-4.2 0.0 5-3.0-6.0-9.1-12.1 0.1 2 * -0.7-1.4-2.0-2.5 0.0 * Mid-span reading adjusted between end support readings Page 25 of 40

TABLE 8 WIND RESISTANCE SAFETY TEST RESULTS RAINSCREEN PANELS Position Pressure (pascals) / Deflection (mm) 3591 Residual -3605 Residual 1 9.5-0.4-8.2-0.1 2 26.7-0.5-14.3-0.4 3 15.5-0.4-12.9-0.4 4 10.5-0.2-6.2-0.2 5 31.2-0.8-19.1-0.5 2 * 14.2-0.1-3.8-0.1 * Mid-span reading adjusted between end support readings Page 26 of 40

9 IMPACT TESTING 9.1 IMPACTOR 9.1.1 Soft body The soft body impactor comprised a canvas spherical/conical bag 400 mm in diameter filled with 3 mm diameter glass spheres with a total mass of approximately 50 kg suspended from a cord at least 3 m long. 9.1.2 Hard body The hard body impactor was a solid steel ball of 50 mm or 62.5 mm diameter and approximate mass of 0.5 kg or 1.0 kg. 9.2 PROCEDURE (BS 8200) 9.2.1 Soft body The impactor almost touched the face of the sample when at rest. It was swung in a pendular movement to hit the sample normal to its face. The test was performed at locations 1 to 7 shown in Figure 5. The impact energies were 120 Nm, 350 Nm and 500 Nm. 9.2.2 Hard body The impactor almost touched the face of the sample when at rest. It was swung in a pendular movement to hit the sample normal to its face. The test was performed at locations 8 to 14 shown in Figure 5. The impact energies were 6 and 10 Nm. IMPACT TEST LOCATIONS External View FIGURE 5 7 6 12 13 14 10 4 11 1 2 3 5 9 8 Locations of hard impact Locations of soft impact Page 27 of 40

9.3 PASS/FAIL CRITERIA Note: Tables 1 to 5 are taken from CWCT TN75. Table 1 Exposure categories Category Description Examples A Readily accessible to public and others with little incentive to exercise care. Prone to vandalism and abnormally rough use External walls of housing and public buildings in vandal prone areas B Readily accessible to public and others with little incentive to exercise care. Chances of accident occurring and of misuse Walls adjacent to pedestrian thoroughfares or playing fields when not in category A Zone of wall up to 1.5 m above pedestrian or floor level C Accessible primarily to those with some incentive to exercise care. Some chance of accident occurring and of misuse Walls adjacent to private open gardens. Back walls of balconies D Only accessible, but not near a common route, to those with high incentive to exercise care. Small chance of accident occurring or misuse Walls adjacent to small fenced decorative garden with no through paths E F Above zone of normal impacts from people but liable to impacts from thrown or kicked objects Above zone of normal impacts from people and not liable to impacts from thrown or kicked objects 1.5 m to 6 m above pedestrian or floor level at location categories A and B Wall surfaces at higher positions than those defined in E above Page 28 of 40

Table 2 Soft body test energy Exposure category Safety Serviceability A No values are given as severity of potential vandalism needs to be assessed B 500 Nm 120 Nm C 500 Nm 120 Nm D No values given as risk of impact is minimal E 350 Nm 120 Nm F 350 Nm 120 Nm Table 3 Hard body test energy Exposure category Safety Serviceability A No values are given as severity of potential vandalism needs to be assessed B 10 Nm 10 Nm C 10 Nm 6 Nm D No values given as risk of impact is minimal E 10 Nm 6 Nm F 3 Nm 3 Nm Page 29 of 40

Table 4 - Classes for safety performance Class Negligible risk Explanation/examples No material dislodged during test, and No damage likely to lead to materials falling subsequent to test, and No sharp edges produced that would be likely to cause severe injury to a person during impact, and Cladding not penetrated by impactor. Low risk Moderate risk High risk Maximum mass of falling particle 50g, and Maximum mass of particle that may fall subsequent to impact 50g, and No sharp edges produced that would be likely to cause severe injury during impact. Maximum mass of falling particle less than 500g, and Maximum mass of particle that may fall subsequent to impact less than 500g, and Cladding not penetrated by impact, and No sharp edges produced that would be likely to cause severe injury during impact. Maximum mass of falling particle greater than 500g, or Cladding penetrated by impact, or Sharp edges produced that would be likely to cause severe injury during impact. Page 30 of 40

Table 5 - Classes for serviceability performance Class Definition Explanation/Examples 1 No damage. 2 Surface damage of an aesthetic nature which is unlikely to require remedial action. 3 Damage that may require remedial action or replacement of components to maintain appearance or long term performance but does not require immediate action. No damage visible from 1m, and Any damage visible from closer then 1m unlikely to lead to significant deterioration. Dents or distortion of panels not visible from more than 5m (note visibility of damage will depend on surface finish and lighting conditions damage will generally be more visible on reflective surfaces), and Any damage visible from closer than 5m unlikely to lead to significant deterioration. Dents or distortion of panels visible from more than 5m, or Spalling of edges of panels of brittle materials, or Damage to finishes that may lead to deterioration of the substrate. 4 Damage requiring immediate action to maintain appearance or performance. Remedial action may include replacement of a panel but does not require dismantling or replacement of supporting structure. 5 Damage requiring more extensive replacement than 4. Significant cracks in brittle materials e.g. cracks that may lead to parts of tile falling away subsequent to test, or Fracture of panels causing significant amounts of material to fall away during test. Buckling of support rails. Page 31 of 40

9.4 RESULTS Test 8 Date: 26 February 2014 Ambient temperature = 6 C TABLE 9 IMPACT TEST RESULTS Impact location Impactor Impact energy (Nm) Observations 1 Soft body 120 (x 3) No damage observed. 2 Soft body 350 Cracks with minor fragments, longest 38 mm. 3 Soft body 350 Hairline cracks, no fragments 4 Soft body 350 No damage observed. 5 Soft body 500 Cracks with minor fragments, longest 33 mm. 6 Soft body 500 No damage observed. 7 Soft body 500 Cracks with minor fragments, longest 32 mm. 8 Hard body 6 Minor surface crack. 9 Hard body 6 No damage observed. 10 Hard body 6 No damage observed. 11 Hard body 10 5-way hairline cracks. 12 Hard body 10 4-way hairline cracks. 13 Hard body 10 Crack on right hand panel. 14 Hard body 10 Crack on left hand panel Page 32 of 40

PHOTO 3516 SOFT BODY IMPACTOR PHOTO 3532 HARD BODY IMPACTOR Page 33 of 40

PHOTO 3518 LOCATION 2 IMPACT PHOTO 3519 LOCATION 2 FRAGMENTS Page 34 of 40

PHOTO 3521 LOCATION 3 IMPACT PHOTO 3523 LOCATION 5 IMPACT Page 35 of 40

PHOTO 3524 LOCATION 5 FRAGMENTS PHOTO 3527 LOCATION 7 IMPACT Page 36 of 40

PHOTO 3528 LOCATION 7 FRAGMENTS PHOTO 3530 LOCATION 8 IMPACT Page 37 of 40

PHOTO 3533 LOCATION 11 IMPACT PHOTO 3534 LOCATION 12 IMPACT Page 38 of 40

PHOTO 3535 LOCATION 13 IMPACT PHOTO 3536 LOCATION 14 IMPACT Page 39 of 40

10 APPENDIX - DRAWINGS The following 4 unnumbered pages are copies of Telling Architectural Ltd. drawings numbered: GF-010 rev C, GF-011 rev C, GF-012 rev C, GF-013 rev C. END OF REPORT Page 40 of 40

ALL ELEVATIONS ARE VIEWED FROM OUTSIDE UNLESS OTHERWISE STATED CONTRACT NUMBER : TILE SYSTEM : SPECIFICATION TP 3008 MODULE MODULE SIZE : COLOUR : 1504 MODULE 1504 MODULE 800 MODULE 592 MODULE Panels 3 1498 6 Joint 1498 6 794 6 586 3 25 190 25 170 635 635 121 100 644 659 206 Horizontal Rails 1500 6 JOINT 1470 21 Panels 1494 1506 Modules 3000 3071 Trim A A 1498*1470 Plate & Panel UKD 1498*708 Plate & Panel UKE 1498*451 Plate & Panel UKF 1498*299 Plate & Panel UKG 3002*1500 Plate & Panel 794*2994 Plate & Panel UKH 586*1470 Plate & Panel UKK 586*1518 Plate & Panel UKJ 3000 Steel 162 900 900 876 162 Carrier Brackets 25 190 25 170 99 206 251 206 508 121 100 644 659 206 Horizontal Rails PANEL JOINT PANEL JOINT PANEL JOINT 1500 6 JOINT 299 6 JOINT 451 6 JOINT 708 21 Panels 305 457 732 1506 Modules 3000 3071 Trim C 29.01.14 Single panel added 3 3 B 19.12.13 Dims updated. TEST ISSUE A 7.11.13 Initial Issue Rev. Date Comments SECTION B-B ELEVATION B B C C SECTION C-C Drawing Status : Contract : GRANITI FIANDRE 6mm PORCELAIN PANELS TAL SYSTEM VINCI TEST PANEL 30 100 270 600 600 600 600 600 600 270 100 30 GRANITI FIANDRE PLATES ALL 6mm THICK MESH BACKED 3 104 416 560 PLAN A-A 560 1200 560 3002 560 1200 4400 Steel 560 600 600 384 104 104 592 104 104 384 104 6 794 6 586 3 25 170 25 190 3002*1500 Plate 1498*1470 Plate UKD 1498*708 Plate UKE 1498*451 Plate UKF 1498*299 Plate UKG 794*2994 Plate UKH 586*1518 Plate UKJ 586*1470 Plate UKK Telling Architectural Ltd 7 The Dell Enterprise Drive Four Ashes Wolverhampton Tel : 01902 797 700 WV10 7DF Fax : 01902 797 720 Drawing Title : Telling Architectural Ltd Do not scale from this drawing. If in doubt ask VINCI TEST PANEL TELLING ARCHITECTURAL PANEL SETOUT Scale : Drawn : 1 : 25 Date : psk 07.11.13 Size A3 Drawing No. GF-010 Rev. C

ALL ELEVATIONS ARE VIEWED FROM OUTSIDE UNLESS OTHERWISE STATED CONTRACT NUMBER : TILE SYSTEM : MODULE SIZE : COLOUR : SPECIFICATION TP 15 Face of stud 15 Face of stud 254 X 254 X 107 UC 254 X 254 X 107 UC 153 x 60 x 1.5mm TRACK 254 X 254 X 107 UC 30 100 270 600 600 600 600 600 600 270 100 30 3000 3000 Steel 3000 A A 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 150 x 60 x 1.5mm STUD 153 x 60 x 1.5mm TRACK 254 X 254 X 107 UC C 29.01.14 Single panel added B 19.12.13 Dims updated. TEST ISSUE A 7.11.13 Initial Issue 25 170 SECTION B-B ELEVATION B B C C 25 170 SECTION C-C Rev. Date Comments Drawing Status : Contract : GRANITI FIANDRE 6mm PORCELAIN PANELS TAL SYSTEM VINCI TEST PANEL 30 100 270 600 600 600 600 600 600 270 100 30 SFS MATERIALS 15 Face of Stud 150 x 60 x 1.5mm STUD 9no 2970 153 x 60 x 1.5mm TRACK 2no 3300 5no CP Lining Boards Telling Architectural Ltd 7 The Dell Enterprise Drive Four Ashes Wolverhampton Tel : 01902 797 700 WV10 7DF Fax : 01902 797 720 Telling Architectural Ltd Do not scale from this drawing. If in doubt ask PLAN A-A 4400 Steel Drawing Title : VINCI TEST PANEL TELLING ARCHITECTURAL STEEL STUD BACKING WALL Scale : Drawn : 1 : 25 Date : psk 07.11.13 Size A3 Drawing No. GF-011 Rev. C

ALL ELEVATIONS ARE VIEWED FROM OUTSIDE UNLESS OTHERWISE STATED CONTRACT NUMBER : TILE SYSTEM : MODULE SIZE : COLOUR : SPECIFICATION TP 25 99 254 X 254 X 107 UC Carrier Brackets 25 99 A A 254 X 254 X 107 UC 416 1200 1200 600 600 384 254 X 254 X 107 UC 162 900 900 876 162 3 2990 7 254 X 254 X 107 UC 3000 Steel 162 900 900 876 162 3 2990 7 3000 C 29.01.14 Single panel added B 19.12.13 Dims updated. TEST ISSUE A 7.11.13 Initial Issue Rev. Date Comments 46 14 ELEVATION B B C C SECTION C-C Drawing Status : Contract : 30 30 GRANITI FIANDRE 6mm PORCELAIN PANELS TAL SYSTEM VINCI TEST PANEL VERTICAL T AND BRACKET 99 12 25 99 99 25 120x45 T SECTION 5no 2900 DOUBLES 5no BRA80/160SFS SINGLES 15no BRA80/85SFS Telling Architectural Ltd 7 The Dell Enterprise Drive Four Ashes Wolverhampton Tel : 01902 797 700 WV10 7DF Fax : 01902 797 720 416 1200 1200 600 600 384 Telling Architectural Ltd Do not scale from this drawing. If in doubt ask Drawing Title : DImension DImension T / STUD RELATIONSHIP PLAN A-A 4400 Steel VINCI TEST PANEL TELLING ARCHITECTURAL VERTICAL T AND BRACKET LAYOUT Scale : Drawn : 1 : 25 Date : psk 07.11.13 Size A3 Drawing No. GF-012 Rev. C

ALL ELEVATIONS ARE VIEWED FROM OUTSIDE UNLESS OTHERWISE STATED CONTRACT NUMBER : TILE SYSTEM : MODULE SIZE : COLOUR : SPECIFICATION TP 54 4292 54 25 160 Horizontal Rails 254 X 254 X 107 UC 25 160 Horizontal Rails 635 635 159 63 644 659 206 3000 63 644 659 206 99 206 251 79 127 508 159 A A 254 X 254 X 107 UC 54 1390 120 1390 1392 54 1510 2902 1510 254 X 254 X 107 UC 3000 Steel 99 206 251 206 508 159 63 644 659 206 3000 254 X 254 X 107 UC C 29.01.14 Single panel added B 19.12.13 Dims updated. TEST ISSUE A 7.11.13 Initial Issue 25 170 SECTION B-B ELEVATION B B C C 25 170 SECTION C-C Rev. Date Comments Drawing Status : Contract : 3 60 70 Clip 38 RAIL SETOUT Dimension 63 Dimension 25 160 54 PLAN A-A 4292 4400 Steel 54 6803 HORIZONTAL RAILS 5no 4292 4no 1510 1no 2902 GRANITI FIANDRE 6mm PORCELAIN PANELS TAL SYSTEM VINCI TEST PANEL Telling Architectural Ltd 7 The Dell Enterprise Drive Four Ashes Wolverhampton Tel : 01902 797 700 WV10 7DF Fax : 01902 797 720 Drawing Title : Scale : Drawn : Size Do not scale from this drawing. If in doubt ask Drawing No. Telling Architectural Ltd VINCI TEST PANEL TELLING ARCHITECTURAL HORIZONTAL RAIL LAYOUT 1 : 25 A3 Date : GF-013 psk 07.11.13 Rev. C

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