>> endobj >> /P 140 0 R >> /S /GoToR The completed assembly, with vacuum still applied, is placed inside an oven with good air circulation, and the composite is produced after a relatively short cycle cure. >> Puncture damage 4. endobj Laminate Splitting Both skins may be damaged. /A << >> /A << /Subtype /Widget /Ff 65536 /A <<
What is damaged, where it is damaged, and how large is the damage are all criterion manufacturers use when providing standard repair data in their publications. >> /AP << >> /Rect [0 770 120 790] << /D [0 /XYZ null null null] >> >> /F (51_toc.pdf) /N 118 0 R /P 136 0 R endobj >> endobj
/Ff 65536 endobj >> >> >> SERVICE MANUAL EXTRA 200 PAGE DATE: 1. /D [0 /XYZ null null null] /Ff 65536
/AP << >> /D [0 /XYZ null null null] /T (B000129) /Dest [241 0 R /XYZ null null null] /Type /Annot /A << /T (B000028) >> /Dest [215 0 R /XYZ null null null] endobj /Ff 65536 /Rect [240 770 360 790] /A << /AP << /P 205 0 R A pre-cured doubler is a sheet of composite material made from layers of fibre reinforced epoxy which has been cured in using heat and pressure. /FT /Btn /F (51_toc.pdf) /Ff 65536 /Subtype /Widget /FT /Btn /Ff 65536 endobj >> /Type /Annot /Rect [120 770 240 790] >> /S /GoToR endobj >> /P 186 0 R << endobj /Type /Annot 176 0 obj
/F (51_toc.pdf)
/Subtype /Widget PRI is considering being the entity to which written and practical exam results for the CRT would be sent for review and would issue the CRT certification. /AP << 170 0 obj <<
<< /AP << << /F (../GIV_SRM.pdf) /T (B000091) /Type /Annot >> endobj An adapted laser and optical machining system were designed to be portable and mountable onto aircraft surfaces even in the field, enabling fully automated composite repairs with greater quality and reliability. Puncture Damage in a Sandwich Structure The damage does not extend through the full length of the part. >> While it may be necessary to remove paint for assessment purposes, you will now need to remove enough paint to accommodate the repair. /D [0 /XYZ null null null]
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/Type /Annot 2). >> 200 0 obj /S /GoToR << /P 231 0 R /Rect [360 770 480 790] /Type /Annot
/Rect [360 770 480 790] >> /T (B000105) /T (B000031) /Type /Annot /P 201 0 R /Rect [240 770 360 790] /Dest [236 0 R /XYZ null null null] /Type /Annot >> /FT /Btn /Rect [240 770 360 790] /Ff 65536 /Type /Annot /Type /Annot /P 240 0 R /Rect [360 770 480 790] /Ff 65536 289 0 obj /Dest [265 0 R /XYZ null null null] 159 0 obj
<<
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/T (B000007) 282 0 obj The repaired structure would be shipped to an independent test lab for both NDI and destructive testing to verify the repair bond’s strength. /FT /Btn /T (B000063) /Type /Annot /Subtype /Widget /P 180 0 R endobj /Type /Annot /Rect [120 770 240 790] To overcome this gap, many OEMs have developed and offer training specific to their types. >>
/Subtype /Widget >> /Subtype /Widget /FT /Btn /T (B000065) /F (51_toc.pdf) /P 205 0 R 146 0 obj >> April 1999 Publication No. /T (B000113) >> >> /S /GoToR /Rect [0 770 120 790] The OEM designers specify which direction the warp fibers must run relative to the structure. /D [0 /XYZ null null null] /FT /Btn endobj /FT /Btn >> /S /GoToR /A << /Subtype /Widget >> /AP << /AP <<
/F (51_toc.pdf) /FT /Btn /N 119 0 R /Ff 65536 >> /Rect [360 770 480 790]
162 0 obj >> >>
>> >> /AP << /T (B000082) /S /GoToR >> /FT /Btn >> >> 238 0 obj Moldex would continue to patch these cars and run them — sometimes as much as 10,000 miles (16,093 km) — until it was no longer worthwhile weight-wise to do so. /F (../GIV_SRM.pdf) /T (B000089) /Subtype /Widget /FT /Btn << << /Type /Annot >> >> /T (B000166) << /AP << endobj /D [0 /XYZ null null null] /FT /Btn 228 0 obj /Type /Annot
endobj 311 0 obj /AP << 182 0 obj /T (B000016) endobj /Subtype /Widget /Subtype /Widget
>> /S /GoToR /P 280 0 R /A << /Subtype /Widget << /FT /Btn /D [0 /XYZ null null null] /Rect [360 770 480 790] /FT /Btn /Rect [120 770 240 790] /S /GoToR /AP << /Ff 65536 The main difference is that composite repair technology most likely represents a new set of skills, processes, and materials to which most technicians have not been exposed. /Rect [360 770 480 790] /Ff 65536 /P 220 0 R >> /Ff 65536
/A << /Ff 65536 /FT /Btn 253 0 obj /S /GoToR >> << /Ff 65536 /AP << B�}�K �1�ѩ>~��Y�z��7�h��Cu,���{�Ou~0���>?^F�A�A��y�M��Y��ھF X�:ԫcn��O��|��Ya��x���:۲�zѰ�1�_�w��G��Yev3�bU�����j(�� ǀX�m�o���>.�V)Y(�?�D����X� �w�EHT�9g�Oh�;�)�=,��,l1m���I�z� z /AP << /T (B000075) This guide aims to give a general approach to composite repair in all applications and will examine both sandwich and laminate structures.