MIL-HDBK-17-3F Volume 3,Index Index Abbreviations Ch1-2,4,8 Acronyms Ch1-10 Adherends. ch6-7,18 Adhesive bonding Ch2-40,50,52,64 Allowable. Ch4-6,16,30 Alumina.. Ch2-8,17,18 Aramid Ch2-6,7,8,12,17,26,27,29,33,34,38,50 Aramid fiber... Ch2-10,17,ch12-5 Autoclave cure....... ch2-53 Bagging... Ch8-44 Barely visible impact damage(BVID) Ch7-3,8,16 Bearing...Ch7-1,49,50,51,53,54,56,57,58,59,60,61,62,63,ch12-6,12,13.15,16,17,18,23,24 Bearing/bypass.......... Ch7-51,58 Bending. Ch6-22,27,30,31,34,35,36,37,38,42,50,52,53,55,56,60,61,64,66,68,70, 76,78,86,88,89,93,94 Beam Ch5-35 Bismaleimide .Ch2-31 Bonding. Ch2-7,27,35,40,49,50,51,52,64,66 Boron 04444044444444444044404044 .Ch2-10,15,17 Boron fiber... Ch2-15,17,Ch5-9 Boron/epoxy.… ..Ch5-10,16 Braiding. .Ch1-15,16,18,21,24,Ch2-9,14,47,48 Buckling.. .Ch6-1,15,17,18,31,61,63,68,70,71,72,73,74,75,76,77,78,79,86,88,89, 92,93,94,114116 Stacking sequence effects... ch6-76 Building block approach........... Ch4-1,3,4,29,34,Ch7-25 Carbon fiber... ch2-2,6 Carbon/epoxy.Ch5-11,12,32,33,35,36,39,54,56,79,81,82,85,88,89,Ch6-5,29,30 31,35,46 Carpet plot Ch5-55,ch12-2,3 Certification.…Ch1 Characteristic damage state...... ch7-65,68,69 Cobonding........... Ch2-51 Commercial Aircraft Composite Repair Committee(CACRC). Ch8-16 Composite cylinder assemblage(CCA)..... Ch5-4,13 Compression after impact.........ch6-68 Computer programs.… Ch5-86,94 Coupon Ch4-35,48,49 Creep....... .Ch6-1,7,89,55,69 Crippling. Ch6-70,71,72,78,79,80,83,84,86,87,88,89,90,91,92,93 Damage.… Ch7-14,20,46,49,50,52,54,56,58,60,61,62,63,69,70,71,99,121,122.135 Ch8-35,48 Damage resistance .Ch7-71 Damage tolerance. Ch7-52,54,58,69,70,71,84,Ch8-1,2,Ch9-3,Ch12-1,4,25 Defects. .Ch7-2,3,816 Definitions Ch1-13,35 Delamination............... Ch5-55,58,59,60,61,62,63,66,70,71,79,92,28,36,60,114,Ch12-4,6, 12,26 1-1MIL-HDBK-17-3F Volume 3, Index I-1 Index Abbreviations ............................................................................................................................... Ch 1-2, 4, 8 Acronyms ........................................................................................................................................... Ch 1-10 Adherends...................................................................................................................................... Ch 6-7, 18 Adhesive bonding ............................................................................................................ Ch 2-40, 50, 52, 64 Allowable.................................................................................................................................. Ch 4-6, 16, 30 Alumina .................................................................................................................................... Ch 2-8, 17, 18 Aramid....................................................................................Ch 2-6, 7, 8, 12, 17, 26, 27, 29, 33, 34, 38, 50 Aramid fiber................................................................................................................... Ch 2-10, 17, Ch 12-5 Autoclave cure ................................................................................................................................... Ch 2-53 Bagging.............................................................................................................................................. Ch 8-44 Barely visible impact damage (BVID) ........................................................................................ Ch 7-3, 8, 16 Bearing... Ch 7-1, 49, 50, 51, 53, 54, 56, 57, 58, 59, 60, 61, 62, 63, Ch 12-6, 12, 13, 15, 16, 17, 18, 23, 24 Bearing/bypass ............................................................................................................................ Ch 7-51, 58 Bending.....................Ch 6-22, 27, 30, 31, 34, 35, 36, 37, 38, 42, 50, 52, 53, 55, 56, 60, 61, 64, 66, 68, 70, 76, 78, 86, 88, 89, 93, 94 Beam ........................................................................................................................................... Ch 5-35 Bismaleimide...................................................................................................................................... Ch 2-31 Bonding..........................................................................................Ch 2-7, 27, 35, 40, 49, 50, 51, 52, 64, 66 Boron ..................................................................................................................................... Ch 2-10, 15, 17 Boron fiber ...................................................................................................................... Ch 2-15, 17, Ch 5-9 Boron/epoxy................................................................................................................................. Ch 5-10, 16 Braiding.......................................................................................Ch 1-15, 16, 18, 21, 24, Ch 2-9, 14, 47, 48 Buckling ......................Ch 6-1, 15, 17, 18, 31, 61, 63, 68, 70, 71, 72, 73, 74, 75, 76, 77, 78, 79, 86, 88, 89, 92, 93, 94, 114, 116 Stacking sequence effects........................................................................................................... Ch 6-76 Building block approach.................................................................................... Ch 4-1, 3, 4, 29, 34, Ch 7-25 Carbon fiber ..................................................................................................................................... Ch 2-2, 6 Carbon/epoxy.......................Ch 5-11, 12, 32, 33, 35, 36, 39, 54, 56, 79, 81, 82, 85, 88, 89, Ch 6-5, 29, 30, 31, 35, 46 Carpet plot ...................................................................................................................... Ch 5-55, Ch 12-2, 3 Certification .......................................................................................................................................... Ch 1-1 Characteristic damage state .................................................................................................. Ch 7-65, 68, 69 Cobonding.......................................................................................................................................... Ch 2-51 Commercial Aircraft Composite Repair Committee (CACRC)........................................................... Ch 8-16 Composite cylinder assemblage (CCA)......................................................................................... Ch 5-4, 13 Compression after impact.................................................................................................................. Ch 6-68 Computer programs..................................................................................................................... Ch 5-86, 94 Coupon .................................................................................................................................. Ch 4-35, 48, 49 Creep ........................................................................................................................... Ch 6-1, 7, 8, 9, 55, 69 Crippling...................................................Ch 6-70, 71, 72, 78, 79, 80, 83, 84, 86, 87, 88, 89, 90, 91, 92, 93 Damage ....................Ch 7-14, 20, 46, 49, 50, 52, 54, 56, 58, 60, 61, 62, 63, 69, 70, 71, 99, 121, 122, 135, Ch 8-35, 48 Damage resistance............................................................................................................................ Ch 7-71 Damage tolerance...................................Ch 7-52, 54, 58, 69, 70, 71, 84, Ch 8-1, 2, Ch 9-3, Ch 12-1, 4, 25 Defects................................................................................................................................... Ch 7-2, 3, 8, 16 Definitions .................................................................................................................................... Ch 1-13, 35 Delamination ......................Ch 5-55, 58, 59, 60, 61, 62, 63, 66, 70, 71, 79, 92, 28, 36, 60, 114, Ch 12-4, 6, 12, 26