SITEID Subcategory SiteAnnFlow0 Grtr1mgy0 SiteDest Weights Rounded Weight 70005 General Metals 702,750 No I 1.98 2 70009 General Metals 1,483 No I 10.55 11 70019 General Metals 13,000 No I 1 1 70022 General Metals 1,483 No I 1.98 2 70026 General Metals 1,483 No I 10.55 11 70031 General Metals 1,483 No I 1.98 2 70042 General Metals 18,326,490 Yes I 1 1 70050 General Metals 1,483 No I 10.55 11 70052 General Metals 190,250 No I 1.98 2 70056 General Metals 18,326,489 Yes I 1 1 70059 General Metals 13,000 No D 23.87 24 70069 General Metals 190,250 No I 1 1 70072 General Metals 2,439,150 Yes I 1.98 2 70078 General Metals 2,439,150 Yes I 10.55 11 70083 General Metals 2,439,150 Yes I 1.98 2 70089 General Metals 1,483 No I 1.98 2 70098 General Metals 1,483 No I 1.98 2 70108 General Metals 1,483 No D 10.55 11 70110 General Metals 2,439,150 Yes I 1.98 2 70111 General Metals 1,483 No I 1.98 2 70116 General Metals 190,250 No I 10.55 11 70123 Printed Wiring Boards 13,000 No I 1.98 2 70131 General Metals 13,000 No I 1.98 2 70138 NonChromium Anodizer 18,326,490 Yes I 1 1 70139 General Metals 18,326,490 Yes I 1.98 2 70147 General Metals 1,483 No I 1.98 2 70161 General Metals 13,000 No I 10.55 11 70169 General Metals 190,250 No D 1 1 70170 General Metals 1,483 No I 10.55 11 70173 General Metals 13,000 No I 10.55 11 70176 MF Job Shop 2,439,150 Yes I 1.98 2 70198 Printed Wiring Boards 13,000 No I 1.98 2 70206 General Metals 190,250 No I 1.98 2 70212 Railroad Line Maintenance 2,439,150 Yes D 1 1 70217 Oily Only 1,483 No I 1 1 70224 General Metals 1,483 No I 1.98 2 70229 General Metals 18,326,490 Yes I 1 1 70232 MF Job Shop 2,439,150 Yes I 23.87 24 70236 General Metals 13,000 No I 1 1 70237 General Metals 18,326,489 Yes D 1 1 70243 General Metals 702,750 No I 1.98 2 70255 Oily Only 2,439,150 Yes I 1.98 2 70269 General Metals 190,250 No I 10.55 11 70272 General Metals 13,000 No I 1 1 70276 General Metals 18,326,491 Yes I 1.98 2 70277 MF Job Shop 18,326,491 Yes I 1.98 2 70282 General Metals 1,483 No I 1.98 2 70286 MF Job Shop 13,000 No I 10.55 11 70294 General Metals 1,483 No I 23.87 24 70295 General Metals 1,483 No I 10.55 11 70307 General Metals 1,483 No I 23.87 24 70322 General Metals 13,000 No I 1.98 2 70332 General Metals 2,439,150 Yes I 1.98 2 70342 Railroad Line Maintenance 13,000 No I 1.98 2 70356 General Metals 13,000 No I 1.98 2 70365 General Metals 1,483 No I 1.98 2 70382 General Metals 18,326,490 Yes I 1 1 70386 General Metals 1,483 No I 1 1 70392 General Metals 18,326,490 Yes I 1.98 2 70394 General Metals 13,000 No I 1.98 2 70396 MF Job Shop 18,326,490 Yes I 1.98 2 70403 General Metals 13,000 No I 1.98 2 70404 General Metals 1,483 No I 10.55 11 70408 General Metals 13,000 No I 1 1 70414 General Metals 702,750 No I 1 1 70416 General Metals 1,483 No I 10.55 11 70417 General Metals 1,483 No I 1.98 2 70419 General Metals 190,250 No I 1.98 2 70423 General Metals 18,326,490 Yes I 1 1 70426 General Metals 2,439,150 Yes I 1.98 2 70432 General Metals 13,000 No I 1.98 2 70434 General Metals 2,439,150 Yes I 1 1 70437 Printed Wiring Boards 13,000 No D 10.55 11 70443 General Metals 1,483 No I 1.98 2 70448 General Metals 13,000 No I 1.98 2 70449 General Metals 2,439,150 Yes I 1 1 70450 General Metals 1,483 No I 1.98 2 70453 General Metals 1,483 No I 1.98 2 70459 Oily Only 1,483 No I 1 1 70462 General Metals 18,326,489 Yes I 1 1 70468 General Metals 190,250 No I 23.87 24 70470 MF Job Shop 702,750 No I 10.55 11 70471 MF Job Shop 702,750 No I 1.98 2 70476 MF Job Shop 18,326,490 Yes I 1 1 70498 General Metals 1,483 No I 1.98 2 70502 General Metals 2,439,150 Yes I 10.55 11 70512 General Metals 18,326,490 Yes I 1.98 2 70531 MF Job Shop 2,439,150 Yes I 10.55 11 70533 General Metals 1,483 No I 10.55 11 70534 MF Job Shop 18,326,490 Yes I 1.98 2 70541 General Metals 2,439,150 Yes I 1 1 70543 General Metals 190,250 No I 10.55 11 70547 General Metals 190,250 No I 1 1 70564 General Metals 190,250 No I 1.98 2 70582 General Metals 702,750 No I 1.98 2 70585 General Metals 190,250 No I 1 1 70586 General Metals 2,439,150 Yes I 1 1 70598 General Metals 2,439,150 Yes I 1 1 70606 General Metals 2,439,150 Yes D 1 1 70608 General Metals 13,000 No I 1.98 2 70616 General Metals 13,000 No I 10.55 11 70620 Printed Wiring Boards 2,439,150 Yes I 10.55 11 70633 General Metals 18,326,490 Yes D 1.98 2 70636 General Metals 1,483 No I 1.98 2 70638 General Metals 13,000 No I 1 1 70657 General Metals 18,326,490 Yes I 1 1 70669 General Metals 702,750 No I 1 1 70671 General Metals 2,439,150 Yes D 1 1 70673 General Metals 190,250 No I 1 1 70682 General Metals 13,000 No I 10.55 11 70689 MF Job Shop 18,326,489 Yes I 10.55 11 70699 General Metals 190,250 No I 10.55 11 70700 General Metals 2,439,150 Yes I 1.98 2 70702 General Metals 1,483 No I 10.55 11 70706 General Metals 1,483 No I 1.98 2 70717 General Metals 13,000 No I 1.98 2 70725 General Metals 13,000 No I 23.87 24 70731 General Metals 18,326,490 Yes I 1 1 70732 General Metals 13,000 No I 1 1 70733 Oily Only 1,483 No I 10.55 11 70746 General Metals 13,000 No I 1 1 70756 General Metals 2,439,150 Yes I 1.98 2 70757 General Metals 1,483 No I 1.98 2 70764 General Metals 702,750 No I 1 1 70772 General Metals 1,483 No I 23.87 24 70773 General Metals 1,483 No I 23.87 24 70780 General Metals 2,439,150 Yes I 1 1 70784 General Metals 190,250 No I 1.98 2 70799 General Metals 2,439,150 Yes I 1 1 70808 NonChromium Anodizer 18,326,490 Yes I 1.98 2 70811 Railroad Line Maintenance 1,483 No I 1 1 70814 General Metals 13,000 No I 1 1 70820 General Metals 2,439,150 Yes I 1 1 70824 General Metals 2,439,150 Yes I 1 1 70830 General Metals 1,483 No I 23.87 24 70832 General Metals 1,483 No I 23.87 24 70850 General Metals 190,250 No I 1.98 2 70866 General Metals 1,483 No I 1.98 2 70867 General Metals 18,326,490 Yes I 1 1 70878 General Metals 1,483 No I 10.55 11 70882 MF Job Shop 18,326,490 Yes I 10.55 11 70885 General Metals 702,750 No D 1.98 2 70888 General Metals 18,326,490 Yes I 1 1 70890 General Metals 13,000 No D 1.98 2 70891 Oily Only 1,483 No I 1.98 2 70892 General Metals 18,326,490 Yes I 1 1 70898 General Metals 18,326,490 Yes I 1 1 70901 General Metals 190,250 No I 1.98 2 70914 MF Job Shop 2,439,150 Yes I 23.87 24 70925 General Metals 1,483 No I 10.55 11 70932 General Metals 1,483 No D 10.55 11 70936 General Metals 190,250 No I 10.55 11 70937 MF Job Shop 702,750 No I 10.55 11 70943 General Metals 1,483 No I 1.98 2 70946 Oily Only 190,250 No I 10.55 11 70950 General Metals 18,326,490 Yes I 1 1 70961 General Metals 2,439,150 Yes I 1.98 2 70968 General Metals 1,483 No I 1.98 2 70970 General Metals 1,483 No I 23.87 24 70984 General Metals 13,000 No I 1.98 2 71002 General Metals 18,326,490 Yes I 1 1 71006 General Metals 1,483 No I 1.98 2 71007 MF Job Shop 1,483 No I 1 1 71008 General Metals 18,326,490 Yes I 1 1 71018 General Metals 1,483 No I 10.55 11 71023 General Metals 190,250 No I 1 1 71031 General Metals 18,326,490 Yes I 1 1 71032 General Metals 1,483 No I 10.55 11 71035 MF Job Shop 1,483 No D 10.55 11 71039 MF Job Shop 1,483 No I 1.98 2 71047 NonChromium Anodizer 13,000 No I 10.55 11 71050 General Metals 1,483 No I 23.87 24 71054 MF Job Shop 2,439,150 Yes I 1 1 71078 General Metals 190,250 No I 1 1 71090 General Metals 18,326,490 Yes D 1 1 71098 General Metals 1,483 No D 23.87 24 71107 MF Job Shop 13,000 No I 1 1 71108 General Metals 18,326,491 Yes I 1.98 2 71109 General Metals 190,250 No I 1.98 2 71118 General Metals 1,483 No I 23.87 24 71124 General Metals 2,439,150 Yes I 1.98 2 71127 General Metals 13,000 No I 1.98 2 71149 MF Job Shop 190,250 No I 10.55 11 71155 General Metals 190,250 No D 1.98 2 71169 Oily Only 1,483 No I 23.87 24 71211 General Metals 1,483 No I 10.55 11 71215 General Metals 13,000 No I 1 1 71219 General Metals 1,483 No I 10.55 11 71224 General Metals 2,439,150 Yes I 1.98 2 71227 General Metals 13,000 No I 1 1 71231 Railroad Line Maintenance 702,750 No I 1 1 71232 Railroad Line Maintenance 18,326,490 Yes D 1.98 2 71252 General Metals 18,326,489 Yes I 1 1 71265 General Metals 13,000 No I 10.55 11 71273 General Metals 1,483 No I 1.98 2 71275 MF Job Shop 190,250 No I 1 1 71276 General Metals 1,483 No I 23.87 24 71298 General Metals 13,000 No I 23.87 24 71299 General Metals 1,483 No I 1.98 2 71307 General Metals 1,483 No I 10.55 11 71312 General Metals 13,000 No I 1 1 71314 General Metals 13,000 No I 1 1 71320 General Metals 13,000 No I 1 1 71332 General Metals 2,439,150 Yes I 1.98 2 71340 General Metals 190,250 No I 1.98 2 71344 General Metals 18,326,490 Yes I 1 1 71345 General Metals 1,483 No I 10.55 11 71348 General Metals 2,439,150 Yes I 1.98 2 71349 General Metals 1,483 No I 1.98 2 71355 General Metals 190,250 No I 1 1 71362 General Metals 190,250 No D 1 1 71369 General Metals 1,483 No I 1.98 2 71373 MF Job Shop 2,439,150 Yes I 10.55 11 71374 General Metals 13,000 No I 1.98 2 71376 General Metals 1,483 No I 10.55 11 71377 General Metals 13,000 No I 1.98 2 71381 General Metals 13,000 No I 1 1 71384 General Metals 18,326,491 Yes I 1 1 71385 General Metals 190,250 No D 1 1 71389 Oily Only 1,483 No I 23.87 24 71390 NonChromium Anodizer 2,439,150 Yes I 1.98 2 71392 General Metals 18,326,490 Yes I 1 1 71394 NonChromium Anodizer 18,326,491 Yes I 1.98 2 71398 Printed Wiring Boards 18,326,490 Yes I 1 1 71399 General Metals 1,483 No I 10.55 11 71400 General Metals 702,750 No I 1.98 2 71402 General Metals 190,250 No I 1 1 71413 General Metals 18,326,490 Yes I 1.98 2 71416 Railroad Line Maintenance 1,483 No D 1 1 71417 General Metals 13,000 No I 1.98 2 71418 General Metals 1,483 No I 1.98 2 71421 MF Job Shop 18,326,489 Yes I 1.98 2 71432 General Metals 2,439,150 Yes I 1 1 71433 General Metals 1,483 No I 10.55 11 71438 General Metals 1,483 No D 23.87 24 71447 General Metals 1,483 No I 10.55 11 71448 MF Job Shop 2,439,150 Yes I 1.98 2 71452 General Metals 13,000 No I 1.98 2 71457 General Metals 13,000 No I 1.98 2 71463 General Metals 13,000 No I 1 1 71472 General Metals 18,326,490 Yes I 1 1 71473 General Metals 2,439,150 Yes I 1.98 2 71474 General Metals 18,326,489 Yes I 1.98 2 71487 General Metals 18,326,490 Yes I 1 1 71495 General Metals 2,439,150 Yes I 1 1 71499 Oily Only 1,483 No I 23.87 24 71500 General Metals 2,439,150 Yes D 1.98 2 71512 General Metals 18,326,490 Yes I 1 1 71519 MF Job Shop 190,250 No I 10.55 11 71531 General Metals 1,483 No I 1.98 2 71533 Oily Only 1,483 No I 10.55 11 71542 General Metals 1,483 No D 10.55 11 71544 General Metals 18,326,490 Yes D 1 1 71551 MF Job Shop 18,326,491 Yes I 10.55 11 71554 General Metals 702,750 No I 1.98 2 71567 General Metals 1,483 No I 1.98 2 71568 General Metals 1,483 No I 1.98 2 71569 General Metals 2,439,150 Yes I 1 1 71576 General Metals 2,439,150 Yes I 1.98 2 71577 General Metals 190,250 No I 1.98 2 71582 General Metals 1,483 No I 23.87 24 71587 General Metals 2,439,150 Yes I 1.98 2 71603 General Metals 1,483 No D 1.98 2 71609 General Metals 1,483 No I 10.55 11 71615 General Metals 13,000 No I 1.98 2 71618 General Metals 13,000 No I 1 1 71620 General Metals 1,483 No I 23.87 24 71630 NonChromium Anodizer 13,000 No D 1.98 2 71637 General Metals 1,483 No I 1.98 2 71655 General Metals 190,250 No D 1 1 71658 General Metals 18,326,490 Yes I 1 1 71663 General Metals 13,000 No I 23.87 24 71667 Oily Only 1,483 No I 23.87 24 71670 General Metals 702,750 No I 10.55 11 71678 MF Job Shop 190,250 No D 1.98 2 71683 General Metals 1,483 No I 23.87 24 71687 General Metals 1,483 No I 10.55 11 71703 General Metals 1,483 No I 10.55 11 71710 General Metals 18,326,490 Yes I 1 1 71714 General Metals 1,483 No I 10.55 11 71718 General Metals 1,483 No I 1.98 2 71726 General Metals 2,439,150 Yes I 1 1 71743 General Metals 1,483 No I 1 1 71752 General Metals 1,483 No I 1.98 2 71760 General Metals 1,483 No I 1.98 2 71771 General Metals 13,000 No I 10.55 11 71775 General Metals 702,750 No I 1.98 2 71782 General Metals 2,439,150 Yes I 1.98 2 71792 MF Job Shop 18,326,489 Yes I 1 1 71807 General Metals 1,483 No I 10.55 11 71808 General Metals 1,483 No I 10.55 11 71812 General Metals 1,483 No I 1.98 2 71815 General Metals 1,483 No I 10.55 11 71820 General Metals 13,000 No I 10.55 11 71825 MF Job Shop 13,000 No I 10.55 11 71831 General Metals 13,000 No I 1.98 2 71833 General Metals 13,000 No I 10.55 11 71836 General Metals 190,250 No I 1 1 71840 General Metals 2,439,150 Yes I 1 1 71842 MF Job Shop 18,326,491 Yes I 10.55 11 71844 General Metals 1,483 No I 1.98 2 71851 General Metals 13,000 No I 1 1 71854 General Metals 2,439,150 Yes I 1.98 2 71858 General Metals 2,439,150 Yes D 1 1 71862 General Metals 2,439,150 Yes I 1.98 2 71865 General Metals 18,326,490 Yes I 1 1 71868 General Metals 1,483 No I 10.55 11 71878 General Metals 190,250 No D 1 1 71883 General Metals 2,439,150 Yes I 1.98 2 71892 General Metals 702,750 No I 1.98 2 71897 General Metals 1,483 No I 1.98 2 71906 General Metals 1,483 No I 10.55 11 71912 General Metals 13,000 No I 1 1 71915 MF Job Shop 1,483 No I 10.55 11 71918 General Metals 1,483 No I 23.87 24 71925 General Metals 2,439,150 Yes I 1.98 2 71932 General Metals 1,483 No I 10.55 11 71946 General Metals 1,483 No I 23.87 24 71952 General Metals 2,439,150 Yes I 1.98 2 71959 General Metals 13,000 No I 10.55 11 71987 General Metals 2,439,150 Yes I 1 1 71992 Oily Only 1,483 No I 10.55 11 71999 General Metals 190,250 No I 1.98 2 72011 General Metals 2,439,150 Yes I 1.98 2 72030 General Metals 13,000 No I 1 1 72043 General Metals 1,483 No I 1.98 2 72048 General Metals 2,439,150 Yes I 1 1 72049 General Metals 1,483 No I 1.98 2 72050 General Metals 702,750 No I 1.98 2 72067 General Metals 13,000 No I 1 1 72078 MF Job Shop 18,326,491 Yes I 10.55 11 72080 General Metals 1,483 No I 10.55 11 72081 General Metals 18,326,490 Yes I 1 1 72086 MF Job Shop 1,483 No I 10.55 11 72096 NonChromium Anodizer 2,439,150 Yes I 1.98 2 72097 General Metals 13,000 No I 23.87 24 72101 General Metals 18,326,490 Yes I 1.98 2 72121 General Metals 1,483 No I 10.55 11 72122 General Metals 1,483 No I 10.55 11 72125 General Metals 190,250 No I 1.98 2 72134 General Metals 1,483 No D 10.55 11 72137 General Metals 1,483 No I 10.55 11 72139 General Metals 190,250 No I 1.98 2 72141 General Metals 1,483 No I 1.98 2 72149 General Metals 1,483 No I 1.98 2 72154 General Metals 1,483 No I 23.87 24 72177 General Metals 1,483 No I 23.87 24 72178 General Metals 190,250 No I 1.98 2 72191 General Metals 18,326,490 Yes I 1 1 72200 General Metals 1,483 No I 10.55 11 72201 General Metals 1,483 No I 1 1 72203 General Metals 190,250 No I 1.98 2 72211 General Metals 1,483 No I 10.55 11 72214 MF Job Shop 2,439,150 Yes I 1 1 72220 General Metals 1,483 No I 10.55 11 72225 Oily Only 1,483 No I 1.98 2 72253 General Metals 13,000 No I 23.87 24 72267 General Metals 13,000 No I 1.98 2 72283 General Metals 13,000 No I 1.98 2 72308 General Metals 1,483 No I 1.98 2 72355 General Metals 2,439,150 Yes I 1 1 72366 General Metals 190,250 No I 1 1 72372 General Metals 1,483 No I 23.87 24 72374 MF Job Shop 190,250 No I 10.55 11 72378 MF Job Shop 1,483 No I 23.87 24 72389 General Metals 18,326,490 Yes I 1 1 72390 General Metals 1,483 No I 10.55 11 72405 General Metals 190,250 No I 1.98 2 72409 General Metals 13,000 No I 1 1 72418 MF Job Shop 702,750 No I 1.98 2 72419 General Metals 13,000 No I 1 1 72425 General Metals 13,000 No I 1.98 2 72426 MF Job Shop 2,439,150 Yes I 23.87 24 72432 Oily Only 1,483 No I 10.55 11 72446 General Metals 1,483 No I 23.87 24 72460 General Metals 1,483 No I 1 1 72470 General Metals 13,000 No D 1 1 72477 General Metals 702,750 No I 1.98 2 72488 General Metals 1,483 No I 23.87 24 72491 General Metals 13,000 No I 10.55 11 72505 General Metals 13,000 No I 10.55 11 72509 General Metals 702,750 No I 1 1 72510 Railroad Line Maintenance 13,000 No I 1 1 72511 General Metals 702,750 No I 10.55 11 72523 Oily Only 13,000 No I 1.98 2 72525 General Metals 702,750 No I 1 1 72526 General Metals 190,250 No I 1.98 2 72542 General Metals 18,326,490 Yes I 1 1 72550 General Metals 190,250 No I 10.55 11 72555 General Metals 1,483 No I 23.87 24 72556 General Metals 2,439,150 Yes D 1.98 2 72563 MF Job Shop 1,483 No I 1.98 2 72565 General Metals 18,326,490 Yes I 1.98 2 72578 General Metals 2,439,150 Yes I 1 1 72602 General Metals 2,439,150 Yes I 1.98 2 72608 General Metals 13,000 No I 1.98 2 72615 General Metals 1,483 No I 1.98 2 72617 General Metals 190,250 No I 1.98 2 72618 General Metals 2,439,150 Yes I 1.98 2 72627 Printed Wiring Boards 18,326,490 Yes I 1.98 2 72631 Oily Only 2,439,150 Yes I 1.98 2 72636 General Metals 1,483 No D 23.87 24 72649 General Metals 18,326,490 Yes I 1 1 72666 General Metals 2,439,150 Yes I 1.98 2 72667 General Metals 13,000 No I 1.98 2 72669 General Metals 18,326,490 Yes D 1 1 72679 General Metals 13,000 No I 1.98 2 72680 General Metals 1,483 No I 10.55 11 72711 General Metals 190,250 No I 1 1 72713 General Metals 18,326,490 Yes I 1.98 2 72736 General Metals 190,250 No I 1.98 2 72743 General Metals 1,483 No I 1.98 2 72744 General Metals 13,000 No I 1 1 72746 Oily Only 1,483 No I 10.55 11 72751 General Metals 1,483 No I 1.98 2 72763 MF Job Shop 702,750 No I 1.98 2 72781 MF Job Shop 13,000 No D 1 1 72804 General Metals 702,750 No I 1.98 2 72805 General Metals 1,483 No I 1.98 2 72817 General Metals 2,439,150 Yes I 1.98 2 72819 General Metals 1,483 No I 10.55 11 72831 General Metals 2,439,150 Yes I 1.98 2 72858 General Metals 1,483 No I 1 1 72889 General Metals 1,483 No I 10.55 11 72901 General Metals 702,750 No I 1 1 72926 General Metals 1,483 No I 10.55 11 72951 General Metals 1,483 No I 10.55 11 72961 General Metals 1,483 No I 1.98 2 72969 General Metals 2,439,150 Yes I 1 1 72973 General Metals 1,483 No I 23.87 24 72987 General Metals 190,250 No I 1 1 72993 General Metals 1,483 No I 10.55 11 73007 General Metals 1,483 No I 10.55 11 73012 General Metals 2,439,150 Yes I 1 1 73014 General Metals 1,483 No I 23.87 24 73025 General Metals 702,750 No I 10.55 11 73029 General Metals 702,750 No I 1.98 2 73043 General Metals 2,439,150 Yes I 1.98 2 73045 General Metals 190,250 No I 10.55 11 73050 MF Job Shop 2,439,150 Yes I 1.98 2 73055 General Metals 2,439,150 Yes I 1.98 2 73074 Printed Wiring Boards 190,250 No I 23.87 24 73077 General Metals 13,000 No I 1.98 2 73079 General Metals 1,483 No I 10.55 11 73084 General Metals 18,326,490 Yes I 1 1 73089 General Metals 702,750 No I 1 1 73098 General Metals 18,326,490 Yes I 1.98 2 73103 General Metals 702,750 No I 23.87 24 73107 General Metals 1,483 No I 10.55 11 73113 General Metals 1,483 No I 10.55 11 73114 General Metals 1,483 No I 10.55 11 73141 General Metals 2,439,150 Yes D 1 1 73170 General Metals 190,250 No I 1.98 2 73178 General Metals 1,483 No I 23.87 24 73185 General Metals 13,000 No I 1 1 73186 General Metals 1,483 No I 1.98 2 73207 General Metals 1,483 No I 10.55 11 73257 General Metals 13,000 No I 1.98 2 73263 General Metals 1,483 No I 1.98 2 73284 General Metals 13,000 No I 1.98 2 73288 General Metals 190,250 No I 1.98 2 73290 General Metals 2,439,150 Yes I 1.98 2 73291 General Metals 1,483 No I 10.55 11 73300 General Metals 1,483 No I 1.98 2 73302 General Metals 1,483 No I 10.55 11 73308 General Metals 2,439,150 Yes I 1 1 73338 MF Job Shop 702,750 No I 23.87 24 73355 General Metals 1,483 No I 23.87 24 73374 General Metals 1,483 No I 1.98 2 73375 General Metals 1,483 No I 10.55 11 73380 General Metals 13,000 No I 10.55 11 73381 General Metals 702,750 No I 1 1 73383 General Metals 1,483 No I 1.98 2 73392 General Metals 190,250 No I 1.98 2 73395 General Metals 1,483 No I 10.55 11 73398 General Metals 1,483 No I 1.98 2 73404 MF Job Shop 1,483 No I 23.87 24 73406 General Metals 702,750 No I 1.98 2 73425 Oily Only 1,483 No I 1.98 2 73429 General Metals 2,439,150 Yes D 1 1 73456 General Metals 1,483 No I 1.98 2 73482 Oily Only 1,483 No I 10.55 11 73497 General Metals 702,750 No I 1.98 2 73516 General Metals 2,439,150 Yes I 1.98 2 73518 General Metals 1,483 No I 10.55 11 73527 General Metals 18,326,489 Yes D 1 1 73541 General Metals 1,483 No I 10.55 11 73563 General Metals 2,439,150 Yes I 1.98 2 73565 General Metals 13,000 No I 10.55 11 73576 General Metals 18,326,490 Yes I 1 1 73605 Printed Wiring Boards 2,439,150 Yes I 1.98 2 73615 General Metals 702,750 No I 1.98 2 73625 General Metals 1,483 No I 1.98 2 73642 General Metals 13,000 No I 1 1 73659 General Metals 13,000 No I 1 1 73691 General Metals 1,483 No I 23.87 24 73696 General Metals 13,000 No I 1 1 73731 General Metals 2,439,150 Yes I 1.98 2 73760 General Metals 1,483 No I 1.98 2 73771 General Metals 702,750 No I 1.98 2 73843 General Metals 18,326,490 Yes I 1 1 73847 General Metals 18,326,490 Yes I 1 1 73848 General Metals 2,439,150 Yes I 1 1 73864 General Metals 2,439,150 Yes I 1 1 73870 MF Job Shop 18,326,490 Yes I 10.55 11 73871 General Metals 1,483 No I 23.87 24 73887 General Metals 1,483 No I 10.55 11 73891 General Metals 18,326,490 Yes I 1 1 73892 General Metals 190,250 No I 1.98 2 73900 General Metals 2,439,150 Yes I 1.98 2 73919 General Metals 18,326,490 Yes I 1 1 73931 General Metals 18,326,490 Yes I 1.98 2 73944 General Metals 13,000 No I 1.98 2 73947 Oily Only 1,483 No I 10.55 11 73956 General Metals 2,439,150 Yes I 10.55 11 73984 MF Job Shop 13,000 No I 10.55 11 73985 General Metals 2,439,150 Yes I 1.98 2 73988 MF Job Shop 18,326,490 Yes I 10.55 11 74000 General Metals 702,750 No I 1.98 2 74006 General Metals 18,326,490 Yes I 1 1 74020 General Metals 13,000 No I 10.55 11 74050 General Metals 1,483 No D 10.55 11 74057 MF Job Shop 2,439,150 Yes I 23.87 24 74087 General Metals 13,000 No I 10.55 11 74117 General Metals 2,439,150 Yes D 1 1 74122 MF Job Shop 13,000 No I 1.98 2 74133 General Metals 18,326,489 Yes D 1 1 74136 General Metals 13,000 No I 10.55 11 74149 General Metals 190,250 No I 1.98 2 74169 General Metals 13,000 No I 10.55 11 74194 General Metals 702,750 No I 1 1 74218 General Metals 190,250 No I 10.55 11 74239 General Metals 1,483 No I 1.98 2 74271 General Metals 1,483 No I 10.55 11 74281 General Metals 1,483 No I 23.87 24 74320 General Metals 1,483 No I 10.55 11 74393 General Metals 13,000 No I 23.87 24 74394 General Metals 1,483 No I 1 1 74442 General Metals 2,439,150 Yes I 10.55 11 74448 General Metals 13,000 No I 1 1 74497 General Metals 1,483 No I 1 1 74528 General Metals 13,000 No I 10.55 11 74586 General Metals 2,439,150 Yes I 1.98 2 74622 General Metals 18,326,490 Yes I 1 1 74736 General Metals 702,750 No I 1.98 2 74872 General Metals 2,439,150 Yes I 1 1 74887 General Metals 13,000 No I 10.55 11 Total Weights 3184.52 3254


Reader’s Guide Quinclorac

CRM: Joy Schnackenbeck

EPA/OPPTS/OPP/SRRD

Reader’s Guide to quinclorac Docket # EPA-HQ-2007-1135

Publication Date: December 19, 2007

EPA has created this document to provide an organizational structure to
the quinclorac docket. The docket index lists the caption entries
sequentially, while this document lists them by subject matter. The
Agency is providing the “Readers Guide” to allow the reader to more
easily access and navigate the various entries contained in the
quinclorac docket.

Federal Register and Docket Organizational Documents:

Docket Entry 1. Federal Register Notice:  Quinclorac Reregistration
Review

Docket Entry 2.  Reader’s Guide to Quinclorac Docket #
EPA-HQ-OPP-2007-1135

Docket Entry 3.  Quinclorac Summary Document Registration Review:
Initial Docket December 19, 2007

Docket Entry 4.  Usage Report in Support of Registration Review for the
herbicide, quinclorac

Docket Entry 5.  Review of Quinclorac Human Health Incident Reports

Docket Entry 6.  Appendix A (Food/Feed & Non-Food/Non-Feed Uses Eligible
for Reregistration)


[Federal Register Volume 76, Number 54 (Monday, March 21, 2011)]
[Notices]
[Pages 15322-15323]
[FR Doc No: 2011-6514]

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DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-2010-E-0400]

Determination of Regulatory Review Period for Purposes of Patent
Extension; VPRIV

AGENCY: Food and Drug Administration, HHS.

ACTION: Notice.

-----------------------------------------------------------------------

SUMMARY: The Food and Drug Administration (FDA) has determined the
regulatory review period for VPRIV and is publishing this notice of
that determination as required by law. FDA has made the determination
because of the submission of an application to the Director of Patents
and Trademarks, Department of Commerce, for the extension of a patent
which claims that human drug product.

ADDRESSES: Submit electronic comments to http://www.regulations.gov.
Submit written petitions along with three copies and written comments
to the Division of Dockets Management (HFA-305), Food and Drug
Administration, 5630 Fishers Lane, rm. 1061, Rockville, MD 20852.

FOR FURTHER INFORMATION CONTACT: Beverly Friedman, Office of Regulatory
Policy, Food and Drug Administration, 10903 New Hampshire Ave., Bldg.
51, rm. 6222, Silver Spring, MD 20993-0002,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The Drug Price Competition and Patent Term
Restoration Act of 1984 (Pub. L. 98-417) and the Generic Animal Drug
and Patent Term Restoration Act (Pub. L. 100-670) generally provide
that a patent may be extended for a period of up to 5 years so long as
the patented item (human drug product, animal drug product, medical
device, food additive, or color additive) was subject to regulatory
review by FDA before the item was marketed. Under these acts, a
product's regulatory review period forms the basis for determining the
amount of extension an applicant may receive.
    A regulatory review period consists of two periods of time: A
testing phase and an approval phase. For human drug products, the
testing phase begins when the exemption to permit the clinical
investigations of the drug becomes effective and runs until the
approval phase begins. The approval phase starts with the initial
submission of an application to market the human drug product and
continues until FDA grants permission to market the drug product.
Although only a portion of a regulatory review period may count toward
the actual amount of extension that the Director of Patents and
Trademarks may award (for example, half the testing phase must be
subtracted as well as any time that may have occurred before the patent
was issued), FDA's determination of the length of a regulatory review
period for a human drug product will include all of the testing phase
and approval phase as specified in 35 U.S.C. 156(g)(1)(B).
    FDA recently approved for marketing the human drug product VPRIV
(velaglucerase alfa). VPRIV is indicated for long-term enzyme
replacement therapy for pediatric and adult patients with type 1
Gaucher Disease. Subsequent to this approval, the Patent and Trademark
Office received a patent term restoration application for VPRIV (U.S.
Patent No. 7,138,262) from Shire Human Genetic Therapies, Inc., and the
Patent and Trademark Office requested FDA's assistance in determining
this patent's eligibility for patent term restoration. In a letter
dated September 30, 2010, FDA advised the Patent and Trademark Office
that this human drug product had undergone a regulatory review period
and that the approval of VPRIV represented the first permitted
commercial marketing or use of the product. Thereafter, the Patent and
Trademark Office requested that FDA determine the product's regulatory
review period.
    FDA has determined that the applicable regulatory review period for
VPRIV is 2,221 days. Of this time, 2,041 days occurred during the
testing phase of the regulatory review period, while 180 days occurred
during the approval phase. These periods of time were derived from the
following dates:
    1. The date an exemption under section 505(i) of the Federal Food,
Drug, and Cosmetic Act (the FD&C Act) (21 U.S.C. 355(i)) became
effective: January 30, 2004. The applicant claims May 20, 2004, as the
date the investigational new drug application (IND) became effective.
However, FDA records indicate that the IND effective date was January
30, 2004, which was 30 days after FDA receipt of the IND.
    2. The date the application was initially submitted with respect to
the human drug product under section 505(b) of the FD&C Act: August 31,
2009. FDA has verified the applicant's claim that the new drug
application (NDA) for VPRIV (NDA 22-575) was initially submitted on
August 31, 2009.
    3. The date the application was approved: February 26, 2010. FDA
has verified the applicant's claim that NDA 22-575 was approved on
February 26, 2010.
    This determination of the regulatory review period establishes the
maximum potential length of a patent extension. However, the U.S.
Patent and Trademark Office applies several statutory limitations in
its calculations of the actual period for patent extension. In its
application for patent extension, this applicant seeks 687 days of
patent term extension.
    Anyone with knowledge that any of the dates as published are
incorrect may submit to the Division of Dockets Management (see
ADDRESSES) either electronic or written comments and ask for a
redetermination by May 20, 2011. Furthermore, any interested person may
petition FDA for a determination regarding whether the applicant for
extension acted with due diligence during the regulatory review period
by September 19, 2011. To meet its burden, the petition must contain
sufficient facts to merit an FDA investigation. (See H. Rept. 857, part
1, 98th Cong., 2d sess., pp. 41-42, 1984.) Petitions should be in the
format specified in 21 CFR 10.30.

    Interested persons may submit to the Division of Dockets Management
(see ADDRESSES) electronic or written comments and written petitions.
It is only necessary to send one set of comments. It is no longer
necessary to send three copies of mailed comments. However, if you
submit a written petition, you must submit three copies of the
petition. Identify comments with the docket number found in brackets in
the heading of this document.
    Comments and petitions that have not been made publicly available
on http://www.regulations.gov may be viewed in the Division of Dockets
Management between 9 a.m. and 4 p.m., Monday through Friday.

    Dated: February 14, 2011.
Jane A. Axelrad,
Associate Director for Policy, Center for Drug Evaluation and Research.
[FR Doc. 2011-6514 Filed 3-18-11; 8:45 am]
BILLING CODE 4160-01-P


[Federal Register Volume 77, Number 93 (Monday, May 14, 2012)]
[Notices]
[Pages 28371-28372]
[FR Doc No: 2012-11570]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Project No. 13590-001]

Lockhart Power Company, Inc.; Notice of Application Accepted for
Filing and Soliciting Motions To Intervene and Protests

    Take notice that the following hydroelectric application has been
filed with the Commission and is available for public inspection.
    a. Type of Application: Subsequent Minor License.
    b. Project No.: 13590-001.
    c. Date filed: August 31, 2010.
    d. Applicant: Lockhart Power Company, Inc.
    e. Name of Project: Riverdale Hydroelectric Project.
    f. Location: On the Enoree River, near Enoree, in Spartanburg and
Laurens counties, South Carolina. The proposed project would not affect
any Federal lands.
    g. Filed Pursuant to: Federal Power Act, 16 U.S.C. 791(a)-825(r).
    h. Applicant Contact: Bryan D. Stone, Chief Operating Officer,
Lockhart Power Company, Inc., 420 River Street, P.O. Box 10, Lockhart,
SC 29364;<PHONE_NUMBER>.
    i. FERC Contact: Sarah Florentino at<PHONE_NUMBER>, or via email
at<EMAIL_ADDRESS>    j. Deadline for filing motions to intervene and protests: 60 days
from the issuance date of this notice.
    All documents may be filed electronically via the Internet. See 18
CFR 385.2001(a)(1)(iii) and the instructions on the Commission's Web
site http://www.ferc.gov/docs-filing/efiling.asp. Commenters can submit
brief comments up to 6,000 characters, without prior registration,
using the eComment system at http://www.ferc.gov/docs-filing/ecomment.asp. You must include your name and contact information at the
end of your comments. For assistance, please contact FERC Online
Support at<EMAIL_ADDRESS>or toll free at 1-866-208-3676,
or for TTY,<PHONE_NUMBER>. Although the Commission strongly encourages
electronic filing, documents may also be paper-filed. To paper-file,
mail an original and seven copies to: Kimberly D. Bose, Secretary,
Federal Energy Regulatory Commission, 888 First Street NE., Washington,
DC 20426.
    The Commission's Rules of Practice require all intervenors filing
documents with the Commission to serve a copy of that document on each
person on the official service list for the project. Further, if an
intervenor files comments or documents with the Commission relating to
the merits of an issue that may affect the responsibilities of a
particular resource agency, they must also serve a copy of the document
on that resource agency.
    k. This application has been accepted, but is not ready for
environmental analysis at this time.
    l. The existing, currently non-operational, Riverdale Project
consists

of: (1) A 12-foot high, 425-foot-long concrete gravity dam with 2-foot
flashboards; (2) a 6.6-acre impoundment; (3) a headrace leading to a
110-foot-long steel penstock; (4) a powerhouse containing a single
1.24-megawatt turbine-generator unit; (5) a 510-foot-long tailrace
channel; and (6) appurtenant facilities. The proposed project would
generate about 5,318 megawatt-hours annually. Lockhart Power Company,
Inc. proposes to repair or upgrade the turbine unit and return the
project operation.
    m. A copy of the application is available for review at the
Commission in the Public Reference Room or may be viewed on the
Commission's Web site at http://www.ferc.gov, using the ``eLibrary''
link. Enter the docket number, excluding the last three digits in the
docket number field to access the document. For assistance, contact
FERC Online Support. A copy is also available for inspection and
reproduction at the address in item h above.
    You may also register online at http://www.ferc.gov/docs-filing/esubscription.asp to be notified via email of new filings and issuances
related to this or other pending projects. For assistance, contact FERC
Online Support.
    n. Anyone may submit a protest or a motion to intervene in
accordance with the requirements of Rules of Practice and Procedure, 18
CFR 385.210, 385.211, and 385.214. In determining the appropriate
action to take, the Commission will consider all protests filed, but
only those who file a motion to intervene in accordance with the
Commission's Rules may become a party to the proceeding. Any protests
or motions to intervene must be received on, or before, the specified
deadline date for the particular application.
    All filings must: (1) Bear in all capital letters the title
``PROTEST'' or ``MOTION TO INTERVENE;'' (2) set forth in the heading
the name of the applicant and the project number of the application to
which the filing responds; (3) furnish the name, address, and telephone
number of the person protesting or intervening; and (4) otherwise
comply with the requirements of 18 CFR 385.2001 through 385.2005.
Agencies may obtain copies of the application directly from the
applicant. A copy of any protest or motion to intervene must be served
upon each representative of the applicant specified in the particular
application.
    o. Procedural schedule and final amendments: The application will
be processed according to the following Hydro Licensing Schedule.
Revisions to the schedule will be made as appropriate.

------------------------------------------------------------------------

------------------------------------------------------------------------
Issue Scoping Document 2 (if necessary)...  May 2012.
Notice of application is ready for          July 2012.
 environmental analysis.
Notice of the availability of the EA......  April 2013.
------------------------------------------------------------------------

    Final amendments to the application must be filed with the
Commission no later than 30 days from the issuance date of the notice
of ready for environmental analysis.

    Dated: May 7, 2012.
Kimberly D. Bose,
Secretary.
[FR Doc. 2012-11570 Filed 5-11-12; 8:45 am]
BILLING CODE 6717-01-P


[Federal Register Volume 81, Number 103 (Friday, May 27, 2016)]
[Proposed Rules]
[Pages 33612-33617]
[FR Doc No: 2016-12353]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2013-0797; Directorate Identifier 2013-NM-007-AD]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Supplemental notice of proposed rulemaking (NPRM); reopening of
comment period.

-----------------------------------------------------------------------

SUMMARY: We are revising an earlier proposed airworthiness directive
(AD) for certain The Boeing Company Model 767-300 and 767-300F series
airplanes. The NPRM proposed to require modification and installation
of components in the main equipment center. For certain other
airplanes, the NPRM proposed to require modification, replacement, and
installation of flight deck air relief system (FDARS) components. The
NPRM was prompted by reports of malfunctions in the flight deck display
units, which resulted in blanking, blurring, or loss of color on the
display. This action revises the NPRM by revising the applicability;
adding certain modifications; and clarifying certain requirements. We
are proposing this supplemental NPRM (SNPRM) to prevent malfunctions of
the flight deck display units, which could affect the ability of the
flightcrew to read the displays for airplane attitude, altitude, or
airspeed, and consequently reduce the ability of the flightcrew to
maintain control of the airplane. Since these actions impose an
additional burden over that proposed in the NPRM, we are reopening the
comment period to allow the public the chance to comment on these
proposed changes.

DATES: We must receive comments on this SNPRM by July 11, 2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
    For service information identified in this SNPRM, contact Boeing
Commercial Airplanes, Attention: Data & Services Management, P.O. Box
3707, MC 2H-65, Seattle, WA 98124-2207; telephone:<PHONE_NUMBER>,
extension 1; fax:<PHONE_NUMBER>; Internet https://www.myboeingfleet.com.
You may view this referenced service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call<PHONE_NUMBER>. It
is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2013-0797.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2013-
0797; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this proposed AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (phone:<PHONE_NUMBER>) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Francis Smith, Aerospace Engineer,
Cabin Safety and Environmental Controls Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-
3356; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2013-0797;
Directorate Identifier 2013-NM-007-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

    We issued an NPRM to amend 14 CFR part 39 by adding an AD that
would apply to certain The Boeing Company Model 767-300 and 767-300F
series airplanes. The NPRM published in the Federal Register on
September 25, 2013 (78 FR 58970) (``the NPRM''). The NPRM proposed to
require modification and installation of components in the main
equipment center. For certain other airplanes, the NPRM proposed to
require modification, replacement, and installation of FDARS
components.

Actions Since the NPRM Was Issued

    Since we issued the NPRM, we have reviewed Boeing Alert Service
Bulletin 767-21A0245, Revision 2, dated September 27, 2013 (for Model
767-300F series airplanes). We referred to Boeing Alert Service
Bulletin 767-21-0245, Revision 1, dated September 30, 2010, as an
appropriate source of service information for accomplishing certain
actions specified in the NPRM. Boeing Alert Service Bulletin 767-
21A0245, Revision 2, dated September 27, 2013, adds instructions for
modifications to reduce noise in the flight compartment when the 3-way
valve is operating by removing flex ducts that connect the center and
aft parts of the air distribution diffuser in the main deck cargo
compartment, installing caps and an orifice assembly in the area
forward of the main equipment center and under the flight deck floor,
and installing an FDARS. Boeing Alert Service Bulletin 767-21A0245,
Revision 2, dated September 27, 2013, also identifies concurrent
actions (relay installation and related wiring changes). Those
concurrent actions are described in Boeing Service Bulletin 767-21-
0235, dated October 8, 2009; and Boeing Service Bulletin 767-21-0235,
Revision 1, dated July 29, 2011.
    We have also reviewed Boeing Alert Service Bulletin 767-21A0247,
Revision 1, dated April 9, 2013 (for Model 767-300F series airplanes).
We referred to Boeing Alert Service Bulletin 767-21A0247, dated October
10, 2011, as an appropriate source of service information for
accomplishing certain actions specified in the NPRM. Boeing Alert
Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013, adds
airplanes to the effectivity of the service bulletin and includes
procedures for

changes to the 3-way valve control logic, modifications to reduce noise
in the flight compartment and main cargo air distribution system
(MCADS), and installation of an FDARS. The service bulletin also adds
concurrent actions (relay installation and related wiring changes) for
a certain group of airplanes. Those concurrent actions are described in
Boeing Service Bulletin 767-21-0235, dated October 8, 2009; and Boeing
Service Bulletin 767-21-0235, Revision 1, dated July 29, 2011.
    We also have reviewed Boeing Service Bulletin 767-31-0073, dated
October 12, 1995, which is referred to as concurrent service
information in Boeing Service Bulletin 767-21-0244, Revision 1, dated
March 8, 2010 (which is referred to as an appropriate source of service
information for changing the 3-way valve control logic and installing a
cooling system for the flight deck display equipment). Boeing Service
Bulletin 767-31-0073, dated October 12, 1995, describes procedures for
installation of an in-flight engine indication and crew alerting system
(EICAS) for the maintenance data selection system.
    We have revised paragraphs (c)(2), (h)(1), and (j) of this proposed
AD to refer to Boeing Alert Service Bulletin 767-21A0245, Revision 2,
dated September 27, 2013. We have also revised paragraphs (c)(3) and
(h)(2) of this proposed AD to refer to Boeing Alert Service Bulletin
767-21A0247, Revision 1, dated April 9, 2013.
    In addition, we removed paragraph (k) of the proposed AD (in the
NPRM), ``Credit for Previous Actions,'' from this proposed AD because
operators that have accomplished the actions in Boeing Service Bulletin
767-21-0245, dated April 16, 2010; or Boeing Alert Service Bulletin
767-21A0245, Revision 1, dated September 30, 2010; must do additional
work when accomplishing the procedures specified in Boeing Alert
Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013. We
have redesignated paragraph (j) of the proposed AD (in the NPRM),
``Concurrent Requirements,'' as paragraph (k)(1) of this proposed AD.
In addition, we have added a new paragraph (k)(2) to this proposed AD
to address the concurrent actions (relay installation and related
wiring changes) identified in Boeing Alert Service Bulletin 767-
21A0247, Revision 1, dated April 9, 2013.
    Also since the issuance of the NPRM, we have reviewed Boeing Alert
Service Bulletin 767-21A0254, dated June 7, 2013 (which was not
referenced in the NPRM). Boeing Alert Service Bulletin 767-21A0254,
dated June 7, 2013, describes procedures for installing the FDARS and
activating the 3-way valve control logic change for certain Model 767-
300F series airplanes. We have redesignated paragraph (g) of the
proposed AD (in the NPRM) as paragraph (g)(1) of this proposed AD, and
added a new paragraph (g)(2) to this proposed AD to require the actions
in Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013.

Comments

    We gave the public the opportunity to comment on the NPRM. The
following presents the comments received on the NPRM and the FAA's
response to each comment.

Request To Clarify the Applicability of the Proposed AD (in the NPRM)

    Boeing requested we state that the proposed AD (in the NPRM) does
not apply to Model 767-300 (passenger) series airplanes. Boeing
explained that the 3-way valve control logic for Model 767-300
(passenger) series airplanes is significantly different from the 3-way
valve control logic for Model 767-300F and Model 767-300BCF (Boeing
Converted Freighter) series airplanes. Boeing indicated that, on Model
767-300 (passenger) series airplanes, pack air (which is a moisture
source on the freighter airplanes) to the flight deck instruments and
equipment is rarely used. Boeing added that Model 767-300 (passenger)
series airplanes only utilize airplane pack air during override and
fuel jettison modes, and there have not been reports of moisture-
related display blanking on these airplanes.
    We find that clarification is necessary. This proposed AD applies
to Model 767-300 and 767-300F series airplanes, as identified in
certain service information. ``Model 767-300 series airplanes'' could
include both passenger and BCF series airplanes. According to the U.S.
type certificate data sheet for Model 767 airplanes, a Model 767-300BCF
series airplane is a Model 767-300 (passenger) series airplane that has
been modified in accordance with specific service information to
operate in a freighter configuration. The service information
identified in the applicability of this proposed AD addresses Model
767-300BCF series airplanes and Model 767-300F series airplanes--not
passenger airplanes. Therefore, this proposed AD does not apply to
Model 767-300 (passenger) series airplanes. We have added this
clarification to paragraphs (c), (i), and (k)(3) of this proposed AD.

Request To Revise the Proposed AD (in the NPRM) To Remove Certain
Service Information References

    Boeing asked that all references to Boeing Service Bulletin 767-21-
0240 be removed from the NPRM, including the applicability statement.
Boeing stated that the intent of this service information is to
incorporate display improvements on Model 767-300BCF series airplanes.
Boeing has confirmed that the actions to prevent display unit blanking
included in Boeing Service Bulletin 767-21-0240 have already been
incorporated on Model 767-300BCF series airplanes during the
conversion, prior to re-delivery.
    Boeing also asked that all references to Boeing Service Bulletin
767-21-0244 be removed from the NPRM, including the applicability
statement. Boeing stated that the intent of this service information is
also to incorporate display improvements on Model 767-300BCF series
airplanes. Boeing has confirmed that the actions to prevent display
unit blanking included in Boeing Service Bulletin 767-21-0244 have
already been incorporated on Model 767-300BCF series airplanes in
advance of this proposed AD.
    Since Boeing Service Bulletin 767-21-0240 has been incorporated on
the affected airplanes during the conversion and prior to re-delivery,
we agree with the commenter's request to remove references to that
service bulletin from this proposed AD. Paragraph (c) of this proposed
AD has been revised to omit Boeing Service Bulletin 767-21-0240,
Revision 1, dated November 12, 2009, from paragraph (c)(1), and
subsequent subparagraphs in paragraph (c) have been redesignated
accordingly.
    However, we do not agree with the commenter's request to remove
references to Boeing Service Bulletin 767-21-0244 from this proposed
AD. The commenter has not submitted documentation to the FAA for
verification that the affected operators of Model 767-300BCF series
airplanes have accomplished the actions to prevent display unit
blanking that are included in Boeing Service Bulletin 767-21-0244,
Revision 1, dated March 8, 2010. Therefore, Boeing Service Bulletin
767-21-0244, Revision 1, dated March 8, 2010, is still referenced in
this proposed AD.
    Paragraph (h)(3) of the proposed AD (in the NPRM) has been omitted
from this proposed AD because it referred to Boeing Service Bulletin
767-21-0240, Revision 1, dated November 12, 2009 (which affects
airplanes on which the service information has been done during the
conversion and prior to re-

delivery), and the airplanes identified in this service information
have been removed from the applicability of this proposed AD, as
explained previously. However, the requirements for the remaining Model
767-300BCF series airplanes (i.e., those subject to accomplishment of
Boeing Service Bulletin 767-21-0244) have been moved from paragraph
(h)(3) of the proposed AD (in the NPRM) to new paragraph (i) of this
proposed AD. Paragraph (k) of this proposed AD, which correlates to
paragraph (j) of the proposed AD (in the NPRM), has been revised to
remove the concurrent requirements for Model 767-300BCF series
airplanes identified in Boeing Service Bulletin 767-21-0240, Revision
1, dated November 12, 2009. The concurrent requirements for Model 767-
300BCF series airplanes identified in Boeing Service Bulletin 767-21-
0244, Revision 1, dated March 8, 2010, are retained in paragraph (k)(3)
of this proposed AD.

Request To Clarify the Requirements of the Proposed AD (in the NPRM)

    Boeing requested that the requirements of the proposed AD for Model
767-300BCF versus Model 767-300F series airplanes be clarified. Boeing
stated that the intended function of the 3-way valve control logic
change is to provide moisture control to mitigate display blanking;
however, the intended function of the FDARS is to mitigate the noise
that resulted from the 3-way valve control logic change, not to control
moisture and mitigate display blanking. Boeing stated that the proposed
3-way valve control logic change and addition of the FDARS should be
required for Model 767-300F series airplanes, and only the 3-way valve
control logic change should be required for Model 767-300BCF series
airplanes.
    We agree to clarify the requirements of this proposed AD. In light
of the commenter's remarks, we revised paragraphs (g)(1) and (g)(2) of
this proposed AD to state that, for Model 767-300F series airplanes,
the required actions include the installation of an FDARS and
activation of or change to the 3-way valve control logic. We also
revised the heading for paragraph (g) of this proposed AD accordingly.
    In addition, we revised paragraphs (h)(1) and (h)(2) of this
proposed AD to state that, for Model 767-300F series airplanes
identified in Boeing Alert Service Bulletin 767-21A0245, Revision 2,
dated September 27, 2013, and Boeing Alert Service Bulletin 767-
21A0247, Revision 1, dated April 9, 2013, respectively, the required
actions include a change of the 3-way valve control logic and MCADS,
and installation of an FDARS. We also revised the heading for paragraph
(h) of this proposed AD accordingly.
    As previously discussed, a new paragraph (i) is included in this
proposed AD. This paragraph specifies that, for Model 767-300BCF series
airplanes, only the installation of the 3-way valve control logic and
flight deck display equipment cooling system is required. The
subsequent paragraphs have been redesignated accordingly.

Request To Revise the Number of Affected Airplanes

    Boeing requested that the number of affected airplanes be changed
from 43 to 58. Boeing stated that based on its current records of
operators, there are 58 Model 767-300F series airplanes of U.S.
registry.
    Based on the number of affected Model 767-300 and 767-300F series
airplanes currently on the U.S. Register, we changed the number of
affected airplanes to 52 in the ``Costs of Compliance'' section of this
SNPRM. We also made additional changes to the ``Costs of Compliance''
section to account for any added requirement of this proposed AD.

Effect of Winglets on Accomplishment of the Proposed Actions

    Aviation Partners Boeing stated that the installation of winglets
per Supplemental Type Certificate (STC) ST01920SE (http://rgl.faa.gov/
Regulatory_and_Guidance_Library/rgstc.nsf/0/
59027f43b9a7486e86257b1d006591ee/$FILE/ST01920SE.pdf) does not affect
the accomplishment of the manufacturer's service instructions.
    We agree with the commenter that STC ST01920SE (http://rgl.faa.gov/
Regulatory_and_Guidance_Library/rgstc.nsf/0/
59027f43b9a7486e86257b1d006591ee/$FILE/ST01920SE.pdf) does not affect
the accomplishment of the manufacturer's service instructions.
Therefore, the installation of STC ST01920SE does not affect the
ability to accomplish the actions required by this AD. We have not
changed this SNPRM in this regard.

Additional Change Made to This Proposed AD

    We incorrectly referred to the original issue date of Boeing
Service Bulletin 767-21-0235 as July 29, 2011, throughout the NPRM. We
have specified the correct date of the original issue of Boeing Service
Bulletin 767-21-0235 as October 8, 2009, in paragraphs (j) and (k) of
this proposed AD.

Related Service Information Under 1 CFR Part 51

    We reviewed the following service information.
     Boeing Alert Service Bulletin 767-21A0245, Revision 2,
dated September 27, 2013. The service information describes procedures
for changing the 3-way valve control logic and MCADS, and installing an
FDARS.
     Boeing Alert Service Bulletin 767-21A0247, Revision 1,
dated April 9, 2013. The service information describes procedures for
changing the 3-way valve control logic and MCADS and installing an
FDARS.
     Boeing Alert Service Bulletin 767-21A0253, dated October
12, 2012. The service information describes procedures for replacing
the existing duct, installing an FDARS, changing the 3-way valve
control logic, and installing a new altitude switch and pitot tube.
     Boeing Alert Service Bulletin 767-21A0254, dated June 7,
2013. The service information describes procedures for replacing the
existing duct with a new duct; installing an FDARS; and activating the
3-way valve control logic.
     Boeing Service Bulletin 767-21-0235, dated October 8,
2009; and Boeing Service Bulletin 767-21-0235, Revision 1, dated July
29, 2011. The service information describes procedures for the relay
installation and related wiring changes.
     Boeing Service Bulletin 767-21-0244, Revision 1, dated
March 8, 2010. The service information describes procedures for
changing the 3-way valve control logic and installing a cooling system
for the flight deck display equipment.
     Boeing Service Bulletin 767-31-0073, dated October 12,
1995. The service information describes procedures for installation of
an in-flight EICAS for the maintenance data selection system.
    This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.

FAA's Determination

    We are proposing this SNPRM because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Certain changes described above expand the scope of the NPRM. As a
result, we have determined that it is necessary to reopen the

comment period to provide additional opportunity for the public to
comment on this SNPRM.

Requirements of This Proposed AD

    This proposed AD would require, depending on airplane model and
configuration, the following actions:
     Replacing the existing duct with a new duct.
     Installing an FDARS.
     Changing or activating the 3-way valve control logic.
     Installing a new altitude switch and pitot tube.
     Changing the 3-way valve control logic and MCADS.
     Installing a flight deck display equipment cooling system.
     Doing a relay installation and related wiring changes.
     Installing an in-flight EICAS for the maintenance data
selection system.
    Refer to the service information described previously for details
on the procedures and compliance times.

Costs of Compliance

    We estimate that this proposed AD affects 52 airplanes of U.S.
registry.
    We estimate the following costs to comply with this proposed AD:

                                                                     Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
                Action                          Labor cost          Parts cost        Cost per product                  Cost on U.S. operators
--------------------------------------------------------------------------------------------------------------------------------------------------------
3-way valve control logic and MCADS     46 work-hours x $85 per        $21,865  $25,775.....................  $1,185,650 (46 airplanes).
 change, and installation of an FDARS    hour = $3,910.
 (Boeing Alert Service Bulletin 767-
 21A0247, Revision 1, dated April 9,
 2013; Groups 2 and 3 airplanes).
3-way valve control logic and MCADS     64 work-hours x $85 per         18,315  23,755......................  47,510 (2 airplanes).
 change, and installation of an FDARS    hour = $5,440.
 (Boeing Alert Service Bulletin 767-
 21A0245, Revision 2, dated September
 27, 2013).
Replacement of the existing duct,       76 work-hours x $85 per         55,663  62,123......................  248,492 (4 airplanes).
 installation of an FDARS, 3-way valve   hour = $6,460.
 control logic change, and
 installation of a new altitude switch
 and pitot tube (Boeing Alert Service
 Bulletin 767-21A0253, dated October
 12, 2012).
3-way valve control logic change and    33 work-hours x $85 per              0  2,805.......................  8,415 (3 airplanes).
 installation of a flight deck display   hour = $2,805.
 equipment cooling system (Boeing
 Service Bulletin 767-21-0244,
 Revision 1, dated March 8, 2010).
Relay installation and related wiring   Up to 10 work-hours x $85   Up to $955  Up to $1,805................  Up to $88,445 (49 airplanes).
 changes (Boeing Service Bulletin 767-   per hour = up to $850.
 21-0235, dated October 8, 2009; or
 Boeing Service Bulletin 767-21-0235,
 Revision 1, dated July 29, 2011).
Installing an in-flight EICAS for the   Up to 13 work-hours......        Up to  Up to $4,640................  Up to $13,920 (3 airplanes).
 maintenance data selection system                                      $3,535
 (Boeing Service Bulletin 767-31-0073,
 dated October 12, 1995).
Replacement of the existing duct,       51 work-hours x $85 per         16,338  20,673......................  (0 airplanes).
 installation of an FDARS and            hour = $4,335.
 activation of 3-way valve control
 logic (Boeing Alert Service Bulletin
 767-21A0254, dated June 7, 2013).
--------------------------------------------------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some of the costs of this proposed
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation Programs''
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed
regulation:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive (AD):

The Boeing Company: Docket No. FAA-2013-0797; Directorate Identifier
2013-NM-007-AD.

(a) Comments Due Date

    We must receive comments by July 11, 2016.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to The Boeing Company Model 767-300 and 767-300F
series airplanes, certificated in any category; as identified in the
service information specified in paragraphs (c)(1) through (c)(5) of
this AD. This AD does not apply to The Boeing Company Model 767-300
(passenger) series airplanes.
    (1) Boeing Service Bulletin 767-21-0244, Revision 1, dated March
8, 2010.
    (2) Boeing Alert Service Bulletin 767-21A0245, Revision 2, dated
September 27, 2013.
    (3) Boeing Alert Service Bulletin 767-21A0247, Revision 1, dated
April 9, 2013.
    (4) Boeing Alert Service Bulletin 767-21A0253, dated October 12,
2012.
    (5) Boeing Alert Service Bulletin 767-21A0254, dated June 7,
2013.

(d) Subject

    Air Transport Association (ATA) of America Code 21, Air
Conditioning.

(e) Unsafe Condition

    This AD was prompted by reports of malfunctions in the flight
deck display units resulting in blanking, blurring, or loss of color
on the display. We are issuing this AD to prevent malfunctions of
the flight deck display units, which could affect the ability of the
flightcrew to read the displays for airplane attitude, altitude, or
airspeed, and consequently reduce the ability of the flightcrew to
maintain control of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified,
unless already done.

(g) Installation of Flight Deck Air Relief System (FDARS), 3-Way Valve
Control Logic Change or Activation, and Additional Actions

    (1) For Model 767-300F series airplanes, as identified in Boeing
Alert Service Bulletin 767-21A0253, dated October 12, 2012: Within
72 months after the effective date of this AD, in the main equipment
center and the area under the left and right sides of the flight
deck floor, replace the existing duct with a new duct; install an
FDARS (including the installation of mounting brackets, ducts,
orifice, outlet valve, and screen); change the 3-way valve control
logic (including modification of the associated wiring and related
actions); and install a new altitude switch and pitot tube; in
accordance with the Accomplishment Instructions of Boeing Alert
Service Bulletin 767-21A0253, dated October 12, 2012.
    (2) For Model 767-300F series airplanes, as identified in Boeing
Alert Service Bulletin 767-21A0254, dated June 7, 2013: Within 72
months after the effective date of this AD, in the main equipment
center and the area under the left and right sides of the flight
deck floor, replace the existing duct with a new duct; install an
FDARS (including the installation of mounting brackets, ducts,
orifice, outlet valve, and screen); and activate the 3-way valve
control logic (including modification of the associated wiring and
related actions); in accordance with the Accomplishment Instructions
of Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013.

(h) Installation of FDARS and a 3-Way Valve Control Logic and Main
Cargo Air Distribution System (MCADS) Change

    (1) For Model 767-300F series airplanes, as identified in Boeing
Alert Service Bulletin 767-21A0245, Revision 2, dated September 27,
2013: Within 72 months after the effective date of this AD, in the
main equipment center and the area under the left and right sides of
the flight deck floor, change the 3-way valve control logic and
MCADS, and install an FDARS, in accordance with the Accomplishment
Instruction of Boeing Alert Service Bulletin 767-21A0245, Revision
2, dated September 27, 2013, except as provided by paragraph (j) of
this AD.
    (2) For Model 767-300F series airplanes, as identified in Boeing
Alert Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013:
Within 72 months after the effective date of this AD, change the 3-
way valve control logic and MCADS and install an FDARS, in
accordance with the Accomplishment Instructions of Boeing Alert
Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013.

(i) Installation of a Flight Deck Display Equipment Cooling System and
a 3-Way Valve Control Logic Change

    For Model 767-300 series airplanes that have been converted by
Boeing to Model 767-300BCF (Boeing Converted Freighter) airplanes,
as identified in Boeing Service Bulletin 767-21-0244, Revision 1,
dated March 8, 2010: Within 72 months after the effective date of
this AD, change the 3-way valve control logic and install a flight
deck display equipment cooling system, in accordance with the
Accomplishment Instructions of Boeing Service Bulletin 767-21-0244,
Revision 1, dated March 8, 2010.

(j) Exception to Paragraph (h)(1) of This AD

    For Model 767-300F series airplanes, as identified in Boeing
Alert Service Bulletin 767-21A0245, Revision 2, dated September 27,
2013: If the 3-way valve control logic change specified in Boeing
Service Bulletin 767-21-0235, dated October 8, 2009; or Revision 1,
dated July 29, 2011; is done prior to or concurrent with the actions
required by paragraph (h)(1) of this AD, operators need to do only
the functional test, FDARS installation, and flex duct change, in
accordance with the Accomplishment Instructions of Boeing Alert
Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013.
Operators do not need to do the other actions specified in the
Accomplishment Instructions of Boeing Alert Service Bulletin 767-
21A0245, Revision 2, dated September 27, 2013, if the actions in the
Accomplishment Instructions of Boeing Service Bulletin 767-21-0235,
dated October 8, 2009; or Revision 1, dated July 29, 2011; are done
concurrently. If the functional test fails, before further flight,
do corrective actions that are approved in accordance with the
procedures specified in paragraph (l) of this AD.

(k) Concurrent Requirements

    (1) For Groups 1 and 3 airplanes, as identified in Boeing Alert
Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013:
Prior to or concurrently with accomplishing the requirements of
paragraph (h)(1) of this AD, do the relay installation and related
wiring changes specified in, and in accordance with, the
Accomplishment Instructions of Boeing Service Bulletin 767-21-0235,
dated October 8, 2009; or Boeing Service Bulletin 767-21-0235,
Revision 1, dated July 29, 2011.
    (2) For Group 1 airplanes, as identified in Boeing Alert Service
Bulletin 767-21A0247, Revision 1, dated April 9, 2013: Prior to or
concurrently with accomplishing the requirements of paragraph (h)(2)
of this AD, do the relay installation and related wiring changes
specified in, and in accordance with, the Accomplishment
Instructions of Boeing Service Bulletin 767-21-0235, dated October
8, 2009; or Boeing Service Bulletin 767-21-0235, Revision 1, dated
July 29, 2011.
    (3) For Model 767-300 series airplanes that have been converted
by Boeing to Model 767-300BCF airplanes, as identified in Boeing
Service Bulletin 767-21-0244, Revision 1, dated March 8, 2010: Prior
to or concurrently with accomplishing the requirements of paragraph
(i) of this AD, do the installation of an in-flight engine
indication and crew alerting system (EICAS) for the maintenance data
selection system specified in, and in accordance with, the
Accomplishment Instructions of Boeing Service Bulletin 767-31-0073,
dated October 12, 1995.

(l) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Seattle Aircraft Certification Office (ACO),
FAA, has the authority to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19. In accordance with 14
CFR 39.19, send your request to your principal inspector or local
Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in paragraph (m)(1) of this AD.
Information may be emailed to<EMAIL_ADDRESS>

    (2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
    (3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle ACO, to make those findings. To be approved, the
repair method, modification deviation, or alteration deviation must
meet the certification basis of the airplane and the approval must
specifically refer to this AD.

(m) Related Information

    (1) For more information about this AD, contact Francis Smith,
Aerospace Engineer, Cabin Safety and Environmental Controls Branch,
ANM-150S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057-
3356; phone:<PHONE_NUMBER>; fax:<PHONE_NUMBER>; email:
<EMAIL_ADDRESS>    (2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone: 206-544-
5000, extension 1; fax:<PHONE_NUMBER>; Internet https://www.myboeingfleet.com. You may review copies of the referenced
service information at the FAA, Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, WA. For information on the availability of
this material at the FAA, call<PHONE_NUMBER>.

    Issued in Renton, Washington, on May 17, 2016.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-12353 Filed 5-26-16; 8:45 am]
 BILLING CODE 4910-13-P