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LEGEND <br /> U V W X Y Z AA AB <br /> 24'-2" 21'-0" 24'-0" 20'-0" 24'-0" 21'-0" 24'-2" <br /> MATCHLINE — SEE 3563 MATCHLINE — SEE 3564 <br /> TS8x4xY4 TS8x4xV44 TS8x4xY4 TS8x4xY4 TS8x4xY4 — <br /> 0o TS8x4xY4 TS8x4xY4 TS8x4xY TS8x4x4 TS8x4xY4 <br /> N� <br /> � O <br /> U� � <br /> m TS8x4xY4 TS8x4xY4 TS8x4xY4 TS8x4xY4 TS8x4xY o o <br /> N� o <br /> AT 3,-2 TS8x4xY4 TS8x4xY4 TS8x4xY4 TS8x4xY4 TS8x4xY4 <br /> COILS Y COVERI_ m GENERAL NOTES <br /> TS8x4xY4 TS8x4xY TS8x4xY TS8x4xY N TS8x4xY4 <br /> 1. BOS EL. = 83'-0" UON. <br /> N <br /> TRUSS 1 <br /> TS8x4xY4 TS8x4xY4 (BOT CHORD) TS8x4xY4 TS8x4xY4 q 2. SEE S500 THRU S504 FOR BRACED FRAME ELEVATIONS. <br /> �I NOTE: — 3S66 5320 <br /> ELEVATION AS READ TO B B TS8x4xY 3. SEE 5320 THRU 5326 FOR TRUSS ELEVATIONS. <br /> SUPPORT SERVICE TS8x4 Y 3566 5510 TS8x4x/4 3566 5510 TS8x4xY TS8x4xY4 <br /> BRIDGE RUNWAY — 4. SEE ARCH FOR DETAILS OF ATTIC FLOOR PANELS. <br /> 6'-10" 6'-10" SEE MECH AND ELEC FOR EQUIPMENT ATTACHED TO <br /> TS8x4 Ya TS8x4xYa 1 TS8x4 Ya TS8x4xYa TS8x4xY4 " o AND MOUNTED ON THE PANELS. <br /> 3566 5546 <br /> TS8x4xY4 TS8x4xY TS8x4x/4 TS8x4xY4 5. [ ] INDICATES THE NUMBER OF 1 1/8"-A490 BOLTS <br /> TS8x4xY TYP = O SINGLE SHEAR (FvTTHE.CO REQUIRED AT EACH END <br /> 3Y" CONIC OVER 20---" TS8x4xY TS8x4xY 2 TS8x4xY TS8x4xY OF THE MEMBER AT THE CONNECTION. <br /> �, of� D © SUPPLY DIFFUSER MOUNTING PER SHEET 3M16. <br /> � GA COMPOSITE DECK SLIDE CONNECTION <br /> g CONNECTION <br /> _ TS8x4xY TS8x4xY 3 �s �s �s �s YP TS8x4xY4 TS8x4 4 <br /> -3'4'-6" 4' 6" -3' — — — — <br /> TS8x4xY4 TS8x4xY4 TS8x4xY B TS8x4xY4 TS8x4xY4 <br /> G <br /> 3566 S518 <br /> 3566 S546 TS8x4xY TS8x4xY4 TYP D S8x4xYa TS8x4xY4 <br /> REFERENCE DRAWINGS <br /> o TS8x4x/4 TS8x4x/4 TS8x4xY TS8x4x/4 TS8x4xY4 <br /> o N <br /> TS8xQ/4 TS8x4x/4 TS8x4A4 TS8x4x/4 TS8xQ/4 <br /> M <br /> TS8x4x/4 TS8x4xY N TS8x4xY TS8xQ/4 TS8xQ/4 <br /> — W16x89 A36 — — — xBRACE 1D A �A71 SEE A/S500 A A 166@29 3566 S529 3566 S323 3S66 S323 3S66 S323 3S66 S323 3 <br /> INSTALL PRIMARY AIR SU7DIFFUSERR MECH, SEESHEET M578.INSTALL SECONDARY AIR PER MECH, SEESHEET M578.INSTALL FRAMING MEMBEOR DETAIL.VERIFY LOCATIONS WITH <br /> Ai b N <br /> PROPRIETARY NOTICE <br /> THIS DOCUMENT IS CONFIDENTIAL AND PROPRIETARY TO THE <br /> BOEING COMPANY,AND BOTH THE DOCUMENT ITSELF AND THE <br /> INFORMATION CONTAINED IN IT SHALL NOT BE REPRODUCED, io <br /> DISCLOSED,OR USED,IN WHOLE OR IN PART,FOR ANY <br /> PURPOSE WTMOUT THE PRIOR WRITTEN AUTHORIZATION OF <br /> THE BOEING COMPANY. THE FACT THAT THIS DOCUMENT MAY <br /> INCLUDE A COPYRIGHT NOHCE DOES NOT IN ANY WAY AFFECT <br /> THE PROPRIETARY STATUS OF THE DOCUMENT. <br /> 3sss 0 <br /> ADDENDUM J2 - 12.09.2021 ACOFFMAN <br /> ISSUE FOR CONSTRUCTION Ph012nUAve,Suite 4001 Seattle,WA 98101 KEY PLAN <br /> Ph 308.833.07i7 1 la><308.838.01)8 <br /> coXman.cOm <br /> LASING o.Oe.M I,�I,+iworenp. <br /> SYM REVISION BY APPROVED DATE SYM REVISION BY APPROVED DATE DRAW DAIE SUBTITLE CURRENT REVISION SYMBOL DATE <br /> �g4 9,ti HSC E ON AND/R CMAG HECKED 02 ,4 s, HIGH ATTIC&BOTTOM CHORD FRAMING <br /> 16 G41F48 1786915 12.09.21 <br /> MILL ORDER 02/12/91 RECORD DRAWINGS 05/28/93 `ve,V6 SPECIFICATION IS APPROVED EDL SHEET <br /> STRUCTURAL PACKAGE 03/05/91 - CAD CONVERSION 1786915 CEI EO 06.29.20 ® APP OVED BY DEPT. DATE T�pINLLK TITLE 45-004 MISCELLANEOUS SYSTEMS 3S66 <br /> A MILL ORDER REVISION 03/05/91 D 45-004 MISCELLANEOUS SYSTEMS 1786915 CEI EO 12.09.21 BOE/A/G CHECKED <br /> A� <br /> B GENERAL REVISIONS 07/22/91 9091 APPROVED BUILDING 45-004 JOB NO. 905801 COMP NO. <br /> �,r. ♦� i <br /> C CONFORM SET 02/26/92 FssloN i E1112 APPROVED STRUCTURAL MASTER COL. R1-V/4-9 EVERETT, WA DWG NO, 45-004-3566 <br /> 121 <br />