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LEGEND <br /> MATCH LINE - DWG 40-26-TNM111-13 <br /> GENERAL NOTES <br /> > QUIC <br /> K-DISCONNECTHANSEN <br /> # E: DIXON 1. COMPRESSED AIR PIPE MATERIAL: BLACK STEEL, <br /> MODEL l i SCHEDULE 40, ASTM A 53, GRADE B WITH <br /> CLASS 150 MALLEABLE IRON THREADED <br /> YAI " FITTINGS ASTM 197/ASTM B16.3 <br /> 2. BALL VALVES: BRONZE BODY, CHROME PLATED <br /> BALL, FULL PORT, REINFORCED PTFE SEATS <br /> AND PACKING, THREADED ENDS, 600 PSI WOG, <br /> WATTS B-6400 OR OTHER APPROVED. <br /> > ❑ a <br /> 3. SELF-EXHAUSTING BALL VALVE: APOLLO <br /> 7K-100-SV OR OTHER APPROVED. <br /> ¢ <br /> ❑ REFERENCE DRAWINGS <br /> 4 (2)1AA QUICK-DI CONNECT COUPLINGS: HANSEN > < (2)1"A I <br /> #1312-H46. SAFETY CHECK VALVE: DIXON (2)112"A <br /> M550 MODEL SC M-12. ❑ <br /> MM 50 <br /> ¢ <br /> - 2H2 2H1 2TI - 1H9 1H8 <br /> a"A A A A a"A A A a 'a a"A A x' a•A A a•n Z B REMOVAL NOTES <br /> J - NS a T7N8 REMOVE COMPRESSED AIR PIPING BACK TO MAIN AND <br /> — CAP. <br /> �1H12' <br /> (2)1"A <br /> o (211 z"A (2)1 i'A J o <br /> I <br /> M`50 M`5�0 ¢ <br /> J�� <br /> 4"A A A A 4A <br /> QUICK-DISONNECT COUPLINGS: HANSEN <br /> #13 H46. SAFETY CHECK VALVE: DIXON > ¢ <br /> = MODEL SCV -12. <br /> a <br /> UGM118 U M503 <br /> 17 <br /> ¢ ❑ D <br /> 1 <br /> D <br /> 2"A 1 B <br /> 1-1/2"A <br /> D <br /> a <br /> z � <br /> D <br /> 112"VALVEWIPLUG a <br /> 112"PLUGGED TEE <br /> 5 7 11 <br /> MATCH LINE - DWG 40-26 1 T <br /> -TNM111-23 A A A A B DG 40 026 T <br /> N <br /> 10 11 12 13 14 0 <br /> N.3 <br /> 15 16 17 18 19 <br /> N. C7 <br /> 20 21 22 23 24 <br /> m <br /> PARTIAL PLAN �vl REMOVAL 25 26 27 28 29 R <br /> SCALE: 1/8"=1'-0" <br /> KEY PLAN BLDG. 40-26 O <br /> SCALE: NONE <br /> PfKusi <br /> ISSUED FOR CONSTRUCTION 8' 4' 0 4' 8' 16, <br /> PROFESSIONAL STAMP & SIGNATURE EERS SCALE: 1/8" <br /> APPLIES TO WORK WITHIN THE CLOUDED Seattle//Spokane//Baltimore DESIGN BY FSI DATE 01.04.24 <br /> REVISION AREAS ONLY AS INDICATED <br /> SYM REVISION BY APPROVED DATE SYM REVISION BY APPROVED DATE ACCEPTABILITY DRAWN DATE SUBTITLE CURRENT REVISION SYMBOL DATE <br /> "qo THIS DESIGN AND/OR oR H K PARTIAL COMPRESSED AIR PLAN-TUNNEL-REMOVAL W8861360 B 01.04.24 <br /> A TOOLING SYSTEMS WBS2523X-RECORD WBS2523X BRPH FSI 09.13.17 hpc ''� SPECIFICATION IS APPROVED SHEET <br /> B 737 NORTH LINE-40-26 WING SYSTEMS INTEGRATION W8861360 FSi KMC 01.04.24BOE/A/G® " APPROVED BY DEPT. I DATE ENGINEER TITLE 737 NORTH LINE - 40-26 WING SYSTEMS INTEGRATION TN M 111 18R <br /> CHECKED <br /> 1NA BUILDING 40-026 JOB NO COMP NO. <br /> fss/oNnl E APPROVED WBS2523X <br /> APPROVED MECHANICAL MASTER COL. N.3-N.7/7-9 EVERETT, WA DWI NO. 40-026-TNM111R <br />