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I" SKYDROL SUPPLY <br /> E <br /> ------------ — ---------------------------r------------------------ <br /> -- ------------------------- ---------------------- ------- <br /> 1 1/4' SKYDROL RETURN I 1= I k I CONSTRUCTION NOTES <br /> 1 N 1 1 1 1 <br /> a a a a a a I CONNECTIONS TO CART SUPPLIED BY BOEING. <br /> r--1— , I <br /> __ I I _ __ I I _ __ I _ __ I CONNECTIONS TO TOOLS AT END OF SWING <br /> ----1L 1 r1l---- , r ----1L 1 r1l---- , ----1L 1 r1l---- , ----1L 1 r1l---- , I ARMS. <br /> 1166 � •�-� bb bb � •�-� bb bb � •�-� bb bb � ;�-� bb <br /> �w GENERAL NOTES <br /> 3/4' TYP. 3/4' TYP. 3/4' TYP. 3/4' TYP. 3/4' TYP. 3/4' TYP. 3/4" TYP. 3/4" TYP. J °' 1. SYSTEM IS DESIGNED TO ASMB B31.3. <br /> 1 0 2. DESIGN PRESSURE = 4000 PSIG <br /> 3. DESIGN TEMPERATURE OF SKYDROL PE-5 <br /> w 1 } g = 150 DEC F. <br /> 3/4"SUPPLY FN " " " " " <br /> 3/4RETUR 3/4SUPPLY 3/4"RETURN 3/4SUPPLY 3/4RETURN 3/4SUPPLY 3/4RETURN I vY 4. REFER TO M608 THRU M611 FOR PIPE <br /> 3/4"RETURN 3/4"SUPPLY 3/4"RETURN 3/4"SUPPLY 3/4"RETURN 3/4"SUPPLY 3/4"RETURN 3/4"SUPPLY Y I MATERIALS. <br /> N I\ I Z <br /> 1 � O <br /> I � K <br /> 1 IO <br /> I <br /> I <br /> I Z <br /> I = <br /> I � <br /> I � <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> I <br /> i <br /> I L <br /> 1" SKYDROL SUPPLY <br /> - -------: ----------------------------] <br /> 1= 1 1/4" SKYDROL RETURN <br /> � T <br /> T <br /> -- --�� <br /> m 3/4" TYP. 3/4" TYP. <br /> a A A <br /> w <br /> 0 3/4"SUPPLY 3/4"RETURN <br /> Q 3/4"RETURN 3/4"SUPPLY <br /> z <br /> of 1" SKYDROL SUPPLY <br /> U E 3 <br /> I------------- 3 <br /> Z-------------- ------- ------- T----------------------- <br /> owl 1= 1= 1 1/4" SKYDROL RETURN <br /> 1 z 1 <br /> a 1� r <br /> bb i •�� � I N bb i ��� <br /> A r <br /> Y A <br /> V. TYP. 3/4" TYP. <br /> I <br /> I <br /> 1 I 1 <br /> 3/4"SUPPLY 3/4"SUPPLY <br /> 3/4"RETURN 3/4"RETURN <br /> I 40-26 FLOOR <br /> I <br /> TUNNELS <br /> HYDRAULICS FLOW DIAGRAM <br /> SCALE: NOT TO SCALE <br /> s� <br /> ISSUED FOR CONSTRUCTION <br /> PROFESSIONAL STAMP & SIGNATURE ENGINEERS <br /> APPLIES TO WORK WITHIN THE CLOUDED Seattle//Spokane//Baltimore DESIGN BY FSi DATE 01.0424 <br /> REVISION AREAS ONLY AS INDICATED <br /> SYM REVISION BY APPROVED DATE SYM REVISION BY APPROVED DATE DRAWN ELITE SUBTITLE CURRENT REVISION SYMBOL DATE <br /> C"o ACCEPTABILITY <br /> BILTR WHeKED 01.04.24 HYDRAULICS FLOW DIAGRAM <br /> q W8861360 O R G 01.04.24 <br /> ORIG 737 NORTH LINE-40-26 WING SYSTEMS INTEGRATION W8861360 `Si KMC 01.04.24 Esv,� KMC 01.04.24 SHEET <br /> �* SPECIFICATION IS APPROVED o <br /> BOE/NG® W • APPROVED BY DEPT. DATE KRL 01.04.24 TITLE 737 NORTH LINE - 40-26 WING SYSTEMS INTEGRATION M 331 <br /> CHECKED <br /> 4 / �`�� APPROVED BUILDING 40-026 JOB N0. COMP N0, p <br /> fss/ONAL ENS\ <br /> APPROVED MECHANICAL MASTER EVERETT, WA DWD No. 40-026-M331 <br />