Laserfiche WebLink
B <br />WIRE/CABLE CODE: <br />NOTE: NO CABLE SUBSTITUTIONS WITHOUT APPROVAL FROM <br />EQUIPMENT LEGEND <br />SYMBOL <br />QTY <br />NEW <br />XISOTY <br />EXIST. <br />DESCRIPTION <br />PART NUMBER <br />MFG. <br />FM -FA <br />- <br />1 <br />MAIN FIRE ALARM PNL. ASSY., 40-24 BLDG. <br />XLS (EXIST.) <br />SIEMENS <br />1 SEATRONICS, INC. <br />BOEING INTRANET <br />CONNECTION <br />(EXISTING) <br />CAT-5 <br />CBL. <br />(EXIST.)FF> <br />S <br />A <br />2A BUILDING <br />(EXISTING) EACP <br />A = CAROL WIRE C2534 OR BELDEN 9460, #18 AWG <br />SHEILDED TWISTED PAIR, STRANDED, JACKETED CABLE <br />(.205" OD) TYPE CM. <br />B = BELDEN P/N 3107A (RS485 COMMUNICATION CABLE, 2 <br />TWISTED SHEILDED PAIRS, 22 AWG, 120 OHM <br />SIEMENS <br />BAT <br />1 <br />3 <br />BATTERY ENCLOSURE <br />CABB-BAT-R <br />VCP (a) <br />- <br />3 <br />VESDA CONTROL PANEL ASSY. <br />EXIST. <br />VDU (a) <br />- <br />3 <br />VESDA DETECTOR PNL ASSY. <br />EXIST. <br />VCP (b) <br />1 <br />- <br />VESDA CONTROL PANEL ASSY. <br />SEE DWG 110773-FA351-0 <br />VDU (b) <br />1 <br />- <br />VESDA DETECTOR PNL. ASSY. <br />SEE DWG 110773-FA352-0 <br />3 VICEMFAP <br />VESDA <br />COMS <br />EQUIPMENT <br />4A,26,2H <br />SIEMENS <br />XLS <br />B, VNET CKT. <br />TO 40-25 BLDG. <br />VESDA CONTROL <br />PANEL AT POS. <br />#2, COL L-2 <br />IMPEDANCE) (.356" OD) <br />C = 2-#10 AWG THHN STRANDED, (RED & BLACK) <br />D = 2- 12 AWG THHN STRANDED RED & BLACK <br /># ( ) <br />E CAROL WIRE P/N C2536A #16 AWG SHEILDED TWISTED <br />PAIR, STRANDED, JACKETED CABLE (.307" OD) TYPE CM. <br />F = CABLE TYPE 'SOOW', 12—#16 AWG. CAROL 09612 OR <br />o <br />1 <br />3 <br />HORN/STROBE COMBINATION UNIT <br />MTH-MC-R <br />SIEMENS <br />VPS <br />1 <br />3 <br />VESDA POWER SUPPLY, 24 VDC, 4 AMP <br />AL4000LX <br />ALTRONIX <br />® <br />— <br />— <br />RELAY IN ENCL., POWER SHUTDOWN INTERFACE <br />— <br />SIEMENS <br />M R <br />1 <br />3 <br />ADDRESSABLE FA MONITOR MODULE W/RELAY <br />HTRI—R <br />CJ <br />1 <br />3 <br />VESDA CONNECTOR J—BOX ASSY., 8x8x4 <br />SEE DWG 111009—FA315-0 <br />2A,6 <br />I (EXISTING) <br />120 VAC IN <br />EQUAL (.70" NOM. OD) <br />G = NOT USED <br />VCE <br />— <br />1 <br />VESDA COMMUNICATIONS ENCLOSURE ASSY. <br />SEE DWG 111009—FA302-0 <br />3#10 <br />H = #16 TEEN OR TEN STRANDED <br />E❑ <br />1 <br />3 <br />MANUAL STATION & MTG. BOX <br />GE <br />103-23 & 103-25 <br />COL. J-1.5 <br />EPS <br />1 <br />3 <br />EMERGENCY POWER SHUTDOWN PNL. ASSY. <br />BY BOEING/ELEC. CONTR. <br />2A,26 <br />3 <br />- <br />SMOKE DETECTOR, PHOTOELECTRIC <br />OP921 <br />SIEMENS <br />A, <br />N. CNTRL. <br />M/R <br />M/R <br />EPS-R4 � <br />FA RLY. <br />MONITO <br />MODULE <br />MSHUTDN. <br />FA RLY. <br />MONITO <br />MODULE <br />WR. <br />A, EPS FAULT MONITOR <br />EPS—R3 13 <br />EPS I POSITION <br />A LLPNL EMERG. PWR. <br />SHUTDN. <br />A, EPS FAULT MONITOR <br />2#12, P WER SHUTDN. CNTRL. <br />M/R A R Y / IEPS R6 EPS-R2 <br />MONITOR Al N <br />MODULE PNL POSITION <br />EMERG. PWR. <br />A SHUTDN. B <br />COL. 1-6.5 <br />VESBA 2 VESDA 4 <br />2A,B <br />VESBA 1 VESDA 3 <br />2A,B <br />Vrt VESDA 2 <br />CONTROL PANEL <br />2A <br />CONTROL PANEL <br />2A <br />CONTROL PANEL <br />VESDA <br />VESDA <br />�► <br />J 1 5 V,, ( <br />MANUAL1 13 <br />F STATION <br />VCP a <br />J-1.5 ( <br />F STATION �1 <br />VCP a <br />1-6.5 <br />B VPS i VPS-3 A,2H <br />B VPS1 VPS-3 A,2H <br />B VPS 0 VPS-2 A,2H <br />VESDA POWER <br />VESDA POWER <br />VESDA POWER <br />120 VAC IN <br />SUPPLY <br />120 VAC IN <br />SUPPLY <br />120 VAC IN <br />SUPPLY <br />3/4"C — 2#10,1#10G <br />(VPS) <br />3/4"C — 2#10,1#10G <br />(VPS) <br />3/4"C — 2#10,1#10G <br />(VPS) <br />2#14 <br />2#14 <br />2#14 <br />BATTERY ENCL. <br />BAT ERY ENCL <br />BATTERY ENCL. <br />2A,B,D,E 2A,B,D,E <br />COL. J-1.5 COL. J-1.5 COL. 1/6.5 <br />IN TRENCH CJ <br />BELOW AIRCRAFT VESDA <br />CONNECT. <br />J—BOX <br />_F <br />VESDA UMBILICAL <br />CABLE <br />LOCATE NEAR <br />VESDA SMOKE NOSE of <br />DETECTOR UNIT AIRLPLANE <br />VDU(a) <br />(ON CART) <br />AIR SAMPLING <br />NETWORK HOSE TO <br />AIRPLANE INTERIOR <br />FINAL ASSEMBLY <br />IN TRENCH CJ <br />BELOW AIRCRAFT VESDA <br />CONNECT. <br />J-BOX <br />—F <br />VESDA UMBILICAL <br />CABLE <br />LOCATE NEAR <br />VESDA SMOKE NOSE of <br />DETECTOR UNIT AIRLPLANE <br />VDU(a) <br />(ON CART) <br />�—Z AIR SAMPLING <br />NETWORK HOSE TO <br />AIRPLANE INTERIOR <br />IN TRENCH WEST CJ <br />OF AIRCRAFT VESDA <br />CONNECT. <br />35-7.1 J—BOX <br />$RLY. <br />EPS FAULT MONITOR <br />2#12, POWER SHUTDN. CNTRL. <br />EPS—R1 <br />AIRPLANE <br />EPS POSITION <br />PNL EMERG. PWR. <br />SHUTDN. <br />VESDA 1 <br />2A VESDA CONTROL PANEL 2A VESDA <br />MANUAL VCP(b) F MANUAL <br />LJ STATION J-8.5 STATION <br />A,2H <br />"ERYPEN <br />120 VAC IN <br />3/4"C - 2#10,1#1OG <br />2#14 <br />2A,B,D,L 2A,B,D,E <br />COL. J-8.5 <br />—F <br />VESDA UMBILICAL <br />CABLE <br />LOCATE NEAR <br />VESDA SMOKE NOSE of <br />DETECTOR UNIT AIRLPLANE <br />VDU(o) <br />(ON CART) <br />AIR SAMPLING <br />NETWORK HOSE TO <br />AIRPLANE INTERIOR <br />CJ <br />ON UTILITY RACK VESDA <br />CONNECT. <br />J—BOX <br />FINAL BODY JOIN WING BODY JOIN/ C&IR <br />B V�---PeST16N 1 POSITION 3 B POSITION 2 <br />4024 BLDG. VESDA SYSTEM ONE LINE WIRING DIAGRAM <br />SCALE: NONE <br />_F® <br />VESDA UMBILICAL <br />CABLE <br />LOCATE NEAR <br />VESDA SMOKE NOSE of <br />DETECTOR UNIT AIRLPLANE <br />VDU(b) <br />(ON CART) <br />—� AIR SAMPLING <br />NETWORK HOSE TO <br />AIRPLANE INTERIOR <br />POSITION 1 <br />CONSTRUCTION NOTES CONT.: <br />PROVIDE HORN/STROBE AND PROTECTIVE CAGE ON <br />BOEING PROVIDED VESDA DETECTION CART. <br />® PROVIDE UMBILICAL CABLE WITH ADEQUATE <br />LENGTH AND COMPATIBLE PLUG TO CONNECT THE <br />VESDA DETECTION CART (NEAR AIRPLANE NOSE) <br />TO THE RECEPTACLE ON UTILITY RACK. CABLE IS <br />PROVIDED ATTACHED TO THE VESDA DETECTOR <br />UNIT. (BY SEATRONICS) <br />PROVIDE NEW 777-9 COMPATIBLE AIR SAMPLING <br />HOSE <br />10 INSTALL SMOKE DETECTOR ABOVE FAR OR VCR. <br />11. PROVIDE FINAL TERMINATION, START—UP, SITE <br />VESDA GRAPHICS AND ALARMING MODIFICATIONS, <br />AND TESTING AND COMMISSIONING SERVICES FROM <br />SEATRONICS, INC. <br />LOCATE MONITOR/RELAY MODULE WITHIN 3 FEET <br />OF EPS PNL. MAINTAIN CLASS 1 CKT. SEPARATION <br />FROM FA POWER LTD. CKTS. <br />RE —LABEL EXISTING VESDA POSITION AS SHOWN. <br />14. NEW VESDA SYSTEM EQUIPMENT PROVIDED BY <br />SEATRONICS. EQUIPMENT IS TO BE MOUNTED <br />/INSTALLED BY BOEING ELECTRICAL CONTRACTOR <br />AS REQUIRED. NEW ELECTRICAL RACEWAY AND <br />CONDUCTORS PROVIDED AND INSTALLED BY <br />ELECTRICAL CONTRACTOR, AIRPLANE EMERGENCY <br />POWER SHUTDOWN SYSTEM DESIGN PROVIDED BY <br />BOEING, EQUIPMENT & INSTALLATION BY <br />ELECTRICAL CONTRACTOR. <br />B <br />BJ <br />GENERAL NOTES: <br />1. SEE DWG. 111009-FA201, 40-24 VESDA SYSTEM <br />OVERALL PLAN, FOR EQUIPMENT LOCATIONS. <br />2� SEE DWG. 111009-FA301, 40-24 VESDA SYSTEM <br />MFAP, FOR ASSY. & WIRING DETAILS. <br />3� SEE DWG. 111009-FA302, 40-24 VESDA <br />COMMUNICATIONS ENCLOSURE (VCE), FOR ENCL. <br />ASSY. DIAGRAM & WIRING DETAILS. <br />® SEE DWG. 111009-FA303, 40-24 VESDA CONTROL <br />PANEL WIRING INTERCONNECT DIAGRAM DETAILS AND <br />MOUNTING ELEV. <br />5� SEE DWG. 111009-FA305, 40-24 VESDA CONTROL <br />PANEL WIRING INTERCONNECT DIAGRAM DETAILS AND <br />MOUNTING ELEV. <br />© NOT USED <br />7� NOT USED <br />® BOEING REFERENCE DRAWINGS: <br />40-024-1E273 BUILDING FACP LOCATION <br />40-024-E506-2 VESDA SHUNT TRIP RESET MAP <br />40-024-E506-3 POS. 62 EPS-R62 DETAILS <br />40-024-E506-4 POS. 43 EPS-R+3 DETAILS <br />40-024-E506-5 POS. 24 EPS-R24 DETAILS <br />40-024-E506-6 POS. 1 EPS-R1 DETAILS <br />CONSTRUCTION NOTES: <br />INSTALL VESDA SYSTEM POSITION PANEL <br />(PROVIDED BY BOEING) AT COL. J/8.5. WALK <br />INSTALLATION WITH ENGINEER FOR EXACT PANEL <br />PLACEMENT. INSTALL NEW PANEL AND DEVICE <br />LABELS. PROVIDE ALL ANCILLARY DEVICES AND <br />APPURTENANCES INCLUDING NEW BATTERIES AND <br />POWER SUPPLY TO MAKE SYSTEM FUNCTIONAL, <br />INCLUDING HORN/STROBE AND MANUAL PULL <br />STATION. CONTROL PANEL TO BE LABELED BY A <br />WA L&I APPROVED TESTING LAB/ENGINEERING <br />EVALUATION. <br />PROVIDE DEDICATED 120V EMERGENCY POWER <br />CIRCUIT AND WIRE TO POWER SUPPLY. SEE <br />DRAWING 40-024-1E68 FOR DETAILS. <br />PROVIDE CONDUIT/WIRE BACK TO VESDA COMMS <br />PANEL AT COLUMN J/1.5 FOR SYSTEM INTERFACE. <br />® PROVIDE NEW EPS-R1 PANEL AND WIRE TO <br />VESDA AND 480V POWER AS SHOWN. SEE Ell <br />SERIES FOR SHUNT TRIP WIRING CONNECTIONS <br />AND DRAWING 40-024-E506-6 FOR PANEL <br />WIRING DIAGRAM AND ENCLOSURE DETAILS. <br />INSTALL POSITION PANEL TO CART CONNECTION AS <br />SHOWN. ALL CONDUIT BODIES AND J-BOXES ARE <br />TO BE PAINTED RED. <br />© PROVIDE NEW RED 8X8X4 VESDA CONNECTOR <br />J-BOX ON UTILITY RACK W/ RECEPTACLE (TYP. <br />BAYONET, 12 SOCKET, ITT CANON P/N <br />CB2-24A24SS). LABEL THE J-BOX TO READ: <br />"VESDA SMOKE SYSTEM". SEE DRAWING <br />40-024-1E118 FOR UTILITY RACK LOCATION. <br />111009-FA101-B <br />SYM <br />REVISION <br />BY <br />APPROVED <br />DATE <br />SYM <br />REVISION <br />BY <br />APPROVED <br />DATE <br />SEATRONICS <br />FIRE PROTECTION SERVICES <br />ef PO BOX 1138 <br />AUBURN, WA 08071 <br />zs3-s3s-soso <br />—PROPRIETARY— <br />THIS INFORMATION IS THE <br />PROPERLY OF SEATRONICS, <br />INC AND SHALL NOT BE <br />OLIZED OR DISCLOSED <br />WITH UT WRITTEN <br />pUTITH UT ION FROM <br />SEATRONICS, INC. <br />DRAWN <br />SFATRON <br />DATE <br />05Os 17 <br />SUBTITLE <br />VESDA SYSTEM <br />ONE LINE WIRING DIAGRAM <br />CURRENT REVISION <br />_ <br />SYMBOL <br />B <br />DATE <br />04/14/23 <br />- <br />FACTORY TRANSFORMATION 40-024 777X F/A LRIP - <br />SEATRON <br />5/08/17 <br />CHECKED <br />SHEET <br />FA 101 <br />A <br />AS -BUILT - <br />SEATRON <br />07/19/17 <br />N IN <br />TITLE <br />BOEING 40-24 BLDG. <br />AIRCRAFT FIRE DETECTION SYSTEM <br />— XX—XX EVERETT <br />e <br />767 euiLo encK PRo�. — <br />To <br />0a 1a 23 <br />/ / <br />CHECKED <br />APPROVED <br />JOB NO <br />- <br />DDMP NO. <br />APPROVED <br />DWG No. <br />111009—FA101—B <br />