|
TO 40-21 BLDG. TO 40-21 BLDG.
<br />VCP-2, COL. B-4.5 VCP-3, COL. C-5
<br />40-21 BLDG
<br />40-22 BLDG.
<br />2A,2B�
<br />2A,2B
<br />BOEING INTRANET
<br />2A BUILDING
<br />BOEING INTRANET
<br />JA
<br />CONNECTION
<br />FACP
<br />D CONNECTION
<br />CAT
<br />14 CAT-5
<br />CBL.
<br />CBL.
<br />2A,B
<br />j
<br />MFAP(b)
<br />TO 40-23 BLDG.
<br />MFAP(a)
<br />1VCP-1,
<br />SIEMENS
<br />COL G-1.s
<br />SIEMENS
<br />5
<br />CERBERUS
<br />XLS
<br />PRO MODULAR
<br />2A,B
<br />nni r e
<br />-120 VAC IN
<br />3#10
<br />3�2A,2B
<br />nni n e
<br />BAT
<br />COL. A-7.5
<br />X
<br />BUILDING
<br />FACP
<br />2
<br />4
<br />WIRE/CABLE CODE:
<br />NOTE: NO CABLE SUBSTITUTIONS WITHOUT APPROVAL FROM
<br />SEATRONICS, INC.
<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 />IMPEDANCE) (.356" OD)
<br />C = 2-#10 AWG THHN STRANDED, (RED & BLACK)
<br />D = 2-#12 AWG THHN STRANDED (RED & BLACK)
<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 />EQUAL (.70" NOM. OD)
<br />G = NOT USED
<br />H = #16 TFFN OR TFN STRANDED
<br />SYMBOL
<br />MFAP (D)
<br />MFAP(b)
<br />BAT
<br />VCP (a)
<br />VDU (a)
<br />VCP (b)
<br />VDU (b)
<br />VPS
<br />❑
<br />M R(a)
<br />M R (b)
<br />CJ
<br />VCE
<br />F❑
<br />EPS
<br />-120 VAC IN
<br />3#10
<br />A, EPS FAULT MONITOR - v — — - v v v — EPS�ULT MONITOR — s A, EPS FAULT MONITOR
<br />2#12, POWER SHUTDN. CNTRL. 2#12, POWER SHUTDN. CNTRL. 2#12, POWER SHUTDN. CNTRL 0 2#12, POWER SHUTDN. CNTRL.
<br />M/R( F ET>EPS-R-R3 R EPS-R2 M/R(0) FA RJv.� EP�1 M/R(b) FA RLY./ 4�EPS-R4
<br />M ILTY R
<br />MONITO AIRPLANE RELAY MONITO AIRPLANE A MODUL AIRPLANE
<br />MODULE EPS EPS AIRPLANE MODULE EPS POSITION MODULE EPS POSITION
<br />POSITION POSITION ( PNL. 3 A EMERG. PWR.
<br />PNL EMERG, PWR. PNL EMERG. PWR. M/R(a) FA Rw./ EMERG. PWR. M/R(b) FA RLY. PNL.
<br />A SHUTDN. SHUTDN. MONITOR SHUTDN. MONITOR SHUTDN.
<br />H/S H/S A,2H H/S MODULE A, EPS ACTIVATED MONITOR H/S MODULE
<br />A, EPS ACTIVATED MONITOR
<br />2H VCP-3 2H VCP-2 B TO 40-32 BLDG. COL E-14 2H A VCP-1 2H A VCP-4
<br />2A B VCP-1 (VNET CKT.) 1
<br />VESDA 3 VESDA 2 VESDA 1 VESDA 4
<br />CONTROL PANEL CONTROL PANEL 2A B CONTROL PANEL 2A VESDA CONTROL PANEL 2A VESDA
<br />VCP(a) ❑F VCP(a) ❑F VCP(a) F MANUAL 7 VCP(b) F MANUAL
<br />STATION STATION
<br />VPS-3 A,2H VPS-2 A,2H VPS-1 A,2H VPS-4 A,2H
<br />VESDA POWER VESDA POWER VESDA POWER VESDA POWER
<br />120 VAC IN SUPPLY 120 VAC IN SUPPLY 120 VAC IN SUPPLY 120 VAC IN SUPPLY
<br />3/4"C - 2#10,1#10G (VPS) 3/4"C - 2#10,1#10G (VPS) 3/4"C - 2#10,1#10G (VPs) 3/4"C - 2#10,1#10G (VPS)
<br />2#14 2#14
<br />BATTERY ENCL BATTERY ENCL.
<br />(BAT) (BAT)
<br />5
<br />COL. E-1.5 2A,B,D,E COL. E-3.75 COL. D-3 2A,B,D,E COL. D6.5 2A,B,D,E
<br />IN TRENCH CJ IN TRENCH CJ CJ
<br />BELOW AIRCRAFT VESDA BELOW AIRCRAFT VESDA ON UTILITY RACK VESDA
<br />CONNECT. F CONNECT. NEAR D-6.5 CONNECT. 6
<br />J-BOX VESDA UMBILICAL J-BOX J-BOX
<br />CABLE, HARD WIRED
<br />BOTH ENDS.
<br />F F F
<br />VESDA UMBILICAL VESDA UMBILICAL VESDA UMBILICAL
<br />CABLE CABLE CABLE
<br />OCATE 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 />POSITION 3
<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 />POSITION 2
<br />LOCATE NI
<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 />POSTION 1
<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 4
<br />(EAST SIDE OF 40-22) (EAST SIDE OF 40-22) (WEST SIDE OF 40-22) (WEST SIDE OF 40-22)
<br />4022 BLDG. VESDA SYSTEM ONE LINE WIRING DIAGRAM
<br />EQUIPMENT LEGEND — 40-22 BLDG. AIRCRAFT VESDA SYSTEM
<br />CITY
<br />VEW
<br />OTY
<br />EXIST.
<br />DESCRIPTION
<br />PART NUMBER
<br />MFG.
<br />-
<br />1
<br />MAIN FIRE ALARM PNL. ASSY., 40-22
<br />XLS (EXIST.)
<br />SIEMENS
<br />1
<br />-
<br />MAIN FIRE ALARM PNL ASSY., 40-21/22
<br />CERBERUS PRO MODULAR
<br />SIEMENS
<br />2
<br />1
<br />BATTERY ENCLOSURE
<br />CABB-BAT-R
<br />SIEMENS
<br />1
<br />3
<br />VESDA CONTROL PANEL ASSY.
<br />EXIST.
<br />1
<br />3
<br />VESDA DETECTOR PNL. ASSY.
<br />EXIST.
<br />1
<br />3
<br />VESDA CONTROL PANEL ASSY.
<br />SEE DWG 110773-FA351-0
<br />1
<br />3
<br />VESDA DETECTOR PNL. ASSY.
<br />SEE DWG 110773-FA352-0
<br />1
<br />3
<br />HORN/STROBE COMBINATION UNIT
<br />MTH-MC-R
<br />SIEMENS
<br />1
<br />3
<br />VESDA POWER SUPPLY, 24 VDC, 4 AMP
<br />AL4000LX
<br />ALTRONIX
<br />-
<br />1
<br />RELAY IN ENCL., POWER SHUTDOWN INTERFACE
<br />EXIST.
<br />-
<br />3
<br />ADDRESSABLE FA MONITOR MODULE W/RELAY
<br />HTRI-R
<br />SIEMENS
<br />2
<br />-
<br />ADDRESSABLE FA MONITOR MODULE W/RELAY
<br />XTRI-R
<br />SIEMENS
<br />1
<br />-
<br />VESDA CONNECTOR JUNCTION BOX ASSY.
<br />SEE DWG 111009-FA315-0
<br />1
<br />-
<br />NETWORK COMMUNICATIONS ENCLOSURE
<br />SEE DWG 110773-FA307-0
<br />1
<br />3
<br />MANUAL STATION & MTG. BOX
<br />I GE
<br />103-23 & 103-25
<br />1
<br />3
<br />EMERGENCY POWER SHUTDOWN PNL.
<br />BY BOEING/ELEC. CONTR.
<br />2
<br />-
<br />SMOKE DETECTOR, PHOTOELECTRIC
<br />OP921
<br />I SIEMENS
<br />CONSTRUCTION NOTES CONT.:
<br />GENERAL NOTES
<br />©
<br />PROVIDE NEW RED 8X8X4 VESDA CONNECTOR
<br />1. SEE DWG. 110773-FA121, 40-21 VESDA SYSTEM
<br />J-BOX ON UTILITY RACK W/ RECEPTACLE (TYP.
<br />ONE LINE DRAWING.
<br />BAYONET, 12 SOCKET, ITT CANON P/N
<br />2. SEE DWG. 110773-FA201, 40-22 OVERALL VESDA
<br />CB2-24A24SS). LABEL THE J-BOX TO READ:
<br />SYSTEM PLAN, FOR EQUIPMENT LOCATIONS.
<br />"VESDA SMOKE SYSTEM". SEE DRAWING
<br />3. SEE DWG. 110773-FA221, 40-21 OVERALL VESDA
<br />40-022-1E112 FOR UTILITY RACK LOCATION.
<br />SYSTEM PLAN, FOR EQUIPMENT LOCATIONS.
<br />CART MOUNTED VESDA DETECTOR UNIT ASSEMBLY
<br />® SEE DWG. 110773-FA306, 40-21/22 VESDA
<br />WITH CAGED HORN/STROBE. POSITION NEAR
<br />SYSTEM MFAP, FOR ASSY. & WIRING DETAILS.
<br />AIRPLANE NOSE. PROVIDED BY SEATRONICS.
<br />SEE DWG. 110773-FA307, 40-21/22 VESDA
<br />®
<br />PROVIDE UMBILICAL CABLE WITH ADEQUATE LENGTH
<br />COMMUNICATIONS ENCLOSURE (VOL), FOR ENCL.
<br />AND COMPATIBLE PLUG TO CONNECT THE VESDA
<br />ASSY. DIAGRAM & WIRING DETAILS.
<br />DETECTION CART (NEAR AIRPLANE NOSE) TO THE
<br />© SEE DWG. 110773-FA308, 40-21/22 VESDA
<br />RECEPTACLE ON UTILITY RACK. CABLE IS PROVIDED
<br />CONTROL PANEL WIRING INTERCONNECT DIAGRAM
<br />ATTACHED TO THE VESDA DETECTOR UNIT. (BY
<br />DETAILS AND MOUNTING ELEV.
<br />SEATRONICS)
<br />BOEING REFERENCE DRAWINGS:
<br />PROVIDE NEW 787 COMPATIBLE AIR SAMPLING HOSE
<br />40-022-E506-10 VESDA SHUNT TRIP RESET MAP
<br />40-022-E506-11 POS. 1 EPS-R1 DETAILS
<br />PROVIDE FIRE ALARM SYSTEM ADDRESSABLE
<br />40-022-E506-12 POS. 3 EPS-R3 DETAILS
<br />MONITOR/RELAY MODULES FOR ACTIVATION CONTROL
<br />40-022-E506-16 POS. 2 EPS-R2 DETAILS
<br />AND SUPERVISION OF EPS PANELS. LOCATE
<br />MODULES WITHIN 3 FEET OF EPS PNL. OBSERVE
<br />40-022-E506-17 POS. 4 EPS-R4 DETAILS
<br />SEPARATION REQUIREMENTS OF CLASS 1 CIRCUIT
<br />40-021-1E263 BLDG. FACP LOCATION
<br />(ACTIVATION CIRCUIT) FROM FA POWER LTD.
<br />MONITORING CIRCUITS.
<br />INSTALL SMOKE DETECTOR ABOVE CONTROL UNIT.
<br />INSTALL NEW MAIN VESDA FAR AT COL. D-5 TO
<br />SERVE NEW 40-21 VESDA SYSTEM AND NEW
<br />40-22 VESDA SYSTEMS,
<br />CONSTRUCTION NOTES:
<br />INSTALL NEW VESDA COMMUNICATIONS EQUIPMENT
<br />ENCLOSURE ADJACAENT TO VESDA MAIN FAR AT
<br />� INSTALL VESDA SYSTEM POSITION PANEL AT COL,
<br />D-5.
<br />D/6.5. WALK INSTALLATION WITH ENGINEER FOR
<br />PROVIDE/INSTALL CONNECTION TO BOEING INTRANET.
<br />EXACT PANEL PLACEMENT. INSTALL NEW PANEL AND
<br />DEVICE LABELS. PROVIDE ALL ANCILLARY DEVICES
<br />1
<br />PROVIDE CONDUIT WIRE BETWEEN VESDA MFAP &
<br />/
<br />AND APPURTENANCES INCLUDING NEW BATTERIES
<br />EXIST. BUILDING PAP. CONTACT BLDG. FACP
<br />AND POWER SUPPLY TO MAKE SYSTEM FUNCTIONAL,
<br />PROVIDER FOR WIRE REQUIREMENTS, MIN. 3
<br />INCLUDING HORN/STROBE AND MANUAL PULL
<br />CIRCUITS FOR BLDG. FACP TO MONITOR VESDA
<br />STATION. CONTROL PANEL TO BE LABELED BY A WA
<br />MFAP ALARM, SUPERVISORY &TROUBLE.
<br />L&I APPROVED TESTING LAB/ENGINEERING
<br />EVALUATION.
<br />16.
<br />PROVIDE FINAL TERMINATION, START-UP, SITE
<br />VESDA GRAPHICS AND ALARMING MODIFICATIONS,
<br />[2::�:> PROVIDE DEDICATED 120V EMERGENCY POWER
<br />AND TESTING AND COMMISSIONING SERVICES FROM
<br />CIRCUIT AND WIRE TO POWER SUPPLY. SEE BOEING
<br />SEATRONICS, INC.
<br />DRAWING 40-022-1E62 FOR DETAILS.
<br />17.
<br />NEW VESDA SYSTEM EQUIPMENT PROVIDED BY
<br />PROVIDE CONDUIT/WIRE BETWEEN VESDA SYSTEM
<br />SEATRONICS. EQUIPMENT IS TO BE MOUNTED
<br />PANEL LOCATIONS AS SHOWN FOR INTER -PANEL
<br />/INSTALLED BY BOEING ELECTRICAL CONTRACTOR AS
<br />COMMUNICATIONS/SIGNALING.
<br />REQUIRED. NEW ELECTRICAL RACEWAY AND
<br />® PROVIDE NEW EPS-R4 PANEL AND WIRE TO VESDA
<br />CONDUCTORS PROVIDED AND INSTALLED BY
<br />ELECTRICAL CONTRACTOR. AIRPLANE EMERGENCY
<br />SYSTEM AND 480V POWER AS SHOWN. SEE E110
<br />POWER SHUTDOWN SYSTEM DESIGN PROVIDED BY
<br />SERIES FOR SHUNT TRIP WIRING CONNECTIONS AND
<br />BOEING, EQUIPMENT & INSTALLATION BY ELECTRICAL
<br />BOEING DRAWING 40-022-E506-17 FOR PANEL
<br />CONTRACTOR.
<br />WIRING DIAGRAM AND ENCLOSURE DETAILS.
<br />INSTALL POSITION PANEL TO VESDA CART CABLE
<br />CONNECTION J-BOX AS SHOWN. ALL CONDUIT
<br />BODIES AND J-BOXES ARE TO BE PAINTED RED.
<br />SCALE: NONE
<br />110773-FA101- D
<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 98071
<br />253-939-6060
<br />-PROPRIETARY-
<br />THIS INFORMATION IS HE
<br />PROPERTY OF SEATRONICS,
<br />INC AND SHALL NOT BE
<br />OLIZED OR DISCLOSED
<br />WRHOUT WRITTEN
<br />AUTHORIZATION FROM
<br />SEATRONICS, INC.
<br />DRAWN
<br />SFATRON
<br />DATE
<br />os 1s 08
<br />SUBTITLE
<br />VESDA SYSTEM
<br />ONE LINE DIAGRAM
<br />CURRENT REVISION
<br />-
<br />SYMBOL
<br />D
<br />DATE
<br />04/14/23
<br />-
<br />NEW -
<br />TD
<br />9/18/06
<br />CHECKED
<br />SHEET
<br />� n A O �1
<br />/-pill -I
<br />A
<br />CONNECTED TEMP. VESDA AT E-4.5 -
<br />TO
<br />7/9/07
<br />"Iry
<br />TITLE _
<br />BOEING 40-22 BLDG.
<br />AIRCRAFT FIRE DETECTION SYSTEM
<br />- EVERETT
<br />e
<br />DELETED FORMER Pos. 1 -
<br />TO
<br />12 22 08
<br />/ /
<br />CHECKED
<br />C
<br />ADDED NEW VESDA POS. 1 -
<br />TO
<br />09/28/17
<br />APPROVED
<br />JOB NO.
<br />-
<br />DDMP NO.
<br />D
<br />ADDED NEW VESDA POS. 4 &MFAP -
<br />TO
<br />04/14/23
<br />APPROVED
<br />DWG No.
<br />110773-FA101-D
<br />
|