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27" 1 0 <br />26" <br />SIEMENS <br />1 10 <br />SMK DET. ABV. FAR - <br />LOCATED Q SEATRONICS. TECH. TO <br />COL. D-5 FIELD VERIFY LOCATION. <br />LOCATE WITHIN 6 FEET LEFT <br />OR RIGHT SIDE OF MFAP <br />1 1 AT CONVENIENT ELEVATION. <br />MFAPE VCE COMMUNICATIONS <br />VESDA <br />ENCLOSURE: + <br />14"w x 16"H x s"D I o TB1 <br />0 16 15 14 13 12 1I1 10 9 <br />120VAC CONDUIT ENTRY <br />O zs"w x v"H x 8°D VESDA CONTROL PANEL POS. 1 <br />�3" MIN. <br />70�� BATT 40-21 COL. e-2 => <br />BATTERY ENCLOSURE: <br />26"W x 12"H x 9"D <br />SMOKE DET. ABV. MFAP <br />AT D-5 <br />LOCATED 5 <br />COL. D-5 I SMKDET <br />OP921 ® 6 <br />MFAP EQUIPMENT MOUNTING ELEVATIONS <br />(NO SCALE) <br />MFAP EXTERIOR FRONT VIEW <br />SCALE: 1/4"=1 SIEMENS CERBERUS PRO MODULAR <br />INTERNAL <br />EQUIPMENT MTG. <br />PNL. <br />M FAP SIEMENS MODEL CERBERUS PRO MODULAR <br />O <br />xDLC <br />0 <br />O n <br />0w r <br />0�. <br />0�, , <br />0= <br />o Ow <br />p 0�.. <br />=o <br />0� <br />;0— <br />XDLC <br />ADDR. <br />001] <br />O 11 NOT USE <br />PI g <br />PSC-12 <br />O RESEi <br />o vovEa <br />o O <br />NODULE 3 <br />o C11 FAIL <br />o r EnFAILIN"' <br />O GNU <br />0 1v "12'FAIL <br />o zav as Fan <br />010 ADDR. <br />A.-D <br />BATTERY IF Fro OF BUS <br />O ❑ <br />POWER TERMINATION BOARD <br />r• <br />!7 <br />MFAP INTERIOR COMPONENT LAYOUT DIAGRAM <br />SCALE: 1/2"=1 <br />REVISION BY APPROVED DATE SYM REVISION <br />BOEING 787 BUILD BACK PROJECT - TD 04/14/23 <br />10 <br />MEAD INTERNAL MODULES WIRING <br />CC5 CARD CAGE #1 BACK PLANE <br />++� <br />E11/E5 (LEFT EDGE) <br />DLC MODULE ADDR. #001 <br />- <br />g +1 <br />< <br />i <br />L. + <br />+ <br />2 + <br />17+ <br />18 <br />19T <br />a-3 <br />ll0oN <br />2 <br />Tig <br />12 —4 <br />_- <br />22 <br />o <br />0 <br />13 m+6 <br />14 <br />�_8 <br />+ WH <br />24 <br />_ <br />15 <br />i6 <br />_ BK <br />PSC-12 MODULE ADDR. #010 <br />TB4 <br />d TB3 <br />P12 <br />P9 <br />TB2 TB2 <br />N 19 N013 <br />NO 20 m Nc 14 <br />C21 C 1 <br />NO 22 NO 16 <br />-�14 <br />NO2 NC 57 <br />C0 <br />24 c 18 <br />SUPERVISORY <br />SYS. BATT. <br />HARNESS <br />A <br />+ <br />+ TB1 <br />16 Fl5 14 113 112 1 11 110 1 9 <br />VESDA CONTROL PANEL POS. 2 <br />40-21 COL. 3-4.5 => <br />—AUX. 24VDC PWR. TO VESDA <br />COMMUNICATIONS ENCL. (VCE) <br />ADJACENT TO MFAP AT D-5. <br />EQUIPMENT LIST <br />CD 40-21/22 BLDG. VESDA SYSTEM MAIN FIRE ALARM PANEL ASSEMBLY (MFAP) <br />ITEM QTY DESCRIPTION PART NUMBER MANUFACTURER <br />1 1 FIRE ALARM CONTROL PNL. ENCL. ASSY. CERBERUS PRO MOD. CERB PRO MOD SIEMENS <br />2 1 CONTROL PANEL MAIN BOARD, CONTROLS & DISPLAY FCM2041-U3 SIEMENS <br />3 1 POWER SUPPLY/CHARGER MODULE PSC-12 SIEMENS <br />4 1 POWER TERMINATION BOARD PTB SIEMENS <br />5 1 MODULE CARD CAGE CC-5 SIEMENS <br />6 1 DIGITAL LINE CARD (SLC CIRCUIT) XDLC SIEMENS <br />7 0 INDICATING CIRCUIT MODULE, 4 NAC OR RELEASING CIRCUITS ZIC-4A SIEMENS <br />8 0 CONTROL RELAY MODULE, 6 DPDT RELAYS CRC-6 SIEMENS <br />9 0 NETWORK INTERFACE CARD NIC-C SIEMENS <br />10 2 ENCLOSURE INNER DOOR BLANK PLATE ID-SP SIEMENS <br />11 1 BATTERY ENCLOSURE CAB-BATT-R SIEMENS <br />12 2 BATTERY, 12V, 55AH PS-12550 POWER SONIC <br />I I TB1 <br />6 15 14 13 112 1 11 110 1 9 <br />VESDA CONTROL PANEL POS. 6 <br />40-21 COL. C-10 T5 <br />i I + <br />� I + <br />TB1 <br />16 115 114 1 13 1 12 1 11 1 10 9 <br />A VESDA CONTROL PANEL POS. 4 <br />40-21 COL. C-8.5 5> <br />A <br />WH _ <br />sLc 1 A A <br />BK <br />CiB A + <br />� I + <br />TB1 <br />6 115 114 113 12 111 110 1 9 <br />2#18 VESDA CONTROL PANEL POS. 3 <br />40-21 COL. C-5 => <br />�X <br />® I + <br />�I j TB 1 <br />Fl 6 115 114 1 13 1 12 1 11 110 1 9 <br />VESDA CONTROL PANEL POS. 4 <br />40-22 COL. D-5 => <br />BATTERY SYSTEM TROUBLE/SUPV SIG. TO <br />BLDG. FAP INTERFACE. <br />12 12 ENCLOSURE <br />3 SYSTEM ALARM SIGNAL TO <br />BLDG. FAP INTERFACE. <br />BATTERY BATTERY <br />SYSTEM SUPERVISORY SIGNAL <br />TO BLDG. FAP INTERFACE. <br />TO 120 VAC -::::fl MFAP WIRING DIAGRAM I FIELD TERMINATIONS <br />DEDICATED CKT. COL. D-5 <br />ON EMERG. PWR. <br />40-21 /22 VESDA SYSTEM MAIN FIRE ALARM PANEL (MFAP) <br />WIRING CONNECTION DETAILS <br />SCALE: NONE <br />APPROVED DATE <br />SEATRONICS-PRQPRIETH <br />THIS INFORMATIONNISIS THE <br />PROPERN OF SEATRONICS, <br />FIRE PROTECTION SERVICES uiiu2eo OR DISCLOSED <br />WITHOUT WRITTEN <br />PO BOX 1138 AUTHORIZATION FROM <br />AUBURN, WA 98071 SEATRONICS, INC. <br />253-939-6060 <br />GENERAL NOTES <br />1. SEE DWG. 110773-FA101, 40-22 VESDA SYSTEM <br />ONELINE DRAWING. <br />2. SEE DWG. 110773-FA121, 40-21 VESDA SYSTEM <br />ONELINE DRAWING. <br />3. SEE DWG. 110773-FA201, 40-22 OVERALL VESDA <br />SYSTEM PLAN, FOR EQUIPMENT LOCATIONS. <br />4. SEE DWG. 110773-FA221, 40-21 OVERALL VESDA <br />SYSTEM PLAN, FOR EQUIPMENT LOCATIONS. <br />� SEE DWG. 110773-FA308, VESDA POSITION <br />INTERCONNECT WIRING DETAILS. <br />©SEE BOEING DWG. 40-021-1E263, BLDG. FACE <br />LOCATION. <br />CONSTRUCTION NOTES: <br />1�INSTALL NEW AIRPLANE VESDA SYSTEM MAIN FIRE <br />ALARM PANEL (MFAP), SIEMENS MODEL CERBERUS <br />PRO MODULAR. <br />120 VAC DEDICATED CKT. ON EMERGENCY POWER. <br />CIRCUIT BREAKER TO BE CLEARLY LABLED "FIRE <br />ALARM" NEXT TO BREAKER AND ON PANEL <br />SCHEDULE. CIRCUIT BREAKER SHALL BE FITTED <br />WITH AN ANTI -TAMPER DEVICE TO PREVENT <br />ACCIDENTAL OR INCIDENTAL TURN-OFF. CKT. <br />SOURCE & NUMBER TO BE LABELED ON PANEL <br />FRONT. <br />INSTALL NEW BATTERY ENCLOSURE BELOW MFAP. <br />® CONTACT BLDG. FACP PROVIDER FOR WIRE <br />REQUIREMENTS, MIN. 3 CIRCUITS FOR 40-21 <br />BLDG. FACE TO MONITOR VESDA MFAP ALARM, <br />SUPERVISORY & TROUBLE. <br />5. NEW VESDA SYSTEM EQUIPMENT PROVIDED BY <br />SEATRONICS. EQUIPMENT IS TO BE MOUNTED <br />/INSTALLED BY BOEING ELECTRICAL CONTRACTOR AS <br />REQUIRED. NEW ELECTRICAL RACEWAY AND <br />CONDUCTORS PROVIDED AND INSTALLED BY <br />ELECTRICAL CONTRACTOR. <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 THEN STRANDED (RED & BLACK) <br />E = CAROL WIRE P/N C2536A #16 AWG SHEILDED TWISTED <br />PAIR, STRANDED, JACKETED CABLE (.307" OD) TYPE <br />CM. <br />F - CABLE TYPE 'SOOW', 12-#16 AWG. CAROL 09612 OR <br />EQUAL (.70" NOM. OD) <br />G = NOT USED <br />H = #16 TEEN OR TEN STRANDED <br />MAIN FIRE ALARM PANEL ASSY. & WIRING DIAGRAM <br />TITLE _ <br />BOEING 40-22 BLDG. <br />AIRCRAFT FIRE DETECTION SYSTEMS <br />EVERI <br />110773-FA306-0 <br />'.EVISION SYMBOL DATE <br />- 04/14/23 <br />FA306 <br />COMP N0. <br />110773—FA306-0 <br />