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LOCATED
<br />AT
<br />BLDG. 45-02
<br />FIRE DEPT.
<br />MEZZANINE LEVEL
<br />VESDA GRAPHICS COMM LINK
<br />BOEING INTRANET-ETHERNET
<br />CONNECTION
<br />TO BOEING
<br />INTRANET
<br />VESDA
<br />SYSTEM
<br />GRAPHICS
<br />SEVER PC
<br />(GRAPHICAL INTERFACE)
<br />CUSTOM GRAPHICS MONITORING & �
<br />CONTROL PC FOR REMOTE MONITORING &
<br />CONTROL OF AIRPLANE VESDA SYSTEMS.
<br />SYSTEM CAN BE MONITORED AND
<br />CONTROLLED OVER INTRANET/INTERNET.
<br />CUSTOM SOFTWARE PROVIDED BY
<br />SEATRONICS.
<br />Permit #:
<br />FA2308-009
<br />Site Address:
<br />Applicant
<br />atr W. Casino Rd
<br />Seatronics Inc
<br />THE BOEING COMPANY
<br />Application Date: 08/11/2023
<br />Description:
<br />New Fight Line Aircraft Detection
<br />BUILDINGS 40-21, 40-22 & 40-24
<br />LOCATED ALONG TRANSPORTATION
<br />LOCATED ON DESIGNATED
<br />BUILDING SUPPORT COLUMNS
<br />LOCATED AT FACTORY FLOOR
<br />LOCATED ONBOARD
<br />Review Status:
<br />Review Date:
<br />1st Review by City &Peer
<br />08/16/2023
<br />Reviewers
<br />AISLE, TYPICALLY ENT NEAR BUILDING
<br />ENTRY
<br />ALONG BUILDING TRANSPORTATION
<br />LEVEL NEAR NOSE OF AIRPLANE
<br />AIRCRAFT
<br />j
<br />AISLES
<br />FINAL ASSEMBLY
<br />EVERECE TT EVERr
<br />AIRCRAFT EARLY WARNING
<br />Everett
<br />Fire Dept. Permit
<br />eview
<br />Status:Approved
<br />Reviewed By: KBro
<br />n
<br />FIRE DETECTION SYSTEMS
<br />VESDA GRAPHICS
<br />CONTROL SYSTEM
<br />08/16/2023 4-22.11
<br />INTERFACE MODULE
<br />VESDA GRAPHICS NETWORK COMS
<br />VESDA GRAPHICS NETWORK COMS
<br />l
<br />PM
<br />(RS-485)
<br />(Rs-485)
<br />I
<br />TO NEXT AIRCRA
<br />BLDG.
<br />HORN/
<br />I I
<br />ASSEMBLY POSITIONS
<br />EVERETT WA
<br />FACP
<br />STROBE
<br />Y
<br />NTERFACE
<br />z o L
<br />VESDA CONTROL
<br />HORN/
<br />a
<br />o
<br />PANEL
<br />STROBE
<br />�-¢
<br />CURRENT PROJECT -GENERAL SCOPE OF WORK
<br />AIRPLANE VESDA
<br />a I
<br />SYSTEMS
<br />VESDA GRAPHICS
<br />CONTROL SYSTEM
<br />POWER &SIGNAL CABLE(S)
<br />VESDA
<br />L J
<br />THE AIRPLANE FINAL ASSEMBLY LINES IN THE 40-21, 40-22 & 40-24 BUILDINGS ARE BEING UPDATED TO BETTER
<br />MAIN FIRE ALARM
<br />INTERFACE MODULE
<br />SUPPORT CURRENT ASSEMBLY REQUIREMENTS OF VARIOUS BOEING AIRPLANE MODELS.
<br />PANEL
<br />DETECTOR UNIT
<br />THIS PROJECT SCOPE INCLUDES NEW VESDA SYSTEMS AS WELL AS UPDATES, MODIFICATIONS AND ADDITIONS TO THE
<br />120 VAC
<br />AIR FLOW
<br />VESDA CONTROL
<br />EXISTING EQUIPMENT FOR THE AIRPLANE VERY EARLY WARNING SMOKE DETECTION SYSTEMS (VESDA SYSTEMS).
<br />(MFAP)
<br />MONITORING
<br />UNT — ALARM
<br />THESE ARE AN AIR SAMPLING TYPE SMOKE DETECTION SYSTEM USED TO DETECT FIRES INSIDE THE AIRPLANE HULLS
<br />DED. CKT.
<br />CONTROL
<br />& SUPERVIsION
<br />WHILE ON THE FINAL ASSEMBLY LINE.
<br />MODULE
<br />OUTPUT SIGNALS
<br />POWER
<br />SHUTU'N
<br />SAVE
<br />PULL
<br />PULr
<br />N
<br />LASTAIRCRAFT ASSEMBLY POSITION
<br />(SOUTH END OF LINE)
<br />SCOPE:
<br />40-21 BUILDING:
<br />INSTALL ONE(1) NEW MAIN VESDA FIRE ALARM PANEL AND FIVE(5) NEW COMPLETE AIRPLANE ASSEMBLY POSITION
<br />SWITCH
<br />VESDA SYSTEMS.
<br />SYSTEM DESCRIPTION
<br />FIRE ALARM SYSTEM COMS
<br />FIRE ALARM SYSTEM
<br />INTERFACE MODULES
<br />FIRE ALARM SYSTEM COWS
<br />120 VAC VESDA POWER AIRCRAFT POSITION
<br />SUPPLY PNL. POWER SHUTDOWN
<br />DED. CKT. INTERFACE RELAY
<br />PANEL
<br />TYPICAL EACH BUILDING -�- TYPICAL PER EACH AIRCRAFT ASSEMBLY POSITION
<br />AIRCRAFT FIRE DETECTION SYSTEMS FUNCTIONAL BLOCK DIAGRAM
<br />The Aircraft Final Assembly Early Warning Fire Detection System is designed
<br />to detect fires in the incipient stages of combustion within the aircraft
<br />interior during final assembly. This is accomplished through the use of the
<br />highly sensitive VESDA early warning air sampling type smoke detector. In
<br />this system, air samples are drawn back to the VESDA detector from an air
<br />sampling hose network placed onboard the aircraft. The detector optically
<br />examines air samples for smoke particles to determine the amount of light
<br />obscuration per foot of the air sample. A signal based on the obscuration
<br />level is sent from the detector to the VESDA Controller. The VESDA
<br />Controller processes this signal to provide a visual indication at the
<br />controller as well as output relays to provide auxiliary control functions. This
<br />early detection capability enhances the ability for emergency response
<br />personnel to take action before a major fire occurs, thus minimizing the
<br />potential for injury to person or property.
<br />The complete system is comprised of the following primary sub —systems:
<br />1. Air sampling hose networks onboard each aircraft.
<br />2. VESDA Detector Unit (VDU) panels — cart mounted enclosures assemblies
<br />(one per airplane) located near the aft entry to the airplane. The
<br />enclosure contains the Vesda air sampling smoke detector unit, aspirator
<br />and filters.
<br />3. VESDA Control Panels (VCR) located on the main floor level along the
<br />transportation aisle (one panel for each aircraft position).
<br />4. VESDA System Main Fire Alarm Panel (MFAP) located along the building
<br />transportation aisle.
<br />5. Accessory control and indicating equipment, ie., Manual Stations, Save
<br />Switches, Audible/Visual annunciating devices.
<br />6. VESDA Graphics System — Web based graphical interface computer system
<br />for remote monitoring and control of the Early Warning Fire Detection
<br />System.
<br />The following is a description of the above listed system components and
<br />their function:
<br />Air Sampling Network:
<br />The air sampling network is comprised of lengths of flexible reinforced vinyl
<br />hose lengths which run from the VESDA detector into and down the length
<br />of the aircraft. The air sampling hose inside the aircraft is suspended
<br />from the ceiling/overhead. The air sampling hose has small air sampling
<br />fittings inserted into it at predetermined intervals along its length. The
<br />fittings are drilled with an air sampling inlet hole. These holes serve as a
<br />smoke detection sampling points. The air samples are drawn back to the
<br />VESDA smoke detector for examination by the detector via a high efficiency
<br />aspirator located inside the VESDA detector unit.
<br />VESDA Detector Unit:
<br />The VESDA Detector Unit (VDU) is a NEMA 12 enclosure which contains the
<br />VESDA detector assembly, aspirator and filters. Each VESDA Detector Unit
<br />assembly panel is cart mounted and is located on the main factory floor
<br />near the aft entry to the airplane which it serves. The air sampling hose
<br />network routes from the detector unit up through a dedicated hatch near
<br />the aft entry door of the airplane and then forward down the length of the
<br />airplane. Air samples drawn into the detector from the air sampling hose
<br />network are illuminated within a chamber in the detector by a high intensity
<br />laser light source. Particles within the air sampling chamber reflect some of
<br />this light to a highly sensitive photocell. The photocell produces a signal
<br />which is conditioned and sent to the VESDA Control Panel for processing.
<br />VESDA Control Panel:
<br />The VESDA Control Panel (VCR) is a NEMA 1 enclosure with hinged locking
<br />door and viewing window. This enclosure houses the VESDA Control/Display
<br />module, power supply, standby batteries, auxiliary relays and addressable
<br />interface modules required to transmit alarm and trouble signals to the
<br />VESDA System Main Fire Alarm Panel (MFAP). A Power Shutdown Interface
<br />Relay junction box is mounted directly above the VESDA Control Panel. The
<br />power shutdown interface relay is connected to the power shutdown control
<br />panel for the position, to provide power shutdown capabilities for the
<br />aircraft assembly position. The power shutdown function is activated by the
<br />activation of a VESDA High Level Smoke Alarm or Manual Station.
<br />The VESDA Controller module is a microprocessor based control module that
<br />monitors, interprets and processes control signals from the VESDA detector.
<br />The controller continuously monitors the detector for proper operation (air
<br />flow, sensitivity, light source, etc.) and processes the smoke level input
<br />signal to display on a borgroph. Three alarm output levels are
<br />programmable based on the smoke level reading as well as a time delay
<br />for each level before it latches into alarm. The controller is also
<br />programmable for day and night sensitivity and alarm levels. The VESDA
<br />Controller communicates to the VESDA Graphics System Server PC computer
<br />via a web enable communications interface module in the Vesda Control
<br />Panel, to present a real time graphical display of alarm and/or fault
<br />conditions.
<br />VESDA System Main Fire Alarm Panel:
<br />The VESDA System Main Fire Alarm Panel (MFAP) is a Siemens model
<br />Cerberus Pro Modular, microprocessor based fire alarm panel. This panel
<br />annunciates and processes alarm and trouble signals that are initiated from
<br />the VESDA Control Panel's VESDA detector, manual stations and power
<br />shutdown Save Switches. A communications loop is run from the MFAP to
<br />all of its respective VESDA Control Panels. Addressable interface modules
<br />located in the VESDA Control Panels are used to input alarm and trouble
<br />signals from the VESDA Control Panels into the MFAP communications loop.
<br />The MFAP also controls power shutdown functions to each aircraft through
<br />an addressable relay module located in the VESDA Control Panels. The MFAP
<br />provides connections for remote trouble and alarm reporting. The MFAP is
<br />connected the building fire alarm network to provide signal annunciation at
<br />the building main fire alarm panel.
<br />VESDA Graphics System Monitoring & Control Computer
<br />The VESDA Graphics System Server PC provides a Web based graphical user
<br />interface for real time display and control of VESDA monitoring and
<br />functions. The monitoring and control functions may be accessed over the
<br />Boeing Intranet by persons with proper login credentials. The system is
<br />primarily monitored by Boeing Fire & Security at GSOC, With local
<br />monitoring at the site Fire Station. The system primary display screen
<br />depicts the factory floor plan displaying all the aircraft positions in the
<br />factory as an airplane outline. Aircraft are shown in colors which indicate
<br />its current status with respect to the VESDA system (green — normal,
<br />yellow — trouble, red — alarm, blue — isolate and white outlined to indicate
<br />no airplane present ("Out of Service").
<br />TO NEXT AIRCRAFT
<br />ASSEMBLY POSITIONS
<br />Secondary control "pop—up" screens are activated by clicking on an airplane
<br />symbol. The pop—up window provides the following control function
<br />selections: "Normal On", "Reset", "Isolate", "Out Of Service" and
<br />"Acknowledge".
<br />Manual Stations:
<br />A Manual Station is provided at each VESDA Control Panel location for
<br />manual initiation of an alarm. The Manual Station transmits alarms to the
<br />MFAP via an addressable interface module located in the VESDA Control
<br />Panel. Activation of the Manual Station will immediately shutdown power to
<br />that aircraft position and transmit alarm signals.
<br />Save Switch: I
<br />A power shutdown Save Switch is provided on the front door of the Vesda
<br />Control Panel for each aircraft position. The Save Switch transmits the
<br />abort signal to the MFAP via an addressable interface module located in the
<br />VESDA Control Panel. If High Level smoke alarm is present on the Vesda
<br />control unit, depressing the yellow mushroom pushbutton switch will reset
<br />the power shutdown time delay back to 60 seconds and an amber lamp
<br />mounted directly above the pushbutton will illuminate. If the pushbutton is
<br />released with the alarm still present, the shutdown timer will restart at 60
<br />seconds timing to shutdown. Depressing the Save Switch with no alarms
<br />present will indicate a trouble at the MFAP.
<br />Audible/Visual Device
<br />An Audible/Visual alarm indicating device is provided at each aircraft
<br />position mounted directly above the VESDA Control Panel. This device
<br />operates whenever a High Level Smoke alarm is initiated on the Vesda
<br />Control Unit or a Manual Station is activated for the respective position. The
<br />Audible/Visual device is silenced by depressing the "Alarm Silence"
<br />push—button located inside the VESDA Control Panel or by depressing the
<br />Alarm Silence" at the MFAP.
<br />40-22 BUILDING:
<br />INSTALL ONE(1) NEW COMPLETE AIRPLANE ASSEMBLY POSITION VESDA SYSTEM.
<br />40-24 BUILDING:
<br />INSTALL ONE(1) NEW COMPLETE AIRPLANE ASSEMBLY POSITION VESDA SYSTEM TO THE EXISTING BUILDING VESDA
<br />SYSTEM. RENAME AND RE -LABEL THE EXISTING THREE POSITIONS AS SHOWN ON PLANS.
<br />EQUIPMENT:
<br />THE NEW MAIN FIRE PANEL THAT SERVES THE 40-21 BLDG. POSITIONS 1,2,3,4 & 6 AND THE 40-22 BLDG.
<br />POSITION 4, SHALL BE SIEMENS MODEL CERBERUS PRO MODULAR AND SHALL INTERFACE TO THE 40-21 BLDG.
<br />LAP.
<br />EACH NEW AIRPLANE POSITION VESDA SYSTEM SHALL INCLUDE THE FOLLOWING:
<br />A. PROVIDE NEW VESDA CONTROL PANEL (VCR), POWER SUPPLY, MANUAL STATION, HORN STROBE AND STANDBY
<br />BATTERIES.
<br />B. PROVIDE FIRE ALARM ADDRESSABLE INTERFACE RELAY/MONITOR MODULE FOR CONTROL AND SUPERVISION OF
<br />AIRPLANE POSITION EMERGENCY POWER SHUTDOWN SYSTEM (EPS). EPS PANEL AND SYSTEM COMPONENTS
<br />PROVIDED BY OTHERS.
<br />C. PROVIDE NEW CART MOUNTED VESDA DETECTOR UNIT (VDU) ASSEMBLY WITH HORN -STROBE, UMBILICAL CABLE &
<br />CONNECTOR. UNIT TO BE LOCATED NEAR NOSE OF AIRPLANE POSITION.
<br />D. PROVIDE ONE(1) NEW VESDA CABLE CONNECTOR JUNCTION BOX ASSEMBLY.
<br />E. PROVIDE ONE(1) NEW AIRPLANE AIR SAMPLING NETWORK HOSE SET.
<br />F. COMMISSION AND TEST ALL NEW OR MODIFIED EQUIPMENT.
<br />VESDA SYSTEM REMOTE MONITORING GRAPHICS SYSTEM:
<br />A. INSTALL NEW VESDA COMMUNICATIONS EQUIPMENT ENCLOSURE TO SUPPORT NEW 40-21/22 VESDA SYSTEMS.
<br />LOCATE ADJACENT TO 40-21/22 MFAP.
<br />B. MODIFY EXISTING VESDA GRAPHICS SYSTEM MONITORING SOFTWARE TO INCLUDE ALL NEW VESDA POSITIONS.
<br />C. RENAME/UPDATE POSITION NAMES AND MESSAGES FOR EXISTING 40-24 BLDG. VESDA POSITIONS.
<br />NOTE — SEATRONICS TO PROVIDE FIRE ALARM AND VESDA SYSTEM EQUIPMENT. BOEING ELECTRICAL CONTRACTOR IS
<br />TO PROVIDE EQUIPMENT INSTALLATION, RACEWAY INSTALLATION, CONDUCTORS AND INSTALLATION MATERIALS. AIRPLANE
<br />POSITION POWER SHUTDOWN SYSTEM DESIGN PROVIDED BY BOEING AND/OR PROJECT ELECTRICAL CONTRACTOR,
<br />INSTALLATION BY PROJECT ELECTRICAL CONTRACTOR.
<br />PROJECT
<br />DRAWING INDEX
<br />DWG. NO.
<br />SHEET NO.
<br />DRAWING TITLE
<br />REV.
<br />110773
<br />FA01a
<br />COVER,
<br />SYSTEM BLOCK DIAGRAM, DESCRIPTION
<br />C
<br />110773
<br />FA121
<br />40-21
<br />BLDG.
<br />VESDA SYSTEM ONE LINE DIAGRAM
<br />—
<br />110773
<br />FA221
<br />40-21
<br />BLDG.
<br />VESDA SYSTEM EQUIPMENT LOCATION OVERALL PLAN
<br />—
<br />110773
<br />FA101
<br />40-22
<br />BLDG.
<br />VESDA SYSTEM ONE LINE DIAGRAM
<br />D
<br />110773
<br />FA201
<br />40-22
<br />BLDG.
<br />VESDA SYSTEM EQUIPMENT LOCATION OVERALL PLAN
<br />D
<br />110773
<br />FA306
<br />40-22
<br />BLDG.
<br />COL. D-5, MAIN FIRE ALARM PANEL ASSY. & WIRING
<br />—
<br />110773
<br />FA307
<br />40-22
<br />BLDG.
<br />VESDA COMMUNICATIONS ENCL. ASSY. & WIRING
<br />—
<br />110773
<br />FA308
<br />40-22
<br />BLDG.
<br />VESDA CONTROL PANEL SYSTEM WIRING CONNECTIONS
<br />_
<br />110773
<br />FA351
<br />VESDA
<br />CONTROL PANEL ASSEMBLY
<br />—
<br />110773
<br />FA352
<br />VESDA
<br />DETECTOR PANEL ASSEMBLY
<br />—
<br />111009
<br />FA101
<br />40-24
<br />BLDG.
<br />VESDA SYSTEM ONE LINE/RISER DIAGRAM
<br />B
<br />111009
<br />FA201
<br />40-24
<br />BLDG.
<br />VESDA SYSTEM EQUIPMENT LOCATION OVERALL PLAN
<br />B
<br />111009
<br />FA301
<br />40-24
<br />BLDG.
<br />MAIN FIRE ALARM PANEL ASSY. & WIRING
<br />B
<br />111009
<br />FA302
<br />40-24
<br />BLDG.
<br />VESDA COMMUNICATIONS ENCLOSURE ASSY. & WIRING
<br />B
<br />111009
<br />FA303
<br />40-24
<br />BLDG.
<br />VESDA CONTROL PANEL SYSTEM WIRING CONNECTIONS, POS. 3 & 4
<br />B
<br />111009
<br />FA305
<br />40-24
<br />BLDG.
<br />VESDA CONTROL PANEL SYSTEM WIRING CONNECTIONS, POS. 1
<br />—
<br />111009
<br />FA315
<br />VESDA
<br />CABLE
<br />CONNECTOR JUNCTION BOX ASSEMBLY
<br />—
<br />REVISION
<br />BY
<br />I APPROVED
<br />DATE
<br />I SYM
<br />REVISION
<br />BY
<br />APPROVED
<br />DATE
<br />SEATRONICS
<br />FIRE PROTECTION SERVICES
<br />-PRQPRIETARY—
<br />THIS INFORMATION IS TBE
<br />PROPERTY OF SEATRONICS,
<br />INC. AND SHALL NOT BE
<br />ILIZED OR ED
<br />UnWITHOUT
<br />TD
<br />1 31 07
<br />JVV""` VLbUH 5Yb I t:Wi
<br />COVER, BLOCK DIAGRAM & INDEX
<br />SUBMITTAL RELEASE 110778
<br />TD
<br />1/31 /07
<br />CHECKED
<br />RECORD DRAWING 110778
<br />TO
<br />8/9/07
<br />N IN
<br />TD
<br />1 31 07
<br />TITLE _
<br />AIRCRAFT FINAL ASSEMBLY
<br />CHECKED
<br />VESDA POS.�O INSTALLATION, VESDA FAR UPGRADE 111130
<br />SEATRON
<br />8/26/22
<br />POBOX
<br />AUBURN, WA 98071
<br />A98
<br />253-939-6060
<br />WRITTEN
<br />AUTHORIZATION PRONC.
<br />SEATRONICS, INC.
<br />APPROVED
<br />APPROVED
<br />FIRE DETECTION SYSTEMS
<br />-
<br />787 BUILD BACK PROJECT -
<br />TD
<br />04/14/23
<br />1 0 73-F 01 a-C
<br />LATE
<br />- SYMBOL G 04/14/23
<br />FA01 a
<br />JOB N0. COMP No
<br />110773—FA01a—C
<br />
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