2A.20 Cabin Management System-Service Calls
Service Call/Chime Control Menu
The Service Call/Chime Control Menu displays three selections:
• SERVICE CALL - allows the cabin crew to review and reset passenger
calls originating from either the seats or the lavatories for a seating area.
• AREA CHIME CONTROL - allows the cabin crew to enable or disable
passenger generated chimes by area.
• SEAT CHIME CONTROL - allows the cabin crew to enable or disable
passenger generated chimes by seat.
MAIN
MENU SERVICE CALL/CHIME CONTROL MENU
SERVICE CALL
AREA CHIME CONTROL
SEAT CHIME CONTROL
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Service Calls
Copyright © The Boeing Company. See title page for details.
2A.20.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Service Call
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.3
2A.20 Cabin Management System-Service Call
Service Call Display
1 MAIN MENU
Push - returns to the Main Menu.
2 PREVIOUS MENU
Push - returns to the Service Call/Chime Control Menu.
3 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segment bar illuminate.
4 Left/Right Arrow Switches
Push - displays the desired area/zone.
PREVIOUS
MENU
ACTIVE LAVATORY CALLS ACTIVE SEAT CALLS
2K
1A A
AREA
RESET
SERVICE CALL
FIRST CLASS
MENU
MAIN
B
2 1
3
4
6
7
9
5
8
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Service Call
Copyright © The Boeing Company. See title page for details.
2A.20.4 D611W302-TBC (200 GenFam)
5 Area Description
Displays the selected area:
• FIRST CLASS
• BUSINESS CLASS
• ECONOMY CLASS - FWD
• ECONOMY CLASS - AFT
• ALL AREAS
• CABIN AREA/CHIME CONTROL
6 ACTIVE LAVATORY CALLS List
Displays active lavatory calls for the selected area.
Note: If the list is longer than the display area, a scroll box with up/down arrow
switches is displayed.
7 AREA RESET
Push - clears all service calls.
Verify the Active Calls displays go blank.
8 Scroll Box with Up/Down Arrows
Displayed - associated list display is full.
One push of an arrow switch displays one new line/entry. Once the top or bottom
of the display list is reached, pushing an arrow switch does not change the display.
The scroll box indicates which part of the list is currently being displayed.
Each time a new area is selected, the display reflects the new area.
9 ACTIVE SEAT CALLS List
Displays active seat calls for the selected area.
Note: If the list is longer than the display area, a scroll box with up/down arrow
switches is displayed.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Service Call
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.5
Service Call Operation
The Service Call display shows:
• the default area in the area description display
• a list of pending seat calls for that area
• a list of pending lavatory calls for that area
To check for active seat and/or lavatory calls:
• push the left/right arrow switches to select the desired area/zone
• observe active calls in the ACTIVE SEAT CALLS display and the
ACTIVE LAVATORY CALLS display.
Note: If the display is full, scroll through the Active Calls by pushing the
up/down scroll switches.
To reset/delete active seat and/or lavatory calls:
• push the left/right arrow switches to select the desired area/zone
• push the AREA RESET switch
Note: Pushing the AREA RESET switch clears all service calls.
• observe that the ACTIVE SEAT CALLS and ACTIVE
LAVATORY CALLS displays are blank.
Panel Selections
CSCP 1L -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS - FWD,
ECONOMY CLASS - AFT, and ALL AREAS.
Note: The ALL AREAS selection is available only when the PANEL
OVERRIDE has been selected.
CACP 2L -
• BUSINESS CLASS.
CACP 4R -
• ECONOMY CLASS FWD, ECONOMY CLASS AFT.
Things to Remember
Service calls display in the order that they are received.
Service calls are displayed by location.
Duplicate or repeated calls only display once.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Service Call
Copyright © The Boeing Company. See title page for details.
2A.20.6 D611W302-TBC (200 GenFam)
Service calls from the flight crew rest appear in the ACTIVE LAVATORY CALLS
display. Flight crew rest service calls display FLT CREW RST when FIRST
CLASS is selected.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Area Chimes
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.7
2A.20 Cabin Management System-Area Chimes
Area Chime Control Display
1 MAIN MENU
Push - returns to the Main Menu.
2 PREVIOUS MENU
Push - returns to the Service Call/Chime Control Menu.
3 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segment bar illuminate.
4 Left/Right Arrow Switches
Push - displays the desired area/zone.
CHIME
DISABLE
CHIME
ENABLE
AREA CHIME CONTROL MENU
MAIN
MENU
PREVIOUS
ALL AREAS
2 1
3
4
6 7
5
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Area Chimes
Copyright © The Boeing Company. See title page for details.
2A.20.8 D611W302-TBC (200 GenFam)
5 Area Description
Displays the selected area:
• FIRST CLASS
• BUSINESS CLASS
• ECONOMY CLASS - FWD
• ECONOMY CLASS - AFT
• ALL AREAS
6 ENABLE CHIME Switch
Push (illuminates green) - enables selected area chimes.
7 DISABLE CHIME Switch
Push (illuminates green) - disables selected area chimes.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Area Chimes
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.9
Area Chime Control Operation
The Area Chime Control display shows:
• the default area in the area description display
• the active state of the chimes (enabled or disabled) for the default area.
To disable chimes by area:
• push the left/right arrow switches to select the desired area/zone.
• push the DISABLE CHIME switch
• verify the DISABLE CHIME switch illuminates green.
To reset disabled chimes:
• push the left/right arrow switches to select the desired area/zone
• push the ENABLE CHIME switch
• verify the ENABLE CHIME switch illuminates green.
Panel Selections
CSCP 1L -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS - FWD,
ECONOMY CLASS - AFT, and ALL AREAS.
Note: The ALL AREAS selection is available only when the PANEL
OVERRIDE has been selected.
CACP 2L -
• BUSINESS CLASS.
CACP 4R -
• ECONOMY CLASS FWD, ECONOMY CLASS AFT.
Things to Remember
Chimes disabled during flight are automatically enabled when the air/ground
sensing system determines the airplane is on the ground.
The ALL AREAS selection is available only when PANEL OVERRIDE has been
selected.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Area Chimes
Copyright © The Boeing Company. See title page for details.
2A.20.10 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Seat Chimes
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.11
2A.20 Cabin Management System-Seat Chimes
Seat Chime Control Display
1 MAIN MENU
Push - returns to the Main Menu.
2 PREVIOUS MENU
Push - returns to the Service Call/Chime Control Menu.
3 CLEAR Switch
Push - clears incorrect row/seat entries.
4 CHIMES DISABLED List
Displays all seats whose chimes are disabled.
26 ABC
23 AB
31 ABCDEF
32 A
35 DEF
SEAT CHIME CONTROL MENU
MAIN
MENU
PREVIOUS
ROW/SEAT
CLEAR
ROW SELECT
0 1 2 3 4
5 6 7 8 9
A B C D E F G H
DISABLE
CHIME
ENABLE
CHIME
J K
CHIMES DISABLED
SEAT SELECT
2 1
4
5
3
8
9
6 7
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Seat Chimes
Copyright © The Boeing Company. See title page for details.
2A.20.12 D611W302-TBC (200 GenFam)
5 Scroll Box with Up/Down Arrows
Displayed - associated list display is full.
One push of an arrow switch displays one new line/entry. Once the top or bottom
of the display list is reached, pushing an arrow switch does not change the display.
The scroll box indicates which part of the list is currently being displayed.
Each time a new area is selected, the display reflects the new area.
6 ENABLE CHIME Switch
Push - enables chimes.
Verify Row/Seat selection is deleted from Chimes Disabled list.
7 DISABLE CHIME Switch
Push - disables chimes.
Verify Row/Seat selection appears in the Chime Disabled list.
8 ROW SELECT and SEAT SELECT Switches
Push - enters Row/Seat selection.
Selection appears in ROW/SEAT list.
Note: SEAT SELECT is not visible until a row has been selected.
9 ROW/SEAT List
Displays the row number and seat letter selected from the Row Select and Seat
Select sections.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Seat Chimes
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.20.13
Seat Chime Control Operation
The Seat Chime Control, Chimes Disabled display, shows the list of disabled seat
chimes for all seating areas, with the first row at the top of the list.
Disable Seat Chime
To Disable a Seat Chime:
• enter ROW SELECT/SEAT SELECT selections
• verify selected row/seat(s) are displayed in the ROW/SEAT list
• push the DISABLE CHIME switch
Note: Pushing the DISABLE CHIME switch when only a row number is entered
into the ROW/SEAT field displays all the valid seats for the selected row.
• verify the chime(s) for the selected row/seat(s) are disabled by observing
the Chimes Disabled list.
To Clear an incorrect Row/Seat entry:
• push the Clear switch
• verify the incorrect row/seat entry is deleted from the ROW/SEAT list.
Enable Seat Chime
To Enable previously Disabled Chimes:
• enter ROW SELECT/SEAT SELECT selections
• verify selected row/seat(s) are displayed in the ROW/SEAT list
• push the ENABLE CHIME switch
• verify the chime(s) for the selected row/seat(s) are enabled by observing
that they have been deleted from the Chimes Disabled list.
To Clear an incorrect Row/Seat entry:
• push the Clear switch
• verify the incorrect row/seat entry is deleted from the ROW/SEAT list.
Panel Selections
CSCP 1L -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS - FWD,
ECONOMY CLASS - AFT, and ALL AREAS.
CACP 2L -
• BUSINESS CLASS.
CACP 4R -
• ECONOMY CLASS FWD, ECONOMY CLASS AFT.
Note: The ALL AREAS selection is available only when the PANEL
OVERRIDE has been selected at CSCP 1L.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Seat Chimes
Copyright © The Boeing Company. See title page for details.
2A.20.14 D611W302-TBC (200 GenFam)
Things to Remember
Disabled chimes automatically reset to enabled when the air/ground sensing
system determines the airplane is on the ground.
Chimes disabled from the Area Chime Control display do not appear on this
display.
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Cabin Temperature Section 25
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.25.1
2A.25 Cabin Management System-Cabin Temperature
Cabin Temperature Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 Segmented Bar
Illuminated - shows the selected area description.
3 Left/Right Arrow Switches
Push - displays the desired area/zone.
C
c
F
ACTUAL TARGET
20
68
20
AREA
RESET
CABIN TEMPERATURE MENU
MAIN
ECONOMY FWD 11 thru 18
2
3
5
6
8
4
7
1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Temperature
Copyright © The Boeing Company. See title page for details.
2A.25.2 D611W302-TBC (200 GenFam)
4 Area Description
Displays the selected area:
• FIRST CLASS 1 THRU 3
• BUSINESS CLASS 6 THRU 7
• BUSINESS CLASS 8 THRU 10
• ECONOMY FWD 11 THRU 18
• ECONOMY MID 19 THRU 26
• ECONOMY AFT 27 THRU 41
5 TARGET Temperature
Displays the default or desired target temperature for the selected area/zone.
6 Up/Down Arrow Switches
Push - increases/decreases the target temperature by one degree.
7 AREA RESET
Push - resets the target temperature to the default level.
8 ACTUAL Temperature
Displays the actual temperature in degrees Celsius and degrees Fahrenheit.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Temperature
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.25.3
Cabin Temperature Control System
Air moves from the passenger cabin to the lower deck, where it is either exhausted
overboard or drawn into the recirculation system.
Hot trim air from the bleed air system is added to the pack conditioned air to
control the temperature in each zone. Each trim air system supplies three zone
supply ducts, with the left trim air system also supplying the flight deck.
The cabin temperature controllers regulate the temperature by controlling the
addition of hot trim air to the cabin temperature zones.
The flight crew sets the master passenger cabin target temperature reference to
between 65 and 85 degrees F on the flight deck. The cabin attendants can use the
CSS to adjust the zone target temperature in any passenger zone (+/-10 degrees F
(+/- 6 degrees C), within the limits of 65 to 85 degrees F (18 to 29 degrees C)).
With the loss of inputs from the flight deck or cabin temperature controllers, the
packs maintain a cabin target temperature of 75 degrees F (24 degrees C).
The cabin temperature controllers automatically compensate for temperature
changes as cabin air humidity and passenger activity change during cruise and
descent. The zone target temperature displayed on the Cabin Temperature screen
is automatically increased (approximately 1 degree per hour to a maximum of 4
degrees) during cruise so the flight attendants do not have to manually increase the
target temperature. The zone target temperature is automatically decreased
(approximately 4 degrees F (2 degrees C)) slowly during descent until all
automatic system corrections are removed.
System operation
Increase Target Temperature
To increase the temperature:
• push the left/right arrow switches to select the desired area/zone
• observe the actual temperature
• use the up arrow to increase the target temperature. Each push of the up
arrow increases the target temperature by 1 degree F (1 degree C).
Note: Do not expect an immediate change in the temperature.
Note: Maximum selectable Target Temperature is 85 degrees F (29 degrees C).
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Temperature
Copyright © The Boeing Company. See title page for details.
2A.25.4 D611W302-TBC (200 GenFam)
Decrease Target Temperature
To decrease the temperature:
• push the left/right arrow switches to select the desired area/zone
• observe the actual temperature
• use the down arrow to decrease the target temperature. Each push of the
down arrow decreases the target temperature by 1 degree F (1 degree C).
Note: Do not expect an immediate change in the temperature.
Note: Minimum selectable Target Temperature is 65 degrees F (18 degrees C).
Reset Target Temperature
To reset a passenger zone temperature to the default (flight crew set) level:
• push the left/right arrow switches to select the desired area/zone
• push the AREA RESET switch.
Note: The AREA RESET switch momentarily illuminates light gray after being
pushed.
Panel Selections
CACP 1L -
• FIRST CLASS 1 thru 3, BUSINESS CLASS 6 and 7, BUSINESS
CLASS 8 thru 10, ECONOMY FWD 11 thru 18, ECONOMY MID 19
thru 26, and ECONOMY AFT 27 thru 41.
CACP 2L -
• BUSINESS CLASS 6 and 7, BUSINESS CLASS 8 thru 10, ECONOMY
FWD 11 thru 18, ECONOMY MID 19 thru 26, and ECONOMY AFT 27
thru 41.
CACP 4R -
• ECONOMY FWD 11 thru 18, ECONOMY MID 19 thru 26, and
ECONOMY AFT 27 thru 41.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Temperature
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.25.5
Things to Remember
The cabin temperature control system automatically increases the cabin/zone
target temperature during cruise and decreases the target temperature during
descent.
Temperature changes do not occur immediately; do not over-correct (i.e., select a
higher zone temperature than required).
The temperature in each passenger zone may be adjusted (+/- 10 degrees F within
the limits of 65 to 85 degrees F; +/- 6 degrees C within the limits of 18 to 29
degrees C) using the UP/DOWN ARROW switches. For example, if the cabin
master temperature is set to 70 degrees F (21 degrees C):
• the passenger zone temperature may be increased by a maximum of 10
degrees F (6 degrees C) to 80 degrees F (27 degrees C) (maximum system
selectable temperature), or
• the passenger zone temperature may be decreased a maximum of 5
degrees F (3 degrees C) to 65 degrees F (18 degrees C) (minimum system
selectable temperature).
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Temperature
Copyright © The Boeing Company. See title page for details.
2A.25.6 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Water/Waste Tank Section 30
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.1
2A.30 Cabin Management System-Water/Waste Tank
Water/Waste Tank Status Menu
The Water/Waste Tank Status Menu displays three selections:
• LAVATORY/WASTE TANK STATUS - allows the cabin crew to monitor
waste tank quantities. The display also shows which lavatories are
connected to which waste tank, and the status of the lavatories (such as
OCCUPIED, VACANT, or INOP)
• LAVATORY INOPERABLE CONTROL - allows the cabin crew to check
the status (OP or INOP) of an individual lavatory and, if necessary, to
illuminate the INOP sign for individual lavatories.
• POTABLE WATER STATUS - allows the cabin crew to monitor the
quantity in the potable water tanks.
MENU
MAIN
WATER/WASTE TANK STATUS MENU
LAVATORY/WASTE TANK STATUS
LAVATORY INOPERABLE CONTROL
POTABLE WATER STATUS
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Water/Waste Tank
Copyright © The Boeing Company. See title page for details.
2A.30.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatories
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.3
2A.30 Cabin Management System-Lavatories
Lavatory/Waste Tank Status Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 PREVIOUS MENU
Push - returns to the Water/Waste Tank Status Menu.
3 Quantity Indicator
Displays the current waste tank quantities:
• green – tank is up to 1/4 full
• amber – tank is between 1/4 full and 3/4 full
• red – tank is between 3/4 full and full
4 LAVATORIES
Displays which lavatories are connected to which waste tank.
Displays individual lavatory status:
• VACANT
• OCCUPIED
• INOP
1/8 1/4 3/8 1/2 5/8 3/4 7/8 F E
1/8 1/4 3/8 1/2 5/8 3/4 7/8 F E
1/8 1/4 3/8 1/2 5/8 3/4 7/8 F E
WASTE TANK 3
WASTE TANK 2
WASTE TANK 1
LAV J INOP
LAV G INOP
LAV D INOP
LAV H VACANT
LAV E VACANT
LAV A OCCUPIED
LAV B VACANT
LAV K INOP
LAV F VACANT
LAV C OCCUPIED
LAVATORIES
LAVATORIES
LAVATORIES
LAVATORY/WASTE TANK STATUS
MAIN
MENU
PREVIOUS
MENU
2 1
3 4
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatories
Copyright © The Boeing Company. See title page for details.
2A.30.4 D611W302-TBC (200 GenFam)
Lavatory/Waste Tank Status Overview
The Lavatory/Waste Tank Status display shows:
• lavatory condition (VACANT, OCCUPIED or INOP)
• which lavatories are associated with each waste tank
• each waste tank quantity level
To monitor lavatory/waste tank status observe the Lavatory/Waste Tank Status
display.
Note: When the waste tank is full, 2 LO/HI chimes sound.
Things to Remember
The WASTE TANK FULL alert message appears when a waste tank is full.
Each time a toilet is flushed, the waste tank quantity bar on the Lavatory/Waste
Tank Status screen increases to the right and could remain there for as long as 50
seconds.
Note: If a waste tank is more than half full and a toilet is flushed, it is possible
that the WASTE TANK FULL alert message may display. Pushing the
Waste Tank Status button on the window will display the Waste Tank
Status Screen. If the quantity bar has not decreased to the left, monitor the
screen for approximately 1 minute. If the waste tank remains full, placard
the affected lavatories inoperable.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatory Inoperable
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.5
2A.30 Cabin Management System-Lavatory Inoperable
Lavatory Inoperable Control Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 PREVIOUS MENU
Push - returns to the Water/Waste Tank Status Menu.
LAVATORY WASTE TANK STATUS
2
3
2
FWD DR 1R
FWD DR 1L
FWD DR 1 CTR
FWD DR 2R
AFT DR 2R
1
1
LAVATORY INOPERABLE CONTROL
MAIN
MENU
PREVIOUS
MENU
INOP
INOP
INOP
INOP
INOP
TANK
FULL
OP
OP
TANK
FULL
OP
2 3
4 5
6
1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatory Inoperable
Copyright © The Boeing Company. See title page for details.
2A.30.6 D611W302-TBC (200 GenFam)
3 STATUS Switches
Displays the active status of the lavatories as INOP, OP, or FULL TANK.
Inoperative (INOP)
Illuminated (green) -
• Illuminates automatically when the associated waste tank becomes full.
Push -
• The INOP light at the associated lavatory illuminates and the INOP
switch on the status display illuminates.
• Can be selected manually if a lavatory is broken.
Operable (OP)
Illuminated (green) -
• The OP switch is visible and illuminates green when the associated
lavatory is operable.
Push -
• The OP switch can be selected manually if a lavatory is returned to an
operable status.
FULL TANK
Illuminated (green) -
• Illuminates automatically when the associated waste tank becomes full.
The FULL TANK switch cannot be selected manually.
4 UP/DOWN ARROWS
Push - scroll through all of the lavatories.
5 WASTE TANK
Displays which lavatory is associated to which waste tank.
6 LAVATORY
Displays the lavatory description.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatory Inoperable
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.7
Lavatory Inoperable Control
The Lavatory Inoperable Control display shows the first 5 lavatory locations.
Note: Only 5 lavatories can be displayed at one time. Use the UP/DOWN arrow
switches to scroll through the display.
• the waste tank associated with each lavatory
• the appropriate status (INOP, OP, or FULL TANK) of the associated
lavatories.
Note: Status is indicated by the green switch.
To disable a lavatory:
• use the UP/DOWN arrow switches to scroll to the desired lavatory
• push the INOP switch
• the OP switch extinguishes and the INOP switch illuminates
• the INOP light at the associated lavatory illuminates.
Things to Remember
FULL TANK status can not be changed.
When the FULL TANK light is illuminated, the INOP switch automatically
illuminates.
If the OP switch is illuminated, the INOP switch is extinguished.
If the INOP switch is illuminated manually, the OP switch extinguishes.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Lavatory Inoperable
Copyright © The Boeing Company. See title page for details.
2A.30.8 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Potable Water
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.9
2A.30 Cabin Management System-Potable Water
Potable Water Status Display
1/4 7/8 3/4 5/8 1/2 3/8 1/8 E F
GALLONS REQUIRED FOR TAKEOFF
GALLONS REMAINING
POTABLE WATER STATUS
MAIN PREVIOUS
164
200
MENU MENU
2 1
3
4
5
1/4 7/8 3/4 5/8 1/2 3/8 1/8 E F
LITERS REQUIRED FOR TAKEOFF
LITERS REMAINING
619
757
POTABLE WATER STATUS
MAIN PREVIOUS
MENU MENU
2 1
3
4
5
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Potable Water
Copyright © The Boeing Company. See title page for details.
2A.30.10 D611W302-TBC (200 GenFam)
1 MAIN MENU
Push - returns to the MAIN MENU.
2 PREVIOUS MENU
Push - returns to the Water/Waste Tank Status Menu.
3 Quantity Indicator
Displays the water quantity.
4 GALLONS (LITERS) REMAINING
Displays the gallons (liters) of water remaining.
5 GALLONS (LITERS) REQUIRED FOR TAKEOFF
Displays the gallons (liters) of water required for takeoff.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Potable Water
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.30.11
Potable Water System
Galley water is supplied from two potable water tanks. The tanks have a combined
usable capacity of approximately 825 liters (218 gallons). Water is not available
while the tanks are being serviced.
Potable Water Status
This Potable Water Status display is available at the CSCP and the CACPs.
The Potable Water Status display shows:
• the number of gallons (liters) of water remaining
• the number of gallons (liters) of water required for takeoff
It is also used to verify that the water required for takeoff is available.
The bar is displayed:
• green when the tanks are more than 1/2 full
• amber when the tanks are between 1/4 full and 1/2 full
• red when the tanks are less than 1/4 full
Use the Potable Water Status display during flight to monitor the water quantity
remaining.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Potable Water
Copyright © The Boeing Company. See title page for details.
2A.30.12 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Passenger Address Section 35
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.35.1
2A.35 Cabin Management System-Passenger Address
Passenger Address Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 Segmented Bar
Segment illuminated (green) - corresponds to the selected area description.
The number of segments in the bar correspond to the number of areas controlled
by the CSCP/CACP.
When ALL AREAS is selected, all segments of the segment bar illuminate.
3 Left/Right Arrow Switches
Push - displays the desired area/zone.
2
STEPS ABOVE
MINIMUM
PASSENGER ADDRESS MENU
MAIN
FIRST CLASS
VOLUME
AREA
RESET
ON
OFF
ANS
APPLIES TO
ENTIRE AIRPLANE
6
5
3
8
4
9
7
2
1
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Passenger Address
Copyright © The Boeing Company. See title page for details.
2A.35.2 D611W302-TBC (200 GenFam)
4 Area Description
Displays the selected area:
• FIRST CLASS
• BUSINESS CLASS
• ECONOMY CLASS
• ALL AREAS
5 STEPS ABOVE MINIMUM
Displays the number of steps that the volume was increased (1 - 16) above the
minimum level.
6 AMBIENT NOISE SENSOR (ANS)
When this switch is ON, the volume automatically adjusts to compensate for
different noise levels.
7 AREA RESET
Push - resets the volume to the default level.
8 VOLUME Control
Push -
• left arrow switch to decrease the volume 1 level
• right arrow switch to increase the volume 1 level
9 Audio Volume Indicator
Illuminated (green) -
• number of illuminated segments shows the volume level above the preset
minimum PA volume level
• the next right segment illuminates green with each push of the right
volume control arrow switch
• one segment extinguishes with each push of the left volume control arrow
switch
Note: If all of the segments are illuminated, pushing the right arrow switch does
not increase the PA volume. The volume cannot be decreased to lower than
the preset minimum PA volume level (all of the segments extinguished).
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Passenger Address
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.35.3
Passenger Address Operations
The Passenger Address display shows:
• the default area in the area description display
• the current volume level
• the Ambient Noise Sensor (ANS) active state
The Passenger Address display is used to increase or decrease the passenger
address volume.
Increase/Decrease PA Volume
To use the Passenger Address display:
• push the left/right arrow switches to select the desired area/zone
• adjust volume, if necessary
• ANS is displayed
Reset PA Volume
To reset the volume to the default level:
• push the left/right arrow switches to select the desired area/zone
• push the AREA RESET switch
• the illuminated bar graph segments extinguish
• the number in the STEPS ABOVE MINIMUM display returns to 0
Panel Selections
CSCP 1L, CACP 2L, CACP 4R -
• FIRST CLASS, BUSINESS CLASS, ECONOMY CLASS, and
ALL AREAS
Things to Remember
STEPS ABOVE MINIMUM display:
• When pushing the right arrow (increase) switch in the VOLUME display,
the number in the display increases by one, to a maximum of 16.
• When pushing the left arrow (decrease) switch in the VOLUME display,
the number in the display decreases by one, to minimum of 0.
AREA RESET - pushing the AREA RESET switch causes:
• all bar graph segments to extinguish
• the STEPS ABOVE MINIMUM display to display 0
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Passenger Address
Copyright © The Boeing Company. See title page for details.
2A.35.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Cabin Door Status Section 40
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.40.1
2A.40 Cabin Management System-Cabin Door Status
Cabin Door Status Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 Door Status
LOCKED -
Green – door is closed and the door handle in the latched position.
NOT LOCKED -
Red – door is open, or the door is closed but the door handle is not in the latched
position.
Cabin Door Status Display
The Cabin Door Status display shows each door identified and labeled as
LOCKED or NOT LOCKED.
Note: This display does not depict the ARMED/DISARMED status of the doors.
CABIN DOOR STATUS
MAIN
MENU
LOCKED
LOCKED
LOCKED
LOCKED
LOCKED LOCKED
NOT LOCKED
NOT LOCKED
2L 3L
4L
4R
3R 2R
1R
1L
1 2
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Cabin Door Status
Copyright © The Boeing Company. See title page for details.
2A.40.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Display Control Section 45
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.45.1
2A.45 Cabin Management System-Display Control
Display Controls Menu
The DISPLAY CONTROLS Menu is available at the CSCP and CACPs.
1 MAIN MENU
Push - returns to the MAIN MENU.
2 PANEL DIMMING
DIM - makes the CSCP/CACP display dimmer.
BRIGHT - makes the CSCP/CACP display brighter.
3 PANEL LOCKOUT
Push - freezes the display for 30 seconds to allow for cleaning or adjusting.
A timer appears in the PANEL LOCKOUT switch and counts down from 30 to 1.
PANEL LOCKOUT
PANEL DIMMING
DISPLAY CONTROLS MENU
MAIN
DIM BRIGHT
3
1
2
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Display Control
Copyright © The Boeing Company. See title page for details.
2A.45.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Smoking Assignments Section 50
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.50.1
2A.50 Cabin Management System-Smoking Assignments
Smoking Assignments
Smoking Assigments Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 Segmented Bar
Illuminated - shows the selected area description.
3 Left/Right Arrow Switches
Push - displays the desired area/zone.
SMOKING SEATS
END
44
BEGIN
RIGHT CENTER LEFT
SMOKING
NO
SMOKING RESET
AREA
SMOKING ROW SELECT
SEAT COLUMN SELECT
MAIN
MENU SMOKING ASSIGNMENTS
50
48 ABCDFGHIL
Economy Smoking ( Rows 44 thru 50 )
50 HIL
49 ABCDFGHIL
3
1 2
10
4
5
11
6 7 8 9
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Smoking Assignments
Copyright © The Boeing Company. See title page for details.
2A.50.2 D611W302-TBC (200 GenFam)
4 Area Description
Displays the selected area.
• Economy Smoking ( Rows 14 thru 34 )
• Economy Smoking ( Rows 36 thru 43 )
• Economy Smoking ( Rows 44 thru 50 ).
5 Up/Down Arrow Switches
Use up/down arrows to scroll through list.
6 AREA RESET
Push - returns the smoking seat assignments to the original configuration.
7 SMOKING SEATS
Displays the seats with smoking privileges in row/seat order.
8 NO SMOKING
Push - makes selected seats no smoking seats.
9 SMOKING
Push - makes selected seats smoking seats.
10 SEAT COLUMN SELECT
Push - selects the left, center, or right seats for the row number(s) displayed in the
Smoking Row Select display.
11 SMOKING ROW SELECT
Displays the begin and end row number for the controlled area.
Push the up/down arrows to change row numbers
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Smoking Assignments
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.50.3
Smoking Assignments Operations
The Smoking Assignments display shows:
• the default area in the area description display
• the begin and end row numbers for the selected area
• the seats with smoking privileges for the selected area.
To add more smoking seats:
• push the left/right arrow switches to select the desired area/zone
• select the desired begin and end row numbers for the new smoking seats
• select the desired seat column (left, right, or center)
• push the smoking switch
• the selected smoking seats are shown in the Smoking Seats display.
To delete smoking seats:
• push the left/right arrow switches to select the desired area/zone
• select the desired begin and end row numbers for the new no smoking
seats
• select the desired seat column (left, right, or center)
• push the no smoking switch
• the selected no smoking seats are deleted from the Smoking Seats display.
To reset a smoking area to its original configuration:
• push the left/right arrow switches to select the desired area/zone
• push the Area Reset switch
• the applicable seats are deleted from or added to the Smoking Seats
display.
Seat Configuration
The following seats are configured as no smoking seats and the no smoking
indicator on the PCU will be illuminated:
• Economy Smoking ( Rows 14 thru 34 )
• Economy Smoking ( Rows 36 thru 43)
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Smoking Assignments
Copyright © The Boeing Company. See title page for details.
2A.50.4 D611W302-TBC (200 GenFam)
Panel Selections
CSCP 1L, CACP 2L, CACP 4R -
• Economy Smoking ( Rows 14 thru 34 ),
Economy Smoking ( Rows 36 thru 43 ), and
Economy Smoking ( Rows 44 thru 50 ).
Things to Remember
There must be a begin and end row number before seat columns (left, center, or
right) can be selected, or a window appears to indicate a selection is required.
Pushing the Smoking switch when no seat columns have seen selected (left,
center, or right) for a row automatically selects all of the seats in that row.
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Boarding Music Section 51
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.51.1
2A.51 Cabin Management System-Boarding Music
Boarding Music Display
1 MAIN MENU
Push - returns to the MAIN MENU.
2 ON
Push - (illuminated green) turns the Boarding Music power ON.
3 OFF
Push - (illuminated green) turns the Boarding Music power OFF.
4 CHANNEL switches
Push - (illuminated green) selects desired channel.
5 VOLUME
Displays the volume incrementally.
4 2 3
BOARDING MUSIC MENU
MAIN
ON OFF
VOLUME
CHANNEL
1
MACHINE #1
4 2 3
ON OFF
VOLUME
CHANNEL
1
MACHINE #2
1
6
4
5
2 3
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Boarding Music
Copyright © The Boeing Company. See title page for details.
2A.51.2 D611W302-TBC (200 GenFam)
6 LEFT/RIGHT ARROW switches
Push - increases or decreases volume.
Boarding Music Operation
The Boarding Music display shows:
• the selected Channel
• the desired Volume
To turn Boarding Music on:
• push the ON switch
• push the desired CHANNEL switch
• the selected CHANNEL switch illuminates
To increase or decrease the volume:
• push the appropriate left/right arrow switch
• the bar graph display increases incrementally to the right, or decreases
incrementally to the left, depending on which arrow switch was pushed
Note: One push of an arrow switch causes one increment on the bar graph display
to illuminate or extinguish, depending on which arrow switch was pushed.
Things to Remember
If the Boarding Music power has been turned OFF and the Boarding Music
display is selected, its default values are:
• power: OFF
• Channel: 1
• volume: midrange.
February 14, 2003
Flight Attendant Manual
Cabin Management System Chapter 2A
Non-Normal Operations Section 60
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.1
[Options shown: Flight Crew Rest (FCR): installed; Lower Crew Rest (LCR),
Overhead Flight Crew Rest (OFCR); Overhead Flight Attendant Rest (OFAR):
installed;
Options: Main Deck Crew Rest (MDCR), Main Deck Flight Crew Rest
(MDFCR)]
2A.60 Cabin Management System-Non-Normal Operations
Alert Messages
Alert messages appear in windows on the CSCP and the CACPs. Alert messages
require crew action. If more than one Alert Message window is activated at the
same time, the windows are overlaid; the window with the highest priority
remains in front, with the other windows layered behind it.
Alert Message priority is shown below:
• Smoke Detection
• Waste Tank Full
• Potable Water Status.
• Cabin Interphone Failure
• Passenger Address Failure
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.2 D611W302-TBC (200 GenFam)
Smoke Detection
Lavatory SMOKE DETECTED
The SMOKE DETECTED window appears if lavatory smoke is detected. A
maximum of four smoke detector alarms can be displayed in the window, with the
most recently activated smoke detector listed first. The window displays the
message SMOKE DETECTED and the location of the associated lavatory(ies) or
crew rest area. Pushing the CLEAR switch removes the window. The message
SMOKE DETECTED is displayed in small red text in the bottom left hand side of
all displays. The message is displayed until the Lavatory Call Indicator/Reset
switch is pushed.
Lavatory smoke detector activation is annunciated by a continuous HI chime and
a flashing master call light.
CLEAR
LAV 2F-1R
SMOKE DETECTED
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.3
Crew Rest SMOKE DETECTED
Crew rest area smoke detection is annunciated in the same manner as lavatory
smoke detection, except:
• a flight crew rest smoke detector is annunciated as FLT CREW RST
Crew rest smoke detector activation is annunciated by a continuous HI chime and
a flashing master call light.
CLEAR
FLT CREW RST
SMOKE DETECTED
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.4 D611W302-TBC (200 GenFam)
Cabin Temperature
ECS No Communication
This window is displayed if the CABIN TEMPERATURE display is selected and
the Environmental Control System (ECS) is not communicating with the cabin
management system.
CABIN TEMPERATURE LOCKOUT
ECS No Communication
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.5
Water/Waste Tank
WASTE TANK FULL
The WASTE TANK FULL window appears when the waste level is 1 inch below
the shut off point of the sensors.
Pushing the Waste Tank Status switch displays the LAVATORY/WASTE TANK
STATUS display. Using the status display information, placard the appropriate
lavatories as INOPERATIVE.
When the waste tank is full, a single LO/HI chime sounds.
WASTE
STATUS
TANK
WASTE TANK FULL
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.6 D611W302-TBC (200 GenFam)
LOW POTABLE WATER
The LOW POTABLE WATER window appears when only 1/4 tank of potable
water remains.
Pushing the CLEAR switch removes the window from the display.
CLEAR
POTABLE WATER LEVEL AT 1/4
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.7
Communications
CABIN INTERPHONE FAILURE
The Cabin Interphone Failure window alert message is displayed if the cabin
interphone controller fails.
The window directs the flight attendant to press the CI NORM/ALT switch,
located on the door 1L Attendant Switch Panel.
Pressing the clear switch removes the window from all displays and displays the
message CABIN INTERPHONE FAILURE. Press CI NORM/ALT Switch in
small red text in the bottom left corner of all displays.
Note: The text remains displayed until the CI NORM/ALT switch is pushed.
CLEAR
CABIN INTERPHONE FAILURE
Press CI NORM/ALT Switch
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.8 D611W302-TBC (200 GenFam)
PASSENGER ADDRESS FAILURE
The Passenger Address Failure window appears if the passenger address
controller fails.
The window displays the message Passenger Address Failure and directs the flight
attendant to press the PA NORM/ALT switch, located on the door 1L Attendant
Switch Panel.
Pressing the clear switch removes the window from all displays and displays the
message PASSENGER ADDRESS FAILURE. Press PA NORM/ALT Switch in
small red text in the bottom left corner of all displays.
Note: The text remains displayed until the PA NORM/ALT switch is pushed.
CLEAR
PASSENGER INTERPHONE FAILURE
Press PA NORM/ALT Switch
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.9
FUNCTION LOCK-OUT Messages
Function Lock-out Messages are associated with certain displays. Function
Lock-out Message windows only appear when the associated display is displayed.
The message FUNCTION LOCK-OUT appears above the reason for the lock-out.
Functions on the affected display cannot be selected as long as the lock-out
remains in effect.
Decompression
The FUNCTION LOCK-OUT Decompression window appears during a cabin
decompression if one of the following displays is selected:
• Cabin Lighting
• Entry Way Lights
The window is removed when the decompression condition no longer exists.
Return to the CABIN CONTROLS MAIN MENU by pushing the MAIN MENU
switch.
Note: A cabin decompression is annunciated by five HI chimes.
FUNCTION LOCKOUT
Decompression
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.10 D611W302-TBC (200 GenFam)
Invalid Data
FUNCTION LOCK-OUT Invalid Data is displayed when the Cabin Door Status,
Potable Water Status, or Waste Tank Status display is selected and the sensor data
information is invalid/unreliable.
The window is removed when the data is valid again.
FUNCTION LOCKOUT
Invalid Data
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.11
Reduced Power
Reduced Power Condition
The REDUCED POWER CONDITION window is displayed when the
cabin/utility switch has been moved to the OFF position by the flight crew. All
night lights, reading lights, and attendant work lights will be illuminated.
Commands from the CSCP or CACP for night light operation will be inoperative.
When the flight deck cabin/utility power switch is placed in the ON position, the
REDUCED POWER CONDITION message is removed and control of the cabin
lighting is returned to the CSCP and CACPs.
Note: During normal airplane operations, the cabin/utility switch on the flight
deck is in the ON position.
Note: CSCP or CACP commands for night light operation will be inoperative
when the flight deck cabin/utility switch is placed in the OFF position by
the flight crew.
REDUCED POWER CONDITION
Fluorescent lights may be off.
Night lights are locked on.
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.12 D611W302-TBC (200 GenFam)
Error Messages
Error message windows display if the system fails to respond to a switch selection
or the user makes an incorrect selection.
NOT A VALID ENTRY Messages
Row Number/Seat Does Not Exist
A NOT A VALID ENTRY message appears on the Seat Chime Control display
for any of the following:
• entry of a number for which no row exists
• entry of a number for an existing row not controlled by the panel
• a seat is selected before a row
• selection of a row switch when the ROW/SEAT field already displays a
row number and a seat letter.
Pushing the CLEAR switch removes the window from the display.
CLEAR
NOT A VALID ENTRY
Row Number/Seat Does Not Exist
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 2A.60.13
Row Not Controlled By This Panel
This window appears when a row number is entered from the Seat Chime Control
display for a row not controlled by that panel.
Pushing the CLEAR switch removes the window from the display.
CLEAR
NOT A VALID ENTRY
Row Not Controlled By This Panel
February 14, 2003
Flight Attendant Manual
Cabin Management System -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
2A.60.14 D611W302-TBC (200 GenFam)
Miscellaneous Messages
ENTRY OUT OF SEQUENCE
The ENTRY OUT OF SEQUENCE Select Row Before Seats window appears
when a seat letter is selected from the Seat Chime Control display before a row
number is entered.
Pushing the CLEAR switch removes the window from the display.
CLEAR
Select Row Before Seats
ENTRY OUT OF SEQUENCE
February 14, 2003
Flight Attendant Manual
Lighting Chapter 3
System Description Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 3.TOC.0.1
3.0 Lighting-System Description
System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1
Lighting Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1
Cabin Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1
Closet Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1
Galley Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.1
Lavatory Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2
Reading Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2
Work Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.2
Emergency Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.3
Emergency Lights - Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.4
Flashlights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.5
Emergency Lights - Exterior. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.10.6
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.20.1
Lighting Non-normals. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.20.1
Replacing a Burned Out Lamp . . . . . . . . . . . . . . . . . . . . . . . . 3.20.1
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
3.TOC.0.2 D611W302-TBC (200 GenFam)
Lighting -
System Description
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Lighting Chapter 3
System Description Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 3.10.1
3.10 Lighting-System Description
Lighting Overview
This chapter provides a description of cabin lighting, and interior and exterior
emergency lighting.
Cabin Lighting
Cabin lighting is provided by white incandescent and fluorescent lights. General
cabin illumination includes ceiling, entry way, and night lights. These are
supplemented by reading, lavatory, work, galley, and closet lights.
All cabin lighting is controlled by the cabin management system (CMS) using the
Lighting Menu.
Note: During normal airplane operations, the cabin/utility switch on the flight
deck is in the ON position. When the cabin/utility switch has been moved
to the OFF position by the flight crew, the REDUCED POWER
CONDITION window is displayed on the CSCP and CACPs, all night
lights, reading lights, and attendant work lights will be illuminated.
Commands from the CSCP or CACP for night light operation will be
inoperative.
When the flight deck cabin/utility power switch is returned to the ON
position, the REDUCED POWER CONDITION message is removed and
control of the cabin lighting is returned to the CSCP and CACPs.
If cabin decompression occurs, all fluorescent ceiling lights illuminate, overriding
the cabin management system lighting controls.
If all main electrical power is lost, the night and supplementary night lights are
automatically turned on.
Closet Lights
A light is provided in each coat closet when normal cabin lighting provides
insufficient illumination.
Galley Lights
The lighting in each galley is controlled by a three-position switch within the
galley. The switch positions are bright, dim, and off.
February 14, 2003
Flight Attendant Manual
Lighting -
System Description
Copyright © The Boeing Company. See title page for details.
3.10.2 D611W302-TBC (200 GenFam)
Lavatory Lights
Lavatories are illuminated by fluorescent lighting. With the airplane on the ground
and the ground service bus powered, the lights illuminate bright regardless of the
door position. In flight, the lights illuminate dim when the door is unlocked and
bright when the door is locked.
Reading Lights
The reading lights are located in the passenger service unit (PSU) and provide
light from above the passenger seats. They can be operated from the passenger
control unit (PCU) or the cabin management system.
Work Lights
1 WORK LIGHT Switch
Turns work light on (illuminated green) or off.
Each flight attendant station is provided with a work light. The lights are
controlled by the WORK LIGHT switches on the attendant switch panel (ASP)
located at each station.
LIGHT 2 LIGHT 1
WORK
WORK
LIGHT 3
WORK
Attendant Switch Panel (typical)
1
February 14, 2003
Flight Attendant Manual
Lighting -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 3.10.3
Emergency Lighting
[Option shown: Door 1L/4R (777-200/777-200ER), 1L/5R
(777-300/777-300ER);
Option: Door 2L/4R (777-200/777-200ER), 2L/5R (777-300/777-300ER)]
The emergency lighting system provides direction to exit locations and
illuminates the egress paths inside and outside the airplane.
The system is normally controlled by a switch on the flight deck and is placed in
the ARMED position prior to flight. In this position, all interior and exterior
emergency lights illuminate automatically if there is a total loss of electrical
power. The flight crew can illuminate the emergency lights at any time by placing
the flight deck emergency lights switch to ON.
The emergency lights switch located on the attendant switch panel at door 1L can
be used to bypass the flight deck emergency lights switch and illuminate the
emergency lights regardless of the position of the flight deck switch.
1 Emergency Lights/Test (EMER LIGHTS/TST) Switch
White.
Push - all emergency lights illuminate for approximately 1 minute.
Note: EMER LIGHTS/TST switches are located at doors 1L and 4R.
2 Emergency Lights (EMER LIGHTS) Switch
Guarded, red.
ACCESSORY
JACK
SERVICE LIGHTS/TST LIGHTS
GROUND EMER EMER
Attendant Switch Panel
1 2
February 14, 2003
Flight Attendant Manual
Lighting -
System Description
Copyright © The Boeing Company. See title page for details.
3.10.4 D611W302-TBC (200 GenFam)
Push - Turns on all emergency lights.
Note: The EMERG LIGHTS switch is located at door 1L.
Emergency Lights - Interior
Exit signs and emergency area lights indicate all passenger cabin exit routes. All
emergency lights and EXIT signs are powered by remote batteries and are
controlled by the emergency lights switches.
Interior emergency lights consists of door, aisle, cross-aisle, escape path, exit
lights, and luminescent exit signs.
Escape path lighting is installed in the centerline passenger seats, spaced at
intervals in the aisles and cross-aisles. When illuminated, escape path lighting
provides visual guidance for emergency evacuation if all sources of lighting more
than four feet above the aisle floor are obscured by smoke.
Battery powered exit lights are located at each cabin exit.
EXIT EXIT
Emergency Escape Path Lights
Exit Sign
February 14, 2003
Flight Attendant Manual
Lighting -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 3.10.5
Flashlights
Flashlights are stowed throughout the airplane. These high intensity flashlights
illuminate automatically when they are removed from the stowage brackets. A
battery indicator light flashes every three to four seconds to indicate adequate
power. The light can be extinguished only by replacing the flashlight back into the
stowage bracket. The batteries cannot be recharged. See Chapter 9, Emergency
Equipment, for specific locations.
Viewport
EMERGENCY
USE ONLY Seal
Condition Light
February 14, 2003
Flight Attendant Manual
Lighting -
System Description
Copyright © The Boeing Company. See title page for details.
3.10.6 D611W302-TBC (200 GenFam)
Emergency Lights - Exterior
Exterior emergency lighting consists of escape slide lights. The lights are located
aft of each door and illuminate the areas at the base of the escape slides. The slides
in doors 2L and 2R have lights built into the sliding lanes. When the slide is
deployed, the lights turn on automatically to illuminate the slide lanes.
Door 2L
and 2R
Note: Lights in
door 2L and 2R
slides only
February 14, 2003
Flight Attendant Manual
Lighting Chapter 3
Non-Normal Operations Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 3.20.1
3.20 Lighting-Non-Normal Operations
Lighting Non-normals
Replacing a Burned Out Lamp
Remove the lens cover:
• grasp and squeeze the lens cover
• turn it counterclockwise to disconnect the tabs from the upper slots. You
should feel/hear a “click”
• remove the lens cover.
Lens Cover
Upper Slots (4)
Bulb
Tabs (4)
Passenger Service Unit (PSU) (Typical)
February 14, 2003
Flight Attendant Manual
Lighting -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
3.20.2 D611W302-TBC (200 GenFam)
Replace the bulb:
• grasp the burned out bulb, push it upwards and gently twist. The bulb will
release.
Note: Use a napkin/linen when handling reading lightbulbs. The bulb may be
very hot or burn out early if fingerprints are on the bulb.
• insert a new bulb into the socket, pushing it upwards and gently twisting,
until a ”click” is heard or felt.
Replace the lens cover:
• grasp the lens cover and line up the tabs with the upper slots and re-insert.
• turn it clockwise. A “click” should be heard or felt which indicates that
the lens cover is locked in place.
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.TOC.0.1
4.0 Communications-Table of Contents
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.10.1
Communications Overview. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.10.1
Cabin Interphone. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.1
Cabin Interphone System Overview . . . . . . . . . . . . . . . . . . . . . . . 4.20.1
Call Light Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.1
Cabin Interphone Directory and Handset . . . . . . . . . . . . . . . . . . . 4.20.2
Cabin Interphone Calls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.4
Call Types . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.20.4
Placing Cabin Interphone Calls . . . . . . . . . . . . . . . . . . . . . . . . 4.20.6
Cabin Interphone System Modes. . . . . . . . . . . . . . . . . . . . . . . 4.20.7
Passenger Address . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.1
Passenger Address System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.1
Passenger Address Priorities . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.1
Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.21.2
Passenger Address Announcements . . . . . . . . . . . . . . . . . . . . 4.21.4
Passenger Address System Modes. . . . . . . . . . . . . . . . . . . . . . 4.21.6
Passenger Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.22.1
Passenger Call System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.22.1
Lavatory Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.23.1
Lavatory Call System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.23.1
Passenger Cabin Signs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.24.1
Passenger Cabin Sign System . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.24.1
No Smoking and Fasten Seat Belt Signs . . . . . . . . . . . . . . . . . 4.24.1
Return to Seat Sign . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.24.2
Automatic Passenger Cabin Sign Operation. . . . . . . . . . . . . . . . . 4.24.2
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
4.TOC.0.2 D611W302-TBC (200 GenFam)
Communications -
Table of Contents
Takeoff and Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.24.2
Loss of cabin pressure and oxygen deployment . . . . . . . . . . 4.24.2
Inflight Entertainment System . . . . . . . . . . . . . . . . . . . . . . . . . . 4.30.1
Inflight Entertainment System Overview . . . . . . . . . . . . . . . . . . 4.30.1
PCU - All Classes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.30.2
PCU - Crew Rest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.30.3
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.40.1
Communications Non-Normal Operations . . . . . . . . . . . . . . . . . 4.40.1
Cabin Interphone System Failure. . . . . . . . . . . . . . . . . . . . . . 4.40.1
Passenger Address System Failure. . . . . . . . . . . . . . . . . . . . . 4.40.2
In-flight Entertainment (IFE) System Smoke or Fire . . . . . . 4.40.3
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Introduction Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.10.1
4.10 Communications-Introduction
Communications Overview
This chapter provides a description of the airplane communications systems used
by the flight attendants. These systems include:
• cabin interphone system
• passenger address system
• passenger call system
• lavatory call system
• passenger signs.
Also, included in this chapter is information on the inflight entertainment (IFE)
system.
February 14, 2003
Flight Attendant Manual
Communications -
Introduction
Copyright © The Boeing Company. See title page for details.
4.10.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Cabin Interphone Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.20.1
4.20 Communications-Cabin Interphone
Cabin Interphone System Overview
The cabin interphone system is a phone network with stations on the flight deck
and at the attendant stations.
There are 10 handsets in the cabin:
• 1 at each forward attendant station at doors 1L, 2L, 2R, 3L, and 3R
• 1 at each aft attendant station at doors 1R, 4L, and 4R
• 1 at the cross-aisle attendant station near door 1
• 1 at the Purser Station
The cabin interphone system can be used to make:
• flight deck-to-attendant calls
• attendant-to-flight deck calls
• attendant-to-attendant calls
• passenger address announcements
The cabin interphone handset is used to initiate and receive calls.
Call Light Panel
The pink cabin interphone crew call lights and attendant station chime
annunciations are used as call indicators at the receiving location. The cabin
interphone crew call light extinguishes when the receiving station handset is
removed from the cradle.
Cabin Interphone Crew
Call Light (pink)
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
4.20.2 D611W302-TBC (200 GenFam)
Cabin Interphone Directory and Handset
2 3
4 5 6
7 8 9
0 * #
1
Push To Talk
Passenger Address
Reset
LIFT HANDSET
** PILOT ALERT
6* CABIN READY
02
61
PURSER
LWR CREW REST
55 ALERT
54 ATT ALL CALL
4* PA ALL PRIORITY
44
43
42
PA LWR REST
PA ECONOMY
PA BUSINESS
40 PA ALL
PILOT 24
DOOR 4 RIGHT 24
DOOR 3 RIGHT
DOOR 2 RIGHT
DOOR 1 RIGHT
23
22
21
01 DOOR 1 CENTER
14 DOOR 4 LEFT
13 DOOR 3 LEFT
12 DOOR 2 LEFT
DOOR 1 LEFT 11
1 2
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.20.3
1 Dial Buttons
Push - Enter the two digit dial code for the desired area.
2 Reset Switch
Momentary switch.
Push - ends the call.
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
4.20.4 D611W302-TBC (200 GenFam)
Cabin Interphone Calls
Cabin interphone calls are initiated by removing the handset from the handset
cradle (dial tone is heard) and dialing the two-digit code for the desired location
or type of call. The calling station hears a ring signal until the handset is picked
up. If the called station is already in use, the caller receives a normal busy signal.
If the caller has dialed a non-existent two-digit code, or is dropped from a call
already in progress, the caller receives a rapid busy signal.
When an attendant station receives a call, the passenger address system (PAS)
sounds a chime, and the pink station cabin interphone crew call light illuminates.
Call Types
Pilot Alert
PILOT ALERT is used to notify the flight crew about an emergency. The pilot
alert call is not inhibited at any time.
The dial code for PILOT ALERT, ** on the handset:
• annunciates the call on the flight deck by sounding a single HI/LO chime
• causes a CABIN ALERT message to appear on the EICAS display on the
flight deck
Note: Pilot alert calls take priority over all other calls to the flight deck. A lower
priority call in progress is automatically disconnected. If more than one
pilot alert call is initiated, all applicable callers are connected via a party
line.
Pilot
A normal two way call to the flight deck may be made by any station. Dialing the
PILOT two digit code, 24:
• annunciates the call on the flight deck by sounding a single HI/LO chime
• causes a CABIN CALL message to appear on the EICAS display on the
flight deck
All Call (ALERT)
The all call selection is includes all flight attendant stations and the flight deck.
Dialing 55, the two digit code for ALERT:
• annunciates the call by three HI/LO chimes and a flashing master call at
all stations light
• connects each handset to the call as it is removed from the handset cradle
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.20.5
Attendant All Call (ALL ATTND)
Dialing the two digit code for attendant all call (ALL ATTND), 54, functions the
same as an ALL CALL but does not include the flight deck. ALL ATTND calls:
• are annunciated by a single HI/LO chime and a flashing master call light
• connects each handset to the call as it is removed from the handset cradle
Cabin Ready
Cabin Ready is used to notify the flight crew that the cabin is secured and ready
for taxi.
Dialing 6*, CABIN READY, on the handset:
• causes the CABIN READY message to appear on the EICAS display on
the flight deck.
• sounds a single HI/LO chime on the flight deck
• caller hears a rapid beep-beep and then a dial tone
Pilot-to-Attendant
Pilot-to-attendant are normal two-way calls initiated by the flight crew.
Pilot-to-attendant calls:
• are annunciated by two HI/LO chimes and a steady master call light
Once a pilot-to-attendant call is made, one or two more stations may be added to
the connection.
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
4.20.6 D611W302-TBC (200 GenFam)
Station-to-Station
Station-to-station calls are normal two-way calls; for example, attendant to
attendant. Any station can make a call to any other station using the two digit dial
code.
Station-to-station calls:
• are annunciated by a single HI/LO chime and a steady master call light
Once a station-to-station call is made, one or two more stations may be added to
the connection.
Placing Cabin Interphone Calls
To place a cabin interphone call:
• remove handset from the cradle (listen for dial tone)
• enter the two digit code for the desired station
When the call is completed:
• push the Reset switch, or
• return the handset to cradle
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.20.7
Cabin Interphone System Modes
1 Cabin Interphone Normal/Alternate (CI NORM/ALT) Switch
Normal Mode (light bar not visible) – normal system operation
Alternate Mode (push, light bar illuminated green) –
• switches cabin interphone system to alternate mode
• clears CABIN INTERPHONE FAILURE message from CSCP and
CACPs
Note: CI NORM/ALT switch located at door 1L only.
The cabin interphone system has two modes: normal and alternate. Pushing the CI
NORM/ALT switch, located on the door 1L flight attendant panel, places the
cabin interphone system in the alternate mode.
If the system fails in the normal mode, the cabin management services failure
message CABIN INTERPHONE FAILURE Press CI NORM/ALT Switch is
displayed on the CSCP and at each CACP.
SERVICE
GROUND
NORM/ALT NORM/ALT LIGHT 2
CI PA WORK
Attendant Switch Panel
1
February 14, 2003
Flight Attendant Manual
Communications -
Cabin Interphone
Copyright © The Boeing Company. See title page for details.
4.20.8 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Passenger Address Section 21
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.21.1
4.21 Communications-Passenger Address
Passenger Address System
The passenger address (PA) system is used for making flight deck, attendant, and
prerecorded announcements to the passenger cabin. Entertainment audio and
boarding music can also be sent through the PA system. Flight attendants can
make PA announcements using the cabin interphone handsets. Those
announcements can be sent through the cabin interphone system or directly to all
cabin areas using the Direct Access switch located on the interphone handset
cradle. The handset cradles located at doors 1L and 3L have Direct Access
switches.
Passenger address announcements are made by selecting the desired area on the
handset and pushing the Push-to-Talk switch on the handset. Direct access
announcements are initiated by pushing the PA switch on the handset cradle.
Passenger Address Priorities
Passenger address announcements are prioritized in the following order:
• flight deck
• direct access
• priority announcements
• normal announcements
• pre-recorded announcements
• video system audio
• boarding music
A higher priority announcement overrides a lower priority announcement. When
the cabin interphone system is used to make PA announcements and a higher
priority announcement is initiated, the cabin interphone system resets and a dial
tone is heard in the handset.
There is a flight deck indication when the PA system is in use in the passenger
cabin.
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Address
Copyright © The Boeing Company. See title page for details.
4.21.2 D611W302-TBC (200 GenFam)
Handset
2 3
4 5 6
7 8 9
0 * #
1
Push To Talk
Passenger Address
Reset
PA
Handset Cradle Handset
1 2 3
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Address
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.21.3
1 Direct Access Switch
Push -
• makes a PA to passenger cabin
• announcement sent to all areas of cabin
• overrides all PA announcements except for flight deck announcements
Note: Direct Access switch located at door 1L and door 3L only.
2 Push-to-Talk Switch (PTT)
Push - connects the handset microphone to a selected PA area.
3 Reset Switch
Momentary switch.
Push - ends the PA announcement.
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Address
Copyright © The Boeing Company. See title page for details.
4.21.4 D611W302-TBC (200 GenFam)
Passenger Address Announcements
Direct Access Announcements
Direct access announcements can be initiated only at interphone handsets with a
direct access switch, located at doors 1L and 3L. Direct access announcements are
sent to all areas of the passenger cabin and override all PA announcements except
an announcement from the flight deck.
To initiate a direct access announcement:
• remove handset from the cradle (listen for dial tone)
• push the Direct Access switch located on the cradle
• push and hold the handset Push-to-Talk switch
• make the announcement
• push the Direct Access switch to disconnect and reset the system
Note: If a flight deck announcement is in progress, the caller receives a busy
signal.
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Address
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.21.5
Priority Announcements
A priority announcement overrides all other PA announcements being made
through the cabin interphone system, except for the flight deck and direct access
announcements.
To make a priority announcement:
• remove handset from the cradle (listen for dial tone)
• enter the two digit PA priority announcement code (PA PRIORITY), 47
• push the handset PTT switch
• make the announcement
• push the Reset switch
Note: If a flight deck, direct access or another PA priority announcement is in
progress, the caller receives a busy signal.
Normal Announcements
To make an announcement:
• remove handset from the cradle (listen for dial tone)
• enter the two digit code for the desired PA area:
• 41, PA FIRST CLASS for first class
• 42, PA BUSINESS CLASS, for business class
• 43, PA ECONOMY CLASS, for all economy class
• 46, PA ALL, for all areas
• push and hold the handset Push-to-Talk switch
• make the announcement
• push the Reset switch
Note: If a flight deck, direct access, or a priority announcement is in progress, the
caller receives a busy signal.
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Address
Copyright © The Boeing Company. See title page for details.
4.21.6 D611W302-TBC (200 GenFam)
Passenger Address System Modes
1 Passenger Address Normal/Alternate (PA NORM/ALT) Switch
Normal Mode (light bar not visible) – normal system operation
Alternate Mode (push, light bar illuminated green) –
• switches passenger address system to alternate mode
• clears PASSENGER ADDRESS FAILURE message from CSCP and
CACP
Note: PA NORM/ALT switch located at door 1L only.
The passenger address system has two modes: normal and alternate. Pushing the
PA NORM/ALT switch, located on the door 1L flight attendant panel, places the
passenger address system in the alternate mode.
If the system fails in the normal mode, the cabin management system failure
message PASSENGER ADDRESS FAILURE Press PA NORM/ALT Switch
window appears on the CSCP and at each CACP.
SERVICE
GROUND
NORM/ALT NORM/ALT LIGHT 2
CI PA WORK
Attendant Switch Panel
1
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Passenger Call Section 22
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.22.1
4.22 Communications-Passenger Call
Passenger Call System
A call from the passenger seating area is made by activating the Attendant Call
switch located on the Passenger Control Unit (PCU) in each passenger seat arm
rest.
Pushing the Attendant Call switch:
• illuminates the row call light in the passenger service unit (PSU) above
the seat
• illuminates a steady blue attendant call light at the attendant station being
called, and
• sounds a single HI chime at the attendant station being called
Passenger Control Unit
Attendant
Call Switch
Attendant
Call Reset
Switch
Call Light Panel
Attendant Call Light (blue)
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Call
Copyright © The Boeing Company. See title page for details.
4.22.2 D611W302-TBC (200 GenFam)
The PSU row call light is extinguished when any Attendant Call Reset switch in
that PSU row is pushed. The blue attendant station Attendant Call light
extinguishes when all activated Attendant Call Reset switches for that area are
reset.
Note: Flight crew rest calls will be annunciated on the SERVICE CALL display
in the FIRST CLASS Active Lavatory Call display.
Passenger calls can also be verified and reset from the cabin management system
SERVICE CALL display. See Chapter 2A, Cabin Management System, Service
Calls.
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Lavatory Call Section 23
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.23.1
4.23 Communications-Lavatory Call
Lavatory Call System
A call from the lavatory is made by pushing the Attendant Call switch located on
the front side of the lavatory sink cabinet.
Pushing the Attendant Call switch:
• illuminates the switch to confirm selection
• illuminates the lavatory call light/reset switch located on the outside wall
over the door of the calling lavatory
• illuminates a steady amber lavatory call light at the attendant station being
called
• sounds a single HI chime at the attendant station being called
Note: Calls from the lower crew rest (LCR) area sound a single LO chime at the
attendant station being called.
Attendant
Call
In Lavatory
Attendant Call Switch
Call Light Panel
Attendant Call Light (amber)
February 14, 2003
Flight Attendant Manual
Communications -
Lavatory Call
Copyright © The Boeing Company. See title page for details.
4.23.2 D611W302-TBC (200 GenFam)
Note: Calls from the crew rest area sound a single HI chime at the attendant
station being called.
The lavatory call light is extinguished by pushing the lavatory call light/reset
switch over the lavatory door. The amber lavatory call light extinguishes when all
lavatory call light/reset switches for that area are reset.
Lavatory calls can also be verified and reset from the cabin management system
Service Call display. See Chapter 2A, Section 20, Service Call Display.
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Passenger Cabin Signs Section 24
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.24.1
[Options shown: No smoking signs - normal operation; Option: partial on, always
on;
Option shown: Return to seat - steady; Option: flashing]
4.24 Communications-Passenger Cabin Signs
Passenger Cabin Sign System
The passenger cabin sign system is comprised of the no smoking, fasten seat belt,
and return to seat signs. The signs are visible to all passengers and flight crew.
No Smoking and Fasten Seat Belt Signs
NO SMOKING and FASTEN SEAT BELT signs are located on the cabin
overhead and in the passenger service unit (PSU).
The passenger signs are controlled from the flight deck either manually or
automatically. On the ground, all signs are illuminated.
A single LO chime sounds over the passenger address system each time any of the
passenger signs illuminate or extinguish.
Occupied Lavatory
Cabin Overhead (Typical)
Passenger Service Unit (PSU) (Typical)
February 14, 2003
Flight Attendant Manual
Communications -
Passenger Cabin Signs
Copyright © The Boeing Company. See title page for details.
4.24.2 D611W302-TBC (200 GenFam)
On the ground, all passenger signs are illuminated.
Return to Seat Sign
A RETURN TO SEAT sign is located in each lavatory and visible only when
illuminated. The RETURN TO SEAT signs illuminate when the FASTEN SEAT
BELT signs are on.
Note: Note: The RETURN TO SEAT sign in the lavatories will not illuminate
if passenger cabin oxygen has been deployed.
Automatic Passenger Cabin Sign Operation
Takeoff and Landing
After takeoff with the passenger signs in the automatic mode, the FASTEN SEAT
BELT, NO SMOKING, and RETURN TO SEAT signs extinguish when the flaps
and landing gear are up.
During descent for landing, the FASTEN SEAT BELT and RETURN TO SEAT
signs illuminate when the airplane flaps are lowered or below 10,000 feet. The NO
SMOKING signs illuminate when the landing gear are lowered.
Loss of cabin pressure and oxygen deployment
The NO SMOKING and FASTEN SEAT BELT signs illuminate automatically if
the cabin altitude exceeds 10,000 feet or if the passenger cabin oxygen system is
manually or automatically deployed.
Note: The RETURN TO SEAT sign in the lavatories will not illuminate if
passenger cabin oxygen has been deployed.
RETURN TO SEAT
In Lavatory
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Inflight Entertainment System Section 30
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.30.1
4.30 Communications-Inflight Entertainment System
Inflight Entertainment System Overview
The inflight entertainment system (IFE) is manufactured by an outside vendor and
conforms to airline specifications. Refer to the vendor manuals for IFE equipment
and operation.
Passenger address announcements from the flight deck or a flight attendant
handset automatically override the audio entertainment program. When the
announcement is complete, the program resumes.
See the inflight entertainment vendor’s operating manuals for detailed
information.
February 14, 2003
Flight Attendant Manual
Communications -
Inflight Entertainment System
Copyright © The Boeing Company. See title page for details.
4.30.2 D611W302-TBC (200 GenFam)
PCU - All Classes
Each passenger seat contains a Passenger Control Unit (PCU). Passengers use the
PCU to select various in-flight entertainment system functions, turn the reading
lights on or off, or call for passenger service.
A headset may be plugged in to listen to the audio on the selected channel. The
PCU includes switches for channel selection and audio volume.
See vendor’s manuals for specific details and operation.
Note: PCU’s, where applicable, must be stowed during ground taxi operations,
takeoff, and landing.
Reading
Light
Control
Attendant
Call Reset
Switch
Attendant
Call Switch
Game
Controls
Game
Controls
Card
Reader
Telephone
February 14, 2003
Flight Attendant Manual
Communications -
Inflight Entertainment System
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.30.3
PCU - Crew Rest
Each crew rest bunk contains a PCU which is used to the select various in-flight
entertainment system functions, turn the reading lights on or off, or call for
service/assistance.
The PCU includes switches for channel selection, audio volume, and headset jacks
for audio.
See vendor’s manuals for specific details and operation.
C
V
O
L
L
H
A
N
E
N
Attendant Call
Reset Switch
Attendant
Call Switch
Reading Light
Control
February 14, 2003
Flight Attendant Manual
Communications -
Inflight Entertainment System
Copyright © The Boeing Company. See title page for details.
4.30.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Communications Chapter 4
Non-Normal Operations Section 40
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.40.1
4.40 Communications-Non-Normal Operations
Communications Non-Normal Operations
Cabin Interphone System Failure
When the cabin interphone system fails in the normal mode, a message is sent to
the cabin management system (CMS). The CMS failure message, CABIN
INTERPHONE FAILURE Press CI NORM/ALT Switch, is displayed on the
CSCP and at each CACP.
Pushing the CI NORM/ALT switch, located on the attendant switch panel at door
1L, will switch the cabin interphone system to the alternate mode. In the alternate
mode, the cabin interphone system operates the same as in the normal mode.
This CABIN INTERPHONE FAILURE message remains displayed until the CI
NORM/ALT switch is pushed.
Note: Pushing the failure window CLEAR switch will remove the failure
window from the display. The failure message, CABIN INTERPHONE
FAILURE Press CI NORM/ALT Switch, is displayed in small red text in
the lower left corner of all screens. The message remains displayed until
the CI NORM/ALT switch is pushed.
Attendant Switch Panel
SERVICE
GROUND
NORM/ALT NORM/ALT LIGHT 2
CI PA WORK
Cabin Interphone
NORM/ALT Switch
February 14, 2003
Flight Attendant Manual
Communications -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
4.40.2 D611W302-TBC (200 GenFam)
Passenger Address System Failure
If the system fails in the normal mode, a message is sent to the cabin management
system. The CMS failure message, PASSENGER ADDRESS FAILURE Press PA
NORM/ALT Switch, appears on the CSCP and at each CACP.
The flight attendant should push the PA NORM/ALT switch located on the
attendant switch panel at door 1L. This will remove the PASSENGER ADDRESS
FAILURE message from the panels and allows the system to operate in the
alternate mode.
Pushing the window CLEAR switch will also remove the window from the panel;
but the message, PASSENGER ADDRESS FAILURE Press PA NORM/ALT
Switch, appears at the bottom of the display. This message remains until the PA
NORM/ALT switch is pushed.
Note: Pushing the failure window CLEAR switch will remove the failure
window from the display. The failure message, PASSENGER ADDRESS
FAILURE Press CI NORM/ALT Switch, is displayed in small red text in
the lower left corner of all screens. The message remains displayed until
the PA NORM/ALT switch is pushed.
SERVICE
GROUND
NORM/ALT NORM/ALT LIGHT 2
CI PA WORK
Attendant Switch Panel
Passenger Address
NORM/ALT Switch
February 14, 2003
Flight Attendant Manual
Communications -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 4.40.3
In-flight Entertainment (IFE) System Smoke or Fire
In the event of smoke or fire caused by any of the in-flight entertainment system
(IFE) components, all electrical power should be removed from the IFE system
and passenger seats.
Immediately notify the flight deck. Request help from other crew members, as
required.
Note: Continuous communication among crew members provides information
essential for making safety-of-flight decisions.
Power is removed by moving the IFE Master Power switch, located in the Video
Control Center (VCC), to the OFF position. This removes electrical power to:
• the in-seat audio/video system equipment
• audio entertainment players
• video entertainment players
• overhead video system and displays/projectors
• in-seat video displays/audio in the passenger cabin
• in-seat video displays/audio in the crew rest areas
• integrated telephones
• the passenger control units (PCUs)
• the passenger seat
• seat motor power (as applicable)
• personal computer power outlet (as applicable)
• in-flight passenger cabin telephones
Note: If the IFE Master Power switch is placed in the OFF position, no passenger
service functions (reading lights or attendant call) are available.
Note: Moving the IFE Master Power switch to the OFF position does not cause
an EICAS message to be displayed on the flight deck.
WARNING: Once power is removed from the IFE system, do not turn the
IFE Master Power switch back on for the remainder of the
flight.
Note: The power to the passenger seats and IFE system may also be removed by
the flight crew. If the IFE/PASS SEATS power switch on the flight deck is
moved to OFF, all power to the cabin IFE and passenger seats is removed.
February 14, 2003
Flight Attendant Manual
Communications -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
4.40.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Lavatories Chapter 5
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.TOC.0.1
5.0 Lavatories-Table of Contents
System Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.1
Lavatories Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.1
Lavatory Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.2
Lavatory Description. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.5
Lavatory Layout. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.5
Lavatory Water System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.6
Water Supply Shutoff Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.8
Water Supply Isolation Valve . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.9
Lavatory Waste System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.10
Lavatory Fire Protection Systems . . . . . . . . . . . . . . . . . . . . . . . . 5.10.11
Lavatory Smoke Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.10.11
Lavatory Fire Extinguishing System . . . . . . . . . . . . . . . . . . . 5.10.12
Lavatory Temperature Indicator . . . . . . . . . . . . . . . . . . . . . . 5.10.13
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.1
Lavatory Non-Normals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.1
Toilet Does Not Flush . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.1
Toilet Flooding. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.2
Toilet Flush Valve Fails to Reset . . . . . . . . . . . . . . . . . . . . . . . 5.20.5
Waste Tanks Improperly Serviced . . . . . . . . . . . . . . . . . . . . . . 5.20.5
Water Faucet Fails to Shut Off . . . . . . . . . . . . . . . . . . . . . . . . 5.20.6
Lavatory Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.8
Bifold Door Unlocking/Locking . . . . . . . . . . . . . . . . . . . . . . . 5.20.8
Bifold Door Removal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.9
Panel Door Unlocking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.20.10
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
5.TOC.0.2 D611W302-TBC (200 GenFam)
Lavatories -
Table of Contents
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Lavatories Chapter 5
System Description Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.1
5.10 Lavatories-System Description
Lavatories Overview
This chapter provides a description of the lavatories and their locations, water and
waste systems, associated cabin management system (CMS) screens, and lavatory
smoke detection, and fire protection systems.
Lavatory controls and displays are located throughout the airplane. See Chapter
2A, Cabin Management System, Water/Waste Tank for information on the
lavatory/waste tank status and potable quantity displays and operations.
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.2 D611W302-TBC (200 GenFam)
Lavatory Locations
Lav 1A-1C
Lav 3F-1R
Lav 4F-R
Lav 2F-1R
Lav 4A-1R
H
D
D
D
D
D
Lav 4A-1L
Lav 3F-1L
Lav 3F-LC
Lav 2F-1L
Lav 2A-1L
D
D
D
D
D
H
Baby Care
Station
Disabled Passenger
H
D
Access
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.3
There are 10 lavatory compartments. Lavatories 2A-1L and 3F-1R are equipped
for handicapped passengers. Each of the lavatories contains baby care stations.
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.5
Lavatory Description
Lavatory Layout
Each lavatory contains a toilet, wash basin, mirror, necessary vanity items, and
disposal units. In addition, there is an attendant call switch, a loudspeaker for
passenger address, a RETURN TO SEAT sign, a no smoking/fasten seat belts
sign, a smoke detector/alarm, a waste compartment fire extinguishing system, a
lockable door, and an overhead compartment containing two oxygen masks.
Closing and latching the lavatory door causes the mirror light and a LAVATORY
OCCUPIED sign to illuminate.
Each toilet has a manual shutoff handle, located at the base of the toilet. If the flush
valve fails in the open position, pulling the handle shuts off the toilet vacuum flush
system.
DIAPER
Water Supply Shut
Off Valve (behind
mirror)
Manual Shut Off
Handle
Passenger Service
Unit (speaker &
oxygen)
Water Heater &
Distribution Drain
Valve (under sink)
Smoke Detector
Waste
Compartment Fire
Extinguisher
Flush Button
Baby Care
Station
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.6 D611W302-TBC (200 GenFam)
Lavatory Water System
The potable water system is supplied from two tanks located beneath the cabin
floor. Potable water is supplied to the lavatory sinks and the toilet flush system.
The two tanks have a combined usable capacity of approximately 218 gallons (825
liters).
The tanks are normally pressurized with air from the airplane bleed air system.
When bleed air pressure is not available, alternate pressurization is automatically
provided by an electrically driven air compressor.
Hot and cold water is available in the lavatories. The water heater is located below
the lavatory sink and has three selectable temperatures:
• low (approximately 105 degrees F, 40.6 degrees C)
• medium (approximately 115 degrees F, 46.1 degrees C)
• high (approximately 125 degrees F, 51.7 degrees C)
Heater Switch
Indicating Light
Water Heater
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.7
An amber indicator light located near the top of the heater is illuminated when the
power switch is on and the heater is operating normally. An ON/OFF switch is
located next to the amber light.
The amount of water remaining in the tanks, and the number of gallons required
for takeoff can be verified on the cabin management system (CMS) Potable Water
Status display.
Note: Water is not available while the tanks are being serviced.
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.8 D611W302-TBC (200 GenFam)
Water Supply Shutoff Valve
Each lavatory has a water supply shutoff valve which may be used to shut off the
lavatory water supply. The water supply shutoff valve has two positions, OFF and
ON, and is located above the sink behind the mirror. A push-button is located
against the lavatory wall, near the facial tissue dispenser. Pushing the button
upwards releases the catch and opens the mirror, allowing access to the handle.
ON
OFF
Mirror Release
Button
Note: Valve behind
mirror.
Mirror
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.9
Water Supply Isolation Valve
If there is a leak in a lavatory that cannot be eliminated by closing the water supply
shutoff valve, the water supply isolation valve is used to shut off the water. The
isolation valves are located on the panel above doors 2L and 4L. Rotate the
isolation valve “T" handle clockwise to close the valve. Closing the water supply
isolation valve at door 2L shuts off the water supply forward of door 2. Closing
the isolation valve at door 4L shuts off all water supply forward of door 4.
Note: Lavatories and galleys located aft of the closed isolation valve will still
have water available.
Water Supply
Isolation Valve
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.10 D611W302-TBC (200 GenFam)
Lavatory Waste System
Waste water from the lavatory sinks is drained overboard through drain masts.
Toilet waste is flushed into three waste holding tanks located in the bulk cargo
area.
Each waste tank holds 63 gallons (238 liters), for a total of 189 gallons (714 liters).
The waste system uses a vacuum to collect the waste material and deposit it in the
tanks. The vacuum is not required above 16,000 feet. Above 16,000 feet, the
pressure difference between the cabin and outside pressure moves the waste from
the toilets to the tanks.
Below 16,000 feet and on the ground, pushing the flush button on the toilet
activates the flush cycle. A flush cycle uses water from the potable water system,
and lasts approximately seven seconds. Once the flush button is pushed, there is
an automatic 15-second delay for a system reset before the next flush cycle can be
initiated. This delay conserves water by preventing consecutive flushes if the flush
button is repeatedly pushed.
Each waste tank system operates independently. There are two sensors attached to
the upper part of each waste tank. Both sensors must signal that the waste tank is
full before the flush module power relay de-energizes. If a sensor fails, it signals
that the tank is full. There is also a sensor in each waste tank drain line. It provides
data to the cabin management system about the amount of waste in the waste
tanks.
Waste tank quantity status can be found on the cabin management system
LAVATORY/WASTE TANK STATUS display, a sub–display of the
WATER/WASTE TANK STATUS display.
Note: Toilet blockages can occur if large objects are flushed down the toilet.
Items which commonly cause blockages are diapers, hand towels, cups,
and large quantities of toilet paper.
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.11
Lavatory Fire Protection Systems
Lavatory Smoke Detector
A smoke detector is mounted in each lavatory ceiling. When activated by either
detecting smoke or pushing the self test switch, a horn sounds in the smoke
detector and the red Alarm Indicator Light illuminates on the smoke detector.
1 Power Indicator Light
Illuminated (green) - smoke detector has power and is operating.
2 Interrupt Switch
Push - silences the horn and suppresses all alarm indications as long as the switch
is pushed.
3 Self Test Switch
Push - activates the smoke detector aural and visual alarms.
Note: The system automatically resets when the test is concluded.
4 Alarm Indicator Light
Illuminated (red) - presence of smoke has been detected.
Lavatory Smoke Detector
(typical)
1 2 3
4
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.12 D611W302-TBC (200 GenFam)
Lavatory Smoke Detector Operation
When smoke is detected in a lavatory, the amber Lavatory Call indicator
light/Reset switch, mounted on the exterior wall above the lavatory door, flashes
and a chime sounds in the cabin near the associated lavatory. The lavatory call
light at the associated lavatory flashes and the SMOKE DETECTED window is
displayed on the CSCP/CACP. The system can be reset by pushing the Lavatory
Call indicator light/Reset switch. When the Lavatory Call indicator/reset switch is
pushed:
• the lavatory master call light extinguishes
• the continuous chime is turned off
• the smoke detector horn silences
• the Lavatory Call indicator/reset switch extinguishes
• the CSCP/CACP SMOKE DETECTED window is no longer displayed
• a smoke alarm suppression cycle is initiated in the smoke detector
Note: If there is still smoke in the lavatory, the red Alarm Indicator Light on
the smoke detector remains illuminated.
• a lavatory smoke alert message is displayed on the flight deck
When the smoke clears, the red Alarm Indicator Light extinguishes, the
suppression cycle ends, and the smoke detector is sensitive to smoke again.
Continue to monitor the lavatory until the red Alarm Indicator Light extinguishes.
Note: When the smoke detector has been activated by smoke, lingering smoke in
the detector sensor may cause reactivation. Blowing air into the detector
sensor (the small screen cutout on the side of the cube extending from the
unit) may clear lingering smoke.
Lavatory Fire Extinguishing System
An automatic fire extinguishing system is located beneath the sink in each
lavatory. A fire extinguisher discharges a halon vapor through either one or both
of the heat-activated nozzles. Both nozzles discharge toward the waste disposal
container. The color of the nozzle tips change to an aluminum color if the
extinguisher has discharged.
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.10.13
Lavatory Temperature Indicator
A temperature indicator is located inside the waste compartment below each sink.
Grey dots on the indicator turn black when exposed to high temperatures. If any
dot has turned black or a nozzle tip has changed color, the extinguisher has
discharged.
CHECK THE FOUR GREY DOTS ON
TEMPERATURE INDICATOR
LOCATED ABOVE WASTE CONTAINER
IF ANY GREY DOT HAS TURNED BLACK
CHECK FOR FIRE DAMAGE
REPLACE FIRE EXTINGUISHER
REPLACE TEMPERATURE INDICATOR
TEMPERATURE INDICATOR
250 230 200 180
TEMPERATURE INDICATOR
February 14, 2003
Flight Attendant Manual
Lavatories -
System Description
Copyright © The Boeing Company. See title page for details.
5.10.14 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Lavatories Chapter 5
Non-Normal Operations Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.20.1
5.20 Lavatories-Non-Normal Operations
Lavatory Non-Normals
Toilet Does Not Flush
If one of the toilets does not flush, use the cabin management system
LAVATORY/WASTE TANK STATUS display to check the status of the waste
tank for that lavatory. If the waste tank is full, placard all lavatories connected to
the full waste tank as inoperative. If the waste tank is not full, the affected lavatory
should be placarded inoperative.
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
5.20.2 D611W302-TBC (200 GenFam)
Toilet Flooding
If a toilet floods due to the water rinse valve sticking open after flushing,
immediately flush the toilet to evacuate excess water from the toilet bowl. If the
toilet does not flush, refer to Inoperative Toilet.
If the toilet flushes, but water continues to flow into the toilet bowl, flush the toilet
once or twice more.
If the water continues flowing, use the water supply shutoff valve to shut off the
water for that lavatory.
Close the water supply shutoff valve handle located above the sink behind the
mirror.
Placard the lavatory as inoperative.
ON
OFF
Mirror Release
Button
Note: Valve behind
mirror.
Mirror
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.20.3
If the leak cannot be eliminated by turning off the water supply shutoff valve, the
isolation valve associated with that lavatory should be closed.
The water supply isolation valves are located in a panel above doors 2L and 4L.
Rotate the isolation valve “T” handle clockwise to close the valve. Closing the
valve at door 2L shuts off all water supply forward of door 2. Closing the valve at
door 4L shuts off all water supply forward of door 4.
Water Supply
Isolation Valve
EXIT
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
5.20.4 D611W302-TBC (200 GenFam)
Turn the distribution drain shutoff valve handle to the open position to drain the
water from the lavatory.
Note: Lavatories located aft of the door 4L water supply isolation valve will still
have water.
Water Heater
Distribution Drain
Shutoff Valve Handle
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.20.5
Toilet Flush Valve Fails to Reset
A loud continuous air noise or sucking noise coming from the toilet is caused by
the flush valve sticking in the open position.
Close the toilet lid and pull the manual shutoff handle located at the base of the
toilet out. This closes the flush valve and stops the noise.
Placard the lavatory as inoperative.
Waste Tanks Improperly Serviced
Verification of waste tank servicing is accomplished prior to departure/dispatch.
The waste tank quantity level on the cabin management system
LAVATORY/WASTE TANK STATUS displays should be in the first quarter (E to
1/4) and the status bar should be green.
A yellow or red display in the status bar indicates an improperly serviced waste
tank. Contact maintenance to service any tanks not showing the proper indication.
Manual Shutoff
Handle
Flush Button
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
5.20.6 D611W302-TBC (200 GenFam)
Water Faucet Fails to Shut Off
If the sink water faucet buttons do not shut off the running water, the water system
for that lavatory must be shut off.
Turn the water supply shutoff valve handle located above the sink behind the
mirror clockwise to the OFF position.
The water system, which includes the sink and the toilet flush, is turned off for that
lavatory.
Placard the lavatory as inoperative.
If the water leak cannot be eliminated by turning off the water supply shutoff
valve, the water supply isolation valve associated with that lavatory should be
closed.
ON
OFF
Mirror Release
Button
Note: Valve behind
mirror.
Mirror
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.20.7
The water supply isolation valves are located in a panel above doors 2L and 4L.
Rotate the isolation valve “T” handle clockwise to close the valve. Closing the
valve at door 2L shuts off all water supply forward of door 2. Closing the valve at
door 4L shuts off all water supply forward of door 4.
Note: Lavatories located aft of the door 4L water supply isolation valve will still
have water.
Water Supply
Isolation Valve
EXIT
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
5.20.8 D611W302-TBC (200 GenFam)
Lavatory Doors
Bifold Door Unlocking/Locking
The lavatory door can be locked or unlocked from the outside by:
• lifting the metal flap above the VACANT/OCCUPIED indicator
• moving the lock slide to left to lock the door
• moving the lock slide to right to unlock the door
Cover Plate
Lock Slide
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 5.20.9
Bifold Door Removal
Occasionally the lavatory door may become blocked from the inside due to
supplies falling out of the storage compartment onto the floor, or an incapacitated
passenger lying on the floor.
The following procedure allows the removal of the door and access to the lavatory
compartment:
• unlock the door
• release the upper and lower pivot shafts on the door
• pull the top shaft down and over
• lift the bottom shaft up and over
• pull the door out at the bottom
• drop the door down and away from the lavatory
Pivot Shaft
February 14, 2003
Flight Attendant Manual
Lavatories -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
5.20.10 D611W302-TBC (200 GenFam)
Panel Door Unlocking
Panel doors are generally associated with lavatories with handicapped facilities.
If the panel door is locked and access must be gained:
• slide a flat object (knife, credit card, fingernail) under the door latch
receiver flap
• pry the door latch receiver flap forward and outward
• pull on door handle at same time as lifting on door latch receiver flap
Door Latch
Receiver Flap
February 14, 2003
Flight Attendant Manual
Galleys Chapter 6
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 6.TOC.0.1
6.0 Galleys-Table of Contents
Galley Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.1
Galley Overview . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.1
Galley Locations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.2
Galley Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.3
Galley Water System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.3
Water Shutoff Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.3
Galley Waste System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.10.3
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.1
Galley Non-Normals. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.1
Galley Emergency Power Off Switch . . . . . . . . . . . . . . . . . . . 6.20.1
Galley Sink Drain Blockages. . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.1
Galley Water Fails to Shut Off. . . . . . . . . . . . . . . . . . . . . . . . . 6.20.2
Low Potable Water . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.20.3
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
6.TOC.0.2 D611W302-TBC (200 GenFam)
Galleys -
Table of Contents
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Galleys Chapter 6
Galley Location Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 6.10.1
6.10 Galleys-Galley Location
Galley Overview
Individual galley modules may contain ovens, waste containers, coffee makers,
refrigeration units, storage/servicing carts, sinks and stowage space to aid in food
preparation and dispensing. Galleys are equipped with electrical power and water
systems. Lighting controls are located on the galley electric panel. A galley vent
system keeps the air fresh.
Service carts are restrained for takeoff and landing. There are stowage areas for
extra carts located at various galleys. The number of food carts shall not exceed
the number of inflight cart restraints available.
Each galley is provided with a heater control for the regulation of the temperature
in the galley area. See the galley vendor provided information for location and
operation.
February 14, 2003
Flight Attendant Manual
Galleys -
Galley Location
Copyright © The Boeing Company. See title page for details.
6.10.2 D611W302-TBC (200 GenFam)
Galley Locations
Galley
Middle 2
Galley Aft 2
Galley
Forward 2
Galley
Middle Left
Galley
Forward 3
Galley
Middle 1
Galley
Forward 1
Galley Aft 4
Galley Aft 3
Galley
Middle Right
Galley
Middle 4
February 14, 2003
Flight Attendant Manual
Galleys -
Galley Location
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 6.10.3
Galley Electrical Power
A Galley Emergency Power Off Switch is located in each galley. The switch is
covered with a red guard. With the red guard closed, the switch is in the
NORMAL (on) position. If there is an emergency, the red guard should be lifted
and the toggle switch placed to the OFF position. This removes all electrical
power to the galley. The Galley Emergency Power Off Switch should be used
only during an emergency situation.
Galley Water System
Galley water is supplied from two potable water tanks. The tanks have a combined
usable capacity of approximately 825 liters (218 gallons). The tanks are normally
pressurized from the airplane bleed air system. When bleed air pressure is not
available, alternate pressurization is automatically provided by an electrically
driven air compressor. Water is not available while the tanks are being serviced.
The quantity of potable water may be verified on the cabin management system
POTABLE WATER display.
Water Shutoff Valve
Each galley that has running water is equipped with a water shutoff valve.
Positioning the water shutoff valve to OFF turns off water to that galley.
Galley Waste System
Galley sink waste water is drained overboard through heated drain masts.
To prevent sink drain blockages do not put solid waste (coffee grounds, tea bags,
fruit pulp, and so on) in the sink drain. Put solid waste in the galley waste bins.
Mixtures, which can curdle and create a drain blockage, should be diluted with an
equal amount of water.
Do not remove the sink drain strainer.
OFF
ON
Water Shutoff Valve
February 14, 2003
Flight Attendant Manual
Galleys -
Galley Location
Copyright © The Boeing Company. See title page for details.
unctions such as
fire, smoke, electrical arcing, and so on.
Note: When placing the galley Emergency Power Off switch to the OFF position,
notify the flight deck.
Galley Sink Drain Blockages
If a sink drain is blocked, or drainage is slow, no more fluids should be poured into
the sink. Dispose of fluids in another galley sink.
EMER POWER
OFF SWITCH
OFF
NORM
February 14, 2003
Flight Attendant Manual
Galleys -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
6.20.2 D611W302-TBC (200 GenFam)
Galley Water Fails to Shut Off
If the water cannot be turned off in any of the galley fixtures, such as the sink water
faucet, coffee maker, or water boiler, the water system for that galley must be shut
off.
Position the galley water shutoff valve to OFF. See the galley vendor’s drawings
for exact location.
OFF
ON
Water Shutoff Valve
February 14, 2003
Flight Attendant Manual
Galleys -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 6.20.3
If the leak that cannot be eliminated by turning off the water shutoff valve, the
isolation drain valve associated with the galley should be closed.
The water supply isolation valves are located in a panel above doors 2L and 4L.
Rotate the isolation valve “T” handle clockwise to close the valve. Closing the
valve at door 2L shuts off all water supply forward of door 2. Closing the valve at
door 4L shuts off all water supply forward of door 4.
Note: Galleys located aft of the door 4L water supply isolation valve will still have
water.
Low Potable Water
The LOW POTABLE WATER alert message appears on the CSCP/CACP
displays when 1/4 tank of potable water remains. Pushing the clear key removes
the window from the display but displays a message at the bottom of the
CSCP/CACP displays stating that the potable water level is at 1/4.
EXIT
Water Supply
Isolation Valve
February 14, 2003
Flight Attendant Manual
Galleys -
Non-Normal Operations
Copyright © The Boeing Company. See title page for details.
6.20.4 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits Chapter 7
Table of Contents Section 0
FCOM Template 12/12/98
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 7.TOC.0.1
7.0 Doors, Slides and Emergency Exits-Table of Contents
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.1
Doors, Slides and Emergency Exits Overview . . . . . . . . . . . . . . . 7.10.1
Passenger Entry Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.1
Passenger Entry Doors Overview . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.1
Passenger Entry Door Controls . . . . . . . . . . . . . . . . . . . . . . . . 7.20.2
Door Mode Select Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.4
Dedicated Assist Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.7
Flight Lock. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.7
Evacuation Slide/Rafts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.8
Slide/Raft Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.10
Evacuation Slide/Rafts - Slides . . . . . . . . . . . . . . . . . . . . . . . 7.20.12
Passenger Entry Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.20.14
Passenger Entry Door Preflight . . . . . . . . . . . . . . . . . . . . . . . 7.20.14
Passenger Entry Normal Door Operation – Interior . . . . . . . 7.20.15
Passenger Entry Door Normal Operation - Exterior . . . . . . . 7.20.16
Non-Normal Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.1
Doors, Slides and Emergency Exits Non-Normal
Operations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.40.1
Passenger Entry Door Non-Normal Operation . . . . . . . . . . . . 7.40.1
February 14, 2003
Flight Attendant Manual
Copyright © The Boeing Company. See title page for details.
7.TOC.0.2 D611W302-TBC (200 GenFam)
Doors, Slides and Emergency
Exits -
Table of Contents
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits Chapter 7
Introduction Section 10
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 7.10.1
7.10 Doors, Slides and Emergency Exits-Introduction
Doors, Slides and Emergency Exits Overview
This chapter describes the passenger entry doors and evacuation slide/rafts. It
includes a description of door preflight, and normal and non-normal operation
from inside and outside the airplane.
Passenger evacuation and ditching guidelines are described in Chapter 9,
Non-Normal Situation Guidelines.
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits -
Introduction
Copyright © The Boeing Company. See title page for details.
7.10.2 D611W302-TBC (200 GenFam)
Intentionally
Blank
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits Chapter 7
Passenger Entry Doors Section 20
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 7.20.1
[Option shown: ARMED/DISARMED; Option:AUTOMATIC/MANUAL;
Option shown: Life raft: Installed]
7.20 Doors, Slides and Emergency Exits-Passenger Entry Doors
Passenger Entry Doors Overview
There are eight identically operated passenger entry doors paired along the
airplane fuselage. They are used to enter and exit the airplane, and also serve as
emergency exits.
There are no other passenger cabin exits. Doors on the left side of the airplane are
identified as 1L, 2L, 3L, and 4L and are generally used for passenger entry. Doors
on the right side of the airplane are 1R, 2R, 3R and 4R and are generally used for
servicing the airplane.
The doors can be opened or closed manually from inside or outside the airplane.
The passenger entry doors are translating, plug-type doors. During opening, the
door first moves inward and upward, then translates outward and forward. Each
door is held in the open position by a gust lock. The gust lock drops into a latch as
the door nears its forward limit of travel. A window in each door allows
observation outside of the airplane.
A dual lane slide/raft is contained in the lower inboard face of each passenger
entry door behind the door bustle.
A vent panel is connected to the door operating handle. The vent remains open and
prevents pressurization to an unsafe level if the door is not fully closed, latched,
and locked.
Rotation of the door operating handle forward to the CLOSED position
automatically locks the door. As the handle is moved past the latched position, the
vent is closed. Initial rotation of the handle aft (toward OPEN) opens the vent to
equalize cabin and outside air pressure.
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits -
Passenger Entry Doors
Copyright © The Boeing Company. See title page for details.
7.20.2 D611W302-TBC (200 GenFam)
Passenger Entry Door Controls
1 Viewing Window
Allows observation outside the airplane.
2 Slide/Raft Gas Bottle Pressure Gage
If the gage needle is outside the green zone, the system is unusable.
3 Door Bustle Release Handle
Pull to remove door bustle for access to slide/raft.
4 Door Mode Select Panel
See following graphic.
EXIT
1
2
4
5
6
7
8
3
9
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits -
Passenger Entry Doors
Copyright © The Boeing Company. See title page for details.
D611W302-TBC (200 GenFam) 7.20.3
5 Emergency Power Assist System (EPAS) Reservoir Pressure Gage
If the gage needle is outside the green zone, EPAS is unusable.
6 Gust Lock Release Lever
Grab and pull inward to close the door.
7 Door Operating Handle
To open the door – rotate in the direction of the arrow.
To close the door – rotate in the opposite direction of the arrow.
8 Door Bustle
The bustle contains the slide/raft.
9 Girt Bar Indicator Flag Viewing Windows
Yellow in view – door and slide/raft are armed for automatic operation and
slide/raft deployment.
Black in view – door and slide/raft are not armed.
Note: A safety strap is installed in the door sill, approximately halfway up on the
left side of the door. It should be used when the door is open.
To use the safety strap, pull the metal handle and attach it to the loop on the
right side of the door sill.
February 14, 2003
Flight Attendant Manual
Doors, Slides and Emergency Exits -
Passenger Entry Doors
Copyright © The Boeing Company. See title page for details.
