To:
HOLDERS OF CABIN HANDBOOK
Bombardier Challenger 300, Serial No. 20074
REVISION A, DECEMBER 2006
HIGHLIGHTS
Pages which have been added or revised are outlined below
together with the highlights of the revision. Remove and insert
the affected pages as listed.
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Completely revised and reissued.
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Cover
Cabin Handbook
December 2006
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Aircraft S/N: 20074
BOMBARDIER CHALLENGER 300*
CABIN HANDBOOK - AIRCRAFT S/N: 20074 (REV. A)
BO
CA
Bombardier Inc.
P. O. Box 6087, Station Centre-ville
Montreal, Quebec, Canada H3C 3G9
Bom
P. O
Mon
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Identification Number should be used: CH 300 COMP CH
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It is understood that this documentation, comprising technical data and other
information in any media shall not be reproduced or disclosed in whole or in part
without Bombardier’s written authorization, is proprietary and confidential to
Bombardier and that all rights to patent, copyright, trademark, trade secret and
other intellectual property rights therein belong to Bombardier. Such
documentation, technical data and other information shall not be modified,
translated, reverse assembled, reverse engineered or de-compiled and shall be
used solely to maintain, operate or repair the aircraft.
It is
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used
Copyright © 2006 by Bombardier Inc. All rights reserved.
*Trademark of Bombardier Inc. or its subsidiaries.
Printed in Canada
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Introduction
Introduction
This Cabin Handbook describes and provides operating instructions for the
custom equipment and furnishings installed at the completion center. This
manual does not replace any manual provided with the aircraft by the
manufacturer. It is strongly recommended that all manuals be thoroughly
reviewed to acquaint the owners and attendants with all equipment and
furnishings. This includes the specific vendor manuals provided by the
equipment manufacturers.
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Aircraft S/N: 20074 (Rev. A)
Date
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Table of Contents
Table of Contents
Section 1 Aircraft Description........................................... 1
Cabin Furnishings ................................................................... 1
Overview .................................................................................1
Cabin Doors ............................................................................2
Entry Area ...............................................................................2
Crew Closet .............................................................................3
Wardrobe Cabinet ...................................................................3
Galley ......................................................................................3
Lavatory ..................................................................................4
Baggage Compartment ...........................................................5
Main Cabin .............................................................................5
Armledge Storage Boxes ........................................................7
Emergency Exit Table ............................................................7
Executive Tables .....................................................................7
Magazine Racks ......................................................................7
Subwoofer Cabinet .................................................................7
Passenger Switch Panels .........................................................8
Pyramid Cabinet .....................................................................8
Single Seats .............................................................................9
VIP Seat ..................................................................................9
Video Monitors .......................................................................9
Window Shades ....................................................................10
Section 2 Aircraft Systems............................................... 11
Communication ..................................................................... 11
Overview ...............................................................................11
Passenger Address ................................................................11
Call Systems .........................................................................11
Airborne Telecommunication System ..................................12
A. Air-to-Ground calling ....................................................15
B. Inplane Calling ...............................................................16
C. Ground-to-Air Calling and Call Handling .....................16
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Entertainment ....................................................................... 19
Overview .............................................................................. 19
Cabin Management System .................................................. 19
Controls ................................................................................ 21
Audio System ....................................................................... 24
Video System ....................................................................... 26
Airshow System ................................................................... 26
Electrical Power .................................................................... 29
Overview .............................................................................. 29
115VAC/60HZ Power System ............................................. 29
Lighting.................................................................................. 31
Overview .............................................................................. 31
Lighting Controls ................................................................. 31
Entry Area Lights ................................................................. 31
Cabin Lighting ...................................................................... 33
Lavatory Lights .................................................................... 33
Baggage Compartment Lights .............................................. 33
Water and Waste .................................................................. 35
Overview .............................................................................. 35
Water System ....................................................................... 35
Waste System ....................................................................... 38
Section 3 Galley .................................................................39
General................................................................................... 39
Overview .............................................................................. 39
Galley Description ................................................................ 39
Galley Waste Disposal ......................................................... 41
Section 4 Lavatory ............................................................43
General................................................................................... 43
Overview .............................................................................. 43
Lavatory Toilet ..................................................................... 43
Lavatory Water Supply ........................................................ 43
Lavatory Waste Disposal ..................................................... 43
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Section 5 Miscellaneous ................................................... 45
General ................................................................................... 45
Non-Approved Electronic Devices .......................................45
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Section 1 Aircraft Description
Cabin Furnishings
Overview
The cabin is divided into the entry area, main cabin, lavatory, and baggage
compartment. Refer to Cabin Layout (Figure 1).
MAIN ENTRY DOOR
ENTRY AREA
MAIN CABIN
EMERGENCY
EXIT
LAVATORY
BAGGAGE
COMPARTMENT
Cabin Layout
Figure 1
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Page 1
Cabin Doors
The passenger cabin is served by a main entry door on the left side of the
aircraft, aft of the cockpit. An emergency exit is located on the aft right side of
the main cabin.
Entry Area
The Entry Area (Figure 2) is located inside the main entry door. It extends
from the cockpit to the entrance of the main cabin. A fabric curtain separates
the cockpit from the entry area. An acoustical curtain separates the main entry
door from the entry area.
Furnishings in the entry area include the following items:
• A crew closet
• The forward wardrobe cabinet
• The galley
• Avionics cabinets
A switch panel, located on the forward wardrobe header, controls the entry
area lighting. Refer to Section 2, Aircraft Systems, Lighting, for more
information.
AVIONICS
CABINET
AVIONICS
CABINET
CREW
CLOSET
MAIN
ENTRY DOOR
GALLEY
WARDROBE
CABINET
Entry Area
Figure 2
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Crew Closet
A crew closet, in the entry area forward of the galley, provides storage for
garments and emergency equipment. A dome light provides general
illumination when the door is opened.
Wardrobe Cabinet
A wardrobe cabinet, aft of the main entrance, provides garment storage, and
provisions for the entertainment and communication equipment. When the
door is opened, a dome light provides general illumination. Two cooling fans
are installed in the wardrobe to supply ventilation for the entertainment system
components. The cooling fans are on as long as power is supplied to the
aircraft. The entry area switch panel, located in the cabinet header, is the main
control point for the cabin management system. Refer to Section 2, Aircraft
Systems, Entertainment, for more information about the cabin management
system.
Galley
The Galley (Figure 3), in the entry area aft of the crew closet, provides
facilities for stowing and preparing food and beverages. The galley has
electrical power for fans and appliances. Refer to Section 3, Galley, for more
information.
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Galley
Figure 3
Lavatory
The Lavatory (Figure 4), located between the main cabin and the baggage
compartment, is separated from the main cabin by a bulkhead and pocket door,
and the baggage compartment by a bulkhead and hinged door. Refer to
Section 4, Lavatory, for more information.
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VANITY
CABINET
POCKET
DOOR
LAVATORY
TOILET
BAGGAGE
STORAGE
CABINET
COMPARTMENT
HINGED
DOOR
Lavatory
Figure 4
Baggage Compartment
The baggage compartment is located aft of the lavatory, and contains a water
tank, a baggage net, a storage cabinet, and coat rods for hanging garments. The
baggage compartment has an increased capacity of 750 pounds, and is not
accessible when the lavatory is occupied.
Main Cabin
The Main Cabin (Figure 5) is located between the entry area and the lavatory.
A bulkhead and pocket door separate the cabin from the lavatory.
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Furnishings in the main cabin include the following items:
• Eight single seats (one VIP seat position)
• Eight armledge storage boxes
• One emergency exit table (stowed in baggage compartment)
• Three executive tables
• Eight passenger switch panels
• One pyramid cabinet
• Two video monitors
• Twelve window shades
• Two magazine racks
• One subwoofer cabinet
VIDEO MONITOR
MAGAZINE RACK
ARMLEDGE
STORAGE BOX
(8 PLACES)
SINGLE SEAT
(8 PLACES)
VIP SEAT
WINDOW SHADE
(12 PLACES)
SUBWOOFER
CABINET
PASSENGER
SWITCH PANEL
(8 PLACES)
EXECUTIVE TABLE
(3 PLACES)
EMERGENCY EXIT
TABLE
PYRAMID CABINET
MAGAZINE RACK
VIDEO MONITOR
Main Cabin
Figure 5
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Armledge Storage Boxes
Eight storage boxes, in the armledges adjacent to each single seat, provide
general storage. The storage boxes adjacent to right-hand seat 2 and left-hand
seat 4 contain telephone handsets. The storage boxes adjacent to left- and righthand seats 2 and 4 contain single electrical outlets.
Emergency Exit Table
There are receptacles for a folding plug-in table below the emergency exit,
behind a closeout panel with a spring-loaded hinge. Table stowage is provided
in the baggage storage cabinet, located on the aft side of the right-hand
baggage bulkhead.
To deploy the plug-in table:
• Remove the leaf from the baggage storage cabinet
• Flip down the lid on the dado panel
• Slide the plug-in table leaf supports into the receptacles
Executive Tables
There are three folding executive tables in the armledges adjacent to the single
seats. The executive tables are manually deployed.
To deploy the executive tables:
• Pull the armledge cover up and out
• Unfold the table leaf
Magazine Racks
There are two magazine racks located in the main cabin. The forward
magazine rack is located on the right side, aft of the galley. The aft magazine
rack is located on the left side, forward of the aft cabin bulkhead, and provides
a drawer for storage.
Subwoofer Cabinet
There is a subwoofer cabinet located on the right side of the main cabin, aft of
right-hand seat 2.
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Passenger Switch Panels
Passenger switch panels, located in the armledges adjacent to each seat
position, control lighting and entertainment features in the main cabin. Refer to
Section 2, Aircraft Systems, Entertainment, for more information.
The passenger switch panel located at the VIP seat, right-hand seat 2, also
controls the cabin call system and cabin temperature.
Pyramid Cabinet
There is a Pyramid Cabinet (Figure 6) in the main cabin on the right side,
forward of the aft cabin bulkhead. It opens on the inboard side and provides
storage for a life raft.
PYRAMID
CABINET
ASHTRAY
LIFE RAFT
DOOR
Pyramid Cabinet
Figure 6
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Single Seats
WARNING: DURING TAXI, TAKEOFF, AND LANDING, ALL SEATS ARE
TO BE IN THE FULL UPRIGHT POSITION; THE
FORWARD-FACING SEATS MUST BE IN THE FULLY AFT
TRACKING POSITION; THE AFT-FACING SEATS MUST BE
IN THE FULLY FORWARD TRACKING POSITION; AND
SEATBELTS MUST BE WORN.
There are eight single seats in the cabin, four on each side. Cabin seating is
referenced by right- or left-hand side. For example, the first seat on the right
side is referred to as right-hand seat 1. Each seat is equipped with the following
features:
• Three-point push button restraint system
• Headrest (aft-facing seats only)
• Recline
• Swivel
• Tracking (8" forward/aft, 5" inboard/outboard)
Note:
Swivel and tracking capabilities are restricted at right-hand seat 3
and right-hand seat 4 to comply with egress requirements at the
emergency exit.
VIP Seat
The VIP seat is designated as right-hand seat 2. The personal switch panel at
this location is distinct because it provides additional control of the lighting
and entertainment systems as well as temperature control. Refer to Section 2,
Aircraft Systems, Entertainment, for more information about the VIP
passenger switch panel.
Video Monitors
There are two video monitors in the main cabin. The forward monitor is
located on the left side, on the aft face of the wardrobe cabinet. The aft monitor
is located on the right side, on the forward face of the aft cabin bulkhead. Refer
to Section 2, Aircraft Systems, Entertainment, for more information.
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Window Shades
There are manually-operated window shades on all windows throughout the
main cabin. They can be set at any position, from fully opened to fully closed.
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Section 2 Aircraft Systems
Communication
Overview
This section describes the communication systems in the aircraft. The
communication equipment includes the passenger address system, the call
system, and the airborne telecommunication system.
Passenger Address
The Passenger Address (PA) system enables crew members to address
passengers from a cockpit microphone over speakers in the main cabin and
lavatory. The cabin entertainment system audio, video, and Airshow passenger
information system output is paused during crew announcements.
Call Systems
The passenger call system enables passengers to alert the flight crew to a need
for assistance. Call switches are incorporated as a menu selection on the
passenger switch panel at the VIP seat, located at right-hand seat 2, and on the
Lavatory Switch Panel (Figure 7) in the lavatory. The cabin entertainment
system audio output is muted, when the call system chime is activated.
FLUSH
READ
UPWASH
MIRROR
CALL
Lavatory Switch Panel
Figure 7
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Press CALL from the lavatory or VIP switch panel to activate the call system.
Once selected, the following alerts are activated:
• The call switch flashes for approximately 10 seconds and then resets
itself
• Aural annunciation is provided through the cabin entertainment
speakers, the headphone jacks, and over chime speakers in the entry
area and cockpit
• Visual annunciation of a call displays in the cockpit on the Engine
Indication and Crew Alerting System (EICAS) for 10 seconds
Airborne Telecommunication System
A MagnaStar C-2000 digital airborne telephone system provides air-to-ground
voice communication. The MagnaStar C-2000 is a terrestrial system that links
with the GTE Airfone ground station network. It operates only in areas
equipped with the appropriate radio stations (the continental United States,
Hawaii, Mexico, and southern Canada).
In addition to providing air-to-ground communication, the MagnaStar system
coordinates and controls the aircraft telephone handsets for all voice calls and
in-cabin intercom functions, when applicable.
All normal operations of the telecommunication system are performed using
the system’s handsets. Each handset has a display and a telephone-style keypad
with two additional keys: + and END CALL. Use the keypad to dial calls and
select various options. Information is provided to the user through a backlit
Liquid Crystal Display (LCD) display 10 characters wide and up to 12 lines
long. Use the two-button volume control on the side of the handset to increase
or decrease the sound level. Optional billing of calls to individual user
accounts is accomplished through a credit card reader is built into the handset.
The handsets are located in the armledge storage boxes at right-hand seat 2 and
left-hand seat 4. Refer to Handset Locations (Figure 8).
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HANDSET
HANDSET
Handset Locations
Figure 8
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The standard MagnaStar handset has a hook switch that is activated by a
magnet in the holder. Remove the handset from the holder to establish an
off-hook condition and activate the handset. Return the handset to the holder to
establish an on-hook condition. Optional handset installations, including
custom holders and portable handsets that plug into jacks, do not provide this
hook-switch function. To place these handsets off-hook, press +. To put these
handsets back on-hook, press +.
While the handset is on-hook, the Services Menu (Figure 9) displays. The
services menu displays those services available to the user. In addition, the
services menu will indicate the inplane number assigned to the handset, and the
Aircall phone number. When the handset is placed off-hook, the services menu
displays for approximately 5 seconds before defaulting to the Main Menu
(Figure 10). The current communication link displays at the top of the main
menu.
Services Menu (Typical)
Figure 9
Main Menu (Typical)
Figure 10
The onboard telecommunication equipment can be used in three ways:
• Air-to-ground calling
• Inplane calling
• Ground-to-air calling and call handling
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A. Air-to-Ground calling
Note:
The following operating instructions are generic and may not
match the system in this aircraft. Refer to the MagnaStar User
Guide for complete instructions
To place a call via the MagnaStar C-2000:
Note:
The MagnaStar C-2000 goes through a system test and warm-up
period of 5 to 10 minutes after power is turned on. Air-Ground
service is not available during this time.
Note:
If a mistake is made while entering information, press * to clear
the entered digits and re-enter the information.
Note:
Calls cannot be coordinated and call hand-off will not occur,
when crossing the US/Mexico border. Refer to the MagnaStar
User Guide for instructions.
•
On the services menu, verify that AIR-GROUND is displayed; if
not, this service is not available and the call cannot be completed
at this time
Remove the handset from the holder, or remove the handset from
the optional location and press + to display the main menu
At the main menu, press 1 for a voice call
Domestic: press 1, the area code, and then the local number
International: press 011, the country code, the city code, and the
local number; then press +
When the number has been sent, ACQUIRING AIR-GROUND
CHANNEL should appear in the display
To end the call, return the handset to the holder or press END
CALL
•
•
•
•
•
•
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Page 15
B. Inplane Calling
The inplane calling feature allows the user to make calls to other handsets
within the aircraft, as long as the handset has been assigned an inplane
number. When the Inplane option is selected from the services menu, the
other handset that has been assigned an inplane number will appear on the
inplane menu along with the corresponding label. Refer to the MagnaStar
User Guide for complete operational details.
To place an inplane call:
• Remove the handset from the holder, or remove the handset from
the optional location and press +
• From the main menu, press INPLANE 2 to access the inplane
menu
• Press the desired inplane number
• When the call is completed, return the handset to the holder or
press END CALL
C. Ground-to-Air Calling and Call Handling
Note:
Many options are available for call handling. The following
operating instructions are for a basic system configuration. Refer
to the MagnaStar User Guide for detailed instructions to operate
this system.
To receive a voice call:
• Take the handset off-hook, when it rings
To transfer an incoming call:
Note:
If a second call is received for an active handset, the handset will
indicate a single-beep call-waiting tone, and the handset display
will indicate an incoming call.
•
•
Press + to place the call on hold
Press INPLANE 2; then press the desired inplane number to add
an inplane conference member
When the party answers, announce that the call is being
transferred
Press + and return the handset to the holder or press END CALL
•
•
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To place the original call on hold and connect the handset to the calling
party:
• Press + to toggle the handset between the two calls
• Press END CALL to terminate the original call and connect the
handset to the calling party
To store a number for later callback:
Note:
If the word Messages appears on the handset Services display,
one or more calls have been stored.
•
•
Press # while the handset is still ringing
The return phone number will be stored with a number to identify
it for later callback
To recall a stored number for callback:
Note:
If a callback number includes an extension, the user must note
the extension number prior to initiating the callback sequence, as
the extension number will no longer be displayed on the callback
screen.
Note:
There are three types of aircall numbers: STATION, where a
number is assigned to each handset; AIRCRAFT, where a
number is assigned to the aircraft; and PERSONAL, where a
number is assigned to individual customers via GTE Airfone
cards. The difference between them is the handset activation
process. Calls to any aircall number are initiated from the
ground in the same manner.
•
•
•
Press + to activate the handset (if applicable)
From the main menu, press 8 to select the Aircall Menu
Press 2 for AIRCRAFT, 3 for STATION, or 4 for PERSONAL to
view stored numbers
Press + (next) or * (previous) to scroll through additional
numbers
When the desired number is displayed, press 1 to initiate the call
to the ground party at that number
•
•
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Section 2 Aircraft Systems
Entertainment
Overview
This section describes the entertainment systems installed in the aircraft. It
includes the cabin management system and the Airshow passenger information
system.
Cabin Management System
A programmable cabin management system provides the passengers and crew
the ability to operate audio and video systems, and other aircraft amenities.
Switch panels, passenger switch panels, and remote controls are used to direct
the operation of various systems and equipment. Cabin Management System
(Figure 11) provides a layout of the cabin management system and switch
panels.
Note:
Many user-programmable features are available for the cabin
management system. The following information applies to a basic
system configuration. The Audio International User’s Guide provides
detailed information on features and programming.
The cabin management system operates the following equipment:
• Cabin temperature control
• Galley appliances
• Call
• Lighting
• Drain mast heat status
• Toilet operation
• Entertainment components
Some of these systems may also be enabled using the two remote controls,
which are provided as loose equipment.
The cabin management system is described in the following sections:
• Controls
• Audio system
• Video System
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ENTRY AREA
SWITCH PANEL
PASSENGER SWITCH
PANELS
PASSENGER SWITCH
PANELS
VIP SEAT
PASSENGER SWITCH
PANELS
PASSENGER SWITCH
PANELS
BAGGAGE LIGHTS
SWITCH PANEL
LAVATORY
SWITCH PANEL
Cabin Management System
Figure 11
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Controls
The cabin management system is controlled by the following equipment:
• Entry area switch panel
• Lavatory switch panel
• Passenger switch panels, located in the armledge at each seat
• Two remote control units
Entry Area Switch Panel
The Entry Area Switch Panel (Figure 12) uses a green-colored dot matrix
display and provides control of cabin lighting and galley functions through
layered menus. Menu selections are made through adjacent buttons, and
are used to turn features on or off, or move up or down in the menus.
When buttons are pressed, a green halo effect backlight appears, denoting
the selection.
Entry Area Switch Panel
Figure 12
The entry area switch panel controls the following cabin lighting:
• Cabin lights (forward and aft upwash, BRT/DIM/OFF)
• Cabin lights (forward and aft downwash, BRT/DIM/OFF)
• Lavatory upwash lights (ON/OFF)
The entry area switch panel controls the following galley features:
• Drain mast heater monitor/test
• Galley work and mini-spot light control (BRT/DIM/OFF)
• Galley drain (ON/OFF)
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•
•
Hot liquid container #1 (ON/OFF)
Hot liquid container #2 (ON/OFF)
The entry area switch panel uses dedicated buttons to control the
miscellaneous lighting features that follow:
• Entry area lights (ON/OFF, or auto off after 20 minutes)
• Baggage lights (ON/OFF, or auto off after 20 minutes)
Lavatory Switch Panel
The Lavatory Switch Panel (Figure 13) uses dedicated buttons to provide
local control of lavatory equipment. When buttons are pressed, a green
halo effect backlight appears, denoting the selection.
FLUSH
READ
UPWASH
MIRROR
CALL
Lavatory Switch Panel
Figure 13
The lavatory switch panel operates the following equipment:
• Lav call (auto reset after 10 seconds)
• Mirror lights (ON/OFF)
• Reading lights (ON/OFF)
• Toilet flush (auto off after 8 seconds)
• Upwash lights (ON/OFF)
A separate switch panel in the lavatory provides local control of the
baggage lights. When the button is pressed, a green halo effect backlight
appears, denoting the selection. The baggage lights can be turned on or off
with this switch, or the lights will automatically turn off after 20 minutes.
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Passenger Switch Panels
The Passenger Switch Panel (Figure 14), located in the armledge at each
seat, is programmable, and uses a green-colored dot matrix display. The
passenger switch panels provide control of cabin audio, video, lighting,
and temperature control functions through layered menus. Menu
selections are made through adjacent buttons, and are used to turn features
on or off, or move up or down in the menus. When buttons are pressed, a
green halo effect backlight appears, denoting the selection.
Note:
Limited control of the cabin temperature is provided by the
passenger switch panel at VIP right-hand seat 2 only.
Passenger Switch Panel (Typical)
Figure 14
The passenger switch panel controls the following audio features:
• Cabin speaker audio source control
• Cabin speaker volume control
• Cabin speakers (ON/OFF)
• Seat audio source control
• Seat audio volume
• Seat headphone jack
The passenger switch panel controls the following video features:
• Forward or aft video monitor source control
• Forward or aft video monitor control (ON/OFF)
The passenger switch panel uses dedicated buttons to control the
following miscellaneous lighting features:
• Seat reading light (ON/OFF)
• Seat table light (ON/OFF)
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Remote Controls
The remote controls provide audio control for the following features:
• Cabin speakers (ON/OFF)
• Cabin speaker source control
• Cabin speaker volume control
The remote controls provide video control for the following features:
• Airshow mode
• Digital Versatile Disc (DVD) player and Compact Disc (CD)
player (e.g., PLAY, PAUSE, SEARCH, SKIP, STOP)
• Forward or aft video monitor source control
• Forward or aft video monitor control (ON/OFF)
Audio System
The audio system provides stereo quality sound from the Airshow system, the
CD player, and the DVD player to headphone jacks and speakers in the cabin.
Passengers control the audio system output through the passenger switch panel
or remote controls. The output of the audio system can be directed to the cabin
speakers or through headphone jacks at each seat. Entertainment System
(Figure 15) shows a layout of the entertainment system audio components.
Audio sources are available through the following equipment:
• CD player
• DVD player
Headphones
The passenger switch panels control headphone audio source selection,
tone adjustment, and volume control from menu selections. Passengers
may listen to any of the available audio sources through headphones.
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AIRSHOW SYSTEM
CD PLAYER
DVD PLAYER
FORWARD
LCD MONITOR
HEADPHONE JACKS
HEADPHONE JACKS
VIP SEAT
SUBWOOFER CABINET
HEADPHONE JACKS
HEADPHONE JACKS
AFT
LCD MONITOR
Entertainment System
Figure 15
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Speakers
The passenger switch panel at the VIP seat, right-hand seat 2, controls
speaker audio source selection, tone adjustment, and volume control from
menu selections. The remote controls do not provide tone control.
Video System
Note:
The following definitions are provided for video formats to avoid
confusing sentences: National Television System Committee (NTSC);
Phase Alternating Line (PAL); and Sequential Color with Memory
(SECAM).
The video system distributes multi-regional video formats (e.g., NTSC, PAL,
and SECAM) from the Airshow system and a DVD player, to two Liquid
Crystal Display (LCD) monitors in the cabin. Passengers control the output of
the video system through the passenger switch panel at the VIP seat, or a
remote control. Control of the LCD monitors can only be performed from the
VIP seat passenger switch panel, or the remote controls. Refer to
Entertainment System (Figure 15) for a layout of the entertainment system
video components.
Video sources are available through the following equipment:
• Airshow system
• DVD player
LCD Monitors
The LCD monitors are flat panel displays, and will accept multi-standard
video formats including NTSC, PAL, and SECAM.
Airshow System
The Airshow 400 passenger information system uses the LCD monitors to
display a moving map and an aircraft symbol depicting current flight position.
It can also display other map and flight data. The Airshow system is also
interfaced to the cabin management system for control over the various
Airshow display modes.
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Audio briefing in English is incorporated into the Airshow system. This
briefing is controlled by the Airshow controller in the cockpit.
The Airshow system is controlled from the cockpit controller, the VIP seat
passenger switch panel, or a remote control.
When AIRSHOW is selected, the AUTO mode is displayed. Press AIRSHOW
MODE SELECT on the entry area switch panel or the VIP passenger switch
panel, or AIRSHOW MODE on a remote control to cycle through the
following modes and displays:
AUTO
This mode cycles through the Relative Location Indicator (RLI), INFO,
and MAP modes. The MAP series in AUTO mode starts with a
low-resolution map of the current aircraft location and zooms through
progressively higher-resolution maps until it reaches the standard MAP
mode display. It then cycles back to RLI, and the sequence begins again.
INFO
Displays real-time flight information. This information can be chosen by
the user from a menu of options which may include:
• Altitude
• Distance to destination
• Ground speed
• Outside air temperature
• Time to destination
MAP
Displays a high-resolution map of the current aircraft location.
RLI
Displays an aircraft symbol on a blue field showing the two cities
currently nearest the aircraft and including vectors, distance information,
and location relative to the aircraft.
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Section 2 Aircraft Systems
Electrical Power
Overview
This section describes the 115VAC/60Hz power system in the aircraft.
115VAC/60HZ Power System
One 2.0kVA 60Hz power converter supplies 115VAC/60Hz to selected galley
and cabin equipment, and the outlets in the galley, cabin, and lavatory.
Operators of electrical devices plugged into these outlets are protected from
electrical shock by the Ground Fault Indicator (GFI) devices located in the
upper galley and in the lavatory vanity cabinet. Over-current protection for the
outlets is provided by the GALLEY, CABIN, and LAV circuit breakers on the
Auxiliary Galley Circuit Breaker Panel (AUX GCBP). Over-current protection
for the GFIs is provided by the MAIN circuit breaker on the AUX GCP.
The outlets are a single receptacle North American style.
WARNING: A GROUND FAULT REPRESENTS A HAZARDOUS
CONDITION. ENSURE THAT THE CONDITION IS
CORRECTED BEFORE RESETTING THE GFI.
A ground fault will pop the RESET button on the GFI. After the condition is
cleared:
• Press the RESET button to reset the fault detection circuitry
Note:
If the GFI does not test properly, notify the crew or ground personnel
of the situation.
To test the integrity of the GFI circuitry:
• Press the TEST button
• The RESET button should pop
• Press the RESET button to restore its function
Electrical Outlet Locations (Figure 16) provides a layout showing the cabin
electrical outlets.
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OUTLET
(6 PLACES)
GFI
(3 PLACES)
Electrical Outlet Locations
Figure 16
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Section 2 Aircraft Systems
Lighting
Overview
This section provides a description of the cabin lighting and interior
emergency lighting. It includes lighting controls, and lighting in the galley,
cabin, lavatory, and baggage compartment.
Lighting Controls
Control of the lighting system is provided by switch panels in the entry area
and the lavatory, and passenger switch panels located in the armledges at each
seat. Refer to the Cabin Management System (Section 2, Aircraft Systems,
Entertainment) for more information on the operation of switch panels.
Lighting Control Locations (Figure 17) provides a cabin layout of lighting
controls.
Entry Area Lights
Lights in the headliner and cabinets provide general illumination in the entry
area. There are two Light-Emitting Diode (LED) light panels in the entry
headliner. There are dome lights in the forward wardrobe and crew closet
which are controlled by microswitches in the doors.
The galley lighting consists of overhead spot lights, and counter lights. An
LED strip light above the counter and five overhead LED spot lights provide
work lighting for the galley.
The entry area lights are controlled from the entry area switch panel. If the
aircraft is operating on battery power, the overhead lights will automatically
turn off after 20 minutes.
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ENTRY AREA
SWITCH PANEL
PASSENGER SWITCH
PANELS
PASSENGER SWITCH
PANELS
PASSENGER SWITCH
PANELS
PASSENGER SWITCH
PANELS
BAGGAGE LIGHTS
SWITCH PANEL
FLUSH
READ
UPWASH
MIRROR
CALL
LAVATORY
SWITCH PANEL
Lighting Control Locations
Figure 17
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Cabin Lighting
The cabin lighting consists of Light Emitting Diode (LED) indirect lighting
(upwash and downwash), and reading and table lights.
Indirect lighting is provided by upwash lights in the headliner and downwash
lights in the Passenger Service Units (PSU). The lights are dimmable, and are
divided into forward and aft sections to allow independent control.
Reading and table lights are installed in the PSU. There are two table lights
above each table, and one reading light above each seat. The reading lights are
also interfaced to the ground service bus, so they can be operated using ground
service power.
The cabin lights are controlled from the entry area switch panel, and the
passenger switch panel at each seat.
Lavatory Lights
The lavatory lighting consists of indirect lighting (upwash), mirror lights, and a
reading light.
The indirect lighting is provided by LED upwash lights in the PSU.
The mirror lights are LED light strips around the lavatory mirror.
The reading light is in the lavatory PSU. The reading light is also interfaced to
the ground service bus, so it can be operated using ground service power.
The lavatory lights are controlled by the lavatory switch panel. The upwash
lights are also controlled by the entry area switch panel.
Baggage Compartment Lights
An LED light panel and an overhead light in the baggage compartment
headliner provide general illumination. The overhead light is interfaced to the
airstair lighting circuit.
The baggage compartment lights are controlled from the baggage lights switch
panel in the lavatory and the entry area switch panel. If the aircraft is operating
on battery power, the lights will automatically turn off after 20 minutes.
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Section 2 Aircraft Systems
Water and Waste
Overview
This section describes the water system in the lavatory, and the waste systems
in the lavatory and the galley.
Water System
A potable water system is installed in the lavatory to provide water to the
lavatory faucet. The system is modular, consisting of a water tank and a water
system pallet.
The water tank is located in the baggage compartment, and has a 2.5 gallon
capacity. It can be filled in place or easily removed for servicing. It is
connected to the water system pallet with a flex hose and quick-disconnect
fitting.
The water system pallet is located in the lower vanity cabinet. It contains a
manual switch, a pump, an in-line water heater, and valves for routing potable
and waste water.
The water system is controlled from the manual switch on the water system
pallet. When the switch is set to ON, the pump will pressurize the water system
to an operating pressure of 32 psi. Once the system reaches 32 psi, the pump
goes into standby mode until pressure drops. The in-line water heater operates
only when the water system is pressurized.
Note:
If water runs for more than 30 seconds or if the water tank is empty,
the water system automatic shut-down feature activates.
The water system pallet has an automatic shut-down feature, which prevents
wasteful water usage and controls the water pump water pressure. The water
reset switch is a black rectangular button that is backlit. The normal mode for
this switch is dark. The water reset switch for the lavatory is located beneath
the lavatory ordinance sign.
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When the water reset switch flashes amber:
• Press the water reset switch
• The water system will activate if the water tank has a water supply
• If there is no water in the water tank, the water system will not
activate
A water system select switch is located behind the facial tissue dispenser on
the upper vanity cabinet. To drain the system, the water system select switch is
toggled from NORMAL to PURGE. This opens a solenoid valve allowing
overboard draining of the water system.
Refer to Baggage Compartment Water System Components (Figure 18) and
Lavatory Water System Components (Figure 19) for the aircraft water system
location.
WATER
TANK
FILL
PORT
MOUNTING
STRAPS
Baggage Compartment Water System Components
Figure 18
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WATER SYSTEM
SWITCHES
WATER SYSTEM
PALLET
WATER
HEATER
WATER SYSTEM SELECT
SWITCH
WATER
SYSTEM
PALLET
WATER SYSTEM
RESET SWITCH
Lavatory Water System Components
Figure 19
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Waste System
Waste water from the galley and lavatory is drained overboard through valves
and hoses to the forward or aft drain masts. Waste water from the galley drip
tray and ice drawers is discharged through the forward drain mast. Waste water
from the lavatory sink is discharged through the aft drain mast.
The drain lines and drain masts are heated to prevent freezing.
The galley drip tray and ice drawers are equipped with drain ports which are
plumbed into an electrically controlled solenoid valve. The galley drains are
controlled from the Entry Area Switch Panel (Figure 20). To drain the galley
drip tray and ice drawer, select GALLEY and then GALLEY DRAIN ON from
the entry area switch panel. To close the galley drains, select GALLEY
DRAIN OFF. The solenoid valve for the galley drain ports is normally closed
(GALLEY DRAIN OFF) with or without power applied to the cabin
management system.
The lavatory sink is equipped with a spring-loaded plunger-type drain. To
drain the lavatory sink, pull up on the drain handle until all of the water has
drained from the sink. Release the handle to close the drain.
Entry Area Switch Panel
Figure 20
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Section 3 Galley
General
Overview
This section provides a description of the galley and the systems that interface
to it. The Galley (Figure 21) is in the cabin entry area. Galley power is
controlled by the AC PWR switch on the cockpit cabin control panel.
Electrical power to individual pieces of galley equipment is controlled by
circuit breakers installed in the galley.
Abbreviated operating instructions are included for some equipment. For
additional instructions, see the manufacturer’s operating manuals.
Galley Description
The galley provides facilities for stowing and preparing food and beverages for
passengers and crew. It is provided with electrical power, liquid waste lines,
and ventilation from aircraft systems. The galley has electrical equipment and
is connected to a waste water drain line. The galley contains stowage
compartments for related items.
The galley also has the following equipment:
• One circuit breaker panel
• Two cup dispensers
• Two hot liquid dispensers
• One ice drawer
• One trash drawer
• One microwave oven (aircraft-certified product)
• One utility outlet
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CIRCUIT
BREAKER PANELS
HOT LIQUID
DISPENSERS
CUP
DISPENSERS
MICROWAVE
OVEN
UTILITY
OUTLET
ICE DRAWER
TRASH DRAWER
Galley
Figure 21
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Galley Waste Disposal
Waste water from the galley is drained overboard through the forward heated
drain mast. The galley drains are controlled from the Entry Area Switch Panel
(Figure 22). To drain the galley drip tray and ice drawer, select GALLEY and
then GALLEY DRAIN ON from the entry area switch panel. To close the
galley drains, select GALLEY DRAIN OFF. The solenoid valve for the galley
drain ports is normally closed (GALLEY DRAIN OFF) with or without power
applied to the cabin management system.
Entry Area Switch Panel
Figure 22
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Section 4 Lavatory
General
Overview
This section describes the lavatory. It includes the toilet, vanity cabinet, water
supply, and waste disposal.
Lavatory Toilet
There is a self-contained electric toilet with a timed flush cycle in the lavatory.
Press the flush switch to activate the flush cycle, which lasts approximately
8 seconds. The toilet is plumbed to be serviced from outside the aircraft using a
standard lavatory servicing cart.
The toilet has a seat belt and can be used to carry an additional passenger. It
can be used as a seat for taxi, takeoff, and landing.
Lavatory Water Supply
Hot and cold potable water are supplied to the lavatory sink by the water
system (Section 2 Aircraft Systems, Water and Waste). There are water
shut-off valves and a water heater in the vanity cabinet.
Water is available at the lavatory faucet, when the water system is pressurized
and the associated valves are open. Pressure is supplied by the water system
pump.
Lavatory Waste Disposal
Waste water from the lavatory sink is drained overboard through valves and
hoses to the aft drain mast.
The drain lines and drain masts are heated to prevent freezing.
The lavatory sink is equipped with a spring-loaded plunger-type drain. To
drain the lavatory sink, pull up on the drain handle until all of the water has
drained from the sink. Release the handle to close the drain.
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Section 5 Miscellaneous
General
Non-Approved Electronic Devices
The following items (unless permanently installed on the airplane) are not
approved for use in flight:
• Portable telephones (e.g., cellular)
• Radios, either battery or cord operated: Amplitude Modulation (AM),
Frequency Modulation (FM), or Very High Frequency (VHF)
• Television (TV) sets, video players, TV cameras, TV camcorders
(battery or cord operated)
• Toys with remote controls
• Data entry pad (a device with a numeric keyboard, hand-held with
umbilical cord attachment; a mouse attached to a computer is not a
data entry pad)
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