CL_604-EMERGENCY_EQUIPMENT庞巴迪挑战者604应急设备

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Table of Contents
For Training Purposes Only
May 03
8-i
P I LOT T R A I N I N G GU I D E EMERGENCY EQUIPMENT
Introduction .........................................................................................................................8-1
Oxygen System.............................................................................................................8-1
Description ..............................................................................................................8-1
Components and Operation ....................................................................................8-1
Controls and Indicators .................................................................................................8-2
Overboard Discharge Indicator(s) ...........................................................................8-2
Flight Compartment.................................................................................................8-4
EICAS Messages..........................................................................................................8-6
Emergency Exits .................................................................................................................8-8
Main Entrance Door ......................................................................................................8-8
Overwing Emergency Exit.............................................................................................8-8
Emergency Egress Lighting ..........................................................................................8-8
Locating Devices.................................................................................................................8-9
Components and Operation..........................................................................................8-9
Emergency Locator Transmitter (ELT)....................................................................8-9
Underwater Locating Devices (ULDs).....................................................................8-9
Controls and Indicators .................................................................................................8-9
Miscellaneous Emergency Equipment.............................................................................. 8-10
Components and Operation........................................................................................ 8-10
Fire Extinguishers ................................................................................................. 8-10
Crash Axe ............................................................................................................. 8-10
First Aid Kit............................................................................................................ 8-11
Life Vest ................................................................................................................ 8-11
Life Raft................................................................................................................. 8-12
Smoke Goggle Units ............................................................................................. 8-12
8-ii For Training Purposes Only
May 03
EMERGENCY EQUIPMENT P I LOT T R A I N I N G GU I D E
Page Intentionally Left Blank
List of Figures
Graphic Title Figure
For Training Purposes Only
May 03
8-iii
P I LOT T R A I N I N G GU I D E EMERGENCY EQUIPMENT
Oxygen System Panel ........................................................................................................8-1
Flight Deck Oxygen Masks .................................................................................................8-2
Quick-Donning Oxygen Mask Settings ...............................................................................8-3
Passenger Oxygen Control Panel.......................................................................................8-4
ELT System - Control Panel ...............................................................................................8-5
Crash Axe ...........................................................................................................................8-6
Life Vest ..............................................................................................................................8-7
Smoke Goggle Units ...........................................................................................................8-8
8-iv For Training Purposes Only
May 03
EMERGENCY EQUIPMENT P I LOT T R A I N I N G GU I D E
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EMERGENCY EQUIPMENT
For Training Purposes Only
May 03
8-1
P I LOT T R A I N I N G GU I D E
CHAPTER 8: EMERGENCY EQUIPMENT Introduction
The Challenger 604 is equipped with emergency equipment essential to the safety of
the passengers and crew.
The systems covered in this chapter are:
• Oxygen system
• Emergency exits
• Locating devices
• Miscellaneous emergency equipment
This chapter deals only with factory-installed equipment. Individual aircraft may have
other important emergency equipment installed. Refer to your Aircraft Operating
Manual and Airplane Flight Manual supplements for the use of items installed at the
Completion Center.
Oxygen System
Description
An 1850-psi gaseous oxygen system is installed at the factory to supply oxygen to the
flight crew and passengers during an emergency. The oxygen system consists of the
following subsystems:
• Flight compartment
• Passenger compartment
• Therapeutic
• Portable oxygen bottle
There are two different configurations of oxygen supply bottles installed on the
Challenger 604. Although each configuration is unique, there is no difference in
operation.
Components and Operation
Single-Bottle System
The single-bottle system consists of one storage bottle, a ground servicing panel, and
associated masks/regulators. The oxygen storage bottle (1260 liters/50.0 cubic feet) is
located in the forward avionics bay.
Dual-Bottle System
The dual-bottle system consists of two storage bottles, a ground servicing panel, and
associated masks/regulators. The flight compartment and passenger oxygen storage
bottles (2603 liters/115 cubic feet per bottle) are located in the forward avionics bay.
EMERGENCY EQUIPMENT
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Jan 04
P I LOT T R A I N I N G GU I D E
Oxygen for the flight crew is provided through a diluter demand regulating system. A
quick-donning, inflatable harness mask is installed in a container at each side console.
Portable Oxygen Bottle
A portable oxygen bottle is provided for the crew to use in moving around the cabin
and is normally located in a placarded position behind the pilot.
Passenger Compartment
Dropdown masks installed above all of the passenger seats and in the lavatory provide
passenger oxygen. The passenger masks are fixed-dilution (free-flow) type, which
provides a mixture of oxygen and cabin air at ambient pressure. They are designed for
use at cabin pressure altitudes below 25,000 feet. When the passenger oxygen system
is active, the PAX OXY ON caution EICAS message is displayed.
Therapeutic
Provisions are made to install therapeutic oxygen ports in the passenger compartment.
This system is used for first aid and normally supplies oxygen to four ports (forward
left, aft left, forward right and aft right) at mid-height along the cabin.
Controls and Indicators
Overboard Discharge Indicator(s)
If the oxygen storage bottle pressure becomes excessive, all oxygen will be vented
overboard through a relief valve in the right forward fuselage.
Single-Bottle System
A green frangible disk located below and aft of the ground servicing panel will
fragment to indicate the relief valve has activated due to an overpressure. The relief
valve will activate when the HP module pressure exceeds approximately 2600 psi or
when the LP module pressure exceeds 130 psi.
Dual-Bottle System
In dual-bottle systems, there are two green frangible disks located below and aft of the
ground servicing panel to indicate that the relief valve has activated. One disk will
rupture if the HP module pressure exceeds approximately 2800 psi. The other disk will
rupture if the LP module pressure exceeds 90 psi.
In all cases, an amber OXY LO PRESS message will be displayed on the EICAS when
the oxygen pressure falls below 800 psi.
EMERGENCY EQUIPMENT
For Training Purposes Only
May 03
8-3
P I LOT T R A I N I N G GU I D E
Oxygen System Panel
Figure 8-1
BRT
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
70 75
1840
3200
200
SPOILERS -0.5
-4
1990
1900
1805
1710
1620
1530
1435
1340
100
80
60
40
20
0
-20
-40
OXY CYL SERVICING
CHARGE CYL AT
RATE NOT TO EXCEED
200 PSI (1379)
MIN. TO “FULL”
PRESSURE
FULL PRESS
AMBIENT
TEMP
STATUS PAGE
Bonding
Jumper
Refill Line
(High press.to
oxygen bottle)
Ground Service
Panel Indicator
Filler Valve Dust Cap and
Chain Assy
Oxygen Pressure
Green
Amber
- 800 psi and above
- below 800 psi
P604_08_007
Service Panel
13720
13100
12445
11790
11169
10549
9894
9239
PSI kPa
37.8
26.7
15.6
4.4
-6.7
-17.8
-28.9
-40.0
F° C°
EMERGENCY EQUIPMENT
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May 03
P I LOT T R A I N I N G GU I D E
Flight Compartment
Oxygen for the flight crew is provided through a diluter demand regulating system. A
quick-donning, inflatable-harness mask is installed in a container at each side console.
Each container has a test lever, a yellow flow (eye) indicator, oxygen ON flag, a set of
quick-release doors and connections for the oxygen and communications lines.
Pressing the RESET/TEST switch can test oxygen flow through the regulator. The
flow indicator (blinker) displays a yellow cross when oxygen is flowing. The flow
indicator is black when there is no flow. When the mask is in use, a white ON flag
comes into view on the left door of the container to indicate that the oxygen shutoff
valve is open. When the mask is no longer required, closing the container doors and
pressing the RESET/TEST switch stops the flow of oxygen to the mask and removes
the white ON flag.
The crew oxygen masks have controls located on the mask. The controls have the
following selections:
Normal /100% Lever
• NORMAL – A diluted mixture of oxygen and ambient air adjusted for cabin
altitude
• 100% - Pure oxygen (100%) is delivered at a pressure dependent on cabin altitude
Emergency Flow Control Knob
• NORMAL (Unmarked) – Oxygen is regulated on demand
• EMERGENCY – A constant flow of oxygen is delivered at a positive pressure
• PRESS TO TEST (Momentary) – Purges the mask of smoke or noxious fumes
Microphone Control
Each mask has a microphone installed, which can be activated on the Audio Control
Panel by selecting MASK/BOOM MIC switch to MASK.
Inflatable Harness Control
The flight deck masks are designed to be removed from their containers and donned
with one hand. This is accomplished by squeezing the red tabs on either side of the
oxygen line to inflate the harness while pulling the mask from the container. The
inflated harness is placed over the head, and the mask is positioned over the nose and
mouth. Releasing the red tabs deflates the harness, pulling the mask snugly against the
face.
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P I LOT T R A I N I N G GU I D E
The harness is not designed to be donned over headsets or
eyeglasses. These should be removed prior to using the mask.
Flight Deck Oxygen Masks
Figure 8-2
NOTE
Press to
Test/
Emergency
Button
Plate
(inflation
control)
Microphone
Lead
Microphone
Regulator
"N-100%"
Manual
Control
Reset/Test
Switch
Oxygen
Line
Oxygen
Supply
Stowage
Box Microphone
Jack
Oxygen
"ON"
Indicator
Flow
Indicator
Reset/
Test
Switch
Oxygen
Shutoff
Valve
Inflatable
Harness
Mask
P604_08_008
Mask
Regulator
Oxygen
Line
EMERGENCY EQUIPMENT
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May 03
P I LOT T R A I N I N G GU I D E
Quick-Donning Oxygen Mask Settings
Figure 8-3
EICAS Messages
MESSAGE MEANING AURAL WARNING
(IF ANY)
GALLEY OVHT Galley overheat detected (if galley overheat detector
installed). TRIPLE ATTENSON
SMOKE BAGGAGE BAY The detector has sensed smoke in the baggage door
compartment. “SMOKE”
SMOKE TOILET The detector has sensed smoke in the lavatory area. “SMOKE”
OXY LO PRESS Crew oxygen bottle pressure is less than 800 psi.
PAX OXY ON Passenger oxygen masks are deployed.
EICAS Messages
Table 8-1
N
100%
PUSH
EMERGENCY
PRESS
TO
TEST
N
100%
PUSH
EMERGENCY
PRESS
TO
TEST
P604_08_011
NORMAL &
HALF-CIRCLE
100% &
HALF-CIRCLE
EMERGENCY PRESS TO TEST
N
100%
PUSH
EMERGENCY
PRESS
TO
TEST
N
100%
PUSH
EMERGENCY
PRESS
TO
TEST
EMERGENCY
OXYGEN
MASK
PRESS
TO
TEST
AND
RESET
EROS
100%
PUSH
OXYGEN STOWAGE BOX
Release Lever
Emergency
Flow Control
Oxygen
Supply Hose
Reset / Test
Lever
Blinker
Normal /
100% Lever
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May 03
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P I LOT T R A I N I N G GU I D E
Passenger Oxygen
The dropdown masks are controlled by the PASSENGER OXYGEN control panel
which is located on the copilot’s side console. There are three modes of operation:
• CLOSED – Stops the oxygen supply to the dropdown masks
• NORMAL – The dropdown masks deploy when the altimetric valve senses the
cabin altitude is greater than 10,500 feet or 14,500 feet (aircraft S/N dependent)
and oxygen is supplied to the masks
• OVERRIDE – The dropdown masks deploy and oxygen is supplied to the masks
In the event the dropdown masks do not deploy, the door on the mask box can be
opened by inserting a long, thin object into the release hole.
Passenger Oxygen Control Panel
Figure 8-4
Therapeutic
Therapeutic oxygen is controlled from the flight compartment by a switch/light on the
PASSENGER OXYGEN control panel. Selecting the switch to ON illuminates the
light and oxygen will be supplied to the ports in the cabin for first aid use.
PASSENGER OXYGEN
THERAPEUTIC
OXYGEN
ON
TEST
PORT
NORMAL
CLOSED OVERRIDE
P604_08_013
EMERGENCY EQUIPMENT
8-8 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
Emergency Exits
Refer to Chapter 1 Airplane General for operation of the passenger door and the
overwing emergency exit.
Main Entrance Door
The main entrance door is classified as a Type I emergency exit and is the normal
means of exit in an emergency.
Overwing Emergency Exit
The overwing emergency exit is a removable plug-type hatch and provides access to
the right upper wing surface. It is classified as a Type III emergency exit. This
emergency exit has an escape rope (lifeline) stored to the right of the exit window,
with one end attached to the fuselage.
Emergency Egress Lighting
The Challenger 604 is equipped with an Emergency Egress Lighting System that
operates for approximately 15 minutes from the time of activation. The Emergency
Egress Lighting System location and operations are covered in Chapter 16 Lighting.
EMERGENCY EQUIPMENT
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May 03
8-9
P I LOT T R A I N I N G GU I D E
Locating Devices
Components and Operation
Emergency Locator Transmitter (ELT)
The ELT is located in the tail cone of the airplane and is activated automatically by
G-forces in the event of a crash. The ELT transmits a signal on the international
emergency frequencies of 121.5 and 243.0. A sealed battery pack is installed inside the
ELT and provides at least 48 hours of operation.
Underwater Locating Devices (ULDs)
In addition to the ELT, there are Underwater Locating Devices (ULDs), which are part
of the Flight Data Recorder (FDR) and the Cockpit Voice Recorder (CVR) systems.
The ULDs automatically provide a locating signal should the airplane become
submerged in water.
Controls and Indicators
The ON/ARM switch located on the ELT panel controls the emergency locator
transmitter.
With the ELT ON/ARM switch set to ARM, the automatic operating mode is selected
and the ELT will activate when impact G forces are sufficient. The ON position
permits ELT manual operation when desired. When the transmitter is in operation, the
ON light on the ELT panel will illuminate.
ELT System - Control Panel
Figure 8-5
ELTE L/TCVR MIC CONTROL PANEL
ON
ARM
FOR AVIATION
EMER USE ONLY
UNAUTHORIZED OPERATION PROHIBITED
ON
P604_08_006
EMERGENCY EQUIPMENT
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May 03
P I LOT T R A I N I N G GU I D E
Miscellaneous Emergency Equipment
Components and Operation
Fire Extinguishers
The Challenger 604 normally has two variable-size handheld fire extinguishers. One
of the extinguishers is located in the Flight Compartment on the bulkhead behind the
copilot’s seat. The other is located at a designated area in the cabin and is marked by a
placard. Handheld fire extinguisher operations are covered in Chapter 9 Fire
Protection.
IF A FIRE EXTINGUISHER IS TO BE DISCHARGED IN THE
FLIGHT COMPARTMENT, ALL FLIGHT CREW MUST WEAR
OXYGEN MASKS WITH EMERGENCY SELECTED (100%
OXYGEN).
Crew exposure to high levels of Halon vapors may result in
dizziness, impaired coordination and reduced mental alertness.
Crash Axe
A crash axe is located on the bulkhead behind the pilot’s seat.
Crash Axe
Figure 8-6
WARNING
NOTE
P604_08_002
EMERGENCY EQUIPMENT
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May 03
8-11
P I LOT T R A I N I N G GU I D E
First Aid Kit
The aircraft is typically equipped with at least one medical first aid kit. The factoryinstalled
first aid kit is normally located on the bulkhead behind the pilot.
Life Vest
Life vests are provided for the pilot, the copilot, and each passenger in the cabin. The
flight crew life vests are stowed in a pocket beneath the crew member’s seat. The
passenger life vests are stowed under each passenger seat. Each life vest includes an
automatic (CO2 cartridge) and a manual (oral inflation) system. In addition, a locator
light powered by an automatic seawater battery is installed.
Life Vest
Figure 8-7
Waist Strap and Clip
Waist strap pull to tighten
Locator Light
(clear)
Waist Strap And Clip
Tab (yellow)
Waist strap - pull to
tighten
Oral
Inflation
Tube (red)
Oral Inflation Tube (red)
Used to manually inflate half
life vest if cartridge inflation
does not work
Automatic
Seawater
Battery
P604_08_005
Inflation Tab (red)
Pulling tab automatically
inflates life vest using CO
cartridge
2
Signal Light Tab
(yellow)
Pull to light
Inflation Tab (red)
Jerk to inflate
EMERGENCY EQUIPMENT
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May 03
P I LOT T R A I N I N G GU I D E
Life Raft
Up to two life rafts of variable size may be installed. The normal location for life raft
storage is beneath the divan near the overwing exit. Location may vary according to
interior completion specifications. Consult your Airplane Flight Manual and
Operating Manual supplements for life raft storage location.
Smoke Goggle Units
Smoke goggle units for each flight crew oxygen mask are contained in a pouch located
in the aft portion of the left and right side consoles.
Smoke Goggle Units
Figure 8-8
P604_08_012