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Main Entrance Door 08−10−10
Overwing Emergency Exit 08−10−10
Emergency Egress Lighting 08−10−10
Locating Devices 08−10−10
Components and Operation 08−10−10
Controls and Indicators 08−10−11
Miscellaneous Emergency Equipment 08−10−11
Fire Extinguishers 08−10−11
Crash Axe 08−10−12
First Aid Kit 08−10−12
Life Vest 08−10−12
Life Raft 08−10−13
Smoke Goggle Units 08−10−13
EICAS Messages 08−10−14
SUMMARY
Power Supply and Circuit Breaker Summary 08−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 08−10−1 Oxygen System Panel 08−10−3
Figure 08−10−2 Flight Deck Oxygen Masks 08−10−5
Figure 08−10−3 Quick−Donning Oxygen Mask Settings 08−10−6
Figure 08−10−4 Passenger Oxygen Control Panel 08−10−7
Figure 08−10−5 ELT System − Control Panel 08−10−11
EMERGENCY EQUIPMENT
Table of Contents
Vol. 2 08−00−1
REV 66, Feb 01/07
CHAPTER 8 - EMERGENCY EQUIPMENT
08−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 08−10−6 Crash Axe 08−10−12
Figure 08−10−7 Life Vest 08−10−13
Figure 08−10−8 Smoke Goggle Units 08−10−14
EMERGENCY EQUIPMENT
Table of Contents
Vol. 2 08−00−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
Page
GENERAL
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
Data on airplane doors and emergency exits is contained in Chapter 1, Airplane General. Data on the
emergency lighting system is contained in Chapter 16, Lighting.
OXYGEN SYSTEM
Description
An 1,850-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 (1,260 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 (2,603
liters/115 cubic feet per bottle) are located in the forward avionics bay.
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.
EMERGENCY EQUIPMENT
Description
Vol. 2 08−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
OXYGEN SYSTEM (CONT'D)
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 provide 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.
　
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