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EMERGENCY EQUIPMENT Description Vol. 2 08.10.7
Oct 05/06
Passenger Oxygen Control Panel Figure 08.10.4
Therapeutic
Therapeutic oxygen is controlled from the flight compartment by a switch/light on the PASSENGER OXYGEN control panel. Pressing the switch to ON illuminates the light, and oxygen will be supplied to the ports in the cabin for first aid use.
EMERGENCY EQUIPMENT Description Vol. 2 08.10.8
Oct 05/06
OXYGEN SYSTEM (CONT'D)
Crew Oxygen Consumption Data (As per FAR 121.333) (Single Bottle)
The following tables show the total time (in hours and minutes) that oxygen will be available at
various mask settings, during various flight conditions, at initial bottle pressures of 1400 psi and
1850 psi. A margin of safety of 10% was subtracted from the full charge of 1850 psi in all cases.
EMERGENCY EQUIPMENT Description Vol. 2 08.10.9
Oct 05/06
OXYGEN SYSTEM (CONT'D)
Crew Oxygen Consumption Data (As per FAR 121.333) (Dual Bottle)
The following tables show the total time (in hours and minutes) that oxygen will be available at
various mask settings, during various flight conditions, at initial bottle pressures of 1400 psi and
1850 psi. A margin of safety of 10% was subtracted from the full charge of 1850 psi in all cases.
EMERGENCY EQUIPMENT Description Vol. 2 08.10.10
Oct 05/06
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 605 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.
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 MHz. 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.
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