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The floor level emergency escape path lighting system operates in conjunction
with the existing emergency light system. The escape path and exit indicators
are designed to motivate the passengers to quickly locate the nearest exit during
emergency evacuations when low visibility conditions exist in the cabin. The
system includes special cues for overwing exit locations and one-way egress
routes. Input power is provided by two 6.0-volt battery packs activated in
conjunction with the existing aircraft emergency lighting system.
The floor level light tracks are installed on the right side of the aisle if facing
forward. The lights are clear and spaced at 20-inch intervals. Opposite each
overwing exit are four red lights spaced at four-inch intervals to identify these
exits. The last two lights in the track at either end of the cabin are red and
spaced four inches apart. The system is armed or activated through the flight
deck emergency exit light switch (OFF-ARMED-ON). The aisle lighting is
considered tested when the emergency exit light system is tested.
>@BCD EMERGENCY ESCAPE PATH AISLE LIGHTS
The floor proximity emergency escape path aisle lighting has been moved from
the floor to an integral mounting on the aisle-side of the passenger seats.
AIRCRAFT GENERAL
Sec. 6.1 Page 72 737
Rev. 11/15/02 #41 Continental Flight Manual
EMERGENCY LIGHTING AND PASSENGER SIGNS
Flight Deck
< Emergency Exit Lights (EMER EXIT LIGHTS) Switch (guarded)
OFF – Prevents emergency lights system operation if aircraft electrical
power fails or is turned off.
ARMED – All emergency lights illuminate automatically if aircraft electrical
power to DC bus No. 1 fails or AC power is turned off.
ON – All emergency lights illuminate.
= Emergency Exit Lights (EMER EXIT LIGHTS) NOT ARMED Light
Illuminated (amber) – EMER EXIT LIGHTS switch not in ARMED position.
> NO SMOKING Lights Switch
OFF – The NO SMOKING signs are not illuminated.
AUTO – The NO SMOKING signs are illuminated or extinguished automatically
with reference to aircraft configuration.
ON – The NO SMOKING signs are illuminated.
? SEAT BELTS Switch
OFF – The FASTEN SEAT BELTS and RETURN TO SEAT signs are not illuminated.
AUTO – The FASTEN SEAT BELTS and RETURN TO SEAT signs are illuminated or
extinguished automatically with reference to aircraft configuration.
ON – The FASTEN SEAT BELTS and RETURN TO SEAT signs are illuminated.
AIRCRAFT GENERAL
737 Sec. 6.1 Page 73
Flight Manual Continental Rev. 11/15/02 #41
Passenger Cabin
>>@
< Passenger Cabin Emergency Exit Lights Switch (guarded, red)
ON – All interior and exterior emergency lights are illuminated.
NORM – Emergency lights OFF unless activated by the flight deck switch.
BCD
< Passenger Cabin Emergency Lights Switch (guarded)
On – Illuminates all emergency lights and bypasses flight deck control.
AIRCRAFT GENERAL
Sec. 6.1 Page 74 737
Rev. 11/15/02 #41 Continental Flight Manual
EMERGENCY EXIT LIGHT LOCATIONS
>
AIRCRAFT GENERAL
737 Sec. 6.1 Page 75
Flight Manual Continental Rev. 11/15/02 #41
37376053
LIGHTING
INTEGRAL SLIDE
passenger cabin above
EMERGENCY EXIT SIGNS
hatches, and above each
the overwing escape
entry and service door.
in the center of the
ceiling.
and aft lowered ceiling,
passenger cabin
- Located in the
EXIT LOCATOR SIGNS
ESCAPE SLIDE
EMERGENCY
LIGHTING
AISLE LIGHTS
EXTERIOR
- Located in the forward
LIGHTING
SEAT MOUNTED FLOOR
PROXIMITY AISLE
LOCATOR LIGHTS
EMERGENCY EXIT LIGHT LOCATIONS
>@BCD
AIRCRAFT GENERAL
Sec. 6.1 Page 76 737
Rev. 11/15/02 #41 Continental Flight Manual
INTENTIONALLY LEFT BLANK
AIRCRAFT GENERAL
737 Sec. 6.1 Page 77
Flight Manual Continental Rev. 11/15/02 #41
OXYGEN SYSTEM
PASSENGER OXYGEN
The passenger oxygen system is supplied by individual chemical generators
located at each Passenger Service Unit (PSU). Four continuous flow masks are
connected to each generator. A generator with two masks is located above each
attendant station and in each lavatory.
The system is activated automatically by a pressure switch at a cabin altitude of
14,000 feet or when the Passenger Oxygen Switch on the aft overhead panel is
positioned to the ON position. When the system is activated, the PASS OXY ON
light will be illuminated and OVERHEAD will be illuminated on the Master
Caution System.
Activating the system causes the masks to drop from the stowage compartments.
　
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