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Figure 16−10−8 Chart Holder and Map Reading Lights − Location 16−10−11
Figure 16−10−9 Centre Lighting Panel 16−10−12
Figure 16−10−10 Pilot’s Lighting Panel 16−10−13
Figure 16−10−11 Copilot’s Lighting Panel 16−10−14
Figure 16−10−12 Boarding Light 16−10−15
Figure 16−10−13 Stair Lights Control 16−10−16
Figure 16−10−14 Passenger Compartment Signs (Typical) 16−10−17
Figure 16−10−15 Nose Landing Gear Service Light 16−10−18
Figure 16−10−16 Service Lights − Location and Controls 16−10−19
Figure 16−10−17 Exterior Emergency Lights 16−10−21
LIGHTING
Table of Contents
Vol. 2 16−00−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
Page
GENERAL
The lighting system provides interior and exterior illumination of the aircraft. In addition, lights provide
information and guidance to passengers in normal and emergency situations.
The lighting system includes:
• Exterior lighting
• Flight compartment lighting
• Passenger compartment (cabin) lighting
• Cargo and service compartment lighting
• Emergency lighting
EXTERIOR LIGHTING
Description
The exterior lighting system is controlled from the EXTERNAL LTS panel or the LANDING LTS
panel, and consists of the following:
• Navigation lights
• Anti-collision lights
• Wing inspection lights
• Beacon light
• Logo lights
• Landing lights
• Recognition/taxi lights
Components and Operation
Navigation Lights
The navigation lights are located in each wing tip, fuselage tail cone tip, and at the tip of the
stabilizer fairing. A wing tip assembly contains two navigation lights that work simultaneously.
The NAV switch controls the navigation lights (see Figure 16−10−2).
Wing Tip Navigation Light
Figure 16−10−1
LIGHTING
Description
Vol. 2 16−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EXTERIOR LIGHTING (CONT'D)
Anti-Collision Lights
The anti-collision lights consist of two wing tip strobe lights, located in the wing tip assembly,
and one strobe light at the tip of the fuselage tail cone, co-located with the navigation lights.
The A/COLL switch controls the anti-collision strobe lights (see Figure 16−10−3).
Wing Inspection Lights
There are two wing inspection lights located on the fuselage, forward of the root of each wing.
The WING-INSP switch controls the left and right wing inspection lights (see Figure 16−10−3).
Beacon Lights
There are two red beacon lights located on the top and bottom of the fuselage, near the middle
of the aircraft.
The BEACON switch controls the beacon lights (see Figure 16−10−4).
Logo Lights
The logo lights are located on top of the aircraft’s engine pylons. When selected, these lights
illuminate the aircraft’s vertical stabilizer.
The LOGO switch controls the logo lights (see Figure 16−10−4).
Landing Lights
There are four landing lights on the aircraft. Two lights are located in the nose, and one light is
located in each wing, at the root.
The NOSE switch, located on the LANDING LTS panel, controls both nose landing lights
simultaneously (see Figure 16−10−7).
The LEFT switch and the RIGHT switch, located on the LANDING LTS panel, control each wing
landing light respectively.
If the optional pulse lighting system is installed, the PULSE light selection is made from a
modified (three-position) version of the left and right landing light switch.
NOTE
Turning on the left or right landing light turns on the respective side
recog/taxi light.
Recognition/Taxi Lights
There are two recognition/taxi lights, co-located outboard of the wing landing lights.
The RECOG/TAXI switch, located on the LANDING LTS panel, controls the recognition/taxi
lights (see Figure 16−10−6).
LIGHTING
Description
Vol. 2 16−10−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EXTERIOR LIGHTING (CONT'D)
Controls and Indicators
Exterior Lights − Navigation Lights Location
Figure 16−10−2
LIGHTING
Description
Vol. 2 16−10−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EXTERIOR LIGHTING (CONT'D)
　
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