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to the hot battery bus and do not require
the battery switch to be in the BATT or
EMER position for operation.
Nose Baggage Compartment
The manual switch assembly of the baggage
light system is an illuminated two-position
rocker switch. The switch is in the baggage
compartment overhead and adjacent to the light
assembly (Figure 3-9). The manual switch applies
DC power to the light. During daylight
hours or when the light is not desired, turn the
manual switch OFF, which disconnects power
from the light. When the switch is OFF, it illuminates
so it is easy to locate at night.
Figure 3-8. No Smoking/Fasten Seat Belt
Sign
Figure 3-7. Emergency Exit Light
3-6 510OM-00
CITATION MUSTANG OPERATING MANUAL
When both nose baggage doors are closed, a
microswitch on each nose baggage door hinge
turns the light off regardless of rocker switch
position.
Aft Baggage Compartment
The toggle switch for the aft baggage light
system is on the right side door opening. The
baggage light is aft of the baggage door on the
upper right side. When the switch is in the
ON position, DC power is applied to the light.
When the aft baggage door is closed, a microswitch
on the door turns the light off regardless
of the manual toggle switch position
(Figure 3-10).
EXTERIOR LIGHTING
LANDING/RECOGNITION/TAXI
LIGHTS
The aircraft is equipped with two lamps that
illuminate for landing and taxi purposes.
The landing lights consist of two 50-watt
sealed high intensity discharge (HID) lamps
in the belly fairing, forward of the forward
wing spar. These lamps are protected behind
tempered glass covers. They are situated so the
flight compartment is shielded from glare
(Figure 3-11).
A LANDING–RECOG TAXI switch on the
LIGHTING panel controls the landing lights.
The LANDING position provides the brightest
illumination for landing. The RECOG TAXI
position dims the lights to a lower intensity.
The landing lights receive power through the
respective LAND/REC LIGHTS circuit breakers
on the aft J-box.
BEACON
The aircraft is equipped with a beacon. The
beacon assembly is on the top of the vertical
stabilizer for optimum line of sight visibility
Figure 3-10. Aft Baggage Light Switch (Figure 3-12).
and Microswitch
Figure 3-9. Nose Baggage Light and
Switch
Figure 3-11. Landing Lights
510OM-00 3-7
CITATION MUSTANG OPERATING MANUAL
The beacon consists of a red LED assembly
with a strobe rate of 50 flashes per minute. The
beacon is controlled by the BEACON switch
on the LIGHTING panel.
ANTICOLLISION LIGHTS
In addition to the navigation lights, each
wingtip assembly contains an anticollision
strobe light. The anticollision lights flash at
a rate of 50 flashes per minute. The lights are
controlled by the ANTI COLL switch on the
LIGHTING panel. The anticollision lights are
powered through the L and R ANTI-COLLISION
LT circuit breakers on the aft J-box.
NAVIGATION LIGHTS
Navigation lights are in assemblies behind
clear tempered glass covers. The lights are
located as follows (Figure 3-13):
• Red forward light—Left wingtip
• Green forward light—Right wingtip
• White rear light—Both wingtips
The navigation lights are controlled by a NAV
switch on the LIGHTING panel. The lights are
powered by the circuit breakers in the aft J-box.
WING INSPECTION LIGHT
A wing inspection light is on the left side of
the fuselage, above and forward of the wing
leading edge. The inspection light assembly
includes a halogen bulb that illuminates the
outboard leading edge of the left wing.
Aircraft crew utilize the light to detect wing
ice accumulation during nighttime flight in
icing conditions. A WING INSP switch on
the LIGHTING panel supplies power to the
lamp. The WING INSP light circuit breaker
is on the left CB panel.
Figure 3-12. Beacon
LEFT (RED)
NAVIGATION
LIGHT
ANTICOLLISION
LIGHT
AFT (WHITE)
NAVIGATION
LIGHT
Figure 3-13. Position Lights
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CITATION MUSTANG OPERATING MANUAL
INTENTIONALLY LEFT BLANK
CHAPTER 4
MASTER WARNING SYSTEM
CONTENTS
Page
INTRODUCTION ................................................................................................................... 4-1
GENERAL.............................................................................................................................. 4-1
DESCRIPTION ....................................................................................................................... 4-2
　
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