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opening too far. Once the door is fully open,
a hook locks the door into position. To unlatch
the hook and let the door close, a release button
inside the cabin (inside left of door opening)
must be pushed (Figure 1-5). This lets the
door move freely.
The locking pins will contact and
damage the painted surface of the
fuselage if an attempt is made to shut
the door with the handle in the closed
(up) position.
The seal system operates passively as the cabin
is pressurized. The seal engages and disengages
when the door opens and closes.
A hinged panel at the main cabin door threshold
is used as a water barrier during ditching
(Figure 1-6). It hinges up to prevent water
from entering the aircraft, and enables the use
of the entrance door as an exit during ditching.
Water barrier must be raised and
latched into position prior to ditching.
WARNING
CAUTION
CITATION MUSTANG OPERATING MANUAL
510OM-00 1-5
Figure 1-5. Entrance Door, Interior Handle, and Latch Release
NOTE
The water barrier is installed at the
main cabin door threshold. Crew
members should be familiar with its
location and operation; and passengers
should be briefed prior to flights
over water.
A monitoring system checks for safe condition
of the door (closed, pins secure, door latched).
There are eight view ports on the inside panel
of the entry door to verify that the eight locking
pins are in the closed position. With the
door closed and handle latched, the pilot
should be able to see the white and green indicators
in each port. (Figure 1-7). Three proximity
switches verify that the door is closed,
latched, and locked by sensing the position of
targets on the closing mechanism of the door
and signals the condition to the CAS:
• The proximity switch on the doorway
surround structure senses the door after
it is closed.
• After the door is latched, a proximity
switch senses the door pin position.
• As the handle catch is engaged, a proximity
switch on the inner handle assembly
senses a flag.
If one of the proximity switches does not sense
its target, the CABIN DOOR message appears
on the CAS.
EMERGENCY EXIT
A plug-type emergency exit (escape hatch) is
on the aft right side of the cabin, above the
wing. It opens inboard. The emergency exit
door can be opened from outside or inside
the airplane (Figure 1-8).
The D-shaped inner door handle is recessed behind
a magnetic cover. The flush-mounted
outer handle is located at the top of the door.
The outer handle is not directly connected to
the inner handle. The outer handle has a green
indicator to show when the door is latched.
Because no other provisions are provided for
securing the escape hatch when the airplane
is unattended, a safety pin with a REMOVE
BEFORE FLIGHT streamer is placed on the
inside of the hatch. The pilot must ensure this
pin is removed prior to flight. The emergency
exit hatch is not connected to the door warning
circuit.
CABIN
The cabin extends from the forward pressure
bulkhead to the aft pressure bulkhead and
CITATION MUSTANG OPERATING MANUAL
1-6 510OM-00
Figure 1-7. Door Pin Indicator
Figure 1-6. Hinged Panel
measures approximately 14 feet in length, 4.7
feet in width, and 4.5 feet in height. Figure 1-
9 shows the interior arrangements. Refer to
Figure 1-10 for interior dimensions.
The standard interior arrangement consists of
two aft-facing and two forward-facing passenger
seats. There is a toilet on the right side of
the fuselage, abeam the cabin entry door. The
toilet is not equipped with a safety belt and cannot
be occupied during taxi, takeoff, or landing.
The cabin area has dropout, constant-flow
oxygen masks for emergency use.
The cabin overhead panels contain individual
air vent outlets and seat lighting for passenger
comfort.
FLIGHT COMPARTMENT
The airplane is equipped with dual controls, including
control yokes, brakes, and rudder pedals
at each crew seat. There are two adjustable
seats with seat belts and shoulder harnesses.
TAIL CONE COMPARTMENT
The tail cone compartment is an unpressurized
area and contains major components of the environmental,
electrical distribution, flight controls,
and engine fire extinguishing systems.
Access is through the tail cone baggage door on
the left side of the fuselage below the engine.
CITATION MUSTANG OPERATING MANUAL
510OM-00 1-7
EXTERIOR
INTERIOR
Figure 1-8. Emergency Exit
　
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