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Figure 1-9. Interior Arrangements
CITATION MUSTANG OPERATING MANUAL
1-8 510OM-00
34.24 IN.
(870 MM)
55.00 IN.
(1,397 MM)
54.00 IN.
(1,372 MM)
FS
144.00 IN.
(3,658 MM)
FS
321.00 IN.
(8,153 MM)
FS
202.76 IN.
(5,150 MM)
A
A
FORWARD
PRESSURE
BULKHEAD
FORWARD
DIVIDER
(0.53 IN. THICK)
(13 MM THICK)
AFT PRESSURE
BULKHEAD
24.00 IN.
(610 MM)
46.00 IN.
(1,168 MM)
54.00 IN.
(1,372 MM)
117.71 IN.
(2,990 MM)
58.76 IN.
(1,493 MM)
VIEW A-A
PASSENGER
COMPARTMENT
FLIGHT
COMPARTMENT
Figure 1-10. Interior Dimensions
This door opens the tail cone baggage compartment
(Figure 1-11), which holds 300 pounds.
The tail cone compartment door is secured at
the aft side by mechanical latches and a key
lock and is hinged at the left forward edge. The
door is secured by a key lock, which is monitored
by the CAS. An amber AFT DOOR message
appears if the door is unlocked.
A light switch on the right side of the door opening
is powered from the battery bus and provides
illumination of the tail cone area for preflight
inspection purposes. If the manual switch is
left on, a microswitch in the door track extinguishes
the light when the door is closed.
WING
The wing assembly attaches to the bottom of the
fuselage and is constructed of aluminum. Each
wing is also a fuel tank. Electromechanical
speedbrakes and flaps, and hydraulically actuated
main landing gear are attached to each
wing (Figure 1-12).
An aileron fence is attached to the inboard side
of each aileron.
The wing leading edges are deiced by inflatable
deice boots, which are inflated by regulated
engine bleed-air. Vortex generators and
stall strips are attached to the leading edge
boots (Figure 1-13).
EMPENNAGE
The empennage consists of a vertical stabilizer
with T-tail mounted horizontal stabilizers
(Figure 1-14). The leading edges of the horizontal
and vertical stabilizers are deiced by inflatable
deice boots.
CITATION MUSTANG OPERATING MANUAL
510OM-00 1-9
Figure 1-12. Wing Trailing Edge
Figure 1-13. Stall Strips
Figure 1-14. Empennage
Figure 1-11. Tail Cone Baggage Door
NOSE SECTION
The nose section is an unpressurized storage
area. Various hydraulics components, pneumatic
bottles, oxygen bottle, fresh-air duct,
and radar antenna are located in this compartment
(Figure 1-15). The nose storage
compartment holds up to 20-cubic feet (320-
pounds) of baggage. It has two swing-up doors
(left and right). Each door has a mechanical
lock. Each door has a key-operated cam lock,
forward pin latch, and two independent paddle
latches. The pin latch shows orange when
not latched. Each latch has a switch and indicates
the latch position with the amber
NOSE DOOR L-R CAS message.
A manual light switch is in the compartment
(Figure 1-16). If the manual light switch is left
on, a microswitch at the left and right storage
door assembly extinguishes the storage compartment
light when the doors are closed.
An over-center gas spring on each door holds
the door in the full open position until the
door is closed manually.
Ensure that the keys are removed from both
nose compartment doors prior to flight to prevent
possible ingestion of a key into an engine.
SYSTEMS
ELECTRICAL SYSTEM
The Mustang is an all-DC aircraft. The 28-
VDC electrical power is supplied by two
starter-generators and one 24-volt, 28 amphour
sealed lead acid battery. An optional battery
is a 24-volt, 28 amp-hour NiCad battery.
An external power receptacle is below the
right engine pylon.
For convenience of pilot and passengers, two
DC power outlets are provided in the cabin,
powered by the DC system through a converter.
One DC outlet is in the cabinet behind
the copilot seat and the other is in the aft center
console.
FUEL SYSTEM
The fuel system has two distinct, identical
halves. Each wing tank stores and supplies the
fuel to its respective engine. Fuel transfer
capability is provided. Fuel is heated through
an oil-to-fuel heat exchanger (PRIST is not
required).
ENGINES
Two pylon-mounted Pratt & Whitney PW615F
turbofan engines are on the rear fuselage, and
CITATION MUSTANG OPERATING MANUAL
1-10 510OM-00
Figure 1-16. Nose Baggage Light
Figure 1-15. Nose Storage Compartment
CITATION MUSTANG OPERATING MANUAL
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Cessna塞斯纳公务机飞行手册(5)
