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CITATION MUSTANG

 

OPERATING MANUAL

1-2

510OM-00

The Citation Mustang is equipped with a
Garmin G-1000 integrated avionics system.
This three-panel display system integrates flight
instruments, flight guidance, navigation, and
communication systems. Also integrated into
the avionics system are the master warning and
master caution systems and hazard avoidance
systems. The engine indication and crew alert-
ing system (EICAS) is a two-column display on
the left side of the center multifunction display
(MFD). The crew alerting system (CAS) mes-
sages are displayed on the lower left of the
MFD to alert the crew of system emergencies,
abnormal situations, or changes in system op-
eration. EICAS and CAS will be referred to
often in the following chapters.

DIMENSIONS

Figure 1-2 shows a three-view drawing of the
Citation Mustang containing the approximate
exterior and cabin dimensions. 

WEIGHT LIMITATIONS

• Maximum ramp 

weight ............................... 8,730 pounds

• Maximum takeoff 

weight .............................. 8,645 pounds

• Maximum landing 

weight .............................. 8,000 pounds

STRUCTURES

The Citation Mustang (Figure 1-1) is an all-
metal, pressurized, low-wing monoplane with
a swept T-tail. The interior has provisions for
up to four passengers and two crewmembers.
It has one cabin entry door and one emergency
exit. The aircraft has baggage compartments
in the nose and tail cone. Two pylon-mounted
Pratt & Whitney PW615F turbofan engines
are on the rear fuselage.

Figure 1-3 shows braking taxi turning dis-
tance, and Figure 1-4 is a diagram of engine
hazard areas.

The aircraft has five doors:

• Entrance door

• Emergency exit (escape hatch)

• Left nose baggage compartment door

• Right nose baggage compartment door

• Aft (tail cone) compartment door

Each door (except the emergency exit) has a
monitoring system, which provides a specific
CAS message for that door if it is not properly
closed. However, if the monitoring system for
the cabin or nose baggage doors fail to pass a
test on the ground, stops operating, or does not
indicate normal operating condition, the amber
CHECK DOORS message appears.

Figure 1-1. Cessna Citation Mustang

Summary of Contents for CITATION MUSTANG

Page 1: ...accor dance with Title 14 of the Code of Federal Regulations 14CFR23 Part 23 including day night visual flight rules VFR instru ment flight rules IFR single pilot and flight into known icing condition...

Page 2: ...pounds Maximum takeoff weight 8 645 pounds Maximum landing weight 8 000 pounds STRUCTURES The Citation Mustang Figure 1 1 is an all metal pressurized low wing monoplane with a swept T tail The interi...

Page 3: ...CITATION MUSTANG OPERATING MANUAL 510OM 00 1 3 43 17 FT 13 0 M 11 79 FT 3 6 M 14 35 FT 4 37 M 40 56 FT 12 36 M 13 10 FT 3 99 M Figure 1 2 Exterior Three View Drawing...

Page 4: ...FEET 8 M 0 30 60 90 120 150 0 9 18 27 36 45 DISTANCE FEET DISTANCE METERS Figure 1 4 Engine Hazard Areas CURBTO CURB 27 32 FEET 8 33 M 11 79 FEET 3 59 M 15 53 FEET 4 734 M WING TIP LIGHT TO WING TIP L...

Page 5: ...elease but ton inside the cabin inside left of door open ing 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...

Page 6: ...itch on the inner handle assem bly 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 h...

Page 7: ...e cabin overhead panels contain individual air vent outlets and seat lighting for passen ger comfort FLIGHT COMPARTMENT The airplane is equipped with dual controls in cluding control yokes brakes and...

Page 8: ...58 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...

Page 9: ...es to the bottom of the fuselage and is constructed of aluminum Each wing is also a fuel tank Electromechanical speedbrakes and flaps and hydraulically actu ated main landing gear are attached to each...

Page 10: ...y Ensure that the keys are removed from both nose compartment doors prior to flight to pre vent possible ingestion of a key into an engine SYSTEMS ELECTRICAL SYSTEM The Mustang is an all DC aircraft T...

Page 11: ...ional cable operated surfaces An aileron rudder interconnect provides improved lateral stability Trimming is provided by aileron elevator and rudder tabs The eleva tor trim is both mechanically and el...

Page 12: ...If any doubt exists or if the conditions are not covered by the checklist the AFM must be consulted FAA approved Citation Mustang Abbreviated Checklist Emergency Abnormal Procedures contains emer genc...

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