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and navigation systems. The navigation sys-
tem includes GPS, ground-based navigation,
and is WAAS-capable. An integrated engine
indicating and crew alerting system (EICAS)
is included. The Garmin G1000 system man-
ages the  instrument and engine displays, the
autopilot, flight guidance systems, and the
flight director. Terrain and traffic avoidance
systems and color radar are standard equip-
ment. Data link weather capability is available
with subscription.

PUBLICATIONS

The following publications must be immedi-
ately available to the flight crew:

• FAA-approved Airplane Flight Manual

(AFM) contains the limitations, data per-
tinent to takeoffs and landings, and
weight and balance data. Information in
the AFM always takes precedence over
any other publication.

• FA A - a p p r o v e d   C i t a t i o n   M u s t a n g

A b b re v i a t e d   C h e c k l i s t — N o r m a l
Procedures contains abbreviated normal
operating procedures and abbreviated
performance data. If any doubt exists or
if the conditions are not covered by the
checklist, the AFM must be consulted.

• FA A - a p p r o v e d   C i t a t i o n   M u s t a n g

Abbreviated Checklist—Emergency/
Abnormal Procedures contains emer-
gency and abnormal procedures. If any
doubt exists or if the conditions are not
covered by the checklist, the AFM must
be consulted.

• Garmin G1000 Cockpit Reference Guide

for the Citation Mustang

Other publications that are not required to be
in the aircraft include:

• Operating Manual

• Garmin G1000 Pilot’s Guide for the

Cessna Citation Mustang

• FA A - a p p r ove d   We i g h t   a n d   B a l a n c e

Manual

SINGLE-PILOT 
OPERATION

The following are required when the airplane
is operated with a crew of one pilot, per ap-
plicable operating rules:

1. Operable GFC-700 Autopilot

2. Headset with microphone (must be worn)

3. FA A - a p p r o v e d   P i l o t s ’ A b b re v i a t e d

Normal Procedures Checklist (as revised)

4. FA A - a p p r o v e d   P i l o t s ’ A b b re v i a t e d

Emergency and Abnormal Procedures
Checklist 
(as revised)

5. Provisions for storage and retention of

navigation charts, accessible to the pilot
from the pilot station

CITATION MUSTANG

 

OPERATING MANUAL

1-12

510OM-00

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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