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CONTROLS AND INDICATIONS ........................................................................................ 4-3
CAS Messages ................................................................................................................. 4-3
Master Indicator Lights.................................................................................................... 4-9
Rotary TEST Knob........................................................................................................ 4-10
CAS Message Description............................................................................................. 4-10
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ILLUSTRATIONS
Figure Title Page
4-1 G1000 Block Diagram ............................................................................................. 4-2
4-2 Multifunction Display .............................................................................................. 4-4
4-3 Primary Flight Display............................................................................................. 4-5
4-4 CAS Scroll Buttons .................................................................................................. 4-7
4-5 Master Indicator Lights ............................................................................................ 4-9
4-6 Rotary TEST Knob ................................................................................................ 4-10
TABLES
Table Title Page
4-1 Emergency Mode CAS Messages............................................................................ 4-9
4-2 Rotary TEST Indications ....................................................................................... 4-11
4-3 Red CAS Messages................................................................................................ 4-12
4-4 Amber CAS Messages ........................................................................................... 4-12
4-5 White CAS Messages ............................................................................................ 4-15
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INTRODUCTION
This chapter describes the master warning systems on the Citation Mustang aircraft. The
master warning systems provide a warning of aircraft system malfunctions, indications
of unsafe operating conditions requiring immediate attention, and indications that some
specific systems are in operation. Audio warnings provide further indications.
GENERAL
The master warning system includes a pair of
MASTER WARNING and MASTER CAUTION
lights, and the crew alerting system
(CAS) messages. CAS messages are displayed
by the G1000 engine indicating and crew alerting
system (EICAS).
These lights and messages provide a visual
indication to the pilots of certain faults, functions,
and/or conditions of selected systems.
Each CAS message indicates an individual
system situation, or simultaneous situations on
both sides (left and right) of a dual system.
Additionally, an audio warning system provides
indication of some situations.
CAS messages appear on the EICAS, which is
on the left side of the multifunction display
(MFD). The pilot and copilot can revert to using
their primary flight display (PFD) to view CAS
messages. A red DISPLAY BACKUP button on
each audio panel selects reversionary mode,
which combines displays from the PFD and
MFD (including CAS messages). The combined
TEST
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displays appear on both the selected PFD and
the MFD. If the MFD fails, it automatically reverts
CAS messages to the pilot PFD. When
the MFD and a PFD are in reversionary mode,
the EICAS displays the CAS messages on the
upper-right section of both display panels.
NOTE
Crew alerts associated with the autopilot,
avionics, and engine fire warning/
suppression are displayed
elsewhere in the displays or cockpit.
The crew alerts are described in the
corresponding chapters in this manual.
The abnormal and emergency procedures in this
section are keyed, where applicable, to the appropriate
CAS messages. The rotary TEST knob
provides testing for the master warning system.
DESCRIPTION
The Mustang master warning system uses
cockpit indications (visual and aural) to advise
the crew of important warnings, cautions,
and advisory information about the aircraft and
its systems.
Pressure sensors, temperature sensors,
　
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