NOTICE

SECTION 3 CESSNA
EMERGENCY PROCEDURES MODEL 208B G1000
GENERAL
OPERATING PROCEDURES - GENERAL
The operating procedures contained in this manual have been
developed and recommended by Cessna Aircraft Company and are
approved for use in the operation of this airplane.
This section contains the Emergency and Abnormal Procedures for
your airplane. For your convenience, definitions of these terms are
listed in Section I. Operating procedures in this airplane flight manual
are organized into Emergency, Abnormal, and Normal Procedures.
Normal procedures are those recommended for routine day-to-day
preflight, flight, and postflight operation and include expanded systems
information and procedures. Some checks, as noted in the Limitations
Section of this airplane flight manual, are required to assure proper
system integrity.
The Garmin G1000 Integrated Avionics System monitors most of the
airplane systems for faults or failures and displays this information to
the crew as messages in the Crew Alerting System (CAS) portion of the
Primary Flight Display (PFD) in front of each pilot. Some Garmin G1000
faults are also displayed as messages in the Primary Flight Display
(PFD) or Multi Function Display (MFD). These messages are listed
within the appropriate portion of the Emergency and Abnormal
procedures sections of the FAA Approved POH/AFM or appropriate
Garmin Cockpit Reference Guide for the 208 series aircraft.
Emergency procedures are generally associated with Red CAS
MSG(s) or Garmin G1000 messages. Some procedures, such as
Maximum Glide/Emergency Landing, are not associated with any
particular message, but can involve one or more messages. All
emergency procedures are organized by appropriate systems and
include each Red CAS or Garmin message if applicable exactly as it
appears on the PFD, or MFD. Emergency Procedures require
immediate pilot recognition and corrective action by the crew. Red CAS
MSG(s) will flash and pressing the WARNING softkey will silence the
repeating chime and change the CAS MSG to steady.
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U.S.
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FAA APPROVED
208BPHBUS-01