Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 124

SECTION 3
EMERGENCY PROCEDURES
GENERAL
(Continued)
OPERATING PROCEDURES - GENERAL
•
White annunciators provide general information, indicate
the need for additional crew awareness and the possible
necessity of future pilot action.
•
In order to avoid confusion due to multiple messages, at
critical times, some annunciator(s) are inhibited when a
Line Replaceable Unit (LRU), such as the GEA-71
(Garmin Engine Airframe Computer), has failed.
•
Generally, the following Emergency and Abnormal
Procedures do not direct the pilot to check/reset circuit
breakers. This is considered basic airmanship and can
be accomplished at the pilot's discretion.
•
Except where specific action is required, these
procedures do not specify action when on the ground.
Conditions resulting in a red or amber message should
be corrected prior to flight. Reasons for white
annunciators should be determined prior to flight.
•
If a red or amber annunciation occurs in flight,
consideration should be given to landing at an airport
where corrective maintenance can be performed.
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 POH/AFM, 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 annunciation and 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 POH/AFM or appropriate
Garmin Cockpit Reference Guide (CRG) for 208 series airplanes.
3-8
NOTE
U.S.
CESSNA
MODEL 208B 867 SHP
GARMIN G1000
(Continued)
FAA APPROVED
208BPHCUS-00