
Cockpit Reference Guide for the Prodigy
™
Flight Deck 300
190-00761-00 Rev. A 81
Abnormal Operation
Flight
Instruments EAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
TRIM
Aileron or rudder mistrim are denoted with yellow arrows pointing in the direction
ofmistrimontheRollandYawTrimindicators(A).
If takeoff configuration has been selected and the pitch trim position is not within
the green band on the pitch trim scale, the pointer turns red and readout turns red
inversevideo(whitetextonredbackground)(B).
Rudder
Mistrim
Aileron
Mistrim
A - Mistrim
B - Pitch Trim
Outside Takeoff
Configuration
REVERSIONARY MODE
IfthesystemdetectsafailureinPFD1orMFD,reversionarymodeisentered
automatically. Reversionary mode must be entered manually in the case of
PFD2failure.
In reversionary mode, critical flight instrumentation is combined with
engine instrumentation on the remaining display.
Manual activation of reversionary display mode is accomplished by pressing the
DISPLAY BACKUP Button on the appropriate audio panel.
• PFD1–BypressingtheDISPLAY BACKUP Button on the left audio panel.
• MFD–BypressingtheDISPLAY BACKUP Button on the left or the right
audio panel.
• PFD2–BypressingtheDISPLAY BACKUP Button on the right audio
panel.
ABNORMAL COM OPERATION
When a COM tuning failure is detected by the system, the emergency frequency
(121.500MHz)isautomaticallyloadedintotheactivefrequency eld of the COM
radio for which the tuning failure was detected. IntheeventofafailureofbothPFDs,
theemergencyfrequency(121.500MHz)automaticallybecomestheactivefrequency
on both COM radios.
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