
Cockpit Reference Guide for the Prodigy
®
Flight Deck 100
190-00685-04 Rev. A 99
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
ABNORMAL OPERATION
NOTE: The Embraer Phenom 100 Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.
ENGINE
When an engine failure occurs, besides the CAS message corresponding to the
failed engine (“E1 FAIL” or “E2 FAIL”), the corresponding N1 gauge displays the
annunciation “FAIL” in yellow inverse video (black text on yellow background).
Detection of an engine fire causes the red inverse video (white text on red background)
annunciation “FIRE” to be displayed over the ITT gauge.
Engine Failure Indication Engine Fire Indication
CABIN PRESSURIZATION
If the cabin altitude (ALT) reaches a caution level, the readout displays black text
on a yellow background. When cabin altitude is 10,000 feet or greater, the readout
displays as a warning with white text on a red background, and the corresponding
CAS message “CAB ALTITUDE HI” is issued.
If low flow or a cabin leak is detected, the cabin pressure change RATE readout
displays white text on a red background, and the trend arrow turns red.
Excessive cabin differential pressure (DELTA-P) causes the pressure readout
to display a yellow background and black text; warnings are indicated with red
background with white readout text. The CAS message “CAB DELTA-P FAIL”
accompanies this condition.
When oxygen system pressure (OXY) drops below 1590 PSI, the readout is indicated
with black text on a white background; pressure below 730 PSI is shown with yellow
text on a black background. The CAS message “OXY LO PRES” is also displayed.
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