Cockpit Reference Guide

Cockpit Reference Guide for the Prodigy
Flight Deck 100
190-00685-02 Rev. A 93
Annunciations & Alerts
Flight
Instruments EAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
Message Description
DC BUS 1 OFF
DC bus 1 offline
DC BUS 2 OFF
DC bus 2 offline
D-I WINGSTB ON
Deice system in wings and tail ON
E1 CHIP DETECTED
Chip detected by engine 1 oil chip detector
E2 CHIP DETECTED
Chip detected by engine 2 oil chip detector
E1 FADEC FAULT
FADEC fault in engine 1
E2 FADEC FAULT
FADEC fault in engine 2
ELEC SYS FAULT
Electrical system fault
EMER BRK CHECK
Emergency accumulator pressure between 1800 and 2300 psi. System
still operative, but servicing will be necessary in the near future.
EMER BUS OFF
Emergency bus OFF
ENG EXCEEDANCE
Limit exceeded in engine(s) during flight
ENG FIREX DISCH
Engine fire extinguisher discharge
ENG NO DISPATCH
FADEC detected no dispatch fault condition in engine(s)
FLAP NOT AVAIL
Flaps not available
FUEL EQUAL
Fuel quantity asymmetry corrected; XFEED SOV is open
FUEL1 FEED FAULT
DC pump on due to low fuel pressure
FUEL2 FEED FAULT
DC pump on due to low fuel pressure
FUEL 1 PSW FAIL
Fuel pressure switch stuck in “high” position
FUEL 2 PSW FAIL
Fuel pressure switch stuck in “high” position
FUEL PUMP 1 FAIL
Fuel pump 1 failure
FUEL PUMP 2 FAIL
Fuel pump 2 failure
GEA 1 FAIL
Failure of GEA 1
GEA 2 FAIL
Failure of GEA 2
GEA 3 FAIL
Failure of GEA 3
GPU CONNECTED
Ground power unit connected to the aircraft
GSD FAIL
Failure of the GSD
HSDB FAULT
An LRU has stopped communicating over an HSDB
HSDB SW REV POS
HSDB switch in reversionary position
MFD FAN FAIL
Failure of MFD fan
OXY SW NOT AUTO
Oxygen system switch in manual mode
PFD 1 FAN FAIL
Failure of PFD 1 fan
PFD 2 FAN FAIL
Failure of PFD 2 fan
PTRIM SW1 FAIL
Failure of pilot pitch trim switch
PTRIM SW2 FAIL
Failure of copilot pitch trim switch
RAM AIR FAIL
Ram air valve failure
SHED BUS OFF
Shed bus off
SWPS ICE SPEED
Stall Warning System activation angles anticipated due to ice conditions