PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Engine Instrument and Crew Alerting System (EICAS)
5-10
Annunciation Meaning
CON Continous
CLB Climb
CRZ Cruise
PWT (To be determined)
T/O--1 Takeoff Mode 1
T/O--2 Takeoff Mode 2
T/O--3 Takeoff Mode 3
ALT T/O--1 Alternate Takeoff Mode 1
ALT T/O--2 Alternate Takeoff Mode 2
ALT T/O--3 Alternate Takeoff Mode 3
R--MODE Reversion Mode
NOTE: At the time of publication of this manual, not all FADEC modes were
activated.
FADEC Modes of Operation
Table 5--2
D FADEC in Control -- The FADEC in control is annunciated as anA
or B next to the N
1
display. It indicates which FADEC is controlling
the engine.
D Automatic Takeoff Thrust Control System (ATTCS) -- When the
reserve takeoff power function is selected, ATTCS is annunciated
in green.
D Reverse Thrust Annunciation -- When reverse thrust is armed,
andthethrustreverserisnormal,a greenREVisdisplayednearthe
N
1
display.
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