PRIMUS
r
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 an A
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,
and the thrust reverser is normal, a green REV is displayed near the
N
1
display.