Honeywell PRIMUS 1000 Pilot's Manual page 324

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System
P
PFD caution and failure display, 4-61
Caution (amber) annunciations, 4-61
Autopilot status annunciations, 4-63
Common symbol generator, 4-61
Course deviation failure, 4-62
Course select failure, 4-62
Distance display failures, 4-62
Flight director (FD) failure, 4-62
Maximum/minimum speed (MAX/MIN SPD), 4-64
Radio altimeter failure, 4-62
Same air data source, 4-61
Same attitude source, 4-61
TCAS messages, 4-64
Vertical deviation failure, 4-62
Windshear annunciation (WDSHEAR), 4-64
Yaw damper status annunciations, 4-63
Excessive attitude declutter, 4-66
Parameters, 4-67
Failure (RED) annunciations, 4-65
Attitude reference system failure, 4-65
Heading (HDG) select failure, 4-66
Micro air data computer (MADC) failures, 4-65
PFD test mode, 4-67
Pilot self--test, A--9
Pilot initiated self--test annunciations, A--9
Pilot writeup, 9-1
Commonly used terms, 9-3
Definitions of terms, 9-3
Typical problems, 9-4
Combined vertical and lateral mode problems, 9-9
Lateral mode problems, 9-4
Vertical mode problems, 9-7
Pitch hold mode, 8-25
AP engaged, 8-25
AP not engaged, 8-25
Power--up test, A--8
Pilot self--test annunciations, A--8
Index
Index--14
Index (cont)
A28--1146--112--00

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