Honeywell PRIMUS 1000 Pilot's Manual page 327

NAV course deviation indicator (CDI) with TO/FROM
indication, 4-40
NAV source distance, 4-40
Navigation (NAV) source annunciations, 4-37
Navigation symbol colors, 4-40
Wind vector (available if FMS is installed), 4-40
Functional divisions, 4-25
ADI (attitude director indicator) display, 4-25
Air Data displays, 4-26
HSI (horizontal situation indicator) display, 4-25
Mode annunciations, 4-25
Slip--skid display, 4-26
IN/HPA button, 4-5
Inclinometer, 4-5
PFD attitude director indicator (ADI), 4-26
Aircraft symbol, 4-31
Airspeed trend vector, 4-34
Altitude trend vector, 4-32
Attitude source annunciation, 4-34
Autopilot status annunciations, 4-32
CAT2 (category 2) ILS annunciations, 4-34
CAT2 deviation scale and pointer, 4-36
Command bar display logic (normal mode), 4-30
Comparison monitor annunciation, 4-33
Flight director couple arrow, 4-31
Flight director mode annunciations, 4-26
Low altitude awareness display, 4-31
Low bank arc, 4-31
Marker beacon, 4-33
MAX SPD/MIN SPD or underspeed warning, 4-34
Pitch limit indicator, 4-29
Pitch scale, 4-29
Radio altitude (RA) decision height annunciator, 4-33
Radio altitude decision height set data, 4-33
Radio altitude display, 4-33
Roll scale and roll pointer, 4-29
Source annunciations, 4-31
Symbol generator (SG) source, 4-34
Vertical deviation scale, 4-30
Vertical track alert (VTA) annunciation, 4-32
Windshear (WDSHEAR) annunciation, 4-34
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
Index (cont)
Index
Index--17