PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--5
Index (cont)
PFD caution and failure display, 4-61
Caution (AMBER) annunciations, 4-61
Excessive attitude declutter, 4-66
Failure (RED) annunciations, 4-65
PFD test mode, 4-67
Primary engine displays, 5-7
Cabin pressure and auxiliary power unit (APU) status, 5-18
Digital turbine (N2) display, 5-12
Engine ignition (IGN) annunciation, 5-11
Engine vibration display, 5-14
Fan (N1) speed display, 5-9
Fuel flow (FF PPH FLOW) digital display, 5-13
Fuel quantity (FUEL LB) digital display, 5-13
Gear/flaps/spoiler positions, 5-15
Interstage turbine temperature (ITT) display, 5-11
Oil pressure (OIL PSI) display, 5-12
Oil temperature (OIL °C) display, 5-14
Pitch/roll/yaw trim display, 5-16
Primary engine displays failure indications, 5-20
Primary flight display (PFD), 4-25
Airspeed display, 4-45
Altimeter display, 4-48
ARC display, 4-41
Full compass display, 4-37
Functional divisions, 4-25
PFD attitude director indicator (ADI), 4-26
Vertical speed (VS) display, 4-51
Standby navigation display, 4-96
RMU backup navigation display, 4-98
System display failure annunciation, 4-95
Display controller failures, 4-95
Display system reversionary modes, 4-95
Typical PFD presentations, 4-53
Approach capture tracking at DH, 4-58
Climb to initial altitude, 4-54
Comparison monitoring, 4-59
Enroute cruise, 4-55
Setup for approach, 4-56
Takeoff (TO) mode, 4-53
Terminal area, 4-57
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