PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Index
Index--15
Index (cont)
Primary engine displays, 5-7
Cabin pressure and auxiliary power unit (APU) status, 5-18
APU exhaust temperature, 5-19
APU status, 5-18
APU turbine speed as a percentage of RPM, 5-19
Cabin pressurization, 5-18
Color differential pressure display, 5-18
Digital turbine (N2) display, 5-12
Engine ignition (IGN) annunciation, 5-11
Ignitor annunciation color definition, 5-11
Engine vibration display, 5-14
Fan (N1) speed display, 5-9
Automatic takeoff thrust control system (ATTCS), 5-10
FADEC in control, 5-10
FADEC mode annunciations, 5-9
FADEC N1 bug and digital target, 5-9
Fan digital display, 5-9
N1 analog scale, 5-9
N1 request bug , 5-9
Reverse thrust annunciation, 5-10
Fuel flow (FF PPH FLOW) digital display, 5-13
Fuel quantity (FUEL LB) digital display, 5-13
Gear/flaps/spoiler positions, 5-15
Flap position, 5-15
Landing gear position, 5-15
Spoiler position, 5-16
Interstage turbine temperature (ITT) display, 5-11
ITT analog scale, 5-11
ITT digital display, 5-11
Oil pressure (OIL PSI) display, 5-12
Oil temperature (OIL °C) display, 5-14
Pitch/roll/yaw trim display, 5-16
Pitch trim, 5-16
Roll trim, 5-17
Yaw trim, 5-17
Primary engine displays failure indications, 5-20
Data acquisition unit (DAU) failure, 5-20
Engine instrument test, 5-21
Engine sensor/interface failure, 5-20
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