Honeywell PRIMUS 1000 Pilot's Manual page 320

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System
M
Maximum permissible exposure level (MPEL), B--12
Memory pages, C--11
MFD bezel controller basic operation, 3-5
Bezel controls, 3-5
Momentary selection, 3-5
Parameter display selection, 3-5
Settable parameters, 3-5
Submenu selection, 3-5
Toggle selection, 3-5
Controller conventions, 3-6
Parameter selected for display, 3-6
Parameter selected for setting, 3-6
Map range control, 3-6
MFD system displays, 4-86
Electrical (ELEC) system, 4-93
Battery voltages and operating temperatures, 4-94
Bus voltage and amperage loads, 4-94
DC power interconnect buses, 4-94
Environmental control system/anti--ice, 4-88
Cabin and cockpit (CKPT) temperature, 4-89
Engine output bleed air temperature, 4-89
Oxygen pressure, 4-89
Fuel system, 4-90
Fuel boost pump status, 4-91
Fuel tank temperature, 4-91
Fuel used, 4-91
Tank fuel quantity, 4-90
Total fuel quantity, 4-91
Hydraulic (HYD) system, 4-92
Brake temperature, 4-93
Electric hydraulic pump status, 4-93
HYD pressure and fluid quantity, 4-92
Takeoff (T/O), 4-86
Aircraft door status, 4-87
Anti--ice (REF A--ICE) status annunciation, 4-87
Engine oil level, 4-87
Engine T/O mode, 4-87
Engine T/O status arrow, 4-88
Reference T/O temperature (REF TO TEMP), 4-87
Index
Index--10
Index (cont)
A28--1146--112--00

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