Honeywell PRIMUS 1000 Pilot's Manual page 17

Integrated avionics system for embraer 145
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Table of Contents (cont)
Figure
4--31 TCAS II Resolution Advisory Approaching the
Glideslope
4--32 Approach Capture Tracking at DH
4--33 Comparison Monitor Annunciators
4--34 PFD With ARC HSI Display and Caution/Failure
Annunciations
4--35 PFD Caution Indications for Vertical and Course
Deviation
4--36 Failure Indications for ATT, MADC, HDG, CRS
Select and FD
4--37 Excessive Attitude Declutter
4--38 PFD Test Mode
4--39 MFD Common Symbols
4--40 MFD Map Display Symbols
4--41 Map Mode With Weather
4--42 Map Failure/Warning
4--43 Map Mode Without Weather
4--44 Map Mode With Weather
4--45 MFD Plan View
4--46 Plan Mode Caution and Warning Displays
4--47 Typical Plan Mode With Navaid Components and
Flight Plan
4--48 Typical Checklist Display
4--49 MFD With Map Mode Display and Optional TCAS
4--50 Takeoff Display
4--51 Environmental Control System (ECS) System
Display
4--52 Fuel Page
4--53 Hydraulic (HYD) System Page
4--54 Electrical (ELEC) System Display
4--55 Standby Navigation Display (Typical)
4--56 RMU Backup Navigation Display
4--57 RMU Backup Navigation Display With Failures
5--1 EICAS Block Diagram
5--2 EICAS Bezel Controller
5--3 Master Warning and Caution Annunciation Switches
5--4 EICAS Display Functional Divisions
5--5 EICAS Engine Instruments Display
5--6 EICAS in the Takeoff Condition (Typical)
5--7 Engine Instrument Display With Failures
A28--1146--112--00
List of Illustrations (cont)
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PRIMUSr1000 Integrated Avionics System
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4-58
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4-72
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4-101
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5-20
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5-21
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