Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: Pro Line 4 CRJ200 Flight Line Maintenance Flight Line Maintenance (Level I) PREREQUISITES: Students should have a basic knowledge of aircraft avionics systems and a working command of the English language. Students should be familiar with MS Windows based Operating Systems. PURPOSE: This course provides line maintenance personnel with training to diagnose faults and perform flight line maintenance on the Pro Line 4 system installed in the CRJ200. OBJECTIVES: Upon completing this course, the student should be able to: 1. Provide an overall understanding of Pro Line 4 Avionics principles and operation. 2. Identify system components and the functional and operational characteristics of each Line Replaceable Unit (LRU). 3. Identify typical aircraft system interface and system architecture. 4. Navigate the diagnostics information viewed on the on-board displays. 5. Perform fault isolation to a faulty LRU using built-in test diagnostics. 6. Utilize the flight guidance computer diagnostics to troubleshoot the autopilot system. COURSE LENGTH: 6 Hour 30 Minutes REFERENCES: 1. Canadair Reginal Jet Avionics System Manual Pro Line 4 Avionics System for the CRJ-700/900/1000 Operator s Guide Collins FMS-4200 Flight Management System Pilot s Guide DLM-900/CMU-900 Data Link Management and Communications Management Units Pilot s Guide Rockwell Collins. All rights reserved. Page 1
2 COURSE OUTLINE 0. Welcome & Introductions A. Objectives 1. Primary Flight Display (PFD) A. Introduction PFD B. Introduction - Air Data Reference Panel (ARP) C. Introduction Flight Control Panel (FCP) 2. Air Data System (ADS) - Video A. Introduction B. Identify ADS Components C. Define ADS Component Functionality D. Describe Air Data Indications E. Summary/Test 3. Attitude Heading System (AHS) - Video A. Introduction B. List the Components AHS replaces 2017 Rockwell Collins. All rights reserved. Page 2
3 C. Identify Digital Data Output Components D. Describe AHS Components E. Define ADC Functionality F. Specify when to perform Compass Alignment G. Define AHC Handling Best Practices H. Summary/Test 4. Multifunction Display (MFD) A. Introduction MFD ii. Theory of Operation B. Introduction Display Control Panel (DCP) C. Introduction Weather Radar Panel (WXP) 5. Electronic Flight Instrument System (EFIS) Video A. Introduction B. Describe EFIS Components C. Describe EFIS Component Functionality D. Describe EFIS Operation Features E. Define Flag Annunciations F. Summary/Test 2017 Rockwell Collins. All rights reserved. Page 3
4 6. Weather Radar System (WXR) Video A. Describe WXR Primary Components B. Describe WXR System Operation C. Describe WXR System Indicators 7. Engine Indication and Crew Alert System (EICAS) A. Introduction B. Description C. Operation D. Theory of Operation E. Summary/Test 8. Display Reversion A. Introduction MFD Reversion Panel B. Introduction Center Reversion Panel C. Summary/Test 9. Control Display Unit (CDU) A. Introduction - CDU 2017 Rockwell Collins. All rights reserved. Page 4
5 B. Introduction Data Base Unit C. Summary/Test 10. Flight Management System (FMS) Video A. Identify FMS Components B. Describe FMS Functionality using CDU C. Describe how to Update FMS using the DBU 11. Radios A. Introduction Radio Tuning Unit (RTU) B. Introduction Stand-by Tuning Panel C. Introduction Audio Control Panel (ACP) 12. Aircraft Communication and Reporting System (ACARS) Video A. Define Purpose of ACARS 2017 Rockwell Collins. All rights reserved. Page 5
6 B. Describe ACARS Components C. Describe ACARS Functionality D. Describe How to Perform an ACARS System Check E. Summary/Test 13. Radio Sensor System (RSS) Video A. List RSS Components B. Describe RTU Functionality C. Describe Automatic Instruments 14. Miscellaneous Controls A. Introduction Compass Panel B. Introduction Yaw Damper Panel C. Introduction Flight Control Switches D. Introduction Miscellaneous Test Panel 2017 Rockwell Collins. All rights reserved. Page 6
7 E. Introduction Caution/Warning Lights F. Summary/Test 15. Flight Control System (FCS) Video A. Describe FCS Component Functionality B. Describe FCS Operations C. Summary/Test 16. Integrated Avionics Process System (IAPS) Video A. List IAPS Components B. Describe IAPS Component Functionality C. Summary/Test 17. ARINC 429 Diagnostic Word A. Identify the Make Up of a 429 Diagnostic Word B. Interpret Diagnostic Guide Codes C. Identify Diagnostic Word Layout on MFD 18. Maintenance Diagnostics A. Enter Maintenance Diagnostics B. Identify Maintenance Diagnostics Data C. Exit Maintenance Diagnostics 19. Flight Control Computer (FCC) Diagnostics A. Identify FCC Diagnostic Description B. Identify FCC Diagnostic Modes 2017 Rockwell Collins. All rights reserved. Page 7
8 C. Summary/Test 20. Diagnose FCC Fault A. Perform a Quick Test B. Enter FCC Diagnostics C. Perform Fault Diagnosis D. Exit Diagnostics E. Summary/Test 2017 Rockwell Collins. All rights reserved. Page 8
9 EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Electronic Flight Display EFD / 004 / 006 / 008 / 010 /012 /016 Air Data Reference Panel ARP / 104 Flight Control Panel FCP Air Data Computer ADC-850A / 125 / 140 / 143 / 145 Attitude Heading Computer AHC-85E Flux Detector Unit FDU Remote Compensation Panel RCP Receiver/Transmitter Antenna Weather Radar Control Panel Receiver/Transmitter Antenna (Turb) Weather Radar Control Panel (Turb) RTA WXP RTA WXP EICAS Control Panel ECP Control Display Unit CDU Data Base Unit DBU Display Control Panel DCP / 006 / 008 Flight Management Computer FMC Flight Management FMC / 006 / Rockwell Collins. All rights reserved. Page 9
10 EQUIPMENT NOMENCLATURE PART NUMBER Computer Radio Tuning Unit RTU / 006 / 106 / 108 / 208 Flight Control Computer FCC / 104 / 204 / 304 / 404 / 604 / 704 Aileron Servo SVO-85A / 101 Elevator Servo SVO-85B / 101 Linear Actuator (Rudder) SVL IAPS Card Cage ICC IAPS Environmental Controller Lightning/HIRF Protection (Left) Lightning/HIRF Protection (Right) IEC LHP LHP IAPS Power Supply PWR / 003 Input/Output Concentrator IOC / 002 / 003 / 004 / 005 / 008 / 009 Configuration Strapping Unit CSU Configuration Strapping Unit CSU Maintenance Diagnostic Computer MDC / 002 / 003 / 004 / 005 / 006 / Rockwell Collins. All rights reserved. Page 10
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