Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: PROLINE 4 CRJ 700/900 Level I Operators & Flightline Maintenance PREREQUISITES: 1. Students should have basic knowledge of aircraft avionics systems and a working command of the English language (interpreters are available for special cases). PURPOSE: This course provides line maintenance personnel with training to operate and perform flightline maintenance for the Proline 4 system. OBJECTIVES: Upon completing this course, the student should be able to: 1. Provide an overall understanding of Proline 4 Avionics principles and operation. 2. Identify system components and the functional/operational characteristics of each line replaceable unit (LRU). 3. Identify typical aircraft system interface/system architecture. 4. Perform fault isolation to a faulty LRU using built in test diagnostics. COURSE LENGTH: 4.5 Days TRAINING DEVICES: 1. CRJ Test Rig (Cedar Rapids) 2. Customer aircraft if available Rockwell Collins. All rights reserved. Page 1
2 TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Information sheets 3. Video/CBT 4. Course Notebook 5. Canadair Regional Jet Avionics System Manual Pro Line 4 Avionics System for the CRJ-700/900/1000 Operator s Guide Canadair Regional Jet Avionics System Diagnostic Guide REFERENCES: 1. Bombardier Regional Aircraft CRJ-700/900 Avionics System Manual Rockwell Collins. All rights reserved. Page 2
3 COURSE OUTLINE 0. Welcome & Introductions A. Training Overview (Customer Ambassador) i. Welcome ii. Student Registration iii. Student Policies and Procedures iv. Introduction to Materials and Handouts v. System Manual Introduction and Use vi. Test and Troubleshooting Guide Introduction 1. Chapter 1 Data Bus A. Why we use Data Buses B. ARINC Data Buses i. ARINC 429 ii. ARINC Chapter 2 Integrated Avionics Processing System (IAPS) A. IAPS System Overview B. System Architecture C. IAPS Card Cage (ICC-4006) iii. Fault Indications D. Lightning HIRF Protection (LHP) iii. Fault Indications E. Power Supply Module (PWR) 2017 Rockwell Collins. All rights reserved. Page 3
4 iii. Fault Indications F. Internal Environmental Controller (IEC) iii. Fault Indications G. Input Output Concentrator (IOC) iii. Fault Indications H. Maintenance Diagnostic Computer (MDC) iii. Fault Indications I. Configuration Strapping Unit (CSU) J. Detailed Functional Theory i. IAPS Power distribution ii. Temperature Monitoring iii. Overheat reporting iv. Power Supply inhibit 3. Chapter 3 Electronic Flight Instrument System (EFIS) B. Electronic Flight Display (EFD) 2017 Rockwell Collins. All rights reserved. Page 4
5 i. Primary Flight Display (PFD) ii. Multifunction Display (MFD) 1. MFD Formats iii. Detailed theory of operation 1. Reversionary modes 2. Cooling requirements C. Display Control Panel (DCP) i. DCP Switchology description ii. Detailed Theory of Operation 4. Chapter 4 Engine Indicating and Crew Alerting System B. Electronic Flight Display (EFD)/EICAS Display (ED) i. Primary ED ii. Secondary ED C. Secondary ED i. Display formats D. EICAS Control Panel (ECP) ii. ECP switchology description iii. Detailed theory of operation E. Data Concentrator Unit (DCU) ii. Integration theory i F. Lamp Driver Unit 2017 Rockwell Collins. All rights reserved. Page 5
6 G. Maintenance and troubleshooting i. Status messages ii. Diagnostics 5. Chapter 5 Maintenance Diagnostic Computer (MDC) B. Maintenance Diagnostic Computer (MDC) iii. Operation 6. Chapter 6 Air Data System (ADS) B. Air Data Computer C. Air Reference Panel (ARP) ii. ARP switchology description i D. Maintenance and troubleshooting i. Status message ii. Diagnostics 7. Chapter 7 Attitude Heading System B. Attitude Heading Computer (AHC) 2017 Rockwell Collins. All rights reserved. Page 6
7 C. Flux Detector Unit (FDU) D. External Compensation Unit (ECU) E. Maintenance and Troubleshooting i. Diagnostics ii. Post Installation Check iii. Compass Compensation Procedure iv. Automatic Leveling Procedure 8. Chapter 8 Flight Control System (FCS) B. Flight Control Computers (FCC) C. Flight Control Panel (FCP) ii. FCP switchology description i D. Primary Servo (SVO) E. Servo Linear Actuator 2017 Rockwell Collins. All rights reserved. Page 7
8 F. Yaw Damper Engage Panel (YDEP) ii. Operation i G. Autopilot and yaw damp detailed theory of operation of fail passive system i of null seeking servo loops ii of yaw damp system H. Autopilot diagnostics i. Entering and using autopilot diagnostics 1. Input mode 2. Output mode 3. Report Mode ii. Servo Spin test iii. Linear actuator test 9. Chapter 9 Flight Management System (FMS) B. Flight Management Computer (FMC) C. Control Display Unit (CDU) D. Data Base Unit (DBU) E. Flight Management Data Base operations 2017 Rockwell Collins. All rights reserved. Page 8
9 i. 28 day database load procedure 10. Chapter 10 Radio Sensor System (RSS) B. Radio Tuning Unit (RTU) ii. Operation i C. VHF Comm receiver/transmitter (VHF) D. VOR/ILS/MB Receiver (VIR) E. Distance Measuring Equipment (DME) F. Automatic Direction Finder receiver (ADF) G. High Frequency receiver/transmitter (HF) H. HF Antenna Coupler (HF) I. Radio Altimeter (ALT) and Radio Altimeter Converter (RAC) 2017 Rockwell Collins. All rights reserved. Page 9
10 J. Mode S transponder (TDR-94D) with Traffic Alert and Collision Avoidance System (TCAS) K. Description i. Theory of operation L. General Maintenance Procedures for Comm /Nav /Pulse Equipment i. Flightline diagnostic procedures ii. Antenna maintenance considerations 11. Chapter 11 Weather Radar B. Microwave Radiation Hazards i. AC 20-68B C. Weather radar theory i. Mediums that reflect ii. VIP or Z levels D. Receiver Transmitter Assembly (RTA-8xx) E. Maintenance i. Radome maintenance (AC 43-13) ii. Flightline diagnostic procedures 12. Chapter 90 Summary/Critique/ Review A. Course Summary and Review B. Course Test C. Graduation 2017 Rockwell Collins. All rights reserved. Page 10
11 EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Air Data Computer ADC-850A XXX Automatic Direction Finder ADF Attitude Heading Computer Attitude Heading Computer AHC-85E AHC-MT Radio Altimeter ALT Radio Altimeter ALT-55B Antenna, ADF ANT-462B Aircraft Personality Module APM Air Data Reference Panel ARP Control Display Unit CDU XXX Control Display Unit CDU Comm Management Unit CMU XXX Comm Management Unit CMU Configuration Strapping Unit CSU Control Tuning Unit CTL Control Tuning Unit CTL-23C Data Base Unit DBU Data Base Unit DBU Data Base Unit DBU Display Control Panel DCP XXX 2017 Rockwell Collins. All rights reserved. Page 11
12 EQUIPMENT NOMENCLATURE PART NUMBER Data Concentrator Unit DCU XXX Distance Measuring Equipment Distance Measuring Equipment DME DME EICAS Control Panel ECP External Compensation Unit ECU XXX Electronic Flight Display EFD XXX EICAS Routing Unit ERU Flight Control Computer FCC XXX Flight Control Panel FCP XXX Flux Detector Unit FDU Flux Detector Unot FDU Flight Management Computer FMC XXX Global Positioning System GPS Global Positioning System GPS-4000A Global Positioning System GPS-4000S HF Radio HF-9031A HF Antenna Coupler HF IAPS Card Cage ICC Internal Environmental Controller IEC Input Output Concentrator IOC XXX 2017 Rockwell Collins. All rights reserved. Page 12
13 EQUIPMENT NOMENCLATURE PART NUMBER Input Output Concentrator IOC Lamp Driver Unit LDU Lightening HIRF Protector LHP Lightening HIRF Protector LHP Maintenance Diagnostic Computer Maintenance Diagnostic Computer MDC-4100 MDC XXX XXX Options Control Module OCM XXX Power Supply PWR Rad Alt Converter RAC XXX Remote Compensation Panel RCP Weather Radar RTA Radio Tuning Unit RTU XXX Radio Tuning Unit RTU Servo Mount SMT-87A Servo Mount SMT-87B Servo Linear Actuator SVL XXX Servo SVO-85A Servo SVO-85B Transponder TDR-94D XXX TCAS Antenna TRE Rockwell Collins. All rights reserved. Page 13
14 EQUIPMENT NOMENCLATURE PART NUMBER Traffic Surveillance System TSS TCAS TTR XXX TCAS TTR VHF Comm Radio VHF XXX VHF Comm Radio VHF-422A VHF Comm Radio VHF-422C VHF NAV Receiver VIR XXX VHF NAV Receiver VIR Weather Radar Control Panel WXP Rockwell Collins. All rights reserved. Page 14
MDC , 402, 403, -404, -405 Display Control Panel DCP , 104, 106, -204, 206 Electronic Flight Display (PFD, MFD)
COURSE TITLE: Pro Line 4 Bombardier Challenger CL-604 Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC 4007 822 0781 001 IAPS Power Supply
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