Publications and Training Solutions Course Syllabus:

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1 COURSE TITLE: PROLINE 4 CRJ (200/700/900 series) Level I Operators & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC IAPS Power Supply PWR I/O Concentrator IOC X Configuration Strapping Unit CSU IAPS Environmental Controller IEC Lightning/HIRF Protection (Left) Lightning/HIRF Protection (Right) Maintenance Diagnostic Computer LHP LHP MDC X Display Control Panel DCP Electronic Flight Display (PFD, MFD) EFD X EICAS Data Concentrator Unit DCU X EICAS Control Panel ECP Electronic Flight Display (ED) EFD X Lamp Driver Unit LDU Air Data Computer ADC 850A Air Data Reference Panel ARP , 104 Attitude Heading Computer AHC-85E Remote Compensation Panel RCP Flux Detector Unit FDU Control Display Unit CDU Flight Management Computer (in IAPS) FMC November 9,

2 EQUIPMENT NOMENCLATURE PART NUMBER Data Base Unit (DSDD Disk Drive) Flight Control Computer (in IAPS) DBU FCC Flight Control Panel FCP Primary Servo (aileron) SVO 85A , 101 Primary Servo (elevator) SVO 85B , 101 Linear Actuator (rudder) SVL Radio Tune Unit RTU VHF Comm Transceiver VHF 422C VHF Navigation Receiver VIR DME Transceiver DME Radio Altimeter ALT 55B Radio Altitude Converter RAC Mode S Transponder TDR 94D HF Receiver/Transmitter HF 9031A HF Antenna Coupler HF GPS Navigation Receiver GPS Receiver/Transmitter/Antenna (14 inch) RTA Weather Radar Control Panel WXP November 9,

3 PREREQUISITES: 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 will 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: 5 Days TRAINING DEVICES: CRJ Test Rig (Cedar Rapids) TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Information sheets 3. Course Notebook 4. Canadair Regional Jet CRJ-700/705/900 Avionics System Manual Excerpt 5. Canadair Regional Jet CRJ-200 Avionics System Manual Excerpt 6. CRJ-200 Diagnostic Guide CRJ-700/900 Diagnostic Guide REFERENCES: 1. Canadair Regional Jet CRJ-700/705/900 Avionics System Manual Canadair Regional Jet CRJ-200 Avionics System Manual Pro Line 4 CRJ Pilot Guide November 9,

4 PROLINE 4 CRJ (CANADAIR REGIONAL JET) I. Welcome A. Training Overview (Customer Ambassador) 1. Welcome 2. Student Registration 3. Student Policies and Procedures II. Introduction to Materials and Handouts A. System manual introduction and use B. Test and troubleshooting guide introduction C. Equipment Description D. Equipment Specifications 1. Business & Regional Systems Equipment Leading Particulars III. Data Bus A. Why we use Data Buses B. Arinc Data Buses 1. Arinc Arinc 453 C. CSDB Data Buses IV. Integrated Avionics Processing System (IAPS) A. Over view B. System architecture C. Integrated Card Cage (ICC) D. Lightning/HIRF protection (LHP) November 9,

5 E. Power supply module (PWR) F. IAPS environmental controller (IEC) G. Input output concentrator (IOC) H. Maintenance Diagnostic Computer (MDC) I. Configuration strapping unit (CSU) J. Detailed functional theory 1. IAPS power distribution 2. Temperature monitoring 3. Overheat reporting 4. Power supply inhibit 5. CSU detailed theory K. Maintenance and troubleshooting 1. PWR fault indications 2. IEC fault indications 3. Status messages 4. Diagnostics V. Maintenance Diagnostics B. Maintenance Diagnostic Computer (MDC) VI. Electronic Flight Instrument System (EFIS) B. Electronic Flight Display (EFD) November 9,

6 1. Primary Flight Display (PFD) 2. Multifunction Display (MFD) a. MFD formats 3. EFD Detailed Theory of operation a. Reversionary mode select b. Cooling requirements C. Display Control Panel (DCP) 1. DCP switchology description 2. Detailed theory of operation VII. Engine Indicating and Crew Alerting System (EICAS) B. Electronic Flight Display (EFD)/EICAS Display (ED) 1. Primary ED 2. Secondary ED C. Secondary ED 1. Display formats D. EICAS Control Panel (ECP) 2. ECP switchology description 3. Detailed theory of operation E. Data Concentrator Unit (DCU) 2. Integration theory 3. Theory of operation F. Lamp Driver Unit G. Maintenance and troubleshooting 1. Status messages 2. Diagnostics VIII. Air Data System (ADS) B. Air Data Computer November 9,

7 C. Air Reference Panel (ARP) 2. ARP switchology description 3. Theory of operation D. Maintenance and troubleshooting 1. Status message 2. Diagnostics IX. Attitude Heading System (AHS) B. Attitude Heading Computer (AHC) C. Remote Compensation Panel (RCP) D. Flux Detector Unit (FDU) E. Maintenance and troubleshooting 1. Diagnostics 2. Alignment procedure X. Flight Control System (FCS) B. Flight Control Computers (FCC) C. Flight Control Panel (FCP) 2. FCP switchology description 3. Theory of operation D. Primary Servo (SVO) November 9,

8 E. Servo Linear Actuator F. Yaw Damper Engage Panel (YDEP) 2. Operation 3. Theory of operation G. Autopilot and yaw damp detailed theory of operation of fail passive system 2. Description of null seeking servo loops 3. Description of yaw damp system H. Autopilot diagnostics 1. Entering and using autopilot diagnostics a. Input mode b. Output mode c. Report Mode 2. Servo Spin test 3. Linear actuator test XI. 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 day database load procedure 2. Fault history download procedure November 9,

9 XII. Database Loading Operations B. Data Base Unit (DBU) 3. Operation a. Uploading databases b. Downloading data C. Personal Computer Dataloader (PCD) 3. Operation a. Uploading databases b. Downloading data XIII. Radio Sensor System B. Radio Tuning Unit (RTU) 2. Operation 3. Theory of operation C. VHF Comm receiver/transmitter (VHF) 3. Datalink/CPDLC/Link D. VOR/ILS/MB Receiver (VIR) E. Distance Measuring Equipment (DME) F. Automatic Direction Finder receiver (ADF) G. High Frequency receiver/transmitter (HF) November 9,

10 H. HF Antenna Coupler (HF) I. Radio Altimeter (ALT) and Radio Altimeter Converter (RAC) J. Mode S transponder (TDR-94D) with Traffic Alert and Collision Avoidance System (TCAS) K. Description 1. Theory of operation L. General Maintenance Procedures for Comm /Nav /Pulse Equipment 1. Flightline diagnostic procedures 2. Antenna maintenance considerations XIV. Weather Radar (WXR) B. Microwave Radiation Hazards 1. AC 20-68B C. Weather radar theory 1. Mediums that reflect 2. VIP or Z levels D. Receiver Transmitter Assembly (RTA-8xx) E. Maintenance 1. Radome maintenance (AC 43-13) 2. Flightline diagnostic procedures XV. Critique/Review November 9,

Publications and Training Solutions Course Syllabus:

Publications and Training Solutions Course Syllabus: COURSE TITLE: Pro Line Fusion King Air C90GT/B200Gt/B200CGT/B300 Level I Operations & Flight Line Maintenance PREREQUISITES: Students should have basic knowledge of aircraft avionics systems and a working