Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: Pro Line 21 Advanced Bombardier Challenger 300/350 Combo, Level I Operations & Flightline Maintenance 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 21 System. OBJECTIVES: Upon completing this course, the student should be able to: 1. Provide an overall understanding of Proline 21 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: Challenger 300 M-184 Test Rig (If available) TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Information Sheets 3. Student Material 4. Bombardier Challenger 300/350 Pro Line 21 Advanced Avionics System Diagnostic Guide REFERENCES: 1. Bombardier Challenger 300/350 Pro Line 21 Advanced Avionics System Manual Bombardier Challenger 300/350 Pro Line 21 Advanced Avionics System Operator s Guide Rockwell Collins. All rights reserved. Page 1
2 3. Bombardier Aerospace Challenger 300 with IFIS Avionics System Diagnostic Guide Bombardier Challenger 300/350 Pro Line 21 Advanced Flight Management System Operator s Guide COURSE OUTLINE 0. Welcome & Introductions A. Course Overview i. Welcome ii. Student Registration 1. Data Bus A. Why We Use Data Buses B. ARINC Data Buses i. ARINC 429 ii. ARINC Integrated Avionics Processing System (IAPS) B. System Architecture C. Integrated Card Cage D. Power Supply Module E. IAPS Environmental Controller (IEC) F. Input Output Concentrator (IOC) 2017 Rockwell Collins. All rights reserved. Page 2
3 G. Maintenance Diagnostic Computer (MDC) H. Configuration Strapping Unit (CSU) I. Detailed Functional Theory i. IAPS Power Distribution ii. Temperature Monitoring iii. Overheat Reporting iv. Power Supply Inhibit v. CSU Detailed Theory J. Maintenance and Troubleshooting i. PWR Fault Indications ii. IEC Fault Indications iii. Status Messages iv. Diagnostics 3. Electronic Flight Instrument System (EFIS) B. Adaptive Flight Display (AFD) i. Primary Flight Display (PFD) 1. Description 2. Theory of Operation 3. Reversionary Mode Select ii. Multifunction Display (MFD) 1. Description 2017 Rockwell Collins. All rights reserved. Page 3
4 2. Theory of Operation 3. Reversionary Mode Select C. Reversion Switch Panel (RSP) i. RSP Switchology Description ii. Operation iii. Detailed Theory of Operation D. Cursor Control Panel (CCP) i. CCP Switchology Description ii. Operation iii. Detailed Theory of Operation 4. Maintenance Diagnostics B. Maintenance Diagnostic Computer (MDC) iii. Operation 5. Synthetic Vision A. Description B. Theory of Operation 6. Engine Indicating and Crew Alerting System (EICAS) B. MFD i. Display Synoptics C. Cursor Control Panel (CCP) i. CCP Switchology Description ii. Operation iii. Detailed Theory of Operation 2017 Rockwell Collins. All rights reserved. Page 4
5 D. Data Concentrator Unit (DCU) ii. Integration Theory i E. Remote Data Concentrator Unit (RDC) ii. Integration Theory i F. Lamp Driver Unit G. Maintenance and Troubleshooting i. Status Messages ii. Diagnostics 7. Integrated Flight Information System (IFIS) i. System Description B. File Server Unit (FSU) iii. Operation 1. Enhanced Map Functions 2. Electronic Charts 3. Graphical Weather C. External Compensation Unit (ECU) D. File Server Application Software (FSA) 2017 Rockwell Collins. All rights reserved. Page 5
6 of Applications E. Encrypted Application Key (EAK) i. Programming EAKs F. Electronic Charts Region Access Keys i. Programming Region Access Keys G. Maintenance and Troubleshooting i. Database Effective Dates 8. Air Data/Attitude Heading System (ADS/AHRS) B. Air Data Computer (ADC) C. Maintenance and troubleshooting i. Status Message ii. Diagnostics D. Attitude Heading Components and Function E. Controls and Indicators 9. Flight Guidance System (FGS) B. Flight Control Computers (FCC) C. Flight Control Panel (FCP) ii. FCP Switchology Description 2017 Rockwell Collins. All rights reserved. Page 6
7 iii. Operation iv. Theory of Operation D. Primary Servos (SVO) E. Servo Linear Actuator F. Autopilot and Yaw Damp Detailed Theory of Operation of Fail Passive System i of Null Seeking Servo Loops ii of Yaw Damp System G. 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 10. Flight Management System (FMS) B. Flight Management Computer (FMC) C. Control Display Unit (CDU) D. Data Base Unit (DBU) 2017 Rockwell Collins. All rights reserved. Page 7
8 E. Flight Management Data Base Operations i. 28 day Database Load Procedure ii. Fault History Download Procedure 11. Database Loading Operations B. Data Base Unit (DBU) iii. Operation 1. Uploading Databases 2. Downloading Data 12. Radio Sensor System (RSS) B. Radio Interface Unit (RIU) ii. Operation i C. Audio Control Panel (ACP) and Control Panel Electronics (CPE) ii. Operation i D. Radio Tuning Operations ii. Operations 2017 Rockwell Collins. All rights reserved. Page 8
9 is E. VHF Comm Receiver/Transmitter (VHF) iii. Datalink/CPDLC/Link F. VOR/ILS/MB/ADF Receiver (NAV) G. Distance Measuring Equipment (DME) H. High Frequency Receiver/Transmitter (HF) I. HF Antenna Coupler J. SATCOM K. Data Link (CPDLC) ii. General Component Description i L. Radio Altimeter (ALT) 2017 Rockwell Collins. All rights reserved. Page 9
10 M. Mode S Transponder (TDR-94D) with Traffic Surveillance System (TSS) N. General Maintenance Procedures for Comm /Nav /Pulse Equipment i. Flight Line Diagnostic Procedures ii. Antenna Maintenance Considerations 13. Multiscan Weather Radar (WXR) B. Microwave Radiation Hazards i. AC 20-68B C. Receiver Transmitter Assembly (RTA-4114/4214) ii. Operation i D. Maintenance i. Radome Maintenance (AC 43-13) ii. Flight Line Diagnostic Procedures 14. Course Conclusion A. Review B. Course Critique 2017 Rockwell Collins. All rights reserved. Page 10
11 EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER ICC 3111 IAPS Card Cage IEC-3000 IAPS Environmental Controller PWR 3000 IAPS Power Supply IOC-4110 I/O Concentrator OCM-3100 Options Control Module CSU 3100 Configuration Strapping Unit MDC 4110 Maintenance Diagnostic Computer IMT-5220 Instrument Mounting Tray AFD-5220E Adaptive Flight Display MFD) CCP-5220 Cursor Control Panel DCP-5020 Display Control Panel RSP-5020 Reversion Switch Panel DCU-5000 Data Concentrator Unit LDU 4000 Lamp Driver Unit RDC-5000 Remote Data Concentrator ADC 3000 Air Data Computer MMT-3000 ADC Mount ECU-3000 External Compensation Unit FGC-3002 Flight Guidance Computer Rockwell Collins. All rights reserved. Page 11
12 EQUIPMENT NOMENCLATURE PART NUMBER FGP-5020 Flight Guidance Panel SVO-3000 Aileron Servo SVO-3000 Elevator Servo SMT-65 Servo Mount SVL-4000 Rudder Linear Actuator FMC-6200 Flight Management Computer CDU 5200 Control Display Unit DBU 5010E Data Base Unit ACP-5200 Audio Control Panel ALT-4000 Radio Altimeter CPE-5200 Control Panel Electronics DME-4000 Distance Measuring Equipment GPS-4000S Global Positioning System HF-9031A HF Receiver-Transmitter HF-9041 HF Antenna Coupler NAV-4000 VHF Navigation Receiver NAV-4500 VHF Navigation Receiver RIU-4100 Radio Interface Unit ,152 TDR-94D Transponder TSS-4100 Traffic Surveillance Transmitter Receiver Rockwell Collins. All rights reserved. Page 12
13 EQUIPMENT NOMENCLATURE PART NUMBER VHF 4000 VHF Communication Transceiver RTA-4114 Receiver/Transmitter/Antenna (14 inch with turbulence detection) RTA 4114 Receiver/Transmitter/Antenna (14 inch) WX-1000E Lightning Detection System Processor TAC-5000 TAWS configuration module TAS-5000 Terrain Awareness Warning System Computer FSU-5010 File Server Unit ECU-3000 External Compensation Unit ,803 SCM-2200 SDU Configuration Module FSA-5000 GWX-3000 GWX-5000 File Server Application -006: Universal Weather -106: XM Weather Graphical Weather Software (XM Weather) Graphical Weather Software (Universal Weather) XMWR-1000 XM Receiver XMA-1000 XM Antenna SVC-3000 Synthetic Vision Computer SVC-3000 VIU SVC Video Interface Unit SVCM-3000 Synthetic Vision Configuration Module Rockwell Collins. All rights reserved. Page 13
Publications and Training Solutions Course Syllabus:
COURSE TITLE: Pro Line 21 King Air C90GTi Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC 3000 822-1129-001 IAPS Environmental Controller
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MDC , 402, 403, -404, -405 Display Control Panel DCP , 104, 106, -204, 206 Electronic Flight Display (PFD, MFD)
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