Publications and Training Solutions Course Syllabus:

Transcription

1 COURSE TITLE: Pro Line Fusion Global 5000/6000 RC Level I/ATA Level III Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER Adaptive Flight Display AFD EVS Infrared Sensor Unit (ISU) CMA-2700-ISU EVS Infrared Window (IRW) CMA-2700-WIN EVS Aircraft Identification Tag (AIT) SVS Module with integrated HUD CMA-2700-AIT SVM-6110H SVS Module (Optional) SVM Air Data Computer ADC Aircraft Configuration Table, Generic Audio Control Panel (Base+VHF+HF1/2+SAT+ADF 1/2) ACT ACP Radio Interface Unit (SELCAL) RIU Radio Interface Unit (SELCAL, Data Link) External Compensation Unit, unprogrammed VHF Comm Tranceiver kHz, DataLink VHF Comm Tranceiver kHz RIU ECU VHF VHF VHF Comm Antenna VHFA Rev: 06/17/16 1

2 EQUIPMENT NOMENCLATURE PART NUMBER HF Transceiver HF-9031A HF Antenna Coupler HF VOR/ILS/MB/ADF Receiver NAV Dual ADF Antenna ANT-462B DME Transceiver DME Global Positioning System, SBAS Capable GPS-4000S Radio Altimeter ALT MultiScan Weather Radar, 18" RTA TCAS and Transponder Unit TSS TSS TCAS & Transponder Software Application TSSA Directional Antenna For TSS TSA External Compensation Unit - TDR, TCAS, Ext Sqtr Diversity Transponder, ADS-B & EHS Common Computing Module with Mass Storage ECU TDR-94D CCM Common Computing Module CCM TAWS Processing Module TPM Terrain Processing Module Application TPMA taws Adaptive Flight Display, 15.1" AFD Rev: 06/17/16 2

3 EQUIPMENT NOMENCLATURE PART NUMBER Control Tuning Panel CTP Cursor Control Panel CCP Multifunction Keyboard Panel MKP Reversion Switch Panel RSP Integrated Processing Cabinet, Common Computing Cover and Environmental Module Power Environment Module, DC Power IPC CEM PEM Digital Switching Module (24 DSM Port AFDX Switch) Common Computing Module CCM Integrated Processing Cabinet, Situational Awareness IPC Cover and Environmental Module CEM Flight Management Computer Application FMCA xxx Flight Control Panel FCP Flight Control System Application FCSA Primary Servo SVO Dual Servo mount SMT Remote Electronics Unit REU File Server Application FSA Rev: 06/17/16 3

4 EQUIPMENT NOMENCLATURE PART NUMBER Electronic Charts Application Key Enhanced Map Overlay Application Key Information Management System ECH OVL IMS DCU Module Cabinet DMC DMC Cover and Environmental Module CEM Data Concentrator Module DCM Data Concentrator Power Producing Module Data Concentrator Input / Output Module Data Concentrator Input / Output Module PPM IOM IOM Aircraft Personality Module APM Onboard Maintenance System Application OMSA XM Weather Receiver XMWR XM Graphical Weather Key GWX XM Graphical Weather Key, Expanded Features XM Graphical Weather Key, Growth Features GWX GWX-3002 tbd-gwx3002 Rev: 06/17/16 4

5 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 Global 5000/6000 aircraft. This course is designed to teach troubleshooting for box replacement and does not include internal maintenance of any component. OBJECTIVES: Upon completing this course, the student will be able to: 1. Provide an overall understanding of Pro Line Fusion 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: Global 5000/6000 Aircraft (if available) Global 5000/6000 Test Rig, Cedar Rapids (if available) TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Student training manual 3. Information handouts REFERENCES: 1. Bombardier Global Vision with Pro Line Fusion Avionics System Manual Bombardier Global Vision 5000/6000 Pro Line Fusion Avionics System Operator s Guide Pro Line Fusion Avionics System for Bombardier Global Vision Diagnostics Guide Rev: 06/17/16 5

6 PRO LINE FUSION GLOBAL 5000/6000 COURSE OUTLINE I. Welcome & Introduction A. Introductions B. Registration C. Course Description D. Course Objectives E. Course Outline F. Course Evaluation G. Course Critique H. Summary II. Display & Display Control System (D&DCS) 1. Adaptive Flight Displays (AFD) 2. Control Tuning Panel (CTP) 3. Cursor Control Panel (CCP) 4. Multifunction Keyboard Panel (MKP) 5. Reversion Switch Panel (RSP) B. Equipment Location C. Equipment Description 1. Adaptive Flight Displays (AFD) 2. Control Tuning Panel (CTP) 3. Cursor Control Panel (CCP) 4. Multifunction Keyboard Panel (MKP) 5. Reversion Switch Panel (RSP) D. Display Formats E. Display Reversion F. Comparators/Failures G. AFD Theory Rev: 06/17/16 6

7 H. Summary III. Integrated Processing System (IPS) 1. Integrated Processing Cabinet and installed modules 2. Installed application software B. Global 5000/6000 Locations C. Integrated Processing System 1. IPC-6210 a. Cover Environmental Module b. Power Environmental Module c. Digital Switching Module d. Common Computing Module 2. IPC-6220 a. Cover Environmental Module b. Power Environmental Module c. Digital Switching Module d. Common Computing Module e. TAWS Processing Module f. Synthetic Vision Module D. Installed application software E. IPS Theory IV. Data Concentration System (DCS) 1. Data Concentrator Unit Module Cabinet (DMC) 2. Aircraft Personality Module 3. Installed software applications 4. Engine Indicating Crew Alerting System (EICAS) 5. Stall Protection System (SPS) B. Data Concentrator Unit Module Cabinet (DMC) 1. DMC Cover and Environmental Module (CEM-6000) 2. Data Concentrator Module (DCM-6000) 3. Data Concentrator Power Producing Module (PPM-6000) 4. Data Concentrator Input/Output Module (IOM-6000) 5. Data Concentrator Input/Output Module (IOM-6500) 6. Aircraft Personality Module (APM-5000) Rev: 06/17/16 7

8 C. Data Concentrator System 1. Crew Alerting System (CAS) 2. Electronic Checklist 3. Aural Alerting 4. Data Acquisition and Distribution D. EICAS 1. Engine Indicating System E. System Synoptics F. DCS Theory G. Summary V. Dataloading 1. Information Management System 2. IMS Terminology B. Data Load Architecture C. Data Load Procedures 1. Load New Databases 2. Load New Documents & Tables 3. Load/Update IMA Aircraft Software Set 4. Load New/Misconfigured LRU Item 5. Reload LRU/LRM 6. Load ARINC 429 LRUs D. Data Loading Theory E. Summary Publications and Training Solutions VI. Onboard Maintenance System (OMS) 1. Onboard diagnostics 2. Aircraft Condition Monitoring 3. Diagnostic downloads Rev: 06/17/16 8

9 B. Maintenance Main Menu 1. View Flight Deck Effects 2. View Fault Messages 3. View Service Messages 4. View System Exceedances 5. View System Trends 6. View Aircraft Life Cycle Data 7. View System Parameters 8. Perform LRU/System Operations 9. View System Configuration Data 10. Write Maintenance Reports 11. Utility Functions C. OMS Theory D. Summary Publications and Training Solutions VII. Heads Up Display/Enhanced Vision System (HUD/EVS) B. HUD Overview C. HUD Components D. HUD Component Installation E. HUD Control F. HUD Display G. HUD Monitor Application (HMA) H. HUD Display Application (HDA) I. HUD Troubleshooting J. EVS Overview K. EVS Components L. EVS Control M. EVS Alignment Rev: 06/17/16 9

10 N. EVS/HUD Troubleshooting O. EVS/HUD Theory VIII. Synthetic Vision System (SVS) B. SVS Overview C. SVS Components D. SVS Display E. SVS Controls F. SVS Theory IX. Air Data System (ADS) B. Air Data Computer C. ADC Locations D. ADS Displays E. ADS Controls F. Reversionary Mode G. Indications & Warnings H. ADC Data Loading I. ADS Theory J. Summary X. Attitude Heading System (AHS) B. Displays and Indications Rev: 06/17/16 10

11 C. Reversionary modes D. AHS Theory E. Summary XI. Integrated Flight Information System (IFIS) B. IFIS Overview C. Electronic Charts D. Enhanced Map Overlays E. Graphical Weather F. Subscriptions G. IFIS Theory H. Summary XII. Automatic Flight Control System (AFCS) B. Flight Control System Application C. Global 5000/6000 Locations D. Flight Control Panel E. Remote Electronics Unit F. Servos G. Yaw Damper Actuator H. Reversion Switch Panel I. AFCS Theory J. Summary XIII. Flight Management System (FMS) Rev: 06/17/16 11

12 B. FMS Overview C. FMS Controls D. Display Operations E. Fault Indications F. FMS Theory G. Summary XIV. Communication System (COMM) B. Digital Audio System C. Radio Management D. Global 5000/6000 Locations E. VHF-4000 F. Controller/Pilot Data Link Communication (CPDLC) G. HF-9000 H. Communication Theory I. Summary XV. Navigation Systems (NAV) B. NAV-4000 C. Global 5000/6000 Locations D. DME-4000 E. GPS-4000 F. Radio Altimeter-4000 Rev: 06/17/16 12

13 G. Navigation Theory H. Summary XVI. TSS/TAWS B. Traffic Surveillance System (TSS) 1. TSS Global 5000/6000 Locations 3. TSS Controls C. Terrain Awareness Warning System (TAWS) 1. CCM TPM-6000 D. Summary XVII. MutliScan Weather Radar A. Receiver Transmitter Assembly (RTA) B. Weather Radar Fundamentals C. MultiScan Theory D. Operation E. WXR Fault Indications F. Hazard Area G. Summary XVIII. Course Summary A. Review B. Summary C. Final Test D. Course critique Rev: 06/17/16 13