Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: Pro Line 21 Lear 60XR Level I Operations & Flightline Maintenance EQUIPMENT TYPES: EQUIPMENT NOMENCLATURE PART NUMBER Integrated Card Cage ICC IAPS Environmental Control IEC Module Input Output Concentrator IOC Module Power Supply Module PWR Central Strapping Unit Module CSU Options Control Module OCM Maintenance Diagnostic MDC XXX Computer Maintenance Diagnostic Tables MDT XXX Adaptive Flight Display (PFD, MFD) AFD-3010E XXX Adaptive Flight Display (PFD, MFD) AFD XXX Cursor Control Panel CCP External Compensation Unit ECU File Server Unit FSU File Server Application Software FSA Collins Portable Access Software CPAS Display Control DCP Panel Data Concentration Unit DCU XXX Air Data Computer ADC-850D XXX Signal Interface Adapter SIA Attitude/Heading Computer AHC External ECU Compensation Unit Flux Detector Unit FDU February 14,
2 EQUIPMENT NOMENCLATURE PART NUMBER Flight Guidance Computer FGC XXX Module Primary Servo SVO-85B Servo Mount SMT-85B Flight Guidance Computer FGC XXX Module Primary Servo SVO-85B Servo Mount SMT-85B Flight Management Computer FMC XXX Module Control Display Unit CDU XXX Data Base Unit DBU ADF Receiver ADF ADF Antenna ANT-462B Radio Altimeter ALT Distance Measuring Equipment DME Global Positioning System GPS-4000A VHF Navigation Receiver VIR Radio Tuning Unit (TCAS) RTU XXX Transponder TDR-94D TCAS TX/RX TTR TCAS Directional Antenna TRE VHF Transceiver VHF-422A Receiver Transmitter Antenna RTA File Server Unit FSU File Server Application FSA Software External Compensation Unit ECU FSU Mount MMT PC Database Unit PCD Electronic Charts ECH Map Overlays OVL Collins Portable Access CPAS Software VHF Transceiver VHF February 14,
3 EQUIPMENT NOMENCLATURE PART NUMBER Communication Management CMU Unit CMU Mount MMT External Compensation Unit ECU MMT-125/MMT-130 VHF-4000/ Piggyback Mount Kit CMU-4000 Mount Kit VHF Transceiver VHF Graphical Weather GWX XM Receiver XMWR XM Antenna XMA NAV/COM Control CTL 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 Pro Line 21 system. OBJECTIVES: Upon completing this course, the student will be able to: 1. Provide an overall understanding of Pro Line 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: 5.0 Days TRAINING DEVICES: Test Rig, Cedar Rapids (if available) TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Information sheets/handouts 3. Student Training Manual REFERENCES: 1. Bombardier Aerospace Learjet 60XR Avionics System with Pro Line 21 IFIS Diagnostics Guide February 14,
4 PRO LINE 21 LEAR 60XR COURSE OUTLINE I. Welcome II. A. Training Overview (Customer Ambassador) 1. Welcome 2. Student Registration 3. Student Policies and Procedures Introduction to Materials and Handouts A. System manual introduction and use B. Diagnostic guide introduction III. C. Equipment Description 1. Business & Regional Systems Equipment Leading Particulars Data Bus A. Why we use Data Buses IV. B. Arinc Data Buses 1. Arinc Arinc 453 Integrated Avionics Processing System (IAPS) B. System architecture C. Integrated Card Cage (ICC) D. Power supply module (PWR) E. Internal environmental controller (IEC) F. Input Output Concentrator (IOC) February 14,
5 G. Maintenance Diagnostic Computer (MDC) H. Configuration Strapping Unit (CSU) I. Detailed functional theory 1. IAPS power distribution 2. Temperature monitoring 3. Overheat reporting 4. Power supply inhibit 5. CSU detailed theory J. Maintenance and troubleshooting 1. PWR fault indications 2. IEC fault indications 3. Status messages 4. Diagnostics V. Maintenance Diagnostics VI. B. Maintenance Diagnostic Computer (MDC) Electronic Flight Instrument System (EFIS) B. Adaptive Flight Display (AFD) 1. Primary Flight Display (PFD) a. Description b. Theory of operation c. Reversionary mode select 2. Multifunction Display (MFD) a. Description b. Theory of operation c. Reversionary mode select February 14,
6 VII. C. Reversion Switch Panel (RSP) 1. RSP switchology description 2. Operation 3. Detailed theory of operation Integrated Flight Information System (IFIS) 1. System description B. File Server Unit (FSU) a. Enhanced map functions b. Electronic charts c. Graphical weather C. External Compensation Unit (ECU) D. File Server Application Software (FSA) of applications E. Encrypted Application Key (EAK) 1. Programming EAKs F. Electronic Charts Region Access Keys 1. Programming region access keys G. Maintenance and troubleshooting 1. Database effective dates VIII. Engine Indicating System (EIS) B. MFD 1. Display Synoptics February 14,
7 C. Data Concentrator Unit (DCU) 2. Integration theory 3. Theory of operation D. Engine Data Concentrator Unit (EDC) 2. Integration theory 3. Theory of operation IX. E. Maintenance and troubleshooting 1. Status messages 2. Diagnostics Air Data System (ADS) B. Air Data Computer (ADC) C. Maintenance and troubleshooting 1. Status message 2. Diagnostics X. Attitude Heading System (AHS) B. Attitude Heading Computer (AHC) C. Flux Detector Unit (FDU) D. External Compensation Unit (ECU) E. Maintenance and troubleshooting 1. Diagnostics 2. Post installation check 3. Compass compensation procedure 4. Automatic leveling procedure February 14,
8 XI. Flight Guidance System (FGS) B. Flight Guidance Computers (FGC) C. Flight Guidance Panel (FGP) 2. FGP switchology description 4. Theory of operation D. Primary Servos (SVO) XII. E. Autopilot and yaw damp theory of operation of fail passive system 2. Description of yaw damp system F. Autopilot diagnostics 1. Entering and using autopilot diagnostics a. Report Mode b. Input Mode c. Output Mode 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 February 14,
9 XIII. Database Loading Operations B. Data Base Unit (DBU) a. Uploading databases b. Downloading data C. Personal Computer Dataloader (PCD) a. Uploading databases b. Downloading data D. Collins Portable Access Software (CPAS) a. Importing databases b. Uploading databases c. Downloading data XIV. Radio Sensor System (RSS) B. Radio Tuning Operations 2. Operations 3. Theory of operations C. VHF Comm receiver/transmitter (VHF) 3. Datalink/CPDLC/Link D. VOR/ILS/MB/ADF Receiver (NAV) February 14,
10 E. Distance Measuring Equipment (DME) F. Radio Altimeter (ALT) G. Mode S transponder (TDR-94D) with Traffic Alert and Collision Avoidance System (TCAS) 3. Video presentation (TCAS II Operations CHANGE ) XV. H. General Maintenance Procedures for Comm /Nav /Pulse Equipment 1. Flight line diagnostic procedures Weather Radar (WXR) B. Microwave Radiation Hazards 1. AC 20-68B C. Weather radar theory 1. Video Presentation (The Next Generation Weather Radar ) D. Receiver Transmitter Assembly (RTA-8XX) 2. Operation 3. Theory of operation E. Maintenance 1. Radome maintenance (AC 43-14) 2. Flight line diagnostic procedures XVI. Summary A. Review & Course Critique XVII. Appendix February 14,
Publications and Training Solutions Course Syllabus:
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