Publications and Training Solutions Course Syllabus:
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1 COURSE TITLE: Pro Line 21 King Air C90GTi Level I Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage ICC IAPS Environmental Controller IEC IAPS Power Supply PWR I/O Concentrator IOC Options Control Module OCM Configuration Strapping Unit CSU Maintenance Diagnostic Computer MDC Adaptive Flight Display (PFD, MFD) AFD Adaptive Flight Display (Ethernet) AFD-3010E Display Control Panel DCP ,-161 File Server Unit FSU Curser Control Panel CCP Communications Management Unit (Use with 3rd VHF data-link option) CMU XM Receiver XMWR External Compensation Unit (FSU) ECU , -999 Data Concentrator Unit DCU Air Data Computer ADC Attitude Heading Computer AHC External Compensation Unit ECU Flux Detector Unit FDU Flight Guidance Computer B200 FGC Flight Guidance Panel FGP Aileron Servo SVO Rev: 02/13/2008 1
2 EQUIPMENT NOMENCLATURE PART NUMBER Rudder Servo B200 SVO Elevator Servo SVO Servo Mount (Aileron) SMT Servo Mount (Rudder/Elevator) SMT Flight Management Computer FMC Control Display Unit CDU /491 Data Base Unit DBU ADF antenna, dual ANT-462B Radio Altimeter ALT Distance Measuring Equipment DME Global Positioning System GPS-4000A HF Transceiver HF-9031A HF Antenna Coupler HF VHF Navigation Receiver NAV VHF Navigation Receiver NAV Radio Tuning Unit Radio Tuning Unit (TCAS) RTU-4200 RTU , Mode S Transponder (Baseline) TDR Mode S Transponder (Diversity) TDR VHF Communication Transceiver VHF VHF Communication Transceiver (Optional 3rd - Datalink) VHF Receiver/Transmitter/Antenna RTA Receiver/Transmitter/Antenna (12 inch with turbulence detection) RTA Rev: 02/13/2008 2
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 flight line 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 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 4. Beechcraft King Air C90GTi/B200GT Avionics System Manual Excerpt Beechcraft King Air C90GT/B200GT Diagnostic Guide REFERENCES: 1. Beechcraft King Air C90GTi/B200GT Avionics System Manual Beechcraft King Air C90GT/B200GT Diagnostic Guide Beechcraft King Air C90GT/B200GT Operator s Guide Rev: 02/13/2008 3
4 PRO LINE 21 C90GTi LEVEL 1 COURSE OUTLINE I. Welcome A. Training Overview 1. Welcome 2. Student Registration 3. Student Policies and Procedures II. Introduction to Materials and Handouts A. System manual introduction and use B. Diagnostic guide introduction C. Equipment Description 1. Business & Regional Systems Equipment Leading Particulars III. Data Bus A. Why we use Data Buses B. Arinc Data Buses 1. Arinc Arinc 453 IV. Integrated Avionics Processing System (IAPS) B. System architecture C. Integrated Card Cage (ICC) D. Power supply module (PWR) E. Internal environmental controller (IEC) Rev: 02/13/2008 4
5 F. Input Output Concentrator (IOC) 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 B. Maintenance Diagnostic Computer (MDC) 3. Operation VI. 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 Rev: 02/13/2008 5
6 2. Multifunction Display (MFD) a. Description b. Theory of operation c. Reversionary mode select VII. C. Reversion Switch Panel (RSP) 1. RSP switch description 2. Operation 3. Detailed theory of operation Integrated Flight Information System (IFIS) 1. System description B. File Server Unit (FSU) 3. Operation 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 Rev: 02/13/2008 6
7 VIII. Engine Indicating System (EIS) B. MFD 1. Display Synoptics 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 E. Maintenance and troubleshooting 1. Status messages 2. Diagnostics IX. 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) Rev: 02/13/2008 7
8 E. Maintenance and troubleshooting 1. Diagnostics 2. Post installation check 3. Compass compensation procedure 4. Automatic leveling procedure XI. Flight Guidance System (FGS) B. Flight Guidance Computers (FGC) C. Flight Guidance Panel (FGP) 2. FGP switch description 3. Operation 4. Theory of operation D. Primary Servos (SVO) 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 XII. Flight Management System (FMS) B. Flight Management Computer (FMC) Rev: 02/13/2008 8
9 C. Control Display Unit (CDU) D. Data Base Unit (DBU) XIII. Data Loading A. CPAS Database loading B. PCD-3000 Database loading C. DBU Database loading XIV. Radio Sensor System (RSS) B. GPS 2. Operations 3. Theory of operations C. VOR/ILS/MB/ADF Receiver (NAV) D. Distance Measuring Equipment (DME) E. VHF Comm receiver/transmitter (VHF) F. Mode S transponder (TDR-94) G. HF Rev: 02/13/2008 9
10 H. Radio Altimeter (ALT) I. Radio Tuning Operations 2. Operations 3. Theory of operations J. General Maintenance Procedures for Comm /Nav /Pulse Equipment 1. Flight line diagnostic procedures XV. Weather Radar (WXR) B. Microwave Radiation Hazards 1. AC 20-68B C. Weather radar theory 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 Rev: 02/13/
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