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1 COURSE TITLE: PRO LINE 4 GULFSTREAM G200 Level 1 Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage (V5.2) ICC IAPS Card Cage (V6.1) ICC IAPS Power Supply PWR I/O Concentrator IOC XXX -301: for baseline V : update V : baseline V5.2 with Flight ID -312: update V6.1 with enhanced surveillance. (SB507 converts -302 status to -312 status.) -313: baseline V5.2 with enhanced surveillance Configuration Strapping Unit CSU IAPS Environmental Controller IEC Lightning/HIRF Protection (Left) -201: update V : baseline V5.2 Lightning/HIRF Protection (Right) -201: update V : baseline V5.2 Maintenance Diagnostic Computer -652: baseline V : update V6.1 Display Control Panel -006: baseline V : update V6.1 LHP 4000 LHP 4001 MDC 4000 DCP XXX XXX XXX XXX November 10,

2 EQUIPMENT NOMENCLATURE PART NUMBER Electronic Flight Display (PFD, MFD) -402: baseline V : update V : FMS update V6.1.2 (SB505 converts -404 status to status) EFD XXX Reversionary Switch Panel RSP Cursor Control Panel CCP EICAS Data Concentrator Unit -002: baseline V : update V6.1 Air Data Computer -454 and -457: baseline V : update V6.1 DCU 4010 ADC 850C XXX XXX Air Data Reference Panel ARP Attitude Heading Computer AHC XXX -001: baseline V : update V6.1 External Compensation Unit -001: baseline V : update V6.1 ECU XXX Flux Detector Unit FDU Data Base Unit (DSDD Disk Drive) -008: update V : update V6.1 Flight Control Computer (in IAPS) -029: update V : baseline V : update V6.1 with Half Bank DBU 4100 FCC XXX XXX Flight Control Panel FCP November 10,

3 EQUIPMENT NOMENCLATURE PART NUMBER Primary Servo (aileron and elevator) SVO 85B Primary Servo (rudder) SVO 85A Control Display Unit CDU Flight Management Computer -043: update V6.1 (SB509 converts -026 status to -043 status) -046: V6.1.2 (FMS update) (SB513 converts -043 status to -046 status) -073: the latest FMS update Radio Tune Unit -214: update V : update V6.1 with Flight ID (SB501 converts -x1x or - x2x status to -x3x status) FMC-6000 RTU XXX XXX ADF Receiver (Baseline) ADF ADF Antenna (Dual ADF) ANT-462B VHF Comm Transceiver (Baseline) VHF-422A: VHF-422B: VHF-422C: VHF-422D: VHF COMM Transceiver (replaces VHF-422 radios with PL21 CNS update V6.1.3) 3rd VHF COMM Control (with 3rd VHF COMM option) VHF Navigation Receiver (Baseline) VHF 422A/B/C/D VHF CTL VIR November 10,

4 EQUIPMENT NOMENCLATURE PART NUMBER VHF NAV Receiver w/adf (replaces a VIR-432 and the ADF-462 receiver with PL21 CNS update V6.1.3) VHF NAV Receiver (replaces a VIR-432 receiver with PL21 CNS update V6.1.3) (If the 2nd ADF option is installed, the NAV-4500 receiver is replaced with a second NAV-4000 receiver in the PL 21 V6.1.3 configuration.) NAV NAV DME Transceiver (Baseline) DME DME Receiver (replaces DME- 442 with PL21 CNS update V6.1.3) DME Radio Altimeter ALT Radio Altimeter Antenna ANT Mode S Transponder -004: baseline -007: provides Flight ID and Enhanced Surveillance capabilities for airplanes not equipped with Rockwell Collins Pro Line 4 or Pro Line 21 avionics systems (SB 501 converts -004/-005/-006 status to -007 status). -008: provides Flight ID and Enhanced Surveillance capabilities for airplanes that are equipped with Rockwell Collins Pro Line 4 or Pro Line 21 avionics systems (SB 502 converts -007 status to -008 status). TDR 94D XXX November 10,

5 EQUIPMENT NOMENCLATURE PART NUMBER GPS Navigation Receiver GPS 4000A TCAS II Directional Antenna TRE TCAS II Transmitter Receiver TTR Receiver/Transmitter/Antenna (precipitation weather only) Weather Radar Control Panel (installed with RTA-848) Receiver/Transmitter/Antenna (precipitation weather and moisture-based turbulence) RTA WXP-4120 Weather Radar Control Panel (installed with RTA- 848) RTA Weather Radar Control Panel WXP PREREQUISITES: Students should have basic knowledge of aircraft avionics systems, be familiar with normal line maintenance procedures, 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: N/A November 10,

6 TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Course Notebook 3. Gulfstream G200 Avionics System Manual Gulfstream G200 Avionics Diagnostic Guide Pro Line 4 Pilot Guide for the Gulfstream G Video The Next Generation Weather Radar (Optional - Time and facilities permitting) REFERENCES: 1. Gulfstream G200 Avionics System Manual Gulfstream G200 Avionics Diagnostic Guide Pro Line 4 Pilot Guide for the Gulfstream G November 10,

7 PRO LINE 4 GULFSTREAM G200 COURSE OUTLINE 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 Busses 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 10,

8 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) 3. Operation November 10,

9 VI. Electronic Flight Instrument System (EFIS) B. Electronic Flight Display (EFD) 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 C. EICAS Control Panel (ECP) 2. ECP switchology description 3. Detailed theory of operation D. Data Concentrator Unit (DCU) 2. Integration theory 3. Theory of operation E. Maintenance and troubleshooting 1. Status messages 2. Diagnostics November 10,

10 VIII. Air Data System (ADS) B. Air Data Computer 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-3000) C. External Compensation Unit (ECU) D. Operation 1. Initialization E. Maintenance and troubleshooting 1. Diagnostics 2. Compass Swing procedure X. Flight Control System (FCS) B. Flight Control Computers (FCC) November 10,

11 C. Flight Control Panel (FCP) 2. FCP switchology description 3. Theory of operation D. Primary Servo (SVO) E. Autopilot and yaw damp detailed theory of operation of fail passive system 2. Description of null seeking servo loops F. Autopilot diagnostics 1. Entering and using autopilot diagnostics a. Input mode b. Output mode c. Report Mode XI. Flight Management System B. Control Display Unit (CDU) 2. Operation a. 28 Data Base load 3. Theory of operation C. Flight Management Computer (FMC) 2. Theory of Operation XII. Radio Sensor System B. Radio Tuning Unit (RTU) 2. Operation 3. Theory of operation November 10,

12 C. VHF Comm receiver/transmitter (VHF) D. VOR/ILS/MB Receiver (VIR) E. Distance Measuring Equipment (DME) F. Automatic Direction Finder receiver (ADF) G. Radio Altimeter (ALT) H. Mode S transponder (TDR-94D) with Traffic Alert and Collision Avoidance System (TCAS) 3. Video presentation TCAS 2 operations CHANGE I. General Maintenance Procedures for Comm /Nav /Pulse Equipment 1. Flight line diagnostic procedures 2. Antenna maintenance considerations XIII. Weather Radar (WXR) 1. Video Presentation The Next Generation Weather Radar B. Microwave Radiation Hazards 1. AC 20-68B C. Weather radar theory 1. Mediums that reflect 2. Turbulence detection D. Receiver Transmitter Assembly (RTA-8xx) November 10,

13 E. Maintenance 1. Radome maintenance (AC 43-13) 2. Flight line diagnostic procedures XIV. Dataloading A. Procedures 1. PCD 2. DBU XV. Course Conclusion A. Review B. Course critique November 10,