COURSE TITLE: PRO LINE 4 GULFSTREAM G200 Level 1 Operations & Flightline Maintenance EQUIPMENT TYPE: EQUIPMENT NOMENCLATURE PART NUMBER IAPS Card Cage (V5.2) ICC 4005 822-1407-001 IAPS Card Cage (V6.1) ICC-4009 822-1407-001 IAPS Power Supply PWR 4000 622 9945 021 I/O Concentrator IOC 4000 622-9814-XXX -301: for baseline V5.2-302: update V6.1-303: 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 4000 822-0049-002 IAPS Environmental Controller IEC 4000 822-0333-001 Lightning/HIRF Protection (Left) -201: update V6.1-502: baseline V5.2 Lightning/HIRF Protection (Right) -201: update V6.1-501: baseline V5.2 Maintenance Diagnostic Computer -652: baseline V5.2-653: update V6.1 Display Control Panel -006: baseline V5.2-008: update V6.1 LHP 4000 LHP 4001 MDC 4000 DCP 4002 822-0287-XXX 822-0332-XXX 622-9818-XXX 822-0321-XXX November 10, 2010 1
EQUIPMENT NOMENCLATURE PART NUMBER Electronic Flight Display (PFD, MFD) -402: baseline V5.2-404: update V6.1-406: FMS update V6.1.2 (SB505 converts -404 status to - 406 status) EFD 4077 622-9978-XXX Reversionary Switch Panel RSP-4000 822-0273-004 Cursor Control Panel CCP 4000 822-1058-002 EICAS Data Concentrator Unit -002: baseline V5.2-003: update V6.1 Air Data Computer -454 and -457: baseline V5.2-463: update V6.1 DCU 4010 ADC 850C 822-0838-XXX 822-0374-XXX Air Data Reference Panel ARP 4002 822-0326-002 Attitude Heading Computer AHC-3000 822-1110-XXX -001: baseline V5.2-002: update V6.1 External Compensation Unit -001: baseline V5.2-002: update V6.1 ECU-3000 822-1200-XXX Flux Detector Unit FDU-3000 822-1193-001 Data Base Unit (DSDD Disk Drive) -008: update V5.2-104: update V6.1 Flight Control Computer (in IAPS) -029: update V6.1-112: baseline V5.2-129: update V6.1 with Half Bank DBU 4100 FCC 4005 822-0014-XXX 822-0807-XXX Flight Control Panel FCP 4004 822-0385-002 November 10, 2010 2
EQUIPMENT NOMENCLATURE PART NUMBER Primary Servo (aileron and elevator) SVO 85B 622-5027-102 Primary Servo (rudder) SVO 85A 622-6717-104 Control Display Unit CDU-6100 822-1354-102 Flight Management Computer -043: update V6.1 (SB509 converts -026 status to -043 status) -046: V6.1.2 (FMS 2.0.2 update) (SB513 converts -043 status to -046 status) -073: the latest FMS update Radio Tune Unit -214: update V6.1-234: update V6.1 with Flight ID (SB501 converts -x1x or - x2x status to -x3x status) FMC-6000 RTU 4220 822-0868-XXX 822-0730-XXX ADF Receiver (Baseline) ADF-462 622-7382-101 ADF Antenna (Dual ADF) ANT-462B 622-7384-001 VHF Comm Transceiver (Baseline) VHF-422A: 622-7292-121 VHF-422B: 622-7293-121 VHF-422C: 822-1115-021 VHF-422D: 822-1116-021 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 622 1115-021 VHF-4000 822-1872-101 CTL-22 622-6520-001 VIR 432 622 7194 201 November 10, 2010 3
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-4000 822-1465-001 NAV-4500 822-1579-001 DME Transceiver (Baseline) DME 442 622 7309 101 DME Receiver (replaces DME- 442 with PL21 CNS update V6.1.3) DME-4000 822-1466-001 Radio Altimeter ALT 4000 822-0615-111 Radio Altimeter Antenna ANT-52 622-6793-001 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 622 9210 XXX November 10, 2010 4
EQUIPMENT NOMENCLATURE PART NUMBER GPS Navigation Receiver GPS 4000A 822 1377 001 TCAS II Directional Antenna TRE-920 622-8973-001 TCAS II Transmitter Receiver TTR-4000 622-1294-002 Receiver/Transmitter/Antenna (precipitation weather only) Weather Radar Control Panel (installed with RTA-848) Receiver/Transmitter/Antenna (precipitation weather and moisture-based turbulence) RTA-848 622-9303-004 WXP-4120 Weather Radar Control Panel (installed with RTA- 848) RTA 858 622-8441-004 Weather Radar Control Panel WXP 4220 622 9932 002 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, 2010 5
TRAINING MATERIALS: 1. PowerPoint Presentation with LCD projector 2. Course Notebook 3. Gulfstream G200 Avionics System Manual 523-0780876 4. Gulfstream G200 Avionics Diagnostic Guide 523-0780877 5. Pro Line 4 Pilot Guide for the Gulfstream G200 523-0780878 6. Video The Next Generation Weather Radar (Optional - Time and facilities permitting) 523-0778191 REFERENCES: 1. Gulfstream G200 Avionics System Manual 523-0780876 2. Gulfstream G200 Avionics Diagnostic Guide 523-0780877 3. Pro Line 4 Pilot Guide for the Gulfstream G200 523-0780878 November 10, 2010 6
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 429 2. 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, 2010 7
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, 2010 8
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, 2010 9
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, 2010 10
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, 2010 11
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 7.0 523-0779-512 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 523-0778-191 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, 2010 12
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, 2010 13