Garmin G5000 Integrated Avionics System Software Update ICA Supplement

Transcription

1 AIRCRAFT DIVISION WICHITA, KANSAS Garmin G5000 Integrated Avionics System Software Update ICA Supplement MODEL NO: 750 SUPPLEMENT NO: ICA SUPPLEMENT DATE: 6/1/2016 Cessna Aircraft Company Form 2261 Rev 1

2 AIRCRAFT DIVISION WICHITA, KANSAS REVISIONS ICA Rev: - Date: Jun 6/2016 ICA Summary Pages 1-6 Manuals Affected Description Title Maintenance Manual Pages Garmin G5000 Integrated Avionics System Software Update This section gives the adjustments and test necessary to update or change the Garmin G5000 software and configuration files from Version 25 to Version 41 for Airplanes to complying with SB Appendix A: Illustrated Parts Catalog Appendix B: Wiring Diagram Manual 1. Export Compliance Not Used Not Used A. This publication contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E Revision Bars A. Revision bars in this ICA supplement identify new ICAs and/or changes to the current ICAs in the released maintenance manual. New ICAs that are not in the current maintenance manual will have a revision bar from top to bottom along the left margin. ICAs that are in the current maintenance manual and have information added, deleted or revised will have a revision bar(s) in the left margin adjacent to the added, deleted or revised information. New or changed illustrations will have a change bar for the entire length of the page. 3. Page Numbering A. The page number system for ICA included in this supplement have three-element numbers that are separated by dashes. The three-element number is found at the bottom right corner of the page, left of the page number. The date is found below the page number. B. When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number ( ), the information is applicable to the entire system. Page 1 of 6 Jun 1/2016 Cessna Aircraft Company

3 AIRCRAFT DIVISION WICHITA, KANSAS C. When the section/subsystem element number is followed with zeros in the subject/unit element number ( ), the information is applicable to the subsystems in the system. D. The subject/unit element number is used to identify information applicable to units in the subsystems. The subject/unit element number continues in sequence from the number -01- with the number of subsystem units in which maintenance information is necessary. E. All system/subsystem/unit (chapter/section/subject) maintenance data is separated into specified types of information: Description and Operation, Troubleshooting, Maintenance Practices, etc. Blocks of page numbers that are in sequence are used to identify the type of information: (1) Description and Operation or Troubleshooting information may not be included if the procedure is easy. When subtopics are short, they may be put together into the Maintenance Practices section. Maintenance Practices can have a mix of subtopics that includes information to service, remove, install, adjust, test, clean, paint or do approved repairs. (2) Longer procedures that are not as easy to do may be included in a specified section. Page 1 through 99 - Description and Operation Page 101 through Troubleshooting Page 201 through Maintenance Practices Page 301 through Servicing Page 401 through Removal/Installation Page 501 through Adjustment/Test Page 601 through Inspection/Check Page 701 through Cleaning/Painting Page 801 through Approved Repairs F. A typical page number: G. Illustrations use the same figure numbers as the page block in which they appear. For example, Figure 202 would be the second figure in a Maintenance Practices section. 4. Supplement Revisions A. Revisions to this supplement may be accomplished if changes to this supplement are required after release of the original issue and prior to incorporation into the manuals listed in the REVISIONS table. B. All revisions to this supplement will have changes identified in detail in the revision block(s) above. C. All pages in this ICA supplement will have the same date and are valid as of the date shown. 5. ICA Incorporation into Applicable Manuals Most ICA supplements will be incorporated in the next available revision to the manuals listed above and should be used in conjunction with those manuals until the next available revision is released. A. The ICA Supplement List located in the Introduction section of each manual listed in the REVISIONS table will indicate the incorporation status as of the release date of the published revision. Page 2 of 6 Jun 1/2016 Cessna Aircraft Company

4 AIRCRAFT DIVISION WICHITA, KANSAS B. The manual revision level of the supplement incorporation will be listed in the "Manual Incorporation Status" column in the ICA Supplement List, when those ICAs associated with that manual have been incorporated. After ICAs are incorporated, the manual that they are incorporated in must now be used for those ICAs instead of the supplement. Based on revision cycle times for the affected manuals, MM ICAs, WDM ICAs, etc. in this supplement may be incorporated in the manuals at different times. There will not be a revision to this supplement to indicate incorporation in the manuals. Users are required to check the ICA Supplement List for each manual affected to determine incorporation status. C. This supplement will be completely superseded by the manuals listed in the REVISIONS table when it has been incorporated in all of the manuals. Page 3 of 6 Jun 1/2016 Cessna Aircraft Company

5 AIRCRAFT DIVISION WICHITA, KANSAS Purpose INTRODUCTION A. The purpose of this Supplement is to provide the maintenance technician with the information necessary to ensure the correct functionality and performance of the Garmin G5000 Integrated Avionics System Software Update on the Cessna Model 750 (-0501 to -0525) complying with SB until this information gets incorporated into the next revision to the manuals listed in the "REVISIONS" section of this supplement. B. This ICA supplement is designed to satisfy the requirements of 14 CFR "Instructions for Continued Airworthiness" associated with this installation. This document is a supplement to the Model 750 (-0501 and on) Maintenance Manual. C. When this information is incorporated in the next revision to the manuals listed in the "REVISIONS" section, those manuals shall take precedence over this supplemental document. Refer to the "ICA Supplement List" in the "Introduction" section of the respective manual for the status of all applicable ICA Supplements. D. Revisions to this supplement may occur if there is a change to any of the ICAs in this supplement prior to incorporation into all of the affected manuals. This document must be placed with the aircraft operator's Technical Library CD-ROM or Cessna Model 750 (-0501 and on) Maintenance Manual and incorporated into the operator's scheduled maintenance program. 2. Effectivity A. These Instructions for Continued Airworthiness (ICA) are effective for the following aircraft model and serialization. Model Beginning Effectivity Ending Effectivity Model 750 (-0501 and On) Complete ICA Documents A. The following document(s), in conjunction with this supplement, constitute the Instructions for Continued Airworthiness for the Garmin G5000 Integrated Avionics System Software Update on the Cessna Model 750 (-0501 to -0525). All items must be available to the operator at initial delivery. (1) Cessna Model 750 (-0501 and On) Maintenance Manual Page 4 of 6 Jun 1/2016 Cessna Aircraft Company

6 AIRCRAFT DIVISION WICHITA, KANSAS LIST OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1. Cessna Model 750 (-0501 and On) Maintenance Manual A. Chapter 34 Navigation (1) Refer to ATA , GARMIN G5000 INTEGRATED AVIONICS SYSTEM SOFTWARE UPDATE - MAINTENANCE PRACTICES. Page 5 of 6 Jun 1/2016 Cessna Aircraft Company

7 AIRCRAFT DIVISION WICHITA, KANSAS Continuous Inspection Program INSPECTION PROGRAM AND AIRWORTHINESS LIMITATIONS A. This ICA Supplement does not affect the current inspection program. 2. Airworthiness Limitations A. Cessna Aircraft Company Model 750 (-0501 and On), Chapter 4 Airworthiness Limitations, contains the system and airframe limitations for the Model 750 (-0501 and On). The Airworthiness Limitations section is FAA-approved and specifies maintenance required under Section and of Title 14 Code of Federal Regulations, unless an alternative program has been FAA approved. (1) There are no new (or additional) airworthiness limitations associated with this equipment and/or installation. Page 6 of 6 Jun 1/2016 Cessna Aircraft Company

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9 GARMIN G5000 INTEGRATED AVIONICS SYSTEM SOFTWARE UPDATE - MAINTENANCE PRACTICES (Airplanes to incorporating SB ) 1. General A. This section gives the adjustments and test necessary to update or change the Garmin G5000 software and configuration files from Version 25 to Version 41 for Airplanes to incorporating SB For more data regarding the Garmin G5000 Integrated Avionics System, refer to the Garmin G5000 Integrated Avionics System Pilot's Guide for the Cessna Citation Model 750 and the Garmin G5000 Integrated Avionics System Line Maintenance Manual, Cessna Citation Model 750. B. Here is a listing of the sections as they appear: (1) General (2) Garmin G5000 System Useful Specifics (3) Garmin G5000 Software Upgrade from Version 25 to Version 41 (4) Installed Options, Empty Weight, Pilot Profiles, Delete CMC Files, and Wireless WiFi Settings (5) Software and Configuration Loading (6) CMC Diagnostic Configuration Upload (7) PERF and TOLD Database Loading (8) Aircraft Configuration Loading (9) Final Verification/Return to Service (10) SD Card Disposal (11) Confirm the FLEET ID (Version 41) (12) Troubleshooting 2. Garmin G5000 System Useful Specifics A. Before proceeding with the G5000 system software upgrade, the following specifics are useful to know: (1) In the G5000 configuration mode, the GDU Controls button on left side of the Home GTC screen is used. (2) Make sure that the PFD 1 button on the left side of the GDU Controls screen of the GTC is selected. (3) The dual concentric knobs on the lower right of the GTC are used and are referred to as the small and large FMS knobs. (4) The Enter key on the right lower section of the GTC screen is used. (5) The PFD and MFD displays can be individually powered down by turning the outer knob of the L PFD GTC DIM, MFD GTC DIM, or R PFD GTC DIM knobs to left to shut off the display unit. Refer to Chapter 33, Flight Compartment Lighting - Description and Operation for location of the L PFD GTC DIM, MFD GTC DIM, and R PFD GTC DIM knobs. (6) Alternately, the PFD and MFD displays can be powered down by disengaging the correct circuit breaker(s) as follows: (a) To remove power from the PFD 1, pull circuit breakers L PFD (Left CB Panel - O4) and L PFD AUX (Left CB Panel - L4). (b) To remove power from MFD, pull the circuit breakers MFD (Right CB Panel DD2) and MFD AUX (Right CB Panel HH4). (c) To remove power from PFD 2, pull the circuit breaker R PFD (Right CB Panel JJ4). 3. Garmin G5000 Software Upgrade from Version 25 to Version 41 A. General (1) This section gives the adjustments and test necessary to update or change the Garmin G5000 software and configuration files from Version 25 to Version 41 (in accordance with SB ) for Airplanes to complying with SB Page 201

10 B. Tools and Equipment For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Chapter 34, Navigation - General. For the supplier publication part number and manufacturer data, refer to the Introduction - Supplier Publication List. (1) Tools and Equipment (a) ACARS Application Unlock SD card (part number: E6) (b) CDMS Diagnostics SD card (part number: ) (c) CMC Configuration SD card (part number: ) (d) CPDLC Unlock SD card (part number: F0) (e) Crew Profile SD card (part number: ) (f) PERF Database SD card (part number: ) (g) Software Loader SD card (part number: ) (h) SurfaceWatch Unlock SD card (part number: E) (i) TOLD Database SD card (part number: ). (2) Special Consumables (a) None. (3) Reference Material (a) Chapter 24, External Electrical Power - Maintenance Practices (b) Chapter 33, Flight Compartment Lighting - Description and Operation C. Prepare the Airplane for the Garmin G5000 Software Upgrade from Version 25 to Version 41 (1) Make sure airplane batteries are installed and connected. (2) Connect external electrical power to the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices. (3) Engage the circuit breakers as given in Table 201. Table 201. G5000 Core and Optional Component Circuit Breakers Garmin G5000 Component GIA-63W #1 GIA-63W #2 Circuit Breaker Model 750 System Requirement Location NAV IAU 1 Core Component Left Circuit Breaker Panel COM 1 Core Component Left Circuit Breaker Panel NAV IAU 2 Core Component Right Circuit Breaker Panel COM 2 Core Component Right Circuit Breaker Panel GSD-41 #1 DCU Core Component Right Circuit Breaker Panel GSD-41 #2 GSD-41 #3 DCU 2 (HZ033) Core Component Left DC Power J-Box DCU 2 AUX (HZ130) Core Component Left DC Power J-Box DCU 3 (HZ036) Core Component Right DC Power J-Box DCU 3 AUX (HZ230) Core Component Right DC Power J-Box GEA-7100 #1 ENGINE INTER 1 Core Component Right Circuit Breaker Panel GEA-7100 #2 ENGINE INTER 2 (HZ029) ENGINE INTER 2 AUX (HZ104) Core Component Core Component Left DC Power J-Box Left DC Power J-Box Page 202

11 Table 201. G5000 Core and Optional Component Circuit Breakers (continued) Garmin G5000 Component GEA-7100 #3 GMA-36 #1 GMA-36 #2 GDU-1400W Circuit Breaker ENGINE INTER 3 (HZ032) ENGINE INTER 3 AUX (HZ204) Model 750 System Requirement Core Component Core Component Location Right DC Power J-Box Right DC Power J-Box AUDIO 1 Core Component Left Circuit Breaker Panel AUDIO 1 AUX Core Component Left Circuit Breaker Panel AUDIO 2 Core Component Right Circuit Breaker Panel AUDIO 2 AUX Core Component Right Circuit Breaker Panel L PFD Core Component Left Circuit Breaker Panel L PFD AUX Core Component Left Circuit Breaker Panel MFD Core Component Right Circuit Breaker Panel MFD AUX Core Component Right Circuit Breaker Panel R PFD Core Component Right Circuit Breaker Panel GCU-275 #1 L PFD GCU Core Component Left Circuit Breaker Panel GCU-275 #2 R PFD GCU Core Component Right Circuit Breaker Panel GMC-7200 AFCS CONT Core Component Left Circuit Breaker Panel Servos AUTOPILOT Core Component Left Circuit Breaker Panel GAC #1 L YAW DAMPER (HZ151) Core Component Left DC Power J-Box GAC #2 R YAW DAMPER (HZ250) Core Component Right DC Power J-Box GDL-59 MAINT Core Component Left Circuit Breaker Panel Transponder #1 XPDR 1 Core Component Left Circuit Breaker Panel Transponder #2 XPDR 2 Core Component Right Circuit Breaker Panel TCAS TCAS Core Component Right Circuit Breaker Panel GWX-70 RADAR Core Component Right Circuit Breaker Panel GDC #1 ADC 1 Core Component Left Circuit Breaker Panel GDC #2 ADC 2 Optional Component Right Circuit Breaker Panel GDL-69A WEATHER Optional Component Left Circuit Breaker Panel GDR-66 DATA COM Optional Component Right Circuit Breaker Panel Page 203

12 Table 201. G5000 Core and Optional Component Circuit Breakers (continued) Garmin G5000 Component Circuit Breaker Model 750 System Requirement Location GSR-56 #1 IRIDIUM DATA Optional Component Left Circuit Breaker Panel GSR-56 #2 IRIDIUM DATA 2 Optional Component Right Circuit Breaker Panel GTC-570 #1 MFD L GTC Core Component Left Circuit Breaker Panel GTC-570 #2 MFD R GTC Core Component Right Circuit Breaker Panel GTC-570 #3 L PFD GTC Core Component Left Circuit Breaker Panel GTC-570 #4 R PFD GTC Core Component Right Circuit Breaker Panel GRA-5500 RADIO ALTIMETER (HZ150) Core Component Left DC Power J-Box (4) Set the switches that follow as shown: (a) Select the L BATT and R BATT switch/lights to ON. (b) Select EXT POWER switch/light to ON. (c) Select the L AVN and R AVN switch/lights to ON. (d) Select the BUS TIE switch/light to the CLOSED position. (e) Select the ELEC switch/lights to the NORM position. (5) Make sure that the left and right glareshield fans are operating. (6) After the Garmin G5000 system is powered up and initialized, it is in Normal mode. D. Update the Garmin G5000 Software Upgrade from Version 25 to Version 41 (1) Update the Garmin G5000 Software from Version 25 to Version 41 as follows: (a) Do the Installed Options, Empty Weight, Pilot Profiles, Delete CMC Files, and Wireless WiFi Settings. (b) Do the Software and Configuration Loading. (c) Do the CMC Diagnostic Configuration Upload. (d) Do the PERF and TOLD Database Loading. (e) Do the Aircraft Configuration Loading. (f) Do the Final Verification/Return to Service. 4. Installed Options, Empty Weight, Pilot Profiles, Delete CMC Files, and Wireless WiFi Settings A. Do the Installed Options, Empty Weight, Pilot Profiles and Delete CMC Files as follows: Make sure that the G5000 system is powered up, initialized and in Normal Mode. (1) Record the Installed Options as follows: (a) Dual HF (FK632K - Second HF (Full Up)). Refer to Figure On the Home screen of either MFD GTC 570, touch the AUDIO and RADIOS tab. 2 On the AUDIO & RADIOS screen of either MFD GTC 570, if the HF 2 is shown, mark YES. Otherwise mark NO. A Figure Page 204

13 (b) ADF (FK658A - ADF). Refer to Figure If ADF controls are displayed on the AUDIO & RADIOS screen of either MFD GTC 570, mark YES. Otherwise mark NO. A Figure 202 (c) GDL69 (FK632L- SiriusXM (Weather/Music)). Refer to Figure On the Home screen of either MFD GTC 570, touch the Weather button. 2 Touch Weather Selection. 3 If a SiriusXM Settings button is displayed, mark YES. Otherwise mark NO. A Figure 203 (d) GSR56 (FK676A - Iridium (Voice/Datalink)). Refer to Figure On the Home screen of either MFD GTC 570, touch the Services button (if applicable). 2 On the Services page, if the Telephone button is displayed, mark YES. Otherwise mark NO. A Figure 204 (2) Record the Empty Weight Value as follows: These data will be entered after the configurations are loaded. (a) On the Home screen of either MFD GTC 570, select Utilities. 1 Select Weight and Fuel. 2 Record the airplane's Basic Empty Weight in Table Record the Pilot(s) and Stores Weight in Table Page 205

14 Table 202. Empty Weight Values Indicated by the GTC Weight Category Basic Empty Weight (Airplane) Pilot(s) and Stores Weight (3) Pilot Profiles Weight (Indicated by the GTC) Software Version 41 is not compatible with the original pilot profiles and consequently, the current pilot profiles are not exported. (a) A new Default Pilot Profile will be installed later in the instructions. (4) Delete the CMC Files as follows: After software is loaded, the wireless settings in the CMC logs are automatically loaded for all scenarios, and consequently do not need to be recorded. (a) (b) (c) (d) (e) (f) (g) (h) (i) (j) (k) (l) (m) Go into the left MFD GTC 570 touch controller and select Aircraft Systems. Select Maintenance. Enter CACCDMS as the password. Select CMC Logs. Select the Faults folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the LH Service Messages Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the RH Service Messages Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the LH Engine Exceedances Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the RH Engine Exceedances Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the LH Engine Trends Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the RH Engine Trends Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the LH Continuous Log Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. Go back and select the RH Continuous Log Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted Page 206

15 (n) Go back and select the LH Eng Cal Data Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. (o) Go back and select the RH Eng Cal Data Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. (p) Go back and select the CAS Messages Folder. 1 Select the Folder Options. 2 Select Delete All. 3 Select OK when prompted. (5) Record the operator's WiFi settings as follows (refer to Table 203): These are the operator's WiFi networks. You will not be able to view the operator's passphrase as it will be represented by asterisks only. OEM service center network information will be entered and verified at the end of this document. (a) (b) (c) (d) (e) On the left MFD GTC 570 controller, select Utilities. Select Setup. Select WiFi Setup. Select the Favorites tab on the left side of the screen. Record the SSID - (non-oem), Airport, Security, Passphrase, and Mode for each network. Table 203. Operator's (Non-OEM) WiFi Settings SSID (Non-OEM) Airport Security Type (WPA, etc) Passphrase Mode 5. Software and Configuration Loading A. Do the Software and Configuration Loading as follows: CAUTION: The three GDU displays, and four GTC touch controllers must be in configuration mode when Garmin G5000 software or configurations are being loaded. Otherwise, the incorrect loading of data will result. This section gives the steps necessary to load the software and configurations to upgrade from Garmin G5000 software version 25 to version 41. (1) Put the PFD 1, PFD 2, MFD, and the four GTC's in configuration mode as follows: (a) Disengage the following circuit breakers: 1 L PFD GTC (Left CB Panel - E4) 2 MFD L GTC (Left CB Panel - N3) 3 MFD R GTC (Right CB Panel MM4) 4 R PFD GTC (Right CB Panel NN4) (b) Turn the dimmer knob to OFF for PFD 1, MFD, and PFD Page 207

16 (c) Insert the Software Loader SD card (part number: ) into the upper slot of PFD 2. (d) Turn aircraft and avionics power on. (e) Push and hold the right knob on the left PFD GTC and engage the L PFD GTC circuit breaker (E4). 1 Release the right knob on the left PFD GTC when you see INITIALIZING on the GTC screen. (f) Push and hold the right knob on the left MFD GTC and engage the MFD L GTC circuit breaker (N3). 1 Release the right knob on the left MFD GTC when you see INITIALIZING on the GTC screen. (g) Push and hold the right knob on the right MFD GTC and engage the MFD R GTC circuit breaker (MM4). 1 Release the right knob on the right MFD GTC when you see INITIALIZING on the GTC screen. (h) Push and hold the right knob on the right PFD GTC and engage the R PFD GTC circuit breaker (NN4). 1 Release the right knob on the right PFD GTC when you see INITIALIZING on the GTC screen. (i) Turn the R PFD dimming knob on to power the display and load files from the Software Loader SD card (part number: ). 1 The PFD 2 will come up in configuration mode. a The SYSTEM STATUS will show at the top of the screen. b Remove the Software Loader SD card (part number: ) from the upper slot of the PFD 2. (j) Insert the Software Loader SD card (part number: ) into the upper slot of the MFD. (k) Turn the MFD dimming knob on to power the display and load files from the Software Loader SD card (part number: ). 1 The MFD will come up in configuration mode. a The SYSTEM STATUS will show at the top of the screen. b Remove the Software Loader SD card (part number: ) from the upper slot of the MFD. (l) Insert the Software Loader SD card (part number: ) into the upper slot of the PFD 1. (m) Turn the L PFD dimming knob on to power the display and load files from the Software Loader SD card (part number: ). 1 The L PFD will come up in configuration mode. a SYSTEM UPLOAD will show at the top of the screen (2) Clear the Maintenance Log in Configuration Mode as follows: The maintenance log must be cleared before loading the software configurations. (a) On the left MFD GTC 570 touch controller, select GDU Controls. (b) Select MFD on the left side of the screen under the GDU block. (c) Rotate the small FMS knob to select the MAINTENANCE LOG on the page. (d) Use the arrow buttons on the GTC and highlight CLEAR at the bottom of the display. (e) Press the Select button on the GTC. 1 The Erase Entire Maintenance Log? prompt will appear. 2 Press the Enter key on the GTC. 3 Wait until Clearing Log disappears before continuing. (f) Select PFD 1 on the GTC 570 to switch the display being controlled. (3) Load the Software and Configuration as follows: (a) Activate the cursor by pushing down on the FMS knob. (b) Rotate the small FMS knob to drop the menu down, and highlight Model 750 Base Configuration in the GROUP field. (c) Press the Enter key on the right lower section of the GTC screen Page 208

17 (d) (e) (f) Rotate the small FMS knob to drop the menu down, and highlight Model 750 Base in the ITEM field. Press the Enter key on the GTC. In the PRODUCT window, the LRUs will be listed. 1 All of the configuration boxes should be checked. Software boxes will check only if the LRU VERS and CARD VERS columns do not match. It will not try to load anything that is still up to date. (g) (h) Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. Press the Select button on the GTC. A full software load takes approximately 2.5 hours. Each of the GTC touch controllers will reboot and verification messages will display as each controller is loaded. (i) (j) (k) (l) (m) (n) (o) Select GDU Controls on the GTC. When the Upload and Crossfill Complete message is displayed, press the Enter key. Use the arrow buttons on the GTC and highlight UPDT CFG at the bottom of the display. Press the Select button on the GTC. Select YES, and press the Enter key. When the Update Config Complete message is displayed, press the Enter key. Verify that the FLEET ID is correct. The FLEET ID is shown in the upper left corner of the PFD1. Since all the configurations were loaded, the Model 750 aircraft should have the same ID at this point. 1 The FLEET ID Verification code is C Do not continue past this step if the FLEET ID is not correct. The initial configuration loading is not correct. (4) Load the Options as follows: CAUTION: Only load the options that were determined as installed in the Record the Installed Options section earlier, or are being added in accordance with SB or SB , or ACARS or CPDLC. This section will provide the steps required to load the options that were installed previously. (a) Load the WX-500 Stormscope (FK629R- Lightning Detect) as follows: This option may not have been installed previously. These instructions will install it for the first time. If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field Page 209

18 (b) 3 Rotate the small FMS knob to drop the menu down, and highlight FK629K- Lightning Detect in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the Upload is Complete window. Load the Dual HF Option (FK632K- Second HF (Full Up)) as follows: If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. (c) 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field. 3 Rotate the small FMS knob to drop the menu down, and highlight FK632K- Second HF (Full Up) in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the Upload is complete window. Load the GDL69 Option (FK632L- SiriusXM (Weather/Music)) as follows: If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. (d) 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field. b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field. 3 Rotate the small FMS knob to drop the menu down, and highlight FK632L- SiriusXM (Weather/Music) in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. Load the ADF Option (FK658A- ADF) as follows: If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field. b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field. 3 Rotate the small FMS knob to drop the menu down, and highlight FK658A- ADF in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display Page 210

19 (e) 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. Load the GSR56 Option (FK676A- Iridium (Voice/Datalink)) as follows: If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. (f) 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field. b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field. 3 Rotate the small FMS knob to drop the menu down, and highlight FK676A- Iridium (Voice/Datalink) in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. Load the TAWS A Voice Callouts Option (CRQ115- Enable TAWS Callouts) as follows: If this is the first option to be loaded, start at Step 1. Otherwise, start at Step 2. 1 If this is the first option to be loaded, do as follows: a Rotate the large FMS knob to the left until in the GROUP field. b Rotate the small FMS knob to drop the menu down, and highlight Options in the GROUP field. c Press the Enter key on the GTC. Go to Step 3. 2 Rotate the large FMS knob to the left until in the ITEM field. 3 Rotate the small FMS knob to drop the menu down, and highlight CRQ115- Enable TAWS Callouts in the ITEM field. 4 Press the Enter key. 5 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 6 Press the Select button on the GTC. 7 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. The procedures that follow use software unlock SD cards. (g) Load the SurfaceWatch (FK614A - SurfaceWatch) as follows: If you have already loaded an option with an unlock card, then steps 1 and 2 are already complete. 1 Rotate the dimmer knob to OFF for L PFD. 2 Remove the Software Loader SD card (part number: ) from the upper slot of PFD 1 if installed. 3 Insert the SurfaceWatch Unlock SD card (part number: E) into the upper slot of PFD 1. 4 Rotate the dimmer knob to ON for L PFD. 5 PFD 1 should come up in configuration mode. a PFD 1 should display on the system upload page. 6 Activate the cursor by pushing down on the FMS knob Page 211

20 (h) 7 Rotate the small FMS knob to drop the menu down, and highlight Enable_SurfaceWatch in the GROUP field. 8 Press the Enter key. 9 Rotate the small FMS knob to drop the menu down, and highlight Enable_SurfaceWatch in the ITEM field. 10 Press the Enter key. 11 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 12 Press the Select button on the GTC. 13 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the Upload is Complete window. 14 Rotate the dimmer knob to OFF for L PFD. 15 Remove the SurfaceWatch Unlock SD card (part number: E) from the upper slot of PFD 1. a Retain the SurfaceWatch Unlock SD card (part number: E) with the AFM. Load the CPDLC (FK677A-VHF DataLink (CPDLC/Link 2000+)) as follows: The CPDLC (FK677A-VHF DataLink (CPDLC/Link 2000+)) is installed on all 750 aircraft and must be loaded. If you have already loaded an option with an unlock card, then steps 1 and 2 are already complete. 1 Rotate the dimmer knob to OFF for L PFD. 2 Remove the Software Loader SD card (part number: ) from the upper slot of PFD 1 if installed. 3 Insert the CPDLC Unlock card (part number: F0) into the upper slot of PFD 1. 4 Rotate the dimmer knob to ON for L PFD. 5 PFD 1 should come up in configuration mode. a PFD 1 should display on the system upload page. 6 Activate the cursor by pushing down on the FMS knob. 7 Rotate the small FMS knob to drop the menu down, and highlight 'Enable_CPDLC in the GROUP field. 8 Press the Enter key. 9 Rotate the small FMS knob to drop the menu down, and highlight FK677A-VHF DataLink (CPDLC/Link 2000+) in the ITEM field. 10 Press the Enter key. 11 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 12 Press the Select button on the GTC. 13 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the Upload is Complete window. 14 Rotate the dimmer knob to OFF for L PFD. 15 Remove the CPDLC Unlock card (part number: F0) from the upper slot of PFD 1. a Retain the CPDLC Unlock card (part number: F0) with the AFM Page 212

21 CAUTION: Determine which ACARS service provider the operator has chosen before loading the applicable ACARS option. (i) As applicable, load the ARINC Direct ACARS (FK632X-ACARS-ARINC Direct) as follows: If you have already loaded an option with an unlock card, then steps 1 and 2 are already complete. 1 Rotate the dimmer knob to OFF for L PFD. 2 Remove the Software Loader SD card (part number: ) from the upper slot of PFD 1 if installed. 3 Insert the ACARS Application Unlock card (part number: E6) into the upper slot of PFD 1. 4 Rotate the dimmer knob to ON for L PFD. 5 The PFD 1 will come up in configuration mode. a The PFD 1 should display the system upload page. 6 Activate the cursor by pushing down on the FMS knob. 7 Rotate the small FMS knob to drop the menu down, and highlight Enable_ACARS in the GROUP field. 8 Press the Enter key. 9 Rotate the small FMS knob to drop the menu down, and highlight Enable ACARS - ARINC Direct in the ITEM field. 10 Press the Enter key. 11 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 12 Press the Select button on the GTC. 13 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the Upload is Complete window. 14 Rotate the dimmer knob to OFF for L PFD. 15 Remove the ACARS Application Unlock card (part number: E6) from the upper slot of PFD 1. a Retain the ACARS Application Unlock card (part number: E6) with the AFM. CAUTION: Determine which ACARS service provider the operator has chosen before loading the applicable ACARS option. (j) As applicable, load the Honeywell GDC ACARS (FK632X-ACARS-Honeywell GDC) as follows: If you have already loaded an option with an unlock card, then steps 1 and 2 are already complete. 1 Rotate the dimmer knob to OFF for L PFD. 2 Remove the Software Loader SD card (part number: ) from the upper slot of PFD 1 if installed. 3 Insert the ACARS Application Unlock card (part number: E6) into the upper slot of PFD 1. 4 Rotate the dimmer knob to ON for L PFD. 5 The PFD 1 will come up in configuration mode. a The PFD 1 should display the system upload page. 6 Activate the cursor by pushing down on the FMS knob. 7 Rotate the small FMS knob to drop the menu down, and highlight Enable_ACARS in the GROUP field. 8 Press the Enter key. 9 Rotate the small FMS knob to drop the menu down, and highlight Enable ACARS - Honeywell GDC in the ITEM field Page 213

22 10 Press the Enter key. 11 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 12 Press the Select button on the GTC. 13 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. 14 Rotate the dimmer knob to OFF for L PFD. 15 Remove the ACARS Application Unlock card (part number: E6) from the upper slot of PFD 1. a Retain the ACARS Application Unlock card (part number: E6) with the AFM. CAUTION: Determine which ACARS service provider the operator has chosen before loading the applicable ACARS option. (k) As applicable, load the Universal ACARS (FK632X-ACARS-Universal) as follows: If you have already loaded an option with an unlock card, then steps 1 and 2 are already complete. 1 Rotate the dimmer knob to OFF for L PFD. 2 Remove the Software Loader SD card (part number: ) from the upper slot of PFD 1 if installed. 3 Insert the ACARS Application Unlock card (part number: E6) into the upper slot of PFD 1. 4 Rotate the dimmer knob to ON for L PFD. 5 PFD 1 should be in configuration model. a PFD 1 should display the system upload page. 6 Activate the cursor by pushing down on the FMS knob. 7 Rotate the small FMS knob to drop the menu down, and highlight Enable_ACARS in the GROUP field. 8 Press the Enter key. 9 Rotate the small FMS knob to drop the menu down, and highlight Enable ACARS Universal Weather in the ITEM field. 10 Press the Enter key. 11 Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 12 Press the Select button on the GTC. 13 Monitor the configuration load. a Press the Enter key when all the loading is complete to acknowledge the upload is complete window. 14 Rotate the dimmer knob to OFF for L PFD. 15 Remove the ACARS Application Unlock card (part number: E6) from the upper slot of PFD 1. a 6. CMC Diagnostic Configuration Upload Retain the ACARS Application Unlock card (part number: E6) with the AFM. When a full configuration software load is completed, the CMC Diagnostics, Aircraft Configurations, and Crew Profiles must be loaded. A. Do the CMC Diagnostic Configuration Upload as follows: (1) If PFD 1 is still powered after performing the option loading, do as follows: (a) Turn the L PFD dimmer knob OFF. (b) Remove the Software Loader card (part number: ) from the upper slot of PFD 1. (2) Insert the CMC Configuration SD card (part number: ) into the upper slot of the PFD Page 214

23 (3) Put the G5000 back in configuration mode by rotating the dimmer knob to ON for PFD 1. (4) The system upload page should be visible on the PFD 1. (a) Push the FMS knob to activate the cursor under the Group line. (b) Rotate the small FMS knob for the drop down menu and highlight the 750 CMC Config. (c) Press the Enter key. (d) The cursor will move to the Item line. (e) Rotate the small FMS knob for the drop down menu and highlight V (f) Press the Enter key. (g) Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. 1 Acknowledge when Upload and Crossfill Complete is displayed. (5) Make sure that the diagnostic configuration upload was successful. (a) Push the FMS knob to deactivate the cursor. (b) Rotate the small FMS knob on the GTC, and scroll to the last page CONFIGURATION MANAGER. (c) Push on the FMS knob to activate the cursor. (d) Rotate the small FMS knob and scroll down to each of the lines listed below. 1 Record the value shown in the FLEET ID column next to each line in the table below. (Refer to Table 204). a CMC ALERTS b CMC TRIGGERS c LOGGING. 2 Make sure that the three FLEET ID values match the expected values. Table 204. Fleet ID Values FLEET ID CMC ALERTS CMC Triggers Logging FLEET ID (LEFT COLUMN) FLEET ID (Expected Value) F54EB25F 90D884C6 6D4E0345 (6) On the MFD, do as follows: (a) Rotate the dimmer knob OFF for the MFD. (b) Insert the Software Loader SD card (part number: ) into the upper slot of the MFD. (c) Rotate the dimmer knob on for the MFD. (d) Wait three minutes for the system to stabilize. (e) Select the MFD button on the GDU tab on the GTC. (f) Rotate the large FMS knob until on the GDU tab. (g) Rotate the small FMS knob to scroll down to the ALERT CONFIGURATION page. (h) Use the arrow buttons on the GTC and highlight LOG at the bottom of the display. (i) Press the Select button on the GTC. (j) Verify the correct CMC part number appears as ALERT #0. (k) Verify ALERT 1 STATIC is either an amber? or T for TRUE. (l) Verify ALERT 9 CMC Record Inhibit is T for TRUE. (7) If the FLEET IDs in the table or alerts were not correct, do not continue. The CMC Diagnostic configuration loading is not correct. (a) If the FLEET IDs are not correct, do the CMC Diagnostic Configuration Upload. (8) Rotate the dimmer knobs OFF for all three displays to power them OFF. (9) Remove the CMC Configuration SD card (part number: ) from the upper slot of PFD 1. (10) Remove the Software Loader SD card (part number: ) from the upper slot of the MFD Page 215

24 7. PERF and TOLD Database Loading A. PERF Database Loading (1) Load the PERF Database as follows: (a) Insert the PERF Database SD card (part number: ) into the upper slot of PFD 2. (b) Rotate the R PFD dimmer knob to ON. 1 Once the R PFD loads the files, the R PFD will boot up into configuration mode. 2 The SYSTEM STATUS will show at the top of the screen. 3 Remove the PERF Database SD card (part number: ) from the upper slot of PFD 2. (c) Insert the PERF Database SD card (part number: ) into the upper slot of the MFD. (d) Rotate the MFD dimmer knob to ON. 1 Once the MFD loads the files, the MFD will boot up into configuration mode. 2 The SYSTEM STATUS should show at the top of the screen. 3 Remove the PERF Database SD card (part number: ) from the upper slot of the MFD. (e) Insert the PERF Database SD card (part number: ) into the upper slot of PFD 1. (f) Rotate the L PFD dimmer knob to ON. 1 Once the L PFD loads the files, the L PFD will boot up into configuration mode. 2 SYSTEM UPLOAD will show at the top of the screen. (g) Activate the cursor by pushing down on the FMS knob. (h) Rotate the small FMS knob to drop the menu down, and highlight PERF Table in the GROUP field. (i) Press the Enter key. (j) Rotate the small FMS knob to drop the menu down, and highlight PERF Table in the ITEM field. (k) Press the Enter key. (l) The PRODUCT window will list the following: 1 PERF Table GTC 1 2 PERF Table GTC 2 3 PERF Table GTC 3 4 PERF Table GTC 4. (m) Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. (n) Press the Select button on the GTC. This procedure can take approximately 25 minutes. Each of the GTC touch controllers will reboot and verification messages will display as each controller is loaded. (o) (p) Select GDU Controls on the GTC. Press the Enter key to acknowledge the Upload and Crossfill Complete window. B. TOLD Database Loading (1) Load the TOLD Database as follows: (a) Rotate the dimmer knob OFF for the L PFD. (b) Remove the PERF Database SD card (part number: ) from the upper slot of PFD 1. 1 Retain the PERF Database SD card (part number: ) with the AFM. (c) Insert the TOLD Database SD card (part number: ) into the upper slot of PFD 1. (d) Rotate the L PFD dimmer knob to ON. 1 It will boot up into configuration mode. 2 The SYSTEM UPLOAD should show at the top of the screen. (e) Activate the cursor by pushing down on the FMS knob Page 216

25 (f) (g) (h) (i) (j) (k) (l) Rotate the small FMS knob to drop the menu down, and highlight TOLD Table in the GROUP field. Press the Enter key. Rotate the small FMS knob to drop the menu down, and highlight TOLD Table in the ITEM field. Press the Enter key. The PRODUCT window will list the following: 1 TOLD Table GTC 1 2 TOLD Table GTC 2 3 TOLD Table GTC 3 4 TOLD Table GTC 4. Use the arrow buttons on the GTC and highlight LOAD at the bottom of the display. Press the Select button on the GTC. This operation will take approximately 10 minutes. Each of the GTC touch controllers will reboot and verification messages will display as each controller is loaded. (m) (n) (o) (p) Select GDU Controls on the GTC. Press the Enter key to acknowledge the Upload and Crossfill Complete window. Rotate the L PFD dimmer knob off. Remove the TOLD Database SD card (part number: ) from the upper slot of PFD 1. 1 Retain the TOLD Database SD card (part number: ) with the AFM. 8. Aircraft Configuration Loading A. Load the Fuel and Aircraft Weight Units as follows: (1) Insert the Software Loader SD card (part number ) into the upper slot of PFD 1. (2) Rotate the L PFD dimmer knob to ON. (3) The PFD 1 will come up in configuration mode. (4) Make sure that the fuel and aircraft weight are set to the desired unit of measurement: (a) Rotate the small FMS knob to go to the SYSTEM SETUP page. 1 If the units are not the desired units, do as follows: a Push the FMS knob to activate the cursor. b Rotate the large FMS knob to FUEL line in the DISPLAY UNITS box. c Rotate the small FMS knob and highlight KILOGRAMS or POUNDS. d Press the Enter key. e Push the FMS knob to deactivate the cursor. B. Load the Transponder and TCAS Configuration as follows: (1) Rotate the small FMS knob to go to the AIRCRAFT CONFIGURATION page. (2) Make sure that the registration and VFR code are correct. If not, do as follows: (a) Push the FMS knob to activate the cursor. (b) The cursor should be on the Aircraft Registration line. (c) Enter the aircraft tail number using the keyboard button on the GTC. (d) A Hexadecimal code is required to be entered for non-us registered aircraft. (e) The VFR code should be set to the correct value for the country of registry. (3) Make sure that the Domain Identifier is correct as follows: (a) Determine the correct ISO ALPHA-3 code for the country of registry as follows: 1 Access the website: txtavsupport.com and log on using your User Name and Password. 2 Under MY MODELS, select 'Citation 750'. 3 Under AVIONICS, select 'Domain Identifier/Country Code'. 4 Find the desired country and the associated three letter Identifier. An example of a three letter Identifier is "USA" for the United States Page 217

26 (b) If the value entered is not correct, enter the three letter Identifier into the Domain Identifier line using the keyboard button on the GTC. (4) Complete the Transponder and TCAS Configuration as follows: These steps are required whether changes were made to the transponder or TCAS settings or not. (a) (b) (c) Use the arrow buttons on the GTC and highlight SET GTX 1 at the bottom of the display. 1 Press the Select button on the GTC. 2 Press the Enter key to select YES. 3 Press Enter to acknowledge. Use the arrow buttons on the GTC and highlight SET GTX 2 at the bottom of the display. 1 Press the Select button on the GTC. 2 Press the Enter key to select YES. 3 Press Enter to acknowledge. Use the arrow buttons on the GTC and highlight SET GTS at the bottom of the display. 1 Press the Select button on the GTC. 2 Press the Enter key to select YES. 3 Press the Enter key to acknowledge. C. Load the Airplane and Engine Serial Numbers as follows: (1) Rotate the large FMS knob until on the GDU page. (2) Rotate the small FMS knob until on the AIRFRAME CONFIGURATION page. The airplane serial number should be in the 7500XXX format without spaces or dashes. The engine serial numbers should be exactly like what is on the engine dataplates without spaces or dashes. (3) If the engine and airplane serial number are not correct, do as follows: (a) Push on the FMS knob to activate the cursor, which should appear in the GAUGES window. (b) Rotate the large FMS knob to place the cursor in the airframe window. 1 Enter the aircraft serial number of 7500XXX (substitute the last 3 digits of the aircraft serial number for the "XXX") using the keyboard button on the GTC. CAUTION: There are no dashes or spaces in this format. 2 Enter the engine serial numbers exactly as they appear on the engine data plates using the keyboard button on the GTC. CAUTION: There are no dashes or spaces in this format. D. Do the Update Configuration as follows: (1) Push the FMS knob to deactivate the cursor as necessary. (2) Rotate the large FMS knob until highlighted on the SYSTEM tab. (3) Rotate the small FMS knob until on the SYSTEM UPLOAD page. (4) Use the arrow buttons on the GTC and highlight UPDT CFG at the bottom of the display. (5) Press the Select button on the GTC. (6) Select YES, and press the Enter key. (7) When the Update Config Complete message is displayed, press the Enter key. E. Configure the AIRCRAFT ID as follows: (1) Configure the AIRCRAFT ID as follows: (a) Rotate the small FMS knob until you are on the CONFIGURATION MANAGER page. The AIRCRAFT ID number is stored in the system for later use as a comparison tool, so it is very important to be sure that the system is configured correctly before confirming the configuration in the steps that follow Page 218