SERVICE LETTER. Inspection 0.5 Modification 2.0

Transcription

1 Citation SERVICE LETTER SL525C TITLE EQUIPMENT/FURNISHINGS - VENUE SYSTEM v4.2 SOFTWARE UPGRADE EFFECTIVITY MODEL 525C (CJ4) SERIAL NUMBERS thru -0003, thru -0081, thru The equivalent of this service letter has been incorporated on production airplanes -0004, -0082, and and On. Cessna strongly encourages operators to have this service letter completed at a Cessna-owned Citation Service Center or a Rockwell Collins authorized service facility. If a step is missed, over looked, or not completed correctly the MCD hard drive could become corrupted and require that the MCD be replaced. REASON The hard drive in the media center device (MCD) can become corrupted and not boot correctly. DESCRIPTION The service letter transmits Rockwell Collins Service Bulletin Cessna-Venue COMPLIANCE DISCRETIONARY. This service letter can be accomplished at the discretion of the owner. LABOR HOURS WORK PHASE MAN-HOURS Inspection 0.5 Modification 2.0 MATERIAL AVAILABILITY Custom LCP software and custom map software will require at least 30 days advanced scheduling. All airplanes require the LSP Software. SERIAL PART NUMBER QUANTITY KEY WORD AVAILABILITY COST ALL LSP Software * * SL525C October 10, 2013 Page 1 of 5 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A , Fax This document 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: 5E991 COPYRIGHT 2013

2 Citation SERVICE LETTER SL525C Airplane serial numbers in the table order the software that follows in addition to the LSP Software. SERIAL PART NUMBER QUANTITY KEY WORD AVAILABILITY COST -0001, -0003, -0004, thru -0011, -0013, thru -0020, -0023, -0024, -0026, -0028, -0030, -0032, -0034, thru -0040, -0042, thru -0047, -0050, thru -0056, thru -0065, thru -0089, -0091, -0092, thru -0115, and LCP Software (Baseline) * * Airplane serial numbers in the table order the software that follows in addition to the LSP Software. SERIAL PART NUMBER QUANTITY KEY WORD AVAILABILITY COST and , -0057, and , -0022, -0029, -0041, -0043, -0044, -0058, and A , -0027, -0033, and , -0035, -0051, and and LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) LCP Software (Custom) * * * * * * * * * * * * * * * * * * * * SL525C Page 2 October 10, 2013

3 Citation SERVICE LETTER SL525C Airplane serial numbers in the table order the software that follows in addition to the LSP Software and LCP Software (Baseline or Custom). SERIAL PART NUMBER QUANTITY KEY WORD AVAILABILITY COST Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom Map * * Custom LCP software and custom map software will require at least 30 days advanced scheduling. * Please contact Cessna Service Parts & Programs for current cost and availability of parts listed in this service letter. Phone at (Domestic) or (International). Send to: dirop@cessna.textron.com or telefax at WARRANTY Eligibility: Parts: All affected airplanes that are identified in the EFFECTIVITY section of this service letter. Authorized Citation Service Facilities, individual operators, or other maintenance facilities may submit a Credit Claim Form for the parts kit(s) required for accomplishment of this service letter, provided the work is completed and the claim submitted by the expiration date shown below. Labor: Authorized Citation Service Facilities may submit a Credit Claim Form for accomplishment of this service letter, on eligible airplanes, provided the work is completed and the claim submitted by the expiration date shown below. Expiration: November 30, 2015 REFERENCES Rockwell Collins Venue System v4.2 Software SL525C October 10, 2013 Page 3

4 Citation PUBLICATIONS AFFECTED None SERVICE LETTER SL525C ACCOMPLISHMENT INSTRUCTIONS 1. Connect external electrical power to the airplane. 2. Move the BATTERY switch to the ON position. 3. Make sure that the INT MASTER switch is in the NORM position. 4. Make sure that the software is not v4.2. A. Make sure that the Venue system is completely booted up. B. Push the center button in the middle of the direction control pad on the personal control panel. NOTE: Some users may have restricted some of the personal control panels. If MAINTENANCE is not an option the personal control panel is restricted. The master or VIP personal control panel must be located to determine the software version of the Venue system. C. Push the down arrow on the directional control pad to highlight MAINTENANCE. D. Push the right arrow on the directional control pad to enter the maintenance screen. E. Push the down arrow on the directional control pad to highlight CONFIGURATION REPORT. F. Push the right arrow on the directional control pad to enter the configuration report screen. G. Push the down arrow on the directional control pad to highlight MCD1. H. Push the right arrow on the directional control pad to display the LCP software part number and release version. I. If the release version is v4.2 the software listed in this service letter is installed. J. If the release version is less than v4.2 go to Step Do the Rockwell Collins Venue System v4.2 Software. 6. Make sure that the software is v4.2. A. Make sure that the Venue system is completely booted up. B. Push the center button in the middle of the direction control pad on the personal control panel. NOTE: Some users may have restricted some of the personal control panels. If MAINTENANCE is not an option the personal control panel is restricted. The master or VIP personal control panel must be located to determine the software version of the Venue system. C. Push the down arrow on the directional control pad to highlight MAINTENANCE. D. Push the right arrow on the directional control pad to enter the maintenance screen. E. Push the down arrow on the directional control pad to highlight CONFIGURATION REPORT. F. Push the right arrow on the directional control pad to enter the configuration report screen. G. Push the down arrow on the directional control pad to highlight MCD1. H. Push the right arrow on the directional control pad to display the LCP software part number and release version. I. Make sure release version is v Move the BATTERY switch to the OFF position. 8. Disconnect external electrical power to the airplane. 9. Disconnect the airplane battery. SL525C Page 4 October 10, 2013

5 Citation SERVICE LETTER SL525C Record that this service letter has been completed. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM C/O Camp Systems International, 8200 East 34th Street North, Building 1600 Suite 1607 Wichita, KS SL525C October 10, 2013 Page 5

6

7 Cessna-Venue CABIN SYSTEMS VENUE SYSTEM SERVICE BULLETIN Cessna-Venue REVISION NO. 2 VENUE SYSTEM v4.2 SOFTWARE Summary TRANSMITTAL INFORMATION SUMMARY This is Revision 2 of Service Bulletin Cessna-Venue for the Venue System. Revision 2 updates material in Material Required section, Custom Map Content procedures in Accomplishment Instructions section 3.A.(1)(c). Black bars in the margins indicate the changes. Service Bulletin Revision History REVISION DATE OF RELEASE Initial Release December 7, 2012 Revision 1 February 4, 2013 Revision 2 May 1, 2013 NOTE: The modification work described in this Service Bulletin shall be performed only by ROCKWELL COLLINS, Inc., or by personnel and facilities officially authorized by ROCKWELL COLLINS to perform this modification, using materials and processes defined in ROCKWELL COLLINS Avionics Standard Shop Practices, CPN Export Control Classification Number (ECCN) for this document is 5E May 01/13 Copyright, 2013 Rockwell Collins, All rights reserved Page1of32

8 Software License and General Conditions of Sale For each software license procured, the Software License for Equipment Specific Software, reproduced below, shall apply. Software License for Equipment Specific Software Software delivered hereunder, either embedded in equipment described herein or specifically designed for use in or with such equipment, is copyrighted by the seller and shall remain the sole and exclusive property of seller. Seller grants the buyer a perpetual, worldwide, non-exclusive license to use the software only in or with the equipment. The buyer shall not copy, modify, or disassemble the software, or permit others to do so. Buyer shall not transfer the license granted hereby or possession of the software except as part of or with the equipment, such transfer being subject to the restrictions contained herein. Seller may terminate this license upon written notice for violation of any of the terms of the foregoing license. Should the customer have any questions concerning the scope of permitted use, please contact your Rockwell Customer Service Engineer. Rockwell Collins General Conditions of Sale (Rev 06/03) are incorporated herein by reference. 2-May 01/13 Page 2

9 1. Planning Information A. Effectivity The purpose of this document is to describe the information and steps necessary to install software associated with the Venue System at the system level. This procedure specifically describes loading software version 4.2. The procedure described in this Service Bulletin affects the installed Venue System software installed on aircraft. SYSTEM SOFTWARE PART NUMBERS TAIL NUMBERS All B. Concurrent Requirements Aircraft with the following tail numbers need to order a new Custom Map Configuration prior to implementing this Service Bulletin: NEED CUSTOM MAP CONFIGURATION PRIOR TO V4.2 SOFTWARE LOAD CJ4 0006, CJ4 0012, CJ4 0013, CJ4 0025, CJ4 0026, CJ4 0033, CJ4 0045, CJ4 0048, CJ4 0049, CJ4 0052, CJ4 0053, CJ CJ4 0064, CJ4 0071, CJ4 0077, CJ4 0090, CJ CJ4 0116, CJ C. Reason (1) Condition Modification Affects MCDs installed in Venue 3.0 may encounter software load errors due to software corruption on the MCD hard drive. (2) Extent Condition Encountered All Cessna CJ4 aircraft with an MCD with Venue v3.xx software installed. (3) Scope of Modification Incorporation of this Service Bulletin is a permanent change. (4) Expected Benefits of Modification The new Venue software will provide a check disk recovery on every bootup on the MCD to prevent software corruption. A new v2 Moving Map with enhanced graphics and options is also included. D. Description This Service Bulletin provides the instructions to install Venue v4.2 software which incorporates fixes for the MCD. 2-May 01/13 Page 3

10 E. Compliance Optional. F. Approval This Service Bulletin contains no modification information that revised the approved configuration and therefore does not require governmental or other regulatory agency approval. G. Labor The estimated labor to accomplish the instructions of this Service Bulletin is given below. TASK ESTIMATED HOURS Preparation 0.5 Installation 1.0 Test 1.0 Total 2.5 H. Weight and Balance Not affected. I. Electrical Load Data Not affected. J. Software Accomplishment Summary The software changes implemented by this Service Bulletin are documented in ROCKWELL COLLINS, Venue Configuration Index Document (CID) Cessna, Document Number Rev -. K. References ROCKWELL COLLINS Installation and Maintenance Manual Venue (ATA ) CPN ROCKWELL COLLINS, Venue Configuration Index Document (CID) Cessna, Document Number Rev -. ROCKWELL COLLINS, Engineering Change Order, ECO , ECO L. Other Publications Affected None. 2-May 01/13 Page 4

11 2. Material Information A. Cost and Availability The material required to perform this modification should be requisitioned from the ROCKWELL COLLINS Customer Response Center. ROCKWELL COLLINS Customer Account Administration, M/S Business and Regional Systems Rockwell Collins 400 Collins Road N.E. Cedar Rapids, IA Telephone, Domestic and International: (319) or (319) FAX NO. (319) Orders must include quantity, Collins Part Number, and reference Software Product Type number(s). Lead time for ordered material is 30 days after receipt of order. The material to incorporate this Service Bulletin will be provided free of charge. B. Material Required Use the following material to modify LSPs and LCPs for aircraft. All materials are Free of Charge (FOC). DELIVERABLE PART NUMBER LSP QTY LIST PRICE DESCRIPTION BUILD FOC Venue NA System Software Media Set MEDIA TYPE USB OLD LCP NEW LCP QTY LIST PRICE FOC Venue System Software with Cessna CJ4 LCP017 DESCRIPTION BUILD MEDIA TYPE NA USB 2-May 01/13 Page 5

12 OLD LCP NEW LCP QTY LIST PRICE FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP021 DESCRIPTION BUILD MEDIA TYPE NA NA USB USB A A02 1 FOC Venue System Software with Cessna CJ4 LCP021A FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP033. NA NA NA NA NA USB USB USB USB USB 2-May 01/13 Page 6

13 OLD LCP NEW LCP QTY LIST PRICE FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP FOC Venue System Software with Cessna CJ4 LCP069. C. Special Equipment or Tooling Required None. DESCRIPTION BUILD MEDIA TYPE NA NA NA USB USB USB 2-May 01/13 Page 7

14 3. Accomplishment Instructions A. Procedure (1) MCD Boot Order Verification (a) Insert the v4.2 LCP Key (b) Apply power to the Venue system. NOTE: The boot up process takes about 5-6 minutes (c) (d) (e) (f) (g) (h) (i) Switch the bulkhead monitor to the Media Center Device (MCD) video output. Verify if the video output of the MCD is displayed on the bulkhead monitor. If the MCD video output is displayed, continue to Step 3.A.(2) (page 9) If there is no MCD video output on the bulkhead monitor and the blue light on the front of the MCD continuously flashes, continue to the next step. Remove the v4.2 Removable Media from the USB port and insert a USB keyboard into the USB port. Connect a VGA monitor to the VGA port behind the front panel of the MCD. Cycle power to the Venue system by turning off the system for 1-2 minutes and turning on the power to the system again. While the system is booting, monitor the MCD boot-up from the VGA monitor. A Radisys splash screen will be displayed on the VGA monitor for a very short period of time. Press the F2 key while the Radisys splash screen is displayed to enter the BIOS menu of the MCD. For units that have the Aptio BIOS (Shown at the top of the BIOS screen) proceed to the next step 3.A.(1)(i)1. (page 8). For Phoenix Bios, proceed to step 3.A.(1)(j) (page 9): 1. Navigate to the Boot tab by using the right arrow, press the enter key to enter the Boot Order Page. 2. Use the down arrow to navigate down to the boot option # with the corresponding to SATA: Hitachi HT. 3. Press the "+" key until the Boot Option # corresponding to SATA: Hitachi HT is moved up to Boot Option #1. 4. Press "F4" to apply the boot order change and exit the BIOS Setup Utility. A confirmation to save will be displayed. 5. Press "Enter" to save the configuration changes and exit. Skip to step 3.A.(1)(m) (page 9). 2-May 01/13 Page 8

15 NOTE: Ensure that the changes are saved prior to exiting the BIOS. (j) For units that have the Phoenix BIOS (Shown at the top of the BIOS screen) proceed to the next step 3.A.(1)(j)1. (page 9): 1. Navigate to the Boot tab by using the right arrow, press the enter key to enter the Boot Order Page. 2. UsethedownarrowtonavigatedowntotheIDEHDDwiththe corresponding to the HITACHI HTSxxxxxx. 3. Press the "+" key until the IDE HDD corresponding HITACHI HTSxxxxxx is moveduptobootorder#1. 4. Press "F10" to apply the boot order change and exit the BIOS Setup Utility. A confirmation to save will be displayed. (k) Press "Enter" to save the configuration changes and exit. NOTE: Ensure that the changes are saved prior to exiting the BIOS. (l) Allow the MCD to reboot, than remove power on the Venue system. (m) Remove keyboard, and re-insert the v4.2 LCP key (n) (o) (p) (q) Apply power to the Venue system. Wait for the UUT to boot. Ensure that the Media Center main menu is shown on the primary display and the Moving Map appears on the bulkhead monitor. If the Moving Map does not appear on the bulkhead monitor, repeat steps 3.A.(1)(a) (page 8) through 3.A.(1)(p) (page 9) again. If the Moving Map appears on the bulkhead monitor remove the VGA monitor and proceed to step 3.A.(2) (page 9) Loading Procedure. (2) Loading procedures for tail specific LCPs, LSPs and Custom Map Content. (a) Overview Perform the following load procedure for the LCP, then repeat the same steps for the LSP and if purchased, the v2 Custom Map Content per section 3.A.(2)(c) (page 30). CAUTION: IF THE LCP IS NOT LOADED PRIOR TO LOADING THE 4.2 LSP, THE 4.2 LSP SOFTWARELOADWILLNOTWORK. 2-May 01/13 Page 9

16 1. Apply power to the Venue system and wait until the system status within the maintenance page indicates a green checkmark. If it does not go green, Rockwell Collins should be contacted. The boot up process takes about 5-6 minutes 2. Switch the bulkhead monitor to the Media Center Device (MCD) video output. 3. When loading applicable LCP, LSP, or Custom Map Content, insert the media into USB port of MCD. Loading will be initiated from the PSW for LCP and LSP loads. NOTE: After any software installation, a power cycle immediately after the load may corrupt the NAND file system. This will result in a recovery routine to run and extend the boot time. It is recommended to wait for a minimum of 5 minutes after loading software before power cycling the system. Software loading should not be started for at least 5 minutes after a system or LRU power cycle or LRU reset. The screen shots showed in this document are only samples. (b) CAUTION: WHEN LOADING WITH A USB STICK, DO NOT LEAVE THE USB STICK IN THE LRU UNATTENDED. THE USB STICK PROTRUDES FROM THE LRU AND IS SUSCEPTIBLE TO BEING BENT OR BROKEN BY PEOPLE PASSING BY OR BY CABINET DOORS WHEN UNITS ARE MOUNTED IN A CABINET. To install tail specific LCPs or LSPs, perform the following procedure: 1 Insert the Removable Media that contains the applicable specific LSP/LCP files to be loaded into USB portofmcd. The folder image will appear on the cabin monitor when the USB drive has been recognized. At this point, you can enter Software Load and see the files. NOTE: It is recommended that any MCD Blu Ray disc be removed prior to the loading process. The system will detect and display the USB drive found with a Venue folder. 2-May 01/13 Page 10

17 2 Go to the Master or a VIP PSW and access Maintenance option. NOTE: The PSW Role may need to be changed to access the Maintenance option. MAINTENANCE SCREEN Figure 1 2-May 01/13 Page 11

18 3 Choose the Software Load option under Maintenance menu. If the PSW is running with a default or a factory LCP, the Software Load option will be right on first screen as the first item. SOFTWARE LOAD SCREEN Figure 2 2-May 01/13 Page 12

19 NOTE: A PSW can be identified as running with default or factory LCP by looking at the screen heading on the first screen. If displayed as Default LCP, it is running with default LCP. If displayed as ROCKWELL COLLINS, it is runningwithafactorylcp. SOFTWARE LOAD SCREEN Figure 3 2-May 01/13 Page 13

20 4 Select the Software Load option by pressing the right side of the D-pad. PSW will display as Searching files. Please wait. SOFTWARE LOAD SCREEN Figure 4 2-May 01/13 Page 14

21 5 WaituntilthePSWshowsupwith the list of Cii files to be loaded. NOTE: If the removable media is not recognized or not inserted properly or does not have the expected folder structure, then the following error message will be displayed: No removable media available with Venue folder in it 6 Select home and re-enter software load. If the same message appears, call Rockwell Collins. SOFTWARE LOAD ERROR Figure 5 2-May 01/13 Page 15

22 7 You are able to browse the list of files on the removable media by pressing D-pad UP or D-pad Down. However, selection of any file(s) is not possible, nor necessary. To continue the software loading, choose Yes by pressing the D-pad RIGHT. You will see the Software Load screen listing LRUs and software PN. NOTE: "No" and "Yes" are controlled via the circular D pad left/right selections. SOFTWARE LOAD SCREEN Figure 6 8 By choosing the Yes option, The PSW will do a compatibility check of the software to be loaded. A "Validating files, Please wait" screen will appear, then "Checking compatibility, Please wait" screen after. The PSW will display as Checking compatibility. Please wait. NOTE: When loading the LCP, the Validating files and Checking Compatibility screens appear quickly. When loading the LSP, the system will show these 2messages longer. 2-May 01/13 Page 16

23 SOFTWARE VALIDATING SCREEN Figure 7 SOFTWARE COMPATIBILITY SCREEN Figure 8 2-May 01/13 Page 17

24 9 Wait until the PSW shows up the confirmation screen. 10 Press the center button of the D-pad to initiate a Force Load. The PSW will display Confirm to load with a red X The red X will be replaced by a green checkmark. SOFTWARE LOAD SCREEN Figure 9 NOTE: NOTE: When performing the LCP load, you will get an Incompatibility message The Force Load selection enables software to be loaded to LRUs regardless of their current load version. 2-May 01/13 Page 18

25 SOFTWARE LOAD SCREEN Figure 10 2-May 01/13 Page 19

26 11 To start the software loading choose Yes by pressing the Right key. By choosing yes, the load will start immediately. Choosing No by clicking Left or Home button will not start the loading. The PSWs will display as Loading started. Within few seconds, those PSWs that are loading will display a red screen showing the loading status. SOFTWARE LOAD SCREEN Figure Once the loading is completed for PSWs, the red screen will go away and will come up with regular UI screens. The loading status for other LRUs (HDAV, MCD and any other PSWs that are still loading) can be observed by choosing the Software Load Status option present under the Maintenance menu. In default/factory LCP, this option will be right on the first screen as the second item. 2-May 01/13 Page 20

27 NOTE: When loading the v4.2 LCP, the end result is a Default GUI, not a "normal CJ4 UI". When loading the LSP, you do get the "normal CJ4 UI". SOFTWARE LOAD STATUS SCREEN Figure 12 2-May 01/13 Page 21

28 SOFTWARE LOAD SCREEN Figure 13 NOTE: When loading the LCP, the load status at the top right corner indicates 100% when it is complete. You must also see MCD on the list to insure that the load has actually completed. If it does not appear on its own, exit Software Load Status and re-enter. It will refresh the list and show the MCD. 2-May 01/13 Page 22

29 SOFTWARE LOAD STATUS SCREEN Figure 14 2-May 01/13 Page 23

30 13 Those LRUs whose status is displayed as Installation Complete have completed their installation. Wait for all the LRUs load status to be displayed as Installation Complete. Withthisstepthe installation is complete. Youwillbeabletoseethestatus bar with messages at the left bottom of the window similar to the one in Figure 13. NOTE: Verify that all LRUs are accounted for before concluding the software installation. 14 UsingthePSWverifyLCPload by selecting "Maintenance option", "System Status", "Conformity", "Conformity Status", then select desired LRU, followed by "LCP" screen. Screen-shoots sequence should appear as displayed in Figures 14 through 18 when loading a LSP. 2-May 01/13 Page 24

31 NOTE: Verify that all LRUs are accounted for before concluding the software installation. NOTE: When loading the LCP, the PSW GUI will display a Default GUI with a heading DEFAULT LCP at the top. SYSTEM STATUS SCREEN Figure 15 2-May 01/13 Page 25

32 SYSTEM STATUS SCREEN Figure 16 2-May 01/13 Page 26

33 CONFORMITY STATUS SCREEN Figure 17 2-May 01/13 Page 27

34 CONFORMITY SCREEN Figure 18 2-May 01/13 Page 28

35 LRU LCP SCREEN (Reference) Figure 19 NOTE: Figure 19 is an example, after the LCP load the expected values and actual values will not match. 15 If conformity fails when loading the LSP, repeat the load procedure from step Remove the USB drive after system conformity passes. Repeat load procedure to load LSP after initially loading the LCP. NOTE: When loading the LCP initially, it is expected that conformity will fail; it is still required to load the LSP. 17 Perform a complete power down of the Venue system after both LCP and LSP are loaded to verify the system is functional. NOTE: Step 17 must be completed at the end of the procedure before placing system back in service. 2-May 01/13 Page 29

36 (c) NOTE: After any software installation, a power cycle immediately after the load may corrupt the NAND file system. This will result in a recovery routine to run and extend the boot time. It is recommended to wait for a minimum of 5 minutes after loading software before power cycling the system. Software loading should not be started for at least 5 minutes after a system or LRU power cycle or LRU reset. The screen shots shown in this document are only samples. To install tail specific V2 Custom Map Content perform the following procedure: 1. From a PSW with a Master or VIP role, select a cabin or seat monitor to display the Airshow Moving Maps. This allows the user to view the MCD load status during the loading process. CAUTION: WHEN LOADING WITH A USB STICK, DO NOT LEAVE THE USB STICK IN THE LRU UNATTENDED. THE USB STICK PROTRUDES FROM THE LRU AND IS SUSCEPTIBLE TO BEING BENT OR BROKEN BY PEOPLE PASSING BY OR BY CABINET DOORS WHEN UNITS ARE MOUNTED IN A CABINET. 2. Insert the USB key containing the MCD Custom Map Content into the MCD USB Port. The MCD detects the USB key within a few seconds. a. If the key contains valid installation data, the MCD displays an installation status screen on the selected monitor. b. The status screen displays the part numbers of the software components that will be installed and a 30-second countdown timer. c. The MCD waits for the countdown to complete before starting the data transfer to allow the user time to cancel the installation. d. If the USB installation key is removed within the 30-second period, the installation is cancelled and the existing Map software will automatically restart. e. If the 30-second countdown period completes and the USB installation key is still inserted in the MCD USB port, the MCD starts to copy the files from the USB key to the MCD. A status screen displays a progress bar indicating the status of the copying process. f. The copying process is completed when the progress bar is filled to 100%. A status screen indicates that the installation files have been copied successfully, and requests the USB key be removed. 3. Remove the USB installation key from the MCD. a. The MCD begins installing the copied files. When the progress bar is filled to 100%, a status screen reports that the installation was successful. 2-May 01/13 Page 30

37 b. The installation is followed by a cleanup process. When the progress bar is filled to 100%, the installation is complete. c. The overall status of the software load is displayed. The screen displays the part numbers of the software that was loaded. d. After the installation is complete, the MCD reboots itself twice. During this time, there will be two periods where the screen will go blank for up to 45 seconds before the boot screen appears. The MCD will restart with the new configuration. NOTE: This part of the process will take approximately 5 minutes to complete. 4. Verify the correct software part numbers and following files were successfully loaded as follows: a. Airshow for MCD Support Filea b. Timezone Database c. Jeppesen Database d. ACE MCD Configuration Update Software Installation Verification (Reference Only) Figure 20 2-May 01/13 Page 31

38 B. Testing Procedure Refer to ROCKWELL COLLINS Installation and Maintenance Manual Venue (ATA ) CPN or the equivalent Cessna documentation for check out procedures. C. Identification Procedure None. 2-May 01/13 Page 32