Maintenance Manual

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MAINTENANCE MANUAL SOFTWARE — MAINTENANCE PRACTICES 1. Modular Avionics Unit / Modular Radio Cabinet — Software Loading (Full Load) A. General This procedure provides instructions for a full load for the Master Operating System (MOS) software / databases. The MOS software / databases are loaded to modules or Line Replaceable Units (LRUs) of the Modular Avionics Unit (MAU) / Modular Radio Cabinet (MRC). Prior training in performing a software load procedure on an aircraft is required. A full load is necessary when new Primus Epic software is available or when one or all of the following have been updated: • • • • • • • • • •

Operational Software Aircraft Personality Module (APM) settings and rigging APM options Aerodynamics-Engine Database (AEDB) Integrated Navigation Data Services (INDS) navigation, charts, terrain, envelope modulation or terrain threat databases FMS Takeoff and Landing Data (TOLD) Electronic Checklist (ECL) database Communication Management Function (CMF) / Airline Modifiable Information (AMI) Loadable Diagnostic Information (LDI) / Aircraft Configuration Monitoring Function (ACMF) database Programmable CAS message database

New software / databases or updates are typically available on the following media: • Universal Serial Bus (USB) flash drive or memory stick • Compact Disks (CD) Current INDS databases are available and may be downloaded from the INDS website. This system contains ESD sensitive components. Ensure all ESD safety precautions and practices are followed while performing maintenance. See Electrostatic Discharge - Standard Practices, 20-23-00, Maintenance Practices. B. Preparation SPECIAL TOOLS AND TEST EQUIPMENT Ethernet cable ..................................................................................................................... Standard Maintenance laptop ............................................................................................................. Standard (1) Reference(s) • Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices • Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices • Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices • Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices • Electrostatic Discharge - Standard Practices, 20-23-00, Maintenance Practices • Honeywell Data Loading Procedures for the Gulfstream PlaneView Primus Epic System (2) Aircraft Preparation

20-22-00 Page 201 November 30/19

MAINTENANCE MANUAL (a) Prepare aircraft for safe ground maintenance. See Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices. (b) Ensure the following Circuit Breakers (CB) are closed: NOMENCLATURE

PANEL

LOCATION

MAU 3B PRI

Pilot

FLT INSTRUMENTS

MAU 3A PRI

Pilot

FLT INSTRUMENTS

MAU 2B SEC

Pilot

FLT INSTRUMENTS

MAU 2A SEC

Pilot

FLT INSTRUMENTS

MAU 1B SEC

Pilot

FLT INSTRUMENTS

MAU 1A PRI

Pilot

FLT INSTRUMENTS

MRC 1 NIM

Pilot

COMM/NAV

MAU 1A SEC

Copilot

FLT INSTRUMENTS

MAU 1B PRI

Copilot

FLT INSTRUMENTS

MAU 2A PRI

Copilot

FLT INSTRUMENTS

MAU 2B PRI

Copilot

FLT INSTRUMENTS

MAU 3A SEC

Copilot

FLT INSTRUMENTS

MAU 3B SEC

Copilot

FLT INSTRUMENTS

DMU

Copilot

COMM/NAV

MRC 2 NIM

Copilot

COMM/NAV

(c) Ensure the following aircraft conditions: • Airspeed less than 50 knots • Throttles at idle (d) Ensure aircraft is in ground mode. If required, place aircraft in ground mode as follows: 1 Open LDG GEAR SVC panel door 122AR. See Figure 201. NOTE:

The WOW OVRD and LG MODE switches are located on the LDG GEAR SVC panel.

2 Select LG MODE switch to MAINT. 3 Move switch slide lock up. NOTE:

Slide lock holds LG MODE switch in MAINT mode.

4 Insert maintenance mode lockout pin. 5 On LDG GEAR SVC panel, verify LG MODE light comes on. 6 Remove safety cable securing WOW OVRD switch cover.

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MAINTENANCE MANUAL WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

7 Select WOW OVRD switch to GND. WARNING:

APPLYING ELECTRICAL POWER TO AIRCRAFT MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE APPLYING ELECTRICAL POWER MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(e) Apply electrical power to aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (f) Ensure all Primus Epic equipment is powered for a minimum of 15 minutes prior to beginning a software load. C. Procedure CAUTION: NOTE:

FAILURE TO OBSERVE ELECTROSTATIC DISCHARGE PROCEDURES MAY CAUSE DAMAGE TO SYSTEM COMPONENTS.

The following procedures are provided: • Procedure 1.C1. - Maintenance Laptop Setup • Procedure 1.C2. - Full Load Procedures

C1. Maintenance Laptop Setup NOTE:

Software / database loading is accomplished using a maintenance laptop with the Central Maintenance Computer (CMC) Remote Terminal (RT) application and Data Loading System (DLS) tool.

(1) Connect maintenance laptop as follows: NOTE:

The Data LAN Management Unit (DLMU) contains a RJ45 jack (Ethernet), USB port and two Secure Digital (SD) memory card slots

(a) Connect Ethernet cable to maintenance laptop. (b) Open DLMU access door. (c) Connect Ethernet cable to DLMU (opposite end connected to maintenance laptop). (2) Perform maintenance laptop preliminary procedures as follows: (a) Connect maintenance laptop to aircraft 60 Hz power outlet. NOTE:

Aircraft 60 Hz power is used to provide a stable power source for software loading. A sufficiently charged maintenance laptop battery may also provide a suitable stable power source for software loading.

(b) Turn maintenance laptop power on. (c) If maintenance laptop kiosk is available, go to Step 1.C1.(3).

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MAINTENANCE MANUAL NOTE:

The kiosk will change the laptop system settings for communication with CMC terminal and DLS.

(d) If laptop kiosk application is unavailable, comply with the following: 1 Disable the following programs or applications which may affect software / database loading as necessary: • • • • •

Firewall software Zone alarm software Norton software Active screen saver Power save options

2 Ensure maintenance laptop Internet Protocol (IP) address is configured as follows: NOTE:

Help on how to www.microsoft.com.

configure

an

IP

address

is

available

at

a Access control panel settings. b Open network connections. c Select local area connection. d Open properties for local area connection. e Select Transmission Control Protocol / Internet Protocol (TCP / IP) connection. f Open properties for TCP / IP connection. g For maintenance laptop with Windows 7, set IP address as follows: • IP address: 192.168.192.1 h For maintenance laptop with Windows XP, set IP address as follows: • IP address: 192.168.192.7 i Set subnet mask to the following: • 255.255.255.0 (3) Verify aircraft LAN is operational and all MAU / MRC modules are communicating as follows: (a) If maintenance laptop kiosk is available, perform the following: 1 Locate Other Utilities menu on maintenance laptop kiosk. 2 Select CyberKit link in Other Utilities menu. 3 Go to Step 1.C1.(3)(c). (b) If laptop kiosk application is unavailable, double click CyberKit Ping shortcut or perform the following: NOTE:

The CyberKit Ping shortcut should be located on maintenance laptop desktop.

1 Click on maintenance laptop START menu. 2 Select programs. 3 Select CyberKit.

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MAINTENANCE MANUAL (c) Ensure CyberKit is properly configured, see Gulfstream Aerospace Corporation (GAC) maintenance applications disk to configure CyberKit for aircraft. NOTE:

A valid module list file of IP addresses resolved to names for the aircraft configuration (modules that directly transmit / receive on the LAN) is necessary to run CyberKit.

(d) Verify CyberKit application window opens and displays an IP address for each MAU and MRC module / LRU as follows: 1 Each MAU and MRC module / LRU listed in Software Matrix Table 201 is operational. 2 Percent loss column for any module does not display more than a 5% loss. NOTE:

Modules experiencing more than a 5% loss typically produce software / database load errors.

(4) Start CMC Remote Terminal application as follows: (a) If maintenance laptop kiosk is available, perform the following: 1 Select CMC Terminal/DLS link in Aircraft System Tools menu. NOTE:

This kiosk link will set the laptop IP address to 192.168.192.1 and disable the firewall, anti-virus and wireless card.

2 Select OK. 3 Go to Step 1.C1.(4)(c). (b) If laptop kiosk application is unavailable, double click CMC.RT.exe shortcut to start CMC Remote Terminal application or perform the following: NOTE:

The CMC.RT.exe shortcut should be located on maintenance laptop desktop.

1 Click on maintenance laptop START menu. 2 Select CMC Remote Terminal. 3 Select CMC RT / DLS tool. (c) Verify CMC Remote Terminal application window opens and connects to aircraft LAN as follows: CMC Remote Terminal Exit Settings ACMF About CMC MAIN MENU

MAINTENANCE MESSAGES SYSTEM DIAGNOSTICS EXTENDED MAINTENANCE END OF FLIGHT PAGE

FAULT HISTORY DATABASE CURRENTLY

0% FULL

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MAINTENANCE MANUAL 1 If CMC Remote Terminal application window displays CMC MAIN MENU, go to Step 1.C1.(5). 2 If CMC Remote Terminal application can not communicate with CMC, perform the following: NOTE:

Communication with the CMC is not possible if the CMC software has not been loaded or the CMC module has failed.

a If CMC software has not been loaded, go to Step 1.C1.(6)(b). b If CMC software load status unknown, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. (5) Ensure appropriate CMC RT / DLS version is installed on maintenance laptop as follows: (a) Select About on menu bar of CMC Remote Terminal application window. NOTE:

The pop-up window About CMC Remote Terminal displays CMC RT / DLS versions.

(b) Verify appropriate version of CMC RT / DLS from GAC maintenance applications disk are installed on maintenance laptop as follows:

(1) (2)

ASC

CMC RT

DLS

Aircraft having ASC 902

26.1(1)

8.2.0(2)

The CMC RT 26.1 / DLS 8.2.0 software are Windows 7 compliant. The DLS main menu supports a refresh allowing the user to change media and refresh the display. When browsing to locate [DR-PN]: file, duplicate part numbers will now contain an (XR) to indicate the part number to be selected.

(c) If CMC RT / DLS are incorrect version, install appropriate version of the CMC RT / DLS from GAC maintenance applications disk. NOTE:

Prior to installation of any CMC RT / DLS tool, it is recommended that all previous versions be removed by utilizing the add / remove programs function provided in the Windows control panel.

(6) Start DLS tool as follows: (a) Select EXTENDED MAINTENANCE button on CMC Remote Terminal application window menu. NOTE:

The CMC Remote Terminal menu provides access to the DLS tool that controls software loading. The CMC Remote Terminal application window is divided with the display area on the left and menu on the right. The maintenance laptop cursor control is used to select CMC Remote Terminal menu buttons and the cursor must be inside the application window for functions to be active.

(b) If DATA LOADER button does not display in CMC Remote Terminal application window, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. (c) Select DATA LOADER button.

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MAINTENANCE MANUAL C2. Full Load Procedures CAUTION:

DO NOT REMOVE POWER AFTER SOFTWARE LOAD HAS BEGUN. LOSS OF POWER CAN CAUSE LOADING ERRORS.

(1) Verify software / databases are correct and latest version. Refer to software configuration data page in aircraft logbook. NOTE:

For assistance if unsure, contact Gulfstream Customer Support.

(2) Perform full load of software / database media as follows: NOTE:

A full load of all media is typically performed in sequence. The Operational Software must be loaded first.

(a) Perform the following in sequence when one or all of have been updated: • • • •

Procedure Procedure Procedure Procedure

1.C3. 1.C4. 1.C5. 1.C6.

-

Load Operational Software Load Aircraft Personality Module Settings and Rigging Data Load Aircraft Personality Module Options Load Aerodynamics Engine Database

(b) Perform the following as necessary: NOTE:

A full load of all media is typically performed in sequence. A full load of individual media is performed for each software / database that has changed or updated from its previous revision cycle.

• Procedure 1.C7. - Load Integrated Navigation Data Services Airspace, Communications, EGPWS and Navigational Data (Red Media) • Procedure 1.C8. - Load Integrated Navigation Data Services Electronic Terminal Charts, Geopolitical Boundaries, Airport Information and Obstacle Data (Blue Media) • Procedure 1.C9. - Load Integrated Navigation Data Services Terrain Data (Green Media) • Procedure 1.C10. - Load Takeoff and Landing Data • Procedure 1.C11. - Load Electronic Checklist Database • Procedure 1.C12. - Load Communication Management Function / Airline Modifiable Information Database • Procedure 1.C13. - Load Loadable Diagnostic Information / Aircraft Configuration Monitoring Function Database • Procedure 1.C14. - Load Programmable CAS Message Database Do not perform with any load verification checks until all new or updated software / databases have been loaded. This aids in determining what modules may require a target load due to any errors during full load. C3. Load Operational Software (1) Ensure Operational Software media is available to CMC RT / DLS. NOTE:

Media (USB or CD) must be available to the CMC RT / DLS during the preloading scan. Unless otherwise specified, insert media in the maintenance laptop (USB port or CD-ROM drive). Media contents or files may be copied to a directory or folder on the maintenance laptop.

(2) Access DLS INSTALLATION FUNCTION as follows:

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MAINTENANCE MANUAL (a) Select DATA LOADER button from EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load Operational Software using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

The CMC RT / DLS display is used to browse available drives, directories and folders on the maintenance laptop and any connected device to locate, select and highlight [DR-PN]: (loadable software / database) files as follows:

• Data Management Unit (DMU) - Browse DMU DRIVES / DMU-0: / CD-ROM • CD in maintenance laptop - Browse REMOTE TERMINAL / CD-ROM D: • USB in maintenance laptop - Browse OTHER DATA SOURCES / AVAILABLE DRIVES / FLOPPY DRIVE E: (DLS tool displays USB device as FLOPPY DRIVE) • Media copied or saved on maintenance laptop - Browse OTHER DATA SOURCES / AVAILABLE DRIVES / HARD DRIVE C: The maintenance laptop up / down arrows may also be used to locate and highlight files or targets. When maintenance laptop up / down arrows are used, the Enter button selects highlighted software or targets for software loading. (c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The DLS tool configuration check includes an IP address and hardware part number loading compatibility check. The configuration check may take several minutes.

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

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Expected load times vary based on software being loaded.

MAINTENANCE MANUAL A full load of Operational Software may take up to 1.5 hours. (h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. The DLS tool display indicates a percentage complete during the data loading sequence. Load times and percent complete indication may change during load process. The DLS tool may encounter an error, retry an operation or identify additional files to load. The working progress bar (blue) may also display inside or behind the DLS window on the maintenance laptop indicating a DLS process is running. Cockpit display units may indicate the following once a software load has been initiated: • X (red) Cockpit display controllers may indicate the following once a software load has been initiated: • No input from MAU At times the DLS tool may appear to be frozen or locked up when it is not. Estimated load time may have counted down to 0 and load process may not be complete. A cockpit display with a X (red) may also indicate process may not be complete. Avoid canceling the load process and allow sufficient time for the full load process to complete. When it becomes necessary to cancel the load process, wait until the load time estimate has counted to zero.

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE / 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If software load failure occurs, perform the following: NOTE:

The DLS tool displays error messages that may occur during software loading. The RETRY button should be used before reattempting a full or target load. The CMC RT / DLS will attempt to reload the software on the modules that experienced the failure and should will yield a shorter load time.

1 Record any module loading errors.

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MAINTENANCE MANUAL 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove Operational Software media. (5) Load APM settings and rigging data. Go to Step 1.C4.(1). C4. Load Aircraft Personality Module Settings and Rigging Data (1) Ensure a backup of Enhanced Vision System (EVS) alignment parameters has been performed as follows: NOTE:

Prior to loading APM settings and rigging media, a backup of rigging data ensures (EVS alignment parameters) have been saved on maintenance laptop. A backup rigging data is typically performed during a full load procedure. The backup of rigging data is performed using DLS and needs to be performed from the maintenance laptop.

(a) Access maintenance laptop shortcuts. NOTE:

The maintenance laptop should have a shortcut to backup rigging data. The shortcut copies EVS rigging data from one of the APMs to a backup file on maintenance laptop. A backup of rigging data is typically performed after adjusting EVS raster patch to save EVS alignment parameters.

(b) Select Rigging Backup shortcut to save rigging data. (c) Access CMC RT / DLS on maintenance laptop. (2) Ensure APM settings and rigging media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(3) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button from menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (4) Load APM settings and rigging data using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate APM settings and rigging [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file.

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MAINTENANCE MANUAL (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If data load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (5) Restore rigging data as follows: NOTE:

A rigging restore is performed to load rigging file alignment parameters. A rigging restore is typically performed during a full load procedure. The rigging restore is not performed using DLS and needs to be performed from the maintenance laptop.

(a) Access maintenance laptop shortcuts.

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MAINTENANCE MANUAL NOTE:

The maintenance laptop should have a shortcut for rigging restore. The shortcut loads EVS rigging data from backup file on maintenance laptop to APMs No. 1 - No. 4.

(b) If Rigging Restore shortcut is not available, load rigging data as follows: 1 Access APM settings and rigging media on maintenance laptop. CAUTION:

RUNNING THIS BATCH FILE WILL REQUIRE ENHANCED VISION SYSTEM ALIGNMENT PROCEDURE TO BE PERFORMED.

2 Select Rigging Init file. NOTE:

The Rigging Init batch file is used to reset APM rigging data in APMs No. 1 - No. 4. Running this Batch File without a rigging backup file will require an EVS alignment procedure to adjust EVS raster patch and save EVS alignment parameters.

(c) Select Rigging Restore shortcut to restore rigging data. (d) Access CMC RT / DLS on maintenance laptop. (6) Remove APM settings and rigging media. (7) Load APM options. Go to Step 1.C5.(1). C5. Load Aircraft Personality Module Options (1) If APM options media has a security code, record security code. • APM options Security Code: ____________ NOTE:

Security code is located on the front of the CD media.

(2) Ensure APM options media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(3) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button from menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (4) Load APM options using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate Epic folder files.

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MAINTENANCE MANUAL NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) For APM options media which includes a security enabled feature, perform the following: 1 Read Licensing agreement. 2 Select I Accept to continue. NOTE:

Selecting I Decline will return to DLS menu.

3 Select Enter Passcode. 4 Select Authorization Code field. 5 Enter code using maintenance laptop keyboard. (g) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(h) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(i) Select START LOAD button on menu. (j) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(k) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (l) If APM options load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors.

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MAINTENANCE MANUAL 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (5) Remove APM options media. (6) Load AEDB file. Go to Step 1.C6.(1). C6. Load Aerodynamics Engine Database (1) Ensure AEDB media (typically located with APM settings and rigging media) is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button from menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load AEDB using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate AEDB [DR-PN] file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight AEDB [DR-PN]: file as follows: • GWWXXXXXXX (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display:

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MAINTENANCE MANUAL CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove AEDB media. (5) To continue full load with all media in sequence, go to Step 1.C7.(1). (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C7. Load Integrated Navigation Data Services Airspace, Communications, EGPWS and Navigational Data (Red Media) (1) Ensure INDS airspace, communications, EGPWS and navigational data (red media) are available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Review epic load instructions document for any database changes or limitations. NOTE:

Epic load Instructions.htm is included with INDS airspace, communications, EGPWS and navigational data.

(3) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

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MAINTENANCE MANUAL (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (4) Load INDS airspace, communications, EGPWS and navigational data using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate INDS airspace, communications, EGPWS and navigational data [DRPN]: files. • [DR-PN]: World 3-3XX (16M FMS) • [DR-PN]: 966-0145-XXX (EGPWM THREAT) • [DR-PN]: 966-0114-XXX (EGPWM ENV MOD) NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded. Any files that display ALREADY LOADED after configuration check, have not changed since previous cycle of IDNS media and will not be updated.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX %

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MAINTENANCE MANUAL NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE / 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (l) Repeat Step 1.C7.(3) thru Step 1.C7.(4)(k) until all changed IDNS media [DR-PN]: files have been loaded. (5) Remove INDS airspace, communications, EGPWS and navigational data (red media). (6) To continue full load with all media in sequence, go to Step 1.C8.(1). (7) To select another media for full load, go to Step 1.C2.(2)(b). (8) If full load complete, go to Step 1.D.(1). C8. Load Integrated Navigation Data Services Electronic Terminal Charts, Geopolitical Boundaries, Airport Information and Obstacle Data (Blue Media) (1) Ensure INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media) are available to CMC RT / DLS as follows: NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays:

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MAINTENANCE MANUAL PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b). The WOW input to DLMU is required.

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded. Any files that display ALREADY LOADED after configuration check, have not changed since previous cycle of IDNS media and will not be updated.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE.

(j) Verify the following message displays:

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MAINTENANCE MANUAL PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media). (5) To continue full load with all media in sequence, go to Step 1.C9.(1). (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C9. Load Integrated Navigation Data Services Terrain Data (Green Media) (1) Ensure INDS terrain data (green media) is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load INDS terrain data using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate INDS terrain data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file.

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MAINTENANCE MANUAL (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded. Any files that display ALREADY LOADED after configuration check, have not changed since previous cycle of IDNS media and will not be updated.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove INDS terrain data (green media). (5) Continue a full load with all media in sequence, go to Step 1.C10.(1).

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MAINTENANCE MANUAL (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C10. Load Takeoff and Landing Data (1) Ensure FMS TOLD media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load FMS TOLD data using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate FMS TOLD data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

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MAINTENANCE MANUAL (h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove FMS TOLD data media. (5) To continue full load with all media in sequence, go to Step 1.C11.(1). (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C11. Load Electronic Checklist Database (1) Ensure ECL database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE

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MAINTENANCE MANUAL (3) Load ECL database using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate ECL database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove ECL database media.

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MAINTENANCE MANUAL (5) To continue full load with all media in sequence, go to Step 1.C12.(1). (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C12. Load Communication Management Function / Airline Modifiable Information Database (1) Ensure CMF AMI database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load CMF AMI database using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate CMF AMI database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE

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MAINTENANCE MANUAL NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove CMF AMI database media. (5) To continue full load with all media in sequence, go to Step 1.C13.(1). (6) To select another media for full load, go to Step 1.C2.(2)(b). (7) If full load complete, go to Step 1.D.(1). C13. Load Loadable Diagnostic Information / Aircraft Configuration Monitoring Function Database (1) Ensure LDI / ACMF database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Wait a minimum of 5 minutes following power up or an Operational Software load before proceeding. (3) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

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MAINTENANCE MANUAL (c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (4) Load LDI / ACMF database using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate LDI / ACMF database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

(g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu.

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MAINTENANCE MANUAL 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (5) Remove LDI / ACMF database media. (6) To continue full load with all media in sequence, go to Step 1.C14.(1). (7) To select another media for full load, go to Step 1.C2.(2)(b). (8) If full load complete, go to Step 1.D.(1). C14. Load Programmable CAS Message Database (1) Ensure programmable CAS message database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 1.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load programmable CAS message database using CMC RT / DLS as follows: (a) Select FULL LOAD button on menu. (b) Browse to locate programmable CAS message database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 1.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Verify selected [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 1.C3.(3)(f).

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MAINTENANCE MANUAL (g) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(h) Select START LOAD button on menu. (i) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for full load to finish. For details, see Step 1.C3.(3)(i).

(j) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (k) If database load failure occurs, perform the following: NOTE:

The RETRY button should be used before reattempting a full or target load. For details, see Step 1.C3.(3)(k).

1 Record any module loading errors. 2 Select RETRY button on menu. 3 If RETRY fails, perform target load on modules that failed. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (4) Remove programmable CAS message database media. (5) To select another media for full load, go to Step 1.C2.(2)(b). (6) If full load complete, go to Step 1.D.(1). D. Follow On (1) On laptop PC, open Primus Epic Maintenance Utilities. (2) Select BITE Tool.exe to open FMS Fault File Retrieval Tool. (3) Select G650 under Aircraft List. (4) Select Setup Hosts File under Utilities Menu and click Run Utility. (5) Select Clear FMS BITE under Utilities Menu, enter Serial Number and Tail Number, then click Run Utility. (6) Pull the following circuit breakers: NOMENCLATURE

PANEL

LOCATION

MAU 3B PRI

Pilot

FLT INSTRUMENTS

MAU 3A PRI

Pilot

FLT INSTRUMENTS

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MAINTENANCE MANUAL NOMENCLATURE

PANEL

LOCATION

MAU 1B SEC

Pilot

FLT INSTRUMENTS

MAU 1B PRI

Copilot

FLT INSTRUMENTS

MAU 3A SEC

Copilot

FLT INSTRUMENTS

MAU 3B SEC

Copilot

FLT INSTRUMENTS

(7) Wait 30 seconds. (8) Close circuit breakers pulled in Step 1.D.(6). (9) After power up, Multi-function Control Display Units (MCDUs) will display the Nav Ident page. (10) Press FLT PLAN push-button on MCDU. (11) Enter any destination in flight plan destination field using scratchpad and selecting Line Select Key (LSK) (5R). (12) Select ACTIVATE. NOTE:

If Built-in Test Equipment (BITE) has not been cleared correctly, the FMS will reset. If the system activates the change without issues, BITE deletion is complete.

(13) Remove electrical power from aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (14) Wait a minimum of 2 minutes. NOTE:

During this period, do not perform any of the following actions: • Remove CMC backshell • Remove left emergency battery • Pull CMC SHUTDOWN circuit breaker

(15) Observe CMC Remote Terminal application window on maintenance laptop displays the following message: CMC CONNECTION FAILED CONNECTING TO 192.168.200.1 * * * (16) Apply electrical power to aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (17) On cockpit overhead panel in DISPLAY UNIT CONTROL section, select switches as follows: • • • •

DU DU DU DU

1 2 3 4

switch switch switch switch

NORM NORM NORM NORM

(18) Wait a minimum of 5 minutes before proceeding to allow CMC to complete power up. (19) Verify CMC Remote Terminal application window displays CMC MENU on maintenance laptop.

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MAINTENANCE MANUAL CMC Remote Terminal Exit Settings ACMF About CMC MAIN MENU

MAINTENANCE MESSAGES SYSTEM DIAGNOSTICS EXTENDED MAINTENANCE END OF FLIGHT PAGE

FAULT HISTORY DATABASE CURRENTLY

0% FULL

(20) On system monitor and test panel, select MAINT TEST switch to on. See Figure 202. NOTE:

The system monitor and test panel is located forward of the REER in the observers panel.

(21) Perform software load verification as follows: (a) Select CMC page on Display Unit (DU) No. 2 with Cursor Control Device (CCD) as follows: 1 Open 2 / 3 window selection drop-down menu. 2 Select CMC. 3 Verify CMC page displays on DU No. 2. (b) Select Configuration Monitor System (CMS) button on CMC page with CCD. (c) Verify system configuration page displays on DU No. 2. (d) If flashing CONFIRM button displays on System Configuration page, perform the following: NOTE:

The flashing CONFIRM button displays indicated Top Level System Part Number has changed.

1 Verify the following part numbers on system configuration page match software configuration data page in aircraft logbook: • Top Level System Part Number • Configuration Part Number 2 If configuration is not correct, contact Gulfstream Customer Support. 3 If configuration is correct, select CONFIRM button. (e) Record data displayed for CMS parameters as follows. 1 Select PAGE UP or PAGE DOWN buttons to select the appropriate configuration page. NOTE:

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Missing data or data shown in amber indicates a possible expired database or database out of configuration.

MAINTENANCE MANUAL CMS OPTIONS / SETTINGS PARAMETERS Parameter

Data

Aircraft Type Aircraft Serial Number Aircraft Transponder Code Aircraft Registration Number Top Level System Part Number Top Level System Mod Status Configuration Part Number

CMS MODULE / LRU PARAMETERS Parameter

Module

FMS 1 NAV

NIC / PROC(1) No. 2 No. 5 No. 6

FMS 2 NAV FMS 3 NAV FMS 1 AIRCRAFT FMS 2 AIRCRAFT FMS 3 AIRCRAFT FMS 1 CUSTOM FMS 2 CUSTOM FMS 3 CUSTOM ECL 1 CHECKLIST CMC LDI CMC 1 ACMF OEM CMF 1 AMI CMF 2 AMI (1)

(2) (3) (4) (5) (6)

Data

NIC / PROC(2) No. 2 No. 5 No. 6 NIC / PROC(3) No. 2 No. 5 No. 6 NIC / PROC(4) No. 3 CMC(5) NIC / PROC(6) No. 1 No. 4

For missing or amber data, see Load INDS Airspace, Communications, EGPWS and Navigational Data (Red Media). For missing or amber data, see Load AEDB Media. Not required databases. For missing or amber data, see Load ECL Database. For missing or amber data, see Central Maintenance Computer Module - Target Load. For missing or amber data, see Load CMF AMI Database.

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MAINTENANCE MANUAL 2 Verify recorded CMS check of part numbers match software configuration data page in aircraft logbook. 3 If module indicates error, perform target load. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. 4 If database date ranges are correct but data is shown in amber, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices (Network Interface Controller / Processor (NIC / PROC) module battery check). (f) Select DB CONFIG button on CMC page with CCD. (g) Verify database configuration page displays on DU No. 2. (h) Record data displayed and color on database configuration page as follows: NOTE:

Missing data or data shown in amber indicates a possible expired database or database out of configuration. A single database (green or amber) displayed under database name indicates that all Line Replaceable Modules (LRMs) have same load status. If database date ranges are correct but database displays in amber, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. A mixture of database (green and amber date ranges) under the same database header indicates a miscompare (mixture of successful / unsuccessful database loads). A miscompare displays LRM No. 1 in first row, LRM No. 2 in second row etc. Green and amber colors indicate the following: • • • •

Green file name / date range - Database successfully loaded Amber dashed line - LRM not functioning or not in normal mode Amber XXXNo FileXXX - Database not loaded on LRM Amber file name / date range - Database not current

1 Select PAGE UP or PAGE DOWN buttons to select appropriate database configuration page.

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MAINTENANCE MANUAL DATABASE CONFIGURATION Module / LRU

(3) (4)

(5)

Airport Comm

Red media(2)

Airport Text

Blue media(3)

En Route Comm

Blue media(3)

Obstacles

Blue media(3)

FMS

Red media(2)

Charts

Blue media(3)

Terrain

Red media(2)

Terrain Server

Green media(5)

NIC / PROC(1) No. 3

Electronic Checklist

ECL database

NIC / PROC(1) No. 1 No. 4

Programmable Message List

Programmable CAS message database

(4)

Data

Color

Red media(2)

Geopolitical

EGPWM(1) No. 1 No. 2

(2)

Source

Special Use Airspace

AGM(1) No. 1 No. 2 No. 3 No. 4

(1)

Database Name

Valid database text displays in green. Invalid database text displays in amber. The INDS airspace, communications, EGPWS and navigational data. The INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data. Env Mod DB (996-0114-XXX) is not validated on DB config page. Ensure Env Mod DB (996-0114-XXX) is loaded or a Terrain Fail (amber) message will display on CAS. The INDS terrain data.

2 Verify recorded database configuration data is valid for actual date and displays in green. 3 If data is missing or displays in amber, see appropriate procedure as follows: a For full load of source media, go to Step 1.C2.(1). b For target load of module / LRU, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (i) Perform DMU chart validation as follows: 1 Select Chart page on DU No. 2 with CCD as follows: a Open 2 / 3 window selection drop-down menu. b Select Charts. c Verify Chart page displays on DU No. 2. 2 Select Revision Info page on DU No. 2 with CCD as follows: a Select airport drop-down menu.

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MAINTENANCE MANUAL NOTE:

Revision Info page is selected from airport drop-down menu located at upper left of Chart page.

b Select Revision Info. c Verify Revision Info page displays on DU No. 2. 3 Verify Dataset Start Date (white) displays for current cycle, after validation. NOTE:

Dataset Start Date (amber) displays at top Revision Info page until data set is validated.

4 If Dataset Start Date (amber) displays, perform the following: a Verify INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media) are current. b Perform target load for advanced graphics module. See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (j) Verify FMS navigation data on MCDU No. 1 as follows: 1 Select NAV push-button. 2 Select NAV IDENT LSK (3L). 3 Verify date range below ACTIVE NDB (1R) is current and displays in green. 4 If date range below ACTIVE NDB (1R) displays in amber, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices (NIC / PROC modules No. 2 / No. 5 / No. 6). NOTE:

Missing data or date range in amber indicates a possible expired database or database out of configuration.

5 Repeat Step 1.D.(21)(j) on MCDU No. 2 and MCDU No. 3. (k) Select CMC page on DU No. 2 with CCD as follows: 1 Open 2 / 3 window selection drop-down menu. 2 Select CMC. 3 Verify CMC page displays on DU No. 2. 4 Select CMC button on CMC page. 5 Verify CMC MAIN MENU page displays on DU No. 2. (l) Verify MEMBER SYSTEM STATUS for each MAU and MRC module with CCD as follows: 1 Select EXTENDED MAINTENANCE button on CMC MAIN MENU. 2 Select MEMBER SYSTEM STATUS button on EXTENDED MAINTENANCE menu. 3 Use scroll knob to verify MEMBER SYSTEM STATUS for the following systems: • • • •

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22 AUTO FLIGHT 23 COMMUNICATIONS 31 INDICATING/RECORDING SYSTEMS 34 NAVIGATION

MAINTENANCE MANUAL 4 Verify each MAU and MRC module / LRU indicates OPERATIONAL status. 5 For any LRU NO COMM status, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. (m) Verify system configuration status for each APM with CCD as follows: 1 Select MAIN MENU button on CMC page. 2 Select SYSTEM DIAGNOSTICS. 3 Use scroll knob to select the following system: • 31 INDICATING/RECORDING SYSTEMS 4 Use scroll knob to select one of the following: • CONFIGURATION MONITOR FUNCTION 1 • CONFIGURATION MONITOR FUNCTION 2 5 Use scroll knob to select the following: • CONFIGURATION MONITOR TEST 6 Verify CONFIGURATION MONITOR SYSTEM STATUS displays the following: • • • •

APM APM APM APM

1 2 3 4

STATUS: STATUS: STATUS: STATUS:

VALID VALID VALID VALID

7 If AMP status INVALID for any module, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. 8 Verify SYSTEM CONFIGURATION STATUS displays the following message: • SYSTEM CONFIGURATION STATUS: PASS NOTE:

System configuration status will list any module / LRM the CMS has determined to have mismatched hardware or software.

a Target load any MAU modules / MRC network interface modules flagged as out of configuration (software mismatches). See Modular Avionics Unit / Modular Radio Cabinet - Software Loading (Target Load), 20-22-00, Maintenance Practices. b Replace module / LRU for hardware mismatches. (22) On maintenance laptop, perform the following: (a) Close all running computer applications. (b) Remove media. (c) Shut down maintenance laptop. (d) Turn power off. (23) Remove maintenance laptop connected in Step 1.C1.(1). (24) Remove all test equipment. (25) Wait a minimum of 90 seconds, then using CCD, select LAN SUMMARY page on CMC and verify LAN integrity.

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MAINTENANCE MANUAL (26) If aircraft was placed into ground mode, close LDG GEAR SVC panel door as follows: WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(a) Select WOW OVRD switch to NORM. (b) Close WOW OVRD switch guard. (c) Remove pin and move slide lock tab down from LG MODE switch. (d) Select LG MODE switch to NORM. (e) Verify LG MODE light goes off. (f) Inspect for presence of foreign objects. (g) Close LDG GEAR SVC panel door 122AR. See Figure 201. (27) Remove electrical power from aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (28) On system monitor and test panel, select MAINT TEST switch to off. See Figure 202. (29) Inspect for presence of foreign objects. (30) Record all maintenance actions in accordance with current governing authority.

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Table 201: Software Matrix

Network Interface(2)

N/A

1

No. 1

X

No. 2 No. 3

X

No. 4

X

X X

X

X

AIOP Lane A (AFCS)(2)

No. 1 or No. 2

5/6

9/10

AIOP Lane B (AFCS)(2)

No. 1 or No. 2 No. 1 - No. 3 N/A

7/8 9/10 11

13/14 7/8

7/8

No. 1 - No. 4 No. 1 - No. 2 No. 1 - No. 2

13/14

5/6 1 15/16

5/6, 13/14 15 9/10

No. 1 - No. 8

15, 16

2, 4

1,2,11,16

NIM

(1) (2) (3) (4) (5) (6)

Page 237 November 30/19

20-22-00

(7) (8)

X X 3, 12 11

X X

X X X

3, 12 4

LDI & ACMF

Prog CAS Messages

ECL

CMF AMI

TOLD

FMS Custom DB

AEDB X(4)

X

X

X

X

X(5)

X(3)

X X

X

X(4) X(5) X(5)

X(3) X(3)

X X X X X X

X X

X X

X

X

X X X

APM No. 1(7) APM No.2(7) APM No. 3(8) APM No. 4(8) No. 1

X X

X X

X X

X X

X X

X X

No. 2

X

X

No software load required. Dual slot module. The FMS Custom DB is not loaded with the DLS. The AEDB file is typically located with the APM settings media. The TOLD DB loaded to NIC / PROC modules No. 2, No. 5 and No. 6. The CMC is limited to one ACMF user defined report at a time. The APM No. 1 and No. 2 are located in backshell of NIC / PROC modules No. 1 and No. 4, respectively. The APM No. 3 and No. 4 are integrated into MRC No. 1 and No. 2 backplanes, respectively.

X

MAINTENANCE MANUAL

2 3, 12 4

System Configuration

Operational SW (EB) X

X

No. 1 - No. 6 No. 1 - No. 3

Control I/O with Video(2) Air Management Module(1)

X

X

Single Generic I/O Custom I/O

Dual Generic I/O(2) CMC(6) AGM(2) EGPWM

X

N/A

No. 5 No. 6 No. 1

Control I/O

Terrain Server

MAU No. 3

Threat/Env Mod

MAU No. 2

Options

(2)

MAU No. 1

MEDIA APM Settings

Power Supply(1) IEVM

Type - No.

INDS DATABASE

Charts

Name

LOCATION

INAV FMS

MODULE

MAINTENANCE MANUAL

122AR 122BR 122CR 132AR

TIL-001623

Lower Forward Midcabin Fuselage Access Doors Figure 201

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MAINTENANCE MANUAL

SEE DETAIL A

AIRCRAFT (6001 - 6049)

AIRCRAFT (6050 - 6999)

DETAIL A TIL-018813

System Monitor and Test Panel Figure 202

20-22-00 Page 239 November 30/19

MAINTENANCE MANUAL 2. Modular Avionics Unit / Modular Radio Cabinet — Software Loading (Target Load) A. General This procedure provides instructions for a target load the Master Operating System (MOS) software / databases. The MOS software / databases are target loaded to a module or Line Replaceable Unit (LRU) under the following conditions: • Modular Avionics Unit (MAU) modules removed and replaced • Modular Radio Cabinet (MRC) Network Interface Module (NIM) removed and replaced • Full load errors which may be corrected through target load Prior training in performing a software load procedure on an aircraft is required. Software / databases are typically available on the following media: • Universal Serial Bus (USB) flash drive or memory stick • Compact Disks (CD) Current Integrated Navigation Data Services (INDS) databases are available and may be downloaded from the INDS website. This system contains ESD sensitive components. Ensure all ESD safety precautions and practices are followed while performing maintenance. See Electrostatic Discharge - Standard Practices, 20-23-00, Maintenance Practices. B. Preparation SPECIAL TOOLS AND TEST EQUIPMENT Ethernet cable ..................................................................................................................... Standard Maintenance laptop ............................................................................................................. Standard (1) Reference(s) • Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices • Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices • Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices • Electrostatic Discharge - Standard Practices, 20-23-00, Maintenance Practices • Honeywell Data Loading Procedures for the Gulfstream PlaneView Primus Epic System (2) Aircraft Preparation (a) Prepare aircraft for safe ground maintenance. See Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices. (b) Ensure the following Circuit Breakers (CB) are closed: NOMENCLATURE

PANEL

LOCATION

MAU 3B PRI

Pilot

FLT INSTRUMENTS

MAU 3A PRI

Pilot

FLT INSTRUMENTS

MAU 2B SEC

Pilot

FLT INSTRUMENTS

MAU 2A SEC

Pilot

FLT INSTRUMENTS

MAU 1B SEC

Pilot

FLT INSTRUMENTS

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MAINTENANCE MANUAL NOMENCLATURE

PANEL

LOCATION

MAU 1A PRI

Pilot

FLT INSTRUMENTS

MRC 1 NIM

Pilot

COMM/NAV

MAU 1A SEC

Copilot

FLT INSTRUMENTS

MAU 1B PRI

Copilot

FLT INSTRUMENTS

MAU 2A PRI

Copilot

FLT INSTRUMENTS

MAU 2B PRI

Copilot

FLT INSTRUMENTS

MAU 3A SEC

Copilot

FLT INSTRUMENTS

MAU 3B SEC

Copilot

FLT INSTRUMENTS

DMU

Copilot

COMM/NAV

MRC 2 NIM

Copilot

COMM/NAV

(c) Ensure the following aircraft conditions: • Airspeed less than 50 knots • Throttles at idle (d) Ensure aircraft is in ground mode. If required, place aircraft in ground mode as follows: 1 Open LDG GEAR SVC panel door 122AR. See Figure 201. NOTE:

The WOW OVRD and LG MODE switches are located on the LDG GEAR SVC panel.

2 Select LG MODE switch to MAINT. 3 Move switch slide lock up. NOTE:

Slide lock holds LG MODE switch in MAINT mode.

4 Insert maintenance mode lockout pin. 5 On LDG GEAR SVC panel, verify LG MODE light comes on. 6 Remove safety cable securing WOW OVRD switch cover. WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

7 Select WOW OVRD switch to GND.

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MAINTENANCE MANUAL WARNING:

APPLYING ELECTRICAL POWER TO AIRCRAFT MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE APPLYING ELECTRICAL POWER MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(e) Apply electrical power to aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (f) Ensure all Primus Epic equipment is powered for a minimum of 15 minutes prior to beginning a software load. C. Procedure CAUTION: NOTE:

FAILURE TO OBSERVE ELECTROSTATIC DISCHARGE PROCEDURES MAY CAUSE DAMAGE TO SYSTEM COMPONENTS.

The following procedures are provided: • Procedure 2.C1. - Maintenance Laptop Setup • Procedure 2.C2. - Target Load Procedures

C1. Maintenance Laptop Setup NOTE:

Software / database loading is accomplished using a maintenance laptop with the Central Maintenance Computer (CMC) Remote Terminal (RT) application and Data Loading System (DLS) tool.

(1) Connect maintenance laptop as follows: NOTE:

The Data LAN Management Unit (DLMU) contains a RJ45 jack (Ethernet), USB port and two Secure Digital (SD) memory card slots

(a) Connect Ethernet cable to maintenance laptop. (b) Open DLMU access door. (c) Connect Ethernet cable to DLMU (opposite end connected to maintenance laptop). (2) Perform maintenance laptop preliminary procedures as follows: (a) Connect maintenance laptop to aircraft 60 Hz power outlet. NOTE:

Aircraft 60 Hz power is used to provide a stable power source for software loading. A sufficiently charged maintenance laptop battery may also provide a suitable stable power source for software loading.

(b) Turn maintenance laptop power on. (c) If maintenance laptop kiosk is available, go to Step 2.C1.(3). NOTE:

The kiosk will change the laptop system settings for communication with CMC terminal and DLS.

(d) If laptop kiosk application is unavailable, comply with the following: 1 Disable the following programs or applications which may affect software / database loading as necessary: • Firewall software • Zone alarm software • Norton software

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MAINTENANCE MANUAL • Active screen saver • Power save options 2 Ensure maintenance laptop Internet Protocol (IP) address is configured as follows: NOTE:

Help on how to www.microsoft.com.

configure

an

IP

address

is

available

at

a Access control panel settings. b Open network connections. c Select local area connection. d Open properties for local area connection. e Select Transmission Control Protocol / Internet Protocol (TCP / IP) connection. f Open properties for TCP / IP connection. g For maintenance laptop with Windows 7, set IP address as follows: • IP address: 192.168.192.1 h For maintenance laptop with Windows XP, set IP address as follows: • IP address: 192.168.192.7 i Set subnet mask to the following: • 255.255.255.0 (3) Verify aircraft LAN is operational and all MAU / MRC modules are communicating as follows: (a) If maintenance laptop kiosk is available, perform the following: 1 Locate Other Utilities menu on maintenance laptop kiosk. 2 Select CyberKit link in Other Utilities menu. 3 Go to Step 2.C1.(3)(c). (b) If laptop kiosk application is unavailable, double click CyberKit Ping shortcut or perform the following: NOTE:

The CyberKit Ping shortcut should be located on maintenance laptop desktop.

1 Click on maintenance laptop START menu. 2 Select programs. 3 Select CyberKit. (c) Ensure CyberKit is properly configured, see Gulfstream Aerospace Corporation (GAC) maintenance applications disk to configure CyberKit for aircraft. NOTE:

A valid module list file of IP addresses resolved to names for the aircraft configuration (modules that directly transmit / receive on the LAN) is necessary to run CyberKit.

(d) Verify CyberKit application window opens and displays an IP address for each MAU and MRC module / LRU as follows:

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MAINTENANCE MANUAL 1 Each MAU and MRC module / LRU listed in Software Matrix Table 201 is operational. 2 Percent loss column for any module does not display more than a 5% loss. NOTE:

Modules experiencing more than a 5% loss typically produce software / database load errors.

(4) Start CMC Remote Terminal application as follows: (a) If maintenance laptop kiosk is available, perform the following: 1 Select CMC Terminal/DLS link in Aircraft System Tools menu. NOTE:

This kiosk link will set the laptop IP address to 192.168.192.1 and disable the firewall, anti-virus and wireless card.

2 Select OK. 3 Go to Step 2.C1.(4)(c). (b) If laptop kiosk application is unavailable, double click CMC.RT.exe shortcut to start CMC Remote Terminal application or perform the following: NOTE:

The CMC.RT.exe shortcut should be located on maintenance laptop desktop.

1 Click on maintenance laptop START menu. 2 Select CMC Remote Terminal. 3 Select CMC RT / DLS tool. (c) Verify CMC Remote Terminal application window opens and connects to aircraft LAN as follows: CMC Remote Terminal Exit Settings ACMF About CMC MAIN MENU

MAINTENANCE MESSAGES SYSTEM DIAGNOSTICS EXTENDED MAINTENANCE END OF FLIGHT PAGE

FAULT HISTORY DATABASE CURRENTLY

0% FULL

1 If CMC Remote Terminal application window displays CMC MAIN MENU, go to Step 2.C1.(5). 2 If CMC Remote Terminal application can not communicate with CMC, perform the following: NOTE:

Communication with the CMC is not possible if the CMC software has not been loaded or the CMC module has failed.

a If CMC software has not been loaded, go to Step 2.C1.(6)(b).

20-22-00 Page 244 November 30/19

MAINTENANCE MANUAL b If CMC software load status unknown, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. (5) Ensure appropriate CMC RT / DLS version is installed on maintenance laptop as follows: (a) Select About on menu bar of CMC Remote Terminal application window. NOTE:

The pop-up window About CMC Remote Terminal displays CMC RT / DLS versions.

(b) Verify appropriate version of CMC RT / DLS from GAC maintenance applications disk are installed on maintenance laptop as follows:

(1) (2)

ASC

CMC RT

DLS

Aircraft having ASC 902

26.1(1)

8.2.0(2)

The CMC RT 26.1 / DLS 8.2.0 software are Windows 7 compliant. The DLS main menu supports a refresh allowing the user to change media and refresh the display. When browsing to locate [DR-PN]: file, duplicate part numbers will now contain an (XR) to indicate the part number to be selected.

(c) If CMC RT / DLS are incorrect version, install appropriate version of the CMC RT / DLS from GAC maintenance applications disk. NOTE:

Prior to installation of any CMC RT / DLS tool, it is recommended that all previous versions be removed by utilizing the add / remove programs function provided in the Windows control panel.

(6) Start DLS tool as follows: (a) Select EXTENDED MAINTENANCE button on CMC Remote Terminal application window menu. NOTE:

The CMC Remote Terminal menu provides access to the DLS tool that controls software loading. The CMC Remote Terminal application window is divided with the display area on the left and menu on the right. The maintenance laptop cursor control is used to select CMC Remote Terminal menu buttons and the cursor must be inside the application window for functions to be active.

(b) If DATA LOADER button does not display in CMC Remote Terminal application window, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. (c) Select DATA LOADER button. C2. Target Load Procedures CAUTION:

FAILURE TO OBSERVE ELECTROSTATIC DISCHARGE PROCEDURES MAY CAUSE DAMAGE TO SYSTEM COMPONENTS.

(1) Perform target load of software / database media as follows: (a) Identify target module / LRU for target load. (b) See Software Matrix Table 201 to identify all media required for module / LRU. (c) Verify software / database media is correct and the latest version. Refer to software

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MAINTENANCE MANUAL configuration data page in aircraft logbook. NOTE:

For assistance if unsure, contact Gulfstream Customer Support.

(d) See applicable procedure for target load of module / LRU as follows: • Procedure 2.C3. - Network Interface Controller / Processor Module (No. 1 / No. 4) - Target Load • Procedure 2.C4. - Network Interface Controller / Processor Module (No. 2 / No. 5 / No. 6) - Target Load • Procedure 2.C5. - Network Interface Controller / Processor Module (No. 3) Target Load • Procedure 2.C6. - Control Input / Output Module - Target Load • Procedure 2.C7. - Single Generic Input / Output Module - Target Load • Procedure 2.C8. - Custom Input / Output Module - Target Load • Procedure 2.C9. - Autoflight Input Output Processor Module - Target Load • Procedure 2.C10. - Dual Generic Input / Output Module - Target Load • Procedure 2.C11. - Central Maintenance Computer Module - Target Load • Procedure 2.C12. - Advanced Graphics Module - Target Load • Procedure 2.C13. - Enhanced Ground Proximity Warning Module - Target Load • Procedure 2.C14. - Aircraft Personality Module - Target Load • Procedure 2.C15. - Network Interface Module - Target Load • Procedure 2.C16. - Integrated Engine Vibration Monitor - Target Load C3. Network Interface Controller / Processor Module (No. 1 / No. 4) - Target Load NOTE:

The six Network Interface Controller / Processor (NIC / PROC) modules are located as follows. • NIC / PROC module No. 1 / No. 2 - MAU No. 1 • NIC / PROC module No. 3 / No. 4 - MAU No. 2 • NIC / PROC module No. 5 / No. 6 - MAU No. 3

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media (USB or CD) must be available to the CMC RT / DLS during the preloading scan. Unless otherwise specified, insert media in the maintenance laptop (USB port or CD-ROM drive). Media contents or files may be copied to a directory or folder on the maintenance laptop.

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load NIC / PROC module using CMC RT / DLS as follows:

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MAINTENANCE MANUAL (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

The CMC RT / DLS display is used to browse available drives, directories and folders on the maintenance laptop and any connected device to locate, select and highlight [DR-PN]: (loadable software / database) files as follows:

• Data Management Unit (DMU) - Browse DMU DRIVES / DMU-0: / CD-ROM • CD in maintenance laptop - Browse REMOTE TERMINAL / CD-ROM D: • USB in maintenance laptop - Browse OTHER DATA SOURCES / AVAILABLE DRIVES / FLOPPY DRIVE E: (DLS tool displays USB device as FLOPPY DRIVE) • Media copied or saved on maintenance laptop - Browse OTHER DATA SOURCES / AVAILABLE DRIVES / HARD DRIVE C: The maintenance laptop up / down arrows may also be used to locate and highlight files or targets. When maintenance laptop up / down arrows are used, the Enter button selects highlighted software or targets for software loading. (c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 1 NIC / PROC 4 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of Line Replaceable Module (LRM) displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The DLS tool configuration check includes an IP address and hardware part number loading compatibility check. The configuration check may take several minutes.

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu.

20-22-00 Page 247 November 30/19

MAINTENANCE MANUAL (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. The DLS tool display indicates a percentage complete during the data loading sequence. Load times and percent complete indication may change during load process. The DLS tool may encounter an error, retry an operation or identify additional files to load. The working progress bar (blue) may also display inside or behind the DLS window on the maintenance laptop indicating a DLS process is running. Cockpit display units may indicate the following once a software load has been initiated: • X (red) Cockpit display controllers may indicate the following once a software load has been initiated: • No input from MAU At times the DLS tool may appear to be frozen or locked up when it is not. Estimated load time may have counted down to 0 and load process may not be complete. A cockpit display with a X (red) may also indicate process may not be complete. Avoid canceling the load process and allow sufficient time for the full load process to complete. When it becomes necessary to cancel the load process, wait until the load time estimate has counted to zero.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) Ensure CMF AMI database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE

20-22-00 Page 248 November 30/19

MAINTENANCE MANUAL (7) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate CMF AMI database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 1 NIC / PROC 4 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (8) Remove CMF AMI database media.

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MAINTENANCE MANUAL (9) Ensure programmable CAS message database media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(10) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (11) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate programmable CAS message database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 1 NIC / PROC 4 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE

20-22-00 Page 250 November 30/19

MAINTENANCE MANUAL

NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (12) Remove programmable CAS message database media. (13) To select another module / LRU for target load, go to Step 2.C2.(1). (14) If target load complete, go to Step 2.D.(1). C4. Network Interface Controller / Processor Module (No. 2 / No. 5 / No. 6) - Target Load NOTE:

The six NIC / PROC modules are located as follows. • NIC / PROC module No. 1 / No. 2 - MAU No. 1 • NIC / PROC module No. 3 / No. 4 - MAU No. 2 • NIC / PROC module No. 5 / No. 6 - MAU No. 3

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file.

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MAINTENANCE MANUAL (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 2 NIC / PROC 5 NIC / PROC 6 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) Ensure Aerodynamics-Engine Database (AEDB) media (typically located with APM settings and rigging media) is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu.

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MAINTENANCE MANUAL (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (7) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate AEDB [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: • GWWXXXXXXX (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 2 NIC / PROC 5 NIC / PROC 6 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu.

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MAINTENANCE MANUAL (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (8) Remove AEDB media. (9) Ensure INDS airspace, communications, EGPWS and navigational data (red media) are available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(10) Review epic load instructions document for any database changes or limitations. NOTE:

Epic load Instructions.htm is included with INDS airspace, communications, EGPWS and navigational data.

(11) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (12) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS airspace, communications, EGPWS and navigational data [DRPN]: files. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: • [DR-PN]: World 3-3XX (16M FMS) (d) Ensure [DR-PN]: file displays in green. NOTE:

File name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows:

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MAINTENANCE MANUAL NIC / PROC 2 NIC / PROC 5 NIC / PROC 6 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (13) Remove INDS airspace, communications, EGPWS and navigational data (red media). (14) Ensure FMS Takeoff and Landing Data (TOLD) media is available to CMC RT / DLS. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(15) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays:

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MAINTENANCE MANUAL PRE-LOADING DMU / CDROM DRIVES - DONE (16) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate FMS TOLD data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 2 NIC / PROC 5 NIC / PROC 6 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays:

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MAINTENANCE MANUAL PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (17) Remove FMS TOLD media. (18) To select another module / LRU for target load, go to Step 2.C2.(1). (19) If target load complete, go to Step 2.D.(1). C5. Network Interface Controller / Processor Module (No. 3) - Target Load NOTE:

The six NIC / PROC modules are located as follows. • NIC / PROC module No. 1 / No. 2 - MAU No. 1 • NIC / PROC module No. 3 / No. 4 - MAU No. 2 • NIC / PROC module No. 5 / No. 6 - MAU No. 3

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 3 (g) Ensure selected NIC / PROC module displays in green.

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MAINTENANCE MANUAL NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) Ensure Electronic Checklist (ECL) database media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (7) Load NIC / PROC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu.

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MAINTENANCE MANUAL (b) Browse to locate ECL database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC module from LRM TO LOAD display as follows: NIC / PROC 3 (g) Ensure selected NIC / PROC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (8) Remove ECL database media. (9) To select another module / LRU for target load, go to Step 2.C2.(1). (10) If target load complete, go to Step 2.D.(1).

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MAINTENANCE MANUAL C6. Control Input / Output Module - Target Load NOTE:

The control Input / Output (I/O) modules are located as follows: • Control I/O No. 1 - MAU No. 1 • Control I/O No. 2 with video No. 2 - MAU No. 2 • Control I/O No. 3 with video No. 1 - MAU No. 3

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load control I/O module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate control I/O module from LRM TO LOAD display as follows: Control I/O 1 Control I/O 2 with video Control I/O 3 with video (g) Ensure selected control I/O module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays:

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MAINTENANCE MANUAL CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C7. Single Generic Input / Output Module - Target Load NOTE:

The six Single Generic I/O (SGIO) modules are located as follows. • SGIO module No. 1 / No. 2 - MAU No. 1 • SGIO module No. 3 / No. 4 - MAU No. 2 • SGIO module No. 5 / No. 6 - MAU No. 3

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE

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MAINTENANCE MANUAL

(3) Load SGIO module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight SGIO module from LRM TO LOAD display as follows: SGIO SGIO SGIO SGIO SGIO SGIO

1 2 3 4 5 6

(g) Ensure selected SGIO module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays:

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MAINTENANCE MANUAL PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C8. Custom Input / Output Module - Target Load NOTE:

The custom I/O module No. 1, No. 2 and No. 3 are located in MAU No. 1, No. 2 and No. 3, respectively.

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. See Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load custom I/O module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight custom I/O module from LRM TO LOAD display as follows: Custom I/O 1 Custom I/O 2 Custom I/O 3 (g) Ensure selected custom I/O module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

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MAINTENANCE MANUAL (h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C9. Autoflight Input Output Processor Module - Target Load NOTE:

The Autoflight Input Output Processor (AIOP) modules are located as follows: • • • •

AIOP AIOP AIOP AIOP

No. No. No. No.

1 1 2 2

(lane A) - MAU No. 1 (lane B) - MAU No. 1 (lane A) - MAU No. 2 (lane B) - MAU No. 2

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. See Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

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The preloading scan may take a few seconds.

MAINTENANCE MANUAL (c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load AIOP module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate AIOP module for lane A or B from LRM TO LOAD display as follows: AFCS AFCS AFCS AFCS

1 2 1 2

-A -A -B -B

(g) Ensure selected AIOP module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

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MAINTENANCE MANUAL (m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C10. Dual Generic I/O Module - Target Load NOTE:

The Dual Generic I/O (DGIO) module No. 1 and No. 2 are located in MAU No. 1 and No. 2, respectively.

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load DGIO module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate DGIO module from LRM TO LOAD display as follows: DGIO 1 DGIO 2 DGIO 3 (g) Ensure selected DGIO module module displays in green.

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MAINTENANCE MANUAL NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C11. Central Maintenance Computer Module - Target Load NOTE:

The CMC is located in MAU No. 1.

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays:

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MAINTENANCE MANUAL PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load CMC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight CMC module from LRM TO LOAD display as follows: CMC (g) Ensure CMC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * *

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MAINTENANCE MANUAL (4) Remove Operational Software media. (5) Ensure Loadable Diagnostic Information (LDI) / Aircraft Configuration Monitoring Function (ACMF) database media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Wait a minimum of 5 minutes following power up or an Operational Software load before proceeding. (7) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (8) Load CMC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate LDI / ACMF database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. NOTE:

Typically, there is only an LDI / ACMF file to load. An update ACMF may be available separate from the LDI / ACMF release. If there is a separate update ACMF [DR-PN]: file, repeat Step 2.C11.(7) thru Step 2.C11.(8)(m).

(d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight CMC module from LRM TO LOAD display as follows: CMC (g) Ensure CMC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays:

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MAINTENANCE MANUAL CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (9) If separate ACMF [DR-PN]: file is available, repeat Step 2.C11.(7) thru Step 2.C11.(8)(m). NOTE:

An update ACMF may be available separate from the LDI / ACMF release.

(10) Remove LDI / ACMF database media. (11) Ensure INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media) are available to CMC RT / DLS as follows: NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(12) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (13) Load CMC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS electronic terminal charts, geopolitical boundaries, airport

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MAINTENANCE MANUAL information and obstacle data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight CMC module from LRM TO LOAD display as follows: CMC (g) Ensure CMC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (14) Remove INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media). (15) Ensure programmable CAS message database media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

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MAINTENANCE MANUAL (16) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (17) Load CMC module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate programmable CAS message database [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight CMC module from LRM TO LOAD display as follows: CMC (g) Ensure CMC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays:

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MAINTENANCE MANUAL PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (18) Remove programmable CAS message database media. (19) To select another module / LRU for target load, go to Step 2.C2.(1). (20) If target load complete, go to Step 2.D.(1). C12. Advanced Graphics Module - Target Load NOTE:

The Advanced Graphics Modules (AGMs) are located as follows: • • • •

AGM AGM AGM AGM

No. No. No. No.

1 2 3 4

-

MAU MAU MAU MAU

No. No. No. No.

3 3 2 1

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load AGM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu.

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MAINTENANCE MANUAL (f) Select and highlight AGM from LRM TO LOAD display as follows: AGM AGM AGM AGM

1 2 3 4

(g) Ensure AGM module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) Ensure INDS airspace, communications, EGPWS and navigational data (red media) are available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu.

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MAINTENANCE MANUAL (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (7) Load AGM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS airspace, communications, EGPWS and navigational data [DRPN]: files. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate AGM from LRM TO LOAD display as follows: AGM AGM AGM AGM

1 2 3 4

(g) Ensure selected AGM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu.

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MAINTENANCE MANUAL (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (n) Remove INDS airspace, communications, EGPWS and navigational data (red media). (8) Ensure INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media) are available to CMC RT / DLS as follows: NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(9) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (10) Load AGM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight AGM from LRM TO LOAD display as follows:

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MAINTENANCE MANUAL AGM AGM AGM AGM

1 2 3 4

(g) Ensure selected AGM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 15 MINUTES FOR AN ADVANCED GRAPHICS MODULE.

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (11) Remove INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media). (12) To select another module / LRU for target load, go to Step 2.C2.(1). (13) If target load complete, go to Step 2.D.(1). C13. Enhanced Ground Proximity Warning Module - Target Load NOTE:

The EGPWM No. 1 and No. 2 are located in MAU No. 3 and No. 2, respectively.

(1) Ensure Operational Software media is available to CMC RT / DLS tool.

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MAINTENANCE MANUAL NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load EGPWM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate EGPWM from LRM TO LOAD display as follows: EGPWM 1 EGPWM 2 (g) Ensure selected EGPWM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

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Expected load times vary based on software being loaded.

MAINTENANCE MANUAL (k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) Ensure INDS airspace, communications, EGPWS and navigational data (red media) are available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(6) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (7) Load INDS EGPWM module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS airspace, communications, EGPWS and navigational data [DRPN]: files. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: • [DR-PN]: 966-0145-XXX (EGPWM THREAT) (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu.

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MAINTENANCE MANUAL (f) Select and highlight appropriate EGPWM from LRM TO LOAD display as follows: EGPWM 1 EGPWM 2 (g) Ensure selected EGPWM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (8) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays:

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MAINTENANCE MANUAL PRE-LOADING DMU / CDROM DRIVES - DONE (9) Load INDS EGPWM module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS airspace, communications, EGPWS and navigational data [DRPN]: files. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: • [DR-PN]: 966-0114-XXX (EGPWM ENV MOD) (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate EGPWM from LRM TO LOAD display as follows: EGPWM 1 EGPWM 2 (g) Ensure selected EGPWM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

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MAINTENANCE MANUAL CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (10) Remove INDS airspace, communications, EGPWS and navigational data (red media). (11) Ensure INDS terrain data (green media) is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(12) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (13) Load INDS EGPWM module using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate INDS terrain data [DR-PN]: files. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file: • 966-0146-XXX (TERRAIN SERVER DB) (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate EGPWM from LRM TO LOAD display as follows: EGPWM 1 EGPWM 2 (g) Ensure selected EGPWM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu.

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MAINTENANCE MANUAL (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

CAUTION:

AVOID CONFIGURATION ERRORS WHEN IT BECOMES NECESSARY TO CANCEL LOAD PROCESS. WAIT UNTIL LOAD TIME ESTIMATE HAS COUNTED TO ZERO AND AN ADDITIONAL 45 MINUTES FOR AN ENHANCED GROUND PROXIMITY WARNING MODULE.

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (14) Remove INDS terrain data (green media). (15) To select another module / LRU for target load, go to Step 2.C2.(1). (16) If target load complete, go to Step 2.D.(1). C14. Aircraft Personality Module - Target Load NOTE:

The Aircraft Personality Modules (APMs) are located as follows: • • • •

APM APM APM APM

No. No. No. No.

1 2 3 4

-

Backshell of NIC / PROC No. 1 Backshell of NIC / PROC No. 4 MRC No. 1 MRC No. 2

After replacing an APM module, appropriate NIC / PROC module or NIM MRC, load with Operational Software before loading APM module with settings, rigging and options data. (1) Ensure a backup of Enhanced Vision System (EVS) alignment parameters has been performed as follows: NOTE:

Prior to target loading an APM, a backup of rigging data ensures (EVS alignment parameters) have been saved on maintenance laptop.

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MAINTENANCE MANUAL The backup of rigging data is performed using DLS and needs to be performed from the maintenance laptop. (a) Access maintenance laptop shortcuts. NOTE:

The maintenance laptop should have a shortcut to backup rigging data. The shortcut copies EVS rigging data from one of the APMs to a backup file on maintenance laptop.

(b) Select Rigging Backup shortcut to save rigging data. (c) Access CMC RT / DLS on maintenance laptop. (2) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(3) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (4) Load Operational Software to NIC / PROC or NIM MRC using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC or NIM MRC from LRM TO LOAD display as follows: NIC / PROC 1 (for APM No. 1) NIC / PROC 4 (for APM No. 2) NIM MRC1 (for APM No. 3) NIM MRC2 (for APM No. 4) (g) Ensure selected NIC / PROC or NIM MRC displays in green. NOTE:

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Name of LRM displays in green on bottom edge of display.

MAINTENANCE MANUAL (h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (5) Remove Operational Software media. (6) Ensure APM settings and rigging media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(7) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU or DATA LOADER button from menu. NOTE:

The DLS MENU button returns to the DLS top menu. The DATA LOADER button provides DLS access from EXTENDED MAINTENANCE menu.

(b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (8) Load APM settings and rigging data using CMC RT / DLS as follows:

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MAINTENANCE MANUAL (a) Select TARGET LOAD button on menu. (b) Browse to locate APM settings and rigging [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIC / PROC or NIM MRC from LRM TO LOAD display as follows: NIC / PROC 1 (for APM No. 1) NIC / PROC 4 (for APM No. 2) NIM MRC1 (for APM No. 3) NIM MRC2 (for APM No. 4) (g) Ensure selected NIC / PROC or NIM MRC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * *

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MAINTENANCE MANUAL (9) Remove APM settings and rigging media. (10) If APM options media has a security code, record security code. • APM options Security Code: ____________ NOTE:

Security code is located on the front of the CD media.

(11) Ensure APM options media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(12) Access DLS INSTALLATION FUNCTION as follows: (a) Select DLS MENU button on menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (13) Load APM options data using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse drives / directories to locate Epic folder. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) For APM options media which includes a security enabled feature, perform the following: 1 Read Licensing agreement. 2 Select I Accept to continue. NOTE:

Selecting I Decline will return to DLS menu.

3 Select Enter Passcode. 4 Select Authorization Code field. 5 Enter code using maintenance laptop keyboard. (g) Observe CMC RT / DLS tool displays LRM TO LOAD. (h) Select and highlight appropriate NIC / PROC or NIM MRC from LRM TO LOAD display as follows:

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MAINTENANCE MANUAL NIC / PROC 1 (for APM No. 1) NIC / PROC 4 (for APM No. 2) NIM MRC1 (for APM No. 3) NIM MRC2 (for APM No. 4) (i) Ensure selected NIC / PROC or NIM MRC module displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(j) Select NEXT button on menu. (k) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(l) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(m) Select START LOAD button on menu. (n) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(o) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (14) Remove APM options media. (15) Restore rigging data as follows: NOTE:

A rigging restore is performed to load rigging file alignment parameters. The rigging restore is not performed using DLS and needs to be performed from the maintenance laptop.

(a) Access maintenance laptop shortcuts. NOTE:

The maintenance laptop should have a shortcut for rigging restore. The shortcut loads EVS rigging data from backup file on maintenance laptop to APMs No. 1 - No. 4.

(b) If Rigging Restore shortcut is not available, load rigging data as follows: 1 Access APM settings and rigging media on maintenance laptop.

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MAINTENANCE MANUAL CAUTION:

RUNNING THIS BATCH FILE WILL REQUIRE ENHANCED VISION SYSTEM ALIGNMENT PROCEDURE TO BE PERFORMED.

2 Select Rigging Init file. NOTE:

The Rigging Init batch file is used to reset APM rigging data in APMs No. 1 - No. 4. Running this Batch File without a rigging backup file will require an EVS alignment procedure to adjust EVS raster patch and save EVS alignment parameters.

(c) Select Rigging Restore shortcut to restore rigging data. (16) To select another module / LRU for target load, go to Step 2.C2.(1). (17) If target load complete, go to Step 2.D.(1). C15. Network Interface Module - Target Load NOTE:

The NIM No. 1 and No. 2 are located in MRC No. 1 and No. 2, respectively.

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays: PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load NIM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight appropriate NIM MRC from LRM TO LOAD display as follows:

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MAINTENANCE MANUAL NIM MRC 1 NIM MRC 2 (g) Ensure selected NIM MRC displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays: PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). C16. Integrated Engine Vibration Monitor - Target Load NOTE:

The Integrated Engine Vibration Monitor (IEVM) is located in MAU No. 1.

(1) Ensure Operational Software media is available to CMC RT / DLS tool. NOTE:

Media must be available during the preloading scan. For details, see Step 2.C3.(1).

(2) Access DLS INSTALLATION FUNCTION as follows: (a) Select DATA LOADER button on EXTENDED MAINTENANCE menu. (b) Observe the following message displays:

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MAINTENANCE MANUAL PRE-LOADING DMU / CDROM DRIVES – NOTE:

The preloading scan may take a few seconds.

(c) Verify the following message displays: PRE-LOADING DMU / CDROM DRIVES - DONE (3) Load IEVM using CMC RT / DLS as follows: (a) Select TARGET LOAD button on menu. (b) Browse to locate Operational Software [DR-PN]: file. NOTE:

Browse available drives, directories and folders. For details, see Step 2.C3.(3)(b).

(c) Select and highlight [DR-PN]: file. (d) Ensure [DR-PN]: file displays in green. NOTE:

The file name displays in green on bottom edge of display.

(e) Select SELECT FILE button on menu. (f) Select and highlight IEVM from LRM TO LOAD display. (g) Ensure IEVM displays in green. NOTE:

Name of LRM displays in green on bottom edge of display.

(h) Select NEXT button on menu. (i) Observe the following message displays: CONFIGURATION CHECK IN PROGRESS . . . % COMPLETE XX NOTE:

The configuration check may take several minutes. For details, see Step 2.C3.(3)(i).

(j) Verify the following message and expected load times display: CONFIGURATION CHECK COMPLETE NOTE:

Expected load times vary based on software being loaded.

(k) Select START LOAD button on menu. (l) Observe the following message displays: PERCENTAGE COMPLETE: XX % NOTE:

Allow sufficient time for target load to finish. For details, see Step 2.C3.(3)(l).

(m) Verify the following message displays:

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MAINTENANCE MANUAL PERCENTAGE COMPLETE: 100% * * * LOADING SEQUENCE COMPLETE * * * (4) Remove Operational Software media. (5) To select another module / LRU for target load, go to Step 2.C2.(1). (6) If target load complete, go to Step 2.D.(1). D. Follow On (1) On laptop PC, open Primus Epic Maintenance Utilities. (2) Select BITE Tool.exe to open FMS Fault File Retrieval Tool. (3) Select G650 under Aircraft List. (4) Select Setup Hosts File under Utilities Menu and click Run Utility. (5) Select Clear FMS Bite under Utilities Menu, enter Serial Number and Tail Number, then click Run Utility. (6) Pull the following circuit breakers: NOMENCLATURE

PANEL

LOCATION

MAU 3B PRI

Pilot

FLT INSTRUMENTS

MAU 3A PRI

Pilot

FLT INSTRUMENTS

MAU 1B SEC

Pilot

FLT INSTRUMENTS

MAU 1B PRI

Copilot

FLT INSTRUMENTS

MAU 3A SEC

Copilot

FLT INSTRUMENTS

MAU 3B SEC

Copilot

FLT INSTRUMENTS

(7) Wait 30 seconds. (8) Close circuit breakers pulled in Step 2.D.(6). (9) After power up, MCDUs will display Nav Ident page. (10) Press FLT PLAN push-button on MCDU. (11) Enter any destination in the flight plan destination field using scratchpad and selecting Line Select Key (LSK) (5R). (12) Select ACTIVATE. NOTE:

If Built-in Test Equipment (BITE) has not been cleared correctly, the FMS will reset. If the system activates the change without issues, BITE deletion is complete.

(13) Remove electrical power from aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (14) Wait a minimum of 2 minutes. NOTE:

During this period, do not perform any of the following actions: • Remove CMC backshell

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MAINTENANCE MANUAL • Remove left emergency battery • Pull CMC SHUTDOWN circuit breaker (15) Observe CMC Remote Terminal application window on maintenance laptop displays the following message: CMC CONNECTION FAILED CONNECTING TO 192.168.200.1 * * * (16) Apply electrical power to aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (17) On cockpit overhead panel in DISPLAY UNIT CONTROL section, select switches as follows: • • • •

DU DU DU DU

1 2 3 4

switch switch switch switch

NORM NORM NORM NORM

(18) Wait a minimum of 5 minutes before proceeding to allow CMC to complete power up. (19) Verify CMC Remote Terminal application window displays CMC MENU on maintenance laptop. CMC Remote Terminal Exit Settings ACMF About CMC MAIN MENU

MAINTENANCE MESSAGES SYSTEM DIAGNOSTICS EXTENDED MAINTENANCE END OF FLIGHT PAGE

FAULT HISTORY DATABASE CURRENTLY

0% FULL

(20) On system monitor and test panel, select MAINT TEST switch to on. See Figure 202. NOTE:

The system monitor and test panel is located forward of the REER in the observers panel.

(21) Perform software load verification as follows: (a) Select CMC page on Display Unit (DU) No. 2 with Cursor Control Device (CCD) as follows: 1 Open 2 / 3 window selection drop-down menu. 2 Select CMC. 3 Verify CMC page displays on DU No. 2. (b) Select Configuration Monitor System (CMS) button on CMC page with CCD. (c) Verify system configuration page displays on DU No. 2.

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MAINTENANCE MANUAL (d) If flashing CONFIRM button displays on System Configuration page, perform the following: NOTE:

The flashing CONFIRM button displays indicated Top Level System Part Number has changed.

1 Verify the following part numbers on system configuration page match software configuration data page in aircraft logbook: • Top Level System Part Number • Configuration Part Number 2 If configuration is not correct, contact Gulfstream Customer Support. 3 If configuration is correct, select CONFIRM button. (e) Record data displayed for CMS parameters as follows. 1 Select PAGE UP or PAGE DOWN buttons to select the appropriate configuration page. NOTE:

Missing data or data shown in amber indicates a possible expired database or database out of configuration.

CMS OPTIONS / SETTINGS PARAMETERS Parameter

Data

Aircraft Type Aircraft Serial Number Aircraft Transponder Code Aircraft Registration Number Top Level System Part Number Top Level System Mod Status Configuration Part Number

CMS MODULE / LRU PARAMETERS Parameter

Module

FMS 1 NAV

NIC / PROC(1) No. 2 No. 5 No. 6

FMS 2 NAV FMS 3 NAV FMS 1 AIRCRAFT FMS 2 AIRCRAFT FMS 3 AIRCRAFT

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NIC / PROC(2) No. 2 No. 5 No. 6

Data

MAINTENANCE MANUAL CMS MODULE / LRU PARAMETERS Parameter

Module

FMS 1 CUSTOM

NIC / PROC(3) No. 2 No. 5 No. 6

FMS 2 CUSTOM FMS 3 CUSTOM ECL 1 CHECKLIST CMC LDI CMC 1 ACMF OEM

CMF 2 AMI

(2) (3) (4) (5) (6)

NIC / PROC(4) No. 3 CMC(5) NIC / PROC(6) No. 1 No. 4

CMF 1 AMI

(1)

Data

For missing or amber data, see Load INDS Airspace, Communications, EGPWS and Navigational Data (Red Media). For missing or amber data, see Load AEDB Media. Not required databases. For missing or amber data, see Load ECL Database. For missing or amber data, see Central Maintenance Computer Module - Target Load. For missing or amber data, see Load CMF AMI Database.

2 Verify recorded CMS check of part numbers match software configuration data page in aircraft logbook. 3 If module indicates error, perform target load, go to Step 2.C2.(1). 4 If database date ranges are correct but data is shown in amber, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices (NIC / PROC module battery check). (f) Select DB CONFIG button on CMC page with CCD. (g) Verify database configuration page displays on DU No. 2. (h) Record data displayed and color on database configuration page as follows: NOTE:

Missing data or data shown in amber indicates a possible expired database or database out of configuration. A single database (green or amber) displayed under database name indicates that all LRMs have same load status. If database date ranges are correct but database displays in amber, see Modular Avionics Unit / Modular Radio Cabinet - Software Loading Fault Isolation, 20-22-00, Maintenance Practices. A mixture of database (green and amber date ranges) under the same database header indicates a miscompare (mixture of successful / unsuccessful database loads). A miscompare displays LRM No. 1 in first row, LRM No. 2 in second row etc. Green and amber colors indicate the following:

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MAINTENANCE MANUAL • • • •

Green file name / date range - Database successfully loaded Amber dashed line - LRM not functioning or not in normal mode Amber XXXNo FileXXX - Database not loaded on LRM Amber file name / date range - Database not current

1 Select PAGE UP or PAGE DOWN buttons to select appropriate database configuration page. DATABASE CONFIGURATION Module / LRU

(3) (4)

(5)

Airport Comm

Red media(2)

Airport Text

Blue media(3)

En Route Comm

Blue media(3)

Obstacles

Blue media(3)

FMS

Red media(2)

Charts

Blue media(3)

Terrain

Red media(2)

Terrain Server

Green media(5)

NIC / PROC(1) No. 5

Electronic Checklist

ECL database

NIC / PROC(1) No. 1 No. 4

Programmable Message List

Programmable CAS message database

(4)

Data

Color

Red media(2)

Geopolitical

EGPWM(1) No. 1 No. 2

(2)

Source

Special Use Airspace

AGM(1) No. 1 No. 2 No. 3 No. 4

(1)

Database Name

Valid database text displays in green. Invalid database text displays in amber. The INDS airspace, communications, EGPWS and navigational data. The INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data. Env Mod DB (996-0114-XXX) is not validated on DB config page. Ensure Env Mod DB (996-0114-XXX) is loaded or a Terrain Fail (amber) message will display on CAS. The INDS terrain data.

2 Verify recorded database configuration data is valid for actual date and displays in green. 3 If data is missing or displays in amber, see appropriate procedure as follows: a For full load of source media, see Modular Avionic Unit / Modular Radio Cabinet - Software Loading (Full Load), 20-22-00, Maintenance Practices. b For target load of module / LRU, go to Step 2.C2.(1). (i) Perform DMU chart validation as follows: 1 Select Chart page on DU No. 2 with CCD as follows: a Open 2 / 3 window selection drop-down menu.

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MAINTENANCE MANUAL b Select Charts. c Verify Chart page displays on DU No. 2. 2 Select Revision Info page on DU No. 2 with CCD as follows: a Select airport drop-down menu. NOTE:

Revision Info page is selected from airport drop-down menu located at upper left of Chart page.

b Select Revision Info. c Verify Revision Info page displays on DU No. 2. 3 Verify Dataset Start Date (white) displays for current cycle, after validation. NOTE:

Dataset Start Date (amber) displays at top Revision Info page until data set is validated.

4 If Dataset Start Date (amber) displays, perform the following: a Verify INDS electronic terminal charts, geopolitical boundaries, airport information and obstacle data (blue media) are current. b Perform target load for advanced graphics module. Go to Step 2.C12.(1). (j) Verify FMS navigation data on Multifunction Control Display Unit (MCDU) No. 1 as follows: 1 Select NAV push-button. 2 Select NAV IDENT LSK (3L). 3 Verify date range below ACTIVE NDB (1R) is current and displays in green. 4 If date range below ACTIVE NDB (1R) displays in amber, go to Step 2.C4.(1). NOTE:

Missing data or date range in amber indicates a possible expired database or database out of configuration.

5 Repeat Step 2.D.(21)(j) on MCDU No. 2 and MCDU No. 3. (k) Select CMC page on DU No. 2 with CCD as follows: 1 Open 2 / 3 window selection drop-down menu. 2 Select CMC. 3 Verify CMC page displays on DU No. 2. 4 Select CMC button on CMC page. 5 Verify CMC MAIN MENU page displays on DU No. 2. (l) Verify MEMBER SYSTEM STATUS for each MAU and MRC module with CCD as follows: 1 Select EXTENDED MAINTENANCE button on CMC MAIN MENU. 2 Select MEMBER SYSTEM STATUS button on EXTENDED MAINTENANCE menu. 3 Use scroll knob to verify MEMBER SYSTEM STATUS for the following systems: • 22 AUTO FLIGHT

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MAINTENANCE MANUAL • 23 COMMUNICATIONS • 31 INDICATING/RECORDING SYSTEMS • 34 NAVIGATION 4 Verify each MAU and MRC module / LRU indicates OPERATIONAL status. 5 For any LRU NO COMM status, go to Step 2.C2.(1). (m) Verify system configuration status for each APM with CCD as follows: 1 Select MAIN MENU button on CMC page. 2 Select SYSTEM DIAGNOSTICS. 3 Use scroll knob to select the following system: • 31 INDICATING/RECORDING SYSTEMS 4 Use scroll knob to select one of the following: • CONFIGURATION MONITOR FUNCTION 1 • CONFIGURATION MONITOR FUNCTION 2 5 Use scroll knob to select the following: • CONFIGURATION MONITOR TEST 6 Verify CONFIGURATION MONITOR SYSTEM STATUS displays the following: • • • •

APM APM APM APM

1 2 3 4

STATUS: STATUS: STATUS: STATUS:

VALID VALID VALID VALID

7 If AMP status INVALID for any module, go to Step 2.C14.(1). 8 Verify SYSTEM CONFIGURATION STATUS displays the following message: • SYSTEM CONFIGURATION STATUS: PASS NOTE:

System configuration status will list any module / LRM the CMS has determined to have mismatched hardware or software.

a Target load any MAU modules / MRC NIMs flagged as out of configuration (software mismatches). Go to Step 2.C2.(1). b Replace module / LRU for hardware mismatches. (22) On maintenance laptop, perform the following: (a) Close all running computer applications. (b) Remove media. (c) Shut down maintenance laptop. (d) Turn power off. (23) Remove maintenance laptop connected in Step 2.C1.(1). (24) Remove all test equipment. (25) Comply with software load check as follows: (26) Wait a minimum of 90 seconds, then using CCD, select LAN SUMMARY page on CMC and verify LAN integrity.

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MAINTENANCE MANUAL (27) If aircraft was placed into ground mode in Step 2.B.(2)(d), close LDG GEAR SVC panel door as follows: WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(a) Select WOW OVRD switch to NORM. (b) Close WOW OVRD switch guard. (c) Remove pin and move slide lock tab down from LG MODE switch. (d) Select LG MODE switch to NORM. (e) Verify LG MODE light goes off. (f) Inspect for presence of foreign objects. (g) Close LDG GEAR SVC panel door 122AR. See Figure 201. (28) Remove electrical power from aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (29) On system monitor and test panel, select MAINT TEST switch to off. See Figure 202. (30) Inspect for presence of foreign objects. (31) Record all maintenance actions in accordance with current governing authority. 3. Modular Avionics Unit / Modular Radio Cabinet — Software Loading Fault Isolation A. General During software loading, user may encounter problems at various stages of the software loading process. This procedure is divided into three primary sections as follows: • General / Setup Problems: Step 3.C.(1) • Data Load System Software Loading Problems: Step 3.C.(2) • Software Load Check Problems: Step 3.C.(3) Each primary section documents solutions / corrective actions for known problems that are encountered during software loading. NOTE:

Do not interchange modules during the software loading process.

B. Preparation (1) Reference(s) • Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices (2) Preparation (a) Prepare aircraft for safe ground maintenance. See Safe Ground Maintenance Procedure, 20-00-00, Maintenance Practices. (b) Ensure the following aircraft conditions: • Airspeed less than 50 knots • Throttles at idle

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MAINTENANCE MANUAL WARNING:

APPLYING ELECTRICAL POWER TO AIRCRAFT MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE APPLYING ELECTRICAL POWER MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(c) Apply electrical power to aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (d) Ensure aircraft is in ground mode. If required, place aircraft in ground mode as follows: 1 Open LDG GEAR SVC panel door 122AR. See Figure 201. NOTE:

The WOW OVRD and LG MODE switches are located on the LDG GEAR SVC panel.

2 Select LG MODE switch to MAINT. 3 Move switch slide lock up. NOTE:

Slide lock holds LG MODE switch in MAINT mode.

4 Insert maintenance mode lockout pin. 5 On LDG GEAR SVC panel, verify LG MODE light comes on. 6 Remove safety cable securing WOW OVRD switch cover. WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

7 Select WOW OVRD switch to GND. (e) On system monitor and test panel, select MAINT TEST switch to on. See Figure 202. NOTE:

The system monitor and test panel is located forward of the REER in the observers panel.

(f) Connect maintenance laptop to aircraft 60 Hz system only. NOTE:

Aircraft 60 Hz power is used to provide a stable power source for software loading. If maintenance laptop is connected to any other power source (hangar, power cart, etc.), the Local Area Network (LAN) will fail and Central Maintenance Computer (CMC) Remote Maintenance Terminal (RMT) application will not connect. A sufficiently charged maintenance laptop battery may also provide a suitable stable power source for software loading.

C. Procedure (1) General / Setup Problems

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MAINTENANCE MANUAL ISSUE Missing DATA LOADER button

SYMPTOM DATA LOADER button is not displayed on CMC RMT.

CAUSE

ACTION

CMC cannot determine that it is on ground and defaults to in-air display where software loading is not allowed.

1. Ensure all initial setup conditions are met as follows: • Aircraft WOW in ground mode •

Airspeed available and <50 knots



All MAU / NIM circuit breakers depressed (1)

2. Pull all MAU and NIM circuit breakers, then depress circuit breakers pulled. 3. Wait 15 seconds. 4. Verify DATA LOADER button now displayed. CMC CONNECTION FAILED

CMC CONNECTION FAILED, The CMC is initializing after power cycle or load. CONNECTION TO 192.168.56.210 is displayed instead of CMC Main Menu.(2) NOTE This can take up to 5 minutes. Power is not applied to the CMC module. The CMC is failed or not loaded with Operational software. NOTE The RT based DLS can still be accessed using the DATA LOADER button. The LAN is not properly connected or is defective. The TCP/IP settings may be incorrect. The Wireless LAN may be active. The following maintenance laptop programs or applications may be active: •

Firewall software



Zone alarm software



Norton software

• •

Active screen saver Power save options

1. Wait at least 5 minutes for CMC to initialize after power cycle or software load, and repeat data loading process. 2. If CMC fails to respond or initialize after waiting at least 5 minutes, verify the following: •

Ensure maintenance laptop power supply is connected to aircraft 60 Hz system only



RMT LAN cable wired properly

3. If Network Interface Controller (NIC) Line Replaceable Modules (LRM)s and CMC responds to Cyberkit or ping command, Target Load operational software and possibly LDI software to CMC. 4. If NIC LRMs respond to Cyberkit or ping command and CMC fails to respond, replace CMC and reload.

20-22-00 Page 298.3 November 30/19

MAINTENANCE MANUAL ISSUE

SYMPTOM

CAUSE

CMC CONNECTION FAILED, There is an open / short somewhere in aircraft LAN. CONNECTION TO 192.168.56.210 is displayed instead of CMC Main Menu.

Inoperative LAN

ACTION Verify the following: •

(2)



LAN is operative using Cyberkit tool or ping command • RMT LAN cable wired properly

NOTE If maintenance laptop is connected to any other power source (hangar, power cart, etc.), the LAN will fail and CMC RMT will not connect. Ping/FTP Failure is seen during DLS Configuration Check on all modules that are trying to be loaded.



RMT network settings configured to GAC factory settings • All LAN interface hardware installed (3) •

Blue working bar never stops

The flashing Blue working bar, seen at various steps in data loading process, appears stuck and never stops.

DLS tool has trouble communicating with Primus Epic system and has locked up.

NOTE

After highlighting the file to download in green and clicking on SELECT FILE button, the SELECT FILE button turns inverse video.

All LAN bulkhead connectors are properly terminated

Wait a minimum of 30 minutes before taking any action. 1. Completely exit CMC RMT application by pressing Exit button on menu bar. 2. Reopen CMC RMT application and repeat data loading process.

In some instances, it is normal for the flashing Blue working bar to remain visible for more than 30 minutes.

Inverse video around SELECT FILE

Ensure maintenance laptop power supply is connected to aircraft 60 Hz system only

3. If blue working bar continues to appear stuck, pull all MAU and NIM circuit breakers, then depress circuit breakers pulled, wait 15 seconds and return to procedure. Load error has been encountered preventing data load to continue.

1. Scroll to file being loaded. 2. Press ENTER. 3. Any load errors present will be displayed below file. 4. To resolve load errors, see Data Load System (DLS) Software Loading Problems below. Step 3.C.(2).

(1) (2) (3)

Power should be applied for a minimum of 15 minutes before beginning software loading. This symptom could also be caused by an unloaded or failed CMC. If not installed, a LAN jumper must be installed.

(2) Data Load System Software Loading Problems NOTE:

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During software loading, user may encounter media or system errors. For each error, an error message is displayed that contains a general description of problem. Error messages along with other errors / events that are not displayed to user are written to log file. User can examine log files to determine content and implications of an error / event that occurs using below tables. Error messages are divided into three categories as follows:

MAINTENANCE MANUAL • Browse Screen Messages • Configuration Check and Loading Status Messages • Loading Error Messages (a) Browse Screen Messages NOTE:

If the displayed DR-PNs are not what was expected to be on the installed CD-ROMs, select the Data Load System (DLS) Main Menu or Browse Menu to refresh the media contents. ERROR

MESSAGE DISPLAYED

DESCRIPTION

SEE STEP

Unavailable

DLS tool does not detect software media source loaded in the maintenance laptop CD-ROM tray.

Step 3.C.(2)(a)1

No Media Installed

DLS tool does not detect software media source loaded in the maintenance laptop CD-ROM tray.

Step 3.C.(2)(a)2

1 Unavailable NOTE:

This error message may show during directory file selection (scrolling to [DR-PN]) before Select File option has been clicked. The error message indicates that the DLS tool cannot detect software media in the maintenance laptop CD-ROM tray. This error message is normal, if there is no software media source in the maintenance laptop CD-ROM drive. This error message may be caused by the following: • Missing / or unreadable media source • Inoperative CD-ROM drive

a Ensure Media is properly installed. b Select Prev Screen or Browse Media and reselect load type. c If not resolved, replace media source with another PlaneView disk and verify that DLS can detect new media source. d If not resolved, exit DLS, cycle power, wait 1 - 2 minutes and retry software load. e If not resolved, use an alternative load source. f If not resolved, request new copy of media. 2 No Media Installed NOTE:

This error message may show during directory file selection (scrolling to [DR-PN]) before Select File option has been clicked. This error message indicates that the DLS tool cannot detect any software media in the maintenance laptop CD-ROM tray. This message is normal if a software media source is not in the maintenance laptop CD-ROM drive. This error message may be caused by the following:

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MAINTENANCE MANUAL • Missing / or unreadable media source • Inoperative CD-ROM drive a If media is installed, ensure media is properly installed. b Select Prev Screen or Browse Media and reselect load type. c If not resolved, use an alternative load source. d If not resolved, request new copy of media. (b) Configuration Check and Loading Status Messages MESSAGE MESSAGE DISPLAYED

DESCRIPTION

ACTION

Nothing To Load

DLS has determined that the DR-PN selected does not contain any files to be loaded for a module on a selected LRM.

See Step 3.C.(2)(b)1.

Already Loaded

DLS has determined that the DR-PN selected is already loaded on the module.

See Step 3.C.(2)(b)2.

Retry [X] to load file An error was detected in the loading of an individual file and See Step a retry is being attempted by DLS. 3.C.(2)(b)3. HW Part Number Mismatch

LRM part number is incompatible with operating software.

Replace LRM and Target Load software.

1 Nothing To Load NOTE:

This message is normal, during the Configuration Check procedure on NIC / Processor (PROC) modules, when the selected software is utilized by one side of the card and not the other. This is a final message in the configuration check and no further status will be reported for the module.

a Do nothing. b Allow DLS loading process to fully complete. 2 Already Loaded NOTE:

This message is normal and indicates that the selected software has been previously loaded on the target module. This is a final message in the configuration check and no further status will be reported for the module.

a Do nothing. b Allow DLS loading process to fully complete. 3 Retry [X] to Load File NOTE:

An error was detected in the loading of an individual file to the target Line Replaceable Module (LRM) and a retry is being attempted by DLS. Symbol X is a counter of the reload attempts that are done automatically.

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MAINTENANCE MANUAL a Do nothing. b Allow DLS loading process to fully complete. c If LRM fails to load, perform the following: NOTE:

If failure occurs during a database load to an Advanced Graphics Module (AGM) or EGPWM module, wait 15 and 30 minutes respectively before continuing.

• • • •

Press Retry button Ping target module Check Local Area Network (LAN) activity Pull all MAU and NIM circuit breakers, then depress circuit breakers pulled • Wait 5 minutes, then Target Load LRM • If not resolved, replace LRM and Target Load software • If not resolved, request new copy of media (c) Loading Error Messages MESSAGE ERROR MESSAGE Cannot Use CMC To Load CMC

DESCRIPTION The onboard CMC DLS cannot be used to load the CMC module.

CMC Can’t Load Its The onboard CMC DLS cannot be used to load the NIC Own NIC module in the channel which the CMC resides.

ACTION Use PC / RT running DLS to load CMC. Use PC / RT running DLS to load CMCs NIC.

CMC/RT Host Resource Issue

RMT / DLS has encountered an issue accessing the data on the media source.

See Step 3.C.(2)(c)1.

Flash Load Fail/ Media Defect

DLS Flash programmer has encountered a problem accessing the software image on the media.

See See Step 3.C.(2)(c)2.

Flash Programmer Failure

DLS has encountered a problem programming a software image into Flash.

See Step 3.C.(2)(c)3.

Ping/FTP Communication Failure

RMT / DLS cannot communicate with the target LRM.

See Step 3.C.(2)(c)4.

Host Resource/ Media Defect

RMT / DLS has encountered an issue accessing the target LRM or data on the media source.

See Step 3.C.(2)(c)5.

HW Initializing, Do not cycle power

LRM is reinitializing as part of the software load process.

Wait for DLS to continue (maximum 45 minutes depending on module).

HW Part Number Mismatch

LRM part number is incompatible with operating software.

Replace LRM and reload.

Internal DLS Failure DLS software has encountered a problem while running its internal software.

See Step 3.C.(2)(c)6.

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MAINTENANCE MANUAL MESSAGE ERROR MESSAGE

DESCRIPTION

ACTION

Media Incompatible/ Source Media incompatible with DLS software. Defective



Request correct version of media



Request new copy of media NOTE

Contact Gulfstream Customer Support to validate media. MLF Version Not Supported

Operational software is incompatible with DLS software.

Ensure that version of DLS being used is compatible with operational software. NOTE Contact Gulfstream Customer Support to validate media.

Module Configuration Error

DLS has determined that the operational software needs to See Step be reloaded to the target LRM before the database load can 3.C.(2)(c)7. commence.

Source Media Defective

DLS has experienced a difficulty reading the source media.

See Step 3.C.(2)(c)8.

Source Media Incompatible

Source Media incompatible with DLS.

Request new copy of media. NOTE Contact Gulfstream Customer Support to validate media.

Source/System Incompatible

Source Media incompatible with Operational software loaded on aircraft.

See Step 3.C.(2)(c)9.

System Out of Config

DLS has determined the operational software is missing or corrupt on the target LRM.

See Step 3.C.(2)(c)10.

System Software Incompatible

Operational software source media is incompatible with current version of DLS.

See Step 3.C.(2)(c)11.

System Status Is In DLS believes the aircraft is not on ground and thus will not Air allow software to be loaded. Timing NICs Not Responding

DLS cannot locate an active Timing NIC. At least one Timing NIC is needed to load software.

See Step 3.C.(2)(c)12 See Step 3.C.(2)(c)13.

1 CMC/RT Host Resource Issue NOTE:

Remote Terminal / DLS has encountered an issue accessing the data on the media source due to insufficient system resources on the maintenance laptop PC.

a Allow DLS loading process to fully complete. b Close all open programs including RT / DLS.

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MAINTENANCE MANUAL c Check available disk space on maintenance laptop hard drive and ensure at least 50M free. d If not resolved, exit DLS, cycle power, wait 1 - 2 minutes and then comply with the following: • If error occurred during full load, Target Load module • If error occurred during Target Load, restart procedure 2 Flash Load Fail/Media Defect NOTE:

Data load system flash programmer has encountered a problem accessing the software image on the media. This may be caused by the following: • Dirty, damaged or unreadable media source • Inoperative CD-ROM drive

a Allow DLS loading process to fully complete. b Visually inspect media for dirt or surface scratches. c Close all open programs. d Press retry button. e If not resolved, exit DLS, cycle maintenance laptop power, wait 1 - 2 minutes and reselect load type. f If not resolved, use an alternative load source. g If not resolved, request new copy of media. NOTE:

Contact Gulfstream Customer Support to validate media.

3 Flash Programmer Failure NOTE:

Data load system has encountered a problem programming a software image into Flash.

a Allow DLS loading process to fully complete. b Close all open programs. c Press retry button. d Verify LAN activity using Cyberkit or Ping command via Command Prompt window. e Pull all MAU and NIM circuit breakers, then depress circuit breakers pulled. f Wait 5 minutes, then Target Load LRM. g If not resolved, use an alternative load source. h If not resolved, request new copy of media. i Replace LRM and Target Load software. NOTE:

Contact Gulfstream Customer Support to validate media.

4 Ping/FTP Communication Failure NOTE:

Data load system had experienced difficulty or failure communicating with the target LRM via the LAN.

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MAINTENANCE MANUAL a Allow DLS loading process to fully complete. b Verify LAN activity using Cyberkit or Ping command via Command Prompt window. NOTE:

If failure occurs during a database load to an AGM or EGPWM module, wait 15 and 30 minutes respectively before continuing.

c Press Retry button. d If not resolved, pull all MAU and NIM circuit breakers, then depress circuit breakers pulled. e Ensure all backshells are properly seated and torqued. f Wait 5 minutes, then Target Load LRM. g If not resolved, use an alternative load source. h If not resolved, request new copy of media. i Replace LRM and Target Load software. 5 Host Resource/Media Defect NOTE:

Remote Terminal / DLS has encountered an issue accessing the target LRM or data on the media source.

a Allow DLS loading process to fully complete. b Press Retry button. c Close all open programs including RT / DLS. d Check available disk space on maintenance laptop hard drive and ensure at least 50M free. e If not resolved, exit DLS, cycle power, wait 1 - 2 minutes and then comply with applicable: • If error occurred during full load, Target Load module • If error occurred during Target Load, restart procedure f If not resolved, pull all MAU and NIM circuit breakers, then depress circuit breakers pulled. g Wait 5 minutes, then Target Load LRM. h If not resolved, use an alternative load source. i If not resolved, request new copy of media. j Replace LRM and Target Load software. 6 Internal Data Load System Failure NOTE:

Data Load System software has encountered a problem while running its internal software.

a If loading from RT, perform the following: • Reboot maintenance laptop and retry operation • Reinstall RT / DLS software located on Maintenance Applications disk and retry operation

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MAINTENANCE MANUAL b If loading from CMC, perform the following: • Cycle system power and retry • Reload CMC module using PC / RT and retry operation • Replace CMC module, Target Load operational software and retry operation 7 Module Configuration Error NOTE:

Data load system has determined that the operational software needs to be reloaded to the target LRM before the database load can commence. This message is typically seen on AGM, EGPWM and NIC/ PROC modules.

a Reload operational software on module and retry database load. b If not resolved, replace LRM, Target Load operational software and retry operation. 8 Source Media Defective NOTE:

Data load system has experienced a difficulty reading the source media. This may be caused by the following: • Dirty, damaged or unreadable media source • Inoperative CD-ROM drive

a Allow DLS loading process to fully complete. b Visually inspect media for dirt or surface scratches. c Close all open programs. d Press retry button. e If not resolved, exit DLS, cycle maintenance laptop power, wait 1-2 minutes and reselect load type. f If not resolved, use an alternative load source. g If not resolved, request new copy of media. NOTE:

Contact Gulfstream Customer Support to validate media.

9 Source / System Incompatible NOTE:

Source media incompatible with current operational software loaded on aircraft.

a Verify version of source media is compatible with operational software loaded on Configuration Monitor System (CMS) page 1. b Reload target LRM with correct version of media. c Request correct version of media. NOTE:

Contact Gulfstream Customer Support to validate media.

10 System Out of Config NOTE:

Data load system has determined the operational software is missing or corrupt on the target LRM.

a Reload operational software on module and retry database load.

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MAINTENANCE MANUAL b If not resolved, replace LRM, Target Load Operational Software and retry operation. NOTE:

Contact Gulfstream Customer Support to validate media.

11 System Software Incompatible NOTE:

Operational Software source media is incompatible with current version of DLS. Earlier versions of DLS are not compatible with later versions of Operational Software.

a Verify version of RT / DLS software. b Verify version of Operational Software source media. c Reload Operational Software and retry. NOTE:

Contact Gulfstream Customer Support to validate media.

12 System Status is in Air NOTE:

Data load system cannot determine that the aircraft is on the ground and defaults to its in air display and thus will not allow software to be loaded.

a Ensure the following aircraft conditions: • Aircraft in WOW condition (on ground) • Throttles must be set to full idle and remain in this configuration throughout the loading process • Airspeed is available and less than 50 knots • All MAU and NIM circuit breakers are depressed, with power being applied for a minimum of 15 minutes prior to beginning a data load b If not resolved, perform the following: c Verify aircraft LAN operational using Cyberkit software. d Pull all MAU and NIM circuit breakers, then depress circuit breakers pulled. e Verify version of Operational Software source media. f Wait 15 minutes. g Confirm Data Loader button is now displayed. 13 Timing Network Interface Cards Not Responding NOTE:

Data load system cannot locate an active Timing NIC. At least one of the Timing NICs (NIC 1, NIC 4, NIM 1 or NIM 2) must be installed and active to load software.

a Ensure Wireless LAN is turned off. b Check / troubleshoot RT / LAN connectivity. c Cycle aircraft power. d Wait at least 5 minutes. e Verify LAN integrity via Cyberkit. f Verify at least one Timing NIC active.

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MAINTENANCE MANUAL g Restart DLS and retry operation. (3) Software Load Check Problems ISSUE

SYMPTOM

Database date Date range on DB range correct (NIC / CONFIG display PROC Battery correct but data Check) shown in yellow

CAUSE

ACTION

Battery on NIC 1 / 1. Verify failure by ensuring one of the PROC No. 1 or No. 4 following maintenance messages is active: which drives 2 system • TNIC 1 RTC / BATTERY FAULT clocks is dead. • TNIC 4 RTC / BATTERY FAULT 2. Replace NIC / PROC No. 1 (TNIC 1 fault) and / or No. 4 (TNIC 4 fault).

System Config Fail message

System Configuration Caused by one of the Fail message (amber) following: displayed on CAS. • Change in operational software occurred and CONFIRM button on CMS display not pressed • Hardware / software mismatch detected by CAS

1. Verify data on CMS display per Software Load Check procedure Step 3.C.(3). 2. Check for hardware / software mismatches per Software Load Check procedure Step 3.C.(3).

D. Follow On (1) If problem not found using above procedure, locate the file folder DlsWork in main directory of hard drive of maintenance laptop used to download software, then comply with the following: NOTE:

Any error codes generated during data download are stored in log files on remote maintenance terminal. Codes can be reviewed by Gulfstream Customer Support to aid in determining best course of action to complete download operation.

• E-mail folder as attachment to Gulfstream Customer Support • Post files in Gulfstream Technical Operations FTP site NOTE:

Along with log file, the following information should also be provided: • • • • • • •

Application (i.e., G650) Version of data load system used Error message number displayed on data load system page Line replaceable module which failed Software / version loaded on system Software / version being loaded Name / phone number of person reporting problem

(2) If aircraft was placed into ground mode in Step 3.B.(2)(d), close LDG GEAR SVC panel door as follows:

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MAINTENANCE MANUAL WARNING:

CHANGING AIRCRAFT AIR / GROUND STATE MAY CAUSE THE FLIGHT CONTROL SURFACES TO MOVE. FAILURE TO ENSURE ALL PERSONNEL AND EQUIPMENT ARE CLEAR OF FLIGHT CONTROL SURFACES BEFORE CHANGING AIRCRAFT AIR / GROUND STATE MAY RESULT IN SERIOUS INJURY, DEATH OR DAMAGE TO AIRCRAFT.

(a) Select WOW OVRD switch to NORM. (b) Close WOW OVRD switch guard. (c) Remove pin and move slide lock tab down from LG MODE switch. (d) Select LG MODE switch to NORM. (e) Verify LG MODE light goes off. (f) Inspect for presence of foreign objects. (g) Close LDG GEAR SVC panel door 122AR. See Figure 201. (3) Remove electrical power from aircraft. See Aircraft Electrical Power - Application, 20-20-10, Maintenance Practices. (4) At REER monitor and test panel, select MAINT TEST switch to off. (5) Inspect for presence of foreign objects. (6) Record all maintenance actions in accordance with current governing authority.

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