Global AIRBORNE FLIGHT INFORMATION SYSTEM MANUFACTURER DASSAULT (cont) MODEL GLOBAL TYPE DESIGNATOR MYSTERE FALCON 900 B DA90B MYSTERE FALCON 900 HEAVY DA90H MYSTERE FALCON 900B HEAVY DA90BH MYSTERE FALCON 900 EX DA90EX KING AIR E90 BE90 KING AIR 200 BE20H KING AIR 300 BE30 KING AIR 350 BE35 KING AIR 400 BE40 KING AIR 400A BE400A KING AIR 400A (Increased landing WT.
Global AIRBORNE FLIGHT INFORMATION SYSTEM MANUFACTURER CESSNA (cont) DORNIER EMBRAER GULFSTREAM ISRAEL AIRCRAFT INDUSTRIES LEAR LEAR (cont) LOCKHEED JETSTAR MITSUBISHI SABRELINER MODEL CITATION III 650 CITATION III 650A (SB 13 & 14) CITATION III 650 HEAVY CITATION III 650 HEAVY (Increased ZFW) CITATION V 560 CITATION VII 650 CITATION XL CITATION X 228-201 228-202 120 PW118 120A PW118A 120A PW118A GULFSTREAM 1 GULFSTREAM II WITH HUSH KIT GULFSTREAM II WITH TIP TANKS GULFSTREAM III GIII ASC70 GULFSTREA
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.1 CONFIGURATION MODULE PROGRAMMING FOR GNS-500A SERIES 4/5 WITH DMU P/N 42000-XX-XX 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position. 3. Press the DATA Key to display the AFIS MENU Page. See Figure 4-1. Figure 4-1 4. Use the UP or DOWN Arrow Key to position the cursor over Option 4, RECALL AFIS FPL and press the ENTER Key. The RECALL AFIS FPL Page appears.
Global AIRBORNE FLIGHT INFORMATION SYSTEM The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration. Select Options 1 to 4 as desired and Figure 4-4 will be displayed. 6. Insert the basic operating weight and press ENTER. See Figure 4-4. Figure 4-4 7. Insert the default for Auto Report and press ENTER. See Figure 4-5. Figure 4-5 8.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 9. This step is applicable only to DMU P/N 42000-03-03 and 42000-04-03. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-7. Figure 4-7 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-8. Figure 4-8 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-9.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 12. In the Flight Number cursor field, insert the number 0001 as shown in Figure 4-10. Press ENTER. NOTE: Currently, 0001 is the only valid entry and may change at a future time. Figure 4-10 13. This step is only applicable to DMU P/N 42000-01-01 and 42000-02-02. Determine the number of NMUs connected to the DMU (there are a maximum of 3), insert the number in the cursor field, and press ENTER. See Figure 4-11. Figure 4-11 14.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 15. If applicable, insert 2 to designate that Port 2 is connected to the GNS-500A system. Press ENTER. See Figure 4-13a for DMU P/N 42000-01-01 and 42000-02-02. See Figure 4-13b for DMU P/N 42000-03-03 and 42000-04-03. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-13A Figure 4-13B NOTE: Program for Port 3 as necessary. Press ENTER to continue. 16. To designate Port 1 as the Master 422 Port, insert 1 and press ENTER. See Figure 4-14.
Global AIRBORNE FLIGHT INFORMATION SYSTEM NOTE The master port refers to the use of one port by the software to have priority over the data from other ports (i.e. CDU2). Global recommends use of Port 1. 17. The 429 port option is not applicable to DMU P/N 42000-XX-XX. This page will only appear if DMU P/N 42000-03-03 or 42000-04-03 is installed. If applicable, insert 3 and press ENTER. See Figure 4-15. Figure 4-15 18. The 429 port option is not applicable to DMU P/N 42000-XX-XX.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 20. Select whether the AFIS system is using a separate antenna and press ENTER. See Figure 4-18. NOTE: The Antenna Switching Unit (ASU) allows the AFIS system to share an antenna with the VHF Com or use its own antenna. Figure 4-18 21. Insert type designator as listed in Table 4-1 and press ENTER. See Figure 4-19. NOTE: If the aircraft type is not listed in Table 4-1, contact Global Data Center to obtain type designator.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 22. Select Option 1 for ARINC network, Option 2 for SITA or AVICOM network. Press ENTER to continue. See Figure 4-20. NOTE: Air Canada network is no longer active. Figure 4-20 23. Steps 23 and 24 are only applicable to Series 4/5 users with Fuel Flow option DMU P/N 42000-02-02 or 42000-04-03. If other versions of the DMU are used, proceed to Step 25.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-22 (PAGE 2) (a) If Option 1 (NO SENSORS) is selected, the system will go to Step 25. (b) If Option 2 (FREQUENCY) is selected, Figure 4-23 appears. Select the appropriate manufacturer and scaling by using the Up and Down arrow keys to place the desired option in the cursor field. Press ENTER. NOTE: See Section 1 to cross-reference the manufacturer part number to the fuel flow type and frequency scaling. LEAR stands for J.E.T.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (c) If Option 3 (PULSE WIDTH) is selected, Figure 4-24 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. ELD stands for ELDEC. See Figure 4-24.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (e) If Option 5 (DC AMPLITUDE) is selected, Figure 4-26 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. AMTK stands for AMETEK.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (f) If Option 6 (AC AMPLITUDE) is selected, Figure 4-27 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. GE stands for General Electric. Figure 4-27 (g) If Option 7 (DC COMP. FREQ.) is selected, Figure 4-28 is displayed.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 25. This step is only applicable to DMU P/N 42000-03-03 and 42000-04-03. If other versions of DMU are used, proceed to Step 26. Select the applicable special feature option and press the ENTER Key to continue. See Figure 4-29. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features. OFF REPORT = logging takeoff times. NO OFF/ON REPORTS = no logging of takeoff and landing times. Figure 4-29 26.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 27. This step is only applicable to DMU P/N 42000-03-03 and 42000-04-03. If other versions of the DMU are used, proceed to Step 30. Select the desired option for Auto Weather update status at power up and press the ENTER Key. See Figure 4-31. Figure 4-31 28. This step is only applicable to Series 4/5 users with Satellite Data Communication System option DMU P/N 42000-03-03 and 42000-04-03. If other versions of the DMU are used, proceed to Step 30.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 29. This step is only applicable to Series 4/5 users with Satellite Data Communication System option DMU P/N 42000-03-03 and 42000-04-03. Also, Option 2 must have been selected in Step 28. If other versions of the DMU are used or Option 1 was selected in the previous step, proceed to Step 30. Select the desired option and press the ENTER Key. See Figure 4-33. Figure 4-33 30.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.2 CONFIGURATION MODULE PROGRAMMING FOR GNS-500A SERIES 4/5 WITH DMU P/N 400-045500-XXXX. NOTE: The following configuration pages are not available for DMU P/N 400-045500-0210 or 400-045500-2010. 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position. 3. Press the DATA Key to display the AFIS MENU Page. See Figure 4-35. Figure 4-35 4.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu Page (Figure 4-37) and press the ENTER Key. The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration. Select Options 1 to 4 as desired and Figure 4-38 will be displayed. Figure 4-37 6. Insert the basic operating weight and press ENTER. See Figure 4-38.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 8. Insert 15 as the Auto Reporting time interval unless advised differently by the pilot/operator and press ENTER. See Figure 4-40. Figure 4-40 9. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-41. Figure 4-41 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-42.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-43. NOTE: Currently, GS is the only valid entry and may change at a future time. Figure 4-43 12. In the Flight Number cursor field, insert the number 0001 as shown in Figure 4-44. Press ENTER. NOTE: Currently, 0001 is the only valid entry and may change at a future time. Figure 4-44 13.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 14. If applicable, insert 2 to designate that Port 2 is connected to the GNS-500A system. Press ENTER. See Figure 4-46. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-46 15. If applicable, insert 2 to designate that Port 3 of connected to the GNS-500A system and press ENTER. See Figure 4-47. Figure 4-47 16. To designate Port 1 as the Master 422 Port, insert 1 and press ENTER. See Figure 4-48.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 17. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only GWS systems are used, insert 3 and press ENTER. See Figure 4-49. Figure 4-49 18. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-50. Figure 4-50 19.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 20. Select whether the AFIS system is using a separate antenna and press ENTER. See Figure 4-52. NOTE: The Antenna Switching Unit (ASU) allows the AFIS system to share an antenna with the VHF Comm or use its own antenna. Figure 4-52 21. Insert type designator as listed in Table 4-1 and press ENTER. See Figure 4-53. NOTE: If the aircraft type is not listed in Table 4-1, contact Global Data Center to obtain type designator.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 22. Select Option 1 for ARINC network, Option 2 for SITA or AVICOM network. Press ENTER to continue. See Figure 4-54. NOTE: Air Canada network is no longer active. Figure 4-54 23. Steps 23 and 24 are only applicable to Series 4/5 users with Fuel Flow option DMU P/N 400-045500-0002, 400-045500-0004 or 400-045500-0006. If other versions of the DMU are used, proceed to Step 25.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-56 (PAGE 2) (a) If Option 1 (NO SENSORS) is selected, the system will go to Step 25. (b) If Option 2 (FREQUENCY) is selected, Figure 4-57 appears. Select the appropriate manufacturer and scaling by using the Up and Down arrow keys to place the desired option in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the manufacturer part number to the fuel flow type and frequency scaling. LEAR stands for J.E.T.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (c) If Option 3 (PULSE WIDTH) is selected, Figure 4-58 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. ELD stands for ELDEC. See Figure 4-58.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (e) If Option 5 (DC AMPLITUDE) is selected, Figure 4-60 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. AMTK stands for AMETEK. CAN is Canadian Marconi, CON is Consolidated Airborne and RAG is Ragen Data System.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (f) If Option 6 (AC AMPLITUDE) is selected, Figure 4-61 is displayed. Use the Up and Down arrow keys to place the appropriate manufacturer/scaling in the cursor field. Press ENTER. NOTE: See Section 1.3.2, SYSTEM SPECIFICATIONS, to cross-reference the fuel flow indicator/transmitter manufacturer’s part number to the appropriate scaling values. GE stands for General Electric. Figure 4-61 (g) If Option 7 (DC COMP. FREQ.) is selected, Figure 4-62 is displayed.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 25. Select the applicable special feature option and press the ENTER Key to continue. See Figure 4-63. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features. OFF REPORT = logging takeoff times. NO OFF/ON REPORTS = no logging of takeoff and landing times. Figure 4-63 26. Select whether stored flight plans, messages and weather will be retained in memory when power is interrupted.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 28. This step is only applicable to Series 4/5 users with Satellite Data Communication System option DMU P/N 400-045500-0003, 400-045500-0004, 400-045500-0005 or 400-045500-0006. If other versions of the DMU are used, proceed to Step 30. If applicable, select Satcom Option 2 and press the ENTER Key. See Figure 4-66. If Option 1 is selected, proceed to Step 30. Options 3 and 4 are only available with DMU P/N 400-045500-0005 or 400-045500-0006. Figure 4-66 29.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.3 CONFIGURATION MODULE PROGRAMMING FOR GNS-1000, GNS-X, GNS-XES, GNS-XL OR GNS-XLS WITH DMU P/N 42000-01-01 OR 42000-03-03 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position. 3. Press the PLAN Key or AFIS Key to display the AFIS MENU Page. See Figure 4-69 or Figure 4-70. Figure 4-69 Figure 4-70 4.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu Page (Figure 4-69) and press the ENTER Key. The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration. Select Options 1 to 4 as desired and Figure 4-72 will be displayed. Figure 4-72 6. Insert the basic operating weight and press ENTER. See Figure 4-73.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 8. Insert 15 as the Auto Reporting time interval unless advised differently by the pilot/operator and press ENTER. See Figure 4-75. Figure 4-75 9. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-76. Figure 4-76 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-77.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-78. NOTE: Currently, GS is the only valid entry and may change at a future time. Figure 4-78 12. In the Flight Number cursor field, insert the number 0001 as shown in Figure 4-79. Press ENTER. NOTE: Currently, 0001 is the only valid entry and may change at a future time. Figure 4-79 13. This step is only applicable to DMU P/N 42000-01-01.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 14. Insert 1 as shown in Figure 4-81 to indicate that Port 1 is connected to the GNS-1000 or GNS-X system and press ENTER. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-81 15. If applicable, insert 1 to designate that Port 2 is connected to the GNS-1000 or GNS-X system. Press ENTER. See Figure 4-82a for DMU P/N 42000-01-01. See Figure 4-82b for DMU P/N 42000-03-03. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 16. If applicable, insert 1 to designate that Port 3 is connected to the GNS-1000 or GNS-X system. Press ENTER. See Figure 4-83a for DMU P/N 42000-01-01. See Figure 4-83b for DMU P/N 42000-03-03. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-83A Figure 4-83B 17. To designate Port 1 as the Master 422 Port, insert 1 and press ENTER. See Figure 4-84.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 18. The 429 port option is not applicable to DMU P/N 42000-XX-XX. This page will only appear if DMU P/N 42000-03-03 is installed. If applicable, insert 3 and press ENTER. See Figure 4-85. Figure 4-85 19. The 429 port option is not applicable to DMU P/N 42000-XX-XX. This page will only appear if DMU P/N 42000-03-03 is installed. If applicable, insert 3 and press ENTER. See Figure 4-86. Figure 4-86 20. The 429 port option is not applicable to DMU P/N 42000-XX-XX.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 21. Select whether the AFIS system is using a separate antenna and press ENTER. See Figure 4-88. NOTE: The Antenna Switching Unit (ASU) allows the AFIS system to share an antenna with the VHF Comm or use its own antenna. Figure 4-88 22. Insert type designator as listed in Table 4-1 and press ENTER. See Figure 4-89. NOTE: If the aircraft type is not listed in Table 4-1, contact Global Data Center to obtain type designator. Figure 4-89 23.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 24. Fuel Flow option is not available for GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS. Insert 1 and press the ENTER Key. See Figure 4-91. Figure 4-91 25. Fuel Flow option is not available for GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS. Select 1 and press the ENTER Key. See Figure 4-92. Figure 4-92 26. This step is only applicable to DMU P/N 42000-03-03. If other versions of DMU are used, proceed to Step 27.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 27. Select whether stored weather will be retained in memory when power is interrupted. Press the ENTER Key to continue. See Figure 4-94. Figure 4-94 28. This step is only applicable to DMU P/N 42000-03-03. If other versions of the DMU are used, proceed to Step 30. Select the desired option for Auto Weather update status at power up and press the ENTER Key. See Figure 4-95. Figure 4-95 29.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 30. This step is only applicable to GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS with Satellite Data Communication System option DMU P/N 42000-03-03. If other versions of the DMU are used, proceed to Step 31. Select the desired option and press the ENTER Key. See Figure 4-97. Figure 4-97 31. Write configuration data to the Configuration Module by selecting 2 and press the ENTER Key. See Figure 4-98.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.4 CONFIGURATION MODULE PROGRAMMING FOR GNS-1000, GNS-X, GNS-XES, GNS-XL OR GNS-XLS WITH DMU P/N 400-045500-0001, 400-045500-0003 OR 400-045500-0005 AND OTHER FMS MANUFACTURES USING DMU P/N 400-045500-0001, 0002, -0003, -0004, -0005, -0006 OR -0130 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4. Use the UP or DOWN Arrow Key or Line >Select keys to position the cursor over the RECALL AFIS FPL option and press the ENTER Key. The RECALL AFIS FPL Page appears. Use the UP or DOWN Arrow Key or Line Select keys to position the cursor over the DATE field and enter 357777. Press the ENTER Key. See Figure 4-101. Figure 4-101 NOTE: ITEMS 4(a) through 4(k) are only available for -0003 or -0130. For other part numbers skip to item 5.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (b) If ACARS page shown in Figure 4-102 appears, press “1" key and the PREFLIGHT Data page, Figure 4-104 will appear. Otherwise proceed to step 4(h). Figure 4-104 (c) Insert a one digit number (eg. 1) in FLT NO: field and press ENTER key. Cursor will move FLT RLS DATE: field. (d) Insert a one digit number (eg. 1) in FLT RLS DATE: field and press ENTER key. Cursor will move to DEPT STN: field. (e) Insert a three character departure station identifier (eg.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (k) Enter 3577 in ETD field and press ENTER key. See Figure 4-106 and proceed to step 5. Figure 4-106 5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu Page (Figure 4-107) and press the ENTER Key. The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 7. Insert the default for Auto Report and press ENTER. See Figure 4-109. Figure 4-109 8. Insert 15 as the Auto Reporting time interval unless advised differently by the pilot/operator and press ENTER. See Figure 4-110. Figure 4-110 9. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-111.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-112. Figure 4-112 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-113. NOTE: Currently, GS is the only valid entry except for the following: XJ for MESABA Airlines, DH for Atlantic Coast Aviation, Part Numbers 400-045500-0003 or 400-045500-0130 ONLY. Figure 4-113 12.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 13. Insert 1 as shown in Figure 4-115 to indicate that Port 1 is connected to the GNS-1000, GNS-X, or other manufactures navigation system and press ENTER. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-115 14. If applicable, insert 1 to designate that Port 2 is connected to the GNS-1000 or GNS-X system. Press ENTER. If no Global systems are connected, select Option 4. See Figure 4-116. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 15. If applicable, insert 1 to designate that Port 3 is connected to the GNS-1000 or GNS-X system. Press ENTER. If no Global systems are connected, select Option 4. See Figure 4-117. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-117 16. To designate Port 1 as the Master 422 Port, insert 1 and press ENTER. See Figure 4-118. NOTE: The master port refers to the use of one port by the software to have priority over the data from other ports (i.e.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 18. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-120. Figure 4-120 19. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-121. Figure 4-121 20. Select whether the AFIS system is using a separate antenna and press ENTER.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 21. Insert type designator as listed in Table 4-1 and press ENTER. See Figure 4-123. NOTE: If the aircraft type is not listed in Table 4-1, contact Global Data Center to obtain type designator. Figure 4-123 22. Select Option 1 for ARINC network or Option 2 for SITA or AVICOM network. Press ENTER to continue. See Figure 4-124. Figure 4-124 23. Fuel Flow option is not available for GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS. Insert 1 and press the ENTER Key.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 24. Fuel Flow option is not available for GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS. Select 1 and press the ENTER Key. See Figure 4-126. Figure 4-126 25. Select the applicable special feature option and press the ENTER Key to continue. (a) If Airline ID of GS has been entered the special selection features page will appear as in Figure 4-127. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (b) If Airline ID XJ or DH has been inserted the special feature option will be displayed as Figure 4-128. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features. OFF REPORT = logging takeoff times. NO OFF/ON REPORTS = no logging of takeoff and landing times. ACARS REPORTS = Customer defined non-standard AFIS features.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Use UP or DOWN arrow keys or right hand line select keys to position cursor over selections. Depress BACK key to cycle between YES and No selection. Press ENTER key to select. Cursor will move to next entry below selection. If cursor is on TITLE PAGE ACARS selection, then pressing ENTER key will activate the page shown in Figure 4-130. BACK key - depressed with cursor off page causes SPECIAL FEATURES selection to appear.
Global AIRBORNE FLIGHT INFORMATION SYSTEM ENTER key - depress to select. Cursor will move to next entry below selection. If over TITLE PAGE ACARS selection, pressing ENTER key will display the page shown in Figure 4-130. 26. Select whether stored flight plans, messages and weather will be retained in memory when power is interrupted. Press the ENTER Key to continue. See Figure 4-132. Figure 4-132 27. Select the desired option for Auto Weather update status at power up and press the ENTER Key.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 28. This step is only applicable to GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS with Satellite Data Communication System option DMU P/N 400-045500-0003, 400-045500-0004, 400-045500-0005, 400-045500-0006 or 400-045500-0130. If other versions of the DMU are used, proceed to Step 30. If applicable, select Satcom Option 2 and press the ENTER Key. See Figure 4-134.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.5 CONFIGURATION MODULE PROGRAMMING FOR GNS-1000, GNS-X, GNS-XES, GNS-XL OR GNS-XLS WITH DMU P/N 400-045500-0210 OR 400-045500-2010. 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position. If DMU has been previously configured for ACARS proceed to step 4(a) otherwise step 3. 3. Press the PLAN Key or AFIS Key to display the AFIS MENU Page. See Figures 4-137 through 4-139.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4. Use the UP or DOWN Arrow Key or Line >Select keys to position the cursor over the RECALL AFIS FPL option and press the ENTER Key. The RECALL AFIS FPL Page appears. Use the UP or DOWN Arrow Key or Line Select keys to position the cursor over the DATE field and enter 357777. Press the ENTER Key. See Figure 4-140. Figure 4-140 NOTE: For non-ACARS programming, proceed to step 5. (a) Press the PLAN key or AFIS key to display the ACARS page.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (b) If ACARS page shown in Figure 4-141 appears, press “1" key and the PREFLIGHT Data page, Figure 4-143 will appear. Otherwise proceed to step 4(h). Figure 4-143 (c) Insert a one digit number (eg. 1) in FLT NO: field and press ENTER key. Cursor will move FLT RLS DATE: field. (d) Insert a one digit number (eg. 1) in FLT RLS DATE: field and press ENTER key. Cursor will move to DEPT STN: field. (e) Insert a three character departure station identifier (eg.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (k) Enter 3577 in ETD field and press ENTER key. See Figure 4-145 and proceed to step 5. Figure 4-145 5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu Page (Figure 4-146) and press the ENTER Key. The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 7. Insert the default for Auto Report and press ENTER. See Figure 4-148. Figure 4-148 8. Insert 15 as the Auto Reporting time interval unless advised differently by the pilot/operator and press ENTER. See Figure 4-149. Figure 4-149 9. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-150.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-151. Figure 4-151 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-152. NOTE: Currently, GS is the only valid entry except for the following: XJ for MESABA Airlines, DH for Atlantic Coast Aviation. Figure 4-152 12. In the Flight Number cursor field, insert the number 0001 as shown in Figure 4-153. Press ENTER.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 13. Insert 1 as shown in Figure 4-154 to indicate that Port 1 is connected to the GNS-1000, GNS-X, or other manufactures navigation system or insert 3 if a graphical GNS-XLS is attached to port 1. Press ENTER. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-154 14.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 15. If applicable, insert 1 to designate that Port 3 is connected to the GNS-1000 or GNS-X system or insert 3 if Port 3 is connected to a Graphical GNS-XLS. Press ENTER. If no Global systems are connected, select Option 4. See Figure 4-156. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-156 16. To designate Port 1 as the Master 422 port, insert 1 and press ENTER. See Figure 4-157.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 18. Insert a 2 if a weather graphics RPU is connected to Cabin Terminal Port 1. Otherwise, insert a 1. See Figure 4-159. Figure 4-159 19. Insert a 2 if a weather graphics RPU is connected to Cabin Terminal Port 2. Otherwise, insert a 1. See Figure 4-160 Figure 4-160 20. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-161.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 21. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-162. Figure 4-162 22. Select whether the AFIS system is using a separate antenna and press ENTER. See Figure 4-163. NOTE: The Antenna Switching Unit (ASU) allows the AFIS system to share an antenna with the VHF Comm or use its own antenna. Figure 4-163 23.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 24. Select Option 1 for ARINC network or Option 2 for SITA or AVICOM network. Press ENTER to continue. See Figure 4-165. Figure 4-165 25. Fuel Flow option is not available for GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS. Insert 1 and press the ENTER Key. See Figure 4-166. If DMU P/N 400-045500-0004, 400-045500-0006 or other NAV system is used, select the appropriate fuel flow pages. Figure 4-166 26.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 27. Select the applicable special feature option and press the ENTER Key to continue. (a) If Airline ID of GS has been entered the special selection features page will appear as in Figure 4-168. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features. OFF REPORT = logging takeoff times. NO OFF/ON REPORTS = no logging of takeoff and landing times.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (c) If Airline ID of DH or *A has been entered, the following page selections will be available. Figure 4-170 Use UP or DOWN arrow keys or right hand line select keys to position cursor over selections. Depress BACK key to cycle between YES and No selection. Press ENTER key to select. Cursor will move to next entry below selection. If cursor is on TITLE PAGE ACARS selection, then pressing ENTER key will activate the page shown in Figure 4-171.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (d) If Airline ID of XJ or *M has been entered, the following configuration selection will be available. See Figure 4-172. Figure 4-172 Use UP or Down arrow or right hand LINE SELECT keys to position cursor over selections. BACK key - depressed to cycle between YES and NO with cursor over desired selection. ENTER key - depress to select. Cursor will move to next entry below selection.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 30. Select the desired option for Auto Weather update status at power up and press the ENTER Key. See Figure 4-175. Figure 4-175 31. This step is only applicable to GNS-1000, GNS-X, GNS-XES, GNS-XL or GNS-XLS with Satellite Data Communication System option DMU P/N 400-045500-0210 or 400-045500-2010. If other versions of the DMU are used, proceed to Step 33. If applicable, select Satcom Option 2 and press the ENTER Key. See Figure 4-176.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 33. Write configuration data to the Configuration Module be selecting 2 and press the ENTER Key. See Figure 4-178. Figure 4-178 34. Power Off DMU and restart. NOTE: This completes AFIS configuration. For ACARS configuration, proceed to step 4(a).
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.6 CONFIGURATION MODULE PROGRAMMING FOR GNS-1000, GNS-X, GNS-XES, GNS-XL OR GNS-XLS WITH DMU P/N 400-045500-0211 OR 400-045500-2011. 1. Install test connector P/N 12870-1 to the front of the DMU on J102. 2. Turn system on. Press the ENTER Key to accept DATE, GMT, and Position. If DMU has been previously configured for ACARS proceed to step 4(a) otherwise step 3. 3. Press the PLAN Key or AFIS Key to display the AFIS MENU Page. See Figures 4-179 through 4-181.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4. Use the UP or DOWN Arrow Key or Line >Select keys to position the cursor over the RECALL AFIS FPL option and press the ENTER Key. The RECALL AFIS FPL Page appears. Use the UP or DOWN Arrow Key or Line Select keys to position the cursor over the DATE field and enter 357777. Press the ENTER Key. See Figure 4-182. Figure 4-182 NOTE: For non-ACARS programming, proceed to step 5. (a) Press the PLAN key or AFIS key to display the ACARS page.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (b) If ACARS page shown in Figure 4-183 appears, press “1" key and the PREFLIGHT Data page, Figure 4-185 will appear. Otherwise proceed to step 4(h). Figure 4-185 (c) Insert a one digit number (eg. 1) in FLT NO: field and press ENTER key. Cursor will move FLT RLS DATE: field. (d) Insert a one digit number (eg. 1) in FLT RLS DATE: field and press ENTER key. Cursor will move to DEPT STN: field. (e) Insert a three character departure station identifier (eg.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (k) Enter 3577 in ETD field and press ENTER key. See Figure 4-145 and proceed to step 5. Figure 4-187 5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu Page (Figure 4-188) and press the ENTER Key. The dates of previously entered configurations are shown in Options 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 7. Insert the default for Auto Report and press ENTER. See Figure 4-190. Figure 4-190 8. Insert 15 as the Auto Reporting time interval unless advised differently by the pilot/operator and press ENTER. See Figure 4-191. Figure 4-191 9. Select Option 1 if reports are not wanted on the ground. Select Option 2 if reports on the ground are required. See Figure 4-192.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 10. Insert complete aircraft registration number (tail number) in the cursor field and press ENTER. See Figure 4-193. Figure 4-193 11. Insert GS as the Airline ID number and press ENTER. See Figure 4-194. NOTE: Currently, GS is the only valid entry except for the following: XJ for MESABA Airlines, DH for Atlantic Coast Aviation. Figure 4-194 12. In the Flight Number cursor field, insert the number 0001 as shown in Figure 4-195. Press ENTER.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 13. Insert 1 as shown in Figure 4-196 to indicate that Port 1 is connected to the GNS-1000, GNS-X, or other manufactures navigation system or insert 3 if a graphical GNS-XLS is attached to port 1. Press ENTER. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-196 14.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 15. If applicable, insert 1 to designate that Port 3 is connected to the GNS-1000 or GNS-X system or insert 3 if Port 3 is connected to a Graphical GNS-XLS. Press ENTER. If no Global systems are connected, select Option 4. See Figure 4-198. NOTE: GNS-X applies also to GNS-XES, GNS-XL and GNS-XLS. Figure 4-198 16. To designate Port 1 as the Master 422 port, insert 1 and press ENTER. See Figure 4-199.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 18. Insert a 2 if a weather graphics RPU is connected to Cabin Terminal Port 2. Otherwise, insert a 1. See Figure 4-201 Figure 4-201 19. The 429 port option is only applicable when other manufacturers navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-202. Figure 4-202 20. The 429 port option is only applicable when other manufacturer’s navigation systems are installed.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 21. The 429 port option is only applicable when other manufacturer’s navigation systems are installed. If only Global systems are used, insert 3 and press ENTER. See Figure 4-204. Figure 4-204 22. Select whether the AFIS system is using a separate antenna and press ENTER. See Figure 4-205. NOTE: The Antenna Switching Unit (ASU) allows the AFIS system to share an antenna with the VHF Comm or use its own antenna. Figure 4-205 23.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 24. Select Option 1 for ARINC network or Option 2 for SITA or AVICOM network. Press ENTER to continue. See Figure 4-207. Figure 4-207 25. Select Option 2 if ACMS (FDAMS) hardware will be installed. Press ENTER key to continue. See Figure 4-208. NOTE: If option 1 is selected, skip to step 28. Figure 4-208 26. Select number of engines applicable. Press ENTER key to continue. See Figure 4-209.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 27. Insert 1-4 Engine Serial Numbers based on number entered in Step 26. Press ENTER key to continue. See Figure 4-210. Figure 4-210 28. Select the applicable special feature option and press the ENTER Key to continue. (a) If Airline ID of GS has been entered the special selection features page will appear as in Figure 4-211. NOTE: OFF/ON REPORTS = logging takeoff and landing times. OPTION 1 = customer defined non-standard AFIS features.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-212 NOTE: If Airline ID is GS, ACARS reports can be accessed by pressing *A or *M and then pressing ENTER key. If ACARS REPORTS, 5, has been selected, see Figure 4-213 for Airline ID DH or see Figure 4-215 for Airline ID XJ; otherwise, proceed to step 31. (c) If Airline ID of DH or *A has been entered, the following page selections will be available. Figure 4-213 Use UP or DOWN arrow keys or right hand line select keys to position cursor over selections.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-214 Use UP or Down arrow or right hand LINE SELECT keys to position cursor over option. NOTE: For airline ID of DH or *A, set OFF OR ON TRIGGERED BY: to 2. BACK key - depressed to cycle between YES and NO with cursor over USE ACARS TIME. ENTER key - depress to select. Cursor will move to next entry below selection. If over OFF OR ON TRIGGERED BY: selection, pressing ENTER key will proceed to step 32.
Global AIRBORNE FLIGHT INFORMATION SYSTEM ENTER key - depress to select. Cursor will move to next entry below selection. If over TITLE PAGE ACARS selection, pressing ENTER key will display the page shown in Figure 4-216 29. Select applicable inputs for use ACARS TIME and OFF OR ON TRIGGERED BY. NOTE: If Airline ID of XJ or *M has been entered, set use ACARS TIME to NO using BACK key and insert 2 for OFF OR ON TRIGGERED BY. See Figure 4-216.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 31. Select whether the AFIS system is using standard default (ground speed) or weight on wheels to trigger in-air detection. Enter selection and press ENTER (see Figure 4-218) Figure 4-218 NOTE: After making a selection, go to step 32. 32. Select whether stored flight plans, messages and weather will be retained in memory when power is interrupted. Press the ENTER Key to continue. See Figure 4-218. Figure 4-219 33.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Select AERO-C option for AERO-C satellite system, ARINC 741 for Aeronautical Standard (ARINC 741) satellite system and SATFONE for SATFONE system. ARINC 741 and SATFONE can only be selected when using DMU P/N 400-045500-2011. Figure 4-221 35. Select the desired option and press the ENTER Key. See Figure 4-222. Figure 4-222 36. Write configuration data to the Configuration Module be selecting 2 and press the ENTER Key. See Figure 4-223. Figure 4-223 37.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.7 CONFIGURATION MODULE PROGRAMMING FOR 739 MCDU AND OTHER FMS MANUFACTURERS WITH DMU P/N 400-45000-2011 OR 400-45000-0211 1. 2. Install test connector P/N 12870-1 to the front of the DMU on J102. Turn system on. If DMU has been configured for ACARS proceed to step 5 otherwise go to step 3. 3. L1 L2 L3 L4 L5 L6 Press line-select-key L4 to access Recall FPL Page. See Figure 4-224.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 5. L1 L2 L3 L4 L5 L6 Enter 3577 in line 13 and press L4. See figure 4-226. 0 1 2 3 4 5 6 7 8 9 0 1 2 3 0 1 H F L A A D E K K D E Y Y E T D D E T L + 2 H T A P K S Y D D E L 3 4 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 : MM I N I T I A L I Z E # C A X X T F Z Z T F T T A D R R 1 1 A X O Z A T C R 2 3 / 1 X X - R1 Z Z - R2 T T - R3 M R R - R4 L - R5 < M E N U 3 5 7 7 T R A N S M I T > - R6 Figure 4-226 6.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 7. L1 L2 L3 L4 L5 L6 Select the AFIS configuration to be read or modified from the AFIS configuration Menu Page (Figure 4-228) by pressing adjacent line-select-key. The dates of previously entered configurations are shown in Option 1 to 3. The newest configuration date appears first. Option 4 allows for the entry of a new configuration. Select Option 1 to 4 as desired and Figure 4-229 will be displayed.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 9. See Figure 4-230 and perform the following steps: a. b. c. d. Enter aircraft type in the scratch pad line 13 and press line-select-key L1. Enter basic operating weight in the scratch pad line 13 and press line-select-key L2. Press line-select-key L3 to toggle separate antenna to yes or no. Press line-select-key L4 to toggle default frequency between U.S. DEFAULT and EUROPEAN DEFAULT. e. Press line-select-key R6 to go to the next page.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 11. See Figure 4-232 and perform the following steps: a. Press line-select-key L1 to toggle the default for Port 1 between GNS-1000/GNS-X and GNS-500. b. Press line-select-key L3 to toggle the default for Port 2 between GNS-1000/GNS-X and GNS-500 c. Press line-select-key L5 to toggle the default for Port 3 between GNS-1000/GNS-X, GNS-500, and NONE. d. Press line-select-key R6 to go to the next page.
Global AIRBORNE FLIGHT INFORMATION SYSTEM L1 L2 L3 L4 L5 L6 0 1 2 3 4 5 6 7 8 9 0 1 2 3 0 1 2 3 4 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 1 2 3 C O N F I G U R A T I O N 6 / 1 1 4 2 9 P R I M A R Y P O R T I S : * 4 2 9 - R1 - R2 4 2 9 S E C O N D A R Y * 5 7 1 P O R T I S : - R3 - R4 4 2 9 T E R T I A R Y * O F F P O R T I S : - R5 < P R E V I O U S N E X T > - R6 Figure 4-233 13. Select whether stored flight plans, messages and weather will be retained in memory when power is interrupted.
Global AIRBORNE FLIGHT INFORMATION SYSTEM See Figure 4-235. a. Press line-select-key L1 to toggle the default for SAT System Available between NO, AERO-C, ARINC741, and SATFONE. b. Press line-select-key L3 to toggle the default for SAT Network Will PWR Up between LAST STATE, ON or OFF. c. Press line-select-key R6 to go to the next page.
Global AIRBORNE FLIGHT INFORMATION SYSTEM L1 L2 L3 L4 L5 L6 0 1 2 3 4 5 6 7 8 9 0 1 2 3 0 1 2 3 4 C M A S T E * P O R 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 1 2 3 O N F I G U R A T I O N 9 / 1 1 R 4 2 2 P O R T I S T 1 - R1 - R2 U S E D M U * Y E S W T - O N - W H E E L I N P T - R3 - R4 F E A T U R E S E L E C T I O N * N O O N / O F F R E P O R T S < P R E V I O U S - R5 N E X T > - R6 Figure 4-236 16.
Global AIRBORNE FLIGHT INFORMATION SYSTEM L1 L2 L3 L4 L5 L6 0 1 2 3 4 5 6 7 8 9 0 1 2 3 0 1 2 3 4 C A R I N C * Y E S S I T A * Y E S A T O F * N O P R I N T * Y E S P R I N T * Y E S 5 6 7 8 9 0 1 2 3 4 5 6 7 8 9 0 O N F I G U R A T I O N 1 0 T I T L E A C Y A C A R S T N O R M F E E D 1 / A E I O 2 1 R S M 3 1 S * - R1 E * - R2 - R3 E R 1 E R 2 - R4 - R5 < P R E V I O U S N E X T > - R6 Figure 4-238 18. Use adjacent line-select-key to toggle and select the configuration items.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.8 4.8.1 AFIS DATA MANAGEMENT UNIT (DMU) (ProComm Plus Reconfiguration Procedure) General This section contains instructions for configuring the AFIS DMU through the test port using a personal computer (PC) and Symantec Corporation’s ProComm Plus for Windows software. The aircraft specific configuration settings reside on the configuration module, not in the DMU itself.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.8.2 Equipment Required A. AFIS System. DMU P/N 400-045500-XXXX Mod 6 and above. B. Computer: (IBM or compatible 386, 486, or higher. 1. Windows 3.1 or higher in enhanced mode. 2. A minimum of 4 Megabytes of RAM. 3. Operating system PC-DOS or MS-DOS, version 3.1 or higher. C. ProComm Plus (for Windows software. D. User Fabricated Interconnect cable.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.8.3 Configuration of Terminal Mode 1. Follow the manufacturer instruction for installing ProComm Plus. 2. Run the ProComm Plus program. (Note: If you’re using a DOS version, it will be necessary to change to the PCPLUS directory from the DOS prompt) 3. The Terminal Window should now be displayed. 4. Select Port Settings from the Setup Menu, or access Port Settings with the command ALT-P (see figure 4-243). 5.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-243 Sample Port Settings Figure 4-244 Sample Terminal Options IMAFISJWA 4-104 March/2001
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.8.4 Programming the AFIS DMU 1) Attach the interconnect cable to the DMU Test Port, and to the laptop. 2) Start the ProComm program. Windows users click the ProComm Plus icon to get to the Terminal Window. 3) Apply power to the DMU. The DMU will indicate that it is ready by sending a string of U’s which appear on the screen at the CMD prompt as indicated in figure 4-245 below. NOTE: The Caps Lock on your computer keyboard must be locked "ON".
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4) Type ON to open the AFIS Terminal. 5) Press ENTER. The message “terminal mode on” will appear briefly followed by the terminal display (see figure 4-246 below).
Global AIRBORNE FLIGHT INFORMATION SYSTEM 6) From the command line, type CM 7) Press ENTER 8) The Configuration Module Menu will be displayed (see figure 4-247 below). Figure 4-247 Configuration Module Menu 9) For specifics on choosing the parameters shown above please reference the appropriate section of the AFIS Installation manual.
Global AIRBORNE FLIGHT INFORMATION SYSTEM NOTE: Don’t forget to use spaces between the CC, NN, and VALUE characters as shown in the example above. 10) After you are finished changing the configuration data, type: PGMCNF (then press ENTER) Entering this command will program the AFIS configuration module with the settings from the ProComm Configuration Module Menu page shown in Figure 4-247 above. 11) The configuration change is now complete.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 4.9 GENERAL This section presents the basic test procedure that should be performed after the AFIS system has been installed. If AFIS is installed with a GNS-500A Series 4/5 system, be sure the GNS-500A System Checkout is done per Report 1228, GNS-500A Series 4/5 Installation Manual, before performing AFIS checkout.
Global AIRBORNE FLIGHT INFORMATION SYSTEM GNS-500A SYSTEM MESSAGE PAGE Figure 4-248 GNS-1000 OR GNS-X SYSTEM MESSAGE PAGE Figure 4-249 1. If the message AFIS LINK FAIL appears on the GNS-500 system message page: (a) Check aircraft wiring connection between CDU and DMU per Section 3. (b) Verify that the + 28 VDC is present on the DMU at the appropriate pin locations as defined in Section 3. 1 Pin designation for + 28 VDC on DMU PN 42000-XX-XX is J1-5, J1-3 with a return on J1-4.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 1 Pin designation for + 28 VDC on DMU PN 42000-XX-XX is J1-5, J1-3 with a return on J1-4. 2 Pin designation for + 28 VDC on DMU PN 400-045500-XXXX is J2-6, J2-7 with a return on J2-1 and J2-2. 3. If the message AFIS LINK FAIL appears on the GNS-X Message Page: (a) Check aircraft wiring connection between the NMU and DMU and between the CDU and DMU (+ 28 VDC Switched On Power Control) per Section 3.
Global AIRBORNE FLIGHT INFORMATION SYSTEM GNS-1000 OR GNS-X INITIALIZATION PAGE Figure 4-251 E. With cursor positioned over the DATE field, perform the following: 1. To accept DATE display, press ENTER key. 2. To enter new date make numerical entry from keyboard in order of day-month-year and press ENTER key. NOTE: For example, 5 Feb 1992 would be entered as 050292.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-252 1. If the NO DISK message appears, verify that the pre-programmed AFIS disk is in the DTU. If the message persists, check wiring between the DMU and DTU per Section 3. See Figure 4-253. Figure 4-253 I.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-255 AFIS MENU 1. WX GRAPHICS 2. TERMINAL WX 3. SIGMETS 4. WINDS ALOFT 5. AFIS FLT PLAN 6. RECALL AFIS FPL 7. SEND AFIS MESSAGE 8. DISPL AFIS MSG 9. OPERATING MODES Figure 4-256 2. Position Cursor over option, SEND AFIS MSG, and press ENTER. MESSAGE page is displayed. See Figure 4-257. Figure 4-257 3. Position Cursor over the # field and insert the word TEST. 4. Press ENTER until cursor is over SEND MESSAGE? field. 5. Press ENTER to send the TEST message.
Global AIRBORNE FLIGHT INFORMATION SYSTEM For Aircraft equipped with the Antenna Switching Unit, if DATA LINK DISABLED message appears, enable the AFIS air to ground data link. GNS-500A SYSTEM MESSAGE PAGE Figure 4-258 GNS-1000 OR GNS-X SYSTEM MESSAGE PAGE Figure 4-259 7. Press DATA key on the GNS-500A or Plan key or AFIS key on the GNS-1000 or GNS-X until the AFIS MENU page appears. 8. Position Cursor over option, DISPL AFIS MSG (see Figures 4-260 through 4-262) and press ENTER.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-261 AFIS MENU 1. 2. 3. 4. 5. 6. 7. 8. 9. WX GRAPHICS TERMINAL WX SIGMETS WINDS ALOFT AFIS FLT PLAN RECALL AFIS FPL SEND AFIS MESSAGE DISPL AFIS MSG OPERATING MODES Figure 4-262 Figure 4-263 J. SEND MESSAGE Test Procedure for AFIS Users EQUIPPED with Satellite Data Communication System (System Functional Test). 1.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-264 Figure 4-265 AFIS MENU 1. 2. 3. 4. 5. 6. 7. 8. 9. WX GRAPHICS TERMINAL WX SIGMETS WINDS ALOFT AFIS FLT PLAN RECALL AFIS FPL SEND AFIS MESSAGE DISPL AFIS MSG OPERATING MODES Figure 4-266 (b) Position Cursor over option, OPERATING MODES, and press ENTER. OPERATING MODES page is displayed. See Figure 4-267.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (c) Verify VHF NETWORK is ON and SAT NETWORK is OFF or perform the following: To turn VHF NETWORK on, position cursor over OFF option of VHF network field, press BACK key and then press ENTER key to turn on. Figure 4-268, VHF LINK CONTROL page appears. Depress ENTER until cursor is off the page and OPERATING MODES page is displayed. To turn SAT NETWORK off, position cursor over ON option of SAT network field, press BACK key and then press ENTER key to turn off.
Global AIRBORNE FLIGHT INFORMATION SYSTEM If ARINC/ACARS or SITA Aircomm, or ground station is not within receiving range, the message NO COMM is displayed on the message page For Aircraft equipped with the Antenna Switching Unit, if DATA LINK DISABLED message appears, enable the AFIS air to ground data link.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-272 Figure 4-273 AFIS MENU 1. 2. 3. 4. 5. 6. 7. 8. 9. WX GRAPHICS TERMINAL WX SIGMETS WINDS ALOFT AFIS FLT PLAN RECALL AFIS FPL SEND AFIS MESSAGE DISPL AFIS MSG OPERATING MODES Figure 4-274 Figure 4-275 2.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (a) Press the DATA key on the GNS-500A or the PLAN key or AFIS key on the GNS-1000 or GNS-X, XL, XES or XLS until the AFIS MENU page appears. See Figures 4-276 through 4-278. Figure 4-276 Figure 4-277 AFIS MENU 1. WX GRAPHICS 2. TERMINAL WX 3. SIGMETS 4. WINDS ALOFT 5. AFIS FLT PLAN 6. RECALL AFIS FPL 7. SEND AFIS MESSAGE 8. DISPL AFIS MSG 9. OPERATING MODES Figure 4-278 (b) Position cursor over option, OPERATING MODES, and press ENTER.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-279 NOTE: This page will not appear if the system is configured for ARINC 741 or SATFONE systems. Figure 4-280 (d) Press BACK key to return to AFIS MENU page. (e) Position cursor over option, SEND AFIS MSG, and press ENTER. MESSAGE page is displayed. See Figure 4-281. Figure 4-281 (f) Position cursor over the # field and insert the word TEST. (g) Press ENTER until cursor is over SEND MESSAGE? field. (h) Press ENTER to send the TEST message.
Global AIRBORNE FLIGHT INFORMATION SYSTEM (i) When MSG annunciator blinks, press MSG key. SEE AFIS MSG appears on the System Message Page. See Figure 4-282 or Figure 4-283. NOTE: If unable to communicate through satellite network, the message NO COMM is displayed on the message page. Figure 4-282 Figure 4-283 (j) Press DATA key on the GNS-500A or PLAN key or AFIS key on the GNS-1000 or GNS-X until AFIS MENU page appears.
Global AIRBORNE FLIGHT INFORMATION SYSTEM Figure 4-285 AFIS MENU 1. 2. 3. 4. 5. 6. 7. 8. 9. WX GRAPHICS TERMINAL WX SIGMETS WINDS ALOFT AFIS FLT PLAN RECALL AFIS FPL SEND AFIS MESSAGE DISPL AFIS MSG OPERATING MODES Figure 4-286 Figure 4-287 K. Fuel Flow Test NOTE: Fuel flow is a customer specified AFIS option for GNS-500A users with DMU P/N 42000-02-02, P/N 42000-04-03, P/N 400-045500-0002, P/N 400-045500-0004 or P/N 400-045500-0006.
Global AIRBORNE FLIGHT INFORMATION SYSTEM 2. Press NAV key on GNS-500A until the Flight Plan Progress Page appears. See Figure 4-288. Figure 4-288 3. Compare actual field (A) for Fuel Flow Per Engine with value displays on panel indicators. The Fuel Flow Per Engine is an average value and will display a reasonable comparison to aircraft fuel flow indicators. 4. If Actual field is blank or value is unreasonable, check configuration module for proper programming. 5. Correct if necessary and repeat test.
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Global AIRBORNE FLIGHT INFORMATION SYSTEM IMAFISJWA EA-13 March/2001
Global AIRBORNE FLIGHT INFORMATION SYSTEM IMAFISJWA EA-14 March/2001
Global AIRBORNE FLIGHT INFORMATION SYSTEM TSO’D UNITS WITHOUT INDIVIDUAL ENVIRONMENTAL QUALIFICATION FORMS Part Number Unit Description 44000-1 ASU C109 E1E1 A MNO E1 XXXXX AAAAA 42000-01-01 AFIS DMU C37c, C38c, C109c E1E1 A MNO E1 XXXXX AAAAA 42000-02-02 AFIS DMU C37c, C38c, C109c E1E1 A MNO E1 XXXXX AAAAA IMAFISJWA TSO Categories DO-160B Environmental Categories EA-15 March/2001
Global AIRBORNE FLIGHT INFORMATION SYSTEM THIS PAGE IS RESERVED IMAFISJWA EA-16 March/2001
