Honeywell MCX-1000A Users Manual

Global

AIRBORNE FLIGHT INFORMATION SYSTEM

MANUFACTURER MODEL GLOBAL TYPE

DASSAULT (cont) MYSTERE FALCON 900 B DA90B

MYSTERE FALCON 900 HEAVY DA90H

MYSTERE FALCON 900B HEAVY DA90BH

MYSTERE FALCON 900 EX DA90EX

BEECHCRAFT 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.) BE400H

BOEING 727-100 (JT8D-7 ENGINES) B727D7

BRITISH AEROSPACE BAE 146-100 BA461

BAE 146-200 BA46

BAE 146-300 BA463

BAE HS126-600A HS600A

BAE HS126-700A HS700A

BAE HS126-700B HS700B

BAE HS126-800A HS800A

BAE HS126-800B HS800B

BAE1000 BA1000

JETSTREAM 3100 BA31

JETSTREAM 3200 BA32

CANADAIR CHALLENGER 600 CL600

CHALLENGER 600W (WINGLETS) CL600W

CHALLENGER 601 CL601

CHALLENGER 601-3A CL61

CHALLENGER 601-3A (45,250 RAMP WT.) CL61H

CESSNA CITATION I 500 CE500

CITATION I 501 CE501

CITATION II 550 CE550

CITATION II 550 (New Cruise mode) CE550A

CITATION II 550 (Increased Max WT) CE550H

CITATION II 550 (New Cruise mode Increased Max WT)

CITATION II S550 S550

CITATION II S550H S550H

DESIGNATOR

CE550I

TABLE 4-1 (Sheet 2 of 3)

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MANUFACTURER MODEL GLOBAL TYPE

CESSNA (cont) CITATION III 650 CE650

CITATION III 650A (SB 13 & 14) CE650A

CITATION III 650 HEAVY CE650H

CITATION III 650 HEAVY (Increased ZFW) CE650Z

CITATION V 560 CE560

CITATION VII 650 CE657

CITATION XL CE560X

CITATION X CE 750

DORNIER 228-201 D2281

228-202 D2282

EMBRAER 120 PW118 E120

120A PW118A E120A

120A PW118A EMB120

GULFSTREAM GULFSTREAM 1 G1

GULFSTREAM II WITH HUSH KIT GUII

GULFSTREAM II WITH TIP TANKS G2TT

GULFSTREAM III GUIII

GIII ASC70 GIII70

GULFSTREAM IV G4

GULFSTREAM IV W/MACH.85 &.86 G4A

ISRAEL AIRCRAFT WESTWIND 1124 W1124

INDUSTRIES WESTWIND 1124A W1124A

WESTWIND 1124 W/AFC 1076 W1124I

WESTWIND 1124 ASTRA W1125

ASTRA JET AJ25

ASTRA JET (INCREASED MAX WT) AJ25H

LEAR LEARJET 31 LE31

LEARJET 31A LE31A

LEARJET 31A INCREASED ZFW-13,000 LE31AZ

LEARJET 35A LE35

LEARJET 36A LE36

LEARJET 55 ECR 2431 LE55

LEARJET 55 ECR 2554 LE55A

DESIGNATOR

LEAR (cont) LEARJET 55C LE55C LOCKHEED JETSTAR GARRET 731 JET731 MITSUBISHI MU300 DIAMOND 1 DIAM1 SABRELINER SABRELINER 60 SABR60

SABRELINER 65 SABR65 SABRELINER 80 SABR80

TABLE 4-1 (Sheet 3 of 3)

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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. Use the UP or DOWN Arrow Key to position the cursor over the DATE field and enter 357777. Press the ENTER Key. See Figure 4-2.

Figure 4-2

5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu

Page (Figure 4-3) and press the ENTER Key.

-------

Figure 4-3

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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. Insert 15 as the Auto Reporting time interval unless advised differently by the

pilot/operator and press ENTER. See Figure 4-6.

Figure 4-6

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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.

NOTE:

Currently, GS is the only valid entry and may change at a future time.

Figure 4-9

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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. Complete this step for all other versions. Insert 2 as shown in Figure 4-12 to indicate

that Port 1 is connected to the GNS-500A system and press ENTER.

NOTE:

GNS-X applies also to GNS-X

ES, GNS-XL

and GNS-XLS.

Figure 4-12

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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-X

Figure 4-13A

ES, GNS-XL

and GNS-XLS.

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.

Figure 4-14

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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

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. 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 4-16.

Figure 4-16

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 or 42000-04-03 is installed. If applicable, insert 3 and press ENTER. See Figure 4-17.

Figure 4-17

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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.

Figure 4-19

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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. If applicable, select the number that corresponds to the number of engines on the aircraft and press the ENTER Key. See Figure 4-21.

Figure 4-21

24. Fuel Flow Interface - Enter one of seven options. See Figure 4-22.

Using the Up and Down arrow keys, move the fuel flow sensor options into the stationary cursor field. Scroll through and press the ENTER Key to select the desired option.

Figure 4-22 (page 1)

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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. fuel flow manufacturer and AERO is AERO Systems.

Figure 4-23 (PAGE 1)

Figure 4-23 (PAGE 2)

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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.

Figure 4-24 (PAGE 1)

Figure 4-24 (PAGE 2)

(d) If Option 4 (PULSE DIFF) is selected, Figure 4-25 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.

Figure 4-25

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(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. CAN is Canadian Marconi, CON is Consolidated Airborne and RAG is Ragen Data System

Figure 4-26 (PAGE 1)

Figure 4-26 (PAGE 2)

Figure 4-26 (PAGE 3)

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(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. 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.

Figure 4-28

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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. Select whether stored weather will be retained in memory when power is interrupted.

Press the ENTER Key to continue. See Figure 4-30.

Figure 4-30

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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.

If applicable, select Satcom Option 2 and press the ENTER Key. See Figure 4-32.

If Option 1 is selected, proceed to Step 30. Option 3 (ARINC 741) and Option 4 (SATFONE) are not available for DMU P/N 42000-03-03 and 42000-04-03. These options apply to other FMS/DMU configurations discussed elsewhere.

Figure 4-32

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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. Write configuration data to the Configuration Module by selecting 2 and press the

ENTER Key. See Figure 4-34.

Figure 4-34

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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. 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. Use the UP or DOWN Arrow Key to position the cursor over the DATE field and enter 357777. Press the ENTER Key. See Figure 4-36.

Figure 4-36

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5. Select the AFIS configuration to be read or modified from the AFIS Configuration Menu

Page (Figure 4-37) and press the ENTER Key.

Figure 4-37

6. Insert the basic operating weight and press ENTER. See Figure 4-38.

Figure 4-38

7. Insert the default for Auto Report and press ENTER. See Figure 4-39.

Figure 4-39

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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.

Figure 4-42

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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. Insert 2 as shown in Figure 4-45 to indicate that Port 1 is connected to the GNS-500A

system and press ENTER.

NOTE:

GNS-X applies also to GNS-X

GNS-XL and GNS-XLS.

ES,

Figure 4-45

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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-X

GNS-XL and GNS-XLS.

ES,

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.

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). Honeywell recommends use of Port 1.

Figure 4-48

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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. 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 4-51.

Figure 4-51

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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.

Figure 4-53

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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. If applicable, select the number that corresponds to the number of engines on the aircraft and press the ENTER Key. See Figure 4-55.

Figure 4-55

24. Fuel Flow Interface - Enter one of seven options. See Figure 4-56.

Using the Up and Down arrow keys, move the fuel flow sensor options into the stationary cursor field. Scroll through and press the ENTER Key to select the desired option.

Figure 4-56 (PAGE 1)

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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. fuel flow manufacturer and AERO is AERO Systems.

Figure 4-57 (PAGE 1)

Figure 4-57 (PAGE 2)

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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.

Figure 4-58 (PAGE 1)

Figure 4-58 (PAGE 2)

(d) If Option 4 (PULSE DIFF) is selected, Figure 4-59 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.

Figure 4-59

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(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:

Figure 4-60 (PAGE 1)

Figure 4-60 (PAGE 2)

Figure 4-60 (PAGE 3)

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(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. 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.

Figure 4-62

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25. Select the applicable special feature option and press the ENTER Key to continue. See Figure 4-63.

NOTE:

Figure 4-63

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 4-64.

Figure 4-64

27. Select the desired option for Auto Weather update status at power up and press the ENTER Key. See Figure 4-65.

Figure 4-65

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