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Jun 25/2010

680-34-27

Page 6

Citation

SERVICE BULLETIN

SB680-34-27

K.

Select "CREATE AND LOAD BINARY FILE" on the last page.

NOTE: A window will appear with a folder list. It is asking where to save the file.

(1)

Select a folder that has read-write access permission.

NOTE: Normally this opens to the temporary folder which is acceptable to use.

(2)

Select "OPEN". If the box appears with the question "FILE EXISTS, DO YOU WISH TO
OVERWRITE", select "YES".

L.

A window will show "ENTER DR FILE PART NUMBER". Leave it blank and select "OK".

M.

After a few moments, a window will appear with an indication of success or failure.

(1)

If success is shown for all four APM’s select "OK", then continue with Step 10.

(2)

If failure is shown for any APM, continue with Step 9N.

N.

Make a note of which APM's were successful.

O.

Select "OK".

P.

Close APM tool windows.

Q.

Wait 3 minutes after the software load completes.

CAUTION:

Before turning the airplane power off, wait 3 minutes after the last software load
completes. Software data could be corrupted or erased if this is not done.

10.

Cycle the airplane power.

A.

Turn the airplane power off.

NOTE: It is not necessary to disconnect external power.

B.

Wait a minimum of 3 minutes.

C.

Turn the airplane power on.

11.

Do a check of the system software load.

A.

Make sure the airplane is in ground mode.

B.

Turn on all avionic systems and allow time for initialization.

C.

Make sure the software version is correct.

(1)

Use the copilot's Cursor Control Display (CCD), select the MAP pull-down menu on DU3.

(2)

Select SCMS and examine SCMS page 1 to make sure the software and database identifiers
are correct.

NOTE: The entry under "Configuration part number" should show TT7038647-XXX as

determined in Step 8.

(3)

Press CONFIRM on the SCMS screen after you make sure of the identifier above.

D.

Make sure that the EICAS message "CONFIGURATION MISMATCH” is not displayed on the EICAS.

NOTE: If the “CONFIGURATION MISMATCH" message is present, the software load and/or

hardware configuration is not correct. This must be corrected before you continue.

12.

Do a check of the GPS sensors.

A.

Position the airplane so that it can receive a GPS signal.

B.

Make sure the airplane is in ground mode.

C.

Turn on all avionic systems and allow time for initialization.

D.

Press the NAV Button until the NAV INDEX menu is displayed on MCDU 1.

Содержание Cessna 680 Citation Sovereign

Страница 1: ...and install all applicable parts supplied with the service bulletin kit Only with written authorization from Cessna Aircraft Company can substitute parts or rebuilt parts be used to replace new parts...

Страница 2: ...fillet seal the antennas MATERIAL Cost and Availability The parts listed below are required to do this service bulletin PART NUMBER QUANTITY ORDERING INFORMATION AVAILABILITY COST S67 1575 135 2 S67 1...

Страница 3: ...Model 680 Maintenance Manual Chapter 34 Honeywell Primus Global Position System GPS Module Maintenance Practices NOTE Operators The existing 245 604067 001 modules may be modified to 245 604067 100 co...

Страница 4: ...attach the antennas to the fuselage 2 Carefully cut the sealant that is between the antenna bases and the airplane skin 3 Disconnect the coax connector from the antennas 4 Remove the antennas from th...

Страница 5: ...e 1 800 835 4000 or 1 316 517 6273 Team Sovereign Phone 1 877 683 7344 or 1 316 517 1695 9 Update the APM settings for WAAS using the definition file in MM7031847 012 A Put the flight software CD MM70...

Страница 6: ...he airplane power A Turn the airplane power off NOTE It is not necessary to disconnect external power B Wait a minimum of 3 minutes C Turn the airplane power on 11 Do a check of the system software lo...

Страница 7: ...be shown after a short period of time 5 Make sure the results are shown J Repeat steps D to I for FMS 2 and GPS 2 13 Turn the airplane Power off 14 Disconnect the airplane battery 15 Disconnect extern...

Страница 8: ...ators The existing 245 604067 001 modules may be modified to 245 604067 100 configuration Contact Citation Parts Distribution CPD Avionics team to schedule modification at 1 316 517 1651 or telefax 1...

Страница 9: ...regarding operational changes as a result of accomplishment of this service bulletin Please remove this summary from the service bulletin and give it to the flight crew This summary is informational...

Страница 10: ......

Страница 11: ...HOURS Modification As Required MATERIAL Cost and Availability PART NUMBER AVAILABILITY COST S67 1575 135 245 604067 100 Please contact Citation Parts Distribution for current cost and availability of...

Страница 12: ......

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