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Software Service Bulletin 0945

Page 14 of 27

November 2, 2009

Revision A

3. TESTING PROCEDURE

3.1.

Software Load Confirmation

1. Using the PFD, go to the System Status page using the small FMS knob.

Activate the cursor and toggle to the LRU window.

2. In the LRU window, highlight each of the items listed in the following table and

verify that the software part number and version displayed on the System Status
page matches those listed in the table.

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13
14
15
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17
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Содержание DA 42 M-NG

Страница 1: ...00 System Software upgrade to Version v0670 03 1 4 Information For detailed technical information refer to the GARMIN Software Service Bulletin No 0945 Revision A which is applicable without any furth...

Страница 2: ...ent or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this document or any revision hereto is strictly prohibite...

Страница 3: ...for the Diamond DA42NG 190 00962 00 G1000 Pilot s Guide for the Diamond DA42NG PRODUCT AFFECTED All G1000 equipped Diamond DA42NG aircraft with G1000 system software versions prior to 0670 03 are aff...

Страница 4: ...s modification is only warranty reimbursable for Diamond DA42NG aircraft with system software version 0670 02 When completing the Garmin warranty claim be sure to include the following information to...

Страница 5: ...roved configuration It is assumed that the person performing the upgrade is familiar with the aircraft and has a working knowledge of typical avionics systems NOTE Instructions contained in this docum...

Страница 6: ...ed to the Testing Procedure section of this bulletin 1 2 Required Materials and Equipment NOTE Make sure that all of the required materials and equipment are on hand before you begin the upgrade proce...

Страница 7: ...is moment all G1000 equipment is receiving power 5 Disengage the MFD and PFD circuit breakers 6 Insert the correct G1000 Loader Card into the MFD top card slot located on the MFD 7 While holding the E...

Страница 8: ...rner of the PFD release the ENT key 16 Press the ENT key to acknowledge the following prompt NOTE A softkey labeled YES appears in the lower right corner and may be used in lieu of the ENT key 17 If a...

Страница 9: ...___ Audio Panel Configuration GMA Configuration page Marker Beacon HI SENSE THRESHOLD __________ Marker Beacon LO SENSE THRESHOLD __________ Disable DME __________ Disable ADF __________ 21 When PFD u...

Страница 10: ...ob 2 Activate the cursor and highlight the AIRFRAME field 3 Using the FMS knob select DA42NG 4 Press the ENT key 5 Using the FMS knob select Diamond DA42NG WAAS or Diamond DA42NG in the FILE field dep...

Страница 11: ...re Service Bulletin 0945 Page 10 of 27 November 2 2009 Revision A 6 Once the correct file has been selected press the ENT key 7 Press the LOAD softkey to begin the software and configuration loading p...

Страница 12: ...rvice Bulletin 0945 Page 11 of 27 November 2 2009 Revision A 8 Monitor the status of the upload process 9 Once all files have been successfully loaded press the ENT key to acknowledge the Upload Compl...

Страница 13: ...urations refer to the Diamond Aircraft MSB 42NG 003 latest revision DA42NG Option Weather Radar NO GDL69 DA42NG Option Weather Radar DA42NG Option Stormscope DA42NG Option TAS600 Series Installation D...

Страница 14: ...ess the ENT key to acknowledge the Upload Complete prompt 8 View the SUMMARY field and ensure that all items are COMPLETED 9 Repeat steps 5 through 8 to load any other equipped options 10 Re enter the...

Страница 15: ...n 1 Using the PFD go to the System Status page using the small FMS knob Activate the cursor and toggle to the LRU window 2 In the LRU window highlight each of the items listed in the following table a...

Страница 16: ...03 2 00 GIA1 006 B0544 2B 5 65 GIA1 AUDIO 006 D0425 05 2 05 GIA2 006 B0544 2B 5 65 GIA2 AUDIO 006 D0425 05 2 05 GMA1 006 B0203 41 4 01 GMU1 006 B0224 00 2 01 GMU1 FPGA 006 C0048 00 2 00 GPS1 006 B033...

Страница 17: ...GMU1 FPGA 006 C0048 00 2 00 GPS1 006 B0093 XX 3 03 GPS2 006 B0093 XX 3 03 GRS1 006 B0223 09 2 11 GRS1 FPGA 006 C0049 00 02 00 GSA PITCH CTL PITCH MON PITCH TRM C PITCH TRIM M ROLL CTL ROLL MON YAW CTL...

Страница 18: ...with post installation procedures Troubleshoot and resolve the issue refer to the G1000 System Maintenance Manual P N 190 00907 00 before continuing 4 Turn off system power 3 2 Software Operational Te...

Страница 19: ...e heading airspeed altitude vertical speed and OAT fields to be invalid during the first 40 60 seconds of PFD power up 10 Verify that no Manifest errors appear when the ALERTS softkey is pressed 11 Ch...

Страница 20: ...a 3D GPS navigation solution within 5 to 10 minutes of startup provided the aircraft is outside or indoors with a GPS repeater Select the AUX GPS STATUS Page on the MFD Two softkeys on the bottom of t...

Страница 21: ...verifies that the DME to G1000 interface operates correctly This check is required for DA42NG aircraft with the Honeywell remote mounted KN63 DME installed 1 On the PFD check to see if the DME window...

Страница 22: ...ormscope installed 1 Using the small FMS knob verify the Map Stormscope page can be displayed on the MFD 3 7 TAS System Verification KTA870 TAS or TAS600 if applicable This check verifies that the KTA...

Страница 23: ...eference Guide for the DA42NG 3 8 1 Autopilot Pre Flight Test NOTE The autopilot pre flight test will run on every full airplane power on 1 Open the AUTOPILOT circuit breaker and reset The AFCS will r...

Страница 24: ...ISC button on the pilot s control stick and hold The pitch trim should stop running and the pitch trim indication should stop moving The pitch trim will not run for as long as the A P DISC button is p...

Страница 25: ...r the pitch axis 20 Disengage the Autopilot by pressing the A P DISC switch 3 8 3 Autopilot Operation Checks 1 Push the HDG knob in to synchronize the heading bug to the present aircraft heading on th...

Страница 26: ...stick and press the CWS button Trim motion should stop 17 Move the control stick to the forward limit and release the CWS button 18 Slowly pull back on the control stick After a similar delay the trim...

Страница 27: ...appropriate entry in the aircraft s maintenance records noting that the instructions in this Software Service Bulletin have been performed Record the G1000 DA42NG Loader Card part number in the maint...

Страница 28: ...ision A MATERIAL INFORMATION G1000 DA42NG Software To accomplish this update the technician must have a G1000 DA42NG Loader Card Garmin P N 010 00670 03 QTY Part Number Description 1 010 00670 03 G100...

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