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Diamond Aircraft DA 42 NG Service Information
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Diamond Aircraft DA 42 NG Service Information

Diamond Aircraft DA 42 NG Service Information

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SERVICE INFORMATION NO. SI-42NG-007
NOTE: SI s are used only:
1) To distribute information from DAI to our customers.
2) To distribute applicable information/documents from our suppliers to our customers with
additional information.
Typically there is no revision service for SI s. Each new information or change of that will be sent
along with a new SI.
1.1 Airplanes affected:
All DA 42 NG and DA 42 M-NG aircraft with G1000 system software versions prior
to 0670.03 are affected.
1.2 Subject:
GARMIN Software Service Bulletin No. 0945, Revision A
ATA-Code: 34-00
1.3 Reason:
The Software Service Bulletin No. 0945, Revision A provides instructions for the GARMIN
G1000 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 further additions or restrictions.
The GARMIN Software Service Bulletin No. 0945, Revision A is attached to this SI.
In case of doubt contact Diamond Aircraft Industries GmbH.
Diamond Aircraft Industries
G.m.b.H.
N.A. Otto-Straße 5
A-2700 Wiener Neustadt
Austria
I. TECHNICAL DETAILS
II. OTHERS
DAI SI 42NG-007
Page 1 of 1
4-Nov-2009
FT

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Summary of Contents for Diamond Aircraft DA 42 NG

  • Page 1 SI. I. TECHNICAL DETAILS 1.1 Airplanes affected: All DA 42 NG and DA 42 M-NG aircraft with G1000 system software versions prior to 0670.03 are affected. 1.2 Subject: GARMIN Software Service Bulletin No. 0945, Revision A ATA-Code: 34-00 1.3 Reason:...
  • Page 2 SOFTWARE SERVICE BULLETIN NO.: 0945, Revision A Diamond Aircraft, Inc. DATE: 2 November 2009 SUBJECT: G1000 System Software Version 0670.03 Update for G1000-equipped Diamond DA42NG Aircraft PURPOSE This service bulletin announces the availability of G1000 System Software Version 0670.03 for Diamond DA42NG aircraft.
  • Page 3 APPROVAL The engineering data contained in this software service bulletin are FAA approved. This bulletin does not provide installation authorization. For approved configurations refer to the Diamond Aircraft MSB 42NG-003, latest version. AFMS AND PILOT’S GUIDE CONSIDERATIONS Flight Manual documentation as required per Diamond Aircraft.

  • Page 4: Warranty Information

    MANPOWER This Software Service Bulletin requires a maximum of two and a half (2.5) hours labor including testing and return-to-service. WARRANTY INFORMATION This 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 ensure proper reimbursement: •...

  • Page 5: Modification Instructions

    MODIFICATION INSTRUCTIONS 1. INTRODUCTION 1.1. Scope These instructions present field upgrade procedures for G1000-equipped Diamond Model DA42NG aircraft. These instructions must be followed step-by-step in order and completely, to upgrade an existing approved configuration of the system software to a newer approved configuration. It is assumed that the person performing the upgrade is familiar with the aircraft and has a working knowledge of typical avionics systems.
  • Page 6 3. This ‘System’ number is the System Software Version. It correlates to the G1000 SW Loader Card used to load the software to the system. For example: EXAMPLE: 0670.03 0670-03 System Software Version ‘ ’ = Loader Card P/N 010-0 If the System Software Version is already at 0670.03, this Software Service Bulletin may have already been performed, proceed to the Testing Procedure section of this bulletin.
  • Page 7 2. G1000 Software Upgrade Procedure NOTE All G1000 screen shots used in this document are intended to provide visual reference only. All information depicted in screen shots, including software file names, versions and part numbers, is subject to change and may not be up to date.
  • Page 8 15. When the words appear in the upper left corner 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.
  • Page 9 19. New software is loaded to the PFD. 20. While in configuration mode write down the following configuration settings: Transponder Configuration (GTX Configuration page) VFR Code: __________ Address Type:__________ Flight ID Type:__________ Audio Panel Configuration (GMA Configuration page) Marker Beacon HI SENSE THRESHOLD:__________ Marker Beacon LO SENSE THRESHOLD:__________ Disable DME:__________ Disable ADF:__________...
  • Page 10 2.2. Initial G1000 Software and Configuration Upload 1. Using the PFD, go to the SYSTEM UPLOAD page using the FMS knob. 2. Activate the cursor and highlight the AIRFRAME field. 3. Using the FMS knob select DA42NG. 4. Press the ENT key. 5.
  • Page 11 6. Once the correct file has been selected, press the ENT key. 7. Press the LOAD softkey to begin the software and configuration loading process. Software Service Bulletin 0945 Page 10 of 27 November 2, 2009 Revision A...
  • Page 12 8. Monitor the status of the upload process. 9. Once all files have been successfully loaded, press the ENT key to acknowledge the Upload Complete prompt. Software Service Bulletin 0945 Page 11 of 27 November 2, 2009 Revision A...
  • Page 13 If the DA42NG is not equipped with any of the following options, proceed to Section 3 of this bulletin. For approved configurations refer to the Diamond Aircraft MSB 42NG-003, latest revision. • DA42NG Option – Weather Radar (NO GDL69) •...
  • Page 14 10. Re-enter the configuration settings as noted in Section 2.1 Step 20 of this bulletin. 11. Refer to the DA 42 NG Airplane Maintenance Manual Section 31-40-00 for instructions on manually setting other configuration settings. 12. Proceed to Section 3 of this bulletin.

  • Page 15: Testing Procedure

    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.
  • Page 16 DA42NG G1000 System Software Version 0670.03 (WAAS-Equipped) SOFTWARE SOFTWARE PART NUMBER VERSION GDC1 006-B0261-12 3.02 GDC1 FPGA 006-C0055-00 1.05 GEA1 006-B0193-05 2.07 GFC CERT (GIA1, GIA2, P C, P M, PT C, 006-D0744-03 2.00 PT M, R C, R M, Y C, Y M) GIA1 006-B0544-2B 5.65...
  • Page 17 DA42NG G1000 System Software Version 0670.03 (Non-WAAS) SOFTWARE SOFTWARE PART NUMBER VERSION GDC1 006-B0261-12 3.02 GDC1 FPGA 006-C0055-00 1.05 GEA1 006-B0193-05 2.07 GFC CERT (GIA1, GIA2, P C, P M, PT C, 006-D0744-03 2.00 PT M, R C, R M, Y C, Y M) GIA1 006-B0190-48 5.65...
  • Page 18 3. De-activate the cursor. NOTE If any software version and/or part number does not match those specified by the table in the Additional Information section of this document, or if the software is not successfully loaded, DO NOT continue with post- installation procedures.
  • Page 19 6. This ‘System’ number is the System Software Version. It correlates to the G1000 SW Loader Card used to load the software to the system: EXAMPLE: 0670.03 0670-03 System Software Version ‘ ’ = Loader Card P/N 010-0 7. Verify that the System Software Version is correct. 8.
  • Page 20 17. The GIA 63 units should normally acquire 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 the display allow the user to toggle between GPS 1 and GPS 2.
  • Page 21 3.3. ADF Checkout (if applicable) This check verifies that the ADF-to-G1000 interface operates correctly. This check is required for DA42NG aircraft with the remote-mount Becker RA3502 ADF installed. 1. On the PFD, check to see if the ADF window(s) is displayed. If not, press the PFD softkey.
  • Page 22 3.6. Stormscope Configuration Verification (if applicable) ® This check verifies that the L-3 Communications Stormscope interface operates correctly. This check is required for DA42NG aircraft with the Stormscope installed. 1. Using the small FMS knob, verify the Map – Stormscope page can be displayed on the MFD.
  • Page 23 3.8. GFC Autopilot Ground Checks (if applicable) The following procedure will verify the proper operation of the GFC 700 AFCS. The technician performing these checks must be thoroughly familiar with the GFC 700 by studying the G1000 Cockpit Reference Guide for the DA42NG. 3.8.1.
  • Page 24 3. Upon successful completion of the pre-flight test, an aural alert will sound and the ‘PFT’ annunciation will clear. Continue to Step 3.8.2. NOTE If the ‘PFT’ annunciation turns red, the test has failed and additional troubleshooting will have to be performed prior to continuing with the test.
  • Page 25 11. Engage the Autopilot. 12. Pull the AUTOPILOT circuit breaker. The Autopilot should command an abnormal disconnect, consisting of a continuous disconnect tone and flashing red ‘AP’. No AFCS annunciations (e.g. AFCS, PFT, Mistrim) should remain on the PFD. 13. Press the AP key on the MFD to silence the autopilot abnormal disconnect tone and then reset the AUTOPILOT breaker.
  • Page 26 10. Hold the control stick and press the CWS button, re-synchronizing the pitch reference and re-centering the control stick. 11. Release the CWS button and verify that servo clutches re-engage before releasing the control stick. 12. Press the NOSE DN key on the MFD twice. Verify that the command bars command down and the control stick begins moving forward.
  • Page 27 3.9. Deicing System Verification (if applicable) This check verifies that the Deicing system interfaces operate correctly. This check is required for DA42NG aircraft with the Deicing option installed. 1. For aircraft with the Deicing system installed, verify that the lower left corner of the System Display on the PFD displays ”DEICE FLUID”.

  • Page 28: Material Information

    MATERIAL INFORMATION G1000, DA42NG Software To accomplish this update, the technician must have a G1000, DA42NG Loader Card, Garmin P/N 010-00670-03. Part Number Description G1000 Software Loader Card (Diamond 010-00670-03 DA42NG) ADDITIONAL INFORMATION Software Service Bulletin 0945 Page 27 of 27 November 2, 2009 Revision A...

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