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Sandel SN4500 Maintenace Manual

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COMPONENT MAINTENANACE MANUAL
FOR
SANDEL SN4500 Primary Navigation Display
Document No. 82009-0133
Revision C, July 14, 2008
SANDEL AVIONICS, INC.
2401 Dogwood Way
Vista, CA 92081
Telephone: (760) 727-4900
Facsimile: (760) 727-4899
www.sandel.com
PROPRIETARY DATA
SANDEL AVIONICS proprietary rights are included in the information disclosed herein. Recipient by
accepting this document agrees that neither this document nor the information disclosed herein nor any
part thereof shall be reproduced or transferred to other documents or used or disclosed to others for
manufacturing or for any other purpose except as specifically authorized in writing by SANDEL
AVIONICS.

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Summary of Contents for Sandel SN4500

  • Page 1 SANDEL AVIONICS.
  • Page 2 Added software release via Service Bulletins Nov 29, 2006 A/R 867; Initial Release 82009-0133-C SN4500 CMM Sandel Avionics Proprietary Page 2 of 6 Use or disclosure of data on this page is subject to the proprietary notice on page 1 of this document.
  • Page 3 System software is released via a Service Information Letter (SIL) or via a Service Bulletin (SB) posted on the Sandel website. The SIL or SB contains links to the software and the related software installation files necessary to load the software. Database updates are available for purchase via the Sandel website.
  • Page 4 1. Carefully lift bezel from unit while disengaging bezel buttons and rubber keypad from bezel. Do not remove or shift keypad, keypad circuit board, or Fresnel lens. 2. Remove existing window from unit. 82009-0133-C SN4500 CMM Sandel Avionics Proprietary Page 4 of 6...
  • Page 5 Step 5. Reinstall bezel: 1. Carefully reinstall bezel onto unit actuator housing. Ensure that the machined lip in window engages bezel opening and that bezel fully seats. 82009-0133-C SN4500 CMM Sandel Avionics Proprietary Page 5 of 6 Use or disclosure of data on this page is subject to the proprietary notice on page 1 of this document.
  • Page 6 1. Ensure that all affected components are installed. 2. Ensure that bezel retaining screws are securely installed. 3. Ensure that all bezel buttons operate freely, without binding. 82009-0133-C SN4500 CMM Sandel Avionics Proprietary Page 6 of 6 Use or disclosure of data on this page is subject to the proprietary notice on page 1 of this document.

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