Self test and initialisation – BendixKing SKYMAP IIIC User Manual

Page 45

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DETAILED OPERATION

Self Test and Initialisation

When the Title Screen is initially displayed, the unit carries out a series of internal check

routines automatically. These are:

1. Verification that the unit has been factory initialised. This consists of a check to see if

there is a special code in NVM. If there is no initialisation code in the NVM a
message saying UNIT NOT INITIALISED will be printed across the centre of the

Screen and the unit will be totally disabled. This is a security feature, safeguarding
against theft of the unit and attempted erasure of your PIN from the NVM. (If your

unit is stolen and the NVM is erased or replaced in an attempt to reset the PIN, the

thief will still not be able to use or sell the unit because these special high security
factory initialisation codes will be missing.)

2. A check for RAM corruption. If RAM has been lost or corrupted due to a severe

‘glitch’ or loss of power in the memory battery a RAM clear will be performed on the
affected areas and Screen 51, Ram Lost Warning Screen, will be displayed (Refer to

APPENDIX B ).

3. A check of the internal Lithium battery voltage. If the internal battery voltage is low,

Screen 52, Internal Battery Warning Screen, will be displayed (Refer to APPENDIX B

).

4. A check to see whether the Automatic Power-On Lock function has been enabled

(see Screen 26 for further details). If it is enabled, Screen 54, Power On Security

PIN Entry Screen, will be displayed after 5 seconds (or if any Key is pressed before
this). If when switched on it is found that three unsuccessful attempts have been

made to enter the Unlock PIN, Screen 55, Lockout Screen, will be displayed (Refer to
APPENDIX B ).

DETAILE

D

OPE

RATION

5. A check to see if a new memory card has been fitted. This involves comparing the

software version number held in NVM with that of the current memory Card. If a
change of card is detected, the integrity of all flight plans will be checked and if any

discrepancies are found Screen 56, Flight Plan Change Warning Screen, will be

displayed (Refer to APPENDIX B ).

6. If the unit is a Skymap IIIC the GPS receiver circuitry will be tested and if any

problems are found, a NO REPLY message will be indicated in the STATUS field of

Screen 3, GPS Status Screen.

If the unit passes all checks 1 to 6 above no warnings will be given

Rev 9 Jul 2006

3-2

Skymap/Tracker IIIC Pilot's Guide

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