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G1000 System Maintenance Manual - Hawker Beechcraft G36 Page 8-1

190-01259-00 Rev. 5

8 SYSTEM RETURN TO SERVICE PROCEDURE

The procedures contained in this section describe the minimum return to service checks that

should be performed upon reinstallation of the software and/or reactivation of SVS/Pathways. If

the software reload or SVS reactivation was as a result of an LRU replacement, the technician

must also perform any additional return to service tests required by the existing Hawker

Beechcraft G36 Airplane Maintenance Manual (listed in Table 1.1) for that LRU.

8.1 Display Testing

The G1000 system is tested while operating in the normal mode unless otherwise specified. If

the system is in configuration mode, restart the displays by cycling the PFD and MFD circuit

breakers to start the display in the normal mode.

a. Apply aircraft power. Observe the MFD power-up screen. Verify the display is formatted as

shown below. Figure 8.1 is a format reference, the illustration on the left may vary. Note

database versions and system software represented in the upper right corner. Refer to

General Arrangement Drawing 005-00620-06 drawing for the correct database and system

software versions.

Figure 8.1 – MFD Initial Power Up page (format reference)

b. The System number reflected in the upper right hand corner is the System Software

Version. It correlates to the G1000 SW Loader Card used to load the software to the

system.

c. Verify that the System Software Version is correct per General Arrangement Drawing 005-

00620-06.

d. Press the ENT key to acknowledge the correct pilot profile on the MFD.

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Garmin Software Version 0858.09 Bedienerhandbuch Seite 67