Garmin G1000 Integrated Avionics System - Beechcraft Baron G58 Pilot Operating Handbook

Model G58

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

1. Upon initial certification, the G1000 system was
equipped with 58/G58 Airframe System Software Ver-
sion 0500.01. The following Airframe System Software
Versions have also been approved for the Model G58:
• 0500.02 that adds autopilot enhancements
• 0857.05 that adds SBAS (WAAS) capability
• 0857.06 that adds SBAS capability for EASA opera-
tional requirements
The airplane must utilize these versions of software, or
later FAA approved versions. Avionics Line Replaceable
Units (LRUs) associated with each version of software are
listed on the following pages.
The following methods may be used to determine the level of
software installed on the airplane.
a. Refer to the MFD upon initial power up. The "Splash
Screen" will display the current system software ver-
sion at the top of the page, (e.g. "Beechcraft 58/G58
System 0857.05").
b. Select the SYSTEM STATUS page of the AUX Group
on the MFD. The current software versions of the
hardware shown in the tables below will be displayed.
c. Refer to the laminated card found at the back of this
manual. This card shows the system software version
and the software associated with each piece of hard-
ware that is currently loaded in the G1000 system.
The loader card is contained in a pouch located next
to the laminated card.
May, 2015
Section 2
Limitations
2-17