Engine Start; Figure 5-2. G1000 Engine/Airframe Indicators - Garmin G1000 Checkout Procedure

d) After several seconds, a new checklist appears in the lower half of PFD1. Press the ENT key
as each item is confirmed. When the CONFIRM AIRCRAFT IS LEVEL field is blinking, press
the ENT key to continue.
4. The result of the pitch/roll offset compensation is displayed on PFD1. If successful, the AHRS
records the required pitch and roll offsets, informs the operator of a successful conclusion and
returns to normal operation.
5. Press the ENT key on PFD1 to conclude this procedure. Repeat Steps 3 - 4 for the GRS2.
6. Restart displays in normal mode and proceed to Section 5.2.
5.2

Engine Start

To carry out the remaining GRS/GMU procedures, the aircraft engines must be started in accordance with
Hawker / Beech C90 engine starting and operating procedures.
Prior to engine start, verify all engine/airframe sensor operation by compliance with G1000 / GFC 700
Power On and Functional Checkout for Raytheon / King Air C90B 190-00682-04. Perform remaining
GRS/GMU calibrations listed in Section 5.3.
Page 5-2 G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5

Figure 5-2. G1000 Engine/Airframe Indicators

190-00682-00