Garmin G1000 System Maintenance Manual

G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 7-51
190-00716-01 Revision 4
12. On the GCU, press the inner FMS knob to activate the cursor then rotate the outer FMS knob to
select the Stability & Protection window on the MFD.
13. Rotate the inner FMS knob to change the status to “DISABLED”.
14. Verify that on the MFD SETUP 2 page Stability & Protection window that the status is
“DISABLED”.
15. Verify on PFD 1 and PFD 2 the ESP Roll Indices are not displayed at 45° on the roll indicator on
the Attitude Display.
16. Verify on PFD 1 and PFD 2 that there is an “ESP OFF” alert message.
17. Remove the cover from both GPS1 and GPS2 antennas.
18. Remove power to the aircraft and avionics systems by placing the aircraft AVIONICS MASTER
PWR and EXP PWR switches to OFF.
19. Wait ~ 1 minute before re-applying aircraft power.
20. Apply power to the aircraft and avionics systems by setting the BAT, EXT PWR and AVIONICS
MASTER PWR switches to ON.
21. During power up and GPS satellite acquisition, verify on PFD1 and PFD2 the ESP Roll Indices
are displayed at 45° on the roll indicator on the Attitude Display.

Garmin G1000 Specifications

General

Display Type	LCD
Primary Flight Display (PFD)	Yes
Multi-Function Display (MFD)	Yes
Terrain Awareness	Yes
Autopilot Integration	Yes
Integrated Flight Deck System	Yes
Weather Radar	Optional
Traffic Advisory System (TAS)	Optional
Terrain Awareness and Warning System (TAWS)	Yes
Resolution	1024 x 768 pixels
Weather Data	Yes
Navigation	Yes
AHRS	Yes
Air Data Computer (ADC)	Yes
Interfaces	ARINC 429, RS-232
Certification	TSO certified
Traffic Information	Optional (requires ADS-B or TCAS)