Garmin G1000 System Maintenance Manual

G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air Page 4-27
190-00716-01 Revision 4
Figure 4-4, Ambient Temperature Conversion Chart
4.11.2 Torque
1. Remove power from aircraft.
2. Disconnect the left engine firewall connector J102.
3. Connect the Signal Generator to pins C (HI) and R (LO) of J102.
4. Apply external power to aircraft and start the G1000 in normal mode.
5. Using the Signal Generator, inject DC signals specified in Table 4-13 and verify the
indications are within the specified tolerances.
Test Point (VDC) Torque Indication (%)
0.000 +/- .02 0 +/- 2
1.035 +/- .02 45 +/- 2
1.725 +/- .02 75 +/- 2
2.300 +/- .02 100 +/- 2
Table 4-13, Torque Indication Test Points
6. On the right hand circuit breaker panel, open the GIA1 (PRI) and GIA1 (SEC) circuit
breakers, and verify the last observed torque indication remains unchanged. Reset the the
GIA1 (PRI) and GIA1 (SEC) circuit breakers.
7. Repeat steps 1 through 5 using right engine firewall connector J103, pins C (HI) and R (LO).
8. Pull the GIA 2 circuit breaker, and verify the last observed torque indication remains
unchanged. Reset the GIA 2 circuit breaker.
9. Remove power from aircraft and reconnect left and right engine firewall connectors.

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)