Instruction Manual

G1000 / GFC 700 System Maintenance Manual - 200/B200 Series King Air Page 4-31
190-00915-01 Revision 8
25. Hold the elevator in the neutral position, press the HDG and ALT buttons on the mode controller and
center the heading bug.
26. Engage the autopilot and turn the heading knob to set the heading bug to the right of center. Hold the
control yoke centered for approximately 10 seconds. Verify that the amber AIL→ annunciator is
displayed on both PFD 1 and PFD 2.
27. Turn the heading knob to set the heading bug to the left of center. Hold the control yoke centered for
approximately 10 seconds. Verify that the amber ←AIL annunciator is displayed on both PFD 1 and
PFD 2.
28. Disengage the autopilot and clear all modes.
29. Ensure the aircraft is on the ground and the nose wheel is approximately straight.
30. Engage the yaw damper and apply firm load on the right rudder pedal for approximately 20 seconds.
31. Verify that the amber ←RUD annunciator is displayed on both PFD 1 and PFD 2.
32. Apply firm load on the left rudder pedal for approximately 20 seconds.
33. Verify that the amber RUD→ annunciator is displayed on both PFD 1 and PFD 2.
34. Disengage autopilot.
35. The Trim Annunciator Check is complete.
4.13 G1000 Miscompare Checks
This procedure will check the AHRS, airspeed and altitude miscompare monitors. Accomplish the
following checks with the aircraft positioned where it can receive GPS signals and magnetic heading.
Access to AHRS1 and AHRS2 will be required during this test.
1. Ensure the G1000 is operating in normal mode.
2. Connect a pitot/static test set to the aircraft ADC1 pitot and static ports (Pilot’s side). (Do not connect
the pitot/static tester to ADC2 ports at this time.)
3. Set the baro-correction on PFD1 and PFD2 to 29.92.
4. On the AFCS mode controller, press the ALT, HDG, and AP buttons and verify autopilot engages.
5. Slowly increase the pitot/static test set to simulate an ADC1 / ADC2 altitude miscompare of greater
than 200 ft., verify the disconnected ADC altitude does not increase, autopilot does not disconnect
and amber comparator window text “ALT MISCOMP” is displayed on PFD1 and PFD2.
6. Reduce ADC1 altitude to ambient pressure.
7. Repeat Step 5 with the pitot/static test set connected to the aircraft ADC2 pitot and static ports.
8. Use the pitot/static test set to simulate an airspeed of 40 kts for ADC1 and 55 kts for ADC2. Verify
the autopilot does not disconnect and amber comparator window text “IAS MISCOMP” is displayed
on PFD 1 and PFD2.
9. Use the pitot/static test set to simulate an airspeed of 55 kts for ADC1 and 40 kts for ADC2. Verify
the autopilot does not disconnect and amber comparator window text “IAS MISCOMP” is displayed
on PFD 1 and PFD2.
10. Use the pitot/static test set to simulate an airspeed of 85 kts for ADC1 and 95 kts for ADC2. Verify
the autopilot does not disconnect and amber comparator window text “IAS MISCOMP” is displayed
on PFD 1 and PFD2.
11. Use the pitot/static test set to simulate an airspeed of 95 kts for ADC1 and 85 kts for ADC2. Verify
the autopilot does not disconnect and amber comparator window text “IAS MISCOMP” is displayed
on PFD 1 and PFD2.