Garmin Software Version 0500.00 User's Guide Page 112

  • Download
  • Add to my manuals
  • Print
  • Page
    / 132
  • Table of contents
  • BOOKMARKS
  • Rated. / 5. Based on customer reviews
Page view 111
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
12-4
SECTION 12 – ANNUNCIATIONS
& ALERTS
12.3 AFCS ALERTS
System Status Field
The following AFCS alert annunciations appear in the
AFCS System Status field on the PFD.
WARNING: Red annunciation is time critical and
indicates an abnormal AFCS condition requiring
immediate pilot attention.
CAUTION: Yellow annunciation indicates the
existence of abnormal AFCS conditions that may
require pilot intervention.
Condition Annunciation Description
Pitch Failure
Pitch axis control failure. AP is inoperative.
Roll Failure
Roll axis control failure. AP is inoperative.
MET Switch Stuck, or
Pitch Trim Axis Control
Failure
If annunciated when AP is engaged, take control of the aircraft and disengage the
autopilot. If annunciated when AP is not engaged, move each half of the MET switch
separately to check if a stuck switch is causing the annunciation.
Yaw Damper Failure
Yaw Damper control failure.
System Failure
AP and MET are unavailable. FD may still be available.
Elevator
Mistrim Up A condition has developed causing the pitch servo to provide a sustained force. Be
prepared to apply nose up control wheel force upon autopilot disconnect.
Elevator
Mistrim
Down
A condition has developed causing the pitch servo to provide a sustained force. Be
prepared to apply nose down control wheel force upon autopilot disconnect.
Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left force. Ensure
the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force. En-
sure the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
Rudder Mistrim Left A condition has developed causing the yaw servo to provide a sustained force. Ensure
the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force. Ensure
the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
Preflight Test
Performing preflight system test. Upon completion, the aural alert will be heard.
Preflight system test has failed.
Figure 12-5 AFCS System Status Field
System Status Field
Page view 111
1 2 ... 107 108 109 110 111 112 113 114 115 116 117 ... 131 132

Comments to this Manuals

No comments