
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 31 of 65
For ←AIL, AIL→ Indication:
1. Rudder Trim........................................VERIFY slip/skid indicator is centered
NOTE
Observe the maximum fuel imbalance limitation.
If annunciation remains:
2. Control Stick..............................................GRASP FIRMLY with both hands
CAUTION
Be prepared for sustained control forces in the direction of the annunciation
arrow. For example, an arrow pointing to the right indicates that sustained right
wing down control stick force will be required upon autopilot disconnect.
3. AP DISC Switch........................................................................................DEPRESS
4. Autopilot........................................ RE-ENGAGE if lateral trim re-established
FLASHING YELLOW MODE ANNUNCIATION
NOTE
Abnormal mode transitions (those not initiated by the pilot or by normal
sequencing of the autopilot) will be annunciated by flashing the disengaged
mode in yellow on the PFD. Upon loss of a selected mode, the system will
revert to the default mode for the affected axis, either ROL or PIT. After 10
seconds, the new mode (PIT or ROL) will be annunciated in green.
Loss of selected vertical mode (FLC, VS, ALT, GS, VPTH, GP)
1. Autopilot mode controls ................ SELECT ANOTHER VERTICAL MODE
If on an instrument approach:
2. Autopilot.............................................DISCONNECT and continue manually,
or execute missed approach
Loss of selected lateral mode (HDG, NAV, GPS, LOC, VAPP, BC):
1. Autopilot mode controls ..................SELECT ANOTHER LATERAL MODE
If on an instrument approach:
2. Autopilot.............................................DISCONNECT and continue manually,
or execute missed approach
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