Garmin Software Version 0321.22 Manual de usuario Pagina 48

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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
WITH HONEYWELL KAP 140 AUTOPILOT
190-00492-12 Rev 6 Diamond DA 40 / DA 40F
4B-4
(c) PFD OVERHEAT caution
AND
MFD OVERHEAT caution
NOTE
The PFD and MFD are both approaching operating temperature limits. The
brightness of both displays is automatically reduced to 50% of maximum.
1. Refer to standby attitude, heading, altimeter, and airspeed instruments
to maintain aircraft control.
2. If either the PFD or MFD fails or is unusable, pull the circuit breaker of
the affected device and select Display Reversionary Mode using the red
DISPLAY BACKUP button on the audio panel.
3. Land as soon as practical at a suitable airport.
If the PFD fails or the PFD circuit breaker is pulled, the autopilot will
operate normally.
If the MFD fails or the MFD circuit breaker is pulled, the autopilot
vertical modes will operate normally. Autopilot lateral modes will be
limited to ROL mode only.
(d) GIA1 OVERHEAT caution
OR
GIA2 OVERHEAT caution
NOTE
Either GIA 1 or GIA 2 is approaching its operating temperature limit.
1. Minimize all COM transmissions to reduce temperature.
(e) GIA1 OVERHEAT caution
AND
GIA2 OVERHEAT caution
NOTE
Both GIA 1 and GIA 2 are approaching their operating temperature limits.
COM 1, COM 2, NAV 1, NAV 2, GPS 1, and GPS 2 may fail.
1. Minimize all COM transmissions to reduce temperature.
2. Land as soon as practical at a suitable airport.
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