Garmin Software Version 0321.22 Manual de usuario descargar pdf (Pagina 53)

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

7-3

G1000/KAP 140 INTERFACE

The G1000 system provides heading and course information, lateral and vertical

navigation flags and both lateral and vertical course deviation signals to the

KAP 140 autopilot. When course deviation signals are available from the

G1000, the KAP 140 may be coupled to those signals as described in the

autopilot documentation.

When navigation changes on the G1000 cause the KAP 140 autopilot to

automatically revert to ROL mode, the G1000 system will provide a message to

alert the pilot to verify that the autopilot mode is as desired.

The G1000 system controls and displays affecting KAP 140 autopilot operation

are;

• PFD mounted CDI selector button

• PFD/MFD mounted heading select knob (HDG)

• PFD/MFD mounted course select knob (CRS)

• Course Deviation Indicator (CDI) and flag

• Vertical Deviation Indicator (GS/VPTH) and flag

No altitude information or altitude preselect settings are exchanged between the

autopilot and the G1000 system. Altitude and barometric setting entries must be

made separately on the G1000 and KAP 140 autopilot systems as appropriate.

When passing the missed approach point (MAP) on an instrument approach, the

aircraft should either be hand flown or the autopilot operated in HDG mode

until the appropriate missed approach path and climb has been established.

Before re-engaging the autopilot, the pilot must carefully assure that the

autopilot programming will result in a turn in the correct direction and the

required climb.

Refer to the appropriate KAP 140 autopilot Airplane Flight Manual or Airplane

Flight Manual Supplement for information and procedures for the KAP 140

autopilot.

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Garmin Software Version 0321.22 Manual de usuario Pagina 53