Model 560XL Appendix – Systems Description
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
A-18
Enroute and Oceanic phase of flight; Terminal and Approach modes do not support DR. Course
deviation information will be displayed with an amber CDI on both PFDs and will remain for up to 20
minutes after GPS position data has been lost. The autopilot and/or flight director may be coupled in
FMS mode while the system is in Dead Reckoning mode up to 20 minutes. Refer to the G5000
Pilot’s Guide for further information. Revert to an alternate means of navigation appropriate to the
route and phase of flight.
Electrical System
Power Distribution
There are no changes to the electrical power generation, power feeders, control, or fault protection.
Only the Avionics power distribution has changed.
The LH and RH circuit breaker panels were modified to support the installation of the G5000 system.
Circuit breaker diagrams are included below in Figures A-4 and A-5.
Figure A-4, Left Circuit Breaker Panel
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