Garmin G5000 - Normal Procedures

Model 560XL Section III – Operating Procedures
AFM Cross Reference
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 3-11
NORMAL PROCEDURES
Preflight Procedures
Preliminary Exterior Inspection....................................................................................... UNCHANGED
Cabin Inspection ............................................................................................................. UNCHANGED
(AVIONICS DOCUMENTS NOT APPLICABLE)
Cockpit Inspection .................................................... MODIFIED WITH ADDITIONAL INFORMATION
Refer to G5000 AFMS
Exterior Inspection .......................................................................................................... UNCHANGED
Cockpit Preparation ........................................................ MODIFIED WITH ADDITIONAL INFORMATION
Refer to G5000 AFMS for Autopilot Check
Delay Before Flight Without APU/External Power ................................................................ UNCHANGED
APU Starting (Ground or In-flight) ......................................................................................... UNCHANGED
APU Shutdown (Ground or In-flight) ..................................................................................... UNCHANGED
Before Starting Engines ........................................................................................................ UNCHANGED
Starting Engines (Ground Start with APU Generator Online) ............................................... UNCHANGED
Before Taxi............................................................................................................................ UNCHANGED
(EFIS Test Switch no longer installed)
Taxi ....................................................................................................................................... UNCHANGED
Before Takeoff ................................................................ MODIFIED WITH ADDITIONAL INFORMATION
Refer to G5000 AFMS for Transponder and TCAS mode verification
Before Starting Engines ........................................................................................................ UNCHANGED
Takeoff
Static Takeoff ................................................................................................................. UNCHANGED
Rolling Takeoff ............................................................................................................... UNCHANGED
After Takeoff/Climb ............................................................................................................... UNCHANGED
Cruise .................................................................................................................................... UNCHANGED
Descent ................................................................................................................................. UNCHANGED
Approach ............................................................................................................................... UNCHANGED
Before Landing ...................................................................................................................... UNCHANGED
Landing ................................................................................................................................. UNCHANGED
All Engine Go-Around ........................................................................................................... UNCHANGED
After Landing .................................................................. MODIFIED WITH ADDITIONAL INFORMATION
Refer to G5000 AFMS for Transponder/TCAS mode
Shutdown .............................................................................................................................. UNCHANGED
Shutdown (Quick Turn) ......................................................................................................... UNCHANGED
Turbulent Air Penetration ...................................................................................................... UNCHANGED
Expanded Preflight Procedures ............................................................................................ UNCHANGED
(Before Taxi – EFIS Test Switch no longer installed)
Wind Components ................................................................................................................ UNCHANGED