Garmin G5000 Airplane Flight Manual Supplement page 100

Model 560XL
TAWS N/A OR TAWS FAIL

TAWS N/A or TAWS FAIL Annunciator displayed
1. If one of these annunciators are displayed on the PFD and MFD, the system will no longer
provide Forward Looking Terrain Avoidance functions (FLTA), Premature Descent Alerting (PDA),
or display relative terrain elevations. The crew must maintain compliance with procedures that
ensure terrain and obstacle separation.
Voice Callout Functionality will be lost if GPS position is not available or when the aircraft
is outside the terrain database area of coverage.
2. If the amber GPWS FAIL status annunciator is also displayed, Voice Callouts will not sound.
Procedure completed
GPWS FAIL

GPWS FAIL Annunciator displayed
1. If this annunciator is displayed on the PFD and MFD, the system will no longer provide GPWS
functions. The crew must maintain compliance with procedures that ensure terrain and obstacle
separation.
GPWS Alerting Functions That Will Be Unavailable:
a. Excessive Descent Rate (EDR)
b. Excessive Closure Rate (ECR)
c. Negative Climb Rate (NCR)
d. Flight Into Terrain (FIT)
e. Glideslope and Glidepath Deviation (GSD)
2. If the amber TAWS N/A or TAWS FAIL status annunciator is also displayed, Voice
Callouts will not sound.
Procedure completed
AMBER SYNC INDICATION

SYNC Annunciator displayed near N
The amber SYNC indication is displayed when Engine Sync is set to FAN or TURB and the landing
gear is extended.
1. Engine Sync – SELECT OFF for takeoff, approach and landing.
Procedure completed
AMBER START INDICATION

START Annunciator displayed near ITT gauge for the affected engine
This indicates that the affected engine starter is still engaged when the N
1. Refer to the appropriate procedure in the aircraft flight manual.
Procedure completed
Textron Aviation Citation 560XL
3-58
or N gauges
1 2
Section III – Operating Procedures
Abnormal Procedures
speed is greater than 45%.
2
190-02313-03 Rev. 8
FAA Approved