Garmin G5000 - Cockpit Reference Guide; Power Plant Indication System Markings

Model 560XL Section II – Limitations
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 2-3
Cockpit Reference Guide
The G5000 Cockpit Reference Guide for Textron Aviation Citation 560XL must be immediately available
to the flight crew during all phases of flight.
Use the G5000 Cockpit Reference Guide for Textron Aviation Citation 560XL, GARMIN part number
190-02538-02, revision A or later approved revision, when System Software Version 3343.02 is installed.
The System Software Version number is displayed on the Airframe Tab of the Avionics Status page on
the GTC (Utilities – Setup – Avionics Status).
Power Plant Indication System Markings
No changes were made to the airplane’s engine operating limits. Refer to the Airplane Flight Manual for
engine limitations. The engine gauges are marked as shown below.
NOTE
Numerical digital displays will flash inverse red/white video for 5 seconds, and then
remain steady red if the indicated engine parameter exceeds its established limit.
Numerical digital displays will flash inverse amber/black video for 5 seconds, and
then remain steady amber for “caution” conditions.
Fan (N1) RPM Indicators:
Models Excel and XLS (Aircraft Serial Numbers 560 – 5001 through 560 – 6000)
N1 Scale Markings
White Band: 0 – 20%
Green Band: 20 – 100%
Amber Line: 100%
Amber Band: 100 – 102%
Red Line: 102%
Red Band: 102% and higher
N
1
Instrument Markings
N
1
Pointer
Color
Numeric N
1
Displa
y
Colo
r
≤ 100% White
Green text, black
background
> 100% and ≤ 102% within
transient time limits *
Amber
Black text, amber
background
> 100% and ≤ 102% exceeding
transient time limits *
Red
White text, red
background
> 102% Red
White text, red
background
* See AFM for transient time limitations