Model 560XL Section III – Operating Procedures
Operating Information
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 3-87
Takeoff and Landing Data – TOLD (Optional)
The optional Takeoff and Landing Data system calculates V-Speeds, takeoff N
1
power settings, and
required field length for takeoff and landing, based on automatic and manually entered parameters.
The TOLD system may be used to calculate takeoff data for dry and wet runway surfaces, and landing
data for dry runway surfaces. For contaminated runway conditions for takeoff, or for wet and
contaminated runway conditions for landing, the Advisory Information section of the airplane flight manual
should be used to compute the additional runway distance required based on the dry runway data
provided by the TOLD system.
It is the responsibility of the flight crew to verify all inputs regarding aircraft weight, aircraft configuration,
runway information, and ambient conditions.
The system uses the calculated takeoff weight and the estimated landing weight from the Takeoff and
Landing tabs, respectively, on the Weight and Fuel page. The TOLD system will not provide takeoff data
for aircraft weight above the maximum takeoff weight. This can occur when the aircraft is above maximum
takeoff weight, but at or below maximum ramp weight. The current aircraft weight must be at or below
maximum takeoff weight before TOLD will generate takeoff data.
Additionally, there are automatic and pilot entries for runway selection, barometric altimeter setting,
temperature, and wind. The pilot enters runway condition, flap and anti-ice settings, and any adjustment
factors.
The system monitors flap position, anti-ice system selection, barometric altimeter setting, temperature,
and estimated takeoff and landing weight, to ensure they match actual aircraft configuration and ambient
conditions. Alerts are provided in the Takeoff Data and Landing Data pages when significant differences
exist. This will cause the V-Speed and N
1
bugs to be replaced with amber dashes.
Weight values may be manually entered on the Takeoff Data and Landing Data pages which will place
the system into Planning Mode, allowing for scenario-based planning. The Accept Takeoff Speeds and
Accept Landing Speeds buttons are not available in Planning Mode. Pressing the Reload Weight button
will update the takeoff or landing weight with the calculated weight from the Weight and Fuel page, taking
the system out of Planning Mode.
If an intended runway is defined in the active flight plan or TOLD, the runway edge boundaries on both
MFD, PFD moving maps, and SVT are highlighted for additional situational awareness.
V-Speed and N
1
bug values may be manually entered on the Speed Bugs page. Values calculated by
TOLD will be displayed in magenta, and manually entered values will be displayed in cyan.
Selecting Steep Approach mode on the TAWS Settings page will invalidate calculated landing data.
Landing data must be manually calculated based on Steep Approach AFMS landing data. V-Speed and
N
1
bugs may be set manually on the Speed Bugs page.
The TOLD database part number is displayed on the PERF page on either GTC.
Refer to Garmin G5000 Integrated Avionics System Pilot’s Guide for more information.
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