User Manual

Garmin G1000 Pilot’s Guide for the Quest Kodiak 100
190-00590-01 Rev. B244
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
When the aircraft is in the air and a destination waypoint has been entered, the fuel calculations can be
completed.
•Estimatedlandingweight=zerofuelweight+estimatedlandingfuelweight.
•Estimatedlandingfuelweight=fuel on board weight - (fuel flow x ETE)
•Excessfuelweight=estimatedlandingfuelweight-fuelreservesweight
If the aircraft is on the ground or a destination waypoint has not been entered, the following fields display
invalid values consisting of six dashes:
•Estimatedlandingweight
•Estimated landing fuel weight
•Excess fuel weight
WEIGHT CAUTION AND WARNING CONDITIONS
If the zero fuel weight is greater than the maximum allowable zero fuel weight, then the zero fuel weight is
displayed in amber.
If the aircraft weight is greater than the maximum allowable takeoff weight, then the aircraft weight is displayed
in amber.
If the estimated landing weight is greater than the maximum allowable landing weight, then the estimated
landing weight is displayed in amber.
If the estimated landing fuel weight is positive, but less than or equal to the fuel reserves weight, the following
values are displayed in amber:
•Estimatedfuelatlandingweight
•Excess fuel weight
If the estimated landing fuel weight is zero or negative, then the following values are displayed in red:
•Estimatedfuelatlandingweight
•Excess fuel weight