Garmin G1000 Socata TBM 850 - Manual (Page 279)

190-00709-02 Rev. B Garmin G1000 Pilot’s Guide for the Socata TBM 850 265
FLIGHT MANAGEMENT
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
Synchronizing the fuel on board with the actual measured fuel on board:
Select the FOB SYNC Softkey; or press the MENU Softkey, highlight ‘Synchronize Fuel on Board’, and press the
ENT Key. The actual measured fuel on board is displayed in the fuel on board field.
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