Garmin G1000 Socata TBM 850 - Manual (Page 105)

190-00709-02 Rev. B Garmin G1000 Pilot’s Guide for the Socata TBM 850 91
ENGINE & AIRFRAME SYSTEMS
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
ELECTRICAL INFORMATION
Currents for the battery (pointers labeled “B”) and generator (pointer labeled “G” for primary generator and
“S” for standby generator) and voltages for the battery and essential bus (pointer labeled “E”) are shown along
color-coded scales, with readouts to the right.
Generator
Current
Essential
Bus Voltage
Battery
Voltage
Battery
Current
Figure 3-12 Electrical Display
TRIM AND FLAP INDICATORS
Elevator, rudder, and aileron trim indications are shown along slide bar scales next to the CAS messages
in normal display mode. Flap deflection is normally displayed beneath the trim indications using a rotating
pointer. Flap positions for takeoff, landing, and up positions are labeled. In Reversionary Mode, only elevator
trim is indicated and flap position (UP, T/O, LDG) is provided as a digital readout.
Figure 3-13 Trim and Flap Indications