General systems, Engine & airframe systems – Garmin G1000 Socata TBM 850 User Manual
Page 108
Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-01 Rev. A
96
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
GENERAL SYSTEMS
The General Synoptics Page aircraft diagram displays open doors in red (CAS messages also generated).
Statuses of stall sensor, propeller, pitot probes, and windshield heat are also indicated on the diagram:
• White indicates that heat is off (propeller and windshield)
• Light blue indicates heat has been selected (windshield)
• Green indicates heat is on
• Yellow indicates heat has failed (stall sensor, propeller and pitot tube).
Invalid sensor information is indicated with a red ‘X’.
Figure 3-26 General Synoptics Page
1
Rear Cargo Door Open
2
Cabin Door Open
3
Pilot Door Open
4
Pitot Probe 1
5
Forward Cargo Door Open
6
Propeller Heaters
7
Right Windshield Heat On
8
Pitot Probe 2
9
Stall Warning Sensor
5
4
8
7
1
2
3
6
9
Figure 3-27 Windshield Heat Status
Windshield
Heat On
Windshield
Heat Off
Left Windshield Heat On
Right Windshield Heat Selected