Garmin G1000 Manual

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85087
FLIGHT INSTRUMENTS
UNUSUAL ATTITUDES
When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the 
horizon	are	displayed	on	the	Attitude	Indicator,	starting	at	50˚	above	and	30˚	below	the	horizon	line.
Figure 2-52  Pitch Attitude Warnings
Nose High
Nose Low
If	
pitch	 exceeds	 +30˚/-20˚	 or	bank	 exceeds	 65˚,	some	 information	 displayed	on	the	 PFD	is removed.  The 
Altimeter	 and...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A88
FLIGHT INSTRUMENTS
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190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85089
ENGINE & AIRFRAME SYSTEMS
SECTION 3  ENGINE AND AIRFRAME SYSTEMS
 NOTE: Refer to the Pilot’s Operating Handbook (POH) for limitations.
The G1000 offers improved flight operations and reduces crew workload by automatically monitoring critical 
system parameters and providing system alerts during all phases of flight using the following:\
•	 The	Engine Indication System (EIS) displays electrical, fuel, engine, pressurization, and...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A90
ENGINE & AIRFRAME SYSTEMS
In the event of a display failure, depending on the failed display(s), the functioning display(s) ma\
y be re-
configured to present Primary Flight Display (PFD) symbology together with engine and CAS informat\
ion 
(refer to the System Overview for more information about Reversionary Mode).  In Reversionary Mode, engine, 
pressurization, fuel, electrical, and trim data is presented in an abbreviated format...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85091
ENGINE & AIRFRAME SYSTEMS
3.1 ENGINE INDICATION SYSTEM (EIS)
Figure 3-4  EIS Display (Reversionary Mode)
17
1
5
6
4
3
2
9
8
12
13
15
16
1Torque
2Propeller Speed
3Generator Speed
4Interturbine Temperature
5Oil Pressure
6Oil Temperature
7CAS Display
8Cabin Pressure Altitude and Change Rate
9Differential Pressure
10Selected Cabin Altitude
11Oxygen Pressure
12Fuel Quantity
13Fuel Flow
14Fuel Pressure
15Battery and Generator Currents...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A92
ENGINE & AIRFRAME SYSTEMS
EIS information is presented using gauges, horizontal and vertical bar indicators, slide bars\
, and digital readouts.  
Green ranges on the instrument scales indicate normal ranges of operation;\
 yellow and red bands indicate caution 
and warning, respectively.  During normal operating conditions, an instrument’s pointer appears in white and the 
readout text is green.  When data is out of the range of...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85093
ENGINE & AIRFRAME SYSTEMS
GENERATOR SPEED GAUGE
Generator speed is indicated as a percentage of maximum safe operating speed (rpm), from 0 to 120%.  If 
generator speed exceeds 104% a warning condition occurs.
Figure 3-7  Generator Speed Gauge
ITT GAUGE
The Interturbine Temperature (ITT) Gauge ranges differ for engine off/start and running conditions.  Values 
between 200 and 1200 degrees Celsius (°C) are shown at engine start;...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A94
ENGINE & AIRFRAME SYSTEMS
CABIN PRESSURIZATION
Cabin pressurization information (cabin altitude, rate of change, and differential cabin pressure) is shown at 
the top of the right EICAS column.  Only readouts for cabin altitude and pressure differential are displayed in 
Reversionary Mode.
Cabin altitude (ALT FT) is shown on a color-coded scale labeled in 5,000-ft increments with a readout (in 
feet) below.  Cabin altitude change...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85095
ENGINE & AIRFRAME SYSTEMS
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.
GeneratorCurrent
Essential
Bus Voltage Battery
Voltage Battery
Current
Figure 3-12  Electrical Display
TRIM AND FLAP...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A96
ENGINE & AIRFRAME SYSTEMS
3.2 SYNOPTICS
The Synoptics pages show current conditions of certain aircraft functionality on aviation system diagrams,  
reducing workload by allowing the flight crew to rapidly analyze the situation.  Aircraft systems graphically 
depicted in the synoptic diagrams include:
•	 Electrical
Once the SYSTEM Softkey is selected, the Synoptics pages can be accessed using softkeys\
 or the small FMS 
Knob.  To...