Cockpit Reference Guide
Table Of Contents
- Section 1: System Overview
- Section 2: Flight Instruments
- Section 3: Engine Indication System (EIS)
- Section 4: NAV/COM and Transponder
- Section 5: Audio Panel
- Section 6: Automatic Flight Control
- Section 7: Navigation
- 7.1 Navigation Map Page
- 7.2 Direct-to Navigation
- 7.3 Navigating an Example Flight Plan
- 7.4 Airport Information
- 7.5 Intersection Information
- 7.6 NDB Information
- 7.7 VOR Information
- 7.8 User Waypoint Information Page
- 7.9 Nearest Airports
- 7.10 Nearest Intersections
- 7.11 Nearest NDB
- 7.12 Nearest VOR
- 7.13 Nearest User Waypoint
- 7.14 Nearest Frequencies
- 7.15 Nearest Airspaces
- Section 8: Flight Planning
- 8.1 User Defined Waypoints
- 8.2 Viewing the Active Flight Plan
- 8.3 Activate a Stored Flight Plan
- 8.4 Activate a Flight Plan Leg
- 8.5 Stop Navigating a Flight Plan
- 8.6 Invert Active Flight Plan
- 8.7 Create a New Flight Plan
- 8.8 Enter an Airway in a Flight Plan
- 8.9 Load a Departure
- 8.10 Load an Arrival
- 8.11 Load an Approach
- 8.12 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan
- 8.13 Store a Flight Plan
- 8.14 Edit a Stored Flight Plan
- 8.15 Delete a Waypoint from the Flight Plan
- 8.16 Invert and Activate a Stored Flight Plan
- 8.17 Copy a Flight Plan
- 8.18 Delete a Flight Plan
- 8.19 Graphical Flight Plan Creation
- 8.20 Trip Planning
- Section 9: Procedures
- Section 10: Hazard Avoidance
- 10.1 Customizing the Hazard Displays on the Navigation Map
- 10.2 STORMSCOPE® (Optional)
- 10.3 XM Weather (Service Optional)
- 10.4 Traffic Systems
- 10.5 Terrain and Obstacle Proximity
- 10.6 Terrain Awareness & Warning System (TAWS) Display (Optional)
- Displaying Terrain on the TAWS Page
- Enable/Disable Aviation Data
- TAWS Inhibit
- Manual System Test
- Forward Looking Terrain Avoidance (FLTA)
- Premature Descent Alert (PDA)
- Excessive Descent Rate Alert (EDR)
- Negative Climb Rate After TakeoffAlert (NCR)
- “Five-Hundred” Aural Alert
- Displaying Terrain and Obstacles on the Navigation Map
- Pop-up Alerts
- TAWS Alerts Summary
- Alert Annunciations
- Section 11: Abnormal Operation
- Section 12: Annunciations & Alerts
- 12.1 Alert Level Definitions
- 12.2 NAV III Aircraft Alerts
- 12.3 CO Guardian Messages
- 12.4 AFCS Alerts
- 12.5 TAWS Alerts
- 12.6 Other G1000 Aural Alerts
- 12.7 G1000 System Annunciations
- 12.8 G1000 System Message Advisories
- MFD & PFD Message Advisories
- Database Message Advisories
- GMA 1347 Message Advisories
- GIA 63 Message Advisories
- GIA 63W Message Advisories
- GEA 71 Message Advisories
- GTX 33 Message Advisories
- GRS 77 Message Advisories
- GMU 44 Message Advisories
- GDL 69A Message Advisories
- GDC 74A Message Advisories
- Miscellaneous Message Advisories
- Index

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
190-00384-08 Rev. A
SECTION 3 – ENGINE
INDICATION SYSTEM (EIS)
3-1
SECTION 3: ENGINE INDICATION
SYSTEM (EIS)
NOTE: Refer to the Pilot’s Operating Handbook
(POH) for limitations.
EIS information is presented in three displays, accessed
using the ENGINE Softkey on the MFD:
• Engine Display – Default display, shows all critical
engine, fuel, and electrical indicators
• Lean Display – Provides engine leaning
information
• System Display – Shows numeric readouts of
critical engine, fuel, and electrical indicators
Green and white bands indicate normal ranges of
operation; yellow and red bands indicate caution and
warning, respectively. If sensory data to an instrument
becomes invalid or unavailable, a red “X” is shown across
the instrument.
3.1 ENGINE DISPLAY
The Engine Display is the default EIS display and can
be displayed after viewing other EIS displays by pressing
the ENGINE Softkey.
The EIS automatically defaults back to the Engine
Display from the Lean or System Display when certain
parameters are exceeded. Fluctuations in engine speed
and fuel quantity above certain levels, depending on the
airframe, also cause reversion back to the Engine Display.
1
Engine Manifold Pressure Gauge (MAN IN)
Models 182T, T182T, 206H, T206H – Displays
engine power in inches of mercury (in Hg).
Turbocharged aircraft have a red portion of the
gauge indicating the maximum manifold pressure
range. A white tick mark is displayed indicating
the cruise manifold pressure (Model T182T only).
2
Tachometer (RPM) – Shows propeller speeds
in revolutions per minute (rpm). Red range
indicates propeller overspeed warning; a white
high-rpm range indicates above normal operating
speeds (Models 172S, 206H, and T206H)
3
Fuel Flow Indicator (FFLOW GPH) – Shows
the current fuel flow in gallons per hour (gph).
For turbocharged aircraft, the indicator displays
a small stand-alone green band indicating
maximum takeoff fuel flow. A white tick mark
indicates the maximum cruise fuel flow (Model
T182T only).
4
Oil Pressure Indicator (OIL PRES) – Displays
pressure of the oil supplied to the engine in
pounds per square inch (psi).
5
Oil Temperature Indicator (OIL TEMP)
– Displays the engine oil temperature in degrees
Fahrenheit (°F).
6
Cylinder Head Temperature Indicator (CHT)
Models 182T, T182T, 206H, T206H – Shows
the head temperature of the hottest cylinder
(number shown in triangular pointer) in degrees
Fahrenheit (°F).
7
Exhaust Gas Temperature Indicator (EGT)
Normally-aspirated Aircraft
– Displays the
exhaust gas temperature of the hottest cylinder
(number shown in triangular pointer) in degrees
Fahrenheit (°F).
8
Turbine Inlet Temperature Indicator (TIT)
Turbocharged Aircraft – Displays the temperature
at the turbine inlet in degrees Fahrenheit (°F).
9
Vacuum Pressure Indicator (VAC) Models
172R and 172S
– Displays vacuum pressure.










