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)
3-7
The ASSIST Softkey aids in the leaning process by
identifying the peak of the first cylinder whose temperature
falls. If the temperature of the peaked cylinder exceeds
the peak value, the peak value is not updated. Press the
ASSIST Softkey to stop peak monitoring.
Normally-aspirated Aircraft
For normally-aspirated aircraft, when a cylinder peaks,
its peak is represented by a hollow block on the EGT Bar
Graph. The EGT readout for the peaked cylinder, indicat-
ed on the bar graph in light blue, appears directly beneath
the bar graph. The system automatically switches to the
first peak obtained and displays the temperature deviation
from peak (∆PEAK) in degrees Fahrenheit (°F) below the
EGT readout.
Turbocharged Aircraft
Leaning for turbocharged aircraft is done with refer-
ence to the Turbine Inlet Temperature (TIT). When the
temperature peaks, the numeric readout (∆PEAK) appears
below the TIT Indicator and displays the difference be-
tween peak and current TITs, in degrees Fahrenheit (°F).
If a peak is not displayed, underscores are shown until
one is established.
3.3 SYSTEM DISPLAY
NOTE: Fuel calculations do not use the aircraft
fuel quantity indicators and are calculated from
the last time the fuel was reset.
NOTE: The pilot should refer to the Pilot’s
Operating Handbook (POH) for fuel values and
limitations. The displayed fuel remaining can be
adjusted up to 53 gal (Models 172R, 172S) or 87
gal (Models 182T, T182T, 206H, T206H).
The System Display is accessed by pressing the
ENGINE Softkey followed by the SYSTEM Softkey and
shows critical engine, fuel, and electrical parameters.
Fuel calculations are based on the fuel flow totalizer
and the displayed fuel remaining, adjusted by the pilot
using the following softkeys:
• RST FUEL – Resets totalizer-based fuel remaining
(GAL REM) to zero and the fuel used (GAL USED)
to zero
• GAL REM – Gives access to softkeys for adjusting
the amount of fuel remaining for purposes of fuel
calculations
Fuel remaining can be adjusted in one or ten-gallon
increments using the appropriate softkeys. Softkeys also
allow entering the full tank quantity for the aircraft or the
tab quantity, which is 35 gallons (Models 172R and 172S)
or 64 gallons (Models 182T, T182T, 206H, and T206H).