- •Section 1 System Overview
- •1.1 System Description
- •1.2 Line Replaceable Units (LRU)
- •1.3 G1000 Controls
- •PFD/MFD Controls
- •Audio Panel Controls
- •1.4 Secure Digital (SD) Cards
- •1.5 System Power-up
- •1.6 System Operation
- •Normal Display Operation
- •Reversionary Display Operation
- •AHRS Operation
- •G1000 System Annunciations
- •Softkey Function
- •GPS Receiver Operation
- •1.7 Accessing G1000 Functionality
- •Menus
- •MFD Page Groups
- •MFD System Pages
- •Electronic Checklists (Optional)
- •1.8 Display Backlighting
- •Automatic Adjustment
- •Manual Adjustment
- •Section 2 flight Instruments
- •2.1 Flight Instruments
- •Airspeed Indicator
- •Attitude Indicator
- •Altimeter
- •Vertical Speed Indicator (VSI)
- •Vertical Deviation, Glideslope, & Glidepath Indicators
- •Horizontal Situation Indicator (HSI)
- •Course Deviation Indicator (CDI)
- •2.2 Supplemental Flight Data
- •Generic Timer
- •Outside Air Temperature
- •Wind Data
- •System Time
- •Vertical Navigation (VNV) Indications
- •2.3 PFD Annunciations and Alerting Functions
- •System Alerting
- •Traffic Annunciation
- •TAWS Annunciations
- •Low Altitude Annunciation
- •Altitude Alerting
- •Minimum Descent Altitude/Decision Height Alerting
- •Marker Beacon Annunciations
- •2.4 Abnormal Operations
- •Abnormal GPS Conditions
- •Unusual Attitudes
- •Section 3 Engine Indication System (EIS)
- •3.1 Engine Display
- •3.2 Lean Display
- •3.3 System Display
- •Section 4 audio panel and CNS
- •4.1 Overview
- •PFD/MFD Controls and Frequency Display
- •Audio Panel Controls
- •4.2 COM Operation
- •COM Transceiver Selection and Activation
- •COM Transceiver Manual Tuning
- •Quick-Tuning and Activating 121.500 MHz
- •Auto-tuning the COM Frequency
- •Frequency Spacing
- •Automatic Squelch
- •Volume
- •4.3 NAV Operation
- •NAV Radio Selection and Activation
- •NAV Receiver Manual Tuning
- •Auto-tuning the NAV Frequency
- •Marker Beacon Receiver
- •DME Tuning (Optional)
- •4.4 GTX 33 Mode S Transponder
- •Transponder Controls
- •Transponder Mode Selection
- •Entering a Transponder Code
- •IDENT Function
- •Flight ID Reporting
- •4.5 Additional Audio Panel Functions
- •Power-Up
- •Mono/Stereo Headsets
- •Speaker
- •Intercom
- •Clearance Recorder and Player
- •Entertainment Inputs
- •4.6 Audio Panel Preflight Procedure
- •4.7 Abnormal Operation
- •Stuck Microphone
- •COM Tuning Failure
- •Audio Panel Fail-Safe Operation
- •Reversionary Mode
- •Section 5 GPS Navigation
- •5.1 Introduction
- •5.2 Navigation Map (MFD)
- •Navigation Map Page
- •5.3 PFD Inset Map and Windows
- •Inset Map
- •PFD Windows
- •5.4 Direct-to-Navigation (MFD)
- •Selecting a Direct-to Waypoint
- •Clearing Vertical Constraints
- •Specifying a Course to a Waypoint
- •Canceling Direct-to Navigation
- •Direct-to Navigation Shortcuts
- •5.5 Direct-to-Navigation (PFD)
- •5.6 Airport Information (MFD)
- •Duplicate Waypoints
- •Additional Airport Runway Information
- •5.7 Intersection Information (MFD)
- •5.8 NDB Information (MFD)
- •5.9 VOR Information (MFD)
- •5.10 User Waypoint Information (MFD)
- •5.11 Nearest Airports (MFD)
- •5.12 Nearest Intersections (MFD)
- •5.13 Nearest NDB (MFD)
- •5.14 Nearest VOR (MFD)
- •5.15 Nearest User Waypoint (MFD)
- •5.16 Nearest Airspaces
- •5.17 Nearest Airports (PFD)
- •5.18 Flight Planning (MFD)
- •Airways/Jetways
- •Display of Airways on the Flight Plan Page
- •Vertical Navigation (VNV)
- •Navigating an Example Flight Plan
- •Parallel Track (PTK)
- •5.19 Flight Planning (PFD)
- •Operations
- •5.20 Procedures (MFD)
- •Leg Types Supported by the G1000
- •5.21 Procedures (PFD)
- •Operations
- •5.22 ABNORMAL OPERATION
- •Dead Reckoning
- •Section 6 Hazard Avoidance
- •6.1 XM Satellite Weather (Service Optional)
- •Activating XM Satellite Services
- •Using XM SATELLITE Weather Products
- •Weather Softkeys on the Weather Data Link Page
- •Setting Up the Weather Data Link Page
- •XM Satellite Weather on the Navigation Map
- •6.2 WX-500 Stormscope (Optional)
- •Setting Up Stormscope on the Navigation Map
- •Selecting the Stormscope Page
- •6.3 Terrain Proximity
- •Requirements
- •GPS Position and GPS-MSL Altitude
- •Displaying Terrain Proximity Data
- •Terrain Proximity Symbols
- •Terrain Proximity Page
- •Navigation Map Page
- •6.4 TAWS (Optional)
- •Requirements
- •TAWS Alerting
- •Using TAWS
- •TAWS Symbols
- •TAWS Alerts
- •6.5 Traffic
- •Traffic Information Service (TIS)
- •Honeywell KTA 870 TAS System (Optional)
- •ADS-B Traffic (Optional)
- •Section 7 Automatic Flight Control System
- •7.1 AFCS Controls
- •7.2 Flight Director Operation
- •Command Bars
- •Activating the Flight Director
- •7.3 Flight Director Modes
- •Pitch Modes
- •Roll Modes
- •7.4 Autopilot Operation
- •Engaging the Autopilot
- •Control Wheel Steering
- •Disengaging the Autopilot
- •7.5 Example Procedures
- •Departure
- •Intercepting a VOR Radial
- •Flying a Flight Plan/GPS Course
- •Descent
- •Approach
- •Go Around/Missed Approach
- •7.6 AFCS Annunciations and Alerts
- •AFCS Status Alerts
- •Overspeed Protection
- •Section 8 Additional Features
- •8.1 SafeTaxi
- •SafeTaxi Cycle Number and Revision
- •8.2 ChartView
- •ChartView Softkeys
- •Terminal Procedures Charts
- •Chart Options
- •Day/Night View
- •ChartView Cycle Number and Expiration Date
- •8.3 FliteCharts
- •FliteCharts Softkeys
- •Terminal Procedures Charts
- •Chart Options
- •Day/Night View
- •FliteCharts Cycle Number and Expiration Date
- •8.4 XM Radio Entertainment (Optional)
- •XM Satellite Radio Service
- •XM Service Activation
- •Using XM Radio
- •Automatic Audio Muting
- •8.5 Abnormal Operation
- •Annunciations and Alerts
- •Alert Level Definitions
- •NAV III Aircraft Alerts
- •CO Guardian Messages
- •G1000 System Annunciations
- •Other G1000 Aural Alerts
- •G1000 System Message Advisories
- •AFCS Alerts
- •TAWS ALERTS
- •TAWS System Status Annunciations
- •SD Card Use
- •Jeppesen Databases
- •Garmin Databases
- •Glossary
- •Frequently Asked Questions
- •General TIS Information
- •Introduction
- •TIS vs. TAS/TCAS
- •TIS Limitations
- •Map Symbols
- •Index
ENGINE INDICATION SYSTEM
3.2 LEAN DISPLAY
NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH).
The Lean Display is accessed by pressing the ENGINE Softkey followed by the LEAN Softkey and provides information for performing engine leaning. The engine gauge(s) and Fuel Quantity Indicator remain on the Lean Display and fuel flow is listed as a numeric readout. Exhaust gas (EGT) and cylinder head (CHT) temperatures for all cylinders are displayed graphically with numeric readouts for the selected cylinder. For turbocharged aircraft, the Turbine Inlet Temperature (TIT) Indicator is shown above the EGT Bar Graph.
Accessing the EIS Lean Display:
1)Press the ENGINE Softkey.
2)Press the LEAN Softkey.
3)To return to the default Engine Display, press the ENGINE or BACK Softkey.
From the Lean Display, the pilot can utilize the CYL SLCT and ASSIST softkeys to obtain information about specific cylinders. Pressing the CYL SLCT (Cylinder Select) Softkey cycles through the cylinders (i.e., changes the cylinder indicated on the bar graphs in light blue). This softkey is disabled when the ASSIST Softkey is pressed or when a cylinder experiences a caution or warning condition; the softkey remains disabled until the temperature returns to normal.
Monitoring the desired cylinder’s EGT and CHT:
From the Lean Display, press the CYL SLCT Softkey to cycle through each cylinder and view its EGT and CHT. The selected cylinder is shown in light blue.
The ASSIST Softkey aids in the leaning process by identifying the peak of the first cylinder whose temperature falls. This cylinder’s bar on the EGT and CHT bar graphs is highlighted in cyan as the selected cylinder. If the temperature of the peaked cylinder exceeds the peak value, the peak value is not updated. Monitoring of the cylinder continues until the ASSIST Softkey is pressed again which disables lean assist, and removes the peak block from the bar graph and the temperature deviation from peak (∆PEAK). The system then returns to seeking the hottest cylinder.
190-00498-02 Rev.A |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
3-5 |
ENGINE INDICATION SYSTEM
1 Engine Manifold Pressure
Gauge (MAN IN)
Models 182T, T182T, 206H,
T206H
2 Tachometer
(RPM)
3 Fuel Flow
(FFLOW GPH)
Displays engine power in inches of mercury (in Hg)
Turbocharged aircraft – Red range indicates maximum manifold pressure Model T182T – A white tick mark indicates the cruise manifold pressure
Displays propeller speeds in revolutions per minute (rpm) Red range indicates propeller overspeed warning
Models 172S, 206H, and T206H – White high-rpm range indicates above normal operating speeds
Displays the current fuel flow in gallons per hour (gph)
4 Turbine Inlet Temperature
Indicator (TIT)
Turbocharged Aircraft
5 Exhaust Gas Temperature
Bar Graph (EGT °F)
6 Cylinder Head Temperature
Bar Graph (CHT)
7 Fuel Quantity Indicator
(FUEL QTY GAL)
Displays the temperature at the turbine inlet in degrees Fahrenheit (°F)
TIT deviation from peak (∆PEAK) is displayed below the indicator when the ASSIST Softkey is pressed.
Displays the exhaust gas temperature of all cylinders in °F; a readout for the selected cylinder (by default, the hottest cylinder) is shown below the bar graph
The selected cylinder is indicated in light blue. Cylinders whose EGTs are in the normal range appear in white.
The EGT deviation from peak (∆PEAK) for the selected cylinder is displayed below the indicator when the ASSIST Softkey is pressed.
Displays the head temperatures of all cylinders in °F; a readout for the selected cylinder (by default, the hottest cylinder) is shown below the bar graph
The selected cylinder is indicated in light blue. Cylinders whose CHTs are in the normal range appear in white. Cylinders whose CHTs enter the caution and warning ranges appear in yellow and red, respectively.
Displays the quantity of fuel in gallons (gal) in each tank (left–L and right– R)
When full, the indicator displays to 35 gal per side (26 gal for Models 172R and 172S).
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Garmin G1000 Pilot’s Guide for Cessna Nav III |
190-00498-02 Rev.A |
2
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7
ENGINE INDICATION SYSTEM
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, indicated 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.
Selecting the Engine Leaning Assist function:
From the Lean Display, press the ASSIST Softkey to identify the peak. The peak temperature for the selected cylinder is indicated with a hollow block on the EGT Bar Graph and the temperature deviation from peak is shown underneath the EGT Bar Graph.
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Figure 3-4 Lean Display (Normally-aspirated Aircraft) |
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190-00498-02 Rev.A |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
3-7 |
ENGINE INDICATION SYSTEM
TURBOCHARGED AIRCRAFT
Leaning for turbocharged aircraft is done with reference to the Turbine Inlet Temperature (TIT). When the temperature peaks, the numeric readout (∆PEAK) appears below the TIT Indicator and displays the differencebetweenpeakandcurrentTITs,indegreesFahrenheit(°F). Ifapeakisnotdisplayed,underscores are shown until one is established.
Selecting the Engine Leaning Assist function:
From the Lean Display, press the ASSIST Softkey to identify the peak. The TIT deviation from peak is shown below the TIT Indicator.
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Cruise Manifold Pressure |
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Figure 3-5 |
Lean Display (Turbocharged Aircraft) |
3-8 |
Garmin G1000 Pilot’s Guide for Cessna Nav III |
190-00498-02 Rev.A |