Garmin Software Version 0563.05- User Manual

Table of Contents:

• Page 3 – Garmin G1000 Cockpit Reference Guide for the Cessna Nav III; Garmin
• Page 7 – RECORD OF REVISIONS; Part Number
• Page 8 – Revision Date of Revision Affected Pages
• Page 9 – TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
• Page 10 – ii; SECTION 7: NAVIGATION
• Page 11 – iii; SECTION 11: ABNORMAL OPERATION
• Page 12 – Blank Page
• Page 13 – SECTION 1; The purpose of this Cockpit Reference Guide is; The pilot should read and thoroughly
• Page 17 – Softkey OFF; Figure 1-3 INSET Softkeys; INSET
• Page 18 – Figure 1-4 PFD Configuration Softkeys; PFD
• Page 19 – OBS; XPDR
• Page 20 – Figure 1-6 MFD Softkeys
• Page 21 – Figure 1-7 Page Group Icon; Turn the large; Knob; FMS; Knob; to select pages within the
• Page 22 – VERTICAL NAVIGATION; All arrival procedure altitudes contained in
• Page 23 – White Text; Table 1-1 VNV Altitude Text Size and Color; Refer to Figure 1-8 and Table 1-1 for more detail; Figure 1-8 VNAV Altitudes; Some altitudes retrieved from the database have; Figure 1-9 Altitude Restrictions; See Section 7 - Navigation, for a sample flight plan
• Page 24 – Figure 1-10 PFD Setup Menu Window; XM Radio audio is automatically muted when the; DATABASE UPDATES; The G1000 System uses Secure Digital (SD) cards to; Jeppesen Aviation Database; After the aviation database is installed,
• Page 25 – Figure 1-12 Database Update Confirmation; Garmin Databases; Since these databases are not stored internally in the; The data contained in the terrain and; ENT; Key or the right most softkey.; MAP; Softkey and check to make sure that the; TOPO; and; TERRAIN; and other database features are functioning.
• Page 27 – SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
• Page 28 – Figure 2-2 Additional PFD Information; Active Flight Plan Leg
• Page 29 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer at Vne; Speed Ranges; ON; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
• Page 30 – Figure 2-7 Altimeter; Selected Altitude Bug; The Selected Altitude Bug is displayed at the Selected; Altitude Trend Vector; The end of the trend vector displays approximately; Barometric Setting Box; Select barometric pressure:; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Visual annunciations appear in the Altitude Reference
• Page 31 – Low Altitude Annunciation; The LOW ALT annunciation is only available; When the Final Approach Fix (FAF) is the active; Figure 2-10 Low Altitude on GPS Approach; Low Altitude
• Page 32 – GLIDESLOPE INDICATOR; The Vertical Deviation and Required Vertical Speed; Figure 2-11 Vertical Deviation Indications; Figure 2-12 Glidepath Indicator; The Glideslope Indicator appears when an ILS approach; Figure 2-13 Glideslope Indicator
• Page 33 – MARKER BEACON ANNUNCIATIONS; Figure 2-14 Marker Beacon Annunciations; VERTICAL SPEED INDICATOR; Figure 2-15 Vertical Speed Indicator; VS; BAROMETRIC ALTITUDE MINIMUMS; Figure 2-16 Barometric Minimum Descent Altitude Settings
• Page 34 – Figure 2-17 Barometric Minimum Descent Altitude; Altitude Reached; HORIZONTAL SITUATION INDICATOR; Figure 2-18 Horizontal Situation Indicator
• Page 35 – Tick marks to the left and right of the lubber line; Figure 2-20 Standard-Rate Turn Indication; Course Pointer; The course pointer is a single line arrow (GPS, VOR1; Figure 2-21 Course Pointer; The CDI scale automatically adjusts to the current; Flight Phase; depending on variables (see
• Page 36 – Figure 2-22 Phases of Flight/CDI Scaling; Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling; Figure 2-24 Typical LNAV/VNAV and LPV Approach CDI Scaling
• Page 37 – Figure 2-25 HSI with Bearing Information; Figure 2-28 DME Information Window; Navigation Source; CDI
• Page 38 – GPS waypoint sequencing is suspended.; The; Softkey is only displayed when; When the window is selected for display, but wind; Option 1; Figure 2-30 Wind Data Window
• Page 39 – Figure 2-31 Timer Status Prompts; large
• Page 41 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; Refer to the Pilot’s Operating Handbook; Model
• Page 42 – Fuel Quantity Indicator (FUEL QTY GAL)
• Page 44 – The pilot should follow the engine man-
• Page 45 – Hollow Block
• Page 46 – Cruise
• Page 47 – Fuel calculations do not use the aircraft
• Page 48 – Engine Manifold Pressure Gauge (MAN IN)
• Page 51 – TRANSPONDER; The NAV/COM controls and frequency boxes share the
• Page 52 – Figure 4-2 Frequency Fields
• Page 53 – RADIO STATUS INDICATIONS; RX; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; Squelch; Figure 4-7 Squelch Indication; COM Frequency Transfer; OPTIONAL NAV RADIOS; DME; Figure 4-8 Radio Tuning Window; Figure 4-9 DME Selection Window
• Page 54 – NRST; Auto-tuning on the MFD; Figure 4-11 Ground Mode; Code Number and; Figure 4-12 Standby Mode; Manual ON Mode; ON Mode
• Page 55 – Altitude Mode is automatically selected when the; Figure 4-14 Altitude Mode; Reply Status; When the transponder sends replies to interrogations,; Figure 4-15 Reply Indication; Reply; Code Selection; VFR Code Selection; The pre-programmed VFR Code is set at; Enter Code Using Softkeys
• Page 56 – If so configured, the Flight ID may be entered in the
• Page 57 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Front Panel Controls
• Page 58 – COM RADIO SELECTION; COM1 MIC; Figure 5-2 Transceivers; SPKR; Figure 5-3 Passenger Address and Speaker Keys; MARKER BEACON RECEIVER; MUTE; Outer Marker; Figure 5-4 Marker Beacon Annunciators on the PFD; Marker Beacon Signal Sensitivity; HI SENS
• Page 59 – Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Pressing; Figure 5-6 Navigation Radios; Press the; Figure 5-7 ICS Isolation
• Page 60 – INTERCOM SQUELCH CONTROL; Figure 5-9 Clearance Recorder Play Key
• Page 61 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 Dedicated AFCS Controls; AP DISC; MET
• Page 62 – FLIGHT DIRECTOR OPERATION; Activating the Flight Director; AFCS Status Box; FD; Command Bars; Figure 6-2 Command Bars
• Page 63 – FLIGHT DIRECTOR MODES; Figure 6-4 Loss of VOR Signal; Pitch Modes
• Page 64 – Table 6-1 lists the pitch modes with their corresponding; ALTS; the Selected Altitude.; Table 6-1 Flight Director Pitch Modes
• Page 65 – Figure 6-5 Pitch Hold Mode; Changing the Pitch Reference
• Page 66 – Figure 6-6 Automatic Mode Transitions During Altitude Capture; Flash Up to 10 sec, Indicating Automatic Transition; Changing the Selected Altitude; Pressing the; CWS; ALT; Turning the; ALT; Knob while in Altitude; CWS
• Page 67 – If the Selected Altitude is reached during CWS; Figure 6-7 Altitude Hold Mode; In Vertical Speed Mode, the flight director acquires
• Page 68 – Figure 6-8 Vertical Speed Mode; Changing the Vertical Speed Reference; The Selected Altitude should be set before; FLC
• Page 69 – Changing the Airspeed Reference; Figure 6-9 Flight Level Change Mode
• Page 70 – Figure 6-10 Vertical Path Tracking Armed Annunciations; VNV
• Page 71 – In conjunction with the “TOD [top of descent] within 1; Figure 6-11 Vertical Path Capture
• Page 72 – Figure 6-12 Vertical Path Tracking Mode; Automatic Pitch Hold Reversion
• Page 73 – Figure 6-13 Flight Level Change VNAV Non-Path Descent; Armed VNAV Target Altitude and Selected; Flash up to 10 sec, Indicating Automatic Transition; Figure 6-14 VNAV Altitude Capture; Changing the VNAV Target Altitude; Button while in VNAV
• Page 74 – Button while Glidepath; Figure 6-15 Glidepath Mode; APR
• Page 75 – Figure 6-16 Glidepath Mode Armed; If vertical guidance becomes or is expected to become; Button while Glideslope; Figure 6-17 Glideslope Mode; Glideslope Mode is available for LOC/ILS approaches; Figure 6-18 Glideslope Mode Armed; Once the localizer has been set as the navigation
• Page 76 – Pushing the; Figure 6-19 Go Around Mode
• Page 77 – Table 6-2 Roll Modes
• Page 78 – Bank Angle; Rolls wings level; Table 6-3 Roll Hold Mode Responses; Changing the Roll Reference; Figure 6-21 Heading Select Mode; Heading Select Mode is activated by pressing; HDG; Knob synchronizes the; The Selected Heading is adjusted using the
• Page 79 – The selected navigation receiver must have; Figure 6-22 Navigation Mode; NAV; Figure 6-23 GPS Navigation Mode Armed
• Page 80 – Changing the Selected Course
• Page 81 – When making a backcourse approach,; Backcourse Mode captures and tracks a localizer; Glideslope Mode Active; Figure 6-25 Backcourse Mode
• Page 82 – AUTOPILOT OPERATION; Refer to the AFM for specific instructions; Flight Control; Pitch Axis and Pitch Trim; Roll Axis; Engaging the Autopilot; Autopilot engagement/disengagement is; Button to disengage the; AP; Figure 6-26 Autopilot Engaged; Autopilot Engaged
• Page 83 – Figure 6-27 CWS Annunciation; Control Wheel Steering; Disengaging the Autopilot; Figure 6-28 Automatic Autopilot Disengagement; Autopilot Automatically Disengaged; Figure 6-29 Manual Autopilot Disengagement; Autopilot Manually Disengaged
• Page 84 – EXAMPLE PROCEDURES; The diagrams in this section are for instruc-; This section provides a scenario-based set of procedures; Figure 6-30 Flight Plan Overview
• Page 85 – Figure 6-31 Departure
• Page 86 – During climb-out, the autopilot continues to fly the; Intercepting a VOR radial:; Arm VOR Navigation Mode:; e CDI; Softkey to set the navigation; CRS; Knob to set the Selected Course to; Figure 6-32 Intercepting a VOR Radial; Key. This arms VOR Navigation
• Page 87 – Changing the navigation source cancels; As the aircraft closes on Salina VOR, GPS is used to; Flying a GPS flight plan:; Transition from VOR to GPS Navigation Mode:; Softkey until GPS is the selected; Flashes up to 10 sec, Transitions to Roll Hold; Figure 6-33 Transition to GPS Flight Plan; Key to activate GPS Navigation; Key is not pressed within 10 seconds
• Page 88 – While flying the arrival procedure, the aircraft is; Flight Level Change descent:; Select Flight Level Change Mode:; Knob, set the Selected Altitude to; Figure 6-34 FLC Descent; Key to activate Flight Level Change
• Page 89 – Figure 6-35 VPTH Descent
• Page 90 – Knob, set the Selected Altitude; Key before the planned TOD
• Page 91 – Flying an ILS approach:; KCOS; Figure 6-37 ILS Approach to KCOS
• Page 92 – Flying a WAAS precision approach:; Figure 6-38 LPV Approach to KCOS
• Page 93 – As a result of calculations performed by; Flying a missed approach:; Flashes 5 sec
• Page 94 – AFCS ANNUNCIATIONS AND ALERTS; AFCS Status Alerts; Figure 6-40 AFCS Status Annunciation; AFCS Status; Table 6-4 AFCS Status Field Alerts
• Page 95 – Overspeed protection is provided in situations where; Figure 6-41 Overspeed Annunciation; Airspeed
• Page 97 – SECTION 7 – NAVIGATION; The majority of the following discussions pertain to; NAVIGATION MAP PAGE; The map display should only be; Select the MAP Page Group; Direct-to Navigation from the MFD; Enter a Direct-to Destination
• Page 99 – Manually Define the Active Direct-to; Figure 7-6 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
• Page 101 – Cancelling Direct-to Navigation; NAVIGATING AN EXAMPLE FLIGHT; The following example flight plan is; The following discussion is an example of navigating a; If the loaded arrival procedure has
• Page 103 – Figure 7-13 Begin Adding V4 to the Flight Plan; Figure 7-14 Entering V4 Entry Point; Figure 7-15 TOP Inserted into the Flight Plan
• Page 104 – Figure 7-16 List of Available Airways for TOP
• Page 105 – Figure 7-19 V4 is Loaded in the Flight Plan; Figure 7-20 Comfirm Active Leg; Figure 7-21 V4 Now Active Leg
• Page 106 – Figure 7-22 Turn on to Active Leg
• Page 107 – Figure 7-25 HYS to LAA Leg Active; Figure 7-26 Direct To OPSHN; Figure 7-27 Enter VNV Altitude
• Page 108 – Figure 7-28 Enter VNV Offset Distance; Key. The altitude entry; PROC
• Page 109 – b) ‘SELECT APPROACH’ should be highlighted as; Figure 7-30 Procedures Window; Key. A list of available approaches; Figure 7-31 List of Available Approaches; Knob to select the LPV approach; Key. A list of available transitions; Figure 7-32 List of Available Transitions; Knob to select the desired
• Page 110 – Figure 7-33 Loaded Approach; Figure 7-34 Vertical Guidance is Active to the FAF
• Page 111 – VNV PROF; Figure 7-35 Adjusting the Descent
• Page 112 – Upon reaching TOD, a descent vertical speed is; Figure 7-38 VDI & RVSI Showing Correctly Established Descent; When the aircraft is one minute from the bottom; Figure 7-40 Turn to intercept OPSHN to FSHER Leg
• Page 113 – After passing OPSHN, the next leg of the arrival; Figure 7-41 Tracking the OPSHN to FSHER Leg; The flight continues through the arrival procedure; Figure 7-42 Approaching PYNON
• Page 114 – Upon passing PYNON the approach procedure; Figure 7-43 Approach Leg is Now Active; Knob to highlight ‘ACTIVATE; Figure 7-44 Activate Missed Approach; Key to activate the approach.; Figure 7-45 Descending Turn to the Initial Approach Fix (IAF)
• Page 115 – After crossing FALUR the next waypoint is the; Figure 7-46 Descending to the FAF; After crossing CEGIX, the aircraft continues; Figure 7-47 Descending to the Missed Approach Point
• Page 116 – SUSP; Figure 7-48 Missed Approach Active
• Page 117 – Figure 7-49 Establishing the Holding Pattern; AIRPORT INFORMATION; Figure 7-51 Airport Information Page; Select the Airport Information Page
• Page 118 – Select an Airport from the Active Flight Plan; Figure 7-52 Flight Plan Airport List; Select a Nearest Airport; Figure 7-53 Nearest Airport List; Select a Recently Entered Airport Identifier; Figure 7-54 Recently Entered Airports List
• Page 119 – Access Runway Information; INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-55 Intersection Information Page; Access Information on an Intersection
• Page 120 – Figure 7-56 NDB Information Page; Select the NDB Information Page; View Information on a Specific NDB; Figure 7-57 VOR Information Page; Select the VOR Information Page; Access Information on a VOR
• Page 121 – USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-58 Nearest Airports Page; Nearest Airport Information on the MFD; Select the Nearest Airports Page
• Page 122 – Figure 7-59 Nearest Airports Window; NEAREST INTERSECTIONS; Figure 7-60 Nearest Intersections Page; Select the Nearest Intersections Page; View Information on the Nearest Intersection
• Page 123 – Figure 7-61 Nearest NDB Page; Select the Nearest NDB Page; Access Information on a Specific NDB; Figure 7-62 Nearest VOR Page; Select the Nearest VOR Page; View Information on the Nearest VOR; Select and Load a VOR Frequency
• Page 124 – NEAREST USER WAYPOINT; Figure 7-63 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; Select a Nearest User Waypoint; Knob to activate the cursor.; NEAREST FREQUENCIES; Figure 7-64 Nearest Frequencies Page; Select the Nearest Frequencies Page; Select and Load the Nearest ARTCC, FSS, or
• Page 125 – NEAREST AIRSPACES; Figure 7-65 Nearest Airspaces Page; Select the Nearest Airspaces Page; Airspace Alerts Box; • If the projected course takes the aircraft inside an; View Additional Details for a Listed Airspace; View and Quickly Load the Frequency for a
• Page 127 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; The following discussions pertain to the Multi Function; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page; Create a New User Waypoint; Modify a User Waypoint; Delete a User Waypoint; the
• Page 128 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Window on the PFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page; ob
• Page 129 – ACTIVATE A FLIGHT PLAN LEG; Figure 8-5 Activate Flight Plan Leg Confirmation; STOP NAVIGATING A FLIGHT PLAN; Figure 8-6 Delete Flight Plan; INVERT ACTIVE FLIGHT PLAN; Key; Figure 8-8 Invert Flight Plan
• Page 130 – CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD; Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the; Figure 8-12 Creating Flight Plan on the PFD
• Page 131 – ENTER AN AIRWAY IN A FLIGHT; FPL; Figure 8-13 Airway Insertion Point; Figure 8-14 Load Airway Entry Point; Figure 8-15 Airway Entry Point Loaded; Figure 8-16 Enter Airway Identifier; LD
• Page 132 – Figure 8-17 Select Desired Exit Point; LOAD A DEPARTURE; STORE A FLIGHT PLAN; Figure 8-19 Store Flight Plan Confirmation
• Page 133 – Figure 8-20 Remove Waypoint Confirmation
• Page 134 – DELETE A FLIGHT PLAN; GRAPHICAL FLIGHT PLAN CREATION; ABOVE; Figure 8-21 Trip Planning Page; Starting WPT; Or
• Page 135 – The Page Mode must be set to MANUAL
• Page 137 – SECTION 9 – PROCEDURES; SECTION 9: PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Figure 9-2 Select Departure Transition; Load and Activate An Arrival Procedure; If any portion of an arrival procedure is
• Page 138 – Knob to; to select the desired; Not all approaches in the database are approved for GPS; WAAS systems only
• Page 139 – Figure 9-6 Selecting an Approach Procedure; Figure 9-7 Selecting an Approach Transition; Activate An Approach in the Active Flight Plan
• Page 141 – SECTION 10 – HAZARD; SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Menu; Figure 10-1 Page Menu; Strike is less than 6 seconds old
• Page 142 – At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page
• Page 143 – ARC; XM Weather is not intended to; Figure 10-7 Navigation Map Page Displaying NEXRAD Weather; WX; Figure 10-8 METAR and TAF Text Displayed on the; METAR
• Page 144 – Figure 10-9 Weather Data Link Page; NEXRAD Limitations; Strikes depicted represent cloud to ground
• Page 145 – Joystick; Weather Products & Symbols
• Page 146 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group; From within the AUX - XM INFORMATION Page, the pilot; LOCK; Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
• Page 147 – TRAFFIC SYSTEMS; Traffic Information Service (TIS) is only; Displaying Traffic on the Traffic Map Page; Figure 10-11 Traffic Map Page; Displaying Traffic on the Navigation Map
• Page 148 – Refer to the Honeywell KTA 870 Pilot’s Guide for a; System Self Test; Figure 10-12 Self Test OK Display; Figure 10-13 Traffic Map Page
• Page 149 – TRAFFIC; Softkey. Traffic is now displayed; Figure 10-14 TAS Traffic on Navigation Map; ADS-B is limited to displaying traffic in the G1000.; Symbol; Traffic Advisory without directional information.; Figure 10-15 Example ADS-B Traffic Advisory
• Page 150 – TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Figure 10-16 Obstacle Symbols
• Page 151 – Red; Displaying Terrain on the TAWS Page
• Page 152 – MENU; Figure 10-20 TAWS Page Menu; TAWS Inhibit; Flying VFR into an area where unique terrain exists; INHIBIT; If TAWS alerts are inhibited when the Final
• Page 153 – A system test is automatically performed at power-up.; OK; Enroute; A Premature Descent Alert is issued when the system; Figure 10-21 PDA Alerting
• Page 154 – The purpose of the Excessive Descent Rate alert is to; Figure 10-22 Excessive Descent Rate; Negative Climb Rate After Takeoff; The purpose of the Negative Climb Rate After Takeoff; Figure 10-23 Negative Climb Rate; “Five-Hundred” Aural Alert; The purpose of the aural alert message “Five-hundred”; Displaying Terrain and Obstacles on the; With the Navigation Map displayed, press the; Softkey. Terrain and obstacle
• Page 155 – When a terrain or obstacle alert is issued, a pop-up; Figure 10-25 TAWS Symbols
• Page 156 – Alert Type
• Page 157 – The following system status annunciations may also be; Alert Annunciations; Figure 10-26 Alert Annunciation on the TAWS Page; Alert Annunciation; Figure 10-27 TAWS Alert Annunciation on the PFD
• Page 159 – SECTION 11 – ABNORMAL; SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary display mode can also be manually; The Cessna Pilot’s Operating Handbook
• Page 160 – Figure 11-2 Extreme Pitch Indication
• Page 161 – DR Mode is inherently less accurate; Symbolic Aircraft
• Page 162 – Also, while the G1000 is in DR Mode, the autopilot
• Page 163 – SECTION 12 – ANNUNCIATIONS; The Cessna aircraft Pilot’s Operating
• Page 164 – ALERT LEVEL DEFINITIONS
• Page 165 – NAV III AIRCRAFT ALERTS; The following alerts are configured specifically for the; WARNING Alerts; OIL PRESSURE; Aural tone is inhibited while the aircraft is on the ground.; CAUTION Alerts; LOW VACUUM; CO GUARDIAN MESSAGES; CO DET SRVC
• Page 166 – The following alert annunciations appear in the AFCS; Condition; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
• Page 168 – The following system status annunciations may also be issued.
• Page 169 – System Annunciation
• Page 171 – Figure 12-6 G1000 System Failure Annunciations
• Page 175 – Message
• Page 179 – TRUE APR
• Page 185 – INDEX; Signal augmentation 5-2
• Page 186 – Forward Looking Terrain Avoidance
• Page 187 – Vertical Navigation flight control 6-