Garmin Software Version 0563.11- User Manual

Table of Contents:

• Page 5 – Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
• Page 9 – RECORD OF REVISIONS; Part Number; Updated system software numbers
• Page 10 – Production release
• Page 12 – ii; TABLE OF CONTENTS
• Page 13 – iii
• Page 14 – iv; Blank Page
• Page 15 – SECTION 1; SECTION 1: SYSTEM OVERVIEW; The purpose of this Cockpit Reference Guide is; The pilot should read and thoroughly
• Page 19 – Softkey OFF; Figure 1-3 INSeT Softkeys; INSET; Cycles through traffic display options:; TERRAIN – Press to display terrain information on
• Page 20 – Figure 1-4 PFD Configuration Softkeys; PFD
• Page 21 – OBS
• Page 23 – EXIT; Figure 1-6 MFD Softkeys; Turn the large; Knob; FMS; Knob; to select pages within the
• Page 24 – VERTICAl NAVIGATION; All arrival procedure altitudes contained in
• Page 25 – White Text; Table 1-1 VNV Altitude Text Size and Color; Some altitudes retrieved from the database have; Figure 1-9 Altitude Restrictions; See Section 7 - Navigation, for a sample flight plan
• Page 26 – Figure 1-10 PFD Setup Menu Window; DATABASE UPDATES; The G1000 System uses Secure Digital (SD) cards; Do not load Jeppesen navigation data; Jeppesen Aviation Database; After the aviation database is installed,
• Page 27 – 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
• Page 29 – SECTION 2; SECTION 2: FlIGhT INSTRUMENTS; Figure 2-1 Default PFD Information
• Page 30 – Figure 2-2 Additional PFD Information; Active Flight Plan Leg
• Page 31 – 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 32 – 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 33 – Metric Display; 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 34 – 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 is tuned; Figure 2-13 Glideslope Indicator
• Page 35 – 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; • When the aircraft altitude descends to within 2500
• Page 36 – Figure 2-17 Barometric Minimum Descent Altitude; Altitude Reached; hORIZONTAl SITUATION INDICATOR; Figure 2-18 Horizontal Situation Indicator
• Page 37 – Turn Rate Indicator and heading Trend Vector; 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 38 – 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 39 – Bearing Pointers and Information Windows; Figure 2-25 HSI with Bearing Information; Figure 2-28 DMe Information Window; Navigation Source; CDI
• Page 40 – The; Softkey is only displayed when; When the window is selected for display, but wind; Option 1; Figure 2-30 Wind Data Window
• Page 41 – Figure 2-31 Timer Status Prompts; large
• Page 43 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; Refer to the Pilot’s Operating Handbook; Model
• Page 44 – Exhaust Gas Temperature Indicator (EGT)
• Page 45 – – A numeric readout gives the time (in
• Page 46 – The pilot should follow the engine manu-
• Page 47 – Hollow Block
• Page 48 – Cruise
• Page 49 – Normally-aspirated Aircraft; Fuel calculations do not use the aircraft
• Page 50 – – Displays the engine
• Page 51 – – Shows
• Page 53 – TRANSPONDER; The NAV/COM controls and frequency boxes share the
• Page 54 – Figure 4-2 Frequency Fields
• Page 55 – 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 56 – Auto-tuning on the PFD; 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 57 – 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 58 – Flight ID Reporting; If so configured, the Flight ID may be entered in the
• Page 59 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEl; Figure 5-1 Front Panel Controls
• Page 60 – 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 61 – Figure 5-5 Marker Beacon; NAV RADIO AUDIO SElECTION; Pressing; Figure 5-6 Navigation Radios; Press the; Figure 5-7 ICS Isolation
• Page 62 – INTERCOM SQUElCh CONTROl; Figure 5-9 Clearance Recorder Play Key; • Pressing the
• Page 63 – SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FlIGhT; Figure 6-1 Dedicated AFCS Controls; AP DISC; MET
• Page 64 – FlIGhT DIRECTOR OPERATION; Activating the Flight Director; AFCS Status Box; FD; Command Bars; Figure 6-2 Command Bars
• Page 65 – FlIGhT DIRECTOR MODES; Figure 6-4 Loss of VOR Signal; Pitch Modes
• Page 66 – Table 6-1 lists the pitch modes with their corresponding; ALTS; the Selected Altitude.; Table 6-1 Flight Director Pitch Modes
• Page 67 – Figure 6-5 Pitch Hold Mode; Changing the Pitch Reference
• Page 68 – Altitude Reference (in this; 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 69 – If the Selected Altitude is reached during CWS; Figure 6-7 Altitude Hold Mode; In Vertical Speed Mode, the flight director acquires
• Page 70 – Figure 6-8 Vertical Speed Mode; Changing the Vertical Speed Reference; The Selected Altitude should be set before; FLC
• Page 71 – Changing the Airspeed Reference; Figure 6-9 Flight Level Change Mode
• Page 72 – VNV; Figure 6-10 Vertical Path Tracking Armed Annunciations
• Page 73 – In conjunction with the “TOD [top of descent] within 1; Figure 6-11 Vertical Path Capture
• Page 74 – Figure 6-12 Vertical Path Tracking Mode; Automatic Pitch Hold Reversion
• Page 75 – Figure 6-13 Flight Level Change VNV Non-Path Descent; • At least ten seconds have passed since the non-path; Armed VNAV Target Altitude and Selected; Figure 6-14 VNAV Altitude Capture; Changing the VNAV Target Altitude; Button while in VNAV
• Page 76 – Changing the current VNAV Target Altitude while; Button while Glidepath; Figure 6-15 Glidepath Mode; Glidepath mode is used to track the WAAS-based
• Page 77 – 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 78 – Pushing the; Figure 6-19 Go Around Mode; Command Bars Indicate Climb
• Page 79 – Roll Modes; Table 6-2 Roll Modes
• Page 80 – 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 81 – The selected navigation receiver must have; Figure 6-22 Navigation Mode; NAV; Figure 6-23 GPS Navigation Mode Armed
• Page 82 – • Different VOR is tuned while in VOR Navigation; Changing the Selected Course
• Page 83 – When making a backcourse approach,; Backcourse Mode captures and tracks a localizer; Figure 6-25 Backcourse Mode
• Page 84 – 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 85 – Figure 6-27 CWS Annunciation; Control Wheel Steering; Disengaging the Autopilot; • Invalid sensor data; Figure 6-28 Automatic Autopilot Disengagement; Autopilot Automatically Disengaged; Figure 6-29 Manual Autopilot Disengagement; Autopilot Manually Disengaged
• Page 86 – EXAMPlE PROCEDURES; The following example flight plan and; This scenario-based set of procedures (based on the; Figure 6-30 Flight Plan Overview; Departure
• Page 87 – Use the; Knob to set the Selected Heading,; Key to activate Heading Select Mode; Figure 6-31 Departure
• Page 88 – Intercepting a VOR Radial; During climb-out, the autopilot continues to fly the; Figure 6-32 Intercepting a VOR Radial
• Page 89 – Flying a Flight Plan/GPS Course; Changing the navigation source cancels; As the aircraft closes on Salina VOR, GPS is used; Transition from VOR to GPS Navigation Mode:; Softkey until GPS is the selected; Key to activate GPS Navigation; Figure 6-33 Transition to GPS Flight Plan
• Page 90 – Descent; While flying the arrival procedure, the aircraft is; Select Flight Level Change Mode:; Knob, set the Selected Altitude to; Figure 6-34 FLC Descent; Key to activate Flight Level Change
• Page 91 – Figure 6-35 VPTH Descent; • Turn the ALT Knob to adjust the Selected
• Page 92 – Knob, set the Selected Altitude; Key before the planned TOD
• Page 93 – Approach; • Push the; AP DISC; • U s e t h e; G A; Figure 6-37 ILS Approach to KCOS
• Page 94 – Figure 6-38 LPV Approach to KCOS
• Page 95 – Go Around/Missed Approach; As a result of calculations performed by; Flashes 5 sec
• Page 96 – AFCS ANNUNCIATIONS AND AlERTS; AFCS Status Alerts; Figure 6-40 AFCS Status Annunciation; AFCS Status; Table 6-4 AFCS Status Field Alerts
• Page 97 – Overspeed Protection; Overspeed protection is provided in situations where; Figure 6-41 Overspeed Annunciation; Airspeed
• Page 99 – SECTION 7 – NAVIGATION; 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 101 – Manually Define the Active Direct-to; Figure 7-6 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
• Page 103 – 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 105 – 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 106 – Figure 7-16 List of Available Airways for TOP
• Page 107 – Figure 7-19 V4 is Loaded in the Flight Plan; Figure 7-20 Comfirm Active Leg; Figure 7-21 V4 Now Active Leg
• Page 108 – Figure 7-22 Turn on to Active Leg
• Page 109 – Figure 7-25 HYS to LAA Leg Active; Figure 7-26 Direct To OPSHN; Figure 7-27 enter VNV Altitude
• Page 110 – Figure 7-28 enter VNV Offset Distance; Key. The altitude entry; PROC
• Page 111 – 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 112 – Figure 7-33 Barometric Minimums enabled
• Page 113 – Figure 7-36 Vertical Guidance is Active to the FAF; VNV PROF; Figure 7-37 Adjusting the Descent
• Page 114 – As seen in Figure 7-38, the aircraft is approaching; Figure 7-40 VDI & RVSI Showing Correctly established Descent; When the aircraft is one minute from the bottom
• Page 115 – The aircraft is approaching OPSHN. The upcoming; Figure 7-42 Turn to intercept OPSHN to FSHeR Leg; After passing OPSHN, the next leg of the arrival; Figure 7-43 Tracking the OPSHN to FSHeR Leg; The flight continues through the arrival procedure
• Page 116 – Figure 7-44 Approaching PYNON; Upon passing PYNON the approach procedure; Figure 7-45 Approach Leg is Now Active; Knob to highlight ‘ACTIVATE; Figure 7-46 Activate Missed Approach; Key to activate the approach.
• Page 117 – The IAF is the next waypoint. At the TOD, establish; Figure 7-47 Descending Turn to the Initial Approach Fix (IAF); After crossing FALUR the next waypoint is the; Figure 7-48 Descending to the FAF
• Page 118 – Figure 7-49 Descending to the Missed Approach Point; Keep Vertical; SUSP
• Page 119 – A direct-to is initiated to MOGAL, which is the; Figure 7-50 Missed Approach Active; The aircraft continues climbing to “AT or ABOVE”; Figure 7-51 establishing the Holding Pattern; The aircraft maintains 10,000 feet while following; Figure 7-52 Hold established
• Page 120 – AIRPORT INFORMATION; Figure 7-53 Airport Information Page; Select the Airport Information Page; Select an Airport from the Database; Select an Airport from the Active Flight Plan; Figure 7-54 Flight Plan Airport List; Select a Nearest Airport; Figure 7-55 Nearest Airport List
• Page 121 – Select a Recently Entered Airport Identifier; Figure 7-56 Recently entered Airports List; Access Runway Information; TX’ – transmit only
• Page 122 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-57 Intersection Information Page; Access Information on an Intersection; Figure 7-58 NDB Information Page; Select the NDB Information Page; View Information on a Specific NDB
• Page 123 – Figure 7-59 VOR Information Page; Select the VOR Information Page; Access Information on a VOR; USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-60 Nearest Airports Page; Nearest Airport Information on the MFD; Select the Nearest Airports Page
• Page 124 – Access Information on a Specific Airport; Nearest Airports Information on the PFD; Figure 7-61 Nearest Airports Window
• Page 125 – NEAREST INTERSECTIONS; Figure 7-62 Nearest Intersections Page; Select the Nearest Intersections Page; View Information on the Nearest Intersection; Figure 7-63 Nearest NDB Page; Select the Nearest NDB Page; Access Information on a Specific NDB
• Page 126 – Figure 7-64 Nearest VOR Page; Select the Nearest VOR Page; View Information on the Nearest VOR; Select and Load a VOR Frequency; NEAREST USER WAYPOINT; Figure 7-65 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; Select a Nearest User Waypoint; Knob to activate the cursor.
• Page 127 – NEAREST FREQUENCIES; Figure 7-66 Nearest Frequencies Page; Select the Nearest Frequencies Page; Select and Load the Nearest ARTCC, FSS, or; NEAREST AIRSPACES; Figure 7-67 Nearest Airspaces Page; Select the Nearest Airspaces Page; Airspace Alerts Box; • If the projected course takes the aircraft inside an
• Page 128 – • If the aircraft has entered an airspace, ‘Inside’ is; View Additional Details for a Listed Airspace; View and Quickly Load the Frequency for a
• Page 129 – 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 130 – 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 131 – 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 132 – 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 133 – 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 134 – Figure 8-17 Select Desired exit Point; lOAD A DEPARTURE; STORE A FlIGhT PlAN; Figure 8-19 Store Flight Plan Confirmation
• Page 135 – Figure 8-20 Remove Waypoint Confirmation
• Page 136 – DElETE A FlIGhT PlAN; GRAPhICAl FlIGhT PlAN CREATION; ABOVE; Figure 8-21 Trip Planning Page; Starting WPT; Or
• Page 137 – The Page Mode must be set to MANUAL
• Page 139 – 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 140 – Knob to; to select the desired; Not all approaches in the database are approved for GPS; WAAS systems only
• Page 141 – load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure; Figure 9-7 Selecting an Approach Transition; Figure 9-8 Selecting Barometric Altitude
• Page 142 – Figure 9-9 entering Minimum Altitude; Activate An Approach in the Active Flight Plan
• Page 143 – SECTION 10 – HAZARD; SECTION 10: hAZARD AVOIDANCE; CUSTOMIZING ThE hAZARD; Menu; Figure 10-1 Page Menu; Strike is less than 6 seconds old
• Page 144 – 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 145 – 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 146 – Figure 10-9 Weather Data Link Page; NEXRAD Limitations; • An individual; Strikes depicted represent cloud to ground
• Page 147 – Joystick; Weather Products & Symbols
• Page 148 – 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; Weather Product
• Page 149 – TRAFFIC SYSTEMS; • If an; 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 150 – 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 151 – 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 152 – TERRAIN AND OBSTAClE PROXIMITY; Terrain data is not displayed when the; Color; RED; Figure 10-16 Obstacle Symbols
• Page 153 – Red; Displaying Terrain on the TERRAIN-SVS Page
• Page 154 – Enable/Disable Aviation Data; MeNU; Turn the small; Alerts are issued when flight conditions meet parameters; CLR
• Page 155 – Alert Type; Table 10-2 TeRRAIN-SVS System Test Status Annunciations
• Page 156 – Figure 10-21 TeRRAIN-SVS Alert Annunciations; Alert; Figure 10-22 Navigation Map Page; Alert Annunciation
• Page 157 – Terrain Inhibit; Softkey. ‘TER INHB’ is annunciated in; INHIBIT; ‘TER INHB” annunciation is removed.; If TERRAIN-SVS alerts are inhibited when; Potential Impact Points; Phase of Flight; Enroute
• Page 158 – Displaying Terrain and Obstacles on the; Displaying Terrain on the TAWS Page
• Page 159 – Figure 10-26 TAWS Page Menu; TAWS Inhibit; Flying VFR into an area where unique terrain exists; If TAWS alerts are inhibited when the Final
• Page 160 – Manual System Test; A system test is automatically performed at power-up.; OK; A Premature Descent Alert is issued when the system; Figure 10-27 PDA Alerting
• Page 161 – The purpose of the Excessive Descent Rate alert is to; Figure 10-28 excessive Descent Rate; Negative Climb Rate After Takeoff; The purpose of the Negative Climb Rate After Takeoff; Figure 10-29 Negative Climb Rate; “Five-hundred” Aural Alert; The purpose of the aural alert message “Five-hundred”; With the Navigation Map displayed, press the; MAP; TeRRAIN; Softkey. Terrain and obstacle
• Page 162 – When a terrain or obstacle alert is issued, a pop-up; Figure 10-31 TAWS Symbols
• Page 163 – TAWS Alerts Summary; The following table shows the possible TAWS alert types
• Page 164 – The following system status annunciations may also be; Alert Annunciations; Figure 10-32 Alert Annunciation on the TAWS Page; Figure 10-33 TAWS Alert Annunciation on the PFD
• Page 165 – SECTION 11 – ADDITIONAL; SECTION 11: ADDITIONAl; SVS requires a terrain database that has; SVS Operation
• Page 166 – SVS Features; Figure 11-2 SVS on the Primary Flight Display; Pathways
• Page 167 – The color of the rectangular boxes may be magenta,; Figure 11-3 Programmed and Selected Altitude; Selected; Pathways provide supplemental glidepath information
• Page 168 – Descent and Approach; Figure 11-4 SVS Pathways, enroute and Descent; From the vertical path descent, glidepath, or glideslope
• Page 169 – Missed Approach; Pathways are displayed along each segment including
• Page 170 – Flight Path Marker; The FPM is always available when the Synthetic Terrain; Flight Path; Figure 11-6 Flight Path Marker and Pathways; Zero Pitch Line; The Zero Pitch Line is drawn completely across the; Horizon Heading; The Horizon Heading is synchronized with the HSI; Traffic; Traffic symbols are displayed in their approximate
• Page 171 – Airport Signs; Airport Signs provide a visual representation of; Figure 11-7 Airport Signs; Runways; Do not use SVS runway depiction; Runway data provides improved awareness of runway; Figure 11-8 Airport Runways
• Page 172 – Terrain-SVS and TAWS Alerting; Terrain alerting on the synthetic terrain display is; Figure 11-9 Terrain Alert; Obstacles are represented on the synthetic terrain
• Page 173 – Field of View; Two dashed lines forming a V-shape in front of the; Figure 11-11 PFD and MFD Field of View Comparison; SVS View on the PFD; Figure 11-12 enabling SVS Field of View; Navigation Map Page OPTIONS Menu
• Page 174 – When viewing at ranges close enough to show the; Figure 11-13 SafeTaxi Depiction on the Navigation Map Page
• Page 175 – Figure 11-15 MAP SeTUP Menu, Aviation Group
• Page 176 – Chart Options; Figure 11-17 Approach Information Page, ALL View
• Page 177 – PROFILE; Figure 11-20 Approach Information Page, Profile View; MINIMUMS; Figure 11-21 Approach Information Page, Minimums View; FIT WIDTH
• Page 178 – Figure 11-23 FliteCharts Softkeys
• Page 179 – CHRT OPT; Figure 11-24 Airport Information Page, ALL View Selected; FIT WIDTH
• Page 180 – XM RADIO ENTERTAINMENT; Refer to the Hazard Avoidance Section; The optional XM Radio entertainment feature is; Using XM Radio; The XM Radio Page provides information and control; Figure 11-25 XM Radio Page; Active Channel and Channel List; The Active Channel Box on the XM Radio Page
• Page 181 – Category; Figure 11-26 Categories List; Presets; PRESETS
• Page 182 – Volume; VOL; Figure 11-28 Volume Control; Automatic Audio Muting; Figure 11-29 PFD Alerts Window
• Page 183 – entering a scheduler message:; highlight the first; • Event—Message issued at the specified; Deleting a scheduler message:; highlight the name
• Page 184 – ElECTRONIC ChECklISTS; The checklists presented here are for; The optional checklist functions are displayed on two; Figure 11-30 Checklist Softkeys
• Page 185 – Key to advance to the next checklist; eXIT; Softkey or hold down the; Figure 11-31 Sample Checklist
• Page 186 – From any page, press the; eMeRGCY; Figure 11-32 emergency Checklist Page example
• Page 187 – SECTION 12 – ABNORMAL; SECTION 12: 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 188 – • Windows displayed in; Figure 12-2 extreme Pitch Indication
• Page 189 – DR Mode is inherently less accurate; Symbolic Aircraft; • Navigation Status Box fields except Active Leg, TAS,
• Page 190 – Also, while the G1000 is in DR Mode, the autopilot will
• Page 191 – SECTION 13 – ANNUNCIATIONS; AlERTS; The Cessna aircraft Pilot’s Operating
• Page 192 – AlERT lEVEl DEFINITIONS
• Page 193 – NAV III AIRCRAFT AlERTS; The following alerts are configured specifically for the; CO LVL HIGH; Aural tone is inhibited while the aircraft is on the ground.; LOW FUeL L; CO GUARDIAN MESSAGES; CO DeT SRVC
• Page 194 – The following alert annunciations appear in the AFCS; Condition; Figure 13-5 AFCS System Status Annunciation; System Status Annunciation
• Page 196 – The following system status annunciations may also be issued.
• Page 197 – System Annunciation; Attitude and Heading Reference System is aligning.
• Page 198 – Display is not receiving valid heading input from AHRS.
• Page 199 – Figure 13-6 G1000 System Failure Annunciations
• Page 200 – MFD & PFD Message Advisories
• Page 201 – Database Message Advisories
• Page 203 – GMA 1347 Message Advisories; Message
• Page 205 – GIA 63W Message Advisories
• Page 208 – GEA 71 Message Advisories
• Page 209 – GRS 77 Message Advisories
• Page 210 – GDl 69/69A Message Advisories
• Page 213 – INDEX; Approach markers
• Page 214 – Load the nearest ARTCC frequency