FLIGHT INSTRUMENTS OVERVIEW SECTION 2 FLIGHT INSTRUMENTS SYSTEM

WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup INSTRUMENTS

instruments. FLIGHT

NOTE: The Automatic Flight Control System (AFCS) provides additional readouts and bugs on selected flight instruments. Refer to the AFCS Section for details on these bugs and readouts, as they appear on the display during certain AFCS modes. EIS Increased situational awareness is provided by replacing the traditional instruments on the panel with an easy- to-scan Primary Flight Display (PFD) that features a large horizon, airspeed, attitude, altitude, vertical speed, and course deviation information. In addition to the flight instruments, navigation, communication, terrain, traffic, AUDIO PANEL and weather information are also presented on the PFD and explained in other sections of this Pilot’s Guide. & CNS The following flight instruments and supplemental flight data are displayed on the PFD: UÊ
ˆÀëii`ʘ`ˆV>̜À]Êà œÜˆ˜} UÊ"ÕÌÈ`iÊ>ˆÀÊÌi“«iÀ>ÌÕÀiÊ­"
/® – Indicated airspeed UÊœÀˆâœ˜Ì>Ê-ˆÌÕ>̈œ˜Ê˜`ˆV>̜À]Êà œÜˆ˜} MANAGEMENT FLIGHT – True airspeed – Turn Rate Indicator – Trend vector – Bearing pointers and information windows qÊ
ˆÀëii`Ê>Ü>Ài˜iÃÃÊÀ>˜}ià qÊ >ۈ}>̈œ˜ÊÜÕÀVi AVOIDANCE – Vspeed reference flags – Course Deviation Indicator (CDI) HAZARD UÊ
Ì̈ÌÕ`iʘ`ˆV>̜ÀÊÜˆÌ Êψ«ÉΈ`ʈ˜`ˆV>̈œ˜ – DME Information Window UÊ
Ìˆ“iÌiÀ]Êà œÜˆ˜} UÊ/À>˜Ã«œ˜`iÀÊ œ`i]Ê œ`i]Ê>˜`Ê`i˜ÌÉ,i«Þ – Trend vector UÊ/ˆ“iÀÉ,iviÀi˜ViÃÊ7ˆ˜`œÜ]Êà œÜˆ˜} AFCS – Barometric setting – Generic timer – Reference altitude – Vspeed values UÊ6iÀ̈V>Ê iۈ>̈œ˜]ʏˆ`iϜ«i]Ê>˜`ʏˆ`i«>Ì Ê qÊ >Àœ“iÌÀˆVÊ ˆ˜ˆ“Õ“Ê iÃVi˜ÌÊ
ÌˆÌÕ`iÊ­
® ADDITIONAL FEATURES Indicators UÊ7ˆ˜`Ê`>Ì> UÊ6iÀ̈V>Ê-«ii`ʘ`ˆV>̜ÀÊ­6-® UÊ6iÀ̈V>Ê >ۈ}>̈œ˜Ê­6 6®Êˆ˜`ˆV>̈œ˜Ã APPENDICES The PFD also displays various alerts and annunciations. INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 47 FLIGHT INSTRUMENTS SYSTEM OVERVIEW 20 19 18

1 17

FLIGHT 16

INSTRUMENTS 15 2 14 EIS

13

3 12 4 & CNS 5

AUDIO PANEL AUDIO 11

6 10 7 9 FLIGHT

MANAGEMENT 8

1 NAV Frequency Box 11 Horizontal Situation Indicator (HSI) 2 Airspeed Indicator 12 Barometric Altimeter Setting HAZARD AVOIDANCE 3 True Airspeed 13 Vertical Speed Indicator (VSI) 4 Current Heading 14 Reference Altitude Bug 5 Turn Rate Indicator 15 Altimeter

AFCS 6 Heading Bug 16 Reference Altitude 7 Outside Air Temperature (OAT) 17 COM Frequency Box 8 Softkeys 18 Navigation Status Box 9 System Time 19 Slip/Skid Indicator

FEATURES 10 Transponder Data Box 20 Attitude Indicator ADDITIONAL

Figure 2-1 Primary Flight Display (Default) APPENDICES INDEX

48 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW SYSTEM

16 15 14 INSTRUMENTS FLIGHT

1

2 13 EIS 12

3 11 AUDIO PANEL 10 & CNS

4

5 9 MANAGEMENT FLIGHT

6 7 8

1 Traffic Annunciation 9 Flight Plan Window AVOIDANCE HAZARD 2 Vspeed Reference 10 Annunciation Window 3 Selected Heading 11 Selected Course 4 Wind Data 12 Current Vertical Speed 5 Inset Map 13 Glideslope Indicator AFCS 6 DME Information Window 14 Marker Beacon Annunciation 7 Bearing Information Windows 15 Terrain Annunciation 8 Minimum Descent Altitude/Decision 16 AFCS Status Annunciation

Height ADDITIONAL FEATURES

Figure 2-2 Additional PFD Information APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 49 FLIGHT INSTRUMENTS

2.1 FLIGHT INSTRUMENTS SYSTEM OVERVIEW AIRSPEED INDICATOR

NOTE: Refer to the Pilot’s Operating Handbook (POH) for airspeed criteria and Vspeed values. FLIGHT

INSTRUMENTS The
ˆÀëii`Ê ˜`ˆV>̜ÀÊ `ˆÃ«>ÞÃÊ >ˆÀëii`Ê œ˜Ê >Ê “œÛˆ˜}Ê Ì>«iÊ Àœˆ˜}Ê ˜Õ“LiÀÊ }>Õ}i°ÊÊ/ iÊ true airspeed is `ˆÃ«>Þi`ʈ˜ÊŽ˜œÌÃÊLiœÜÊÌ iÊ
ˆÀëii`ʘ`ˆV>̜À°ÊÊ/ iʘՓiÀˆVʏ>LiÃÊ>˜`ʓ>œÀÊ̈VŽÊ“>ÀŽÃʜ˜ÊÌ iʓœÛˆ˜}Ê Ì>«iÊ>ÀiÊà œÜ˜Ê>Ìʈ˜ÌiÀÛ>ÃʜvÊ£äʎ˜œÌðÊÊ/ iʓˆ˜œÀÊ̈VŽÊ“>ÀŽÃʜ˜ÊÌ iʓœÛˆ˜}ÊÌ>«iÊ>ÀiÊà œÜ˜Ê>Ìʈ˜ÌiÀÛ>ÃʜvÊ wÛiʎ˜œÌðÊÊ-«ii`ʈ˜`ˆV>̈œ˜ÊÃÌ>ÀÌÃÊ>ÌÊÓäʎ˜œÌÃ]ÊÜˆÌ ÊÈäʎ˜œÌÃʜvÊ>ˆÀëii`ÊۈiÜ>LiÊ>ÌÊ>˜ÞÊ̈“i°ÊÊ/ iÊindicated EIS >ˆÀëii`ʈÃÊ`ˆÃ«>Þi`ʈ˜Ãˆ`iÊÌ iÊL>VŽÊ«œˆ˜ÌiÀ°ÊÊ/ iÊ«œˆ˜ÌiÀÊÀi“>ˆ˜ÃÊL>VŽÊ՘̈ÊÀi>V ˆ˜}ʘiÛiÀ‡iÝVii`Êëii`Ê

(V ), at which point it turns red. & CNS

AUDIO PANEL AUDIO Vspeed References Indicated Airspeed Airspeed

FLIGHT Trend Speed Vector MANAGEMENT Ranges

True Airspeed HAZARD AVOIDANCE Figure 2-3 Airspeed Indicator (Model 182T) Figure 2-4 Red Pointer Showing Overspeed (Model 172R)

ÊVœœÀ‡Vœ`i`Ê­Ü ˆÌi]Ê}Àii˜]ÊÞiœÜ]Ê>˜`ÊÀi`®Êëii`ÊÀ>˜}iÊÃÌÀˆ«ÊˆÃʏœV>Ìi`ʜ˜ÊÌ iʓœÛˆ˜}ÊÌ>«i°ÊÊ/ iÊVœœÀÃÊ AFCS denote flaps operating range, normal operating range, caution range, and never-exceed speed (V ®°ÊÊ
ÊÀi`ÊÀ>˜}iÊ is also present for low speed awareness. / iÊ
ˆÀëii`Ê /Ài˜`Ê 6iV̜ÀÊ ˆÃÊ >Ê ÛiÀ̈V>]Ê “>}i˜Ì>Ê ˆ˜iÊ Ì >ÌÊ >««i>ÀÃÊ ÌœÊ Ì iÊ Àˆ} ÌÊ œvÊ Ì iÊ VœœÀ‡Vœ`i`Ê Ã«ii`Ê À>˜}iÊÃÌÀˆ«ÊÜ i˜Ê>ˆÀëii`ʈÃÊiˆÌ iÀÊ>VViiÀ>̈˜}ʜÀÊ`iViiÀ>̈˜}°ÊÊ"˜iÊi˜`ʜvÊÌ iʓ>}i˜Ì>ʏˆ˜iʈÃÊ>˜V œÀi`ÊÌœÊ the tip of the airspeed pointer while the other end moves continuously up or down corresponding to the rate FEATURES

ADDITIONAL of acceleration or deceleration. For any constant rate of acceleration or deceleration, the moving end of the line shows approximately what the indicated airspeed value will be in six seconds. If the trend vector crosses

V , the text of the actual airspeed readout changes to yellow. The trend vector is absent if the speed remains constant or if any data needed to calculate airspeed is not available due to a system failure. APPENDICES INDEX

50 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW SYSTEM

Vspeeds (Glide, VR, VX, and VY,®ÊV>˜ÊLiÊV >˜}i`Ê>˜`ÊÌ iˆÀÊy>}ÃÊÌÕÀ˜i`ʜ˜ÉœvvÊvÀœ“ÊÌ iÊ/ˆ“iÀÉ,iviÀi˜ViÃÊ Window. When active (on), the Vspeeds are displayed to the right of the airspeed scale. Changing Vspeeds and turning Vspeed flags on/off: INSTRUMENTS

1) Press the TMR/REF Softkey. FLIGHT 2) Turn the large FMS Knob to highlight the field of the desired Vspeed to be changed. 3) Use the FMS Knob to enter the desired value. When a speed has been changed from a default value, an asterisk appears next to the speed. 4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field. EIS 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or the TMR/REF Softkey. AUDIO PANEL & CNS MANAGEMENT FLIGHT

Figure 2-5 Timer/References Window and Menu AVOIDANCE Turning all Vspeed flags on/off: HAZARD 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) To activate all Vspeed flags, press the ENT Key with All References On highlighted. AFCS 4) To remove all Vspeed flags, turn the FMS Knob to highlight All References Off and press the ENT Key. Restoring all Vspeed defaults: ADDITIONAL

1) Press the TMR/REF Softkey. FEATURES 2) Press the MENU Key. 3) Turn the FMS Knob to highlight Restore Defaults and press the ENT Key. APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 51 FLIGHT INSTRUMENTS

ATTITUDE INDICATOR SYSTEM

OVERVIEW
Ì̈ÌÕ`iʈ˜vœÀ“>̈œ˜ÊˆÃÊ`ˆÃ«>Þi`ʜÛiÀÊ>ÊۈÀÌÕ>ÊLÕiÊÎÞÊ>˜`ÊLÀœÜ˜Ê}ÀœÕ˜`ÊÜˆÌ Ê>ÊÜ ˆÌiÊ œÀˆâœ˜Êˆ˜i°ÊÊ/ iÊ
Ì̈ÌÕ`iʘ`ˆV>̜ÀÊ`ˆÃ«>ÞÃÊÌ iÊÊ«ˆÌV ]ÊÀœ]Ê>˜`Êψ«ÉΈ`ʈ˜vœÀ“>̈œ˜°

9

FLIGHT 1 8 Roll Pointer INSTRUMENTS 1 2 Roll Scale 7 3 Horizon Line 2 4 Aircraft Symbol EIS 6 5 Land Representation 3 6 Pitch Scale 7 Slip/Skid Indicator

4 8 Sky Representation & CNS 5 9 AUDIO PANEL AUDIO Roll Scale Zero

Figure 2-6 Attitude Indicator

FLIGHT / iÊ œÀˆâœ˜Êˆ˜iʈÃÊ«>ÀÌʜvÊÌ iÊ«ˆÌV ÊÃV>i°ÊÊ
LœÛiÊ>˜`ÊLiœÜÊÌ iÊ œÀˆâœ˜Êˆ˜i]ʓ>œÀÊ«ˆÌV ʓ>ÀŽÃÊ>˜`ʘՓiÀˆVÊ

MANAGEMENT >LiÃÊ>ÀiÊà œÜ˜ÊvœÀÊiÛiÀÞÊ£äÂ]ÊÕ«Ê̜Ênä°ÊÊ ˆ˜œÀÊ«ˆÌV ʓ>ÀŽÃÊ>ÀiÊà œÜ˜ÊvœÀʈ˜ÌiÀÛi˜ˆ˜}ÊxÂʈ˜VÀi“i˜ÌÃ]ÊÕ«ÊÌœÊ ÓxÂÊLiœÜÊ>˜`Ê{xÂÊ>LœÛiÊÌ iÊ œÀˆâœ˜Êˆ˜i°ÊÊ iÌÜii˜ÊÓäÂÊLiœÜÊ̜ÊÓäÂÊ>LœÛiÊÌ iÊ œÀˆâœ˜Êˆ˜i]ʓˆ˜œÀÊ«ˆÌV ʓ>ÀŽÃÊ œVVÕÀÊiÛiÀÞÊÓ°x°ÊÊvÊÌ iÊ-Þ˜Ì ïVÊ6ˆÃˆœ˜Ê-ÞÃÌi“Ê­œ«Ìˆœ˜>®ÊˆÃÊ>V̈Û>Ìi`]ÊÌ iÊ«ˆÌV ÊÃV>iʈÃÊÀi`ÕVi`Ê̜ʣäÂÊÕ«Ê>˜`Ê Ç°xÂÊ`œÜ˜ÆÊÀiviÀÊ̜ÊÌ iÊ
``ˆÌˆœ˜>Êi>ÌÕÀiÃÊÃiV̈œ˜° HAZARD

AVOIDANCE / iʈ˜ÛiÀÌi`ÊÜ ˆÌiÊÌÀˆ>˜}iʈ˜`ˆV>ÌiÃÊâiÀœÊœ˜ÊÌ iÊÀœÊÃV>i°ÊÊ >œÀÊ̈VŽÊ“>ÀŽÃÊ>ÌÊÎäÂÊ>˜`ÊÈäÂÊ>˜`ʓˆ˜œÀÊ̈VŽÊ “>ÀŽÃÊ>ÌÊ£äÂ]ÊÓäÂ]Ê>˜`Ê{xÂÊ>ÀiÊà œÜ˜Ê̜ÊÌ iʏivÌÊ>˜`ÊÀˆ} ÌʜvÊÌ iÊâiÀœ°ÊÊ
˜}iʜvÊL>˜ŽÊˆÃʈ˜`ˆV>Ìi`ÊLÞÊÌ iÊ«œÃˆÌˆœ˜Ê of the pointer on the roll scale. The -ˆ«É-Žˆ`Ê ˜`ˆV>̜ÀÊ ˆÃÊ Ì iÊ L>ÀÊ Li˜i>Ì Ê Ì iÊ ÀœÊ «œˆ˜ÌiÀ°ÊÊ"˜iÊ L>ÀÊ `ˆÃ«>Vi“i˜ÌÊ ˆÃÊ iµÕ>Ê ÌœÊ œ˜iÊ L>Ê AFCS displacement on a traditional inclinometer. The indicator bar moves with the roll pointer and moves laterally >Ü>ÞÊvÀœ“ÊÌ iÊ«œˆ˜ÌiÀÊ̜ʈ˜`ˆV>ÌiÊ՘VœœÀ`ˆ˜>Ìi`Êyˆ} Ì°ÊÊ-ˆ«Ê­ˆ˜Ãˆ`iÊÌ iÊÌÕÀ˜®ÊœÀÊΈ`Ê­œÕÌÈ`iÊÌ iÊÌÕÀ˜®ÊˆÃÊ indicated by the location of the bar relative to the pointer. FEATURES ADDITIONAL APPENDICES Figure 2-7 Slip/Skid Indication INDEX

52 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW ALTIMETER SYSTEM The
Ìˆ“iÌiÀÊ`ˆÃ«>ÞÃÊÈääÊviiÌʜvÊL>Àœ“iÌÀˆVÊ>ÌˆÌÕ`iÊÛ>ÕiÃÊ>ÌÊ>Ê̈“iʜ˜Ê>ʓœÛˆ˜}ÊÌ>«iÊÀœˆ˜}ʘՓLiÀÊ}>Õ}i°ÊÊ Õ“iÀˆVʏ>LiÃÊ>˜`ʓ>œÀÊ̈VŽÊ“>ÀŽÃÊ>ÀiÊà œÜ˜Ê>Ìʈ˜ÌiÀÛ>ÃʜvÊ£ääÊviiÌ°ÊÊ ˆ˜œÀÊ̈VŽÊ“>ÀŽÃÊ>ÀiÊ>Ìʈ˜ÌiÀÛ>ÃʜvÊÓäÊ viiÌ°ÊÊ/ iʈ˜`ˆV>Ìi`Ê>ÌˆÌÕ`iʈÃÊ`ˆÃ«>Þi`ʈ˜Ãˆ`iÊÌ iÊL>VŽÊ«œˆ˜ÌiÀ° INSTRUMENTS FLIGHT The -iiVÌi`Ê
ÌˆÌÕ`iʈÃÊ`ˆÃ«>Þi`Ê>LœÛiÊÌ iÊ
Ìˆ“iÌiÀʈ˜ÊÌ iÊLœÝʈ˜`ˆV>Ìi`ÊLÞÊ>ÊÃiiV̈œ˜ÊLÕ}ÊÃޓLœ°ÊÊ
ÊLÕ}Ê VœÀÀi뜘`ˆ˜}Ê̜ÊÌ ˆÃÊ>ÌˆÌÕ`iʈÃÊà œÜ˜Êœ˜ÊÌ iÊÌ>«i°ÊÊvÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`iÊiÝVii`ÃÊÌ iÊÀ>˜}iÊà œÜ˜Êœ˜ÊÌ iÊ tape, the bug appears at the upper or lower edge of the tape. When the metric value is selected it is displayed ˆ˜Ê>ÊÃi«>À>ÌiÊLœÝÊ>LœÛiÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i°

ʓ>}i˜Ì>Ê
ÌˆÌÕ`iÊ/Ài˜`Ê6iV̜ÀÊiÝÌi˜`ÃÊիʜÀÊ`œÜ˜ÊÌ iʏivÌʜvÊÌ iÊ>ÌˆÌÕ`iÊÌ>«i]ÊÌ iÊi˜`ÊÀiÃ̈˜}Ê>ÌÊÌ iÊ EIS approximate altitude to be reached in six seconds at the current vertical speed. The trend vector is not shown if altitude remains constant or if data needed for calculation is not available due to a system failure.

Setting the Selected Altitude: AUDIO PANEL & CNS Turn the ALT Knob to set the Selected Altitude (large knob for 1000-ft increments, small knob for 100-ft increments). If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for the Selected Altitude. MANAGEMENT

Selected FLIGHT Altitude Selected (Meters) Altitude Selected Altitude

Bug AVOIDANCE HAZARD Indicated Altitude (Meters) Altitude Indicated Trend Altitude Vector AFCS Selected Barometric Altitude Minimums Bug Bug

Barometric ADDITIONAL

Barometric FEATURES Setting Setting Box (Hectopascals) Figure 2-8 Altimeter Settings, In Hg and Metric

ÌˆÌÕ`iÃÊV>˜Ê>ÃœÊLiÊ`ˆÃ«>Þi`ʈ˜Ê“iÌiÀðÊÊ œÌiÊÌ >ÌÊÌ iÊ>ÌˆÌÕ`iÊÌ>«iÊ`œiÃʘœÌÊV >˜}iÊÃV>i° APPENDICES Displaying altitude in meters: 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. INDEX 3) Press the METERS Softkey to turn on metric altitude readouts. 4) Press the BACK Softkey to return to the top-level softkeys.

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 53 FLIGHT INSTRUMENTS

The L>Àœ“iÌÀˆVÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}ʈÃÊ`ˆÃ«>Þi`ÊLiœÜÊÌ iÊ
Ìˆ“iÌiÀʈ˜Êˆ˜V iÃʜvʓiÀVÕÀÞÊ­ˆ˜Ê}®ÊœÀÊ iV̜«>ÃV>ÃÊ ­ *>®ÊÜ i˜Ê“iÌÀˆVÊ՘ˆÌÃÊ>ÀiÊÃiiVÌi`°ÊÊ
`ÕÃ̈˜}ÊÌ iÊ>Ìˆ“iÌiÀÊL>Àœ“iÌÀˆVÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}ÊVÀi>ÌiÃÊ`ˆÃVœ˜Ìˆ˜ÕˆÌˆiÃÊ SYSTEM OVERVIEW ˆ˜Ê6 6ÊÛiÀ̈V>Ê˜>ۈ}>̈œ˜]ʓœÛˆ˜}ÊÌ iÊ`iÃVi˜ÌÊ«>Ì °ÊÊœÀʏ>À}iÊ>`ÕÃ̓i˜ÌÃ]ʈÌʓ>ÞÊÌ>ŽiÊÃiÛiÀ>Ê“ˆ˜ÕÌiÃÊvœÀÊÌ iÊ >ˆÀVÀ>vÌÊ̜ÊÀi‡iÃÌ>LˆÃ ʜ˜ÊÌ iÊ`iÃVi˜ÌÊ«>ÌV °ÊÊvÊÌ iÊV >˜}iʈÃʓ>`iÊÜ ˆiʘi>Àˆ˜}Ê>ÊÜ>Þ«œˆ˜ÌÊÜˆÌ Ê>Ê6 6Ê/>À}iÌÊ
ÌˆÌÕ`i]ÊÌ iÊ>ˆÀVÀ>vÌʓ>ÞʘœÌÊÀi‡iÃÌ>LˆÃ ʜ˜ÊÌ iÊ`iÃVi˜ÌÊ«>Ì Êˆ˜Ê̈“iÊ̜ʓiiÌÊÌ iÊÛiÀ̈V>ÊVœ˜ÃÌÀ>ˆ˜Ì° Selecting the altimeter barometric pressure setting: FLIGHT

INSTRUMENTS Turn the BARO Knob to select the desired setting. Selecting standard barometric pressure:

EIS 1) Press the PFD Softkey to display the second-level softkeys.. 2) Press the STD BARO Softkey; STD BARO is displayed in barometric setting box (Figure 2-9). & CNS AUDIO PANEL AUDIO

Figure 2-9 Standard Barometric Altimeter Setting

FLIGHT Changing altimeter barometric pressure setting units: MANAGEMENT 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey.

HAZARD 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). AVOIDANCE Or: Press the HPA Softkey to display the barometric pressure setting in hectopascals (hPa). 4) Press the BACK Softkey to return to the top-level softkeys.
Ê >ÀœÊ/À>˜ÃˆÌˆœ˜Ê
iÀÌʈÃÊ«ÀœÛˆ`i`Ê̜ʘœÌˆvÞÊÌ iÊ«ˆœÌÊ̜ÊV >˜}iÊÌ iÊL>Àœ“iÌÀˆVÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}ÊÜ i˜ÊVÀœÃȘ}Ê AFCS Ì iÊL>ÀœÊÌÀ>˜ÃˆÌˆœ˜Ê>ÌˆÌÕ`i°ÊÊvÊÌ iÊ>ˆÀVÀ>vÌʈÃÊ>Ìʏi>ÃÌÊxääÊviiÌÊLiœÜÊÌ iÊÌÀ>˜ÃˆÌˆœ˜Ê>ÌˆÌÕ`iÊ>˜`ÊÌ i˜ÊVˆ“LÃÊ through this altitude and the STD BAROÊ-œv̎iÞÊ >ÃʘœÌÊLii˜Ê«ÀiÃÃi`]ÊÌ iÊL>Àœ“iÌÀˆVÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}Êy>à iÃÊ ˆ˜Êˆ} ÌÊLÕiÊ՘̈ÊÌ iÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}ʈÃÊV >˜}i`°ÊÊvÊÌ iÊ>ˆÀVÀ>vÌʈÃÊ>Ìʏi>ÃÌÊxääÊviiÌÊ>LœÛiÊÌ iÊÌÀ>˜ÃˆÌˆœ˜Ê>ÌˆÌÕ`iÊ >˜`ÊÌ i˜Ê`iÃVi˜`ÃÊÌ ÀœÕ} ÊÌ ˆÃÊ>ÌˆÌÕ`iÊ>˜`ÊÌ iÊL>Àœ“iÌÀˆVÊ«ÀiÃÃÕÀiÊÃiÌ̈˜}Ê >ÃʘœÌÊLii˜ÊV >˜}i`ÊvÀœ“Ê-/ Ê
,"]ÊÌ iÊÃiÌ̈˜}Êy>à iÃʈ˜Êˆ} ÌÊLÕiÊ՘̈ÊˆÌʈÃÊV >˜}i`Ê­ˆ}ÕÀiÊӇ£ä®° FEATURES ADDITIONAL Setting the Baro Transition Alert: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor.

APPENDICES 3) Turn the large FMS Knob to highlight ‘OFF or ON’ in the ‘BARO TRANSITION ALERT’ box. 4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key. 5) With the altitude field highlighted, turn the small FMS Knob to select the desired altitude and press the ENT

INDEX Key. 6) To cancel the selection, press the FMS Knob.

54 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW SYSTEM INSTRUMENTS

Pressure setting flashes during climb above Pressure setting flashes during descent below FLIGHT transition altitude if the STD BARO Softkey transition altitude to indicate setting has not has not been pressed. been changed from STD BARO. EIS AUDIO PANEL & CNS MANAGEMENT FLIGHT

Figure 2-10 Baro Transition Alert AVOIDANCE (AUX - System Setup Page) HAZARD

VERTICAL SPEED INDICATOR (VSI) The 6iÀ̈V>Ê-«ii`ʘ`ˆV>̜ÀÊ­6-®Ê`ˆÃ«>ÞÃÊÌ iÊ>ˆÀVÀ>vÌÊÛiÀ̈V>Êëii`ʜ˜Ê>ÊwÝi`ÊÃV>iÊÜˆÌ Ê>LiÃÊ>ÌÊ£äääÊ>˜`Ê AFCS ÓäääÊv«“Ê>˜`ʓˆ˜œÀÊ̈VŽÊ“>ÀŽÃÊiÛiÀÞÊxääÊv«“Ê­ˆ}ÕÀiÊӇ££®°ÊÊ ˆ}ˆÌÃÊ>««i>Àʈ˜ÊÌ iÊ«œˆ˜ÌiÀÊÜ i˜ÊÌ iÊVˆ“LʜÀÊ `iÃVi˜ÌÊÀ>ÌiʈÃÊ}Ài>ÌiÀÊÌ >˜Ê£ääÊv«“°ÊÊvÊÌ iÊÀ>ÌiʜvÊ>ÃVi˜ÌÉ`iÃVi˜ÌÊiÝVii`ÃÊÓäääÊv«“]ÊÌ iÊ«œˆ˜ÌiÀÊ>««i>ÀÃÊ>ÌÊÌ iÊ edge of the tape and the rate appears inside the pointer. ADDITIONAL

ʓ>}i˜Ì>ÊV iÛÀœ˜ÊˆÃÊ`ˆÃ«>Þi`Ê>ÃÊÌ iÊ,iµÕˆÀi`Ê6iÀ̈V>Ê-«ii`ʘ`ˆV>̈œ˜Ê­,6-®ÊvœÀÊÀi>V ˆ˜}Ê>Ê6 6Ê/>À}iÌÊ FEATURES
ÌˆÌÕ`iʜ˜ViÊÌ iʺ/" ÊQ/œ«ÊœvÊ iÃVi˜ÌRÊÜˆÌ ˆ˜Ê£Ê“ˆ˜ÕÌi»Ê>iÀÌÊ >ÃÊLii˜Ê}i˜iÀ>Ìi`°ÊÊ-iiÊÌ iʏˆ} ÌÊ >˜>}i“i˜ÌÊ >˜`Ê
 -ÊÃiV̈œ˜ÃÊvœÀÊ`iÌ>ˆÃʜ˜Ê6 6Êvi>ÌÕÀiÃ]Ê>˜`ÊÀiviÀÊ̜Ê-iV̈œ˜ÊÓ°Ó]Ê-Õ««i“i˜Ì>Êˆ} ÌÊ >Ì>]ÊvœÀʓœÀiÊ ˆ˜vœÀ“>̈œ˜Ê>LœÕÌÊ6 6ʈ˜`ˆV>̈œ˜Ãʜ˜ÊÌ iÊ* ° APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 55 FLIGHT INSTRUMENTS

VERTICAL DEVIATION SYSTEM OVERVIEW NOTE: The Glidepath Indicator is only shown for aircraft with GIA 63W Integrated Avionics Units when SBAS is available.

/ iÊ6iÀ̈V>Ê iۈ>̈œ˜Ê˜`ˆV>̜ÀÊ­6 ®ÊˆÃÊ>ʓ>}i˜Ì>ÊV iÛÀœ˜Êˆ˜`ˆV>̈˜}ÊÌ iÊL>Àœ‡6 6ÊÛiÀ̈V>Ê`iۈ>̈œ˜Ê

FLIGHT Ü i˜Ê6iÀ̈V>Ê >ۈ}>̈œ˜Ê­6 6®ÊˆÃÊLiˆ˜}ÊÕÃi`°ÊÊ/ iÊ6 Ê>««i>ÀÃʈ˜ÊVœ˜Õ˜V̈œ˜ÊÜˆÌ ÊÌ iʺ/" ÊÜˆÌ ˆ˜Ê£Ê

INSTRUMENTS “ˆ˜ÕÌi»Ê>iÀÌ°ÊÊ/ iÊ6 ʈÃÊÀi“œÛi`ÊvÀœ“ÊÌ iÊ`ˆÃ«>ÞʈvÊÛiÀ̈V>Ê`iۈ>̈œ˜ÊLiVœ“iÃʈ˜Û>ˆ`°ÊÊ-iiÊÌ iʏˆ} ÌÊ >˜>}i“i˜ÌÊ-iV̈œ˜ÊvœÀÊ`iÌ>ˆÃʜ˜Ê6 6Êvi>ÌÕÀiÃ]Ê>˜`ÊÀiviÀÊ̜Ê-iV̈œ˜ÊÓ°Ó]Ê-Õ««i“i˜Ì>Êˆ} ÌÊ >Ì>]ÊvœÀʓœÀiÊ ˆ˜vœÀ“>̈œ˜Ê>LœÕÌÊ6 6ʈ˜`ˆV>̈œ˜Ãʜ˜ÊÌ iÊ* °

EIS The ˆ`iϜ«iʘ`ˆV>̜ÀÊ>««i>ÀÃÊ̜ÊÌ iʏivÌʜvÊÌ iÊ
Ìˆ“iÌiÀÊÜ i˜iÛiÀÊ>˜Ê-ÊvÀiµÕi˜VÞʈÃÊÌ՘i`ʈ˜ÊÌ iÊ >V̈ÛiÊ
6Êwi`Ê>˜`ÊÌ iÊ>ˆÀVÀ>vÌÊ i>`ˆ˜}Ê>˜`ÊÃiiVÌi`ÊVœÕÀÃiÊ>ÀiÊÜˆÌ ˆ˜Ê£äÇ°ÊÊ
Ê}Àii˜Ê`ˆ>“œ˜`Ê>VÌÃÊ>ÃÊÌ iÊ ˆ`iϜ«iʘ`ˆV>̜À]ʏˆŽiÊ>Ê}ˆ`iϜ«iʘii`iʜ˜Ê>ÊVœ˜Ûi˜Ìˆœ˜>Êˆ˜`ˆV>̜À°ÊÊvÊ>ʏœV>ˆâiÀÊvÀiµÕi˜VÞʈÃÊÌ՘i`Ê >˜`ÊÌ iÀiʈÃʘœÊ}ˆ`iϜ«i]ʺ "Ê-»ÊˆÃÊ`ˆÃ«>Þi`ʈ˜Ê«>ViʜvÊÌ iÊ`ˆ>“œ˜`° / iÊ}ˆ`i«>Ì ÊˆÃÊ>˜>œ}œÕÃÊ̜ÊÌ iÊ}ˆ`iϜ«iÊvœÀÊ*-Ê>««Àœ>V iÃÊÃÕ««œÀ̈˜}Ê-
-ÊÛiÀ̈V>Ê}Ո`>˜ViÊ­
6³6]Ê & CNS É6
6]Ê*6®°ÊÊ7 i˜Ê>˜Ê>««Àœ>V ʜvÊÌ ˆÃÊÌÞ«iʈÃʏœ>`i`ʈ˜ÌœÊÌ iÊyˆ} ÌÊ«>˜Ê>˜`Ê*-ʈÃÊÌ iÊÃiiVÌi`ʘ>ۈ}>̈œ˜Ê AUDIO PANEL AUDIO source, the Glidepath Indicator appears as a magenta diamond during the approach. If the approach type `œÜ˜}À>`iÃÊ«>ÃÌÊÌ iÊw˜>Ê>««Àœ>V ÊwÝÊ­
®]ʺ "Ê*»ÊˆÃÊ`ˆÃ«>Þi`ʈ˜Ê«>ViʜvÊÌ iÊ`ˆ>“œ˜`° Full-scale deflection of two dots is 1000 feet. FLIGHT VNV Target MANAGEMENT Altitude

Vertical Speed HAZARD

AVOIDANCE Indicator Vertical Deviation Indicator Glideslope Glipepath Indicator Indicator AFCS Required Vertical Vertical Speed Speed Pointer Indicator FEATURES ADDITIONAL Vertical Speed and Deviation Glideslope Indicator Glidepath Indicator Indicator (VSI and VDI) Figure 2-11 Vertical Speed and Vertical Deviation Indications APPENDICES INDEX

56 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW HORIZONTAL SITUATION INDICATOR (HSI) SYSTEM The œÀˆâœ˜Ì>Ê-ˆÌÕ>̈œ˜Ê˜`ˆV>̜ÀÊ­-®Ê`ˆÃ«>ÞÃÊ>ÊÀœÌ>̈˜}ÊVœ“«>ÃÃÊV>À`ʈ˜Ê>Ê i>`ˆ˜}‡Õ«ÊœÀˆi˜Ì>̈œ˜°ÊÊiÌÌiÀÃÊ ˆ˜`ˆV>ÌiÊÌ iÊV>À`ˆ˜>Ê«œˆ˜ÌÃÊÜˆÌ Ê˜Õ“iÀˆVʏ>LiÃÊiÛiÀÞÊÎä°ÊÊ >œÀÊ̈VŽÊ“>ÀŽÃÊ>ÀiÊ>ÌÊ£äÂʈ˜ÌiÀÛ>ÃÊ>˜`ʓˆ˜œÀÊ̈VŽÊ “>ÀŽÃÊ>ÀiÊ>ÌÊxÂʈ˜ÌiÀÛ>Ã°ÊÊ
Ê`ˆ}ˆÌ>ÊÀi>`ˆ˜}ʜvÊÌ iÊVÕÀÀi˜ÌÊ i>`ˆ˜}Ê>««i>ÀÃʜ˜Ê̜«ÊœvÊÌ iÊ-]Ê>˜`ÊÌ iÊVÕÀÀi˜ÌÊ INSTRUMENTS ÌÀ>VŽÊˆÃÊÀi«ÀiÃi˜Ìi`ʜ˜ÊÌ iÊ-ÊLÞÊ>ʓ>}i˜Ì>Ê`ˆ>“œ˜`°ÊÊ/ iÊ-Ê>ÃœÊ«ÀiÃi˜ÌÃÊÌÕÀ˜ÊÀ>Ìi]ÊVœÕÀÃiÊ`iۈ>̈œ˜]Ê FLIGHT Li>Àˆ˜}]Ê>˜`ʘ>ۈ}>̈œ˜ÊÜÕÀViʈ˜vœÀ“>̈œ˜°ÊÊ/ iÊ-ʈÃÊ>Û>ˆ>Liʈ˜ÊÌܜÊvœÀ“>ÌÃ]Ê>ÊÎÈäÂÊVœ“«>ÃÃÊÀœÃiÊ>˜`Ê>Ê £{äÂÊ>ÀV° Changing the HSI display format:

1) Press the PFD Softkey EIS 2) Press the HSI FRMT Softkey. 3) Press the 360 HSI or ARC HSI Softkey. AUDIO PANEL

/ iÊÎÈäÂÊ-ÊVœ˜Ì>ˆ˜ÃÊ>Ê œÕÀÃiÊ iۈ>̈œ˜Ê˜`ˆV>̜ÀÊ­ ®]ÊÜˆÌ Ê>Ê œÕÀÃiÊ*œˆ˜ÌiÀ]Ê/œÉÀœ“ʘ`ˆV>̜À]Ê>˜`Ê>Ê & CNS ψ`ˆ˜}Ê`iۈ>̈œ˜ÊL>ÀÊ>˜`ÊÃV>i°ÊÊ/ iÊVœÕÀÃiÊ«œˆ˜ÌiÀʈÃÊ>ÊȘ}iʏˆ˜iÊ>ÀÀœÜÊ­*-]Ê6",£]Ê>˜`Ê" £®ÊœÀÊ>Ê`œÕLiÊ ˆ˜iÊ>ÀÀœÜÊ­6",ÓÊ>˜`Ê" Ó®ÊÜ ˆV Ê«œˆ˜ÌÃʈ˜ÊÌ iÊ`ˆÀiV̈œ˜ÊœvÊÌ iÊÃiÌÊVœÕÀÃi°ÊÊ/ iÊ/œÉÀœ“Ê>ÀÀœÜÊÀœÌ>ÌiÃÊÜˆÌ Ê Ì iÊVœÕÀÃiÊ«œˆ˜ÌiÀÊ>˜`ʈÃÊ`ˆÃ«>Þi`ÊÜ i˜ÊÌ iÊ>V̈ÛiÊ
6
 ʈÃÊÀiViˆÛi`° MANAGEMENT

17 16 15 FLIGHT

1 2 14 AVOIDANCE

3 HAZARD

4 13 5 12 6 11 10 AFCS 7 9 8 ADDITIONAL FEATURES 1 Turn Rate Indicator 10 To/From Indicator 2 Selected Heading 11 Heading Bug 3 Current Track Indicator 12 Course Pointer 4 Lateral Deviation Scale 13 Flight Phase APPENDICES 5 Navigation Source 14 Selected Course 6 Aircraft Symbol 15 Turn Rate and Heading Trend Vector 7 Course Deviation Indicator (CDI) 16 Current Heading 8 Rotating Compass Card 17 Lubber Line 9 OBS Mode Active INDEX

Figure 2-12 Horizontal Situation Indicator (360˚ HSI)

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 57 FLIGHT INSTRUMENTS

/ iÊ
ÀVÊ -Ê ˆÃÊ >Ê £{äÂÊ iÝ«>˜`i`Ê ÃiV̈œ˜Ê œvÊ Ì iÊ Vœ“«>ÃÃÊ ÀœÃi°ÊÊ/ iÊ
ÀVÊ -Ê Vœ˜Ì>ˆ˜ÃÊ >Ê œÕÀÃiÊ *œˆ˜ÌiÀ]Ê Vœ“Lˆ˜i`Ê/œÉÀœ“ʘ`ˆV>̜ÀÊ>˜`Ê>Êψ`ˆ˜}Ê`iۈ>̈œ˜Êˆ˜`ˆV>̜À]Ê>˜`Ê>Ê`iۈ>̈œ˜ÊÃV>i°ÊÊ1«œ˜ÊÃÌ>̈œ˜Ê«>ÃÃ>}i]ÊÌ iÊ SYSTEM OVERVIEW /œÉÀœ“ʘ`ˆV>̜ÀÊyˆ«ÃÊ>˜`Ê«œˆ˜ÌÃÊ̜ÊÌ iÊÌ>ˆÊœvÊÌ iÊ>ˆÀVÀ>vÌ]ʍÕÃÌʏˆŽiÊ>ÊVœ˜Ûi˜Ìˆœ˜>Ê/œÉÀœ“Êy>}°ÊÊ i«i˜`ˆ˜}Ê œ˜ÊÌ iʘ>ۈ}>̈œ˜ÊÜÕÀVi]ÊÌ iÊ ʜ˜ÊÌ iÊ
ÀVÊ-ÊV>˜Ê>««i>Àʈ˜ÊÌܜÊ`ˆvviÀi˜ÌÊÜ>ÞÃ]Ê>˜Ê>ÀÀœÜ i>`Ê­*-]Ê6",]Ê " -®ÊœÀÊ>Ê`ˆ>“œ˜`Ê­" ®°

Course Pointer FLIGHT INSTRUMENTS Navigation Flight Phase Source Annunciation

EIS Course Lateral Deviation Deviation and To/From Scale Indicator Figure 2-13 Arc HSI

& CNS The ÃiiVÌi`Ê i>`ˆ˜}ʈÃÊà œÜ˜Ê̜ÊÌ iÊÕ««iÀʏivÌʜvÊÌ iÊ-Ê>˜`ʈÃÊ`ˆÃ«>Þi`ʈ˜Êˆ} ÌÊLÕi°ÊÊ/ iʏˆ} ÌÊLÕiÊ AUDIO PANEL AUDIO heading bug on the compass rose corresponds to the selected heading. Adjusting the selected heading: Turn the HDG Knob to set the selected heading. FLIGHT

MANAGEMENT Press the HDG Knob to synchronize the bug to the current heading. The -iiVÌi`Ê œÕÀÃiʈÃÊà œÜ˜Ê̜ÊÌ iÊÕ««iÀÊÀˆ} ÌʜvÊÌ iÊ-°ÊÊ/ iÊVœœÀʜvÊÌ iÊ-iiVÌi`Ê œÕÀÃiÊVœÀÀi뜘`ÃÊÌœÊ Ì iÊÃiiVÌi`ʘ>ۈ}>̈œ˜ÊÜÕÀVi\ʓ>}i˜Ì>ÊvœÀÊ*-ʜÀÊ}Àii˜ÊvœÀÊ
6Ê­6",]Ê" ®°

HAZARD Adjusting the Selected Course: AVOIDANCE Turn the CRS Knob to set the Selected Course. Press the CRS Knob to re-center the CDI and return the course pointer to the bearing of the active waypoint or navigation station (see OBS Mode for adjusting a GPS course). AFCS Current Heading Heading Bug

Selected Selected Heading Course FEATURES ADDITIONAL

Figure 2-14 Heading and Course Indications (Magnetic) APPENDICES INDEX

58 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW >ۈ}>̈œ˜Ê>˜}iÃÊ­ÌÀ>VŽ]Ê i>`ˆ˜}]ÊVœÕÀÃi]ÊLi>Àˆ˜}®Ê>ÀiÊVœÀÀiVÌi`Ê̜ÊÌ iÊVœ“«ÕÌi`ʓ>}˜ïVÊÛ>Àˆ>̈œ˜Ê­ >}Ê SYSTEM 6>À®ÊœÀÊÀiviÀi˜Vi`Ê̜ÊÌÀÕiʘœÀÌ Ê­/®]ÊÃiÌʜ˜ÊÌ iÊ
18ʇÊ-ÞÃÌi“Ê-iÌÕ«Ê*>}i°ÊÊ7 i˜Ê>˜Ê>««Àœ>V ÊÀiviÀi˜Vi`ÊÌœÊ true north has been loaded into the flight plan, the system generates a message to change the navigation angle setting to True at the appropriate time. INSTRUMENTS FLIGHT EIS Figure 2-15 Heading and Course Indications (True)

Changing the navigation angle true/magnetic setting: AUDIO PANEL & CNS 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Nav Angle in the Display Units box. MANAGEMENT

4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. FLIGHT sTRUE - References angles to true north (T) sMAGNETIC - Angles corrected to the computed magnetic variation (Mag Var) AVOIDANCE HAZARD AFCS ADDITIONAL FEATURES APPENDICES

Figure 2-16 Navigation Angle Settings (AUX - System Setup Page) INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 59 FLIGHT INSTRUMENTS

TURN RATE INDICATOR SYSTEM

OVERVIEW The /ÕÀ˜Ê,>Ìiʘ`ˆV>̜ÀʈÃʏœV>Ìi`Ê`ˆÀiV̏ÞÊ>LœÛiÊÌ iÊÀœÌ>̈˜}ÊVœ“«>ÃÃÊV>À`°ÊÊ/ˆVŽÊ“>ÀŽÃÊ̜ÊÌ iʏivÌÊ>˜`ÊÀˆ} ÌÊ œvÊÌ iʏÕLLiÀʏˆ˜iÊ`i˜œÌiÊ >v‡ÃÌ>˜`>À`Ê>˜`ÊÃÌ>˜`>À`ÊÌÕÀ˜ÊÀ>ÌiðÊÊ
ʓ>}i˜Ì>Ê/ÕÀ˜Ê,>ÌiÊ/Ài˜`Ê6iV̜ÀÊà œÜÃÊÌ iÊ VÕÀÀi˜ÌÊÌÕÀ˜ÊÀ>Ìi°ÊÊ/ iÊi˜`ʜvÊÌ iÊÌÀi˜`ÊÛiV̜ÀÊ}ˆÛiÃÊÌ iÊ i>`ˆ˜}Ê«Ài`ˆVÌi`ʈ˜ÊÈÊÃiVœ˜`Ã]ÊL>Ãi`ʜ˜ÊÌ iÊ«ÀiÃi˜ÌÊ ÌÕÀ˜ÊÀ>Ìi°ÊÊ
ÊÃÌ>˜`>À`‡À>ÌiÊÌÕÀ˜ÊˆÃÊà œÜ˜Êœ˜ÊÌ iʈ˜`ˆV>̜ÀÊLÞÊÌ iÊÌÀi˜`ÊÛiV̜ÀÊÃ̜««ˆ˜}Ê>ÌÊÌ iÊÃÌ>˜`>À`ÊÌÕÀ˜Ê À>ÌiÊ̈VŽÊ“>ÀŽ]ÊVœÀÀi뜘`ˆ˜}Ê̜Ê>Ê«Ài`ˆVÌi`Ê i>`ˆ˜}ʜvÊ£nÂÊvÀœ“ÊÌ iÊVÕÀÀi˜ÌÊ i>`ˆ˜}°ÊÊ
ÌÊÀ>ÌiÃÊ}Ài>ÌiÀÊÌ >˜Ê{Ê FLIGHT `i}ÉÃiV]Ê>˜Ê>ÀÀœÜ i>`Ê>««i>ÀÃÊ>ÌÊÌ iÊi˜`ʜvÊÌ iʓ>}i˜Ì>ÊÌÀi˜`ÊÛiV̜ÀÊ>˜`ÊÌ iÊ«Ài`ˆV̈œ˜ÊˆÃʘœÊœ˜}iÀÊÛ>ˆ`° INSTRUMENTS Half-standard Turn Rate Arrow Shown EIS Standard for Turn Rate Turn Rate > 4 deg/sec

Figure 2-17 Turn Rate Indicator and Trend Vector & CNS

AUDIO PANEL AUDIO BEARING POINTERS AND INFORMATION WINDOWS Two Li>Àˆ˜}Ê«œˆ˜ÌiÀÃÊ>˜`Ê>ÃÜVˆ>Ìi`ʈ˜vœÀ“>̈œ˜ÊV>˜ÊLiÊ`ˆÃ«>Þi`ʜ˜ÊÌ iÊ-ÊvœÀÊ
6]Ê*-]Ê>˜`Ê
Ê sources by pressing the PFDÊ-œv̎iÞÊÌ i˜Ê>ÊBRG or DME -œv̎iÞ°ÊÊ/ iÊbearing pointers are light blue and are Ș}i‡ˆ˜iÊ­ ,£®ÊœÀÊ`œÕLi‡ˆ˜iÊ­ ,Ó®°ÊÊ
Ê«œˆ˜ÌiÀÊÃޓLœÊˆÃÊà œÜ˜Êˆ˜ÊÌ iʈ˜vœÀ“>̈œ˜Ê܈˜`œÜÃÊ̜ʈ˜`ˆV>ÌiÊ FLIGHT the navigation source. The bearing pointers never override the CDI and are visually separated from the CDI MANAGEMENT by a white ring. Bearing pointers may be selected but not necessarily visible due to data unavailability. When Ì iÊ
ÀVÊ-ʈÃÊ`ˆÃ«>Þi`]ÊÌ iÊ i>Àˆ˜}ʘvœÀ“>̈œ˜Ê܈˜`œÜÃÊ>˜`Ê«œˆ˜ÌiÀÃÊ>ÀiÊ`ˆÃ>Li`°

HAZARD NOTE: ADF radio installation is optional. AVOIDANCE

Tuning Mode Bearing 1 Bearing 2

AFCS Frequency Pointer Pointer Distance

Distance to Station ADF Bearing Source Identifier Frequency FEATURES ADDITIONAL

Bearing Source Pointer 1 Pointer 2 Bearing Source

APPENDICES Bearing 1 Information Window Bearing 2 Information Window

Figure 2-18 HSI with Bearing and Distance Information INDEX

60 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW When a bearing pointer is displayed, the associated information window is also displayed. The Bearing SYSTEM ˜vœÀ“>̈œ˜Ê 7ˆ˜`œÜÃÊ ­ˆ}ÕÀiÊ Ó‡£n®Ê >ÀiÊ `ˆÃ«>Þi`Ê >ÌÊ Ì iÊ œÜiÀÊ Ãˆ`iÃÊ œvÊ Ì iÊ -Ê >˜`Ê }ˆÛiÊ Ì iÊ vœœÜˆ˜}Ê information:

UÊ i>Àˆ˜}ÊÜÕÀViÊ­
6]Ê*-]Ê
® UÊ-Ì>̈œ˜ÉÜ>Þ«œˆ˜Ìʈ`i˜ÌˆwiÀÊ­
6]Ê*-® INSTRUMENTS FLIGHT UÊ*œˆ˜ÌiÀʈVœ˜Ê­ ,£ÊrÊȘ}iʏˆ˜i] ,ÓÊrÊ`œÕLiÊ UÊ*-‡`iÀˆÛi`Ê }Ài>ÌÊ VˆÀViÊ `ˆÃÌ>˜ViÊ ÌœÊ bearing line) source UÊÀiµÕi˜VÞÊ­
6]Ê
® 7 i˜ÊÌ iÊ
6ÊÀ>`ˆœÊˆÃÊÌ՘i`Ê̜Ê>˜Ê-ÊvÀiµÕi˜VÞÊÌ iÊLi>Àˆ˜}ÊÜÕÀViÊ>˜`ÊÌ iÊLi>Àˆ˜}Ê«œˆ˜ÌiÀʈÃÊÀi“œÛi`Ê

vÀœ“ÊÌ iÊ-°ÊÊ7 i˜Ê
6£ÊœÀÊ
6ÓʈÃÊÌ iÊÃiiVÌi`ÊLi>Àˆ˜}ÊÜÕÀVi]ÊÌ iÊvÀiµÕi˜VÞʈÃÊÀi«>Vi`ÊLÞÊÌ iÊÃÌ>̈œ˜Ê EIS ˆ`i˜ÌˆwiÀÊÜ i˜ÊÌ iÊÃÌ>̈œ˜ÊˆÃÊÜˆÌ ˆ˜ÊÀ>˜}i°ÊÊvÊ*-ʈÃÊÌ iÊLi>Àˆ˜}ÊÜÕÀVi]ÊÌ iÊ>V̈ÛiÊÜ>Þ«œˆ˜Ìʈ`i˜ÌˆwiÀʈÃÊ `ˆÃ«>Þi`ʈ˜ÃÌi>`ʜvÊ>ÊvÀiµÕi˜VÞ°

/ iÊLi>Àˆ˜}Ê«œˆ˜ÌiÀʈÃÊÀi“œÛi`ÊvÀœ“ÊÌ iÊ-Ê>˜`Ê "Ê
/
ʈÃÊ`ˆÃ«>Þi`ʈ˜ÊÌ iʈ˜vœÀ“>̈œ˜Ê܈˜`œÜʈvÊ AUDIO PANEL

Ì iÊ
6ÊÀ>`ˆœÊˆÃʘœÌÊÀiViˆÛˆ˜}Ê>Ê6",ÊÃÌ>̈œ˜ÊœÀʈvÊ*-ʈÃÊÌ iÊLi>Àˆ˜}ÊÜÕÀViÊ>˜`Ê>˜Ê>V̈ÛiÊÜ>Þ«œˆ˜ÌʈÃʘœÌÊ & CNS selected. Selecting bearing display and changing sources: MANAGEMENT 1) Press the PFD Softkey. FLIGHT 2) Press a BRG Softkey to display the desired bearing pointer and information window with a NAV source. 3) Press the BRG Softkey again to change the bearing source to GPS. 4) To remove the bearing pointer and information window, press the BRG Softkey again. AVOIDANCE HAZARD DME INFORMATION WINDOW The ʘvœÀ“>̈œ˜Ê7ˆ˜`œÜʈÃÊ`ˆÃ«>Þi`Ê>LœÛiÊÌ iÊ ,£Ê˜vœÀ“>̈œ˜Ê7ˆ˜`œÜʜ˜ÊÌ iÊÎÈäÂÊ-Ê>˜`ʈ˜Ê >ÊLœÝÊ>LœÛiÊ>˜`Ê>œ˜}ÊÈ`iÊÌ iÊ
ÀVÊ-°ÊÊÌÊà œÜÃÊÌ iÊ Ê>Li]ÊÌ՘ˆ˜}ʓœ`iÊ­
6£]Ê
6Ó]ʜÀÊ" ®]Ê vÀiµÕi˜VÞ]Ê>˜`Ê`ˆÃÌ>˜Vi°ÊÊ7 i˜Ê>ÊÈ}˜>ÊˆÃʈ˜Û>ˆ`]ÊÌ iÊ`ˆÃÌ>˜ViʈÃÊÀi«>Vi`ÊLÞÊq°qÊqÊ ÊÊ,iviÀÊ̜ÊÌ iÊ
Õ`ˆœÊ *>˜iÊ>˜`Ê -Ê-iV̈œ˜ÊvœÀʈ˜vœÀ“>̈œ˜Êœ˜ÊÌ՘ˆ˜}ÊÌ iÊ ° AFCS

NOTE: DME installation is optional. ADDITIONAL Displaying the DME Information Window: FEATURES 1) Press the PFD Softkey. 2) Press the DME Softkey to display the DME Information Window.

3) To remove the DME Information Window, press the DME Softkey again. APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 61 FLIGHT INSTRUMENTS

COURSE DEVIATION INDICATOR (CDI) SYSTEM OVERVIEW NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI switches to the opposite side of the deviation scale and displays reverse sensing.

The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation

FLIGHT scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not

INSTRUMENTS displayed.

360º HSI

EIS Navigation Source Flight Arc HSI Phase Navigation Flight Source Phase Scale & CNS

AUDIO PANEL AUDIO Crosstrack Error CDI CDI CDI Scale FLIGHT

MANAGEMENT Figure 2-19 Course Deviation Indicator

/ iÊ ÊV>˜Ê`ˆÃ«>ÞÊÌܜÊÜÕÀViÃʜvʘ>ۈ}>̈œ˜]Ê*-ʜÀÊ6",É" °ÊÊ/ iÊVœœÀʈ˜`ˆV>ÌiÃÊÌ iÊVÕÀÀi˜ÌÊnavigation ÜÕÀVi]ʓ>}i˜Ì>ÊvœÀÊ*-Ê>˜`Ê}Àii˜ÊvœÀÊ6",Ê>˜`Ê" °ÊÊ/ iÊvՏÊÃV>iʏˆ“ˆÌÃÊvœÀÊÌ iÊ Ê>ÀiÊ`iw˜i`ÊLÞÊ>Ê*-‡ HAZARD

AVOIDANCE `iÀˆÛi`Ê`ˆÃÌ>˜ViÊÜ i˜Ê˜>ۈ}>̈˜}Ê*-°ÊÊ7 i˜Ê˜>ۈ}>̈˜}ÊÕȘ}Ê>Ê6",ʜÀʏœV>ˆâiÀÊ­" ®]ÊÌ iÊ ÊÕÃiÃÊÌ iÊ same angular deviation as a mechanical CDI. If the CDI exceeds the maximum deviation on the scale (two dots) Ü ˆiʘ>ۈ}>̈˜}ÊÜˆÌ Ê*-]ÊÌ iÊVÀœÃÃÌÀ>VŽÊiÀÀœÀÊ­8/®ÊˆÃÊ`ˆÃ«>Þi`ÊLiœÜÊÌ iÊÜ ˆÌiÊ>ˆÀVÀ>vÌÊÃޓLœ° AFCS FEATURES ADDITIONAL APPENDICES

Figure 2-20 Navigation Sources INDEX

62 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW Changing navigation sources: SYSTEM 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning INSTRUMENTS box over the NAV2 standby frequency. FLIGHT 3) Press the CDI Softkey a third time to return to GPS.

NAV1 Selected for Tuning NAV2 Selected for Tuning EIS

GPS LOC1 VOR2 AUDIO PANEL Selected Selected Selected & CNS

Pressing the CDI Softkey MANAGEMENT

Cycles through FLIGHT Navigation Sources

Figure 2-21 Selecting a Navigation Source AVOIDANCE

/ iÊÃÞÃÌi“Ê>Õ̜“>̈V>ÞÊÃ܈ÌV iÃÊvÀœ“Ê*-Ê̜Ê" ʘ>ۈ}>̈œ˜ÊÜÕÀViÊ>˜`ÊV >˜}iÃÊÌ iÊ ÊÃV>ˆ˜}Ê>VVœÀ`ˆ˜}ÞÊ HAZARD when all of the following occur: UÊ
ʏœV>ˆâiÀʜÀÊ-Ê>««Àœ>V Ê >ÃÊLii˜Êœ>`i`ʈ˜ÌœÊÌ iÊ>V̈ÛiÊyˆ} ÌÊ«>˜ UÊ/ iÊw˜>Ê>««Àœ>V ÊwÝÊ­
®ÊˆÃÊÌ iÊ>V̈Ûiʏi}]ÊÌ iÊ
ʈÃʏiÃÃÊÌ >˜Ê£xʘ“Ê>Ü>Þ]Ê>˜`ÊÌ iÊ>ˆÀVÀ>vÌʈÃʓœÛˆ˜}Ê ÌœÜ>À`ÊÌ iÊ
 AFCS UÊ
ÊÛ>ˆ`ʏœV>ˆâiÀÊvÀiµÕi˜VÞÊ >ÃÊLii˜ÊÌ՘i` UÊ/ iÊ*-Ê Ê`iۈ>̈œ˜ÊˆÃʏiÃÃÊÌ >˜Ê£°ÓÊ̈“iÃÊvՏ‡ÃV>iÊ`iyiV̈œ˜ *-ÊÃÌiiÀˆ˜}Ê}Ո`>˜ViʈÃÊÃ̈Ê«ÀœÛˆ`i`Ê>vÌiÀÊÌ iÊ Ê>Õ̜“>̈V>ÞÊÃ܈ÌV iÃÊ̜Ê" Ê՘̈Ê" ÊV>«ÌÕÀi]ÊÕ«Ê ADDITIONAL ̜ÊÌ iʈ˜>Ê
««Àœ>V ʈÝÊ­
®ÊvœÀÊ>˜Ê-Ê>««Àœ>V ]ʜÀÊ՘̈Ê*-ʈ˜vœÀ“>̈œ˜ÊLiVœ“iÃʈ˜Û>ˆ`°ÊÊ
V̈Û>̈˜}Ê>Ê FEATURES 6iV̜À‡Ìœ‡ˆ˜>Ê­6/®Ê>ÃœÊV>ÕÃiÃÊÌ iÊ Ê̜ÊÃ܈ÌV Ê̜Ê" ʘ>ۈ}>̈œ˜ÊÜÕÀVi°ÊÊ*-ÊÃÌiiÀˆ˜}Ê}Ո`>˜ViʈÃʘœÌÊ provided after the switch. APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 63 FLIGHT INSTRUMENTS

GPS CDI SCALING SYSTEM

OVERVIEW 7 i˜Ê *-Ê ˆÃÊ Ì iÊ ÃiiVÌi`Ê ˜>ۈ}>̈œ˜Ê ÜÕÀVi]Ê Ì iÊ yˆ} ÌÊ «>˜Ê i}ÃÊ >ÀiÊ ÃiµÕi˜Vi`Ê >Õ̜“>̈V>ÞÊ >˜`Ê >˜˜Õ˜Vˆ>̈œ˜ÃÊ>««i>Àʜ˜ÊÌ iÊ-ÊvœÀÊÌ iÊyˆ} ÌÊ« >Ãi°Êʏˆ} ÌÊ« >ÃiÊ>˜˜Õ˜Vˆ>̈œ˜ÃÊ>ÀiʘœÀ“>ÞÊà œÜ˜Êˆ˜Ê magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan ˆÃÊ>Ê i>`ˆ˜}ʏi}]Ê Ê ʈÃÊ>˜˜Õ˜Vˆ>Ìi`ʈ˜Ê“>}i˜Ì>ÊLi˜i>Ì ÊÌ iÊ>ˆÀVÀ>vÌÊÃޓLœ°

FLIGHT / iÊVÕÀÀi˜ÌÊ*-Ê ÊÃV>iÊÃiÌ̈˜}ʈÃÊ`ˆÃ«>Þi`Ê>ÃÊ-ÞÃÌi“Ê ʜ˜ÊÌ iÊ
18ʇÊ-ÞÃÌi“Ê-iÌÕ«Ê*>}iÊ>˜`ÊÌ iÊvՏ‡

INSTRUMENTS ÃV>iÊ`iyiV̈œ˜ÊÃiÌ̈˜}ʓ>ÞÊ>ÃœÊLiÊV >˜}i`Ê­Ó°äʘ“]Ê£°äʘ“]Êä°Îʘ“]ʜÀÊ
Õ̜®ÊvÀœ“ÊÌ ˆÃÊ«>}i°ÊÊvÊÌ iÊÃiiVÌi`Ê scaling is smaller than the automatic setting for enroute and terminal phases, the CDI is scaled accordingly and the selected setting is displayed rather than the flight phase annunciation.

EIS Changing the selected GPS CDI setting: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Selected in the GPS CDI box. & CNS

AUDIO PANEL AUDIO 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. 5) To cancel the selection, press the FMS Knob or the CLR Key. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS

Figure 2-22 GPS CDI Settings (AUX - System Setup Page) FEATURES ADDITIONAL

7 i˜ÊÃiÌÊ̜Ê
Õ̜ʭ`iv>Տ̮]ÊÌ iÊ*-Ê ÊÃV>iÊ>Õ̜“>̈V>ÞÊ>`ÕÃÌÃÊ̜ÊÌ iÊ`iÈÀi`ʏˆ“ˆÌÃÊL>Ãi`ÊÕ«œ˜ÊÌ iÊ VÕÀÀi˜ÌÊ« >ÃiʜvÊyˆ} ÌÊ­ˆ}ÕÀiÊӇÓÎ]Ê/>LiÊӇ£®° APPENDICES INDEX

64 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW SYSTEM 2.0 nm 1.0 nm 1.0 nm 1.0 nm

Refer to accompanying INSTRUMENTS 0.3 nm approach CDI scaling figures 0.3 nm FLIGHT CDI Full-scale Deflection

Enroute Missed Departure Terminal (Oceanic if >200 nm Terminal Approach Approach from nearest airport) EIS

Figure 2-23 Automatic CDI Scaling AUDIO PANEL & CNS UÊ"˜ViÊ>Ê`i«>ÀÌÕÀiÊ«ÀœVi`ÕÀiʈÃÊ>V̈Û>Ìi`]ÊÌ iÊ ʈÃÊÃV>i`ÊvœÀÊdepartureÊ­ä°Îʘ“®° UÊ/ iÊÃÞÃÌi“ÊÃ܈ÌV iÃÊvÀœ“Ê`i«>ÀÌÕÀiÊ̜Êterminal CDI scaling (1.0 nm) under the following conditions:

- The next leg in the departure procedure is not aligned with the departure runway MANAGEMENT FLIGHT ‡Ê / iʘiÝÌʏi}ʈ˜ÊÌ iÊ`i«>ÀÌÕÀiÊ«ÀœVi`ÕÀiʈÃʘœÌÊ>Ê
]Ê ]Ê ]Ê ]Ê ,]Ê ]Ê
]Ê ]Ê ]Ê ]Ê]ʜÀÊ/Ê­ÃiiÊ Glossary for leg type definitions) ‡Ê
vÌiÀÊ>˜Þʏi}ʈ˜ÊÌ iÊ`i«>ÀÌÕÀiÊ«ÀœVi`ÕÀiÊÌ >ÌʈÃʘœÌÊ>Ê
ʜÀÊ
AVOIDANCE

UÊ
ÌÊÎäʘ“ÊvÀœ“ÊÌ iÊ`i«>ÀÌÕÀiÊ>ˆÀ«œÀÌ]ÊÌ iÊenroute phase of flight is automatically entered and CDI scaling HAZARD V >˜}iÃÊ̜ÊÓ°äʘ“ÊœÛiÀÊ>Ê`ˆÃÌ>˜ViʜvÊ£°äʘ“]ÊiÝVi«ÌÊ՘`iÀÊÌ iÊvœœÜˆ˜}ÊVœ˜`ˆÌˆœ˜Ã\ - When navigating with an active departure procedure, the flight phase and CDI scale does not change ՘̈ÊÌ iÊ>ˆÀVÀ>vÌÊ>ÀÀˆÛiÃÊ>ÌÊÌ iʏ>ÃÌÊ`i«>ÀÌÕÀiÊÜ>Þ«œˆ˜ÌÊ­ˆvʓœÀiÊÌ >˜ÊÎäʘ“ÊvÀœ“ÊÌ iÊ`i«>ÀÌÕÀiÊ>ˆÀ«œÀ̮ʜÀÊ the leg after the last departure waypoint has been activated or a direct-to waypoint is activated.

UÊvÊ>vÌiÀÊVœ“«ï˜}ÊÌ iÊ`i«>ÀÌÕÀiÊ«ÀœVi`ÕÀiÊÌ iʘi>ÀiÃÌÊ>ˆÀ«œÀÌʈÃʓœÀiÊÌ >˜ÊÓääʘ“Ê>Ü>ÞÊvÀœ“ÊÌ iÊ>ˆÀVÀ>vÌÊ AFCS and the approach procedure has not yet commenced, the CDI is scaled for oceanicÊyˆ} ÌÊ­Ó°äʘ“®° UÊ7ˆÌ ˆ˜ÊΣʘ“ÊœvÊÌ iÊ`iÃ̈˜>̈œ˜Ê>ˆÀ«œÀÌÊ­terminalÊ>Ài>®]ÊÌ iÊ ÊÃV>iÊ}À>`Õ>ÞÊÀ>“«ÃÊ`œÜ˜ÊvÀœ“ÊÓ°äʘ“Ê

̜ʣ°äʘ“ÊœÛiÀÊ>Ê`ˆÃÌ>˜ViʜvÊ£°äʘ“ÆÊiÝVi«ÌÊ՘`iÀÊÌ iÊvœœÜˆ˜}ÊVœ˜`ˆÌˆœ˜Ã\ ADDITIONAL FEATURES Ê ‡Ê 1«œ˜ÊÀi>V ˆ˜}ÊÌ iÊwÀÃÌÊÜ>Þ«œˆ˜ÌʜvÊ>˜Ê>ÀÀˆÛ>ÊÀœÕÌiÊÌ >ÌʈÃʓœÀiÊÌ >˜ÊΣʘ“ÊvÀœ“ÊÌ iÊ`iÃ̈˜>̈œ˜Ê>ˆÀ«œÀÌ]Ê Ì iÊyˆ} ÌÊ« >ÃiÊV >˜}iÃÊ̜ÊÌiÀ“ˆ˜>Ê>˜`ÊÌ iÊ ÊÃV>iÊLi}ˆ˜ÃÊ̜ÊÌÀ>˜ÃˆÌˆœ˜Ê`œÜ˜ÊvÀœ“ÊÓ°äʘ“Ê̜ʣ°äʘ“Ê over a distance of 1.0 nm.

UÊ ÕÀˆ˜}Êapproach]ÊÌ iÊ ÊÃV>iÊÀ>“«ÃÊ`œÜ˜ÊiÛi˜ÊvÕÀÌ iÀÊ­ˆ}ÕÀiÃÊӇÓ{Ê>˜`ÊӇÓx®°ÊÊ/ ˆÃÊÌÀ>˜ÃˆÌˆœ˜Ê˜œÀ“>ÞÊ APPENDICES œVVÕÀÃÊÜˆÌ ˆ˜ÊÓ°äʘ“ÊœvÊÌ iÊw˜>Ê>««Àœ>V ÊwÝÊ­
®°ÊÊ/ iÊ ÊÃ܈ÌV iÃÊ̜Ê>««Àœ>V ÊÃV>ˆ˜}Ê>Õ̜“>̈V>ÞÊ once the approach procedure is activated or if Vectors-To-Final (VTF) are selected. ‡Ê vÊÌ iÊ>V̈ÛiÊÜ>Þ«œˆ˜ÌʈÃÊÌ iÊ
]ÊÌ iÊ}ÀœÕ˜`ÊÌÀ>VŽÊ>˜`ÊÌ iÊLi>Àˆ˜}Ê̜ÊÌ iÊ
ʓÕÃÌÊLiÊÜˆÌ ˆ˜Ê{xcʜvÊÌ iÊ final approach segment course.

- If the active waypoint is part of the missed approach procedure, the active leg and the preceding missed INDEX approach legs must be aligned with the final approach segment course and the aircraft must not have passed the turn initiation point.

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 65 FLIGHT INSTRUMENTS

CDI scale is set to the smaller of 0.3 nm or an angle set by the system SYSTEM OVERVIEW 1.0 nm 1.0 nm 0.3 nm

angle set angle based 0.3 nm by system on database 350 ft CDI Full-scale Deflection CDI Full-scale Deflection information

2 nm 2 nm course width FAF FAF Landing Threshold FLIGHT INSTRUMENTS

CDI scale varies if VTF is activated CDI scale varies if VTF is activated EIS Figure 2-24 Typical LNAV and LNAV+V Approach CDI Scaling Figure 2-25 Typical LNAV/VNAV and LPV Approach CDI Scaling

UÊ7 i˜Ê>Êmissed approachʈÃÊ>V̈Û>Ìi`]ÊÌ iÊ ÊÃV>iÊV >˜}iÃÊ̜Êä°Îʘ“° UÊ/ iÊÃÞÃÌi“Ê>Õ̜“>̈V>ÞÊÃ܈ÌV iÃÊL>VŽÊ̜Êterminal mode under the following conditions: & CNS - The next leg in the missed approach procedure is not aligned with the final approach path AUDIO PANEL AUDIO - / iʘiÝÌʏi}ʈ˜ÊÌ iʓˆÃÃi`Ê>««Àœ>V Ê«ÀœVi`ÕÀiʈÃʘœÌÊ>Ê
]Ê ]Ê ]Ê ]Ê ,]Ê ]Ê
]Ê ]Ê ]Ê ]Ê]ʜÀÊ/ ‡Ê
vÌiÀÊ>˜Þʏi}ʈ˜ÊÌ iʓˆÃÃi`Ê>««Àœ>V Ê«ÀœVi`ÕÀiÊÌ >ÌʈÃʘœÌÊ>Ê
ʜÀÊ

FLIGHT Flight Phase Annunciation* Automatic CDI Full-scale Deflection MANAGEMENT Departure DPRT 0.3 nm Terminal TERM 1.0 nm Enroute ENR 2.0 nm

HAZARD Oceanic OCN 2.0 nm AVOIDANCE Approach LNAV (Non-precision) 1.0 nm decreasing to 350 feet depending on Approach variables (Figure 2-24) AFCS (Non-precision with LNAV + V Vertical Guidance) Approach L/VNAV (LNAV/VNAV) 1.0 nm decreasing to a specified course width, then Approach 0.3 nm, depending on variables (Figure 2-25)

FEATURES LPV ADDITIONAL (LPV) Missed Approach MAPR 0.3 nm * Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. Table 2-1 Automatic GPS CDI Scaling APPENDICES INDEX

66 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW OBS MODE SYSTEM

NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. INSTRUMENTS

˜>Lˆ˜}Ê"“˜ˆ‡Li>Àˆ˜}Ê-iiV̜ÀÊ­" -®Ê œ`iÊÃÕëi˜`ÃÊÌ iÊ>Õ̜“>̈VÊÃiµÕi˜Vˆ˜}ʜvÊÜ>Þ«œˆ˜ÌÃʈ˜Ê>Ê*-Ê FLIGHT yˆ} ÌÊ«>˜Ê­*-ʓÕÃÌÊLiÊÌ iÊÃiiVÌi`ʘ>ۈ}>̈œ˜ÊÜÕÀVi®]ÊLÕÌÊÀiÌ>ˆ˜ÃÊÌ iÊVÕÀÀi˜ÌÊ
V̈Ûi‡ÌœÊÜ>Þ«œˆ˜ÌÊ>ÃÊÌ iÊ ˜>ۈ}>̈œ˜ÊÀiviÀi˜ViÊiÛi˜Ê>vÌiÀÊ«>ÃȘ}ÊÌ iÊÜ>Þ«œˆ˜Ì°ÊÊ" -ʈÃÊ>˜˜Õ˜Vˆ>Ìi`Ê̜ÊÌ iʏœÜiÀÊÀˆ} ÌʜvÊÌ iÊ>ˆÀVÀ>vÌÊ symbol when " -Ê œ`iʈÃÊÃiiVÌi`° 7 ˆiÊ " -Ê ˆÃÊ i˜>Li`]Ê >Ê VœÕÀÃiÊ ˆ˜iÊ ˆÃÊ `À>Ü˜Ê Ì ÀœÕ} Ê Ì iÊ >V̈Ûi‡ÌœÊ Ü>Þ«œˆ˜ÌÊ œ˜Ê Ì iÊ “œÛˆ˜}Ê “>«°ÊÊvÊ

`iÈÀi`]ÊÌ iÊVœÕÀÃiÊ̜ÉvÀœ“ÊÌ iÊÜ>Þ«œˆ˜ÌÊV>˜Ê˜œÜÊLiÊ>`ÕÃÌi`°ÊÊ7 i˜Ê" -Ê œ`iʈÃÊ`ˆÃ>Li`]ÊÌ iÊ*-Êyˆ} ÌÊ EIS «>˜ÊÀiÌÕÀ˜ÃÊ̜ʘœÀ“>Êœ«iÀ>̈œ˜]ÊÜˆÌ Ê>Õ̜“>̈VÊÃiµÕi˜Vˆ˜}ʜvÊÜ>Þ«œˆ˜ÌÃ]ÊvœœÜˆ˜}ÊÌ iÊVœÕÀÃiÊÃiÌʈ˜Ê" -Ê Mode. The flight plan on the moving map retains the modified course line. AUDIO PANEL & CNS GPS Selected MANAGEMENT

OBS Mode FLIGHT Extended Enabled Course Line Pressing the OBS Pressing the OBS Softkey Enables Softkey Again

OBS Mode Disables OBS Mode AVOIDANCE HAZARD

Figure 2-26 Omni-bearing Selector (OBS) Mode

Enabling/disabling OBS Mode while navigating a GPS flight plan:

1) Press the OBS Softkey to select OBS Mode. AFCS 2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. ADDITIONAL 3) Press the OBS Softkey again to return to automatic waypoint sequencing. FEATURES APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 67 FLIGHT INSTRUMENTS

ÃÊ Ì iÊ >ˆÀVÀ>vÌÊ VÀœÃÃiÃÊ Ì iÊ “ˆÃÃi`Ê >««Àœ>V Ê «œˆ˜ÌÊ ­
*®]Ê >Õ̜“>̈VÊ >««Àœ>V Ê Ü>Þ«œˆ˜ÌÊ ÃiµÕi˜Vˆ˜}Ê ˆÃÊ ÃÕëi˜`i`°ÊÊ-1-*Ê>««i>ÀÃʜ˜ÊÌ iÊ-Ê>ÌÊÌ iʏœÜiÀÊÀˆ} ÌÊ œvÊÌ iÊ>ˆÀVÀ>vÌÊ ÃޓLœ°ÊÊ/ iÊ OBSÊ-œv̎iÞÊ >LiÊ SYSTEM OVERVIEW V >˜}iÃÊ̜ʈ˜`ˆV>ÌiÊÌ iÊÃÕëi˜Ãˆœ˜ÊˆÃÊ>V̈ÛiÊ>ÃÊà œÜ˜Êˆ˜Êˆ}ÕÀiÊӇÓÇ°ÊÊ*ÀiÃȘ}ÊÌ iÊSUSPÊ-œv̎iÞ]Ê`i>V̈Û>ÌiÃÊ Ì iÊÃÕëi˜Ãˆœ˜Ê>˜`ÊÀiÃՓiÃÊ>Õ̜“>̈VÊÃiµÕi˜Vˆ˜}ʜvÊ>««Àœ>V ÊÜ>Þ«œˆ˜Ìð FLIGHT INSTRUMENTS EIS

SUSP & CNS SUSP Softkey Annunciation AUDIO PANEL AUDIO

Figure 2-27 Suspending Automatic Waypoint Sequencing FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS FEATURES ADDITIONAL APPENDICES INDEX

68 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW 2.2 SUPPLEMENTAL FLIGHT DATA SYSTEM

NOTE: Pressing the DFLTS Softkey turns off metric Altimeter display, the Inset Map and wind data display. INSTRUMENTS

In addition to the flight instruments, the PFD also displays various supplemental information, including FLIGHT Ìi“«iÀ>ÌÕÀiÃ]Ê܈˜`Ê`>Ì>]Ê>˜`Ê6iÀ̈V>Ê >ۈ}>̈œ˜Ê­6 6®Êˆ˜`ˆV>̈œ˜Ã° OUTSIDE AIR TEMPERATURE The "ÕÌÈ`iÊ
ˆÀÊ/i“«iÀ>ÌÕÀiÊ­"
/®ÊˆÃÊ`ˆÃ«>Þi`ʈ˜Ê`i}ÀiiÃÊ iÃˆÕÃÊ­c ®ÊœÀÊ> Ài˜ iˆÌÊ­c®Ê>ÃÊÃiiVÌi`ÊLÞÊÌ iÊ EIS pilot, in the lower left of the PFD under normal display conditions. Temperature is displayed below the true airspeed in reversionary mode.

Normal Display AUDIO PANEL & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD

Reversionary Mode AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 2-28 Outside Air Temperature

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 69 FLIGHT INSTRUMENTS

Changing temperature display units:

SYSTEM 1) Select the AUX - System Setup Page on the MFD using the FMS Knob. OVERVIEW 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the TEMP field in the Display Units box. 4) Turn the small FMS Knob to highlight either CELSIUS or FAHRENHEIT and press the ENT Key to confirm the FLIGHT selection. INSTRUMENTS 5) To cancel the selection, press the FMS Knob or the CLR Key. EIS & CNS AUDIO PANEL AUDIO FLIGHT MANAGEMENT

Figure 2-29 Temperature Selection (AUX - System Setup Page) HAZARD AVOIDANCE AFCS FEATURES ADDITIONAL APPENDICES INDEX

70 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW WIND DATA SYSTEM 7ˆ˜`Ê`ˆÀiV̈œ˜Ê>˜`Êëii`ʈ˜ÊŽ˜œÌÃÊV>˜ÊLiÊ`ˆÃ«>Þi`ÊÀi>̈ÛiÊ̜ÊÌ iÊ>ˆÀVÀ>vÌʈ˜Ê>Ê܈˜`œÜÊ̜ÊÌ iÊÕ««iÀʏivÌʜvÊ Ì iÊ-°ÊÊ7 i˜ÊÌ iÊ܈˜`œÜʈÃÊÃiiVÌi`ÊvœÀÊ`ˆÃ«>Þ]ÊLÕÌÊ܈˜`ʈ˜vœÀ“>̈œ˜ÊˆÃʈ˜Û>ˆ`ʜÀÊ՘>Û>ˆ>Li]ÊÌ iÊ܈˜`œÜÊ `ˆÃ«>ÞÃÊ "Ê7 Ê
/
°ÊÊ7ˆ˜`Ê`>Ì>ÊV>˜ÊLiÊ`ˆÃ«>Þi`ʈ˜ÊÌ ÀiiÊ`ˆvviÀi˜ÌÊÜ>Þð INSTRUMENTS FLIGHT Option 1 Option 2 EIS

Option 3 No Data AUDIO PANEL & CNS MANAGEMENT FLIGHT Figure 2-30 Wind Data

Displaying wind data: AVOIDANCE 1) Press the PFD Softkey. HAZARD 2) Press the WIND Softkey to display wind data below the selected heading. 3) Press one of the OPTN softkeys to change how wind data is displayed: sOPTN 1: Wind direction arrows with headwind/tailwind and crosswind components sOPTN 2: Wind direction arrow and numeric speed AFCS sOPTN 3: Wind direction arrow with numeric True direction and numeric speed 4) To remove the window, press the OFF Softkey. ADDITIONAL FEATURES APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 71 FLIGHT INSTRUMENTS

VERTICAL NAVIGATION (VNV) INDICATIONS SYSTEM

OVERVIEW 7 i˜Ê>Ê6 6Êyˆ} ÌÊ«>˜Ê >ÃÊLii˜Ê>V̈Û>Ìi`]Ê6 6ʈ˜`ˆV>̈œ˜ÃÊ­6 6Ê/>À}iÌÊ
ÌˆÌÕ`i]Ê,6-]Ê6 ®Ê>««i>Àʜ˜ÊÌ iÊ * ʈ˜ÊVœ˜Õ˜V̈œ˜ÊÜˆÌ ÊÌ iʺ/" ÊÜˆÌ ˆ˜Ê£Ê“ˆ˜ÕÌi»Ê“iÃÃ>}iÊ>˜`ʺ6iÀ̈V>ÊÌÀ>VŽ»ÊۜˆViÊ>iÀÌ°ÊÊ-iiÊÌ iʏˆ} ÌÊ >˜>}i“i˜ÌÊ>˜`Ê
 -ÊÃiV̈œ˜ÃÊvœÀÊ`iÌ>ˆÃʜ˜Ê6 6Êvi>ÌÕÀiðÊÊ6 6ʈ˜`ˆV>̈œ˜ÃÊ>ÀiÊÀi“œÛi`ÊvÀœ“ÊÌ iÊ* Ê >VVœÀ`ˆ˜}Ê̜ÊÌ iÊVÀˆÌiÀˆ>ʏˆÃÌi`ʈ˜ÊÌ iÊ/>LiÊӇӰ

FLIGHT Top of Descent Message INSTRUMENTS

VNV Target Altitude EIS Vertical Deviation Indicator Required Vertical Speed

& CNS Indicator AUDIO PANEL AUDIO

GPS is the Selected Phase of Navigation Flight FLIGHT Source MANAGEMENT

HAZARD Figure 2-31 Vertical Navigation Indications AVOIDANCE

VNV Indication Removed Criteria Required Vertical Vertical VNV Target AFCS Speed (RVSI) Deviation (VDI) Altitude* Aircraft > 1 min before the next TOD due to flight plan change X X X VNV cancelled (CNCL VNV Softkey pressed on MFD) X X X Distance to active waypoint cannot be computed due to unsupported flight plan leg type (see Flight Management X X X FEATURES ADDITIONAL Section) Aircraft > 250 feet below active VNV Target Altitude X X X Current crosstrack or track angle error has exceeded limit X X X Active altitude-constrained waypoint can not be reached within X X maximum allowed flight path angle and vertical speed APPENDICES Table 2-2 VNV Indication Removal Criteria INDEX

72 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW 2.3 PFD ANNUNCIATIONS AND ALERTING FUNCTIONS SYSTEM

/ iÊvœœÜˆ˜}Ê>˜˜Õ˜Vˆ>̈œ˜ÃÊ>˜`Ê>iÀ̈˜}Êv՘V̈œ˜ÃÊ>ÀiÊ`ˆÃ«>Þi`ʜ˜ÊÌ iÊ* °ÊÊ,iviÀÊ̜Ê
««i˜`ˆÝÊ
ÊvœÀʓœÀiÊ

information on alerts and annunciations. INSTRUMENTS FLIGHT SYSTEM ALERTING iÃÃ>}iÃÊ>««i>Àʈ˜ÊÌ iÊ
iÀÌÃÊ7ˆ˜`œÜʈ˜ÊÌ iʏœÜiÀÊÀˆ} ÌÊVœÀ˜iÀʜvÊÌ iÊ* ÊÜ i˜Ê>ÊÜ>À˜ˆ˜}]ÊV>Ṏœ˜]Ê>`ۈÜÀÞÊ >iÀÌ]ʜÀÊÃÞÃÌi“Ê“iÃÃ>}iÊ>`ۈÜÀÞʜVVÕÀðÊÊ-ÞÃÌi“Ê>iÀÌʓiÃÃ>}iÃÊ>ÀiÊ«ÀœÛˆ`i`ÊvœÀÊ>Ü>Ài˜iÃÃʜvÊÃÞÃÌi“Ê«ÀœLi“ÃÊ œÀÊÃÌ>ÌÕÃÊ>˜`ʓ>ÞʜÀʓ>ÞʘœÌÊÀiµÕˆÀiÊ«ˆœÌÊ>V̈œ˜°ÊÊ/ iÊ
iÀÌÃÊ7ˆ˜`œÜÊ>œÜÃÊÃÞÃÌi“Ê>iÀÌÃÊ̜ÊLiÊ`ˆÃ«>Þi`Ê

simultaneously. The FMSʘœLʈÃÊÕÃi`Ê̜ÊÃVÀœÊÌ ÀœÕ} ÊÌ iÊ>iÀÌʓiÃÃ>}iðÊÊ/ iÊ
iÀÌÃÊ7ˆ˜`œÜʈÃÊi˜>Li`É EIS disabled by pressing the ALERTSÊ-œv̎iÞ°ÊÊIf the window is already open when a new message is generated, pressing the ALERTSÊ-œv̎iÞÊ̜Ê>VŽ˜œÜi`}iÊÌ iʓiÃÃ>}iÊÌÕÀ˜ÃÊÌ iÊÜv̎iÞÊ}À>Þ°

The ALERTSÊ-œv̎iÞʏ>LiÊV >˜}iÃÊ̜Ê`ˆÃ«>ÞÊÌ iÊ>««Àœ«Àˆ>ÌiÊ>˜˜Õ˜Vˆ>̈œ˜ÊÜ i˜Ê>˜Ê>iÀÌʈÃʈÃÃÕi`°ÊÊ/ iÊ AUDIO PANEL

>˜˜Õ˜Vˆ>̈œ˜Êy>à iÃÊ>˜`ÊÌ iÊ>««Àœ«Àˆ>ÌiÊ>ÕÀ>Ê>iÀÌÊÜ՘`ÃÊ՘̈Ê>VŽ˜œÜi`}i`ÊLÞÊ«ÀiÃȘ}ÊÌ iÊÜv̎iÞ°ÊÊ/ iÊ & CNS Üv̎iÞÊÌ i˜ÊÀiÛiÀÌÃÊ̜ÊÌ iÊALERTSÊ-œv̎iÞʏ>Li]Ê>˜`ÊÜ i˜Ê«ÀiÃÃi`Ê>}>ˆ˜Êœ«i˜ÃÊÌ iÊ
iÀÌÃÊ7ˆ˜`œÜÊ̜Ê`ˆÃ«>ÞÊ a descriptive message of the alert.

/ iÊ
˜˜Õ˜Vˆ>̈œ˜Ê7ˆ˜`œÜÊ>««i>ÀÃÊ̜ÊÌ iÊÀˆ} ÌʜvÊÌ iÊ6iÀ̈V>Ê-«ii`ʘ`ˆV>̜ÀÊ>˜`Ê`ˆÃ«>ÞÃÊ>LLÀiۈ>Ìi`Ê MANAGEMENT

annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts in white, FLIGHT >˜`ÊÃ>viʜ«iÀ>̈˜}Ê>˜˜Õ˜Vˆ>̈œ˜Ãʈ˜Ê}Àii˜°ÊÊ iÜÊ>iÀÌÃÊ>ÀiÊ`ˆÃ«>Þi`Ê>ÌÊÌ iÊ̜«ÊœvÊÌ iÊ
˜˜Õ˜Vˆ>̈œ˜Ê7ˆ˜`œÜ]Ê Ài}>À`iÃÃʜvÊ«ÀˆœÀˆÌÞ°ÊÊ"˜ViÊ>VŽ˜œÜi`}i`]ÊÌ iÞÊ>ÀiÊÃiµÕi˜Vi`ÊL>Ãi`ʜ˜Ê«ÀˆœÀˆÌÞ°

Annunciation AVOIDANCE Window HAZARD

Alerts Window AFCS ADDITIONAL FEATURES Softkey Annunciations

Figure 2-32 System Alerting APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 73 FLIGHT INSTRUMENTS

MARKER BEACON ANNUNCIATIONS SYSTEM

OVERVIEW >ÀŽiÀÊ i>Vœ˜Ê
˜˜Õ˜Vˆ>̈œ˜ÃÊ>ÀiÊ`ˆÃ«>Þi`ʜ˜ÊÌ iÊ* Ê̜ÊÌ iʏivÌʜvÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i°ÊÊ"ÕÌiÀʓ>ÀŽiÀÊ ÀiVi«Ìˆœ˜ÊˆÃʈ˜`ˆV>Ìi`ʈ˜ÊLÕi]ʓˆ``iʈ˜ÊÞiœÜ]Ê>˜`ʈ˜˜iÀʈ˜ÊÜ ˆÌi°ÊÊ,iviÀÊ̜ÊÌ iÊ
Õ`ˆœÊ*>˜iÊ>˜`Ê -Ê-iV̈œ˜Ê vœÀʓœÀiʈ˜vœÀ“>̈œ˜Êœ˜Ê >ÀŽiÀÊ i>Vœ˜Ê
˜˜Õ˜Vˆ>̈œ˜Ã°

Outer Marker Middle Marker Inner Marker FLIGHT INSTRUMENTS EIS Altimeter

Figure 2-33 Marker Beacon Annunciations & CNS

AUDIO PANEL AUDIO TRAFFIC ANNUNCIATION /À>vwVʈÃÊ`ˆÃ«>Þi`ÊÃޓLœˆV>Þʜ˜ÊÌ iÊ* ʘÃiÌÊ >«]ÊÌ iÊ  Ê >ۈ}>̈œ˜Ê >«Ê*>}i]Ê>˜`ÊÛ>ÀˆœÕÃÊœÌ iÀÊ  Ê«>}iʓ>«Ã°ÊÊ,iviÀÊ̜ÊÌ iÊ>â>À`Ê
ۜˆ`>˜ViÊ-iV̈œ˜Ê>˜`ÊÌ iÊ
««i˜`ˆÝÊvœÀʓœÀiÊ`iÌ>ˆÃÊ>LœÕÌÊÌ iÊ/À>vwVÊ

FLIGHT ˜vœÀ“>̈œ˜Ê-iÀۈViÊ­/-®Ê>˜`ʜ«Ìˆœ˜>Ê/À>vwVÊ
`ۈÜÀÞÊ-ÞÃÌi“ÃÊ­/
-®°ÊÊ7 i˜Ê>ÊÌÀ>vwVÊ>`ۈÜÀÞÊ­/
®ÊˆÃÊ`iÌiVÌi`]Ê

MANAGEMENT the following automatically occur: UÊ/ iÊ* ʘÃiÌÊ >«ÊˆÃÊi˜>Li`Ê>˜`Ê`ˆÃ«>ÞÃÊÌÀ>vwV UÊ
Êy>à ˆ˜}ÊL>VŽ‡œ˜‡ÞiœÜÊ/,
 Ê>˜˜Õ˜Vˆ>̈œ˜Ê>««i>ÀÃÊ̜ÊÌ iÊ̜«ÊivÌʜvÊÌ iÊ
Ì̈ÌÕ`iʘ`ˆV>̜ÀÊvœÀÊwÛiÊ ÃiVœ˜`ÃÊ>˜`ÊÀi“>ˆ˜ÃÊ`ˆÃ«>Þi`Ê՘̈Ê˜œÊ/
ÃÊ>ÀiÊ`iÌiVÌi`ʈ˜ÊÌ iÊ>Ài> HAZARD AVOIDANCE UÊ
ÊȘ}iʺ/,
 »Ê>ÕÀ>Ê>iÀÌʈÃÊ i>À`]Ê՘iÃÃÊ>˜Êœ«Ìˆœ˜>Ê/À>vwVÊ
`ۈÜÀÞÊ-ÞÃÌi“Ê­/
-®ÊˆÃʈ˜ÃÌ>i`°ÊÊ,iviÀÊ ÌœÊÌ iÊ>««ˆV>LiÊ/
-Ê`œVՓi˜Ì>̈œ˜ÊvœÀÊ>iÀÌÃÊ}i˜iÀ>Ìi`ÊLÞÊ/
-ÊiµÕˆ«“i˜Ì° vÊ>``ˆÌˆœ˜>Ê/
ÃÊ>««i>À]ʘiÜÊ>ÕÀ>Ê>˜`ÊۈÃÕ>Ê>iÀÌÃÊ>ÀiÊ}i˜iÀ>Ìi`° AFCS

Traffic

FEATURES Symbols ADDITIONAL Inset Traffic Enabled

APPENDICES Figure 2-34 Traffic Annunciation and Inset Map with TIS Traffic Displayed INDEX

74 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW TAWS ANNUNCIATIONS SYSTEM /iÀÀ>ˆ˜Ê
Ü>Ài˜iÃÃÊ>˜`Ê7>À˜ˆ˜}Ê-ÞÃÌi“Ê­/
7-®Ê>˜˜Õ˜Vˆ>̈œ˜ÃÊ>««i>Àʜ˜ÊÌ iÊ* Ê>ÌÊÌ iÊ̜«ÊivÌʜvÊÌ iÊ
Ìˆ“iÌiÀ°ÊÊ ,iviÀÊ̜ÊÌ iÊ>â>À`Ê
ۜˆ`>˜ViÊ-iV̈œ˜Ê>˜`Ê
««i˜`ˆÝÊ
ÊvœÀʈ˜vœÀ“>̈œ˜Êœ˜Ê/
7-Ê>iÀÌÃÊ>˜`Ê>˜˜Õ˜Vˆ>̈œ˜Ã° INSTRUMENTS FLIGHT EIS AUDIO PANEL & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD Figure 2-35 Traffic and TAWS Annunciations AFCS ADDITIONAL FEATURES APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 75 FLIGHT INSTRUMENTS

ALTITUDE ALERTING SYSTEM

OVERVIEW
ÌˆÌÕ`iÊ
iÀ̈˜}Ê«ÀœÛˆ`iÃÊÌ iÊ«ˆœÌÊÜˆÌ Ê>ÊۈÃÕ>Ê>iÀÌÊÜ i˜Ê>««Àœ>V ˆ˜}ÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i°ÊÊ7 i˜iÛiÀÊÌ iÊ -iiVÌi`Ê
ÌˆÌÕ`iʈÃÊV >˜}i`]ÊÌ iÊ
ÌˆÌÕ`iÊ
iÀÌiÀʈÃÊÀiÃiÌ°ÊÊ
ÌˆÌÕ`iÊ>iÀ̈˜}Ê̜˜iÃÊ>˜`ÊۈÃÕ>Ê>iÀÌÃʜVVÕÀʜ˜ÞʈvÊ Ì iÊ ÊÇääʈÃʈ˜ÃÌ>i`°ÊÊ/ iÊvœœÜˆ˜}ʜVVÕÀÊÜ i˜Ê>««Àœ>V ˆ˜}ÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i\ UÊ1«œ˜Ê«>ÃȘ}ÊÌ ÀœÕ} Ê£äääÊviiÌʜvÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`iÊ>˜Ê>ÕÀ>Ê̜˜iʈÃÊ i>À`°ÊÊ/ iÊ-iiVÌi`Ê
ÌˆÌÕ`iÊV >˜}iÃÊ

FLIGHT ̜ÊL>VŽÊÌiÝÌʜ˜Ê>ʏˆ} ÌÊLÕiÊL>VŽ}ÀœÕ˜`Ê>˜`Êy>à iÃÊvœÀÊxÊÃiVœ˜`ð

INSTRUMENTS UÊ7 i˜ÊÌ iÊ>ˆÀVÀ>vÌÊ«>ÃÃiÃÊÜˆÌ ˆ˜ÊÓääÊviiÌʜvÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i]ÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`iÊV >˜}iÃÊ̜ʏˆ} ÌÊLÕiÊ ÌiÝÌʜ˜Ê>ÊL>VŽÊL>VŽ}ÀœÕ˜`Ê>˜`Êy>à iÃÊvœÀÊxÊÃiVœ˜`ð UÊ
vÌiÀÊÀi>V ˆ˜}ÊÌ iÊ-iiVÌi`Ê
ÌˆÌÕ`i]ʈvÊÌ iÊ«ˆœÌÊyˆiÃʜÕÌÈ`iÊÌ iÊ`iۈ>̈œ˜ÊL>˜`Ê­´ÓääÊviiÌʜvÊÌ iÊ-iiVÌi`Ê EIS
ÌˆÌÕ`i®Ê>˜Ê>ÕÀ>Ê̜˜iʈÃÊ i>À`°ÊÊ/ iÊ-iiVÌi`Ê
ÌˆÌÕ`iÊV >˜}iÃÊ̜ÊÞiœÜÊÌiÝÌʜ˜Ê>ÊL>VŽÊL>VŽ}ÀœÕ˜`Ê>˜`Ê y>à iÃÊvœÀÊxÊÃiVœ˜`ð

Within 1000 ft Within 200 ft Deviation of ±200 ft & CNS AUDIO PANEL AUDIO Figure 2-36 Altitude Alerting Visual Annunciations

LOW ALTITUDE ANNUNCIATION FLIGHT MANAGEMENT NOTE: A Low Altitude Annunciation is available only when SBAS is available. This annunciation is not shown for systems with TAWS, unless TAWS is inhibited.

HAZARD 7 i˜ÊÌ iʈ˜>Ê
««Àœ>V ʈÝÊ­
®ÊˆÃÊÌ iÊ>V̈ÛiÊÜ>Þ«œˆ˜Ìʈ˜Ê>Ê*-Ê-
-Ê>««Àœ>V ÊÕȘ}ÊÛiÀ̈V>Ê}Ո`>˜Vi]Ê AVOIDANCE >ÊœÜÊ
ÌˆÌÕ`iÊ
˜˜Õ˜Vˆ>̈œ˜Ê“>ÞÊ>««i>ÀʈvÊÌ iÊVÕÀÀi˜ÌÊ>ˆÀVÀ>vÌÊ>ÌˆÌÕ`iʈÃÊ>Ìʏi>ÃÌÊ£È{ÊviiÌÊLiœÜÊÌ iÊ«ÀiÃVÀˆLi`Ê >ÌˆÌÕ`iÊ>ÌÊÌ iÊ
°ÊÊ
ÊL>VŽ‡œ˜‡ÞiœÜÊ"7Ê
/Ê>˜˜Õ˜Vˆ>̈œ˜Ê>««i>ÀÃÊ̜ÊÌ iÊ̜«ÊivÌʜvÊÌ iÊ
Ìˆ“iÌiÀ]Êy>à ˆ˜}Ê for several seconds, then remaining displayed until the condition is resolved. AFCS FEATURES ADDITIONAL Figure 2-37 Low Altitude on GPS SBAS Approach APPENDICES INDEX

76 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING SYSTEM œÀÊ>ÌˆÌÕ`iÊ>Ü>Ài˜iÃÃ]Ê>ÊL>Àœ“iÌÀˆVÊ ˆ˜ˆ“Õ“Ê iÃVi˜ÌÊ
ÌˆÌÕ`iÊ­
®ÊœÀÊ iVˆÃˆœ˜Êiˆ} ÌÊ­ ®ÊV>˜ÊLiÊÃiÌÊ ˆ˜ÊÌ iÊ/ˆ“iÀÉ,iviÀi˜ViÃÊ7ˆ˜`œÜÊ>˜`ʈÃÊÀiÃiÌÊÜ i˜ÊÌ iÊ«œÜiÀʈÃÊVÞVi`°ÊÊ7 i˜Ê>V̈Ûi]ÊÌ iÊ>ÌˆÌÕ`iÊÃiÌ̈˜}ʈÃÊ `ˆÃ«>Þi`Ê̜ÊÌ iÊLœÌ̜“ʏivÌʜvÊÌ iÊ
Ìˆ“iÌiÀ°ÊÊ"˜ViÊÌ iÊ>ÌˆÌÕ`iʈÃÊÜˆÌ ˆ˜ÊÌ iÊÀ>˜}iʜvÊÌ iÊÌ>«i]Ê>ÊLÕ}Ê>««i>ÀÃÊ INSTRUMENTS >ÌÊÌ iÊÀiviÀi˜ViÊ>ÌˆÌÕ`iʜ˜ÊÌ iÊ
Ìˆ“iÌiÀ°ÊÊ/ iÊvœœÜˆ˜}ÊۈÃÕ>Ê>˜˜Õ˜Vˆ>̈œ˜ÃʜVVÕÀÊÜ i˜Ê>««Àœ>V ˆ˜}ÊÌ iÊ FLIGHT
É \ UÊ7 i˜ÊÌ iÊ>ˆÀVÀ>vÌÊ>ÌˆÌÕ`iÊ`iÃVi˜`ÃÊ̜ÊÜˆÌ ˆ˜ÊÓxääÊviiÌʜvÊÌ iÊ
É ÊÃiÌ̈˜}]ÊÌ iÊ
,"Ê  ÊLœÝÊ>««i>ÀÃÊ with the altitude in light blue text. The bug appears on the altitude tape in light blue once in range.

UÊ7 i˜ÊÌ iÊ>ˆÀVÀ>vÌÊ«>ÃÃiÃÊÌ ÀœÕ} Ê£ääÊviiÌʜvÊÌ iÊ
É ]ÊÌ iÊLÕ}Ê>˜`ÊÌiÝÌÊÌÕÀ˜ÊÜ ˆÌi° EIS UÊ"˜ViÊÌ iÊ>ˆÀVÀ>vÌÊÀi>V iÃÊ
É ]ÊÌ iÊLÕ}Ê>˜`ÊÌiÝÌÊÌÕÀ˜ÊÞiœÜÊ>˜`ÊÌ iÊ>ÕÀ>Ê>iÀÌ]ʺ ˆ˜ˆ“Õ“Ã°Ê ˆ˜ˆ“Փû]Ê is heard.

Light Blue Within 2500 ft White Within 100 ft Yellow When Altitude Reached AUDIO PANEL & CNS

MDA/DH Bug MANAGEMENT FLIGHT

Barometric Minimum

Box AVOIDANCE HAZARD Figure 2-38 Barometric MDA/DH Alerting Visual Annunciations

Setting the barometric Minimum Descent Altitude/Decision Height and bug:

1) Press the TMR/REF Softkey. AFCS 2) Turn the large FMS Knob to highlight the Minimums field. 3) Turn the small FMS Knob to select BARO. Off is selected by default. Press the ENT Key or turn the large FMS

Knob to highlight the next field. ADDITIONAL FEATURES 4) Use the small FMS Knob to enter the desired altitude from zero to 16,000 feet. 5) To remove the window, press the CLR Key or the TMR/REF Softkey. APPENDICES

Figure 2-39 MDA/DH Setting (Timer/References Window)

iÀ̈˜}ʈÃʈ˜ ˆLˆÌi`ÊÜ ˆiÊÌ iÊ>ˆÀVÀ>vÌʈÃʜ˜ÊÌ iÊ}ÀœÕ˜`Ê>˜`Ê՘̈ÊÌ iÊ>ˆÀVÀ>vÌÊÀi>V iÃÊ£xäÊviiÌÊ>LœÛiÊÌ i Ê INDEX
É °ÊÊvÊÌ iÊ>ˆÀVÀ>vÌÊ«ÀœVii`ÃÊ̜ÊVˆ“LÊ>vÌiÀÊ >ۈ˜}ÊÀi>V i`ÊÌ iÊ
É ]ʜ˜ViʈÌÊÀi>V iÃÊxäÊviiÌÊ>LœÛiÊÌ iÊ
É ]Ê>iÀ̈˜}ʈÃÊ`ˆÃ>Li`°

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 77 FLIGHT INSTRUMENTS

2.4 ABNORMAL OPERATIONS SYSTEM OVERVIEW ABNORMAL GPS CONDITIONS / iÊ>˜˜Õ˜Vˆ>̈œ˜ÃʏˆÃÌi`ʈ˜Ê/>LiÊӇÎÊV>˜Ê>««i>Àʜ˜ÊÌ iÊ-ÊÜ i˜Ê>L˜œÀ“>Ê*-ÊVœ˜`ˆÌˆœ˜ÃʜVVÕÀ°ÊÊ,iviÀÊÌœÊ Ì iʏˆ} ÌÊ >˜>}i“i˜ÌÊ-iV̈œ˜ÊvœÀʓœÀiʈ˜vœÀ“>̈œ˜Êœ˜Ê i>`Ê,iVŽœ˜ˆ˜}Ê œ`i° FLIGHT

INSTRUMENTS Annunciation Location Description Lower left of Loss of Integrity Monitoring–GPS integrity is insufficient for the current LOI aircraft symbol phase of flight

EIS Lower left of Integrity OK–GPS integrity has been restored to within normal limits INTEG OK aircraft symbol (annunciation displayed for 5 seconds) Upper right of Dead Reckoning–System is using projected position rather than GPS position DR aircraft symbol to compute navigation data and sequence active flight plan waypoints

& CNS Table 2-3 Abnormal GPS Conditions Annunciated on HSI AUDIO PANEL AUDIO FLIGHT MANAGEMENT

HAZARD Figure 2-40 Example HSI Annunciations AVOIDANCE

i>`Ê,iVŽœ˜ˆ˜}Ê­ ,®Ê œ`iÊV>ÕÃiÃÊÌ iÊvœœÜˆ˜}ʈÌi“Ãʜ˜ÊÌ iÊ* Ê̜ÊLiÊà œÜ˜Êˆ˜ÊÞiœÜÊÜ i˜Ê*-ʈÃÊÌ iÊ ÃiiVÌi`ʘ>ۈ}>̈œ˜ÊÜÕÀViÊ`ÕÀˆ˜}Ê ˜ÀœÕÌiÊ­ ,®ÊœÀÊ"Vi>˜ˆVÊ­" ®Ê« >ÃiÃʜvÊyˆ} Ì\ AFCS UÊ Ê­Ài“œÛi`Ê>vÌiÀÊÓäʓˆ˜ÕÌiî UÊ ÕÀÀi˜ÌÊ/À>VŽÊ Õ} UÊ7ˆ˜`Ê >Ì> UÊ ˆÃÌ>˜ViÃʈ˜ÊÌ iÊ i>Àˆ˜}ʘvœÀ“>̈œ˜Ê7ˆ˜`œÜà FEATURES ADDITIONAL UÊ*-ÊLi>Àˆ˜}Ê«œˆ˜ÌiÀà UÊÀœÕ˜`Ê-«ii` It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become ˆ˜VÀi>Ș}ÞÊ՘Àiˆ>LiÊ>˜`ʓÕÃÌʘœÌÊLiÊÕÃi`Ê>ÃÊ>Ê܏iʓi>˜Ãʜvʘ>ۈ}>̈œ˜°ÊÊ-iiÊÌ iʏˆ} ÌÊ >˜>}i“i˜ÌÊÃiV̈œ˜Ê APPENDICES for more information about DR mode INDEX

78 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A FLIGHT INSTRUMENTS OVERVIEW UNUSUAL ATTITUDES SYSTEM When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the horizon warn of extreme «ˆÌV °ÊÊ/ iÊV iÛÀœ˜ÃÊ>ÀiÊ`ˆÃ«>Þi`ʜ˜ÊÌ iÊ
Ì̈ÌÕ`iʘ`ˆV>̜À]ÊÃÌ>À̈˜}Ê>ÌÊxäÂÊ>LœÛiÊ>˜`ÊÎäÂÊLiœÜÊÌ iÊ œÀˆâœ˜Ê line. INSTRUMENTS FLIGHT Nose High Nose Low EIS AUDIO PANEL & CNS

Figure 2-41 Pitch Attitude Warnings MANAGEMENT FLIGHT vÊ«ˆÌV ÊiÝVii`ÃʳÎäÂɇÓäÂʜÀÊL>˜ŽÊiÝVii`ÃÊÈxÂ]Êܓiʈ˜vœÀ“>̈œ˜Ê`ˆÃ«>Þi`ʜ˜ÊÌ iÊ* Êis removed. The
Ìˆ“iÌiÀÊ>˜`Ê
ˆÀëii`]Ê
Ì̈ÌÕ`i]Ê6iÀ̈V>Ê-«ii`]Ê>˜`ÊœÀˆâœ˜Ì>Ê-ˆÌÕ>̈œ˜Êˆ˜`ˆV>̜ÀÃÊÀi“>ˆ˜Êœ˜ÊÌ iÊ`ˆÃ«>ÞÊ >˜`ÊÌ iÊ i>Àˆ˜}ʘvœÀ“>̈œ˜]Ê
iÀÌÃ]Ê>˜`Ê
˜˜Õ˜Vˆ>̈œ˜Ê܈˜`œÜÃÊV>˜ÊLiÊ`ˆÃ«>Þi`Ê`ÕÀˆ˜}ÊÃÕV ÊÈÌÕ>̈œ˜Ã°ÊÊ/ iÊ vœœÜˆ˜}ʈ˜vœÀ“>̈œ˜ÊˆÃÊÀi“œÛi`ÊvÀœ“ÊÌ iÊ* Ê>˜`ÊÌ iˆÀÊÜv̎iÞÃÊ>ÀiÊ`ˆÃ>Li`ÊÜ i˜ÊÌ iÊ>ˆÀVÀ>vÌÊiÝ«iÀˆi˜ViÃÊ AVOIDANCE unusual attitudes: HAZARD UÊ/À>vwVÊ
˜˜Õ˜Vˆ>̈œ˜Ã UÊ7ˆ˜`œÜÃÊ`ˆÃ«>Þi`ʈ˜ÊÌ iʏœÜiÀÊ UÊ6iÀ̈V>Ê iۈ>̈œ˜]Ê ˆ`iϜ«i]Ê UÊ
 -Ê
˜˜Õ˜Vˆ>̈œ˜Ã right corner of the PFD: and Glidepath Indicators Uʏˆ} ÌÊ ˆÀiV̜ÀÊ œ““>˜`Ê >Àà qÊ/ˆ“iÀÉ,iviÀi˜Vià UÊ
Ìˆ“iÌiÀÊ >Àœ“iÌÀˆVÊ-iÌ̈˜}

UʘÃiÌÊ >« qÊ i>ÀiÃÌÊ
ˆÀ«œÀÌà UÊ-iiVÌi`Ê
ÌˆÌÕ`i AFCS UÊ"ÕÌÈ`iÊ
ˆÀÊ/i“«iÀ>ÌÕÀiÊ­"
/® – Flight Plan UÊ6 6Ê/>À}iÌÊ
ÌˆÌÕ`i UÊ7ˆ˜`Ê >Ì> qÊ
iÀÌà UÊ-ÞÃÌi“Ê/ˆ“i ADDITIONAL UÊ-iiVÌi`Êi>`ˆ˜}Ê,i>`œÕÌ – Procedures UÊ/À>˜Ã«œ˜`iÀÊ-Ì>ÌÕÃÊ œÝ FEATURES UÊ-iiVÌi`Ê œÕÀÃiÊ,i>`œÕÌ UÊ ˆ˜ˆ“Õ“Ê iÃVi˜ÌÊ
ÌˆÌÕ`iÉ iVˆÃˆœ˜Êiˆ} ÌÊ,i>`œÕÌ UÊ* Ê-iÌÕ«Ê i˜Õ APPENDICES INDEX

190-00498-07 Rev. A Garmin G1000 Pilot’s Guide for Cessna Nav III 79 FLIGHT INSTRUMENTS SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS & CNS AUDIO PANEL AUDIO FLIGHT MANAGEMENT

BLANK PAGE HAZARD AVOIDANCE AFCS FEATURES ADDITIONAL APPENDICES INDEX

80 Garmin G1000 Pilot’s Guide for Cessna Nav III 190-00498-07 Rev. A