Integrated Flight Deck Cockpit Reference Guide Cessna Nav III
Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0563.05 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in Cessna Nav III aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00384-03 (Rev. A) 190-00384-03 (Rev. B) 190-00384-04 (Rev. A) Reformatted manual to new format Added TAS capability 190-00384-04 (Rev. B) Added DONE Softkey, XM-INFORMATION Page, and XM-RADIO Page operation. 190-00384-05 (Rev.
RECORD OF REVISIONS Revision Date of Revision Affected Pages A November, 2007 i through Index-4 RR-2 Description Production release Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-5 MFD Softkeys .......................................................... 1-8 MFD Page Groups ................................................... 1-9 Vertical Navigation .............................................. 1-10 Backlighting ............
TABLE OF CONTENTS 6.4 Autopilot Operation ............................................ 6-22 Flight Control ............................................................ 6-22 Engaging the Autopilot.............................................. 6-22 Control Wheel Steering.............................................. 6-23 Disengaging the Autopilot ......................................... 6-23 6.5 Example Procedures ............................................ 6-24 Departure ...................................
TABLE OF CONTENTS 10.4 Traffic Systems ...................................................... 10-7 Traffic Information Service (TIS) .................................. 10-7 Traffic Advisory System (TAS) (Optional) ..................... 10-8 ADS-B Traffic (Optional) ............................................. 10-9 10.5 Terrain and Obstacle Proximity ....................... 10-10 Displaying Terrain and Obstacles on the Terrain Proximity Page ........................................................
TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the Garmin G1000 Pilot’s Guide for the Cessna Nav III (19000498-03). 190-00384-08 Rev.
SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS 1 2 4 3 5 6 7 8 9 17 18 24 19 25 20 26 21 27 22 28 23 29 GFC 700 AFCS Only 1-2 10 14 11 15 12 16 13 Figure 1-1 PFD/MFD Controls Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same. 8 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field. 9 COM VOL/SQ Knob – Controls COM audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume level is shown in the field as a percentage. 1 NAV VOL/ID Knob – Controls the NAV audio level.
SECTION 1 SYSTEM OVERVIEW side of the display, indicating the availability of additional items within the selected category. Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list. 14 15 16 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. PROC Key – Selects approaches, departures and arrivals from the flight plan.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON Softkey OFF Figure 1-2 PFD Top Level Softkeys DME ALERTS STRMSCP ALERTS Press the BACK or OFF Softkey to return to the top-level softkeys. Figure 1-3 INSET Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey.
SECTION 1 SYSTEM OVERVIEW DME DME ALERTS ALT UNIT HSI FRMT BRG1 (NAV1) BRG2 (NAV2) BRG1 (GPS) BRG2 (GPS) BRG1 (ADF) BRG2 (ADF) BRG1 (OFF) BRG2 (OFF) 360 HSI ALERTS Press the STD BARO or BACK Softkey to return to the top-level softkeys ARC HSI ALERTS ALERTS METERS IN HPA ALERTS Figure 1-4 PFD Configuration Softkeys PFD – Press to display the additional softkeys for additional configuration of the PFD. DFLTS – Press to reset default settings on the PFD.
SECTION 1 SYSTEM OVERVIEW GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF in the BRG2 Information Window when an otional ADF is installed. OFF – Removes the BRG2 Information Window. ALT UNIT – Displays softkeys for setting the altimeter and BARO settings to metric units: METERS – When enabled, displays altimeter in meters. IN – Press to display the BARO setting as inches of mercury. HPA – Press to display the BARO setting as hectopacals.
SECTION 1 SYSTEM OVERVIEW IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports Window. ALERTS – Press to display the Alerts Window. 1.3 MFD SOFTKEYS MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Traffic on the Navigation Map.
SECTION 1 SYSTEM OVERVIEW AIRWAYS – Pressing this softkey displays/removes airways information. The default is dependent on map setup option selected. Pressing cycles through all airways displayed (AIRWY ON), low altitude airways only (AIRWY LO), and high altitude airways only (AIRWY HI). STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the Navigation Map.
SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION One of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance for a WAAS approach after the Final Approach Fix. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-WAAS systems. The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation.
SECTION 1 SYSTEM OVERVIEW White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical speed and deviation guidance.
SECTION 1 SYSTEM OVERVIEW 1.6 BACKLIGHTING 1.8 Manually adjust the backlight for the PFD and MFD: 1) Press the MENU Key on the PFD to display the PFD Setup Menu window. 2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the small FMS Knob to display the selection window. 4) Turn the small FMS Knob to select ‘MANUAL’, then press the ENT Key. 5) With the intensity value now highlighted, turn the small FMS Knob to select the desired backlighting.
SECTION 1 SYSTEM OVERVIEW 2) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the databases are initialized and displayed on the scrolling window of the splash screen. When updating the terrain and FliteCharts databases, an ‘in progress’ message may be seen. If this message is present, wait for the system to finish loading before verifying the correct databases are initialized, then proceed to step 3.
SECTION 1 SYSTEM OVERVIEW Blank Page 1-14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 15 1 14 2 13 12 3 11 4 10 5 9 8 7 6 1 Traffic Annunciation 2 Vspeed References 3 Selected Heading Box 4 Wind Data Window 5 Inset Map 6 BRG1 Information Window 7 DME Information Window 8 BRG2 Information Window 9 Flight Plan Window 10 Barometric Minimums Box 11 Selected Altitude Bug 12 Selected Course Box 13 Barometric Minimums Bug 14 Vertical Deviation/Glidepath (WAAS enabled systems only)/Glidesope Indicator 15 Marker Beacon Annunciation F
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Actual Airspeed Vspeed References Vspeed References Speed Ranges Airspeed Trend Vector True Airspeed Box Figure 2-4 Airspeed Indicator Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Trend Vector Altitude Reference Box Altitude Reference Bug The end of the trend vector displays approximately what the altitude will be in six seconds if the current rate of vertical speed is maintained. Barometric Setting Box Altitude Trend Vector Current Altitude Select barometric pressure: Turn the BARO Knob to select the desired setting. Quickly enter standard pressure: 1) Press the PFD Softkey.
SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation Metric Display Display altitude in meters and barometric pressure in hectopascals: 1) Press the PFD Softkey to display the second level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to display altitude in meters. 4) Press the HPA Softkey to display the barometric setting in hectopascals. Press the IN Softkey to display the barometric setting in inches of mercury.
SECTION 2 FLIGHT INSTRUMENTS 2.4 VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach (see Figure 2-11). In systems that are WAAS enabled, the Glidepath Indicator appears at a point prior to the FAF when executing an LPV, LNAV/VNAV, or LNAV+V approach (see Figure 2-12).
SECTION 2 FLIGHT INSTRUMENTS 2.5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker 2.7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitude minimums can be set in the Timer/References Window. The altitude ranges from 0 to 16,000 feet in 10-foot increments. The minimums are reset anytime the power is cycled. Figure 2-16 Barometric Minimum Descent Altitude Settings Altimeter Figure 2-14 Marker Beacon Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft HSI FRMT Softkey, followed by the 360 HSI or the ARC HSI Softkey. 15 Barometric Minimum Bug 14 1 13 2 Barometric Minimum Box Altitude Reached 3 12 4 11 5 10 9 6 8 7 Figure 2-17 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2 Set the barometric altitude minimums: 3 1) Press the TMR/REF Softkey. 4 2) Turn the large FMS Knob to highlight the ‘Minimums’ field (Figure 2-16).
SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
Departure Enroute Terminal Terminal (Oceanic if >200 nm from nearest airport) 0.3 nm 1.0 nm 1.0 nm 2.0 nm 1.0 nm 0.3 nm CDI Full-scale Deflection SECTION 2 FLIGHT INSTRUMENTS Refer to accompanying approach CDI scaling figures Missed Approach Approach Drawing not to scale 2 nmFAF 2 nmFAF CDI scale varies if Vectors-To-Final is activated CDI scale varies if Vectors-To-Final is activated Drawing not to scale Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling 2-10 0.
SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer. Press the BRG1 or BRG2 Softkey to cycle through selecting NAV1/2, GPS, or ADF for display using the corresponding pointer.
SECTION 2 FLIGHT INSTRUMENTS • OBS – Displayed when operating in OBS Mode. • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. • DR – Navigating using Dead Reckoning due to an error in the GPS solution. 2.9 WIND DATA When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”.
SECTION 2 FLIGHT INSTRUMENTS 2.10 GENERIC TIMER Figure 2-31 Timer Status Prompts Change the Generic Timer: 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. 2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now highlighted.
SECTION 2 FLIGHT INSTRUMENTS Blank Page 2-14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpm range indicates above normal operating speeds (Models 172S, 206H, and T206H) 3 Fuel Flow Indicator (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 10 11 Fuel Quantity Indicator (FUEL QTY GAL) – Shows the quantity of fuel in the tanks, in gallons, ranging from zero to full (F) for each fuel tank (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S). 12 Voltmeter (M, E BUS VOLTS) – Displays the main and essential bus voltages. 13 Ammeter (M, S BATT AMPS) – Shows the main and standby battery load in amperes.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 Cruise Fuel Flow 4 3 4 5 5 6 6 8 8 10 10 12 12 13 13 Model T182T Maximum Takeoff Fuel Flow Model T206H Figure 3-2 Engine Display (Turbocharged Aircraft) 190-00384-08 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 LEAN DISPLAY for the selected cylinder to be displayed below the indicator. NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH). 3-4 1 Engine Manifold Pressure Gauge (MAN IN) Models 182T, T182T, 206H, T206H – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 2 1 2 1 2 5 2 5 3 3 Hollow Block Represents Peak 5 5 6 6 3 3 7 7 Model 172R 6 6 7 Model 172S 7 Model 182T Model 206H Figure 3-3 Lean Display (Normally-aspirated Aircraft) 190-00384-08 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 3 4 4 5 5 6 6 7 7 Model T182T Model T206H Figure 3-4 Lean Display (Turbocharged Aircraft) The Lean Display is accessed by pressing the ENGINE Softkey followed by the LEAN Softkey and provides information for performing engine leaning. 3-6 From the Lean Display, the pilot can utilize the CYL SLCT and ASSIST softkeys to obtain information about specific cylinders.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) The ASSIST Softkey aids in the leaning process by identifying the peak of the first cylinder whose temperature falls. If the temperature of the peaked cylinder exceeds the peak value, the peak value is not updated. Press the ASSIST Softkey to stop peak monitoring. Normally-aspirated Aircraft For normally-aspirated aircraft, when a cylinder peaks, its peak is represented by a hollow block on the EGT Bar Graph.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-8 1 Engine Manifold Pressure Gauge (MAN IN) Models 182, T182, 206, T206 – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182 only). 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 2 2 3 3 4 4 7 7 8 8 9 9 10 10 11 11 12 12 Model 172R Model 172S 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 11 11 12 12 Model 182T Model 206H Figure 3-5 System Display (Normally-aspirated Aircraft) 190-00384-08 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 11 11 12 12 Model T182T Model T206H Figure 3-6 System Display (Turbocharged Aircraft) 3-10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes share the same locations on the on the Primary Flight Display and the Multi-Function Display. NAV Controls NAV Frequency Box COM Frequency Box Figure 4-1 G1000 VHF NAV/COM Interface (PFD shown) 190-00384-08 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Standby COM Frequency Field Tuning Box Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS Squelch Indication • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Figure 4-7 Squelch Indication • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.4 • ID – When the Morse code identifier is ON for a NAV radio, a white ‘ID’ indication appears to the left of the corresponding active NAV frequency.
SECTION 4 – NAV/COM & TRANSPONDER 4.7 ADF Radio (optional) The G1000 does not support tuning of the ADF in Nav III aircraft. ADF tuning is accomplished through the Bendix/King KR 87 ADF Radio. ADF volume must also be adjusted through the KR 87. 4.6 FREQUENCY AUTO-TUNING TRANSPONDER Mode Selection The STBY, ON, ALT, GND, VFR, CODE, and IDENT Softkeys can be accessed by pressing the XPDR Softkey.
SECTION 4 – NAV/COM & TRANSPONDER Altitude Mode (Automatic or Manual) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. All transponder replies requesting altitude information are provided with pressure altitude information.
SECTION 4 – NAV/COM & TRANSPONDER Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference Window. Flight ID Figure 4-16 Timer/References Window 1) Press the TMR/REF Softkey to display the Timer/ References Window. 2) Turn the large FMS Knob to place the cursor in the Flight ID field. 3) Turn the small FMS Knob to enter the desired first character. 4) Turn the large FMS Knob to place the cursor in the next desired field.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters Receiver Audio Disabled Passenger Address (Disabled on 172R/S) Cabin Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (Optional, disabled if ADF and/or DME are not installed) Aircraft Navigation Radio Audio Disabled Manual Squelch Digital Clearance Recorder Play Key ICS Isolation VOL/SQ VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Front Panel Controls 190-00384-08 Rev.
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key. Figure 5-2 Transceivers 5.
SECTION 5 – AUDIO PANEL 5.6 Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1. Figure 5-5 Marker Beacon 5.5 INTERCOM SYSTEM (ICS) ISOLATION NAV RADIO AUDIO SELECTION Pressing DME, ADF, NAV1, or NAV2 selects and deselects the audio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These four keys can be selected individually or together.
SECTION 5 – AUDIO PANEL 5.7 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively. • Pressing the MKR/MUTE Key while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL NOTE: The Aircraft Flight Manual (AFM) always supersedes the information in this guide. This section only applies to the GFC 700 Automatic Flight Control System (AFCS). 6.1 AFCS CONTROLS The following dedicated AFCS keys are located on the bezels of the PFD and MFD: acknowledge an autopilot disconnect and mute the associated aural tone.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.2 FLIGHT DIRECTOR OPERATION With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (+20°/-15°) and bank (22°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification. The flight director also provides commands to the autopilot.
SECTION 6 – AUTOMATIC FLIGHT CONTROL AFCS Status Box Flight director roll modes are shown on the left and pitch on the right. Armed modes are annunciated in white and active in green. Autopilot status is displayed in the center of the AFCS Status Box. 6.3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Table 6-1 lists the pitch modes with their corresponding controls and annunciations. The mode reference (shown with default measurement units) is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/ NOSE DN Keys can be used to change the pitch mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) Changing the Pitch Reference When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when the mode is activated.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Selected Altitude Capture Mode (ALTS) Selected Altitude Capture Mode arms automatically when the flight director is in Pitch Hold, Vertical Speed, Flight Level Change, or Go Around Mode. This mode is also armed automatically under Vertical Path Tracking Mode when the Selected Altitude is to be captured instead of the VNAV Target Altitude. The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 6-5 for example).
SECTION 6 – AUTOMATIC FLIGHT CONTROL If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed. To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected Altitude is reached.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode Active Vertical Selected Altitude Capture Speed Mode Armed Reference Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Figure 6-8 Vertical Speed Mode Changing the Vertical Speed Reference The Vertical Speed Reference (shown both in the AFCS Status Box and above/below the Vertical Speed Indicator) may be changed by: • Using the NOSE UP/NOSE DN Keys • By pressing the CWS Butt
SECTION 6 – AUTOMATIC FLIGHT CONTROL descent). The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Navigation Modes (VPTH, ALTV) NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The autopilot guides the aircraft back to the descent path upon release of the CWS Button. NOTE: VNAV flight director pitch modes are available only in conjunction with GPS roll modes. NOTE: The Selected Altitude takes precedence over any other vertical constraints.
SECTION 6 – AUTOMATIC FLIGHT CONTROL In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Data Box, VNAV indications (VNAV Target Altitude, vertical deviation, and vertical speed required) appear on the PFDs in magenta (Figure 6-11).
SECTION 6 – AUTOMATIC FLIGHT CONTROL When a descent leg is captured (Figure 6-12), Vertical Path Tracking becomes active and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.
SECTION 6 – AUTOMATIC FLIGHT CONTROL VNAV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile recapture.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture mode are armed in preparation to capture the new VNAV Target Altitude or the Selected Altitude, depending on which altitude is to be intercepted first. VNAV target altitudes can be changed while editing the active flight plan (see the Navigation section for details).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Figure 6-16 Glidepath Mode Armed If vertical guidance becomes or is expected to become unavailable and the approach downgrades, Glidepath Mode is disarmed. When vertical guidance becomes available again, Glidepath Mode is automatically re-armed under GPS Approach Mode. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around (GA) Mode Pushing the GA Switch engages the flight director in a wings level, 7° pitch-up attitude, allowing the execution of a missed approach or a go around. This mode is a coupled pitch and roll mode and is annunciated as ‘GA’ in both the pitch and roll active mode fields. Go Around Mode disengages the autopilot and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the aircraft attitude (i.e.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Roll Modes • Roll Hold (default mode) — Holds the current aircraft roll attitude or rolls the wings level, depending on the commanded bank angle • Heading Select — Captures and tracks the Selected Heading • Navigation (GPS, VOR, LOC) — Captures and tracks the selected navigation source • Backcourse — Captures and tracks a localizer signal for backcourse approaches • Approach (GPS, VAPP, LOC) — Captures and tracks the selected navigation source with greater sensitivity f
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) Figure 6-20 Roll Hold Mode Annunciation Bank Angle Flight Director Response < 6° Rolls wings level 6° to 22° Maintains current aircraft roll attitude > 22° Limits bank to 22° Heading Select Mode is activated by pressing HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes of more than 330° at a time result in turn reversals. Navigation Mode (GPS, VOR, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Backcourse Mode (BC) Changing the Selected Course NOTE: When making a backcourse approach, set the Selected Course to the localizer front course. Backcourse Mode captures and tracks a localizer signal. The mode may be selected by pressing the BC Key. Backcourse Mode is armed if the CDI is greater than one dot when the mode is selected. The flight director creates roll steering commands from the Selected Course and deviation when in Backcourse Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.4 AUTOPILOT OPERATION NOTE: Refer to the AFM for specific instructions regarding emergency procedures. Cessna Nav III’s autopilot operates flight control surface servos to provide automatic flight control. The autopilot controls the aircraft pitch and roll attitudes following commands received from the flight director. Pitch autotrim provides trim commands to the pitch trim adapter to relieve any sustained effort required by the pitch servo.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Control Wheel Steering During autopilot operation, the aircraft may be handflown without disengaging the autopilot. Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand-flown. At the same time, the flight director is synchronized to the aircraft attitude during the maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS maneuvers.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.5 EXAMPLE PROCEDURES NOTE: The diagrams in this section are for instructional purposes only and should not be used for navigation. This section provides a scenario-based set of procedures showing various GFC 700 AFCS modes used while following a previously entered flight plan. The following example closely follows the example flight plan discussed in the Navigation section. Refer to the example in Section 7 - Navigation when studying the this example.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure c) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode. Climbing to the Selected Altitude and flying an assigned heading: 1) Use the ALT Knob to set the Selected Altitude to 12,000 feet after takeoff. Depart KMKC: 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). a) Adjust the aircraft’s vertical speed to the desired 1,000 fpm.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan/GPS Course b) Press the NAV Key to activate GPS Navigation Mode. The autopilot guides the aircraft along the active flight plan leg. NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level). If the NAV Key is not pressed within 10 seconds of VOR signal loss, the flight director reverts to Roll Hold Mode (wings rolled level).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Descent While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for the descent from 12,000 ft: • Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a constant airspeed. This descent method does not account for flight plan waypoint altitude constraints.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV Target Altitude: • Turn the ALT Knob to adjust the Selected Altitude • Press the VNV Key 1) Select VNV flight control: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT Knob, set the Selected Altitude at least 75 feet below the flight plan’s VNV Target Altitude of 10,000 feet.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Non-path descent using Flight Level Change Mode: The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 1) Command a non-path descent using Flight Level Change Mode: a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach KCOS Flying an ILS approach: PETEY 2 G HD e od M PYNON 1 GPS NAV Mode 2) Arm LOC Approach and Glideslope modes. a) Ensure the appropriate localizer frequency is tuned. b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. 3 LOC APR/ GS Mode 1) Transition from GPS Navigation Mode to Heading Select Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a WAAS precision approach: 2) Press the APR Key once clearance for approach has been acquired. GPS Approach Mode is activated and Glidepath Mode is armed. 4 CEGIX 3 GPS APR/ GP Mode 1) Arm flight director modes for a precision approach: a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). b) Load the Runway 35R LPV approach for KCOS into the flight plan.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around/Missed Approach NOTE: As a result of calculations performed by the system while flying the holding pattern, the display may re-size automatically and the aircraft may not precisely track the holding pattern. Flying a missed approach: 1) Push the GA Switch at the Decision height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Alerts The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Overspeed Protection Overspeed protection is provided in situations where the flight director cannot acquire and maintain the vertical Mode Reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed. When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-36 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The majority of the following discussions pertain to the Multi Function Display. In discussions pertaining to the PFD, the controls are located on the PFD. 7.1 NAVIGATION MAP PAGE WARNING: The map display should only be used for situational awareness. Any map display indication should be compared with approved navigation sources. 7.
SECTION 7 – NAVIGATION 9) Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field. 10) Enter the desired target altitude offset from the selected Direct-to. 11) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘COURSE’ field. 12) Enter the desired course to the waypoint. Select a Direct-to Destination to a Nearest Airport 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left.
SECTION 7 – NAVIGATION 9) Turn the large FMS Knob to place the cursor in the ‘COURSE’ field. 10) Enter the desired course. 11) Press the ENT Key. The cursor now highlights ‘ACTIVATE?’. Figure 7-5 Recently Entered Waypoints List (MFD) 3) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints as shown in Figure 7-5. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to.
SECTION 7 – NAVIGATION Enter a Direct-to Destination Select a Direct-to Destination to a Flight Plan Waypoint 1) Press the Direct-to Key ( ). 2) Turn the large FMS Knob to place the cursor in the desired selection field. 1) While navigating an active flight plan, press the Direct-to ( ) Key. 3) Turn the small FMS Knob to begin selecting the desired identifier, location, etc. 2) Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7-8. 4) Press the ENT Key.
SECTION 7 – NAVIGATION 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press the ENT Key again to activate a Direct-to. Select a Direct-to Destination to a Recently Entered Identifier 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-8. The list is only populated when navigating a flight plan.
SECTION 7 – NAVIGATION 2) Figure 7-11 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight phase displayed on the HSI indicating 1.0 nm CDI scaling. 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 7-12. Figure 7-12 Assigned Heading of 290º Figure 7-11 Assigned Heading of 240º 7-6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 7 – NAVIGATION 4) V4 is now entered into the flight plan. a) Press the FMS Knob to activate the cursor. b) The desired entry point for V4 (TOP) must now be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point as shown in Figure 7-13. The V4 entry point (TOP) is placed immediately above the highlighted waypoint (SLN). c) Turn the small FMS Knob to display the Waypoint Information Window.
SECTION 7 – NAVIGATION e) With SLN still highlighted as in Figure 7-15, turn the small FMS Knob to the right. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. Figure 7-17 List of Available Exits for V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as seen in Figure 7-17.
SECTION 7 – NAVIGATION l) V4 is now loaded into the flight plan as shown in Figure 7-19. (XTK) distance on the HSI indicating 16.9 nm to the intercept point. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed to 2.0 nm. Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 is now made the active leg of the flight plan.
SECTION 7 – NAVIGATION 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 7-22. 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 7-23. Figure 7-23 Turn to Intercept V244 9) As seen in Figure 7-24, V244 is now the active flight plan leg. Figure 7-22 Turn on to Active Leg 7-10 Figure 7-24 V244 Now Active Leg Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 7-25. Figure 7-26 Direct To OPSHN Figure 7-25 HYS to LAA Leg Active d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7-27. 11) ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and issues a crossing altitude restriction of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor.
SECTION 7 – NAVIGATION f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database, those altitudes are displayed as white numerals. This indicates the altitudes will not be used by the system for vertical guidance until manually accepted by the pilot. To accept the displayed altitude, place the cursor over the altitude and press the ENT Key.
SECTION 7 – NAVIGATION b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7-31. e) Press the ENT Key. A list of available transitions for the selected approach is displayed as shown on Figure 7-32. Figure 7-30 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 7-31.
SECTION 7 – NAVIGATION h) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 7-34.
SECTION 7 – NAVIGATION a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 7-35. b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to enter the desired value. 15) As seen in Figure 7-36, the aircraft is approaching TOD. Note the target vertical speed required to reach the selected altitude.
SECTION 7 – NAVIGATION 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-38. Keep Vertical Deviation Pointer Centered 18) The aircraft is approaching OPSHN. The upcoming turn and next heading is annunciated at the top left of the PFD as seen in Figure 7-40. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
SECTION 7 – NAVIGATION 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 7-41. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-41 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 7-42).
SECTION 7 – NAVIGATION 21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-43). 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
SECTION 7 – NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-46) when the final approach course becomes active.
SECTION 7 – NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368FT’) is not part of the published procedure. It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach is exceeded.
SECTION 7 – NAVIGATION 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 7-49. 7.4 AIRPORT INFORMATION Figure 7-51 Airport Information Page Figure 7-49 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 7-50. Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION Select an Airport from the Active Flight Plan 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7-52. Figure 7-52 Flight Plan Airport List 3) Turn the large FMS Knob to select the desired airport. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key.
SECTION 7 – NAVIGATION Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport. Continue turning the small FMS Knob to select the desired runway. 7.
SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-56 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1) With the NDB Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired selection field (identifier, name or closest city).
SECTION 7 – NAVIGATION 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.9 NEAREST AIRPORTS Access Information on a Specific Airport 1) With the Nearest Airports Page displayed, press the APT Softkey to place the cursor in the ‘NEAREST AIRPORTS’ field. The first airport in the nearest airports list is highlighted. 2) Turn either FMS Knob to highlight the desired airport.
SECTION 7 – NAVIGATION Nearest Airports Information on the PFD Bearing TO 7.10 NEAREST INTERSECTIONS Distance Airport Symbol Identifier Runway Length Primary COM Frequency Figure 7-59 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports Window. View Information on a Specific Airport in the List 1) With the Nearest Airports Window displayed, turn either FMS Knob to place the cursor on the desired airport identifier.
SECTION 7 – NAVIGATION 7.11 NEAREST NDB 7.12 NEAREST VOR Figure 7-62 Nearest VOR Page Figure 7-61 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon. Access Information on a Specific NDB 1) With the Nearest NDB Page displayed, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired NDB.
SECTION 7 – NAVIGATION 2) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. Waypoint Page pertains to the selected Nearest User Waypoint. 3) Press the FMS Knob to remove the flashing cursor. 3) Press the FMS Knob to remove the flashing cursor. 7.13 NEAREST USER WAYPOINT Figure 7-63 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1) Turn the large FMS Knob to select the ‘NRST’ page group.
SECTION 7 – NAVIGATION 3) Press the ENT Key to load the frequency into the COM frequency standby field. • If the aircraft has entered an airspace, ‘Inside’ is displayed. 4) Press the FMS Knob to remove the flashing cursor. View Additional Details for a Listed Airspace 7.15 NEAREST AIRSPACES 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to scroll through the list, highlighting the desired airspace.
SECTION 7 – NAVIGATION Blank Page 7-30 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS 4) Repeat steps 2 and 3 until the desired name is entered. 5) Press the ENT Key. 6) Press the ENT Key again to accept the new waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position.
SECTION 8 – FLIGHT PLANNING 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 2) Press the ACT LEG Softkey (using MFD only). Or: Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD. 3) With ‘Activate’ highlighted, press the ENT Key.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. Create a New Flight Plan Using the PFD NOTE: A flight plan cannot be entered using the PFD if another flight plan is active. NOTE: After the first leg is entered (using the PFD only), it is immediately activated.
SECTION 8 – FLIGHT PLANNING 8.8 ENTER AN AIRWAY IN A FLIGHT PLAN 5) When the desired entry point is entered, press the ENT Key. 1) Press the FPL Key to display the active flight plan or display a stored flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the waypoint before which the airway is to be entered.
SECTION 8 – FLIGHT PLANNING 8) Turn either FMS Knob to scroll through the list of available exit points. 8.11 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures. 8.12 REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT PLAN 1) With the Active or Stored Flight Plan Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted.
SECTION 8 – FLIGHT PLANNING 8.14 EDIT A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 8.16 INVERT AND ACTIVATE A STORED FLIGHT PLAN 2) Press the FMS Knob to activate the cursor. 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired flight plan and press the ENT Key. 2) Turn the large FMS Knob to highlight the desired flight plan.
SECTION 8 – FLIGHT PLANNING 8.18 DELETE A FLIGHT PLAN 8.20 TRIP PLANNING 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 1) Turn the large FMS Knob to select the ‘AUX’ page group. 2) Turn the large FMS Knob to highlight the flight plan to be deleted. 2) Turn the small FMS Knob to select the first rectangular page icon. 3) Press the DELETE Softkey. 3) The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’.
SECTION 8 – FLIGHT PLANNING For point-to-point planning, turn the FMS Knobs to enter the identifier of the starting waypoint. Once the waypoints identifier is entered, press the ENT Key to accept the waypoint. The flashing cursor moves to the ending waypoint. Again, turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) If a flight plan is active, the departure airport is displayed as the default. A list of available departures is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 9.2 APPROACHES NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. Figure 9-3 Select Arrival 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key.
SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a flight plan is active, the destination airport is displayed as the default. A list of available approaches is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 7) The cursor moves to the TRANSITIONS field.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ group (Figure 10-2) to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob until the Stormscope Page is selected. This is the third rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE Change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (SERVICE OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – Pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • Winds Aloft • County Warnings • Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group displays the weather products available for the current subscription. A green box by the weather product means that it is available. From within the AUX - XM INFORMATION Page, the pilot may switch to the AUX - XM RADIO Page by pressing the RADIO Softkey.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC SYSTEMS • If Traffic information Service (TIS) is configured, a STANDBY, OPERATE, and TNA MUTE Softkey are displayed. • If a Traffic Advisory System (TAS) is configured, a STANDBY, NORMAL, TEST, and ALT MODE Softkey are displayed. • If an ADS-B traffic system is configured, only the ALT MODE Softkey is displayed. has entered Coast Mode. The system maintains the traffic display (up to 60 seconds) until the next data reception.
SECTION 10 – HAZARD AVOIDANCE Traffic Advisory System (TAS) (Optional) Refer to the Honeywell KTA 870 Pilot’s Guide for a detailed discussion of the KTA 870 system. System Self Test 1) Set the range to 2/6 nm. 2) Press the STANDBY Softkey. 3) Press the TEST Softkey. 4) Self test takes approximately eight seconds to complete. When completed successfully, traffic symbols are displayed as shown in Figure 10-12 and a voice alert “TAS System Test OK” is heard.
SECTION 10 – HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1) Ensure the KTA 870 system is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Traffic is now displayed on the map. Traffic Advisory Symbol Description Traffic Advisory with directional information. Points in the direction of the intruder aircraft track. Traffic Advisory without directional information. Traffic Advisory out of the selected display range.
SECTION 10 – HAZARD AVOIDANCE 10.5 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. 4) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the last rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map Displaying Terrain on the TAWS Page 1) With the Navigation Map displayed, press the MAP Softkey. 2) Press the TERRAIN Softkey. Terrain and obstacle proximity is now displayed on the map. 10.6 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Figure 10-20 TAWS Page Menu TAWS Inhibit Figure 10-18 TAWS Page (360˚ View) Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled. Inhibit TAWS: While the TAWS Page is displayed, press the INHIBIT Softkey. ‘TAWS INHB’ is annunciated in the lower right of portion of the screen.
SECTION 10 – HAZARD AVOIDANCE A system test is automatically performed at power-up. After successful completion of the test, “TAWS System Test, OK” is heard. The system test may also be initiated manually, but only when the aircraft is on the ground. To manually verify proper operation of the aural and visual annunciations of the system, perform the following steps. 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS’. 3) Press the ENT Key.
The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 10-22 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up).
SECTION 10 – HAZARD AVOIDANCE Pop-up Alerts When a terrain or obstacle alert is issued, a pop-up window is displayed on the MFD with the appropriate alert. Figure 10-24 TAWS Alert Pop-Up Press the ENT Key to display the TAWS Page, or press the CLR Key to remain on the existing page.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 10 – HAZARD AVOIDANCE Blank Page 10-18 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters Reversionary Mode. In Reversionary Mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the Reversionary Mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 11 – ABNORMAL OPERATION 11.6 DEAD RECKONING WARNING: DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the lack of satellite measurements needed to determine a position. Changes in wind speed and/or wind direction compound the relative inaccuracy of DR Mode. Because of this degraded accuracy, the crew must maintain position awareness using other navigation equipment until GPS-derived position data is restored.
SECTION 11 – ABNORMAL OPERATION Also, while the G1000 is in DR Mode, the autopilot will not couple to GPS, and both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. 11-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Cessna aircraft Pilot’s Operating Handbook (POH) supersedes information found in this document. The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is based on alert levels described later in the Alert Levels Definitions section.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Cessna Nav III aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention. A warning alert is annunciated in the Annunciation Window and is accompanied by a continuous aural tone. Text appearing in the Annunciation Window is RED. A warning alert is also accompanied by a flashing WARNING Softkey annunciation, as shown in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 NAV III AIRCRAFT ALERTS The following alerts are configured specifically for the Cessna Nav III aircraft. See the Cessna Pilot’s Operating Handbook (POH) for information regarding pilot responses. Safe Operating Annunciation (T182, T206, and 206 with Prop De-Ice Only) Annunciation Window Text PROP HEAT Audio Alert No Tone 12.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.5 TAWS ALERTS The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 12 – ANNUNCIATIONS & ALERTS The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.7 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on areas associated with the failed data. Refer to the POH for additional information regarding pilot responses to these annunciations. NOTE: Upon power-up of the G1000 system, certain boxes remain invalid as G1000 equipment begins to initialize. All boxes should be operational within one minute of power-up.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. Display is not receiving valid transponder information. ‘LOI’ Indicates Loss of Integrity of GPS information. GPS information is either not present or is invalid for navigation use.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch, communication halted. MANIFEST – MFD1 software mismatch, communication halted. PFD1 CONFIG – PFD1 config error. Config service req’d. MFD1 CONFIG – MFD1 config error.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Message MFD1 DB ERR – MFD1 aviation database error exists. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. MFD1 DB ERR – MFD1 terrain database missing. PFD1 DB ERR – PFD1 terrain database missing.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. MFD1 DB ERR – MFD1 SafeTaxi database error exists. PFD1 DB ERR – PFD1 SafeTaxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. DB MISMATCH – Aviation database version mismatch. Xtalk is off. DB MISMATCH – Aviation database type mismatch.
SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Message GMA1 FAIL – GMA1 is inoperative. GMA1 CONFIG – GMA1 config error. Config service req’d. MANIFEST – GMA1 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. The audio panel configuration settings do not match backup configuration memory.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments MANIFEST – GIA1 software mismatch, communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch, be serviced. communication halted. COM1 TEMP – COM1 over temp. The system has detected an over temperature condition in COM1 and/or COM2. The Reducing transmitter power. transmitter is operating at reduced power.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments ABORT APR – Loss of GPS navigation. Abort approach due to loss of GPS navigation. Abort approach. TRUE APR – True north approach. Displayed after passing the first waypoint of a true north approach when the nav Change hdg reference to TRUE. angle is set to ‘AUTO’. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories Message GIA1 CONFIG – GIA1 configuration error. Config service req’d. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced. GDL 69A Message Advisories Message GDL69 CONFIG – GDL 69 config error.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Parallel track unavailable: bad geometry PTK FAIL – Parallel track unavailable: invalid leg type. PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. VNV – Unavailable. Unsupported leg type in flight plan. VNV – Unavailable. Excessive crosstrack error.
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-6, 1-7, 5-3 ADS-B RR-1, 10-7, 10-9, 12-6 AFCS 12-4 Age 10-6 AHRS 12-19, 12-20 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-25 Airport information 7-21 Airspace alerts 7-29 Airspeed indicator 2-3 Airspeed Reference 6-8 Airspeed trend vector 2-3 Airways 8-5 Alerting system 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-15 ALT 1-4, 1-7, 2-4, 6-4, 6-6, 6-13, 7-19, 10-8 Altitude alerting 2-4 Altitude constraints
INDEX Forward Looking Terrain Avoidance 10-13 Freezing level 10-5 Frequency toggle key 1-3, 4-3 Fuel Calculations 3-7 Flow totalizer 3-7 Remaining 3-8 Used 3-8 Fuel Flow 3-1, 3-3, 3-4, 3-8 Fuel Quantity 3-2, 3-4, 3-8 N Key(s) 1-4 Nav/Com controls 4-1 NAV1 5-3 NAV2 5-3 Navigation 7-1 Navigation database 1-10, 1-11, 7-5 Navigation Mode 6-19–6-20, 6-26–627 Navigation status window 2-2 NAV frequency window 4-1 NCR 10-14 Nearest Airports Page 7-21, 7-25 – 729, 8-1 Nearest ARTCC & FSS frequencies 7-28 Negative
INDEX R T Red pointer 2-3 Remove departure, arrival, or approach 8-6 Replies 4-5 Required Vertical Speed 2-6, 7-15 Required Vertical Speed Indicator 7-15 Reversionary mode 5-1, 11-1 ROC 10-13, 10-16, 12-5 Roll Hold Mode (ROL) 6-17 Roll modes, flight director 6-17–6-20 Roll Reference 6-18 RTC 10-13 RVSI 7-15, 7-16 RX indicator 4-3 R indication 4-5 TA 10-7 Tachometer 3-1, 3-4, 3-8 TAF 10-3 TAS 10-7, 10-8, 10-9, 12-19 TAWS 10-11 – 10-13, 10-15 – 10-17, 12-5, 12-6 TAWS-B 10-11 TAWS system test 10-13 Temperatu
INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-08 Rev.
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