Integrated Flight Deck Cockpit Reference Guide Cessna Nav III
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATIONS ANNUNCIATIONS & ALERTS INDEX
COPYRIGHT Copyright © 2004-2011 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0563.25 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.
COPYRIGHT AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance 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 avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources.
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 PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. CAUTION: The Garmin G1000 does not contain any user-serviceable parts.
WARNINGS, CAUTIONS, & NOTES Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
RECORD OF REVISIONS Part Number 190-00384-03 (Rev. A) Change Summary Added XM Radio and XM Weather Added ADF capability Added DME capability Added BRG1/BRG2 pointers Added dual audio panel operation Added C172 parameters Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Added Flight ID capability (Rev. B) 190-00384-04 (Rev. A) Updated system software numbers (Rev. B) 190-00384-05 (Rev. A) Added DONE Softkey, XM-INFORMATION Page, and XM-RADIO Page operation.
RECORD OF REVISIONS Part Number 190-00384-07 (Rev. A) 190-00384-08 (Rev. A) 190-00384-09 (Rev. A) 190-00384-10 190-00384-11 190-00384-12 Change Summary Added GDU 8.02 parameters, Airways, and ADS-B Added GDU 8.20 parameters, including gradient background on the PFD and GFC 700 for the C172. Added GDU 9.03 parameters. Removed gradient background. Added Additional Features section Changed tab structure Added GDU 9.
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........................................................... 1-9 MFD Page Groups.................................................. 1-10 Vertical Navigation............................................... 1-11 Arrival Alerts.........
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 Activate An Approach in the Active Flight Plan.............. 9-4 Activate A Missed Approach in the Active Flight Plan..... 9-4 SECTION 10: HAZARD AVOIDANCE............................ 10-1 10.1 Customizing the Hazard Displays on the Navigation Map........................................ 10-1 10.2 STORMSCOPE® (Optional)................................... 10-1 Displaying Stormscope Lightning Data on the Navigation Map Page.................................................
TABLE OF CONTENTS 11.3 ChartView (Optional).......................................... 11-11 Chart Options.......................................................... 11-12 Day/Night View........................................................ 11-13 11.4 FliteCharts............................................................. 11-14 Chart Options.......................................................... 11-15 Day/Night View........................................................ 11-15 11.
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 (19000498-07). 190-00384-12 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 190-00384-12 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 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 PRECIP or DL LTNG or METAR STRMSCP WX LGND TRFC-1 ALERTS Press the BACK Softkey to return to the top-level softkeys. TRFC-2 Figure 1-2 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.
SECTION 1 SYSTEM OVERVIEW STRMSCP (optional) – Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD/PRECIP(optional) – Press to display NEXRAD weather and coverage information on the Inset Map or FIS-B/GFDS precipitation disabling Synthetic Vision features. PATHWAY – Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan. SYN TERR – Enables synthetic terrain depiction.
SECTION 1 SYSTEM OVERVIEW OPTN 3 – Wind direction arrow with direction and speed. OFF – Information not displayed. DME (optional) – Press to display the DME Information Window. BRG1 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the appropriate information. NAV1 – Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window.
SECTION 1 SYSTEM OVERVIEW XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select Standby Mode. ON – Press to select Mode A. ALT – Press to select Altitude Reporting Mode. GND – Press to select Ground Mode. VFR – Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries). CODE – Press to display transponder code selection softkeys 0-7.
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW METAR – Pressing this softkey displays METAR flags on airport symbols on the Navigation flag. LEGEND – Pressing this softkey displays the Legend BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys. DCLTR (declutter) – Pressing this softkey removes map information in three levels. SHW CHRT (Show Chart)(optional) – Pressing this softkey displays optional FliteCharts or ChartView charts.
SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION One of two altitude sources is used by the G1000 when giving vertical navigation guidance. SBAS GPS altitude is used when giving guidance for an SBAS approach after the Final Approach Fix. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-SBAS 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 ARRIVAL ALERTS The Arrival Alert Box on the System Setup Page allows the Alerts Window arrival alert to be turned ON/OFF. The alert trigger distance (up to 99.9 units) may also be set for alerts in the Alerts Window and the PFD Navigation Status Box. An arrival alert can be set to notify the pilot with a message upon reaching a user-specified distance from the final destination (the direct-to waypoint or the last waypoint in a flight plan).
SECTION 1 SYSTEM OVERVIEW 1.8 LOADING UPDATED DATABASES CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system. NOTE: When loading database updates, the ‘DB Mismatch’ message will be displayed until database synchronization is complete, followed by turning system power off, then on. Synchronization can be monitored on the AUX-SYSTEM STATUS Page.
SECTION 1 SYSTEM OVERVIEW 12) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1 DB). Verify the correct database cycle information is shown for each database for each display.
SECTION 1 SYSTEM OVERVIEW 9) Turn the large FMS Knob to select the AUX Page group on the MFD. 10) Turn the small FMS Knob to select the System Status Page. 11) The new database is copied to the SD card in the bottom card slot of each PFD. Progress can be monitored in the SYNC STATUS field. When copying is finished, ‘Complete’ is displayed. NOTE: During the synchronization process, version differences between standby navigation databases will exist.
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 (SBAS enabled systems only)/Glideslope Indicator 15 Marker Beacon Annunciation
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 Metric Display Low Altitude Annunciation 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 SBAS 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 Set the barometric altitude minimums: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the ‘Minimums’ field (Figure 2-16). 3) Turn the small FMS Knob to select BARO.
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 190-00384-12 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182T only). 2 NOTE: Refer to the Pilot’s Operating Handbook (POH) for limitations. EIS information is presented in three displays, accessed using the ENGINE Softkey on the MFD.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 2 2 1 1 3 3 2 2 4 4 5 5 3 3 4 4 5 5 6 6 7 7 10 10 7 7 9 9 10 10 11 11 12 12 12 12 13 13 13 13 Model 172R Model 172S Model 182T Model 206H Figure 3-1 Engine Display (Normally-aspirated Aircraft) 7 8 3-2 Exhaust Gas Temperature Indicator (EGT) Normally-aspirated Aircraft – Displays the exhaust gas temperature of the hottest cylinder (number shown in triangular pointer) in degrees Fahrenheit (°F).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 11 Engine Hours (Tach) (ENG HRS) Models 172R and 172S – A numeric readout gives the time (in hours) the engine has been in service. 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) 3.2 LEAN DISPLAY 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) 1 2 2 1 2 2 Blue Block Represents Peak 5 5 3 3 5 6 6 3 3 7 7 5 6 Model 172R 6 7 Model 172S 7 Model 182T Model 206H Figure 3-3 Lean Display (Normally-aspirated Aircraft) 190-00384-12 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) 2 2 3 3 4 4 7 7 8 8 9 9 10 10 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 11 11 11 11 12 12 12 12 Model 172R Model 172S Model 182T Model 206H Figure 3-5 System Display (Normally-aspirated Aircraft) 3-8 4 Oil Temperature (OIL °F) – Displays the engine oil temperature in degrees Fahrenheit (°F). 7 Fuel Flow (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph).
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 T206H Model T182T Figure 3-6 System Display (Turbocharged Aircraft) 9 Set Fuel Remaining (GAL REM) – Shows current fuel remaining in gallons as set by the pilot and adjusted for fuel burn since last set.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Blank Page 3-10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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) 190-00384-12 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Selected COM 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 ADF Radio (optional) 4.7 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. Mode Selection 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD TRANSPONDER 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 Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
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 190-00384-12 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 PLAY Key once plays the latest recorded memory block, then returns to normal operation. • Pressing the MKR/MUTE Key while playing a memory block stops play.
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 Speed Reference Selected Altitude Capture Mode Armed Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Reference 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 pressin
SECTION 6 – AUTOMATIC FLIGHT CONTROL Airspeed Reference and the desired flight profile (climb or 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) appears on the PFD 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 Non-Path Descents Pitch Hold, Vertical Speed, and Flight Level Change modes can also be used to fly non-path descents while 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 re-capture.
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.
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) 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) Intercepting and Flying a DME Arc The AFCS will intercept and track a DME arc that is part of the active flight plan provided that GPS Navigation Mode is engaged, GPS is the active navigation source on the CDI, and the DME arc segment is the active flight plan leg.
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 Departure Climbing to the Selected Altitude and flying an assigned heading: NOTE: The following example flight plan and diagrams (not to be used for navigation) in this section are for instructional purposes only and should be considered not current. Numbered portions of accompanying diagrams correspond to numbered procedure steps. 1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 4) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4. Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading.
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 NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level). As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is currently tracking inbound on Airway V4. Flying a GPS flight plan: 1) Transition from VOR to GPS Navigation Mode: a) Press the CDI Softkey until GPS is the selected navigation source.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Descent b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed automatically. While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV Target Altitude: • Turn the ALT Knob to adjust the Selected Altitude 1) Select VNV flight control: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. • Press the VNV Key If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Non-path descent using Flight Level Change Mode: 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. b) Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed. The Airspeed Reference defaults to the current aircraft airspeed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach 3) There are two options available at this point, as the autopilot flies the ILS approach: NOTE: If an approach contains a DME arc, the arc must be flown in Navigation Mode with the GFC 700. When receiving vectors from ATC, Navigation Mode must be selected prior to intercepting the ARC. Flying an ILS approach: • Push the AP DISC Switch at the decision height and land the aircraft. • Use the GA Switch to execute a missed approach.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a RNAV GPS approach with vertical guidance: 2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and Glidepath Mode is armed. 3) Once the glidepath is captured, Glidepath Mode becomes active. The flight director now provides guidance to the missed approach point.
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 go around 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 190-00384-12 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. Figure 7-11 Assigned Heading of 240º 7-6 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 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
SECTION 7 – NAVIGATION 4) Enter V4 into the flight plan. a) Press the FMS Knob to activate the cursor. b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point (SLN) as shown in Figure 7-13. When the V4 entry point (TOP) is inserted, it is placed immediately above the highlighted waypoint (SLN) as indicated by the insertion point indicator (small blue triangle).
SECTION 7 – NAVIGATION d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 7-15. f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. Figure 7-15 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 7-15, turn the small FMS Knob clockwise. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available.
SECTION 7 – NAVIGATION h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 7-17. j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in Figure 7-18. Figure 7-17 List of Available Exits for V4 Figure 7-18 Ready to Load V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in Figure 7-17. 190-00384-12 Rev. A k) Press the ENT Key.
SECTION 7 – NAVIGATION l) V4 is now loaded into the flight plan as shown in Figure 7-19. d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 7-21, the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active.
SECTION 7 – NAVIGATION 6) The aircraft continues on heading 290º. When crosstrack distance is less than 2.0 nm, the XTK disappears from the HSI and the CDI is positioned on the last dot indicating a 2.0 nm distance from the centerline of the next course. 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.
SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 7-25. 11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises to expect an altitude of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to select OPSHN in the flight plan list. c) Press the Direct-to ( ) Key. The Direct-to Window is now displayed as shown in Figure 7-26.
SECTION 7 – NAVIGATION d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7-27. Figure 7-27 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by ATC. 190-00384-12 Rev. A f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. Figure 7-28 Enter VNV Offset Distance g) Enter the offset, or distance from the waypoint at which to reach the selected altitude.
SECTION 7 – NAVIGATION h) Press the ENT Key twice to activate the directto. Note, in Figure 7-29, the magenta arrow indicating the direct-to OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset distance and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure have no database specified altitudes, therefore, dashes are displayed. Keep the CDI centered and maintain a track along the magenta line to OPSHN.
SECTION 7 – NAVIGATION c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 7-31. Figure 7-31 List of Available Approaches 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 in Figure 7-32. Figure 7-32 List of Available Transitions f) Turn either FMS Knob to select the desired transition.
SECTION 7 – NAVIGATION h) Barometric Minimums To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key. i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-34. Or: To skip setting minimums, press the ENT Key.
SECTION 7 – NAVIGATION 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 7-35. Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the SBAS GPS altitude source, therefore, the displayed altitude values are for reference only.
SECTION 7 – NAVIGATION 15) As seen in Figure 7-37, the aircraft is approaching TOD. Note the target vertical speed required to reach the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are now displayed on the PFD as shown in Figure 7-38. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 7-38, and an aural alert ‘Vertical track’ will be heard.
SECTION 7 – NAVIGATION 17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 7-40. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet. 18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 7-41. 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 7-42. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-42 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 7-43).
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 7-44). 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 7-47) when the final approach course becomes active.
SECTION 7 – NAVIGATION In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded. This altitude is provided by Jeppesen, and may be below, equal to, or above the published minimums for this approach.
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 7-50. 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 7-51. Figure 7-51 Hold Established Figure 7-50 Establishing the Holding Pattern 7-24 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
SECTION 7 – NAVIGATION 7.4 AIRPORT INFORMATION 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. 4) To remove the flashing cursor, press the FMS Knob.
SECTION 7 – NAVIGATION Display AOPA Airport Directory Information With the Airport Information Page displayed, press the INFO softkey until INFO-2 is displayed. The Airport Directory Page is now displayed. 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 7-54.
SECTION 7 – NAVIGATION Select a Recently Entered Airport Identifier 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-54. The list is populated only when navigating a flight plan. 7.5 INTERSECTION INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-58 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 NDB INFORMATION. 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). 3) Enter an identifier, name or city and press the ENT Key.
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 7-61 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 7-64 Nearest VOR Page Figure 7-63 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 NEAREST NDB. 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. The remaining information on the Nearest NDB Page pertains to the selected 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 7-65 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. 4) Press the FMS Knob to remove the flashing cursor. 7.15 NEAREST AIRSPACES • If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside, ‘Within 2 nm’ is displayed. • If the aircraft has entered an airspace, ‘Inside’ is displayed.
SECTION 7 – NAVIGATION Blank Page 7-34 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 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 (deleted automatically when the system is turned off). If the waypoint is to remain in the system, proceed to step 7. a) Turn the large FMS Knob one click to the left to highlight ‘TEMPORARY’. b) Press the ENT Key to place a check-mark in the box. Turn the large FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
SECTION 8 – FLIGHT PLANNING 6) Turn the small FMS Knob to select RAD/RAD (radial/ radial). c) Turn the large FMS Knob to select the desired waypoint. 7) Press the ENT Key. d) Press the ENT Key. 8) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name.
SECTION 8 – FLIGHT PLANNING 6) Turn the small FMS Knob to select RAD/DIS (radial/ distance). c) Turn the large FMS Knob to select the desired waypoint. 7) Press the ENT Key. d) Press the ENT Key. 8) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first waypoint name highlighted, use the FMS Knobs to enter the desired waypoint name.
SECTION 8 – FLIGHT PLANNING 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. 9) Press the GO BACK Softkey to return to the map page. Delete a User Waypoint 1) With the User Defined Waypoint Page displayed , press the FMS Knob to activate the cursor.
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 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. NOTE: After the first leg is entered (using the PFD only), it is immediately activated. 1) Press the FPL Key, then press the FMS Knob to activate the cursor. Figure 8-10 Create FPL on MFD 3) Turn the small FMS Knob to display the Waypoint Information Window. 2) Turn the small FMS Knob to enter the first letter of the destination waypoint identifier.
SECTION 8 – FLIGHT PLANNING 5) Turn either FMS Knob to highlight an empty or existing flight plan. 6) Press the IMPORT Softkey; or press the MENU Key, select “Import Flight Plan”, and press the ENT Key. If an empty slot is selected, a list of the available flight plans on the SD card will be displayed. Or: If an existing flight plan is selected, an “Overwrite existing flight plan? OK or CANCEL” prompt is displayed.
SECTION 8 – FLIGHT PLANNING Figure 8-16 Load Airway Entry Point 5) When the desired entry point is entered, press the ENT Key. Figure 8-18 Enter Airway Identifier 7) When the desired airway is entered, press the LD AIRWY Softkey. 8) Turn either FMS Knob to scroll through the list of available exit points. Figure 8-17 Airway Entry Point Loaded 6) Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired airway identifier.
SECTION 8 – FLIGHT PLANNING 8.14 STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. Figure 8-20 Airway Added to Flight Plan 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. 8.10 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8.
SECTION 8 – FLIGHT PLANNING 3) Press the CLR Key to display a ‘REMOVE (Wpt Name)’ confirmation window. Figure 8-22 Remove Waypoint Confirmation 4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 5) Once all changes have been made, press the FMS Knob to remove the cursor. 8.
SECTION 8 – FLIGHT PLANNING 5) After placing the cursor at the desired point in the list of waypoints, press the LD WPT Softkey. 6) To change the user waypoint name, follow the procedure for modifying a user waypoint. 8.21 TRIP PLANNING 1) Turn the large FMS Knob to select the ‘AUX’ page group. 2) Turn the small FMS Knob to select TRIP PLANNING. 3) The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey.
SECTION 8 – FLIGHT PLANNING 7) Turn the FMS Knobs to enter the fuel flow. Press the ENT Key when finished. Note that in automatic page mode, fuel flow is provided by the system. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the EXPORT Softkey. 8) The flashing cursor moves to the fuel on board field. Turn the FMS Knobs to modify the fuel on board. Press the ENT Key when finished.
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 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. Figure 9-4 Select Arrival Transition 8) A third window is displayed listing the available runways. Turn either FMS Knob to select the desired runway and press the ENT Key. Figure 9-5 Select Arrival Runway 9) With ‘LOAD?’ highlighted, 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. 5) Turn the large FMS Knob to highlight the Approach field.
SECTION 9 – PROCEDURES 9) The cursor moves to the altitude field. Turn the small FMS Knob to enter the published decision altitude for the selected approach procedure. Press the ENT Key. Activate A Missed Approach in the Active Flight Plan 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A confirmation window is displayed. 4) With ‘ACTIVATE’ highlighted, press the ENT Key. Or: Press the GA switch.
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. Select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1) With the Weather Group selected, press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’. 2) Turn the large FMS Knob to select ‘STRMSCP MODE’. 3) Turn the small FMS Knob to display the ‘Cell/Strike’ window. 4) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE 10.3 XM WEATHER (SERVICE OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 2) Turn the small FMS Knob to select AIRPORT INFORMATION. 3) Press the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). 1) From the Navigation Map Page, press the MAP Softkey.
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 WEATHER DATA LINK. 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. Press the small FMS Knob or the ENT Key to return to the map.
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 Enabling/disabling winds aloft data display in Profile View: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key 4) Turn the small FMS Knob to select the Profile Group and press the ENT Key 5) Turn the large FMS Knob to select ‘Profile Winds’. 6) Turn the small FMS Knob to select ‘On’ or ‘Off’. 7) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
SECTION 10 – HAZARD AVOIDANCE Wx Product Status Icons Description ICING POTENTIAL - The age of the displayed data is shown at the right. The altitude selection is shown at the bottom. No Status Icon TFR- Depicted as an area outlined in yellow Table 10-2 NOTE: The LOCK Softkey on the AUX - XM INFORMATION Page is used to save the GDL 69(A) activation data when the XM services are initially set up.
SECTION 10 – HAZARD AVOIDANCE FIS-B Weather Data Link Page, a box containing a symbol for the product and its age (in minutes) is shown in the upper right. If weather data has not been received yet, ‘N/A’ is shown next to the product symbol instead of age. The age of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time.
SECTION 10 – HAZARD AVOIDANCE 2) Turn the small FMS Knob to select the desired Weather Data Link Page. 3) Press the MENU Key. 4) Turn the large FMS Knob to select ‘Display GFDS Weather’ or ‘Display XM’ Weather’ or ‘Display FIS-B Weather’ (choice dependent on current weather source) and press the ENT Key. Viewing Legends for Displayed FIS-B Weather Products 1) Select the FIS-B Weather Data Link Page. 2) Select the LEGEND Softkey to display the legends for the displayed weather products.
SECTION 10 – HAZARD AVOIDANCE 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 10-11 Navigation Map Page Menu Figure 10-13 Navigation Map Page Setup Menu, Weather Group Figure 10-12 Navigation Map Page Setup Menu FIS-B Weather Products Precipitation Precipitation data is not real-time. The lapsed time between collection, processing, and dissemination of radar images can be significant and may not reflect the current radar synopsis.
SECTION 10 – HAZARD AVOIDANCE 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text. 5) Press the FMS Knob or the CLR Key to return to the FIS-B Weather Data Link Page.
SECTION 10 – HAZARD AVOIDANCE Airport Selected with Map Pointer Instructions for Viewing METAR and TAF Text 10.5 WORLDWIDE WEATHER (OPTIONAL) NOTE: Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather. Do not utilize Worldwide Weather information to penetrate hazardous weather. Weather data is provided when the pilot initiates either a manual or automatic GFDS data request on the GFDS Weather Data Link Page on the MFD.
SECTION 10 – HAZARD AVOIDANCE 5) Press the MENU Key. If necessary, select ‘Display GFDS Weather’. 6) Press ENT Key. The ‘GARMIN FLIGHT DATA SERVICE REGISTRATION’ Window is now displayed. 7) Press the MENU Key. The Page Menu window is now displayed. 8) Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field. 9) Press the ENT Key. REGISTER will now be highlighted. 10) Press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE Weather Product Symbol Expiration Refresh Rate Time (Minutes) (Minutes) Pilot Weather Report 90 Continuous (PIREPs) Temporary Flight no Restrictions product 60 Continuous (TFRs) image Terminal no Aerodrome product 60 Continuous Reports image (TAFs) * The composite precipitation image is updated every 3 minutes, but individual radar sites may take between 3 and 10 minutes to provide new data.
SECTION 10 – HAZARD AVOIDANCE 4) Press the MENU Key. 5) Highlight the desired default(s) to restore (all or for selection) and press ENT Key. Viewing Legends for Displayed GFDS Weather Products 1) Select the GFDS Weather Data Link Page. 2) Select the LEGEND Softkey to display the legends for the displayed weather products. Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT Key. 3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window.
SECTION 10 – HAZARD AVOIDANCE GFDS Weather Data Requests The GFDS Data Request window provides the flight crew with the options to define the requested weather coverage area(s), choose automatic weather update intervals (if desired), and the ability to send or cancel weather data requests. The window also displays the status of the GFDS data request process. 6) Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted.
SECTION 10 – HAZARD AVOIDANCE Next 80 nm of Flight Plan Selected, 200 nm Route Width Requested Present Position Selected, 200 nm Diameter Requested Figure 10-24 Present Position Data Request Figure 10-26 Route Data Request Off-Route Waypoint Selected, 200 nm Diameter Requested Destination Selected, 200 nm Diameter Requested Figure10-27 Off-Route Data Request Figure 10-25 Destination Data Request 190-00384-12 Rev.
SECTION 10 – HAZARD AVOIDANCE data request is processing by pressing the FMS Knob; the data request will continue to process in the background. GFDS Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength. The system retrieves all available Worldwide Weather products within the selected coverage area during an initial GFDS Data Request, regardless of which products (if any) are currently enabled for display.
SECTION 10 – HAZARD AVOIDANCE Weather Request Status Message Description Request Failed - Try The weather data request timed-out. Again Re-send data request. Invalid Coverage Area The weather data request coverage area does not contain at least one of the following: a waypoint, a flight plan, or a flight plan destination. Verify at least one of the coverage options is enabled (checked) and contains required criteria, then resend the data request.
SECTION 10 – HAZARD AVOIDANCE NOTE: Precipitation data cannot be displayed on the Navigation Map Page at the same time as terrain. Displaying Precipitation Weather Information No Radar Coverage 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the GFDS Weather Data Link Page. Boundary of GFDS weather data request 2) Select the PRECIP Softkey. Radar data shown represents lowest level, base reflectivity, of radar returns.
SECTION 10 – HAZARD AVOIDANCE Displaying SIGMETs and AIRMETs Infrared Satellite Infrared Satellite (IR SAT) data depicts cloud top temperatures from satellite imagery. Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes. 1) Select the GFDS Weather Data Link Page. 2) Select the SIG/AIR Softkey. Displaying Cloud Tops information 3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon.
SECTION 10 – HAZARD AVOIDANCE 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Select the WX Softkey to select the Weather Information Page. 2) Press the FMS Knob to display the cursor. 3) Use the FMS Knob to enter the desired airport and press the ENT Key. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note that the METAR text must be completely scrolled through before scrolling through the TAF text.
SECTION 10 – HAZARD AVOIDANCE 10.6 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. the traffic display (up to 60 seconds) until the next data reception. If no data is received after 60 seconds, traffic is removed from the display.
SECTION 10 – HAZARD AVOIDANCE Traffic Advisory Systems (Optional) Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. GTS 800 Traffic System (Optional) Testing the Traffic System: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Turn the Range knob to set the range to 2/6 nm to allow for proper test pattern display. 4) Press the TEST Softkey.
SECTION 10 – HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1) Ensure TIS is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Traffic is now displayed on the map. Switching from operating mode to standby mode: On the Traffic Page, press the STANDBY Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Standby Mode’. 2) Press the ENT Key.
SECTION 10 – HAZARD AVOIDANCE KTA 870 Traffic System (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 Traffic Advisory Symbol Description Non-threat traffic with no directional information. (GDL 90 and GTS 800) Traffic located on the ground with directional information. Points in the direction of the aircraft track. Ground traffic is only displayed when own aircraft is below 1,000 feet AGL or on the ground. (GDL 90 only) Ground traffic without directional information. Ground traffic is only displayed when own aircraft is below 1,000 feet AGL or on the ground.
SECTION 10 – HAZARD AVOIDANCE 10.7 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area. Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the ‘MAP’ page group. Displaying Terrain and Obstacles on the Navigation Map 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.
SECTION 10 – HAZARD AVOIDANCE 10.8 TERRAIN-SVS DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area. NOTE: TERRAIN-SVS operation is only available when the Synthetic Vision System is installed. TAWS will take precedence over TERRAIN-SVS when installed. Displaying Terrain on the TERRAIN-SVS Page 1) Turn the large FMS Knob to select the ‘MAP’ page group. 2) Turn the small FMS Knob to select the TERRAIN-SVS Page.
SECTION 10 – HAZARD AVOIDANCE Figure 10-41 Terrain-Color Code Enable/Disable Aviation Data 1) While the TERRAIN-SVS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”. 3) Press the ENT Key. Figure 10-42 Terrain-SVS Page Menu TERRAIN-SVS Alerts Alerts are issued when flight conditions meet parameters that are set within TERRAIN-SVS software algorithms. TERRAIN-SVS alerts typically employ a CAUTION or a WARNING alert severity level, or both.
SECTION 10 – HAZARD AVOIDANCE PFD/MFD Alert Annunciation Alert Type MFD Pop-Up Alert Aural Message Reduced Required Terrain Clearance Warning (RTC) “Warning; Terrain, Terrain” Imminent Terrain Impact Warning (ITI) “Warning; Terrain, Terrain” Reduced Required Obstacle Clearance Warning (ROC) “Warning; Obstacle, Obstacle” Imminent Obstacle Impact Warning (IOI) “Warning; Obstacle, Obstacle” Reduced Required Terrain Clearance Caution (RTC) “Caution; Terrain, Terrain” Imminent Terrain Impact Cautio
SECTION 10 – HAZARD AVOIDANCE Alert Annunciation Pop-up Alert Figure 10-43 TERRAIN-SVS Alert Annunciations Terrain Display Enabled Terrain Legend Alert Annunciation Figure 10-44 Navigation Map Page (After TERRAIN-SVS Pop-up Alert Acknowledgment) 10-32 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
SECTION 10 – HAZARD AVOIDANCE Terrain Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. Inhibit TERRAIN-SVS: While the TERRAIN-SVS Page is displayed, press the INHIBIT Softkey. ‘TER INHB’ is annunciated in the lower right of portion of the screen. Enable TERRAIN-SVS: If TERRAIN-SVS has been inhibited, from the TERRAIN-SVS Page press the INHIBIT Softkey. The ‘TER INHB” annunciation is removed.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1) With the Navigation Map displayed, press the MAP Softkey. 2) Press the TERRAIN Softkey. Terrain and obstacle proximity are now displayed on the map. 3) Terrain and obstacles may be displayed in the Profile View by selecting the PROFILE Softkey. 10.
SECTION 10 – HAZARD AVOIDANCE Figure 10-49 TAWS-B Page Menu TAWS Inhibit Figure 10-47 TAWS-B 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-B Page is displayed, press the INHIBIT Softkey. ‘TAWS INHB’ is annunciated in the lower right of portion of the screen.
SECTION 10 – HAZARD AVOIDANCE 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-B Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS’. 3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS-B Page. When all is in working order, “TAWS System Test, OK” is heard.
SECTION 10 – HAZARD AVOIDANCE “Five-Hundred” Aural Alert Pop-up Alerts The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the air crew that the aircraft is five-hundred feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Five-hundred” is heard. There are no display annunciations or pop-up alerts that accompany the aural message.
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 Alert Annunciation Alert Type TERRAIN-SVS Page Annunciation Aural Message TAWS TEST None None “TAWS System Test OK” None None System Test in Progress System Test Pass None TAWS Alerting is disabled MFD Terrain or Obstacle database unavailable or invalid.
SECTION 10 – HAZARD AVOIDANCE Blank Page 10-40 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
SECTION 11 – ADDITIONAL FEATURES SECTION 11: ADDITIONAL FEATURES 11.1 SYNTHETIC VISION SYSTEM (SVS) (OPTIONAL) WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
SECTION 11 – ADDITIONAL FEATURES HRZN HDG, APTSIGNS, and PATHWAY Softkeys are only available when the SYN TERR Softkey is activated (gray with black characters). After activating the SYN TERR Softkey, the HRZN HDG, APTSIGNS, and PATHWAY softkeys may be activated in any combination to display desired features. When system power is cycled, the last selected state (on or off) of the SYN TERR, HRZN HDG, APTSIGNS, and PATHWAY softkeys is remembered by the system.
SECTION 11 – ADDITIONAL FEATURES which the pathway boxes are displayed is determined by the selected altitude during climb, cruise, and when the active leg is the final approach course prior to intercepting the glidepath/glideslope. During a descent (except while on the approach glidepath/glideslope), the pathway boxes are displayed at the selected altitude, or the VNAV altitude programmed for the active leg in the flight plan, or the published altitude constraint, whichever is higher (Figure 11-3).
SECTION 11 – ADDITIONAL FEATURES Descent and Approach Pathways are shown descending only for a programmed descent (Figures 11-4 and 11-5). When the flight plan includes programmed descent segments, pathways are displayed along the descent path provided that the selected altitude is lower than the programmed altitude. During a Vectors-to-Final (VTF) approach transition, pathways are displayed along the final approach course inbound to the Missed Approach Point (MAP).
SECTION 11 – ADDITIONAL FEATURES Missed Approach Pathways are displayed along each segment including the path required to track course reversals that are part of a procedure, such as holding patterns. Pathways boxes will not indicate a turn to a MAHP unless a defined geographical waypoint exists between the MAP and MAHP.
SECTION 11 – ADDITIONAL FEATURES Zero Pitch Line Flight Path Marker The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed and direction relative to the three-dimensional terrain display. The FPM is always available when the Synthetic Terrain feature is in operation.
SECTION 11 – ADDITIONAL FEATURES Airport Signs Airport Signs provide a visual representation of airport location and identification on the synthetic terrain display. When activated, the signs appear on the display when the aircraft is approximately 15 nm from an airport and disappear at approximately 4.5 nm. Airport signs are shown without the identifier until the aircraft is approximately eight nautical miles from the airport. Airport signs are not shown behind the airspeed or altitude display.
SECTION 11 – ADDITIONAL FEATURES Terrain-SVS and TAWS Alerting Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA) alerts, and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays. For more detailed information regarding Terrain-SVS and TAWS, refer to the Hazard Avoidance Section. In some instances, a terrain or obstacle alert may be issued with no conflict shading displayed on the synthetic terrain.
SECTION 11 – ADDITIONAL FEATURES Field of View Two dashed lines forming a V‑shape in front of the aircraft symbol on the MFD map, represent the forward viewing area shown on the PFD. 2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key. 3) Turn the FMS Knob to select the Map Group and press the ENT Key.
SECTION 11 – ADDITIONAL FEATURES 11.2 SAFETAXI Configuring SafeTaxi range: When viewing at ranges close enough to show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges.
SECTION 11 – ADDITIONAL FEATURES 11.3 CHARTVIEW (OPTIONAL) The optional ChartView feature resembles the paper version of Jeppesen terminal procedures charts. The MFD depiction shows the aircraft position on the moving map in the plan view of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta. ChartView functions are displayed on three levels of softkeys.
SECTION 11 – ADDITIONAL FEATURES If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, pressing the SHW CHRT Softkey displays the chart for the nearest airport, if available. When no terminal procedure chart is available for the nearest airport or the selected airport, the banner CHART NOT AVAILABLE appears on the screen.
SECTION 11 – ADDITIONAL FEATURES Pressing the PROFILE Softkey displays the approach chart descent profile strip. If the chart scale has been adjusted to view a small area of the chart, pressing the FIT WIDTH Softkey changes the chart size to fit the available screen width. Day/Night View ChartView can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment.
SECTION 11 – ADDITIONAL FEATURES 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. 5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to change the percentage value. The percentage value is the day/night crossover point based on the percentage of backlighting intensity. For example, if the value is set to 15%, the day/ night display changes when the display backlight reaches 15% of full brightness.
SECTION 11 – ADDITIONAL FEATURES NOTAMs are not available with FliteCharts. The NOTAM Softkey label appears subdued and is disabled. When no terminal procedure chart is available, the banner CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the FliteCharts subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport.
SECTION 11 – ADDITIONAL FEATURES 11.6 XM RADIO ENTERTAINMENT (SERVICE OPTIONAL) NOTE: Refer to the Hazard Avoidance Section for information about XM Weather products. The optional XM Radio entertainment feature is available for the pilot’s and passengers’ enjoyment throughout the Continental U.S. Using XM Radio The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio.
SECTION 11 – ADDITIONAL FEATURES Category Presets The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other contents. One of the optional categories is PRESETS to view channels that have been programmed. Selecting a category: 1) Press the CATGRY Softkey on the XM Radio Page. 2) Press the CAT + and CAT - Softkeys to cycle through the categories.
SECTION 11 – ADDITIONAL FEATURES Volume Radio volume is shown as a percentage. Volume level is controlled by pressing the VOL Softkey, which brings up the MUTE Softkey and the volume increase and decrease softkeys. Adjusting the volume: 1) With the XM Radio Page displayed, press the VOL Softkey. 2) Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL Softkey is pressed, the volume can also be adjusted using the small FMS Knob.
SECTION 11 – ADDITIONAL FEATURES 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. 8) For periodic and one-time message, use the FMS Knob to enter the timer value (HH:MM:SS) from which to countdown and press the ENT Key. 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
SECTION 11 – ADDITIONAL FEATURES 11.8 ELECTRONIC CHECKLISTS Accessing and navigating checklists: NOTE: The checklists presented here are for example only and may not reflect checklists actually available for the Cessna NAV III Aircraft. This material is not intended to replace the checklist information presented in the AFM or the Pilot Safety and Warning Supplements document. NOTE: Garmin is not responsible for the content of checklists.
SECTION 11 – ADDITIONAL FEATURES 7) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window. If all items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’ will be displayed in yellow text.\ 8) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor. 9) Press the ENT Key to advance to the next checklist. 10) Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
SECTION 11 – ADDITIONAL FEATURES Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. 7) Press the ENT Key to advance to the next checklist. Press the CLR Key or UNCHECK Softkey to remove a check mark from an item. 8) Press the RETURN Softkey to return to the previous checklist. 5) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window.
SECTION 11 – ADDITIONAL FEATURES 11.9 FLIGHT DATA LOGGING NOTE: Some aircraft installations may not provide all aircraft/engine data capable of being logged by the system. The Flight Data Logging feature will automatically store critical flight and engine data on an SD data card (up to 8GB) inserted into the top card slot of the MFD. Approximately 1,000 flight hours can be recorded for each 1GB of available space on the card.
SECTION 11 – ADDITIONAL FEATURES The .csv file may be viewed with Microsoft Excel® or other spreadsheet applications. The file containing the recorded data will appear in the format shown in Figure 11-33. This file can be imported into most computer spreadsheet applications. Local Date YYMMDD Local 24hr Time HHMMSS Nearest Airport (A blank will be inserted if no airport is found) 11.
SECTION 11 – ADDITIONAL FEATURES ENGINE MAP INPUT SETUP VID ZM+ VID ZM- MAP ACTV HIDE MAP VID ACTV CNTRST - CNTRST + BRIGHT - BRIGHT + SAT - RESET SAT + BACK Pressing the BACK Softkey returns to the Previous Level Softkeys. Figure 11-36 Video Display Softkeys Selecting video menu options: 1) While viewing the AUX - VIDEO Page press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key.
SECTION 11 – ADDITIONAL FEATURES Zoom/Range Figure 11-37 AUX - Video Split-Screen Pressing the VID ZM + or VID ZM - Softkeys increases or decreases video display magnification between 1x and 10x. The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and out on the video display. While in the Split-Screen mode, pressing the MAP ACTV or VID ACTV Softkey determines which display the RANGE Knob adjusts.
SECTION 12 – ABNORMAL OPERATION SECTION 12: ABNORMAL OPERATION 12.1 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. Reduced navigation capability is available on the Reversionary Mode display.
SECTION 12 – ABNORMAL OPERATION 12.2 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. 12.
SECTION 12 – ABNORMAL OPERATION 12.6 DEAD RECKONING WARNING: DR Mode is inherently less accurate than the standard GPS/SBAS 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. While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode.
SECTION 12 – ABNORMAL OPERATION Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20 minutes. Terrain Proximity, TERRAIN-SVS, and TAWS are also disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. 12-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 190-00384-12 Rev.
SECTION 13 – ANNUNCIATIONS & ALERTS SECTION 13: 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 13 – ANNUNCIATIONS & ALERTS 13.1 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 13-2.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.2 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. WARNING Alerts (172R, 172S, 182T, T182T, 206H, and T206H) Annunciation Window Text Audio Alert CO LVL HIGH HIGH VOLTS Continuous Aural Tone LOW VOLTS* OIL PRESSURE PITCH TRIM** No Tone * Aural tone is inhibited while the aircraft is on the ground.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 13-5 AFCS System Status Annunciation Condition Annunciation Description Pitch Failure Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.5 TERRAIN-SVS ALERTS The following table shows the possible Terrain-SVS alert types with corresponding annunciations and aural messages.
SECTION 13 – ANNUNCIATIONS & ALERTS PFD/MFD Alert Annunciation Alert Type No GPS position TERRAIN-SVS Page Annunciation Aural Message NO GPS POSITION “Terrain System Not Available” None “Terrain System Not Available” None “Terrain System Available” Excessively degraded GPS signal, Out of database coverage area Sufficient GPS signal received after loss None 13.6 TAWS ALERTS The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 13 – ANNUNCIATIONS & ALERTS PFD/MFD TAWS-B Page Annunciation Alert Type MFD Pop-Up Alert Aural Message Premature Descent Alert Caution (PDA) Altitude Callout “500” “Too Low, Terrain” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) “Don’t Sink” or “Too Low, Terrain” or TAWS SYSTEM STATUS ANNUNCIATIONS PFD/MFD Alert Annunciation Alert Type System Test in Progress TERRAIN-SVS Page Annunciation Aural Message TAWS TEST None Sy
SECTION 13 – ANNUNCIATIONS & ALERTS 13.7 OTHER G1000 AURAL ALERTS Aural Alert “Minimums, minimums” “Vertical track” “Traffic” “Traffic not available” Description The aircraft has descended below the preset barometric minimum descent altitude. The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.8 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 13 – 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. Different versions of GDU software are installed in the PFD and MFD. This can also indicate different versions of navigation databases are installed in the PFD and MFD.
SECTION 13 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 13-6 illustrates all possible flags and the responsible LRUs.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.9 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section. NOTE: This section provides information regarding G1000 message advisories that may be displayed by the system.
SECTION 13 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message PFD1 KEYSTK – PFD1 [key name] Key is stuck. MFD1 KEYSTK – MFD [key name] Key is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage Comments A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists.
SECTION 13 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists. MFD1 DB ERR – MFD1 obstacle database missing. PFD1 DB ERR – PFD1 obstacle database missing. MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing.
SECTION 13 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message DB MISMATCH – Navigation database mismatch. Xtalk is off. Comments The PFD and MFD have different navigation database versions or regions installed. Crossfill is off. Check the AUX-SYSTEM STATUS Page to determine versions or regions. Also, check the AUX-SYSTEM STATUS Page for a database synchronization function not completed. After synchronization is complete, power must be turned off, then on.
SECTION 13 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Message Comments GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced. GMA1 CONFIG – GMA1 config The audio panel configuration settings do not match backup configuration memory. error. Config service req’d. The system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed. The system should be serviced.
SECTION 13 – 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 13 – 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.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories Message GIA1 CONFIG – GIA1 config error. Config service req’d. GIA2 CONFIG – GIA2 config 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 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message MANIFEST – GIA1 software mismatch, communication halted. MANIFEST – GIA2 software mismatch, communication halted. MANIFEST – GFC software mismatch, communication halted. MANIFEST– COM1 software mismatch, communication halted. MANIFEST– COM2 software mismatch, communication halted. MANIFEST– NAV1 software mismatch, communication halted. MANIFEST– NAV2 software mismatch, communication halted. COM1 TEMP – COM1 over temp.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message 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. LOI – GPS integrity lost. Crosscheck with other NAVS. GPS NAV LOST – Loss of GPS navigation. Insufficient satellites. GPS NAV LOST – Loss of GPS navigation. Position error. GPS NAV LOST – Loss of GPS navigation. GPS fail.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message 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. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. FAILED PATH – A data path has failed. Comments The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state.
SECTION 13 – 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 system should be serviced. The transponder has incorrect software installed. The system should be serviced.
SECTION 13 – 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 69/69A Message Advisories Message GDL69 CONFIG – GDL 69 config error.
SECTION 13 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message FPL TRUNC – Flight plan has been truncated. LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. APR INACTV – Approach is not active. SLCT FREQ – Select appropriate frequency for approach.
SECTION 13 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message VNV – Unavailable. Excessive track angle error. VNV – Unavailable. Unsupported leg type in flight plan. VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable. Parallel course selected. NON WGS84 WPT – Do not use GPS for navigation to -[xxxx] TRAFFIC FAIL – Traffic device has failed. NON WGS84 WPT – Do not use GPS for navigation to-[xxxx] STRMSCP FAIL – Stormscope has failed.
SECTION 13 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message [PFD1 or MFD1] CARD 1 REM – Card 1 was removed. Reinsert card. [PFD1 or MFD1] CARD 2 REM – Card 2 was removed. Reinsert card. [PFD1 or MFD1] CARD 1 ERR – Card 1 is invalid. [PFD1 or MFD1] CARD 2 ERR – Card 2 is invalid. TRN AUD FAIL – Trn Awareness audio source unavailable. TERRAIN AUD CFG – Trn Awareness audio config error. Service req’d. REGISTER GFDS – Data services are inoperative, register w/GFDS.
SECTION 13 – ANNUNCIATIONS & ALERTS Flight Plan Import/Export Results ‘Too many points. Flight plan truncated.’ Description The flight plan on the SD card contains more waypoints than the system can support. The flight plan was imported with as many waypoints as possible. ‘Some waypoints not loaded. Waypoints The flight plan on the SD card contains one or more waypoints that the locked.’ system cannot find in the navigation database.
INDEX A Abnormal COM operation 12-2 Activate a flight plan 8-4 Active channel 11-16 Active database 1-14 Active flight plan 8-4 Active Navigation Database 1-14 ADF 1-7, 5-3 ADS-B RR-2, 10-12, 10-14, 13-7 AFCS 13-4 Age 10-7 AHRS 13-21, 13-22 Aircraft alerts 13-3 AIRMET 10-5 Airport frequency 7-29 Airport information 7-25 Airspace alerts 7-33 Airspeed indicator 2-3 Airspeed Reference 6-8 Airspeed trend vector 2-3 Airways 8-7 Alerting system 13-1 Alerts 13-1 Alert levels 13-2 Alert Pop-Up 10-24 ALT 1-4, 1-8, 2
INDEX EDR 10-23 Electronic checklists 11-20, 11-21, 11-22 Emergency checklist 11-21 Engine Hours 3-3, 3-8 Engine Leaning 3-6 Engine Page 3-1 Excessive Descent Rate 10-23 Exhaust Gas Temperature 3-2, 3-4 F FD 1-4, 13-4 FIS-B Weather 10-7, 10-8, 10-9, 1010, 10-11 Five-Hundred Aural Alert 10-24 FLC 1-4 Flight director 6-2–6-3 Pitch modes 6-3–6-9 Roll modes 6-17–6-19 Flight ID 4-5 Flight level change 1-4 Flight Level Change Mode 6-28, 6-30 Flight Level Change Mode (FLC) 6-8 Flight plan import/export messages 1
INDEX NAV2 5-3 Navigation 7-1 Navigation database 1-11, 1-12 Navigation Mode 6-19–6-20 Navigation Mode, AFCS 6-26–6-27 Navigation status window 2-2 NAV frequency window 4-1 NCR 10-23 Nearest Airports Page 7-25, 7-29, 7-30, 7-31, 7-32, 7-33, 8-1 Nearest ARTCC & FSS frequencies 7-32 Negative Climb Rate After Takeoff 10-23 NEXRAD 10-3, 10-4, 10-7, 10-11 NEXRAD Softkey 10-10 Non-path descent 6-13, 6-30–6-31 O OBS 2-12 Obstacles 10-15, 10-20, 10-24, 13-13, 13-18 Oil Pressure 3-1, 3-7 Oil Temperature 3-1, 3-8 Op
INDEX Transponder standby mode 4-4 Transponder Status bar 4-5 Trim adapter 6-22 Tropical storms 10-5 Turbine Inlet Temperature 3-2, 3-4, 3-7 Turbine Inlet Temperature (TIT) 3-7 TX 4-3, 7-25 U Unable to display chart 11-12, 11-15 Unlighted obstacle 10-20, 10-24 V Vacuum Pressure 3-2, 3-8 VDI 7-18 Vertical Deviation 2-2, 2-6 Vertical deviation guidance 1-11, 1-12 Vertical Deviation Indicator 7-18 Vertical navigation 1-11, 1-12 Vertical Navigation flight control 6-10–6-14 Vertical Path Tracking Mode 6-10–6-1
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