Integrated Flight Deck Cockpit Reference Guide Cessna Nav III
Copyright © 2004-2006 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0563.00 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in Cessna Nav III aircraft, has a very high degree of functional integrity.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00384-03 (Rev. A) 190-00384-03 (Rev. B) 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 Updated system software numbers 190-00384-04 (Rev. A) Reformatted manual to new format Added TAS capability 190-00384-04 (Rev.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
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 .......................................................... 1-7 MFD Page Groups ................................................... 1-9 Vertical Navigation ................................................ 1-9 Backlighting ...........
TABLE OF CONTENTS Roll Modes................................................................ 6-17 Roll Hold Mode (ROL) ........................................... 6-17 Heading Select Mode (HDG) ................................. 6-18 Navigation Mode (GPS, VOR, LOC) ........................ 6-19 Approach Mode (GPSa, VAPP, LOC)....................... 6-20 Backcourse Mode (BC) ......................................... 6-21 6.4 Autopilot Operation ............................................
TABLE OF CONTENTS 7.12 Nearest VOR ........................................................... 7-21 Select the Nearest VOR Page ..................................... 7-21 View Information on the Nearest VOR ................... 7-21 Select and Load a VOR Frequency ......................... 7-21 7.13 Nearest User Waypoint........................................ 7-22 Select the Nearest User Waypoint Page ...................... 7-22 Select a Nearest User Waypoint ............................ 7-22 7.
TABLE OF CONTENTS Enable/Disable Aviation Data ................................... 10-12 TAWS Inhibit ........................................................... 10-12 Manual System Test................................................. 10-12 Forward Looking Terrain Avoidance (FLTA) ................ 10-12 Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) ...... 10-12 Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) .........................................
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 (19000498-01).
SECTION 1 SYSTEM OVERVIEW 1.
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 PROC Key – Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/ or arrival airport are automatically suggested.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON BACK – Press to return to the previous level softkey configuration. ALERTS – Press to display the Alerts Window. Softkey OFF WIND 360 HSI ARC HSI Press the DFLTS Softkey to change the PFD metric values to standard. Press the STD BARO or BACK Softkeys to return to the top level softkeys. Figure 1-3 PFD Softkey Flow Chart – 1 Figure 1-2 PFD Top Level Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD.
SECTION 1 SYSTEM OVERVIEW Press the DFLTS Softkey to change the PFD metric values to standard. Press the STD BARO or BACK Softkeys to return to the top level softkeys. Figure 1-4 PFD Softkey Flow Chart – 2 BRG2 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the appropriate information. NAV2 – Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window.
SECTION 1 SYSTEM OVERVIEW Press the BACK Softkey to return to the top level softkeys GND Press the BACK Softkey to return to the top level softkeys Figure 1-5 PFD Softkey Flow Chart – 3 IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC).
SECTION 1 SYSTEM OVERVIEW ENGINE DCLTR MAP CHKLIST (optional) DCLTR-1 LEAN ENGINE SYSTEM BACK DCLTR-2 DCLTR-3 Press the BACK Softkey on this level to return to the top softkey level. ENGINE LEAN SYSTEM RST FUEL BACK GAL REM TRAFFIC TOPO TERRAIN (optional) (optional) (optional) STRMSCP NEXRAD XM LTNG BACK Press the ENGINE or BACK Softkey on any level to return to the default page level.
SECTION 1 SYSTEM OVERVIEW 1.4 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-7. Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1-7 Page Group Icon 1.5 VERTICAL NAVIGATION The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation.
SECTION 1 SYSTEM OVERVIEW or rendered invalid as a result of manually changing an altitude to a non-designated altitude. To help interpret the meanings of how the altitudes are presented, keep the following points in mind: Refer to Figure 1-8 and Table 1-1 for more detail regarding the significance of text size and color. • When the altitude is displayed in light blue, the system is using that altitude (designated) to determine vertical speed and deviation guidance.
SECTION 1 SYSTEM OVERVIEW Some altitudes retrieved from the database have associated restrictions indicating to stay ‘At’, ‘At or Above’, or ‘At or Below’ a specific altitude. These restrictions are indicated using a ‘bar’ above and/or below the appropriate altitude as shown in Figure 1-9. Stay AT or ABOVE 5,000 ft Stay AT 2,300 ft Stay AT or BELOW 3,000 ft Figure 1-9 Altitude Restrictions See Section 7 - Navigation, for a sample flight plan which further illustrates vertical navigation in more detail. 1.
SECTION 1 SYSTEM OVERVIEW 1.8 DATABASE UPDATES The G1000 System uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD cards are required for database storage as well as Jeppesen aviation and ChartView database updates. The following procedures pertain to updating the G1000 system with SD cards obtained as outlined in Appendix B of the G1000 Cessna Nav III Pilot’s Guide.
SECTION 1 SYSTEM OVERVIEW Garmin Databases Since these databases are not stored internally in the MFD or PFD, a Supplemental Data Card containing identical database versions must be kept in each display unit. NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data.
SECTION 1 SYSTEM OVERVIEW Blank Page 1-14 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
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 Altitude Reference Bug 12 Selected Course Box 13 Barometric Minimums Bug 14 Vertical Deviation/Glidepath (WAAS enabled systems only)/Glidesope 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 Barometric Setting Box Altitude Reference Box Altitude Reference Bug Select barometric pressure: 1) Turn the BARO Knob to select the desired setting. 2) Push the BARO Knob to select standard pressure 29.92.
SECTION 2 FLIGHT INSTRUMENTS VNAV Target Altitude Vertical Deviation Indicator Figure 2-9 Altimeter (Metric) 2.4 Required Vertical Speed Figure 2-10 Vertical Deviation Indications 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 2-10).
SECTION 2 FLIGHT INSTRUMENTS The Glideslope Indicator appears when an ILS approach has been activated and an ILS is tuned in the active NAV receiver field (see Figure 2-12). 2.6 VERTICAL SPEED INDICATOR Selected Vertical Speed Marker Beacon Annunciation Vertical Speed Bug Vertical Speed Pointer Glideslope Indicator Figure 2-14 Vertical Speed Indicator Figure 2-12 Glideslope Indicator 2.
SECTION 2 FLIGHT INSTRUMENTS Visual annunciations alert the pilot when approaching the MDA: • When the aircraft altitude descends to within 2500 feet of the MDA setting, the Barometric Minimum Box appears with the altitude in light blue text. The bug appears on the tape in light blue once in range. • When the aircraft passes through 100 feet of the MDA, the bug and text turn white. • Once the aircraft descends past the MDA, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated.
SECTION 2 FLIGHT INSTRUMENTS 15 Turn Rate Indicator and Heading Trend Vector 14 1 13 2 3 12 4 11 5 10 9 6 8 7 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Turn Rate Indicator Ground Track Bug Lateral Deviation Scale Navigation Source Aircraft Symbol Course Deviation Indicator Rotating Compass Rose OBS Mode TO/FROM Indicator Heading Bug Course Pointer Flight Phase Turn Rate and Heading Trend Vector Heading Lubber Line Tick marks to the left and right of the lubber line denote half-standard and standard
SECTION 2 FLIGHT INSTRUMENTS Course Deviation Indicator (CDI) Distance to Bearing Source The CDI scale automatically adjusts to the current phase of flight (enroute 2.0 nm, terminal area 1.0 nm, or approach 0.3 nm). Scaling may be selected manually from the MFD System Setup Page. See the System Setup section in the G1000 Pilot’s Guide for more details. Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys.
SECTION 2 FLIGHT INSTRUMENTS • LOI - GPS position integrity is inadequate for the current procedure being flown. If GPS is being used as primary navigation, and LOI is annunciated, other means of primary navigation will be required, such as VHF. LOI is also displayed during GPS position initialization. • WARN – GPS detects a position error. • 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.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm). Red range indicates propeller overspeed warning; a white high-rpm range indicates above normal operating speeds (Models 172S, 206H, and T206H) 3 Fuel Flow Indicator (FFLOW GPH) – Shows the current fuel flow in gallons per hour (gph).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 10 11 Fuel Quantity Indicator (FUEL QTY GAL) – Shows the quantity of fuel in the tanks, in gallons, ranging from zero to full (F) for each fuel tank (left–L and right–R). When full, the indicator displays to 35 gallons per side (26 gallons for the Models 172R and 172S). 12 Voltmeter (M, E BUS VOLTS) – Displays the main and essential bus voltages. 13 Ammeter (M, S BATT AMPS) – Shows the main and standby battery load in amperes.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 Cruise Fuel Flow 4 3 4 5 5 6 6 8 8 10 10 12 12 13 13 Model T182T Maximum Takeoff Fuel Flow Model T206H Figure 3-2 Engine Display (Turbocharged Aircraft) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3-3
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 LEAN DISPLAY for the selected cylinder to be displayed below the indicator. NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH). 3-4 1 Engine Manifold Pressure Gauge (MAN IN) Models 182T, T182T, 206H, T206H – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 2 1 2 1 2 5 2 5 3 3 Hollow Block Represents Peak 5 5 6 6 3 3 7 7 Model 172R 6 6 7 Model 172S 7 Model 182T Model 206H Figure 3-3 Lean Display (Normally-aspirated Aircraft) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3-5
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 3 4 4 5 5 6 6 7 7 Model T182T Model T206H Figure 3-4 Lean Display (Turbocharged Aircraft) The Lean Display is accessed by pressing the ENGINE Softkey followed by the LEAN Softkey and provides information for performing engine leaning. 3-6 From the Lean Display, the pilot can utilize the CYL SLCT and ASSIST softkeys to obtain information about specific cylinders.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) The ASSIST Softkey aids in the leaning process by identifying the peak of the first cylinder whose temperature falls. If the temperature of the peaked cylinder exceeds the peak value, the peak value is not updated. Press the ASSIST Softkey to stop peak monitoring. Normally-aspirated Aircraft For normally-aspirated aircraft, when a cylinder peaks, its peak is represented by a hollow block on the EGT Bar Graph.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-8 1 Engine Manifold Pressure Gauge (MAN IN) Models 182, T182, 206, T206 – Displays engine power in inches of mercury (in Hg). Turbocharged aircraft have a red portion of the gauge indicating the maximum manifold pressure range. A white tick mark is displayed indicating the cruise manifold pressure (Model T182 only). 2 Tachometer (RPM) – Shows propeller speeds in revolutions per minute (rpm).
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 2 2 3 3 4 4 7 7 8 8 9 9 10 10 11 11 12 12 Model 172R Model 172S 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 11 11 12 12 Model 182T Model 206H Figure 3-5 System Display (Normally-aspirated Aircraft) Garmin G1000 Cockpit Reference Guide for the Cessna Nav III 3-9
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Cruise Manifold Pressure 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 11 11 12 12 Model T182T Model T206H Figure 3-6 System Display (Turbocharged Aircraft) 3-10 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
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.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field 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. • Press to change tuning box positions.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • TX – When a COM radio is transmitting, a white TX indication appears to the right of the corresponding COM frequency. • 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. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. 4.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD 4.7 TRANSPONDER Mode Selection The STBY, ON and ALT Softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-9 Nearest Airports Window (PFD) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn either FMS Knob to highlight the desired frequency.
SECTION 4 – NAV/COM & TRANSPONDER Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference Window. Flight ID Figure 4-12 Timer/References Window 1) Press the TMR/REF Softkey to display the Timer/ References Window. 2) Turn the large FMS Knob to place the cursor in the Flight ID field. 3) Turn the small FMS Knob to enter the desired first character. 4) Turn the large FMS knob to place the cursor in the next desired field.
SECTION 4 – NAV/COM & TRANSPONDER Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters Receiver Audio Disabled Passenger Address 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 Garmin G1000 Cockpit Reference Guide for the Cess
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Outer Marker Annunciator Middle Marker Annunciator 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.
SECTION 5 – AUDIO PANEL 5.3 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. 5.4 INTERCOM SYSTEM (ICS) ISOLATION 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.
SECTION 5 – AUDIO PANEL 5.5 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 MKR/MUTE while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key will begin playing the next previously recorded block.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL NOTE: The Aircraft Flight Manual (AFM) always supersedes the information in this guide. This section only applies to the GFC 700 Automatic Flight Control System (AFCS). NOTE: The GFC 700 AFCS is not available for the Cessna 172. 6.1 AFCS CONTROLS The following dedicated AFCS keys are located on the bezels of the PFD and MFD: forward of the MET Switch on the pilot’s control wheel left grip.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.2 FLIGHT DIRECTOR OPERATION With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (+20°/-15°) and bank (22°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification. The flight director also provides commands to the autopilot.
SECTION 6 – AUTOMATIC FLIGHT CONTROL AFCS Status Box Flight director roll modes are shown on the left and pitch on the right. Armed modes are annunciated in white and active in green. Autopilot status is displayed in the center of the AFCS Status Box. 6.3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Table 6-1 lists the pitch modes with their corresponding controls and annunciations. The mode reference (shown with default measurement units) is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/ NOSE DN Keys can be used to change the pitch mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) Changing the Pitch Reference When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when the mode is activated.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Selected Altitude Capture Mode (ALTS) Selected Altitude Capture Mode arms automatically when the flight director is in Pitch Hold, Vertical Speed, Flight Level Change, or Go Around Mode. This mode is also armed automatically under Vertical Path Tracking Mode when the Selected Altitude is to be captured instead of the VNAV Target Altitude. The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 6-5 for example).
SECTION 6 – AUTOMATIC FLIGHT CONTROL If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed. To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected Altitude is reached.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode Active Vertical Selected Altitude Capture Speed Mode Armed Reference Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Figure 6-8 Vertical Speed Mode Changing the Vertical Speed Reference The Vertical Speed Reference (shown both in the AFCS Status Box and above/below the Vertical Speed Indicator) may be changed by: • Using the NOSE UP/NOSE DN Keys • By pressing the CWS Butt
SECTION 6 – AUTOMATIC FLIGHT CONTROL descent). The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Navigation Modes (VPTH, ALTV) NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The autopilot guides the aircraft back to the descent path upon release of the CWS Button. NOTE: VNAV flight director pitch modes are available only in conjunction with GPS roll modes. NOTE: The Selected Altitude takes precedence over any other vertical constraints.
SECTION 6 – AUTOMATIC FLIGHT CONTROL In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Data Box, VNAV indications (VNAV Target Altitude, vertical deviation, and vertical speed required) appear on the PFDs in magenta (Figure 6-11).
SECTION 6 – AUTOMATIC FLIGHT CONTROL When a descent leg is captured (Figure 6-12), Vertical Path Tracking becomes active and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.
SECTION 6 – AUTOMATIC FLIGHT CONTROL VNAV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile recapture.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture mode are armed in preparation to capture the new VNAV Target Altitude or the Selected Altitude, depending on which altitude is to be intercepted first.
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 couple 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 (GPSa, VAPP, LOC) — Captures and tracks the selected navigation source with greater sensitivity
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) Figure 6-20 Roll Hold Mode Annunciation Bank Angle Flight Director Response < 6° Rolls wings level 6° to 22° Maintains current aircraft roll attitude > 22° Limits bank to 22° Heading Select Mode is activated by pressing HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes of more than 340° at a time result in turn reversals. Navigation Mode (GPS, VOR, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Backcourse Mode (BC) Changing the Selected Course NOTE: When making a backcourse approach, set the Selected Course to the localizer front course. Backcourse Mode captures and tracks a localizer signal. The mode may be selected by pressing the BC Key. Backcourse Mode is armed if the CDI is greater than one dot when the mode is selected. The flight director creates roll steering commands from the Selected Course and deviation when in Backcourse Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.4 AUTOPILOT OPERATION NOTE: Refer to the AFM for specific instructions regarding emergency procedures. Cessna Nav III’s autopilot operates flight control surface servos to provide automatic flight control. The autopilot controls the aircraft pitch and roll attitudes following commands received from the flight director. Pitch autotrim provides trim commands to the pitch trim adapter to relieve any sustained effort required by the pitch servo.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Control Wheel Steering During autopilot operation, the aircraft may be handflown without disengaging the autopilot. Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand-flown. At the same time, the flight director is synchronized to the aircraft attitude during the maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS maneuvers.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.5 EXAMPLE PROCEDURES Departure NOTE: The diagrams in this section are for instructional purposes only and should not be used for navigation. This section provides a scenario-based set of procedures showing various GFC 700 AFCS modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT).
SECTION 6 – AUTOMATIC FLIGHT CONTROL The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/NOSE DN keys or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed Reference.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V107 to Panoche VORTAC (PXN) should now be intercepted. Intercepting a VOR: 1) Tune the VOR frequency and activate Navigation Mode. a) Use the CDI Softkey to set the navigation source to VOR. b) Use the CRS Knob to set the Selected Course to 116°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly 070°.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan/GPS Course a) Use the CDI Softkey to select GPS as the navigation source. This causes the flight director to lose the VOR signal, and the VOR annunciation flashes yellow as the autopilot rolls the wings level. NOTE: Changing the navigation source cancels the flight director’s Navigation Mode and causes the flight director to automatically revert to Roll Hold Mode, wings level.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Descent While flying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT.
SECTION 6 – AUTOMATIC FLIGHT CONTROL c) If Vertical Path Tracking Mode is armed more than five minutes prior to descent path capture, acknowledgment is required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL b) Press the FLC Key before the planned TOD during a vertical profile level leg (tracked using Altitude Hold Mode). The Airspeed Reference defaults to the current aircraft airspeed. Vertical Path Tracking and Selected Altitude Capture Mode is armed automatically. 4) When the next TOD is reached,Vertical Path Tracking becomes active (may require acknowledgment to allow descent path capture).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach 2) Use Heading Select Mode to comply with ATC vectors as requested. Flying an ILS approach: 3) Tune the localizer frequency. 1) Transition from GPS Navigation Mode to Heading Select Mode. 4) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. a) Load the Runway 29R ILS approach for KFAT into the flight plan. b) Select ‘VECTORS’ for the transition.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 2) Press the APR Key once clearance for approach has been acquired. GPS Approach Mode is activated (provided the crosstrack error is less than 2 nm) and Glidepath Mode is armed. NOTE: Support for WAAS precision approaches is available only in installations with GIA 63W Integrated Avionics Units and when WAAS is available.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around/Missed Approach 1) Push the GA Switch at the Decision Height and apply full power to execute a missed approach. The flight director Command Bars establish a climb to follow. de 27 21 12 18 S V NA a) Press the AP Key to re-engage the autopilot. CZQ 9 24 4 GP 2) Start the climb to the prescribed altitude in the published Missed Approach Procedure.
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
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 ‘VNAV’ 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. Select a Direct-to Destination to a Nearest Airport 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 7-3.
SECTION 7 – NAVIGATION 7) Enter the desired offset distance. 8) Press the ENT Key. 9) Turn the large FMS Knob to place the cursor in the ‘COURSE’ field. 10) Enter the desired course. 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 75. 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 1) Press the Direct-to Key ( ). Select a Direct-to Destination to a Flight Plan Waypoint 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 3) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position as shown in Figure 7-9. 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. 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.
SECTION 7 – NAVIGATION 2) The aircraft is being flown along the active MCI to DOSOA leg. 3) Now that DOSOA is passed and the DOSOA to KDFW leg is active, maintain a track along the magenta line (as in Figure 7-12) keeping the CDI centered. Note the CDI flight mode is in enroute (ENR) mode. Figure 7-13 Loaded Arrival 5) It is now determined that the aircraft will proceed directly to MLC. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to select MLC in the flight plan list.
SECTION 7 – NAVIGATION Figure 7-15 Enter Offset Distance Figure 7-14 Direct-to First Arrival Waypoint 6) While proceeding to MLC, instructions are received to descend to 8,000 feet prior to BYP. An Along-track Offset waypoint will be used to accomplish this. e) Press the ENT Key. The cursor is now displayed in the ‘ALT’ field. f) Enter the desired altitude constraint, in this case 8,000 feet. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight the BYP waypoint.
SECTION 7 – NAVIGATION h) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 7-17. i) At this point, the desired descent vertical speed can be selected, or the desired descent flight path angle (FPA) can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to entered the desired value. In this example, a 500 foot per minute vertical speed is selected. 7) The aircraft is approaching MLC.
SECTION 7 – NAVIGATION 8) After passing MLC the previous leg will no longer be displayed on the map. The magenta arrow in the flight plan list now indicates the MLC to BYP leg is now active. The CDI flight mode will change from enroute to terminal (TERM). Keep the CDI centered and maintain a track to follow the magenta line. 9) The aircraft has reached TOD. Note the target vertical speed and the required vertical speed that will be required to reached the selected altitude.
SECTION 7 – NAVIGATION 10) Establish a descent vertical speed which places the VSI pointer in line with the RVSI. Upon reaching the offset waypoint, the aircraft will be at 8,000 feet. 11) The aircraft is approaching BYP. The upcoming turn and next heading will be annunciated at the top left of the PFD. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the BYP to KARLA leg and center the CDI.
SECTION 7 – NAVIGATION 12) After passing BYP the next leg of the arrival will turn magenta. The magenta arrow in the flight plan list now indicates the MLC to BYP leg is now active. Keep the CDI centered and maintain a track to follow the magenta line. plan will automatically sequence to the FAF as the active leg. Manually activate the approach by performing the following steps: a) Press the PROC Key. b) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
SECTION 7 – NAVIGATION Figure 7-28 Descending to the Initial Approach Fix (IAF) Figure 7-30 Turning to the Initial Approach Fix (IAF) Leg 16) At DRAAK, establish another descent as done previously to obtain an altitude of 3,000 feet at INWOD. Figure 7-29 Establish Descent Rate to the IAF 15) Upon making the descending turn, the RIVET to DRAAK leg is now active. Keep the CDI centered to track the magenta line and maintain 4,000 feet to DRAAK.
SECTION 7 – NAVIGATION 17) If the installed GPS system is WAAS capable, at (or just prior to) the FAF, the VDI changes to the Glidepath Indicator as shown in Figure 7-34. Continue the descent through INWOD using the Glidepath Indicator, as one would use a Glideslope Indicator, to obtain an altitude “AT” 2,300 feet at the FAF (MENOL). Also, the CDI flight mode will change from terminal mode to LPV mode. Note the altitude restriction lines over and under (‘At’) the altitude in the ‘ALT’ field.
SECTION 7 – NAVIGATION Figure 7-36 Following the Glidepath to the MAP 19) Upon reaching the MAP, it is decided to execute a missed approach. a) Press the PROC Key. b) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. Figure 7-38 Missed Approach Active 20) At POLKE follow the next turn prompts in the upper left of the PFD. Follow the POLKE to BACKS (MAHP) leg. Continue climbing to “AT or ABOVE” 5,000 feet at BACKS.
SECTION 7 – NAVIGATION 21) A holding pattern will be established at the MAHP (BACKS). 7.4 AIRPORT INFORMATION Figure 7-42 Airport Information Page Figure 7-40 Reaching the Missed Approach Hold Point 22) Maintain 5,000 feet and follow the magenta line through the hold. Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the first rectangular page icon.
SECTION 7 – NAVIGATION 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-43. The list is populated only when navigating a flight plan. Figure 7-43 Flight Plan Airport List 3) Turn the small FMS Knob to the right to display the ‘RECENT’ airports as shown in Figure 7-45. 3) Turn the large FMS Knob to select the desired airport. 4) Press the ENT Key.
SECTION 7 – NAVIGATION 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. Access Frequency Information 7.5 INTERSECTION INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon.
SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-47 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1) With the NDB Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired selection field (identifier, name or closest city).
SECTION 7 – NAVIGATION 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.9 NEAREST AIRPORTS Access Information on a Specific Airport 1) With the Nearest Airports Page displayed, press the APT Softkey to place the cursor in the ‘NEAREST AIRPORTS’ field. The first airport in the nearest airports list is highlighted. 2) Press the FMS Knob, then turn the large 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 7-50 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. 2) Press the ENT Key to display airport information.
SECTION 7 – NAVIGATION 7.11 NEAREST NDB 7.12 NEAREST VOR Figure 7-53 Nearest VOR Page Figure 7-52 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page icon. Access Information on a Specific NDB 1) With the Nearest NDB Page displayed, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired NDB.
SECTION 7 – NAVIGATION 2) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. Nearest User 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.
SECTION 7 – NAVIGATION COM frequency standby field. 4) Press the FMS Knob to remove the flashing cursor. 7.15 NEAREST AIRSPACES • If the aircraft has entered an airspace, ‘Inside’ is displayed. View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to scroll through the list, highlighting the desired airspace. 3) Press the ALERTS Softkey to place the cursor in the ‘AIRSPACE ALERTS’ field.
SECTION 7 – NAVIGATION Blank Page 7-24 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS 4) Repeat steps 2 and 3 until the desired name is entered. 5) Press the ENT Key. 6) Press the ENT Key a again to accept the new waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knobs to select a waypoint name. 5) Press the ENT Key to accept the selected name.
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 3) 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. 4) With ‘Activate’ highlighted, press the ENT Key.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. 8) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list.
SECTION 8 – FLIGHT PLANNING 8.8 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8.9 LOAD AN ARRIVAL Figure 8-13 Store Flight Plan Confirmation 8.13 EDIT A STORED FLIGHT PLAN See the Procedures section for a discussion on loading and activating arrival procedures. 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 8.10 LOAD AN APPROACH 2) Press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING 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. 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired flight plan. 3) Press the INVERT Softkey.
SECTION 8 – FLIGHT PLANNING 8.19 TRIP PLANNING 1) Turn the large FMS Knob to select the ‘AUX’ page group. 2) Turn the small FMS Knob to select the first rectangular page icon. 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. Starting WPT Ending WPT 5) For point-to-point planning, turn the FMS Knobs to enter the identifier of the starting waypoint.
SECTION 8 – FLIGHT PLANNING 9) 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. 10) 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. In ‘AUTOMATIC’ mode, fuel onboard is provided by the entry made in ‘GAL REM’ on the EIS System Page. 11) The flashing cursor moves to the calibrated airspeed field.
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 will be 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. will not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS).
SECTION 9 – PROCEDURES 6) Turn either FMS Knob to highlight the desired approach. Press the ENT Key. 7) The cursor will move to the TRANSITIONS field. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key. (The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ group (Figure 10-2) to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob until the Stormscope Page is selected. This is the third rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE Change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (SERVICE OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – Pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • • • • Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available. From within the AUX - XM INFORMATION Page, the pilot may switch to the AUX - XM RADIO Page by pressing the RADIO Softkey.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ TNA Mute above & descending, moving in Traffic out of Status Traffic Mode the direction of the line range NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. NOTE: If the G1000 is configured to use a Traffic Advisory System (TAS), TIS will not be available for use.
SECTION 10 – HAZARD AVOIDANCE 10.5 TRAFFIC ADVISORY SYSTEM (TAS) (OPTIONAL) Refer to the Honeywell KTA 870 Pilot’s Guide for a detailed discussion of the KTA 870 system. System Self Test 1) Set the range to 2/6 nm. 2) Press the STANDBY Softkey. 3) Press the TEST Softkey. 4) Self test will take approximately eight seconds to complete. When completed successfully, traffic symbols will be displayed as shown in Figure 10-12 and a voice alert “TAS System Test OK” will be heard.
SECTION 10 – HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 1) Ensure the KTA 870 system is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Traffic will now be displayed on the map. Traffic Advisory 2) Turn the small FMS Knob to select the last rectangular page icon. 3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys. When the ARC Softkey is pressed, a radar-like 120° view is displayed.
SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Figure 10-16 Obstacle Symbols 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 will now be displayed on the map. 10.
SECTION 10 – HAZARD AVOIDANCE Figure 10-17 TAWS Page (360˚ View) Color Red Figure 10-18 TAWS Page (ARC View) Terrain/Obstacle Location Terrain/Obstacle at or within 100’ below or above aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Black Terrain/Obstacle is more than 1000’ below aircraft altitude.
SECTION 10 – HAZARD AVOIDANCE Enable/Disable Aviation Data 1) While the TAWS 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 10-19 TAWS Page Menu A system test is automatically performed at power-up. After successful completion of the test, “TAWS System Test, OK” will be heard. The system test may also be initiated manually, but only when the aircraft is on the ground.
SECTION 10 – HAZARD AVOIDANCE Terminal 350 ft. 300 ft. Approach 150 ft. 100 ft. Departure 100 ft. 100 ft. During the final approach phase of flight, RTC/ROC/ ITI/IOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or is below 125 feet AGL while within 1 nm of the runway.
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 TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 11 – ABNORMAL OPERATION 11.6 DEAD RECKONING If at any time the G1000 detects an invalid GPS solution or is unable to calculate a GPS position, the system will automatically revert to Dead Reckoning (DR) mode. In DR mode, the G1000 uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position.
SECTION 11 – ABNORMAL OPERATION Blank Page 11-4 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Cessna aircraft Pilot’s Operating Handbook (POH) supersedes information found in this document. The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is based on alert levels described later in the Alert Levels Definitions section.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Cessna Nav III aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention. A warning alert is annunciated in the Annunciation Window and is accompanied by a continuous aural tone. Text appearing in the Annunciation Window is RED. A warning alert is also accompanied by a flashing WARNING Softkey annunciation, as shown in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 NAV III AIRCRAFT ALERTS The following alerts are configured specifically for the Cessna Nav III aircraft. See the Cessna Pilot’s Operating Handbook (POH) for information regarding pilot responses. Safe Operating Annunciation (T182, T206, and 206 with Prop De-Ice Only) Annunciation Window Text PROP HEAT Audio Alert No Tone 12.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS (182 & 206 ONLY) System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 12-5 AFCS System Status Annunciation Condition Pitch Failure Description Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.5 TAWS ALERTS The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 12 – ANNUNCIATIONS & ALERTS The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Available” will be heard when sufficient GPS signal is re-established.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Indicates a configuration module failure. This annunciation will only be seen when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal flight parameter, possibly caused by strong turbulence. In this case, the situation should correct itself within a few seconds. If there is an actual failure, a red “X” will soon appear over the Attitude Indicator.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving valid transponder information. ‘LOI’ Indicates Loss of Integrity of GPS information. GPS information is either not present or is invalid for navigation use. ‘DR’ may also be seen indicating that GPS is in Dead Reckoning Mode. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFMS).
SECTION 12 – ANNUNCIATIONS & ALERTS TIS Voice Alerts The following voice alerts can be configured for ‘Male’ or ‘Female’ gender by using the Aux System Setup Page on the MFD. Voice Alert “Traffic” Alert Trigger Played when a Traffic Advisory (TA) is issued. “Traffic Not Available” Played when the traffic system fails or cannot communicate. NOTE: Voice alerts are provided to the G1000 by GIA 63/W #1. Should this unit fail, audio and voice alerts will no longer be available. 12.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch. Communication halted. MANIFEST – MFD1 software mismatch. Communication halted. PFD1 CONFIG – PFD1 configuration error. Config service req’d.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Message MFD1 DB ERR – MFD1 aviation database error exists. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message DB MISMATCH – Aviation database version mismatch. Xtalk is off. DB MISMATCH – Aviation database type mismatch. Xtalk is off. DB MISMATCH – Terrain database version mismatch. Xtalk is off. DB MISMATCH – Terrain database type mismatch. Xtalk is off. DB MISMATCH – Obstacle database version mismatch. Xtalk is off DB MISMATCH – Airport Terrain database mismatch.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories Message Comments GIA1 CONFIG – GIA1 configuration error. Config service req’d. The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The G1000 system should be serviced. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments COM1 SERVICE – COM1 needs service. Return unit for repair. The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The G1000 system should be serviced when possible. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or is stuck. “pressed”) position.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Message Comments GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still GPS2 SERVICE – GPS2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. A failure has been detected in the NAV1 and/or NAV2 receiver.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message 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. Return the unit for repair. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted.
SECTION 12 – 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 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch. Communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GRS 77 Message Advisories (Cont.) Message GEO LIMITS – AHRS1 too far North/ South, no magnetic compass. MANIFEST – GRS1 software mismatch. Communication halted. Comments The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged as invalid. The #1 AHRS has incorrect software installed. The G1000 system should be serviced. GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message ARSPC NEAR – Airspace near – less than 2 nm. LEG UNSMOOTH – Flight plan leg will not be smooth. APPR INACTV – Approach is not active. SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Bad geometry, parallel offset not activated. PTK FAIL – Invalid leg type, parallel offset not activated. PTK FAIL – Past IAF, parallel offset not activated.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message TRAFFIC FAIL – Traffic device has failed. STRMSCP FAIL – Stormscope has failed. FAILED PATH – A data path has failed. MAG VAR WARN – Large magnetic variance. Verify all course angles. SCHEDULER [#] – . Comments The G1000 is no longer receiving data from the traffic system. The traffic device should be serviced. Stormscope has failed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS Blank Page 12-24 Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-5, 1-6, 5-3 AFCS 12-4 Age 10-6 AHRS 12-19, 12-20 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-19 Airport information 7-15 Airspace alerts 7-23 Airspeed indicator 2-3 Airspeed Reference 6-8, 6-28 Airspeed trend vector 2-3 Alerting system 12-1 Alerts 12-1 Alert levels 12-2 Alert Pop-Up 10-14 Along-track Offset 7-7 ALT 1-4, 1-6, 2-4, 4-4, 6-4, 6-6, 6-13, 6-24, 6-25, 6-28, 6-29, 6-30, 6-33, 7-7, 7-11, 7-13, 10-8, 1
INDEX Flight Plan Catalog 9-1, 9-2 FLTA 10-12 Forward Looking Terrain Avoidance 10-12 FPL key 1-3 Freezing level 10-5 Frequency toggle key 1-3, 4-3 Fuel Calculations 3-7 Flow totalizer 3-7 Remaining 3-8 Used 3-8 Fuel Flow 3-1, 3-3, 3-4, 3-8 Fuel Quantity 3-2, 3-4, 3-8 FUEL softkey 3-7 MKR/MUTE 5-2, 5-4 Mode selection softkeys 4-4 Morse code identifier 4-3 K Nav/Com controls 4-1 NAV1 5-3 NAV2 5-3 Navigation 7-1 Navigation database 1-9, 1-10 Navigation Mode 6-19–6-20 Navigation Mode (VOR, GPS, LOC, BC) 6-26
INDEX Pitch hold 1-4 Pitch Hold Mode (PIT) 6-5 Pitch modes, flight director 6-3–6-9 Pitch Reference 6-5 PLAY key 5-4 Premature Descent Alert 10-13 Procedure examples, AFCS 6-24–6-31 PROC key 1-4 R Red pointer 2-3 Remove departure, arrival, or approach 8-5 Replies 4-4 Required Vertical Speed 2-5, 7-9 Required Vertical Speed Indicator 7-9 Reversionary mode 5-1, 11-1 ROC 10-12, 10-13, 10-15, 12-5 Roll Hold Mode (ROL) 6-17 Roll modes, flight director 6-17–6-20 Roll Reference 6-18 RTC 10-12 RVSI 7-9, 7-10, 7-11 R
INDEX Vertical Navigation flight control 6-10–6-14 Vertical Path Tracking Mode 6-10–6-11, 6-28 Vertical speed 1-4, 2-6 Vertical Speed Bug 2-6 vertical speed guidance 1-10 Vertical Speed Mode 6-7 Vertical Speed Mode (VS) 6-24 Vertical Speed Reference 6-7, 6-24 VHF 4-1 VNAV 1-9, 1-10, 7-1, 7-2, 7-3, 7-4, 7-8, 7-11, 7-13, 12-22 VNAV ALT 7-11, 7-13 VNAV Target Altitude 6-10–6-13 VNAV Target Altitude Capture Mode 6-13 Voice alerts 12-3 VOL/PUSH ID 4-2 VOL/PUSH SQ 4-2, 4-3 Voltmeter 3-2, 3-8 Volume/squelch 5-4 VS
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00384-06 Rev. A © 2004-2006 Garmin Ltd.
