Integrated Flight Deck Cockpit Reference Guide Cessna 350/400
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ABNORMAL OPERATIONS ANNUNCIATIONS & ALERTS INDEX
Copyright © 2006, 2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0530.04 or later for the Cessna 400 and System Software version 0545.00 or later for the Cessna 350. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc.
WARNINGS, CAUTIONS, & NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in the Cessna 350/400 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00567-00 Rev A Rev B 190-00567-01 Rev A Change Summary Production release. Added C350 parameters, TAWS changes, and Stormscope. Added GDU 8.10 parameters, WAAS, VNAV, Airways, and Charts Revision Date of Revision Affected Pages B 12/07 i-Index-4 190-00567-01 Rev.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 PFD/MFD Controls................................................... 1-2 GCU 476 Controls .................................................... 1-5 PFD Softkeys............................................................ 1-7 MFD Softkeys ........................................................ 1-10 MFD Page Groups ................................................. 1-11 Vertical Navigation .....
TABLE OF CONTENTS 6.5 Example Procedures Using AFCS ....................... 6-23 Departure ................................................................. 6-24 Intercepting a VOR Radial .......................................... 6-25 Flying a Flight Plan/GPS Course ................................. 6-26 Descent .................................................................... 6-27 Approach .................................................................. 6-30 Go Around/Missed Approach ................
TABLE OF CONTENTS 10.6 Terrain And Obstacle Proximity ........................ 10-9 Displaying Terrain and Obstacles on the Terrain Proximity Page .......................................................... 10-9 Displaying Terrain and Obstacles on the Navigation Map.......................................................................... 10-9 10.7 Terrain Awareness & Warning System (TAWS) Display (Optional) ................................ 10-10 Displaying Terrain on the TAWS Page .......................
TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide.
SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS 1 2 3 5 4 17 6 7 8 9 Figure 1-1 PFD/MFD Controls 18 10 14 19 24 11 15 20 25 12 16 21 26 22 27 23 28 13 MFD Only 1-2 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. 1 NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies.
SECTION 1 SYSTEM OVERVIEW G1000 displays a list that is too long for the display screen, a scroll bar appears along the right 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 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.
SECTION 1 SYSTEM OVERVIEW 1.2 GCU 476 CONTROLS The indicators above the PFD, MFD, NAV, and COM Keys are lit when the respective control mode key is pressed. The unit is in MFD Control Mode by default, until the PFD Control Mode selection key is pressed. Many of the controls duplicate the controls on the PFD and MFD. The discussions later in this manual are centered around using the controls on the PFD and/or MFD.
SECTION 1 SYSTEM OVERVIEW 1-6 9 ENT Key – Validates or confirms a menu selection or data entry. 10 CLR Key – Erases information, cancels entries, or removes page menus. Press and hold to immediately display the Navigation Map Page. 11 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box (light blue box around the softkey label) to the right and left, respectively. 12 Decimal Key – Enters a decimal point.
SECTION 1 SYSTEM OVERVIEW 1.3 PFD SOFTKEYS Softkey ON Softkey OFF Figure 1-3 PFD Top Level Softkeys ALERTS STRMSCP ALERTS Press the BACK or OFF Softkey to return to the top-level softkeys. Figure 1-4 INSET Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey.
SECTION 1 SYSTEM OVERVIEW ALERTS ALT UNIT HSI FRMT BRG1 (NAV1) BRG2 (NAV2) BRG1 (GPS) BRG2 (GPS) BRG1 (OFF) BRG2 (OFF) 360 HSI ALERTS Press the STD BARO or BACK Softkey to return to the top-level softkeys ARC HSI ALERTS ALERTS METERS IN HPA ALERTS Figure 1-5 PFD Configuration Softkeys PFD – Press to display the additional softkeys for additional configuration of the PFD. DFLTS – Press to reset default settings on the PFD. WIND – Displays softkeys to select wind data parameters.
SECTION 1 SYSTEM OVERVIEW ALT UNIT – Displays softkeys for setting the altimeter and BARO settings to metric units: METERS – When enabled, displays altimeter in meters. IN – Press to display the BARO setting as inches of mercury. HPA – Press to display the BARO setting as hectopacals. STD BARO – Press to set the barometric pressure to standard pressure. BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window.
SECTION 1 SYSTEM OVERVIEW 1.4 MFD SOFTKEYS SYSTEM – Selecting this softkey makes available the Engine Display functions. Refer to the Engine Indication System section. MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Traffic on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map. TERRAIN – Pressing this softkey displays/removes terrain and obstacle data on the Navigation Map.
SECTION 1 SYSTEM OVERVIEW 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. CHKLIST (checklist)(optional) – Pressing the CHKLIST Softkey displays the Checklist Page. SYSTEM – Displays engine softkeys. DONE – Pressing this softkey checks off a checklist item.
SECTION 1 SYSTEM OVERVIEW 1.6 VERTICAL NAVIGATION In WAAS capable installations, one of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance for a WAAS approach. Baro corrected altitude is used when vertical guidance is given in all other situations and in non-WAAS systems. The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation.
SECTION 1 SYSTEM OVERVIEW White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical speed and deviation guidance.
SECTION 1 SYSTEM OVERVIEW 1.7 BACKLIGHTING 1.8 When system power is turned off, all manual backlighting settings will return to the factory default settings. Manually adjust the backlight for the PFD and MFD: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. 2) Press the small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the small FMS Knob to display the selection window. 4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key.
SECTION 1 SYSTEM OVERVIEW 1) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of the PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. Figure 1-13 Database Update Confirmation 4) After the update completes, the PFD starts in normal mode. 2) Apply power to the G1000 System. View the MFD power-up splash screen.
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SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated. The gradient color background shown in the following illustrations, is used in WAAS capable systems.
SECTION 2 FLIGHT INSTRUMENTS 13 12 1 2 11 3 10 4 9 5 8 6 7 1 Traffic Annunciation 6 Bearing Information Windows 11 Vertical Deviation/Glideslope Indicator 2 Vspeed References 7 Selected Course 12 Marker Beacon Annunciation 3 Selected Heading 8 Alerts Window 13 AFCS Status Annunciation 4 Wind Data 9 Barometric Minimum Descent Altitude 5 Inset Map 10 Annunciation Window Figure 2-2 Additional PFD Information Active Flight Plan Leg Distance to Next Waypoint Bearing to Next W
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Airspeed Trend Vector Airspeed Trend Vector Vspeed References Actual Airspeed Speed Ranges True Airspeed The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Vspeed References Vspeed References are turned on or off in the Timer/References Window. Select the TMR/REF Softkey to display the widow.
SECTION 2 FLIGHT INSTRUMENTS 2.2 2.3 ATTITUDE INDICATOR The Slip/Skid Indicator is located under the Roll Pointer and moves laterally away from the pointer to indicate lateral acceleration. One Slip/Skid indicator displacement is equal to one ball displacement when compared to a traditional slip/skid indicator.
SECTION 2 FLIGHT INSTRUMENTS Barometric Setting Box Metric Display Select barometric pressure: Turn the BARO Knob to select the desired setting. Quickly enter standard pressure: 1) Press the PFD Softkey. 2) Press the STD BARO Softkey. Altitude Alerting Within 1000 ft Within 200 ft Deviation of ±200 ft Figure 2-8 Altitude Alerting Visual Annunciations Display altitude in meters and barometric pressure in hectopascals: 1) Press the PFD Softkey to display the second level softkeys.
SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation (WAAS Only) NOTE: The LOW ALT annunciation is not available when the G1000 is configured with TAWS (Terrain Awareness & Warning System), unless TAWS is inhibited. When the Final Approach Fix (FAF) is the active waypoint in a GPS WAAS approach using vertical guidance, a LOW ALT (Low Altitude) annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAF. The annunciation initially flashes.
SECTION 2 FLIGHT INSTRUMENTS 2.5 MARKER BEACON ANNUNCIATIONS Outer Marker Middle Marker Inner Marker Glidepath Indicator Altimeter Figure 2-14 Marker Beacon Annunciations Figure 2-12 Glidepath Indicator 2.6 VERTICAL SPEED INDICATOR The Glideslope Indicator appears when an ILS is tuned in the active NAV receiver field (see Figure 2-13).
SECTION 2 FLIGHT INSTRUMENTS 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 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 2.8 HORIZONTAL SITUATION INDICATOR (HSI) 14 NOTE: When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled.
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 (Oceanic if >200 nm from nearest airport) Terminal Refer to accompanying approach CDI scaling figures 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 Missed Approach Approach Drawing not to scale CDI scale is set to the smaller of 0.3 nm or an angle set by the system Bearing Pointers and Information Windows angle set by system 350 ft 0.3 nm 1.
SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source Waypoint Identifier Bearing Pointer Source Icon Figure 2-27 BRG1 Information Window • WARN – GPS detects a position error. • 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.
SECTION 2 FLIGHT INSTRUMENTS 2.9 WIND DATA 2.10 GENERIC TIMER When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”.
SECTION 2 FLIGHT INSTRUMENTS Blank Page 2-14 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) The Engine Instrument Display is displayed on the left side of the MFD.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.1 Trim EIS DISPLAY Selecting the SYSTEM Softkey on the MFD acesses the Engine Indication System (EIS) Display. For all instruments, green indicates the acceptable operating range; yellow and red indicate caution and warning, respectively. Oxygen System (Optional) Selecting the OXYGEN Softkey on the MFD turns the oxygen system on or off. If no oxygen system is installed, the oxygen gauges will be blank.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 ENGINE LEANING ASSIST DISPLAY Engine Leaning for the Cessna 350 NOTE: The Cessna 350 Airplane Flight Manual (AFM) supersedes information found in this section. Leaning for Best Power 3) Lean the mixture until one of the cylinder’s exhuast temperature peaks. This is indicated by ‘1st’ being displayed below the first cylinder to peak. A bar is also displayed at that point on that cylinder’s bar graph. See Figure 3-3.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Leaning for Best Economy 1) Select the SYSTEM Softkey. 2) Select the ASSIST Softkey. 3) Lean the mixture until one of the cylinder’s exhuast temperature peaks. This is indicated by ‘1st’ being displayed below the first cylinder to peak. See Figure 3-3. 5) Monitor the � Peak temperature and continue leaning the mixture until reaching the value indicated in the Cessna Airplane Flight Manual (AFM). Selecting the ASSIST Softkey returns the MFD to the EIS Display.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Engine Leaning for the Cessna 400 NOTE: The Cessna 400 Airplane Flight Manual (AFM) supersedes information found in this section. 4) Richen the mixture to obtain the desired delta (�) values as specified in the AFM. Leaning for Best Economy 1) Select the SYSTEM Softkey. 2) Select the ASSIST Softkey. Leaning for Best Power 1) Select the SYSTEM Softkey. 2) Select the ASSIST Softkey. 3) Lean the mixture to obtain peak temperature on the TIT displays. See Figure 3-5.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 FUEL CALCULATIONS Fuel Quantity Gauge (Left) Indicates Selected Fuel Tank Fuel Quantity Gauge (Right) Fuel Remaining Fuel Used Calculation Endurance Calculation Range Calculation Figure 3-6 EIS Display - Fuel Calculations Group Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all calculated based on the last manual adjustment of the fuel remaining (GAL USED). Measured fuel quantity has no effect on fuel calculations.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes are located on the Primary Flight Display and the MultiFunction Display in the same locations. Operations in the following discussions may also be performed with the corresponding controls on the MFD/PFD Control Unit. NAV Controls NAV Frequency Box COM Frequency Box COM Controls Figure 4-1 G1000 VHF NAV/COM Controls (PFD) 190-00567-01 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Standby COM Frequency Field Tuning Box Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 TRANSPONDER Manual ON Mode Mode Selection The STBY, ON, ALT, GND, VFR, CODE, and IDENT Softkeys can be accessed by pressing the XPDR Softkey. Press the ON Softkey. ON Mode generates Mode A and Mode S replies, but Mode C altitude reporting is inhibited. ON Mode (No Altitude Reporting) Ground Mode (Automatic or Manual) GND is displayed when the aircraft is on the ground or when the GND Softkey is pressed.
SECTION 4 – NAV/COM & TRANSPONDER Code Selection 5) Turn the small FMS Knob to enter the second two digits. VFR Code Selection 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 6) Press the ENT Key to activate the code immediately, or wait 10 seconds and the code will become active. 2) Press the VFR Softkey to enter the VFR code. Pressing the VFR Softkey again restores the previous identification code. NOTE: The pre-programmed VFR Code is set at the factory to 1200.
SECTION 4 – NAV/COM & TRANSPONDER Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Split COM Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (DME, ADF, & AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Audio Panel Controls
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 Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-6 Navigation Radios Figure 5-5 Marker Beacon 5.4 5.5 NAV RADIO AUDIO SELECTION Pressing NAV1 or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These two keys can be selected individually or together.
SECTION 5 – AUDIO PANEL 5.6 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 6.1 AFCS CONTROLS The following dedicated AFCS keys are located on the bezels of the MFD: the CWS button will activate the flight director in the default pitch and roll hold modes. • GA (Go Around) Button —Located on the instrument panel, the Go Around Button disengages the autopilot and selects the Go Around (wings level) mode. • MET (Manual Electric Trim) Switch — This switch is used to operate manual electric pitch trim.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Active Mode Autopilot Status Armed Mode Roll Axis Modes Mode Reference Armed Mode Active Mode AFCS Status Box Pitch Axis Modes Selected Altitude Box Aircraft Attitude Symbol Flight Director Command Bars Figure 6-2 PFD AFCS Display Command Bars AFCS Status Box Upon activation of the flight director, Command Bars are displayed on the PFD as a single cue.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 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). In the absence of specific mode selection, the flight director reverts to the default pitch and/or roll mode(s). Armed modes are annunciated in white and active in green in the AFCS Status Box.
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 (see the discussion on Vertical Navigation Modes later in this section).
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 Command Bars Indicate Climb to Attain Vertical Speed Vertical Speed Reference Bug 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 But
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 Roll Modes Go Around (GA) Mode Pushing the GO AROUND button 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 both a 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.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Table 6-2 relates each roll mode to its respective control and annunciation. Refer to the pitch modes section for information regarding Go Around Mode. The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach modes. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS Button.
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. 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).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, BC) 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. Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source on the HSI (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected navigation source.
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 6.4 AUTOPILOT OPERATION NOTE: Refer to the AFM for specific instructions regarding emergency procedures. The autopilot operates flight control surface servos to provide automatic flight control. Pitch and roll commands are provided to the servos, based on the active flight director modes. The autopilot uses pitch and roll rates to stabilize the aircraft attitude during upsets and flight director maneuvers.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Disengaging the Autopilot Automatic disengagement occurs due to: • System failure • Inability to compute default flight director modes (FD also disengages automatically) • Invalid sensor data Automatic autopilot disengagement is indicated by a flashing red ‘AP’ annunciation and by the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC or MET Switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.5 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in this section are for instructional purposes only and should not be used for navigation. This section provides a scenario-based set of procedures showing various GFC 700 AFCS modes used while following a previously entered flight plan. The following example closely follows the example flight plan discussed in the GPS Navigation section.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure c) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode. Climbing to the Selected Altitude and flying an assigned heading: 1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob. 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). a) Adjust the vertical speed to the desired value.
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 2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS Navigation Mode, course changes defined by the flight plan are automatically made without pilot action required. NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level).
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 coupled VNAV: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT Knob, set the Selected Altitude at least 75 feet below the flight plan’s VNV Target Altitude of 10,000 feet.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Non-path descent using Flight Level Change Mode: The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 1) Command a non-path descent using Flight Level Change Mode: a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach KCOS Flying an ILS approach: PETEY 2 G HD M e od PYNON 1 GPS NAV Mode 2) Arm LOC Approach and Glideslope modes. a) Ensure the appropriate localizer frequency is tuned. b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. 3 LOC APR/ GS Mode 1) Transition from GPS Navigation Mode to Heading Select Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a WAAS precision approach: 2) Press the APR Key once clearance for approach has been acquired. GPS Approach Mode is activated and Glidepath Mode is armed. 4 CEGIX 3 GPS APR/ GP Mode 1) Arm flight director modes for a precision approach: a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around/Missed Approach Flying a missed approach: 1) Push the GA Switch at the Decision height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing yellow for 5 seconds and the autopilot disconnect aural alert.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Annunciation AFCS Status Alerts The annunciations in Table 6-4 (listed in order of increasing priority) can appear on the PFDs 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 While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director and pitch commands are limited for overspeed protection. Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 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. Select the MAP Page Group 1) Turn the large FMS Knob until ‘MAP’ is highlighted in the page group box in the lower right of the MFD display.
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 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 See the Procedures section for loading departures and arrivals. Note the magenta arrow in Figure 7-11 indicating the active departure leg. 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. After takeoff, ATC assigns a heading of 240º. 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.
SECTION 7 – NAVIGATION 4) V4 will now be entered into the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight the desired entry point as shown in Figure 7-13. The V4 entry will be placed immediately above the highlighted waypoint. Figure 7-14 Entering V4 Entry Point d) Press the ENT Key. TOP is now inserted into the flight plan as in Figure 7-15.
SECTION 7 – NAVIGATION f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as seen in Figure 7-17. j) Press the ENT Key. The selected airway and exit are displayed the prompt “LOAD?” highlighted as in Figure 7-18. Figure 7-16 List of Available Airways for TOP g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 7-16.
SECTION 7 – NAVIGATION remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed to 2.0 nm. Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 will now be made the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg.
SECTION 7 – NAVIGATION 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 7-22. 8) At SLN, Victor Airway 244 (V244) will be intercepted. Turn prompts will be displayed in the PFD Navigation Status Box as seen in Figure 7-23. Figure 7-23 Turn to Intercept V244 9) As seen in Figure 7-24, V244 is now the active flight plan leg.
SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 will be intercepted. See Figure 7-25. Figure 7-26 Direct To OPSHN Figure 7-25 HYS to LAA Leg Active d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7-27. 11) ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and issues a crossing altitude restriction of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor.
SECTION 7 – NAVIGATION f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database, those altitudes will be displayed as white numerals. This indicates the altitudes will not be used by the system for vertical guidance until manually accepted by the pilot. To accept the displayed altitude, place the cursor over the altitude and press the ENT Key.
SECTION 7 – NAVIGATION b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7-31. e) Press the ENT Key. A list of available transitions for the selected approach is displayed as shown on Figure 7-32. Figure 7-30 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport will be displayed as in Figure 7-31.
SECTION 7 – NAVIGATION h) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values will always be displayed as white text, as in Figure 7-34.
SECTION 7 – NAVIGATION a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 7-35. b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to enter the desired value. 15) As seen in Figure 7-36, the aircraft is approaching TOD. Note the target vertical speed required to reach the selected altitude.
SECTION 7 – NAVIGATION 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-38. Keep Vertical Deviation Pointer Centered 18) The aircraft is approaching OPSHN. The upcoming turn and next heading will be annunciated at the top left of the PFD as seen in Figure 7-40. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
SECTION 7 – NAVIGATION 19) After passing OPSHN, the next leg of the arrival will turn magenta as shown in Figure 7-41. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-41 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 7-42).
SECTION 7 – NAVIGATION 21) Upon passing PYNON the approach procedure will automatically become active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-43). 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
SECTION 7 – NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-46) when the final approach course becomes active.
SECTION 7 – NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368FT’) is not part of the published procedure. It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach is exceeded.
SECTION 7 – NAVIGATION 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern will be established at the MAHP (MOGAL) as shown in Figure 7-49. 7.4 AIRPORT INFORMATION Figure 7-53 Airport Information Page Figure 7-49 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 750. Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION 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. Figure 7-54 Flight Plan Airport List 3) Turn the small FMS Knob to the right to display the ‘RECENT’ airports as shown in Figure 7-56. 3) Turn the large FMS Knob to select the desired airport. 4) Press the ENT Key.
SECTION 7 – NAVIGATION Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport. Continue turning the small FMS Knob to select the desired runway. 7.
SECTION 7 – NAVIGATION 7.6 NDB INFORMATION Figure 7-58 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 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 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the flashing cursor. Access Runway Information for the Selected Airport 1) With the Nearest Airports Page displayed, press the RNWY Softkey to place the cursor in the ‘RUNWAYS’ field.
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 7-63 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 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. The remaining information on the Nearest NDB Page pertains to the selected NDB.
SECTION 7 – NAVIGATION 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. 2) Turn the small FMS Knob to select the fifth rectangular page icon. Select a Nearest User Waypoint 7-28 3) Press the FMS Knob to remove the flashing cursor. 7.
SECTION 7 – NAVIGATION 7.15 NEAREST AIRSPACES View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor. 2) Turn either 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. 4) Turn either FMS Knob to select the desired airspace. 5) Press the FMS Knob to remove the flashing cursor.
SECTION 7 – NAVIGATION Blank Page 7-30 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS 4) Repeat steps 2 and 3 until the desired name is entered. 5) Press the ENT Key. 6) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be modified by changing the reference waypoint. Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint.
SECTION 8 – FLIGHT PLANNING 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. The first reference waypoint field is highlighted. 8.3 ACTIVATE A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
SECTION 8 – FLIGHT PLANNING step must be used when activating a leg from the PFD. 3) With ‘Activate’ highlighted, press the ENT Key. 2) Turn the large FMS Knob to highlight ‘Invert Flight Plan’ and press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location. 3) With ‘OK’ highlighted, press the ENT Key to invert the flight plan. Figure 8-5 Activate Flight Plan Leg Confirmation 8.
SECTION 8 – FLIGHT PLANNING 4) Turn the small FMS Knob to the right enter the first character of the identifier of the departure airport. Turning the knob to the left will access the FPL, NRST, and RECENT waypoint list. 4) Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint. 5) Turn the large FMS Knob to move the cursor to the next character field. Repeat steps 4 and 5 until the desired identifier has been entered.
SECTION 8 – FLIGHT PLANNING 4) Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired airways entry point. 6) Turn the small FMS Knob to display the Waypoint Information Window. Figure 8-16 Display Waypoint Information Window Figure 8-14 Load Airway Entry Point 5) When the desired entry point is entered, press the ENT Key. 7) Press the LD AIRWY Softkey. A list of available airways is now displayed.
SECTION 8 – FLIGHT PLANNING 10) Turn either FMS Knob to highlight the desired exit point. 8.11 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures. 8.12 REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT PLAN 1) With the Active or Stored Flight Plan Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the title for the approach, departure, arrival, or airway to be deleted.
SECTION 8 – FLIGHT PLANNING flight plan and press the EDIT Softkey. 4) Turn the large FMS Knob to place the cursor in the desired locations for entering changes. 5) Turn the FMS Knobs to make the desired changes, then press the ENT Key. 6) Press the FMS Knob to return to the Flight Plan Catalog Page. 8.15 DELETE A WAYPOINT FROM THE FLIGHT PLAN 1) With either the Active or Stored Flight Plan displayed, press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING 8.19 GRAPHICAL FLIGHT PLAN CREATION Starting WPT Ending WPT 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the Joystick to activate the map pointer. Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan. 3) Press the LD WPT Softkey. The selected waypoint will be inserted at the end of the flight plan. The default user waypoint naming is USR000, USR001, USR002 and so on.
SECTION 8 – FLIGHT PLANNING FMS Knob to select the desired flight plan (already stored in memory), by number. Turn the large FMS Knob to highlight the ‘LEG’ field and turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ will display an active flight plan. If an active flight plan is selected, ‘REM’ will be an available option to display planning data for the remainder of the flight plan.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) If a flight plan is active, the departure airport 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 9.2 APPROACHES NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. Figure 9-3 Select Arrival 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key.
SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a flight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 7) The cursor will move to the TRANSITIONS field.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ or ‘Traffic’ group 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.
SECTION 10 – HAZARD AVOIDANCE Change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. Displaying METAR and TAF information on the Airport Information Page Display METAR and TAF text on the Airport Information Page: 2) Select the VIEW Softkey. The 360 and ARC Softkeys are displayed. Select the 360 Softkey to display a 360˚ viewing area or select the ARC Softkey to display a 120˚ viewing area. 1) Turn the large FMS Knob to select the WPT Page Group.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on 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 Weather Data Link Page. 3) Select the available softkeys to select the desired XM weather product. 4) Select 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 Softkey to return to the map.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Selecting 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 – Selecting the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Select 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 Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols • • • • • • City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Weather Product 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.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range NOTE: If the G1000 is configured to use the optional Ryan 9900BX Traffic Advisory System, TIS will not be available for use. NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
SECTION 10 – HAZARD AVOIDANCE 10.5 RYAN® 9900BX TRAFFIC ADVISORY SYSTEM (TAS) (OPTIONAL) Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Refer to the Ryan 9900BX pilot’s guide for a detailed discussion and an explanation of the aural alerts. Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. ‘OPERATING’ is displayed in the Traffic Mode field.
SECTION 10 – HAZARD AVOIDANCE 4) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Traffic Advisory Non-Bearing Traffic Off Scale Traffic Advisories Banner Non-Threat Traffic Figure 10-13 TAS Traffic on Navigation Map 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
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 10-15 Obstacle Symbols 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Red Terrain/Obstacle above 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. Potential Impact Point Projected Flight Path 100' Threshold Unlighted Obstacle 1000' Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key.
SECTION 10 – HAZARD AVOIDANCE 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS’. 3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center of the TAWS Page. When all is in working order, “TAWS System Test, OK” will be heard.
The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 10-19 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up).
SECTION 10 – HAZARD AVOIDANCE Pop-up Alerts Alert Annunciations When the Navigation Map Page is displayed, and a terrain or obstacle alert is issued, a pop-up window is displayed with the appropriate alert. Alert Annunciation Figure 10-24 Alert Annunciation on the TAWS Page Alert Annunciation Figure 10-22 Alert Pop-Up Press the ENT Key to display the TAWS Page, or press the CLR Key to remain on the Navigation Map Page.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” 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 NOTE: Dead Reckoning Mode will only function in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution will produce a “NO GPS POSITION” annunciation on the map and the G1000 will stop navigating in GPS Mode. DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in Figure 11-4.
SECTION 11 – ABNORMAL OPERATION Blank Page 11-4 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Airplane Flight Manual supersedes information found in this document. System Annunciation Red ‘X’ Annunciation Window Alerts Window Figure 12-1 G1000 Alerting System ALERTS Softkey Annunciation 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.
SECTION 12 – ANNUNCIATIONS & ALERTS • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. Figure 12-2 WARNING Softkey Annunciation 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Cessna 350/400 aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS See the Airplane Flight Manual for information regarding pilot responses.
SECTION 12 – ANNUNCIATIONS & ALERTS Annunciation Advisory Annunciation Window Text OXYGEN ON SPEED BRAKES Alerts Window Message Reminder: Turn off oxygen Speed brakes are active Audio Alert None None Message Advisory Alerts Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. AVIONICS FAN – The cooling fan for remote avionics is inoperative. TIMER ZERO – Timer has counted down to zero.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.5 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations 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 Availble” will be heard when sufficient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
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 A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs. GIA 63 Integrated Avionics Units GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS Or GMU 44 Magnetometer GEA 71 Engine Airframe Unit Or GIA 63 Integrated Avionics Unit GIA 63 Integrated Avionics Units GDC 74A Air Data Computer Figure 12-6 G1000 System Failure Annunciations 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 config error. Config service req’d. MFD1 CONFIG – MFD1 config error.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Message MFD1 DB ERR – MFD1 aviation database error exists. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. MFD1 DB ERR – MFD1 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. DB MISMATCH – Terrain database type mismatch. DB MISMATCH – Obstacle database version mismatch. DB MISMATCH – Airport Terrain database mismatch. Comments The PFD and MFD have different aviation database versions installed. Crossfill is off.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories Message Comments GIA1 CONFIG – GIA1 config 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 config 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. GIA2 CONFIG – GIA2 audio config error.
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 Message GIA1 CONFIG – GIA1 configuration error. Config service req’d. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced. GDL 69A Message Advisories Message GDL69 CONFIG – GDL 69 config error.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Parallel track unavailable: bad geometry PTK FAIL – Parallel track unavailable: invalid leg type. PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. VNV – Unavailable. Unsupported leg type in flight plan. VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable.
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-2 Active flight plan 8-2 ADVISORY 12-1 Advisory alerts 12-4 AFCS 1-3, 6-1, 6-2, 6-23, 12-5 AFCS Status Box 2-1 Age 10-6 AHRS 12-19, 12-20 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-25 Airport information 7-21 Airspace alerts 7-29 Airspeed Indicator 2-1 Airspeed indicator 2-3 Airspeed Reference 6-8 Airspeed trend vector 2-3 Airways 8-5 Alerting System 12-1 Alerts 12-1 Alerts Window 2-2 Alert levels 12-2 Alert Pop-Up 10-14 ALT 1-4, 1-9, 6-4,
INDEX Flight Plan Catalog 9-1, 9-2 FLTA 10-12 Forward Looking Terrain Avoidance 10-12 Freezing level 10-5 Frequency toggle key 1-3, 4-3 Fuel remaining 3-6 Fuel used 3-6 G GA 6-1 Glidepath 2-6, 7-19 Glidepath Mode 6-14, 6-20 Glidepath Mode (GP) 6-31 Glideslope 2-6, 2-7, 7-19 Glideslope Indicator 2-2 Glideslope Mode 6-15, 6-20, 6-30 GMA 1347 1-1 Go Around 6-1 Go Around Mode 6-32–6-33 Go Around Mode (GA) 6-16 H Heading 2-1 Heading indication 2-10 Heading Select 1-3, 1-4 Heading Select Mode 6-18 Heading Selec
INDEX R Remove departure, arrival, or approach 8-6 Replies 4-4 Required Vertical Speed 2-6, 7-15 Required Vertical Speed Indicator 7-15 Reversionary mode 11-1 ROC 10-12, 10-15, 12-6 Roll Axis Modes 6-2 Roll Hold Mode (ROL) 6-17 Roll modes, flight director 6-16–6-19 Roll Reference 6-17 RTC 10-12 RVSI 7-15, 7-16 RX indicator 4-3 R indication 4-4 S Secure Digital (SD) card 1-14 Selected Altitude 2-1, 6-6, 6-10, 6-13 Selected Altitude Bug 2-1 Selected Altitude Capture Mode 6-6, 6-10, 6-13 Selected Course 2-2, 6
INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Cessna 350/400 190-00567-01 Rev.
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 Liberty House, Bulls Copse Road Hounsdown Business Park Southampton, SO40 9RB, 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 190-00567-01 Rev.
