G1000 ® Integrated Flight Deck Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown 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:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Cessna Citation Mustang Garmin AT, Inc.
SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATING & CREW ALERTING SYSTEM AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES APPENDICES INDEX
Copyright © 2006-2008 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0435.11 or later for the Cessna Citation Mustang. 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., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Limited Warranty LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost.
Warnings, Cautions, and Notes WARNING: The G1000 TAWS feature does not relieve the pilot from the responsibility of being aware of surroundings during flight. The TAWS feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
Warnings, Cautions, and Notes WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.
Warnings, Cautions, and Notes NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65.
Revision Information Record of Revisions Part Number 190-00494-00 Revision Date A October, 2006 B November, 2006 Page Range i through I-6 4-7, 4-16, 4-34 5-108 through 5-126 7-33 through 7-45 190-00494-01 A B February, 2007 May, 2007 i through I-6 i through I-6 190-00494-02 A April, 2008 i through I-6 B May, 2008 All 190-00494-02 Rev. B Description Production release Added ‘SQ’ and ‘RX’ annunciations. Added transponder code entry using the FMS Knob.
Revision Information Blank Page vi Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Table of Contents 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 Section 1 System Overview System Description.................................................. 1 Line Replaceable Units (LRU).................................. 2 G1000 Controls......................................................... 7 PFD Controls................................................................. 7 Controls Associated With the MFD.................................. 9 AFCS Controls...................................................
Table of Contents 4.4 GTX 33/33D Mode S Transponders..................... 121 Transponder Controls. ............................................... 121 Transponder Mode Selection. ..................................... 122 Entering a Transponder Code...................................... 125 IDENT Function......................................................... 126 Flight ID Reporting.................................................... 127 4.5 Additional Audio Panel Functions......................
Table of Contents 6.3 Terrain Awareness & Warning System (TAWS).. 332 Displaying TAWS Data. .............................................. 333 TAWS Page............................................................... 335 TAWS Alerts.............................................................. 337 System Status........................................................... 344 6.4 Traffic Information Service (TIS)......................... 345 Displaying TRAFFIC Data............................................
Table of Contents Appendices Annunciations and Alerts.............................................. 489 CAS Messages.......................................................... 489 Comparator Annunciations......................................... 490 Reversionary Sensor Annunciations............................. 491 G1000 System Annunciations..................................... 491 G1000 System Message Advisories............................. 494 AFCS Alerts....................................................
System Overview SYSTEM OVERVIEW Section 1 System Overview FLIGHT INSTRUMENTS 1.1 System Description This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna Citation Mustang. The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays.
SYSTEM OVERVIEW System Overview 1.2 Line Replaceable Units (LRU) AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS • GDU 1040A (2) – Each unit is configured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution. The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.
System Overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS • GDC 74B (2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with the on-side GIA 63W, on-side GDU 1040A and on-side GRS 77, using an ARINC 429 digital interface (it also interfaces directly with the on-side GTP 59). The GDC 74B is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace.
SYSTEM OVERVIEW System Overview EICAS FLIGHT INSTRUMENTS • GMA 1347D (2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with the on-side GIA 63W, using an RS-232 digital interface.
System Overview SYSTEM OVERVIEW • GCU 475 (1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital interface. FLIGHT INSTRUMENTS • GMC 710 (1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing communication with both PFDs. EICAS AUDIO PANEL & CNS • GTP 59 (2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview GMC 710 EICAS GWX 68 GDU 1040A (PFD #1) GDL 69A GCU 475 GDU 1040A (PFD #2) GDU 1500 FLIGHT MANAGEMENT AUDIO PANEL & CNS (MFD) GMA 1347D #1 GMA 1347D #2 GMU 44 #1 GMU 44 #2 GRS 77 #1 HAZARD AVOIDANCE GRS 77 #2 AFCS GIA 63W #1 GIA 63W #2 VHF COM VHF NAV/LOC GPS/WAAS G/S GDC 74B #1 AFCS Mode Logic Flight Director Servo Management GTP 59 #1 GDC 74B #2 VHF COM VHF NAV/LOC GPS/WAAS G/S GTP 59 #2 AFCS Mode Logic Flight Director Servo Ma
System Overview SYSTEM OVERVIEW 1.3 G1000 Controls FLIGHT INSTRUMENTS NOTE: The Audio Panel (GMA 1347D) and AFCS controls (GMC 710) are described in the CNS & Audio Panel and AFCS sections respectively. The G1000 system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section.
SYSTEM OVERVIEW System Overview 1 NAV VOL/ID Knob – Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON and OFF. Volume level is shown in the NAV frequency field as a percentage. 2 NAV Frequency Transfer Key – Toggles the standby and active NAV frequencies. 3 Dual NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2.
System Overview SYSTEM OVERVIEW Controls Associated With the MFD FLIGHT INSTRUMENTS The controls for the MFD (GDU 1500) are located on both the MFD bezel and the MFD Control Unit (GCU 475). The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide documentation.
Joystick – Changes the map range when rotated. Activates the map pointer when pressed. 7 Alphanumeric Keys – Allow the user to enter data quickly, without having to select individual characters with the FMS Knob. 8 Plus (+) Minus (-) Key – Toggles a (+) or (-) character. 9 Decimal Key – Enters a decimal point. 10 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box to the right and left, respectively.
System Overview FLC Key – Selects/deselects Flight Level Change Mode. 9 CRS2 Knob – Sets the copilot-selected course on the HSI of PFD2 when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The copilot-selected course provides course reference to the copilot-side flight director when operating in Navigation and Approach modes. 10 SPD Key – Switches the Flight Level Change mode reference speed between IAS and MACH number.
SYSTEM OVERVIEW System Overview AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Audio Panel Controls 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 FLIGHT MANAGEMENT 18 19 20 21 HAZARD AVOIDANCE 17 22 23 24 AFCS Figure 1-5 Audio Panel Controls (GMA 1347D) 1 COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the #1 COM receiver to be heard.
System Overview MUSIC – Not used on the Cessna Citation Mustang. 10 SPKR – Pressing this key selects and deselects the corresponding cockpit speaker. COM and NAV receiver audio will be heard on the speaker. 11 MKR/MUTE – Mutes the currently received marker beacon receiver audio. Unmutes when new marker beacon audio is received. 12 HI SENS – Press to increase Marker Beacon Receiver sensitivity. Press again to return to normal. 13 DME – Pressing turns DME audio on or off.
SYSTEM OVERVIEW System Overview 1.4 Secure Digital Cards FLIGHT INSTRUMENTS NOTE: Refer to the Appendices for instructions on updating the aviation database. NOTE: Ensure that the G1000 system is powered off before inserting the SD card. EICAS The GDU 1040A and GDU 1500 data card slots use Secure Digital (SD) cards and are located on the top right portion of the display bezels. Each display bezel is equipped with two SD card slots.
System Overview SYSTEM OVERVIEW NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. FLIGHT INSTRUMENTS The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical busses.
SYSTEM OVERVIEW System Overview 1.6 System Operation FLIGHT INSTRUMENTS The displays are connected together via a single Ethernet bus, thus allowing for high-speed communication. As shown in Figure 1-1, each GIA 63W is connected to the on-side PFD. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the G1000 system.
System Overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS EICAS Figure 1-10 Reversionary Mode (Manual) AUDIO PANEL & CNS If the system detects a failure in PFD1, reversionary mode is entered automatically. Reversionary mode must be entered manually in the case of PFD2 or MFD failure. FLIGHT MANAGEMENT Reversionary mode is manually activated by pressing the dedicated DISPLAY BACKUP button at the bottom of the audio panel (see Figure 1-11 and refer to the Audio Panel section for further details).
SYSTEM OVERVIEW System Overview Note: Aggressive maneuvering in any of the three reversionary modes listed in Table 1-1 can degrade AHRS accuracy.
System Overview SYSTEM OVERVIEW fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer inputs are available and valid. Air Data Input Failure FLIGHT INSTRUMENTS A failure of the air data input has no effect on AHRS output while AHRS is operating in normal mode. A failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid attitude and heading information on the PFD (as indicated by red “X” flags).
SYSTEM OVERVIEW System Overview Softkey Function FLIGHT INSTRUMENTS The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background.
System Overview XM LTNG PFD ADDITIONAL FEATURES BRG2 AFCS BRG1 HAZARD AVOIDANCE WIND FLIGHT MANAGEMENT DFLTS AUDIO PANEL & CNS SYN VIS EICAS ADC1 ADC2 AHRS1 AHRS2 FLIGHT INSTRUMENTS SENSOR APPENDICES Displays softkeys for setting the altimeter and BARO settings to metric units ALT UNIT 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 INDEX STD BARO 190-00494-02 Rev.
SYSTEM OVERVIEW System Overview OBS FLIGHT INSTRUMENTS CDI ADF/DME XPDR EICAS XPDR1 XPDR2 STBY AUDIO PANEL & CNS ON ALT FLIGHT MANAGEMENT GND HAZARD AVOIDANCE VFR CODE 0—7 BKSP IDENT APPENDICES ADDITIONAL FEATURES AFCS TMR/REF NRST MSG Selects OBS mode on the CDI when navigating by GPS (only available with active leg) Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI Displays the ADF/DME Tuning Window, allowing tuning of the ADF, ADF Mode selection, ADF volume control, and selec
System Overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS TRFC-1 Select the BACK or OFF Softkey to return to the top-level softkeys. TRFC-2 EICAS Figure 1-17 INSET Softkeys AUDIO PANEL & CNS ADC1 ADC2 AHRS1 BACK AHRS2 MSG FLIGHT MANAGEMENT Press the BACK Softkey to return to the top level softkeys.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview MSG Press the BACK Softkey to return to the top-level softkeys. EICAS MSG AUDIO PANEL & CNS Press the BACK Softkey to return to the top-level softkeys.
System Overview CAS ↓ DCLTR MAP (optional) (optional) SHW CHRT CHKLIST SYSTEM OVERVIEW CAS ↑ DCLTR-1 FLIGHT INSTRUMENTS DCLTR-2 DCLTR-3 Select the BACK Softkey on this level to return to the top softkey level.
SYSTEM OVERVIEW System Overview Selecting the GPS receiver for which data may be reviewed 1) Use the FMS Knob to select the AUX - GPS Status Page. FLIGHT INSTRUMENTS 2) To change the selected GPS receiver: a) Select the desired GPS Softkey. Or: a) Press the MENU Key. EICAS b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key.
System Overview SYSTEM OVERVIEW Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status FLIGHT INSTRUMENTS The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM).
SYSTEM OVERVIEW System Overview Predicting RAIM availability 1) Select the GPS Status Page. FLIGHT INSTRUMENTS 2) If necessary, select the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the desired waypoint: EICAS a) Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer to Section 1.
System Overview • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date SYSTEM OVERVIEW FLIGHT INSTRUMENTS • SBAS Selection (SBAS Softkey is selected)(WAAS capable systems only) In certain situations, such as when the aircraft is outside or on the fringe of the WAAS coverage area, it may be desireable to disable WAAS (although it is not recommended).
SYSTEM OVERVIEW System Overview 3) Press the ENT Key to select the desired option. FLIGHT INSTRUMENTS 4) The CLR Key may be pressed to remove the menu and cancel the operation. Pressing the FMS Knob also removes the displayed menu.
System Overview SYSTEM OVERVIEW There are also several pages (Airport Information and XM Information pages) which are selected first from within a main page group with the FMS Knobs, then with the appropriate softkey at the bottom of the page. In this case, the page remains set to the selected screen until a different screen softkey is selected.
SYSTEM OVERVIEW System Overview Auxiliary Pages (AUX) FLIGHT INSTRUMENTS Weight Planning Trip Planning Utility GPS Status EICAS System Setup XM Satellite pages XM Satellite Pages AUDIO PANEL & CNS - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) System Status HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 1-28 Auxiliary Pages Nearest Pages (NRST) Nearest Airports Nearest Intersections AFCS Nearest NDB Nearest VOR ADDITIONAL FEATURES Nearest User Waypoints Nearest Frequencies APPENDIC
System Overview SYSTEM OVERVIEW The Flight Plan Pages are accessed using the FPL Key on the MFD. Main pages within this group are selected by turning the small FMS Knob.
SYSTEM OVERVIEW System Overview MFD System Pages FLIGHT INSTRUMENTS In the Auxiliary (AUX) Page Group, there are two system pages: System Setup (page 5 of 7) and System Status (page 7 of 7). The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000 system LRUs.
System Overview SYSTEM OVERVIEW Date/Time FLIGHT INSTRUMENTS The Date/Time Box on the System Setup Page displays the current date and time and allows the pilot to set the time format (local 12-hr, local 24-hr, or UTC) and offset. The time offset is used to define current local time. UTC (also called “GMT” or “Zulu”) date and time are calculated directly from the GPS satellites signals and cannot be changed.
SYSTEM OVERVIEW System Overview Airspace Alerts FLIGHT INSTRUMENTS The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the MFD Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace.
System Overview SYSTEM OVERVIEW MFD Data Bar Fields FLIGHT INSTRUMENTS The MFD Data Bar Fields Box on the System Setup Page displays the current configuration of the MFD Navigation Status Box. By default, the Navigation Status Bar is set to display ground speed (GS), desired track (DTK), track (TRK), and estimated time enroute (ETE). To change the information shown in an MFD Navigation Status Bar field: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
SYSTEM OVERVIEW System Overview To change the ILS CDI capture setting: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to highlight the ILS CDI capture field in the GPS CDI Box. 3) Turn the small FMS Knob to select the desired mode and press the ENT Key. COM Configuration NOTE: 8.33 kHz VHF communication frequency channel spacing is not approved for use in the United States. EICAS Select the 25.
System Overview SYSTEM OVERVIEW System Status Page FLIGHT INSTRUMENTS The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and a Cessna service center or Garmin dealer informed.
SYSTEM OVERVIEW System Overview Utility Page HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS For flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the AUX - Utility Page. The timers available include a stopwatch-like generic timer, a total time in flight timer, and a record of the time of departure. Trip statistics—odometer, trip odometer, and average trip and maximum groundspeeds— are displayed from the time of the last reset.
System Overview SYSTEM OVERVIEW 5) Turn the large FMS Knob to highlight ‘START?’ and press the ENT Key to start the timer. The field changes to ‘STOP?’. 6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. FLIGHT INSTRUMENTS 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset.
SYSTEM OVERVIEW System Overview Resetting trip statistics readouts 1) Use the FMS Knob to select the AUX - Utility Page. FLIGHT INSTRUMENTS 2) Press the MENU Key.
System Overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 1-35 Manual Display Backlighting Adjustment EICAS 2) Turn the small FMS Knob to display the selection box. Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key. The intensity value becomes highlighted. AUDIO PANEL & CNS 3) Turn the small FMS Knob to select the desired backlighting, then press the ENT Key. 4) Turn the large FMS Knob to highlight ‘AUTO’ to the right of ‘MFD DSPL’ or ‘PFD2 DSPL’, respectively, and repeat steps 2 and 3.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview Blank Page 44 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Flight Instruments SYSTEM OVERVIEW Section 2 Flight Instruments FLIGHT INSTRUMENTS WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup instruments. Note: The Automatic Flight Control System (AFCS) provides additional readouts and bugs on selected flight instruments. Refer to the AFCS Section for details on these bugs and readouts, as they appear on the display during certain AFCS flight director modes.
SYSTEM OVERVIEW Flight Instruments FLIGHT INSTRUMENTS 24 23 22 21 20 1 19 18 2 EICAS 17 AUDIO PANEL & CNS 16 3 15 4 14 5 13 FLIGHT MANAGEMENT 6 12 7 11 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 8 9 10 1 NAV Frequency Box 13 Selected Heading Bug 2 Airspeed Indicator 14 Turn Rate Indicator 3 Mach Number 15 Barometric Altimeter Setting 4 Current Heading 16 Vertical Speed Indicator (VSI) 5 Current Track Indicator 17 Selected Altitude Bug 6 Course De
Flight Instruments SYSTEM OVERVIEW FLIGHT INSTRUMENTS 16 15 14 1 EICAS 13 AUDIO PANEL & CNS 12 2 11 10 4 9 5 8 2 Flap Speed Reference 3 Selected Heading 4 Wind Data 5 Inset Map 6 DME Information Window 7 Bearing Information Windows 8 Timer/References Window Minimum Descent Altitude/ Decision Height 10 Selected Course 9 11 Required Vertical Speed 12 Current Vertical Speed 13 Vertical Deviation Indicator (VDI) 14 Comparator Window 15 VNV Target Altitude 16 AFCS Status
SYSTEM OVERVIEW Flight Instruments 2.1 Flight Instruments FLIGHT INSTRUMENTS Airspeed Indicator Note: Refer to the Airplane Flight Manual (AFM) for speed criteria and Vspeed values. NOTE: VREF cannot be set above the indicated value for VAPR. AUDIO PANEL & CNS EICAS The Airspeed Indicator displays airspeed on a rolling number gauge using a moving tape.
Flight Instruments SYSTEM OVERVIEW Flap extension maximum speed references (for takeoff/approach, TA, and landing, LD, conditions) are displayed as flags to the right of the Airspeed Indicator for altitudes below 18,000 feet. These flags cannot be turned off or modified. The airspeed pointer will turn red upon exceeding these speeds if the flaps are in the corresponding configuration. FLIGHT INSTRUMENTS Vspeeds can be changed and their flags along the right of the airspeed scale turned on/off.
SYSTEM OVERVIEW Flight Instruments Vspeed flags can be turned on or off and values restored all at once or by category (takeoff and landing). Modifying Vspeeds (on, off, restore defaults): FLIGHT INSTRUMENTS 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired selection. 4) Press the ENT Key. AUDIO PANEL & CNS EICAS 5) To remove the window, press the CLR Key or the TMR/REF Softkey.
Flight Instruments SYSTEM OVERVIEW Attitude Indicator Attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The Attitude Indicator displays the pitch, roll, and slip/skid information.
SYSTEM OVERVIEW Flight Instruments FLIGHT INSTRUMENTS The yellow symbolic aircraft on the Attitude Indicator changes appearance based on selection of AFCS flight director Command Bar format (see the AFCS Section for details). Both PFDs show the same Command Bar format and Aircraft Symbol. When the single-cue or the cross-pointer Command Bar format is selected, the Aircraft Symbol appears as shown.
Flight Instruments SYSTEM OVERVIEW Altimeter FLIGHT INSTRUMENTS The Altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge. Numeric labels and major tick marks are shown at intervals of 100 feet. Minor tick marks are at intervals of 20 feet. The indicated altitude is displayed inside the black pointer. The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol.
SYSTEM OVERVIEW Flight Instruments Altitudes can also be displayed in meters (Figure 2-14). Note that the altitude tape does not change scale. Displaying altitude in meters: FLIGHT INSTRUMENTS 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to turn on metric altitude readouts.
Flight Instruments SYSTEM OVERVIEW If the barometric altimeter settings differ between PFDs by more than 0.02 in Hg, the readouts turn yellow (Figure 2-13). The settings can be synchronized from the AUX - System Setup Page on the MFD. Once the settings are synchronized (BARO SYNC turned on), they remain synchronized for the entire flight. FLIGHT INSTRUMENTS Synchronizing the altimeter barometric pressure settings: 1) Use the FMS Knob to select the AUX - System Setup Page.
SYSTEM OVERVIEW Flight Instruments A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing the transition altitude (in either direction). This is displayed by the barometric pressure setting flashing light blue when crossing the transition altitude. FLIGHT INSTRUMENTS Setting the Baro Transition Alert: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor.
Flight Instruments SYSTEM OVERVIEW Vertical Speed Indicator (VSI) FLIGHT INSTRUMENTS The Vertical Speed Indicator (VSI) displays the aircraft vertical speed with numeric labels and tick marks at 2000 and 4000 fpm in each direction on the non-moving tape. Minor tick marks are at intervals of 1000 fpm. The current vertical speed is displayed in the pointer, which also points to that speed on the non-moving tape. Digits appear in the pointer when the climb or descent rate is greater than 100 fpm.
SYSTEM OVERVIEW Flight Instruments Horizontal Situation Indicator (HSI) FLIGHT INSTRUMENTS The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters indicate the cardinal points and numeric labels occur every 30˚. Major tick marks are at 10˚ intervals and minor tick marks at 5˚ intervals. The HSI presents heading, turn rate, course deviation, bearing, and navigation source information in a 360˚ compass-rose format.
Flight Instruments SYSTEM OVERVIEW FLIGHT INSTRUMENTS A digital reading of the current heading appears on top of the HSI. The current track is represented on the HSI by a magenta diamond bug. To the upper left of the HSI, the Selected Heading is shown in light blue; the light blue bug on the compass rose corresponds to the Selected Heading. The Selected Course is shown to the upper right of the HSI.
SYSTEM OVERVIEW Flight Instruments Changing the navigation angle setting: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Nav Angle in the Display Units box. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
Flight Instruments SYSTEM OVERVIEW Turn Rate Indicator FLIGHT INSTRUMENTS The Turn Rate Indicator is located directly above the rotating compass card. 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 6 seconds, based on the present turn rate.
SYSTEM OVERVIEW Flight Instruments • Bearing source (NAV, GPS, ADF) • Pointer icon (single line for BRG1, double line for BRG2) FLIGHT INSTRUMENTS • Frequency (NAV, ADF) • Station/waypoint identifier (NAV, GPS) • GPS-derived great circle distance to bearing source EICAS If the NAV radio is the bearing source and is tuned to an ILS frequency, the bearing pointer is removed from the HSI and the frequency is replaced with ILS.
Flight Instruments SYSTEM OVERVIEW Course Deviation Indicator (CDI) FLIGHT INSTRUMENTS The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not displayed.
SYSTEM OVERVIEW Changing navigation sources: FLIGHT INSTRUMENTS Flight Instruments 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency. 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 3) Press the CDI Softkey a third time to return to GPS.
Flight Instruments SYSTEM OVERVIEW If the same VOR/LOC navigation source is selected on both PFDs, the navigation source annunciation turns yellow on both displays (unless synchronized). Once the CDIs are synchronized (CDI turned on), they remain synchronized for the entire flight. Synchronization setting is maintained through power cycles. FLIGHT INSTRUMENTS Synchronizing the CDIs: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor.
SYSTEM OVERVIEW Flight Instruments GPS CDI Scaling FLIGHT INSTRUMENTS When GPS is the selected navigation source, the flight plan legs are sequenced automatically and annunciations appear on the HSI for the flight phase. Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan is a heading leg, HDG LEG is annunciated in magenta beneath the aircraft symbol.
Enroute (Oceanic if >200 nm from nearest airport) Terminal Approach 0.3 nm 1.0 nm 1.0 nm 2.0 nm 0.3 nm 1.0 nm Terminal Refer to accompanying approach CDI scaling figures FLIGHT INSTRUMENTS Departure SYSTEM OVERVIEW CDI Full-scale Deflection Flight Instruments Missed Approach EICAS Figure 2-30 Automatic CDI Scaling AUDIO PANEL & CNS • Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm). • The system switches from departure to terminal CDI scaling (1.
2 nm FAF CDI scale varies if VTF is activated 0.3 nm 1.0 nm 2 nm FAF EICAS angle based on database information course width angle set by system CDI Full-scale Deflection 0.3 nm 1.0 nm CDI scale is set to the smaller of 0.
Flight Instruments SYSTEM OVERVIEW OBS Mode NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. FLIGHT INSTRUMENTS Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS flight plan (GPS must be the selected navigation source), but retains the current Active-to waypoint as the navigation reference even after passing the waypoint. OBS is annunciated to the lower right of the aircraft symbol when OBS Mode is selected.
SYSTEM OVERVIEW Flight Instruments Enabling/disabling OBS Mode while navigating a GPS flight plan: 1) Press the OBS Softkey to select OBS Mode. FLIGHT INSTRUMENTS 2) Turn a CRS Knob to select the desired course to/from the waypoint. Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to return to automatic waypoint sequencing.
Flight Instruments SYSTEM OVERVIEW 2.2 Supplemental Flight Data FLIGHT INSTRUMENTS Note: Pressing the DFLTS Softkey turns off metric Altimeter display, the Inset Map and wind data display. In addition to the flight instruments, the PFD also displays various supplemental information, including temperatures, wind data, and Vertical Navigation (VNV) indications.
SYSTEM OVERVIEW Flight Instruments Wind Data Option 1 Option 2 Option 3 No Data FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Wind direction and speed (relative to the aircraft) can be displayed in a window to the upper left of the HSI. When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”. Figure 2-36 Wind Data HAZARD AVOIDANCE Displaying wind data: 1) Press the PFD Softkey.
Flight Instruments SYSTEM OVERVIEW Vertical Navigation (VNV) Indications FLIGHT INSTRUMENTS When a VNV flight plan has been activated, VNV indications (VNV Target Altitude, RVSI, VDI) appear on the PFD in conjunction with the “TOD within 1 minute” message and “Vertical track” voice alert. See the Flight Management and AFCS sections for details on VNV features. VNV indications are removed from the PFD according to the criteria listed in the table.
SYSTEM OVERVIEW Flight Instruments 2.3 PFD Annunciations and Alerting Functions FLIGHT INSTRUMENTS The following annunciations and alerting functions are displayed on the PFD. Refer to the EICAS Section for information on the Crew Alerting System (CAS) and to Appendix A for more information on alerts and annunciations. System Alerting AUDIO PANEL & CNS EICAS The System Messages Window conveys messages to the flight crew regarding problems with the G1000 System.
Flight Instruments SYSTEM OVERVIEW Marker Beacon Annunciations Outer Marker Middle Marker FLIGHT INSTRUMENTS Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker reception is indicated in blue, middle in amber, and inner in white. Refer to the Audio Panel and CNS Section for more information on Marker Beacon Annunciations.
SYSTEM OVERVIEW Flight Instruments Minimum Descent Altitude/Decision Height Alerting FLIGHT INSTRUMENTS For altitude awareness, a barometric Minimum Descent Altitude (MDA) or Decision Height (DH), based on barometric altitude can be set. When active, the altitude setting is displayed to the lower left of the Altimeter and with a bug at the corresponding altitude along the Altimeter (once the altitude is within the range of the tape).
Flight Instruments SYSTEM OVERVIEW Altitude Alerting FLIGHT INSTRUMENTS The Altitude Alerting function provides visual and audio alerts when approaching the Selected Altitude. Whenever the Selected Altitude is changed, Altitude Alerting is reset. Altitude Alerting is based on the altitude information shown on the PFD selected with the XFR Key on the AFCS Control Unit. Altitude Alerting is independent of the AFCS.
SYSTEM OVERVIEW Flight Instruments 2.4 Abnormal Operations FLIGHT INSTRUMENTS Abnormal GPS Conditions The annunciations listed in the table can appear on the HSI when abnormal GPS conditions occur. Refer to the Flight Management Section for more information on Dead Reckoning Mode.
Flight Instruments SYSTEM OVERVIEW Unusual Attitudes When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the horizon are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Instruments Blank Page 80 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Engine Indication & Crew Alerting System SYSTEM OVERVIEW Section 3 Engine Indication & Crew Alerting System (EICAS) FLIGHT INSTRUMENTS Note: Refer to the Airplane Flight Manual (AFM) for limitations. The Cessna Citation Mustang’s Engine Indication and Crew Alerting System (EICAS) offers improved flight operations and reduces crew workload by automatically monitoring critical system parameters and providing system alerts during all phases of flight.
SYSTEM OVERVIEW Engine Indication & Crew Alerting System In the event of a display failure, depending on the failed display(s), the remaining display(s) may be reconfigured to present Primary Flight Display (PFD) symbology together with EICAS information (refer to the System Overview for more information about reversionary mode). FLIGHT INSTRUMENTS In reversionary mode, the data is pared down to a single column on any display.
Engine Indication & Crew Alerting System SYSTEM OVERVIEW 3.1 Engine Indication System (EIS) FLIGHT INSTRUMENTS 5 1 1 EICAS 6 2 5 7 AUDIO PANEL & CNS 3 6 FLIGHT MANAGEMENT 8 2 4 3 7 HAZARD AVOIDANCE 9 8 10 10 AFCS Figure 3-3 EICAS Display (Normal Mode) Figure 3-4 EIS Display (Reversionary Mode) 6 Engine High Pressure Turbine Rotation Speed 2 Oil Pressure and Temperature 7 Electrical Display 3 Fuel Display 8 Pressurization Display 4 CAS Display (refer to Section 3.
SYSTEM OVERVIEW Engine Indication & Crew Alerting System FLIGHT INSTRUMENTS EIS information is presented using horizontal and vertical bar indicators and digital readouts. Green ranges on the instrument scales indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. During normal operating conditions, an instrument’s pointer appears in white or green and readout text is green. Refer to each instrument description for additional details on display behavior.
Engine Indication & Crew Alerting System SYSTEM OVERVIEW Oil Pressure and Temperature FLIGHT INSTRUMENTS The oil pressure and temperature for each engine are shown below the N1 display under normal display operating conditions. Oil pressure is shown in pounds per square inch (psi) and temperature in degrees Celsius (°C). When oil pressure and temperature are in the normal operating range, no readout is provided. When an abnormal operating condition occurs, the readouts appear in the corresponding color.
SYSTEM OVERVIEW Engine Indication & Crew Alerting System Interstage Turbine Temperature FLIGHT INSTRUMENTS Interstage Turbine Temperatures (ITT) are displayed along a slider scale in °C. ITT values and limits are obtained from the FADEC. ITT is shown in the same format in display reversionary mode. During normal operations, the sliders appear in white and no readout is shown.
Engine Indication & Crew Alerting System SYSTEM OVERVIEW Pressurization Display FLIGHT INSTRUMENTS Cabin pressurization information (cabin altitude and rate of change, destination elevation, differential cabin pressure) is shown beneath the electrical display. Only cabin altitude and the pressure differential readouts are displayed in reversionary mode. Cabin altitude is shown on a color-coded scale labeled in 5,000-ft increments with a readout (in feet) below (unless on the ground).
SYSTEM OVERVIEW Engine Indication & Crew Alerting System The destination elevation (from -1,000 to 14,000 feet) entered in the PFD Timer/References Window is displayed below the cabin altitude readings. This value is retained by the G1000 on power-down. FLIGHT INSTRUMENTS Setting the destination elevation: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the ‘DEST ELV’ field.
Engine Indication & Crew Alerting System SYSTEM OVERVIEW 3.2 Crew Alerting System (CAS) NOTE: Aural alerts associated with abnormal conditions and advisories are managed through the Audio FLIGHT INSTRUMENTS Panels. Refer to the Audio Panel and CNS Section for more information. NOTE: If there is a mismatch between databases or software on the PFDs, CAS is inoperative.
SYSTEM OVERVIEW Engine Indication & Crew Alerting System Any CAS messages that come up when the system is first powered on are considered already acknowledged. They do not flash or trigger the Master Warning or Master Caution. CAS messages listed in Table 3-4 are shown in the acknowledged state (text corresponding to criticality on a black background).
Engine Indication & Crew Alerting System SYSTEM OVERVIEW CAS Display Inhibits Inhibits prevent certain CAS messages from being displayed if the message is triggered during the following conditions: • Aircraft in air (AIR) • Emergency bus power (EMER) • Landing (LOPI) • Engine start (Engine Start Inhibit, ESI) • Engine shutdown (Engine Shutdown Inhibit, ESDI) FLIGHT INSTRUMENTS • Aircraft on ground (GROUND) EICAS • Takeoff (TOPI) Inhibits affecting each CAS message are indicated with an “X” under th
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication & Crew Alerting System BATTERY O’TEMP EICAS AFT DOOR AFT JBOX CB L-R* AFT JBOX LMT L-R* ANTISKID FAIL BATTERY O’TEMP BATT TEMP FAIL CABIN ALT CABIN DOOR CHECK DOORS DUCT O’HEAT L-R* ENG A/I COLD L-R* ENG CTRL SYS L-R* ENGINE FAIL L-R* F/W SHUTOFF L-R* FLAPS FAIL FUEL BOOST L-R* FUEL FLTR BP L-R* FLIGHT MANAGEMENT AUDIO PANEL & CNS Caution FUEL LVL LO L-R* FUEL PRES LO L-R* HAZARD AVOIDANCE GEN OFF L-R GEN OFF L-R* HYD PRESS LO HYD PUMP ON NOS
Audio Panel and CNS SYSTEM OVERVIEW Section 4 Audio Panel and CNS FLIGHT INSTRUMENTS 4.1 Overview The Communication/Navigation/Surveillance (CNS) system includes the Audio Panels, communication radios, navigation radios, and Mode S transponders. The System Overview Section provides a block diagram description of the Audio Panels and CNS system interconnection.
SYSTEM OVERVIEW Audio Panel and CNS PFD Controls and Frequency Display 2 3 4 5 6 7 8 FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 1 9 10 HAZARD AVOIDANCE 11 12 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-1 PFD Controls, COM/NAV Frequency Tuning Boxes, and ADF/DME Tuning Window 94 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Audio Panel and CNS 5 COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM transceiver frequency is displayed in green. 6 COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz). Press to move the tuning box (light blue box) and Frequency Transfer Arrow between COM1 and COM2. 7 COM Frequency Transfer Key – Transfers the standby and active COM frequencies.
SYSTEM OVERVIEW Audio Panel and CNS AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Audio Panel Controls 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 FLIGHT MANAGEMENT 18 19 20 21 HAZARD AVOIDANCE 17 22 23 24 AFCS Figure 4-2 Audio Panel Controls INDEX APPENDICES ADDITIONAL FEATURES NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 96 1 COM1 MIC – Selects the #1 transmitter for transmitting.
Audio Panel and CNS SPKR – Selects and deselects the on-side flight deck speaker. COM and NAV receiver audio will be heard on the speaker. 11 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity. 13 DME – Turns DME audio on or off.
SYSTEM OVERVIEW Audio Panel and CNS 4.2 COM Operation FLIGHT INSTRUMENTS COM Transceiver Selection and Activation NOTE: During PA Mode, the COM MIC Annunciator is extinguished and the COM active frequency color changes to white, indicating that neither COM transmitter is active. NOTE: When turning on the G1000 for use, the system remembers the last frequencies used and the active EICAS COM transceiver state prior to shutdown.
Audio Panel and CNS SYSTEM OVERVIEW Transmit/Receive Indications FLIGHT INSTRUMENTS During COM transmission, a white TX appears by the active COM frequency replacing the Frequency Transfer Arrow. On the Audio Panel, when the active COM is transmitting, the active transceiver COM MIC Key Annunciator flashes approximately once per second. During COM signal reception, a white RX appears by the active COM frequency replacing the Frequency Transfer Arrow.
SYSTEM OVERVIEW Audio Panel and CNS Selecting the Radio to be Tuned FLIGHT INSTRUMENTS Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. EICAS Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other AUDIO PANEL & CNS Figure 4-6 Switching COM Tuning Boxes Quick-tuning and Activating 121.
Audio Panel and CNS SYSTEM OVERVIEW Auto-tuning the COM Frequency COM frequencies can be automatically tuned from the following: • Nearest Airports Window (PFD) • NRST – Nearest Frequencies Page (ARTCC, FSS, WX) FLIGHT INSTRUMENTS • WPT – Airport Information Page • NRST – Nearest Airspaces Page • NRST – Nearest Airports Page Auto-tuning from the PFD EICAS COM frequencies for the nearest airports can be automatically tuned from the Nearest Airports Window on the PFD.
SYSTEM OVERVIEW Audio Panel and CNS Auto-tuning from the MFD FLIGHT INSTRUMENTS Frequencies can be automatically loaded into the COM Frequency Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key (Figures 4-9, 4-10, and 4-11). Auto-tuning a COM frequency from the WPT and NRST Pages: 1) From any page that the COM frequency can be auto-tuned, activate the cursor by pressing the FMS Knob on the MFD control unit or selecting the appropriate softkey.
Audio Panel and CNS SYSTEM OVERVIEW Or: 1) Press the MENU Key on the MFD control unit (Figure 4-9) to display the page menu (Figure 4-10). 2) Turn the large FMS Knob to scroll through the menu options. FLIGHT INSTRUMENTS 3) Press the ENT Key to place the cursor on the desired selection. 4) Scroll through the frequency selections with the FMS Knob or the ENT Key. 5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio.
SYSTEM OVERVIEW Audio Panel and CNS FLIGHT INSTRUMENTS On the WPT - Airport Information Page, the cursor can be placed on the frequency field by pressing the FMS Knob and scrolling through the list. The frequency is transferred to the COM Standby Field with the ENT Key. EICAS Selected Airport Identifier and Information Runway Information FLIGHT MANAGEMENT AUDIO PANEL & CNS Press ENT Key to load frequency into PFD1 COM Standby Field. Cursor then advances to the next frequency.
Audio Panel and CNS SYSTEM OVERVIEW COM frequencies can also be auto-tuned from the NRST – Nearest Airspaces, NRST – Nearest Frequencies, and NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key.
SYSTEM OVERVIEW Audio Panel and CNS Frequency Spacing FLIGHT INSTRUMENTS The G1000 COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list. COM channel spacing is set on the System Setup Page of the AUX Page Group. EICAS 8.
Audio Panel and CNS SYSTEM OVERVIEW Automatic Squelch FLIGHT INSTRUMENTS Automatic Squelch quiets unwanted static noise when no audio signal is received, while still providing good sensitivity to weak COM signals. To disable Automatic Squelch, press the VOL/SQ Knob. When Automatic Squelch is disabled, COM audio reception is always on. Continuous static noise is heard over the headsets and speaker, if selected. Pressing the VOL/SQ Knob again enables Automatic Squelch.
SYSTEM OVERVIEW Audio Panel and CNS 4.3 NAV Operation FLIGHT INSTRUMENTS NAV Radio Selection and Activation The NAV Frequency Box is composed of four fields; two standby fields and two active fields. The active frequencies are on the right side and the standby frequencies are on the left. EICAS A NAV radio is selected for navigation by pressing the CDI Softkey located on the PFD. The active NAV frequency selected for navigation is displayed in green.
Audio Panel and CNS SYSTEM OVERVIEW NAV radios are selected for listening by pressing the corresponding keys on the Audio Panel. Pressing the NAV1, NAV2, ADF, or DME Key selects and deselects the navigation radio source. Selected audio can be heard over the headset and the speakers (if selected). All radios can be selected individually or simultaneously.
SYSTEM OVERVIEW Audio Panel and CNS Selecting the Radio to be Tuned FLIGHT INSTRUMENTS Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. EICAS Press the NAV Knob to Switch the Tuning Box from One NAV Radio to the Other Figure 4-20 Switching NAV Tuning Boxes AUDIO PANEL & CNS VOR/LOC ID When the Morse code Identifier audio is on for a NAV radio, a white ID appears to the left of the active NAV frequency.
Audio Panel and CNS SYSTEM OVERVIEW Auto-tuning a NAV Frequency from the MFD NAV frequencies can be selected and loaded from the following MFD pages: • WPT – Airport Information • NRST – Nearest VOR • NRST – Nearest Frequencies (FSS, WX) • NRST – Nearest Airports • NRST – Nearest Airspaces FLIGHT INSTRUMENTS • WPT – VOR Information EICAS The MFD provides auto-tuning of NAV frequencies from waypoint and nearest pages.
SYSTEM OVERVIEW Audio Panel and CNS Or: 1) When on the NRST pages, press the MENU Key on the MFD control unit to display the page menu. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to scroll through the menu options. 3) Press the ENT Key to place the cursor in the desired window. 4) Scroll through the frequency selections with the FMS Knob or the ENT Key. 5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.
Audio Panel and CNS SYSTEM OVERVIEW In the example shown, the VOR list is selected with the VOR Softkey or from the page menu. The FMS Knob or ENT Key is used to scroll through the list. The cursor is placed on the frequency with the FREQ Softkey and loaded into the NAV Tuning Box with the ENT Key. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Press the ENT Key to Load the Frequency into the NAV Standby Field.
SYSTEM OVERVIEW Audio Panel and CNS APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS While enroute, NAV frequencies can also be auto-tuned from the NRST – Nearest Airports, WPT – Airport Information, WPT – VOR Information, and NRST – Nearest Frequencies Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key.
Audio Panel and CNS SYSTEM OVERVIEW Auto-tuning NAV Frequencies on Approach Activation NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach. FLIGHT INSTRUMENTS NOTE: When an ILS/LOC approach has been activated in GPS Mode, the system switches to NAV Mode as the final approach course is intercepted (within 15 nm of the FAF). See the Flight Management Section for details.
SYSTEM OVERVIEW Audio Panel and CNS Marker Beacon Receiver NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be turned FLIGHT INSTRUMENTS off. The marker beacon receiver is used as part of the ILS. The marker beacon receiver is always on and detects any marker beacon signals within the reception range of the aircraft.
Audio Panel and CNS SYSTEM OVERVIEW ADF/DME Tuning NOTE: When another auxiliary window is turned on, the ADF/DME Tuning Window is replaced on the PFD. FLIGHT INSTRUMENTS See the Flight Instruments Section for displaying the DME and bearing information windows (ADF) and using the ADF as the source for the bearing pointer. The G1000 system tunes the ADF receiver (optional) and DME transceiver (standard).
SYSTEM OVERVIEW Audio Panel and CNS ADF Tuning FLIGHT INSTRUMENTS ADF frequencies in the 190.0-kHz to 1799.5-kHz range are entered in the standby ADF frequency field of the ADF/DME Tuning Window. The G1000 System does not tune the ADF emergency frequency, 2182.0‑kHz. Tuning an ADF frequency: 1) Press the ADF/DME Softkey to display the ADF/DME Tuning Window. 2) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field.
Audio Panel and CNS SYSTEM OVERVIEW Selecting ADF Receiver Mode The following modes can be selected: (In all modes NDB audio can be heard by pressing the ADF Key on the Audio Panel.) FLIGHT INSTRUMENTS • ANT (Antenna) – The ADF bearing pointer parks on the HSI at 90 degrees. Best mode for listening to NDB audio. • ADF (Automatic Direction Finder) – The ADF pointer points to the relative bearing of the NDB station.
SYSTEM OVERVIEW Audio Panel and CNS DME Tuning NOTE: When turning on the G1000 for use, the system remembers the last frequency used for DME tuning FLIGHT INSTRUMENTS and the NAV1, NAV2, or HOLD state prior to shutdown. EICAS The DME transceiver is tuned by selecting NAV1, NAV2, or HOLD in the ADF/DME Tuning Window.
Audio Panel and CNS SYSTEM OVERVIEW 4.4 GTX 33/33D Mode S Transponders FLIGHT INSTRUMENTS The GTX 33 Mode S Transponder and GTX 33D Diversity Mode S Transponder provide Mode A, Mode C, and Mode S interrogation and reply capabilities. Diversity incorporates antennas mounted on the top and bottom of the aircraft for dependable operation while maneuvering.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Audio Panel and CNS XPDR1 XPDR2 STBY ON ALT GND VFR XPDR IDENT CODE IDENT BACK MSG Pressing the BACK Softkey returns to the top-level softkeys. EICAS 0 1 2 3 4 5 6 7 IDENT BKSP BACK MSG AUDIO PANEL & CNS Pressing the BACK Softkey returns to the mode selection softkeys.
Audio Panel and CNS SYSTEM OVERVIEW Ground Mode FLIGHT INSTRUMENTS Ground Mode is normally selected automatically when the aircraft is on the ground. The transponder powers up in the last mode it was in when shut down. Ground Mode can be overridden by pressing any one of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of the Transponder Data Box.
SYSTEM OVERVIEW Altitude Mode (Automatic or Manual) FLIGHT INSTRUMENTS Audio Panel and CNS If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure altitude information. Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey.
Audio Panel and CNS SYSTEM OVERVIEW Entering a Transponder Code Entering a transponder code with softkeys: FLIGHT INSTRUMENTS 1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Press the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry. EICAS 3) Press the digit softkeys to enter the code in the code field.
SYSTEM OVERVIEW Audio Panel and CNS VFR Code FLIGHT INSTRUMENTS The VFR code can be entered either manually or by pressing the XPDR Softkey, then the VFR Softkey. When the VFR Softkey is pressed, the pre-programmed VFR code is automatically displayed in the code field of the Transponder Data Box. Pressing the VFR Softkey again restores the previous identification code. The pre-programmed VFR Code is set at the factory to 1200.
Audio Panel and CNS SYSTEM OVERVIEW Flight ID Reporting FLIGHT INSTRUMENTS The flight crew must enter the Flight ID before flight operation. The number is entered in the Timer/ References Window on the PFD. The Flight ID is not to exceed seven characters. No space is needed when entering Flight ID. When a Flight ID contains a space, the system automatically removes it upon completion of Flight ID entry. If configuration is set to “SAME AS TAIL” the aircraft tail number will always be displayed.
SYSTEM OVERVIEW Audio Panel and CNS 4.5 Additional Audio Panel Functions FLIGHT INSTRUMENTS Power-up The Audio Panels perform a self-test during power-up. During the self-test all Audio Panel annunciator lights illuminate for approximately two seconds. Once the self-test is completed, most of the settings are restored to those in use before the unit was last turned off. The exceptions are the speaker and intercom, which are always selected during power up.
Audio Panel and CNS SYSTEM OVERVIEW Intercom FLIGHT INSTRUMENTS Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may select or deselect the intercom. The MAN SQ Key allows either automatic or manual control of the intercom squelch setting.
SYSTEM OVERVIEW Audio Panel and CNS Passenger Address (PA) System FLIGHT INSTRUMENTS A passenger address system is provided by pressing the PA Key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the INTR COM Key is enabled. PA messages are one way from the flight deck to the passengers. A Push-to-talk (PTT) must be pressed to deliver PA announcements to the passengers over their headphones.
Audio Panel and CNS SYSTEM OVERVIEW Clearance Recorder and Player FLIGHT INSTRUMENTS The Audio Panels contain a digital clearance recorder that records up to 2.5 minutes of the selected COM radio signal. Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Pressing the REC Key enables recording of audio from the COM radio selected for transmission.
SYSTEM OVERVIEW Audio Panel and CNS 4.6 Audio Panels Preflight Procedure FLIGHT INSTRUMENTS NOTE: If the flight crew is using headsets that have a high/low switch or volume control knob, verify that the switch is in the high position and the volume control on the headsets are at max volume setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the audio system.
Audio Panel and CNS SYSTEM OVERVIEW Setting the Audio Panels during preflight: 1) Verify that the INTR COM Key is selected. 2) Verify that the MAN SQ Annunciator is extinguished. FLIGHT INSTRUMENTS 3) Turn the MSTR Knob (Master Volume Control) on both Audio Panels clockwise two full turns. This will set the headset audio level to max volume (least amount of attenuation). 4) Adjust radio volume levels (COM, NAV, etc.) to a suitable level.
SYSTEM OVERVIEW Audio Panel and CNS 4.7 Abnormal Operation FLIGHT INSTRUMENTS Abnormal operation of the G1000 includes equipment failures of the G1000 components and failure of associated equipment, including switches and external devices. Stuck Microphone If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of continuous operation. An alert appears on the PFD to advise the crew of a stuck microphone.
Audio Panel and CNS SYSTEM OVERVIEW PFD Failure, Dual System FLIGHT INSTRUMENTS If PFD1 fails, COM1 and NAV1 display a red X on both remaining displays. NAV1 is unavailable. COM1 automatically tunes 121.500 MHz, but the frequency is not shown. The COM1 emergency frequency is available to both the copilot and pilot.
SYSTEM OVERVIEW Audio Panel and CNS Audio Panel Fail-safe Operation FLIGHT INSTRUMENTS If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot’s headset and microphone directly to the COM1 transceiver and the copilot’s headset directly to the COM2 transceiver. Audio will not be available on the speakers. If there is a failure of one Audio Panel, the remaining one will not have access to the others side’s COM and NAV.
Flight Management SYSTEM OVERVIEW Section 5 Flight Management FLIGHT INSTRUMENTS 5.1 Introduction The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the G1000. EICAS The most prominent part of the G1000 are the three full color displays: two Primary Flight Displays (PFD) and a Multi Function Display (MFD).
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Navigation Status Box Navigation Mode AUDIO PANEL & CNS EICAS Inset Map Location of: - Direct To Window - Flight Plan Window - Procedures Window - Nearest Airports Window Figure 5-1 GPS Navigation Information on the PFD FLIGHT MANAGEMENT Navigation Status Box Map Orientation Navigation Map HAZARD AVOIDANCE - Aviation Data - Geographic Data - Topographic Data - Hazard Data Active Flight Plan Leg AFCS Aircraft Icon at Present Position ADDITI
Flight Management SYSTEM OVERVIEW Navigation Status Box The Navigation Status Box located at the top of the PFD contains two fields displaying the following information: FLIGHT INSTRUMENTS PFD Navigation Status Box The Navigation Status Box located at the top of the MFD contains four data fields, each displaying one of the following items: • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g.
SYSTEM OVERVIEW Flight Management 4) Turn the small FMS Knob to display and scroll through the data options list. 5) Select the desired data. FLIGHT INSTRUMENTS 6) Press the ENT Key. Selecting the DFLTS Softkey returns any field to its default setting. 5.2 Using Map Displays Map displays are used extensively in the G1000 to provide situational awareness in flight.
Flight Management SYSTEM OVERVIEW • North up (NORTH UP) aligns the top of the map display to north (default setting). • Track up (TRK UP) aligns the top of the map display to the current ground track. • Desired track up (DTK UP) aligns the top of the map display to the desired course. FLIGHT INSTRUMENTS • Heading up (HDG UP) aligns the top of the map display to the current aircraft heading.
SYSTEM OVERVIEW Flight Management Map Group Selection AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Orientation Field FLIGHT MANAGEMENT Figure 5-5 Map Setup Menu Window - Map Group 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. HAZARD AVOIDANCE 6) Press the FMS Knob to return to the base page. Map Range ADDITIONAL FEATURES AFCS There are 28 different map ranges available, from 500 feet to 2000 nm.
Flight Management SYSTEM OVERVIEW Auto Zoom FLIGHT INSTRUMENTS Auto zoom allows the G1000 to change the map display range to the smallest range clearly showing the active waypoint. Auto zoom can be overridden by adjusting the range with the Joystick, and remains until the active waypoint changes, a terrain or traffic alert occurs, the aircraft takes off, or the manual override times out (timer set on Map Setup Window).
SYSTEM OVERVIEW Flight Management Auto Zoom: FLIGHT INSTRUMENTS Off, MFD Only, PFD Only, All On AUDIO PANEL & CNS EICAS Manual Range Override Expiration Time Maximum Look Forward Time Minimum Look Forward Time FLIGHT MANAGEMENT Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom Configuring automatic zoom: HAZARD AVOIDANCE 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed.
Flight Management SYSTEM OVERVIEW Map Panning Map panning allows the pilot to: • View parts of the map outside the displayed range without adjusting the map range FLIGHT INSTRUMENTS • Highlight and select locations on the map • Review information for a selected airport, NAVAID or user waypoint • Designate locations for use in flight planning • View airspace and airway information EICAS AUDIO PANEL & CNS When the panning function is selected by pressing the Joystick, the Map Pointer flashes on the map d
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was not originally displayed on the map). When any map feature or object is selected on the map display, pertinent information is displayed.
Flight Management SYSTEM OVERVIEW When the Map Pointer crosses an airspace boundary, the boundary is highlighted and airspace information is shown at the top of the display. The information includes the name and class of airspace, the ceiling in feet above Mean Sea Level (MSL), and the floor in feet MSL.
SYSTEM OVERVIEW Flight Management Reviewing information for an airport, NAVAID, or user waypoint: 1) Place the Map Pointer on a waypoint. FLIGHT INSTRUMENTS 2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint. 3) Press the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page.
Flight Management SYSTEM OVERVIEW Viewing airspace information for a special-use or controlled airspace: 1) Place the Map Pointer on an open area within the boundaries of an airspace. 2) Press the ENT Key to display an options menu. FLIGHT INSTRUMENTS 3) ‘Review Airspace?’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace Information Page for the selected airspace. 4) Press the CLR or ENT Key to exit the Airspace Information Page.
SYSTEM OVERVIEW Flight Management Measuring Bearing and Distance FLIGHT INSTRUMENTS Distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be calculated using the ‘Measure Bearing and Distance’ selection from Navigation Map page menu. The bearing and distance tool displays a dashed Measurement Line and a Measure Pointer to aid in graphically identifying points with which to measure.
Flight Management SYSTEM OVERVIEW Topography FLIGHT INSTRUMENTS All navigation maps can display various shades of topography colors representing land elevation, similar to aviation sectional charts. Topographic data can be displayed or removed as described in the following procedures.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EICAS TOPO DATA On/Off TOPO DATA Range Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup The topographic data range is the maximum map range on which topographic data is displayed. FLIGHT MANAGEMENT Note: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g.
Flight Management SYSTEM OVERVIEW Maximum Displayed Elevation Minimum Displayed Elevation FLIGHT INSTRUMENTS Aircraft Altitude (MSL) Range of Displayed Elevations EICAS Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) AUDIO PANEL & CNS Figure 5-16 Navigation Map - TOPO SCALE FLIGHT MANAGEMENT Displaying/removing the topographic scale (TOPO SCALE): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
SYSTEM OVERVIEW Flight Management Map Symbols FLIGHT INSTRUMENTS This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the symbols from the map using the DCLTR Softkey is also discussed.
Flight Management SYSTEM OVERVIEW Aviation Symbols The following items are configured on the aviation menu: Aviation Symbols Symbol Default Maximum Range (nm) Range (nm) 2000 500 300 100 20 100 30 Non-directional Beacon (NDB WAYPOINT) 15 30 VOR (VOR WAYPOINT) 150 300 Class B Airspace/TMA (CLASS B/TMA) 200 500 Class C Airspace/TCA (CLASS C/TCA) 200 500 Class D Airspace (CLASS D) 150 300 Restricted Area (RESTRICTED) 200 500 Military Operations Area [MOA(MILITARY)] 200 500 Other/Air D
SYSTEM OVERVIEW Flight Management Symbol Setup FLIGHT INSTRUMENTS All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option.
Flight Management SYSTEM OVERVIEW 7) Press the ENT Key to accept the selected range. 8) Press the FMS Knob to return to the Navigation Map Page.
SYSTEM OVERVIEW Flight Management Map Declutter FLIGHT INSTRUMENTS The declutter feature allows the pilot to progressively step through four levels of removing map information. The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option.
Flight Management SYSTEM OVERVIEW Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the various levels of declutter.
SYSTEM OVERVIEW Flight Management Airways FLIGHT INSTRUMENTS This airways discussion is based upon the North American airway structure. The airway structure in places other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or Victor Airways) primarily serve smaller piston-engine, propeller-driven airplanes on shorter routes and at lower altitudes.
Flight Management SYSTEM OVERVIEW Airways may be displayed on the map at the pilot’s discretion using either a combination of AIRWAYS Softkey selections, or menu selections using the MENU Key from the Navigation Map Page. The Airway range can also be programmed to only display Airways on the MFD when the map range is at or below a specific number. FLIGHT INSTRUMENTS Displaying/removing airways: 1) Select the MAP Softkey. 2) Select the AIRWAYS Softkey.
SYSTEM OVERVIEW Flight Management The following range items are configurable on the airways menu: Airway Type Symbol FLIGHT INSTRUMENTS Low Altitude Airway (LOW ALT AIRWAY) Default Maximum Range (nm) Range (nm) 200 500 High Altitude Airway (HI ALT AIRWAY) 300 500 EICAS Table 5-4 Airway Range Information Track Vector AUDIO PANEL & CNS The Navigation Map can display a track vector that is useful in minimizing track angle error.
Flight Management SYSTEM OVERVIEW Nav Range Ring On/Off FLIGHT INSTRUMENTS Wind Vector On/Off Track Vector - On/Off - Look Ahead Time EICAS Fuel Range - On/Off - Fuel Reserve Time AUDIO PANEL & CNS Figure 5-25 Navigation Map Setup Menu -TRACK VECTOR, WIND VECTOR, NAV RANGE RING, FUEL RANGE RING Setup Wind Vector HAZARD AVOIDANCE Wind Direction FLIGHT MANAGEMENT The map displays a wind vector arrow in the upper right-hand portion of the screen.
SYSTEM OVERVIEW Flight Management Nav Range Ring FLIGHT INSTRUMENTS The Nav Range Ring shows the direction of travel (ground track) on a rotating compass card. The range is determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map).
Flight Management SYSTEM OVERVIEW Fuel Range Ring FLIGHT INSTRUMENTS The map can display a fuel range ring which shows the remaining flight distance. A dashed green circle indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only reserve fuel remains, the range is indicated by a solid yellow circle.
SYSTEM OVERVIEW Flight Management Field of View (SVS) FLIGHT INSTRUMENTS The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view. The field of view is shown as two dashed lines forming a V shape in front of the aircraft symbol on the map. This is only available if SVS is installed on the aircraft.
Flight Management SYSTEM OVERVIEW 5.3 Waypoints FLIGHT INSTRUMENTS Waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are used for all phases of flight planning and navigation. Communication and navigation frequencies can be tuned “automatically” from various Waypoint Information (WPT) pages, Nearest (NRST) pages, and the Nearest Airports Window (on PFD). This auto-tuning feature simplifies frequency entry over manual tuning.
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Identifier with Duplicates EICAS Duplicate Waypoints AUDIO PANEL & CNS Duplicate Message FLIGHT MANAGEMENT Figure 5-31 Waypoint Information Window - Duplicate Identifier Airports Note: ‘North Up’ orientation on the Airport Information Page cannot be changed; the pilot needs to be HAZARD AVOIDANCE aware of proper orientation if the Navigation Map orientation is different from the Airport Information Page Map.
Flight Management SYSTEM OVERVIEW Airport Information Navigation Map Showing Selected Airport FLIGHT INSTRUMENTS - ID/Facility/City - Usage Type/Region - Lat/Long/Elev - Fuel Available - Time Zone (UTC Offset) Runway Information Airport/Runway Diagram EICAS - Designation - Length/Width/Surface - Lighting Available COM/NAV Freq. Info.
SYSTEM OVERVIEW Flight Management View a destination airport: FLIGHT INSTRUMENTS From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination Airport is displayed.
Flight Management SYSTEM OVERVIEW Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list.
SYSTEM OVERVIEW Flight Management Nearest Airports FLIGHT INSTRUMENTS - ID/Type - Bearing/Distance Navigation Map Showing Nearest Airport Airport Information - Facility/City/Elevation Runway Information EICAS - Designation/Surface - Length/Width COM/NAV Freq. Info.
Flight Management SYSTEM OVERVIEW Viewing runway information for a specific airport: 1) With the Nearest Airports Page displayed, press the RNWY Softkey; or press the MENU Key, highlight ‘Select Runway Window’; and press the ENT Key. The cursor is placed in the ‘RUNWAYS’ Box. FLIGHT INSTRUMENTS 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor.
SYSTEM OVERVIEW Flight Management Intersections Note: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR FLIGHT INSTRUMENTS used to define the intersection. EICAS The Intersection Information Page is used to view information about intersections.
Flight Management SYSTEM OVERVIEW The Nearest Intersections Page can be used to quickly find an intersection close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest intersections in three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’. FLIGHT INSTRUMENTS The selected intersection is indicated by a white arrow. Up to seventeen Intersections are visible at a time.
SYSTEM OVERVIEW Flight Management NDBs FLIGHT INSTRUMENTS The NDB Information Page is used to view information about NDBs. In addition to displaying a map of the currently selected NDB and surrounding area, the page displays NDB information in four boxes labeled ‘NDB’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT.
Flight Management SYSTEM OVERVIEW The Nearest NDB Page can be used to quickly find a NDB close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest NDBs in three boxes labeled ‘NEAREST NDB’, ‘INFORMATION’, and ‘FREQUENCY’. FLIGHT INSTRUMENTS A white arrow before the NDB identifier indicates the selected NDB. Up to seventeen NDBs are visible at a time. If there are more than can be shown, each list can be scrolled.
SYSTEM OVERVIEW Flight Management VORs FLIGHT INSTRUMENTS The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals can be received on a NAV receiver), or to quickly auto-tune a VOR or ILS frequency. Localizer information cannot be viewed on the VOR Information Page. If a VOR station is combined with a TACAN station it is listed as a VORTAC on the VOR Information Page and if it includes only DME, it’s displayed as VOR-DME.
Flight Management SYSTEM OVERVIEW Or: 1) With the Nearest VOR Page displayed, press the MENU Key. 2) Highlight ‘SELECT VOR WINDOW’, and press the ENT Key. FLIGHT INSTRUMENTS 3) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box. 4) Press the FMS Knob to remove the flashing cursor. EICAS The Nearest VOR Page can be used to quickly find a VOR station close to the aircraft.
SYSTEM OVERVIEW Flight Management User Waypoints FLIGHT INSTRUMENTS The G1000 can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on the map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance from an existing waypoint or bearing from two existing waypoints.
Flight Management SYSTEM OVERVIEW Nearest User Wpt List FLIGHT INSTRUMENTS - Identifier - Bearing/Distance from aircraft position Navigation Map Showing Selected User Waypoint EICAS Selected User Waypoint User Waypoint Info AUDIO PANEL & CNS - Comment - Lat/Long Reference Wpt Info - Identifier - Radial/Distance FLIGHT MANAGEMENT Figure 5-44 Nearest User Waypoint Page Creating User Waypoints HAZARD AVOIDANCE User waypoints can be created from the User Waypoint Information Page in the following
SYSTEM OVERVIEW Flight Management 6) Press the ENT Key to accept the new waypoint. AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 7) Press the FMS Knob to remove the flashing cursor. Figure 5-45 User Waypoint Information Page Menu FLIGHT MANAGEMENT Creating user waypoints from map pages: 1) Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint. 2) Press the ENT Key. The User Waypoint Information Page is displayed with the captured position.
Flight Management SYSTEM OVERVIEW Renaming user waypoints: 1) Highlight a user waypoint in the User Waypoint List. Select the RENAME Softkey, or press the MENU Key and select ‘Rename User Waypoint’ FLIGHT INSTRUMENTS 2) Enter a new name. 3) Press the ENT Key. The message ‘Do you want to rename the user waypoint AAAAAA to BBBBBB?’ is displayed. 4) With ‘YES’ highlighted, press the ENT Key. EICAS 5) Press the FMS Knob to remove the flashing cursor.
SYSTEM OVERVIEW Flight Management Deleting User Waypoints Deleting a single user waypoint FLIGHT INSTRUMENTS 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field. 2) Select the DELETE Softkey or press the CLR Key. ‘Yes’ is highlighted in the confirmation window. 3) Press the ENT Key. 4) Press the FMS Knob to remove the flashing cursor.
Flight Management SYSTEM OVERVIEW 5.4 Airspaces FLIGHT INSTRUMENTS The G1000 can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA (Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR).
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. An altitude buffer is also provided which “expands” the vertical range above or below an airspace.
Flight Management SYSTEM OVERVIEW Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu: See Table 5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace area. FLIGHT INSTRUMENTS The Nearest Airspaces Page can be used to quickly find airspaces close to the flight path. In addition, a selected frequency associated with the airspace can be loaded from the Nearest Airspaces Page.
SYSTEM OVERVIEW Flight Management Pressing the PFD MSG Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: EICAS FLIGHT INSTRUMENTS Message INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead – less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. Comments The aircraft is inside the airspace. Special use airspace is ahead of aircraft.
Flight Management SYSTEM OVERVIEW 5.5 Direct-to-Navigation FLIGHT INSTRUMENTS The Direct-to method of navigation, initiated by pressing the Direct-to Key on either the MFD or PFD, is quicker to use than a flight plan when the desire is to navigate to a single point such as a nearby airport. Once a direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the selected direct-to destination.
SYSTEM OVERVIEW Flight Management Direct-to Point Info - Identifier/Symbol/City - Facility Name FLIGHT INSTRUMENTS VNV Constraints - Altitude at Arrival - Along Track Offset Direct-to Point Info - Bearing/Distance - Desired Course EICAS Activation Command AUDIO PANEL & CNS Figure 5-50 Direct-to Window - PFD Any waypoint can be entered as a direct-to destination from the Direct-to Window.
Flight Management SYSTEM OVERVIEW Selecting an active flight plan waypoint as a direct-to destination: 1) While navigating an active flight plan, press the Direct-to Key. The Direct-to Window is displayed with the active flight plan waypoint as the default selection. FLIGHT INSTRUMENTS 2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). 3) Select the desired waypoint. 4) Press the ENT Key.
SYSTEM OVERVIEW Flight Management Selecting a nearby airport as a direct-to destination: 1) Select the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page. FLIGHT INSTRUMENTS 2) Select the desired airport (the nearest one is already selected). 3) Press the Direct-to Key. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to.
Flight Management SYSTEM OVERVIEW Page Menu FLIGHT INSTRUMENTS - Cancel Direct-To Navigation EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-52 Direct-to Window - Cancelling Direct-to Navigation HAZARD AVOIDANCE When navigating a direct-to, the G1000 sets a direct great circle course to the selected destination. The course to a destination can also be manually selected using the course field (‘COURSE’) on the Direct-to Window. Selecting a manual direct-to course: 1) Press the Direct-to Key.
SYSTEM OVERVIEW Flight Management Entering a VNV altitude and along-track offset for the waypoint: 1) Press the Direct-to Key to display the Direct-to Window. FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. 3) Enter the desired altitude. 4) Press the ENT Key. The option to select MSL or AGL is now displayed. 5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 6) Press the ENT Key. The cursor is now flashing in the VNV offset distance field.
Flight Management SYSTEM OVERVIEW 5.6 Flight Planning Flight Plan Leg Type FLIGHT INSTRUMENTS Flight planning on the G1000 consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The G1000 allows flight planning information to be entered from either the MFD or PFD.
SYSTEM OVERVIEW Flight Management The following could cause the airway update to fail: • Airway identifier, entry waypoint or exit waypoint not found in the new database. FLIGHT INSTRUMENTS • Airway entry/exit waypoint is not an acceptable waypoint for the airway – either the waypoint is no longer on the airway, or there is a new directional restriction that prevents it being used. • Loading the new airway sequence would exceed the capacity of the flight plan.
Flight Management SYSTEM OVERVIEW Active Flight Plan Comment FLIGHT INSTRUMENTS Active Flight Plan Leg Active Flight Plan Waypoint List - Waypoint ID - Desired Track to Waypoint - Distance to Waypoint - Airway Identifier EICAS Figure 5-55 Active Flight Plan Window on PFD AUDIO PANEL & CNS Catalog Contents - # Used - # Empty FLIGHT MANAGEMENT Flight Plan List - Comment HAZARD AVOIDANCE Selected Flight Plan Map AFCS Selected FPL Info - Departure Waypoint - Destination Waypoint - Total Flight Plan
SYSTEM OVERVIEW Flight Management 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, or airway waypoints).
Flight Management SYSTEM OVERVIEW Adding Waypoints to an Existing Flight Plan FLIGHT INSTRUMENTS Waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the desired point of insertion, enter the waypoint, and it is added in front of the selected waypoint. Flight plans are limited to 99 waypoints (including waypoints within airways and procedures). If the number of waypoints in the flight plan exceeds 99, the message “Flight plan is full.
SYSTEM OVERVIEW Flight Management Adding a waypoint to a stored flight plan: 1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. FLIGHT INSTRUMENTS 2) Highlight the desired flight plan. 3) Select the EDIT Softkey; or press the ENT Key, turn the large FMS Knob clockwise to select “EDIT” and press the ENT Key. The Stored Flight Plan Page is displayed. 4) Select the point in the flight plan to add the new waypoint.
Flight Management SYSTEM OVERVIEW Creating and adding user waypoints to the active flight plan: 1) Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location of the desired user waypoint. FLIGHT INSTRUMENTS 2) Select the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of the active flight plan.
SYSTEM OVERVIEW Flight Management 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. FLIGHT INSTRUMENTS 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted.
Flight Management SYSTEM OVERVIEW Restrictions on Adding Airways Some airways have directional restrictions on all or part of the route. Airway “A2” in Europe has a directional restriction over the whole route such that it can be flown only in the direction MTD-ABB-BNE-DEVAL.
SYSTEM OVERVIEW Flight Management Departure (DP) FLIGHT INSTRUMENTS A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. The route is defined by selection of a departure, the transition waypoints, and a runway.
Flight Management SYSTEM OVERVIEW Departure Airport FLIGHT INSTRUMENTS Selected Departure Selected Runway Selected Transition Preview of Selected Departure Departure Transition Points Available EICAS Departure Waypoint Sequence AUDIO PANEL & CNS Selected Departure End Point FLIGHT MANAGEMENT Figure 5-65 Departure Loading Page - Selecting Transition HAZARD AVOIDANCE Inserted Departure Header AFCS - Departure Identifier: [departure airport]-[departure runway]. [departure transition].
SYSTEM OVERVIEW Flight Management Arrival (STAR) FLIGHT INSTRUMENTS A Standard Terminal Arrival (STAR) is loaded at the destination airport in the flight plan. Only one arrival can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints, and a runway.
Flight Management SYSTEM OVERVIEW Destination Airport FLIGHT INSTRUMENTS Selected Arrival Selected Transition Transitions Available with DBRY1 EICAS Arrival Waypoint Sequence Preview of Selected Arrival AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-68 Arrival Loading Page - Selecting the Transition HAZARD AVOIDANCE Inserted Arrival Header AFCS - Arrival Identifier: [arrival airport]-[arrival transition]. [arrival].[arrival runway] (e.g., KCOS-ALS.DBRY1.
SYSTEM OVERVIEW Flight Management Approach (APPR) FLIGHT INSTRUMENTS An Approach Procedure (APPR) can be loaded at any airport that has an approach available. Only one approach can be loaded at a time in a flight plan. The route for a selected approach is defined by designating transition waypoints.
Flight Management SYSTEM OVERVIEW Destination Airport FLIGHT INSTRUMENTS Selected Approach Selected Transition Transitions Available with Selected Approach EICAS Preview of Selected Approach Approach Waypoint Sequence AUDIO PANEL & CNS Load Approach? FLIGHT MANAGEMENT Figure 5-71 Approach Loading Page - Selecting the Transition HAZARD AVOIDANCE Inserted Approach Header AFCS - Approach Identifier: [approach airport].
SYSTEM OVERVIEW Flight Management Flight Plan Storage FLIGHT INSTRUMENTS The G1000 can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when the G1000 is powered off or when another flight plan is activated. Details about each stored flight plan can be viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page. Viewing information about a stored flight plan: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
Flight Management SYSTEM OVERVIEW Sort Flight Plans The stored flight plans can be sorted alphanumerically based on the flight plan name (comment) assigned to each flight plan. FLIGHT INSTRUMENTS Sorting by flight plan name (comment): 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the MENU Key. 3) Highlight ‘Sort By Comment’ and press the ENT Key. A confirmation window is displayed.
SYSTEM OVERVIEW Flight Management 3) Select the COPY Softkey; or press the MENU Key, highlight ‘Copy Flight Plan’, and press the ENT Key. The ‘Copy to Flight Plan XX?’ window is displayed. FLIGHT INSTRUMENTS 4) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Delete a Stored Flight Plan Individual or all stored flight plans can be deleted from the G1000 memory.
Flight Management SYSTEM OVERVIEW Deleting Flight Plan Items FLIGHT INSTRUMENTS Individual waypoints, entire airways, and entire procedures can be deleted from a flight plan. Some waypoints in the final approach segment (such as the FAF or MAP) can not be deleted individually. Attempting to delete a waypoint that is not allowed results in a window displaying ‘Invalid flight plan modification.
SYSTEM OVERVIEW Flight Management Deleting an individual waypoint from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. FLIGHT INSTRUMENTS 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key.
Flight Management SYSTEM OVERVIEW 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. FLIGHT INSTRUMENTS 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed.
SYSTEM OVERVIEW Flight Management entered from 1 to 99 nm in increments of 1 nm. Entering a negative offset distance results in an along track offset waypoint inserted before the selected waypoint, whereas entering a positive offset distance results in an along track offset waypoint inserted after the selected waypoint. Multiple offset waypoints are allowed.
Flight Management SYSTEM OVERVIEW Parallel Track FLIGHT INSTRUMENTS The Parallel Track (PTK) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the current flight plan. When Parallel Track is activated, the course line drawn on the map pages shows the parallel course, and waypoint names have a lower case “p” placed after the identifier. Using direct-to, loading an approach, a holding pattern, or editing and activating the flight plan automatically cancels Parallel Track.
SYSTEM OVERVIEW Flight Management Offset Direction Offset Distance FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Activation Prompt HAZARD AVOIDANCE Figure 5-76 Parallel Track Window Parallel Track Waypoints - TIFTO-p - TOP-p - SLN-p - HYS-p - LAA-p Activating Parallel Track affects the entire active flight segment (e.g.
Flight Management SYSTEM OVERVIEW results in the message ‘Parallel Track Unavailable Invalid Route Geometry’. If an approach leg is active the status indicates that the system is unable to activate the parallel track with the message ‘Parallel Track Unavailable Approach Leg Active’. If the offset direction and distance results in an unreasonable route geometry the status indicates that the system is unable to activate the parallel track because of invalid geometry.
SYSTEM OVERVIEW Flight Management Cancelling parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) FLIGHT INSTRUMENTS 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with ‘CANCEL PARALLEL TRACK?’ highlighted. 3) Press the ENT Key.
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS New Active Flight Plan Leg EICAS Confirmation Window AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-81 Active Flight Plan Page - New Active Leg Inverting a Flight Plan HAZARD AVOIDANCE Any flight plan may be inverted (reversed) for navigation back to the original departure point.
SYSTEM OVERVIEW Flight Management Flight Plan Views FLIGHT INSTRUMENTS Information about flight plans can be viewed in more than one way. The active flight plan can be configured to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan; and the active flight plan can be viewed in a narrow or wide view.
Flight Management SYSTEM OVERVIEW Active Flight Plan Narrow View Active Flight Plan Wide View FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey Figure 5-83 Active Flight Plan - Wide vs. Narrow View HAZARD AVOIDANCE Collapsing Airways The G1000 allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan Page/Window. When airways have been collapsed, it is indicated on the airway heading.
SYSTEM OVERVIEW Flight Management Q3.FEPOT Airway AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Collapsed View Expanded View Figure 5-84 Expanded/Collapsed Airways Collapsing/expanding the airways in the active flight plan: FLIGHT MANAGEMENT 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) 2) Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are collapsed/expanded.
Flight Management SYSTEM OVERVIEW 5.7 Vertical Navigation FLIGHT INSTRUMENTS Note: The G1000 supports vertical navigation for all lateral leg types except for CA, CI, FA, FM, HA, HM, PI, VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans. Current Vertical Navigation Profile EICAS The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute and teminal phases of flight.
SYSTEM OVERVIEW Flight Management Disabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. FLIGHT INSTRUMENTS 2) Select the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. EICAS Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid.
Flight Management SYSTEM OVERVIEW Activating a vertical navigation direct-to: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint. FLIGHT INSTRUMENTS Note: The selected waypoint must have a designated altitude constraint (light blue number) to be used. If not, the first waypoint in the flight plan with a designated altitude constraint is selected.
SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS White Text Light Blue Text Light Blue Subdued Text Large Altitude calculated by the system Text 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 manually. Altitude is designated for use in giving vertical speed and deviation guidance.
Flight Management SYSTEM OVERVIEW An altitude constraint is invalid if: • Meeting the constraint requires the aircraft to climb • Meeting the constraint requires the maximum flight path angle or maximum vertical speed to be exceeded FLIGHT INSTRUMENTS • The altitude constraint results in a TOD behind the aircraft present position • The constraint is within a leg type for which altitude constraints are not supported • The altitude constraint is added to the FAF of an approach that provides vertical guidan
SYSTEM OVERVIEW Flight Management 5.8 Procedures FLIGHT INSTRUMENTS The G1000 can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs), and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the Procedures (PROC) Key. AUDIO PANEL & CNS EICAS The selected procedure for the departure or arrival airport is added to the active flight plan.
Flight Management SYSTEM OVERVIEW Available Procedure Actions Departure Airport FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS Departure Preview FLIGHT MANAGEMENT Loaded Procedures Departure Choices Figure 5-88 Departure Selection Loaded Departure HAZARD AVOIDANCE Selected Departure AFCS ADDITIONAL FEATURES APPENDICES Procedure Loading Page Selection Softkeys 190-00494-02 Rev.
SYSTEM OVERVIEW Viewing available departures at an airport: FLIGHT INSTRUMENTS Flight Management 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 1) From the Airport Information Page (first page in the WPT group), select the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page.
Flight Management SYSTEM OVERVIEW Arrivals FLIGHT INSTRUMENTS A Standard Terminal Arrival (STAR) can be loaded at any airport that has one available. Only one arrival can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active flight plan, the new arrival replaces the previous arrival. The route is defined by selection of an arrival, the transition waypoints, and a runway.
SYSTEM OVERVIEW Flight Management Loaded Arrival FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Selected Arrival Procedure Loading Page Selection Softkeys Figure 5-91 Arrival Loading HAZARD AVOIDANCE Viewing available arrivals at an airport: 1) From the Airport Information Page (first page in the WPT group), select the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport Information Page.
Flight Management SYSTEM OVERVIEW Removing an Arrival from the Active Flight Plan When plans change while flying IFR, arrivals can be easily removed from the Active Flight Plan. FLIGHT INSTRUMENTS Removing an arrival from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) 2) Press the MENU Key, and highlight ‘Remove Arrival’. 3) Press the ENT Key. A confirmation window is displayed listing the arrival procedure.
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed on the G1000 PFD in the same location as the ILS glideslope using a magenta diamond. In all cases where LNAV+V is indicated by the system during an approach, LNAV minima are used.
Flight Management SYSTEM OVERVIEW Destination Airport Available Procedure Actions FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS Approach Preview FLIGHT MANAGEMENT Loaded Procedures Approach Choices Figure 5-92 Approach Selection Loaded Approach HAZARD AVOIDANCE Selected Approach AFCS ADDITIONAL FEATURES APPENDICES Procedure Loading Page Selection Softkeys LOAD or ACTIVATE? Annunciation 190-00494-02 Rev.
SYSTEM OVERVIEW Viewing available approaches at an airport: FLIGHT INSTRUMENTS Flight Management 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 1) From the Airport Information Page (first page in the WPT group), select the APR Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page.
Flight Management SYSTEM OVERVIEW In many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the destination airport. Later, if vectored to final, use the steps below to select ‘Activate Vector-To-Final’ — which makes the inbound course to the FAF waypoint active. FLIGHT INSTRUMENTS Activating a previously loaded approach with vectors to final: 1) Press the PROC Key to display the Procedures Window.
SYSTEM OVERVIEW Flight Management Course To Altitude EICAS FLIGHT INSTRUMENTS In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway centerline until the required altitude required to safely make the first turn toward the MAHP is exceeded.
Flight Management SYSTEM OVERVIEW 5.9 Trip Planning FLIGHT INSTRUMENTS The G1000 allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight planning is also available, based on fuel sensor data and the active flight plan (to estimate remaining fuel).
SYSTEM OVERVIEW Trip Statistics FLIGHT INSTRUMENTS Flight Management In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected, the waypoints are the starting and ending waypoints of the selected flight plan. The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs.
Flight Management SYSTEM OVERVIEW Fuel Statistics FLIGHT INSTRUMENTS The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already been flown. • Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the current fuel flow. • Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes.
SYSTEM OVERVIEW Selecting automatic or manual page mode: FLIGHT INSTRUMENTS Flight Management Selecting flight plan or waypoint mode: Select the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and press the ENT Key. Select the FPL Softkey or the WPTS Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints Mode’, and press the ENT Key.
Flight Management SYSTEM OVERVIEW Weight Planning Note: All weight planning page data fields display data rounded to the nearest 10 pounds or 5 kilograms.
SYSTEM OVERVIEW Flight Management 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. FLIGHT INSTRUMENTS Entering the average passenger weight: 1) Press the FMS Knob to activate the cursor and highlight the passenger weight field. 2) Turn the small FMS Knob to enter the average passenger weight. 3) Press the ENT Key to confirm the entry. EICAS 4) Press the FMS Knob to remove the flashing cursor.
Flight Management SYSTEM OVERVIEW When the aircraft is in the air and a destination waypoint has been entered, the fuel calculations can be completed. • Estimated landing weight = zero fuel weight + estimated landing fuel weight.
SYSTEM OVERVIEW Flight Management 5.10 RAIM Prediction FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches).
Flight Management SYSTEM OVERVIEW 4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. FLIGHT INSTRUMENTS 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation.
SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS SBAS Status SBAS SELECTION Box FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS - WAAS Enable/Disable SBAS Softkey (displays SBAS Selection) RAIM Softkey (displays RAIM PREDICTION) HAZARD AVOIDANCE Figure 5-100 SBAS Display - Active Enabling/Disabling SBAS: 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The SBAS SELECTION ‘WAAS’ field is highlighted. INDEX APPENDICES ADDITIONAL FEATURES AFCS 3) Press the ENT Key to disable SBAS.
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS SBAS Status SBAS SELECTION Box - WAAS Enable/Disable EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT SBAS Softkey (displays SBAS Selection) RAIM Softkey (displays RAIM PREDICTION) Figure 5-101 SBAS Display - Disabled HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Flight Management 5.11 Navigating a Flight Plan FLIGHT INSTRUMENTS The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the G1000 provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the same way, but would not include vertical guidance when the final approach course is active. nOTE: The following example flight plan is for instructional purposes only.
Flight Management SYSTEM OVERVIEW 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 5-103. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-103 Assigned Heading of 290º 4) Enter V4 into the flight plan. a) Press the FMS Knob to activate the cursor. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point (SLN) as shown in Figure 5-104. When the V4 entry point (TOP) is inserted, it is placed immediately above the highlighted waypoint (SLN).
Flight Management SYSTEM OVERVIEW d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-106. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-106 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-106, turn the small FMS Knob clockwise. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Select the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-107.
SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-108. FLIGHT MANAGEMENT Figure 5-108 List of Available Exits for V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in Figure 5-107. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE j) Press the ENT Key.
Flight Management SYSTEM OVERVIEW l) V4 is now loaded into the flight plan as shown in Figure 5-110. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-110 V4 is Loaded in the Flight Plan 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. HAZARD AVOIDANCE b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. c) Select the ACT LEG Softkey.
SYSTEM OVERVIEW Flight Management HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-112, the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active.
Flight Management SYSTEM OVERVIEW 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-113. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-113 Turn on to Active Leg HAZARD AVOIDANCE 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-114. AFCS ADDITIONAL FEATURES APPENDICES Figure 5-114 Turn to Intercept V244 INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 9) As seen in Figure 5-115, V244 is now the active flight plan leg. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-115 V244 Now Active Leg 260 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Flight Management SYSTEM OVERVIEW 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-116. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-116 HYS to LAA Leg Active HAZARD AVOIDANCE 11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises to expect an altitude of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to select OPSHN in the flight plan list.
SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-118. FLIGHT MANAGEMENT Figure 5-118 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by ATC. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 5-119.
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-120, the magenta arrow indicating the directto OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset distance and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure have no database specified altitudes, therefore, dashes are displayed.
SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-121. FLIGHT MANAGEMENT Figure 5-121 Proceudures Window APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-122. Figure 5-122 List of Available Approaches INDEX d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-122.
Flight Management SYSTEM OVERVIEW e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-123. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-123 List of Available Transitions HAZARD AVOIDANCE f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is used. g) Press the ENT Key.
FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Figure 5-124 Barometric Minimums Set INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 5-125. Figure 5-125 Loaded Approach 266 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Flight Management SYSTEM OVERVIEW 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-126. These altitudes are loaded from the database and are displayed as light blue text, indicating these values are “designated” for use in computing vertical deviation guidance. a) Press the FMS Knob to activate the cursor. b) Turn the small FMS Knob to highlight the desired altitude. c) Press the CLR Key. d) Press the FMS Knob to deactivate the cursor.
SYSTEM OVERVIEW Flight Management 14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FPA. To change the vertical flight path, perform the following steps. FLIGHT INSTRUMENTS a) Select the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 5-127.
Flight Management SYSTEM OVERVIEW 15) As seen in Figure 5-128, the aircraft is approaching TOD. Note the target vertical speed required to reached the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are now displayed on the PFD as shown in Figure 5-129.
SYSTEM OVERVIEW Flight Management EICAS FLIGHT INSTRUMENTS 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 5-130.
Flight Management SYSTEM OVERVIEW 18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5-132. 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.
SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-133. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. HAZARD AVOIDANCE Figure 5-133 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 5-134).
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 5-134 Approaching PYNON 190-00494-02 Rev.
SYSTEM OVERVIEW Flight Management HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 5-135).
Flight Management SYSTEM OVERVIEW 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude is 9,000 feet upon reaching HABUK. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-137 Descending Turn to the Initial Approach Fix (IAF) AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Flight Management HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 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.
Flight Management SYSTEM OVERVIEW 24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE” 6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-139. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-139 Descending to the Missed Approach Point HAZARD AVOIDANCE AFCS In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure.
SYSTEM OVERVIEW A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-140. The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the HSI. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS 25) Upon reaching the MAP, it is decided to execute a missed approach. Automatic waypoint sequencing is suspended past the MAP.
Flight Management SYSTEM OVERVIEW 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 5-141. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-141 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-142.
SYSTEM OVERVIEW Flight Management 5.12 Abnormal Operation FLIGHT INSTRUMENTS This section discusses the Dead Reckoning mode of operation and the subsequent indications. Note: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the G1000 stops using GPS.
Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS Distance & Bearing EICAS Dead Reckoning Annunciaion Wind Data GPS Navigation Lost Message AUDIO PANEL & CNS Track Bug (if shown) Bearing Pointer/ Distance FLIGHT MANAGEMENT Navigation Data Bar Wind Data All data except Active Leg, TAS, and DTK are in yellow HAZARD AVOIDANCE Dead Reckoning Annunciation AFCS Subdued Aircraft Symbol ADDITIONAL FEATURES Figure 5-143 Dead Reckoning Mode - GPS Derived Data Shown in Yellow APPENDICES Note: The
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Blank Page 282 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Hazard Avoidance SYSTEM OVERVIEW Section 6 Hazard Avoidance FLIGHT INSTRUMENTS The G1000 hazard avoidance features are designed to provide advisory information of potential hazards to flight safety associated with weather, terrain, and air traffic.
SYSTEM OVERVIEW Hazard Avoidance XM Satellite Radio uses the coded IDs to send an activation signal that allows the G1000 to display weather data and/or entertainment programming provided through the GDL 69A. FLIGHT INSTRUMENTS Activating the XM Satellite Weather and XM Satellite Radio Services: 1) Contact XM Satellite Radio by email (address listed on their website, www.xmradio.com) or by the customer service phone number listed on the website.
Hazard Avoidance SYSTEM OVERVIEW Using XM SATELLITE Weather Products The primary map for viewing XM Weather data is the Weather Data Link Page in the Map Page Group. This is the only G1000 map display capable of showing information for all available XM weather products. FLIGHT INSTRUMENTS Viewing 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.
SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS This table shows the weather product symbols, the expiration time and the refresh rate. The refresh rate represents the interval at which XM Satellite Radio broadcasts new signals that may or may not contain new weather data. It does not represent the rate at which weather data is updated or new content is received by the Data Link Receiver.
Hazard Avoidance SYSTEM OVERVIEW Cloud Top (CLD TOP) + Echo Top (ECHO TOP) + Nearest Page Group Flight Plan Pages + AUX - Trip Planning Page Weather Data Link Page + Weather Information Page Navigation Map Page + + + + + + + + + + Cell Movement (CELL MOV) + + + + + + + + + METARs + City Forecast (CITY) + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + Winds Aloft (WIND) + County Warnings (COUNTY) + Cyclone Warnings (CYCLONE) + Radar Coverage TFRs + + +
SYSTEM OVERVIEW Hazard Avoidance Weather Softkeys on the Weather Data Link Page FLIGHT INSTRUMENTS Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (The figure shows the weather product softkeys for the Weather Data Link Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product is enabled. Unavailable weather products have subdued softkey labels (softkeys are disabled from selection).
Hazard Avoidance SYSTEM OVERVIEW Setting up and customizing the Weather Data Link Page: 1) Select the Weather Data Link Page with the FMS Knob. 2) On the Weather Data Link Page press the MENU Key. FLIGHT INSTRUMENTS 3) Select the Weather Setup option on the Page Menu and press the ENT Key. 4) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 5) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).
SYSTEM OVERVIEW Hazard Avoidance Maps other than the Weather Data Link Page use settings based on those selected for the Navigation Map Page. FLIGHT INSTRUMENTS Setting up and customizing weather data for the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-5). 4) Turn the small FMS Knob to select the Weather Group and press the ENT Key (Figure 6-6).
Hazard Avoidance SYSTEM OVERVIEW Each active weather product has an associated legend which can be displayed on the Weather Data Link Page. Viewing legends for displayed weather products FLIGHT INSTRUMENTS 1) Select the Weather Data Link Page with the FMS Knob. 2) Select the LEGEND Softkey to display the legends for the displayed weather products. Or: 1) Press the MENU Key. EICAS 2) Select Weather Legend and press the ENT Key. 3) Turn the FMS Knob to scroll through the legends.
SYSTEM OVERVIEW NEXRAD FLIGHT INSTRUMENTS Hazard Avoidance WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar systems that are operated by the National Weather Service (NWS). NEXRAD data provides centralized meteorological information for the continental United States and selected overseas locations. The maximum range of a single NEXRAD radar site is 250 nm.
Hazard Avoidance SYSTEM OVERVIEW Displaying NEXRAD weather information: 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link Page. FLIGHT INSTRUMENTS 2) Select the NEXRAD Softkey. Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reflectivity from the individual radar sweeps. The display of the information is color-coded to indicate the weather severity level.
SYSTEM OVERVIEW Hazard Avoidance Reflectivity FLIGHT INSTRUMENTS Reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the NEXRAD display directly correlate to the level of detected reflectivity. Reflectivity as it relates to hazardous weather can be very complex. The role of radar is essentially to detect moisture in the atmosphere. Simply put, certain types of weather reflect radar better than others.
Hazard Avoidance SYSTEM OVERVIEW The following may cause abnormalities in displayed NEXRAD radar images: • Ground clutter • Strobes and spurious radar data FLIGHT INSTRUMENTS • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows • Metallic dust from military aircraft, which can cause alterations in radar scans NEXRAD Limitations (Canada) EICAS • Radar coverage extends to 55ºN.
SYSTEM OVERVIEW ECHO TOPs FLIGHT INSTRUMENTS Hazard Avoidance Echo Tops data shows the location, elevation, and direction of the highest radar echo. The highest radar echo does not indicate the top of a storm or clouds; rather it indicates the highest altitude at which precipitation is detected. Information is derived from NEXRAD data. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Note: Display of Echo Tops is mutually exclusive with Cloud Tops and NEXRAD.
Hazard Avoidance SYSTEM OVERVIEW Displaying Echo Tops information: 1) Select the Weather Data Link Page with the FMS Knob. 2) Select the ECHO TOPS Softkey. FLIGHT INSTRUMENTS To display the Echo Tops legend, select the LEGEND Softkey when Echo Tops is selected for display. Since Echo Tops and Cloud Tops use the same color scaling to represent altitude, display of these weather products is mutually exclusive. When Echo Tops is activated, NEXRAD and Cloud Tops data are removed.
SYSTEM OVERVIEW Hazard Avoidance Cloud TOPs FLIGHT INSTRUMENTS Note: Cloud Tops and Echo Tops cannot be displayed at the same time. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Cloud Tops data depicts cloud top altitudes as determined from satellite imagery. Figure 6-15 Cloud Tops Data AFCS Displaying Cloud Tops information: 1) Select the Weather Data Link Page with the FMS Knob. 2) Select the CLD TOP Softkey.
Hazard Avoidance SYSTEM OVERVIEW XM Lightning FLIGHT INSTRUMENTS Lightning data shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. The exact location of the lightning strike is not displayed.
SYSTEM OVERVIEW Displaying XM Lightning information: FLIGHT INSTRUMENTS Hazard Avoidance 2) Select the XM LTNG Softkey (LTNG Softkey on the Weather Data Link Page). 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link Page. EICAS To display the XM Lightning legend on the Weather Data Link Page, select the LEGEND Softkey when XM Lightning is selected for display.
Hazard Avoidance SYSTEM OVERVIEW Displaying Cell Movement information: 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link Page. FLIGHT INSTRUMENTS 2) Select the NEXRAD Softkey (CEL MOV Softkey on the Weather Data Link Page). For Cell Movement to be displayed on maps other than the Weather Data Link Page, Cell Movement must be turned on in the Navigation Map Setup Menu (see “Setting Up XM Satellite Weather”).
SYSTEM OVERVIEW Hazard Avoidance Displaying SIGMETs and AIRMETs: 1) Select the Weather Data Link Page with the FMS Knob. FLIGHT INSTRUMENTS 2) Select the SIG/AIR Softkey. 3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon. 4) Press the ENT key. The figure below shows a sample of SIGMET text.
Hazard Avoidance SYSTEM OVERVIEW Instructions for Viewing METAR and TAF Text FLIGHT INSTRUMENTS Selected Airport EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-23 METAR Flags on the Weather Data Link Page TAF (Terminal Area Forecast) is the standard format for 24-hour weather forecasts. TAFs may contain some METAR data, but generally cover a smaller area. It typically forecasts significant weather changes, temporary changes, probable changes, and expected changes in weather conditions.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance EICAS METAR Text AUDIO PANEL & CNS METAR Symbol FLIGHT MANAGEMENT TAF Text HAZARD AVOIDANCE Figure 6-24 METAR with Text ADDITIONAL FEATURES AFCS To display the METAR legend on the Weather Data Link Page, select the LEGEND Softkey when METARs are selected for display. The METAR flag color is determined by the information in the METAR text. The METAR flag is gray when the METAR text does not contain adequate information.
Hazard Avoidance SYSTEM OVERVIEW Surface Analysis and City Forecast Note: Surface Analysis and City Forecast data are displayed only within the installed Aviation Database FLIGHT INSTRUMENTS service area. Surface Analysis and City Forecast information is available for current and forecast weather conditions. Forecasts are available for intervals of 12, 24, 36, and 48 hours.
SYSTEM OVERVIEW Hazard Avoidance EICAS FLIGHT INSTRUMENTS To display the Surface Analysis and City Forecast legend, select the LEGEND Softkey when Surface Analysis and City Forecast are selected for display. Figure 6-27 Surface Analysis Legend AUDIO PANEL & CNS Freezing Level APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Freezing Level data shows the color-coded contour lines for the altitude and location at which the first isotherm is found.
Hazard Avoidance SYSTEM OVERVIEW Displaying Freezing Level information: 1) Select the Weather Data Link Page with the FMS Knob. 2) Select the MORE WX Softkey. FLIGHT INSTRUMENTS 3) Select the FRZ LVL Softkey. To display the Freezing Level legend, select the LEGEND Softkey when Freezing Level data is selected to be displayed.
FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance Figure 6-30 Winds Aloft at 27,000 Feet AFCS HAZARD AVOIDANCE To display the Winds Aloft legend, select the LEGEND Softkey when Winds Aloft is selected for display. INDEX APPENDICES ADDITIONAL FEATURES Figure 6-31 Winds Aloft Data with Legend 308 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Hazard Avoidance SYSTEM OVERVIEW County Warnings FLIGHT INSTRUMENTS County data provides specific public awareness and protection weather warnings from the National Weather Service (NWS). This can include information on fires, tornadoes, severe thunderstorms, flood conditions, and other natural disasters.
SYSTEM OVERVIEW Hazard Avoidance Cyclone AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS The Cyclone weather product shows the current location of cyclones (hurricanes) and their projected tracks. FLIGHT MANAGEMENT Cyclone HAZARD AVOIDANCE Figure 6-34 Cyclone Data Selected for Display Displaying cyclone (hurricane) track information: 1) Select the Weather Data Link Page with the FMS Knob. 2) Select the MORE WX Softkey. AFCS 3) Select the CYCLONE Softkey.
Hazard Avoidance SYSTEM OVERVIEW 6.2 Airborne Color Weather Radar System Description FLIGHT INSTRUMENTS The Garmin GWX 68 Airborne Color Weather Radar is a four-color digital pulsed radar with 6.5 kilowatts of output power. It combines excellent range and adjustable scanning profiles with a high-definition target display. The pulse width is four microseconds (µs) on all ranges except the 2.5 nm range.
SYSTEM OVERVIEW Hazard Avoidance NEXRAD and Airborne Weather Radar FLIGHT INSTRUMENTS Both Airborne Weather Radar and NEXRAD measure weather reflectivity in decibels (dB). A decibel is a logarithmic expression of the ratio of two quantities. Airborne Weather Radar measures the ratio of power against the gain of the antenna, while NEXRAD measures the energy reflected back to the radar, or the radar reflectivity ratio.
Hazard Avoidance SYSTEM OVERVIEW Radar Signal Attenuation FLIGHT INSTRUMENTS The phenomenon of radar signal attenuation affects the operation of weather radar. When the radar signal is transmitted, it is progressively absorbed and scattered, making the signal weaker. This weakening, or attenuation, is caused by two primary sources, distance and precipitation.
SYSTEM OVERVIEW Hazard Avoidance Radar Signal Reflectivity Precipitation HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Precipitation or objects more dense than water, such as the surface of the earth or solid structures, are detected by the weather radar. The weather radar does not detect clouds, thunderstorms, or turbulence directly. It detects precipitation associated with clouds, thunderstorms, and turbulence.
Hazard Avoidance SYSTEM OVERVIEW Ground Returns FLIGHT INSTRUMENTS The intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (Angle of Incidence) and the reflective properties of that target. The gain can be adjusted so shorelines, rivers, lakes, and cities are well-defined. Increasing the gain too much causes the display to fill in between targets, thus obscuring some landmarks. EICAS Cities normally provide a strong return signal.
SYSTEM OVERVIEW Hazard Avoidance Safe Operating Distance FLIGHT INSTRUMENTS The following information establishes a minimum safe distance from the antenna for personnel near operating weather radar. The minimum safe distance is based on the FCC’s exposure limit at 9.3 to 9.5 GHz for general population/uncontrolled environments, which is 1 mW/cm2. See Advisory Circular 20-68B for more information on safe distance determination.
Hazard Avoidance SYSTEM OVERVIEW Practical Application Using the Basic Tilt Setup FLIGHT INSTRUMENTS With the antenna tilt set as previously described, any displayed target return should be scrutinized when flying at altitudes between 2,000 and 30,000 feet AGL. If the displayed target advances on the screen to within 5 nautical miles of the aircraft, avoid it. This may be either weather or ground returns that are 2,000 feet or less below the aircraft.
SYSTEM OVERVIEW Hazard Avoidance Weather Mapping and Interpretation Weather Display Interpretation AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS When evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates shown in the table. Weather Mode Color Intensity Black Green Yellow Red Magenta < 23 dBZ 23 dBZ to < 32 dBZ 32 dBZ to < 41 dBZ 41 dBZ to < 50 dBZ 50 dBZ and greater Approximate Precipitation Rate (in/hr.) < .01. .01 - 0.1. 0.1 - 0.5 0.
Hazard Avoidance SYSTEM OVERVIEW Along squall lines (multiple cells or clusters of cells in a line) individual cells may be in different stages of development. Areas between closely spaced, intense targets may contain developing clouds not having enough moisture to produce a return. However, these areas could have strong updrafts or downdrafts. Targets showing wide areas of green are generally precipitation without severe turbulence.
SYSTEM OVERVIEW Hazard Avoidance EICAS FLIGHT INSTRUMENTS In areas of multiple heavy cells, use the Vertical Scan feature along with antenna tilt management to examine the areas. Remember to avoid shadowed areas behind targets. AUDIO PANEL & CNS The Blind Alley at Close Range The Large Storm Behind Figure 6-44 The Blind Alley FLIGHT MANAGEMENT Tornadoes There are no conclusive radar target return characteristics which identify a tornado.
Hazard Avoidance SYSTEM OVERVIEW Hail shafts are associated with the same radar target return characteristics as tornados. U-shaped cloud edges three to seven miles across can also indicate hail. These target returns appear quite suddenly along any edge of the cell outline. They also change in intensity and shape in a matter of seconds, making vigilant monitoring essential. FLIGHT INSTRUMENTS Operation in Weather Mode WARNING: Begin transmitting only when it is safe to do so.
SYSTEM OVERVIEW Hazard Avoidance Displaying weather on the Weather Radar Page: 1) Select the Weather Radar Page in the Map Page Group with the FMS Knob. FLIGHT INSTRUMENTS 2) Select the MODE Softkey. 3) While on the ground, select the STANDBY Softkey. A one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar enters the Standby Mode. a) Select the WEATHER Softkey. A confirmation window is displayed.
Hazard Avoidance SYSTEM OVERVIEW Vertically scanning a storm cell: NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant FLIGHT INSTRUMENTS adjustment of the Bearing Line. 1) While in the Horizontal Scan view, select the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. Press the ENT Key.
AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance FLIGHT MANAGEMENT Figure 6-48 Vertical Scan Display Adjusting Antenna Tilt Angle HAZARD AVOIDANCE In order to make an accurate interpretation of a storm cell, the radar beam should be pointed at the wet part of the weather cell to record the proper rainfall intensity (color level). The ideal aiming point is just below the freezing level of the storm. The best way to find this point is to use the Vertical Scan feature.
Hazard Avoidance SYSTEM OVERVIEW Adjusting antenna tilt on the Vertical Scan display: 1) Select the TILT Softkey to activate the cursor in the TILT field and display the Tilt Line. FLIGHT INSTRUMENTS If the Tilt Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Tilt Line. Press the ENT Key. 2) Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is again selected.
SYSTEM OVERVIEW Hazard Avoidance Adjusting Gain WARNING: Changing the gain in weather mode causes precipitation intensity to be displayed as a color FLIGHT INSTRUMENTS not representative of the true intensity. Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation. 1) Select the GAIN Softkey to activate the cursor in the GAIN field. EICAS 2) Turn the small FMS Knob to adjust the gain for the desirable level.
Hazard Avoidance SYSTEM OVERVIEW Sector Scan FLIGHT INSTRUMENTS 1) While in horizontal scan mode, select the BRG Softkey to display the Bearing Line and place the cursor in the BEARING field. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. 2) Press the ENT Key.
AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance FLIGHT MANAGEMENT Figure 6-52 40˚ Sector Scan Antenna Stabilization 1) To activate or deactivate the antenna stabilization, select the MODE Softkey. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display.
Hazard Avoidance SYSTEM OVERVIEW Weather Attenuated Color Highlight (WATCH®) EICAS AUDIO PANEL & CNS Displayed intensity is questionable. Potentially stronger than displayed. FLIGHT INSTRUMENTS WATCH® identifies deceptively strong or unknown intensity parts of a storm. While in horizontal scan mode, this feature can be used as a tool to determine areas of possible inaccuracies in displayed intensity due to weakening of the radar energy. This weakening is known as attenuation.
SYSTEM OVERVIEW Hazard Avoidance Weather Alert FLIGHT INSTRUMENTS The Weather Alert feature indicates the presence of heavy precipitation between the ranges of 80 and 320 nm regardless of the currently displayed range. Weather Alert targets appear as red bands along the outer range ring at the approximate azimuth of the detected returns. If a Weather Alert is detected within ±10° of the aircraft heading, an alert is displayed on the PFD in the Messages Window.
Hazard Avoidance SYSTEM OVERVIEW Ground Mapping and Interpretation FLIGHT INSTRUMENTS A secondary use of the weather radar system is for the presentation of terrain. This can be a useful tool for verifying aircraft position. A picture of the ground is represented much like a topographical map that can be used as a supplement to the navigation map on the MFD. EICAS Ground Map mode uses a different gain range than Weather mode. Different colors are also used to represent the intensity levels.
SYSTEM OVERVIEW Hazard Avoidance 6.3 Terrain Awareness & Warning System (TAWS) Warning: Do not use TAWS information for primary terrain avoidance. TAWS is intended only to enhance FLIGHT INSTRUMENTS situational awareness. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South. NOTE: The data contained in the TAWS databases comes from government agencies.
Hazard Avoidance SYSTEM OVERVIEW Displaying TAWS Data FLIGHT INSTRUMENTS TAWS uses yellow (caution) and red (warning) to depict terrain and obstacles with heights greater than 200 feet above ground level, AGL. Alerts are given relative to aircraft altitude. Colors are adjusted automatically as the aircraft altitude changes. The colors and symbols shown in the figure and table below are used to represent terrain, obstacles, and potential impact points.
SYSTEM OVERVIEW Hazard Avoidance Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings and cautions are issued are shown when terrain is selected for display and the map range is within the setting limit. FLIGHT INSTRUMENTS Maps other than the TAWS Page use settings based on those selected for the Navigation Map Page. The maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation Map.
Hazard Avoidance SYSTEM OVERVIEW TAWS Page FLIGHT INSTRUMENTS The TAWS Page is specialized to show terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest potential point of impact on the TAWS Page.
SYSTEM OVERVIEW Hazard Avoidance Map Orientation FLIGHT INSTRUMENTS Current Aircraft GPSderived MSL Altitude Map Range Rings EICAS Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) Red Terrain (Above or Within 100’ Below the Aircraft Altitude) AUDIO PANEL & CNS Black Terrain (More than 1000’ Below the Aircraft Altitude) Terrain Legend FLIGHT MANAGEMENT Figure 6-60 TAWS Page, 360º View Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) HAZARD AVOIDANCE Red Terr
Hazard Avoidance SYSTEM OVERVIEW TAWS Alerts FLIGHT INSTRUMENTS Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms. TAWS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-6 shows TAWS alert types with corresponding annunciations and aural messages. When an alert is issued, annunciations appear on the PFD and MFD.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Potential Impact Point Alert Annunciation HAZARD AVOIDANCE Figure 6-64 TAWS PULL UP Alert Annunciation on the MFD TAWS Inhibit ADDITIONAL FEATURES AFCS PDA and FLTA aural and visual alerts can be manually inhibited. Use caution when inhibiting TAWS as the system should be enabled when appropriate. When TAWS is inhibited, the alert annunciation TAWS INHB is shown on the PFD and MFD.
Hazard Avoidance MFD Pop-Up Alert Aural Message Excessive Descent Rate Warning (EDR) “Pull Up” or * “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”* or “Terrain, Terrain; Pull Up, Pull Up” or * “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”* or “Obstacle, Obstacle; Pull Up, Pull Up” Imminent Obstacle Impact Warning (IOI) Reduced Required Terrain Clearance Caution (RTC) “Terrain Ahead; Terrain Ahead”* or “Caution, Terrain; Caution, Terrain” * “Terrain Ahead; Terrain Ahead”* or “Caution, Terra
SYSTEM OVERVIEW Hazard Avoidance Excessive Descent Rate Alert FLIGHT INSTRUMENTS The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. The following figure shows the parameters for the alert as defined by TSO-C151b.
Hazard Avoidance SYSTEM OVERVIEW Forward Looking Terrain Avoidance The Forward Looking Terrain Avoidance (FLTA) alert is used by TAWS and is composed of: FLIGHT INSTRUMENTS • Reduced Required Terrain Clearance and Reduced Required Obstacle Clearance Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values.
SYSTEM OVERVIEW Premature Descent Alerting FLIGHT INSTRUMENTS Hazard Avoidance PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.5 nm from the runway threshold or is at an altitude of 125 feet AGL while within 1.0 nm of the threshold. During the final descent, algorithms set a threshold for alerting based on speed, distance, and other parameters.
Hazard Avoidance SYSTEM OVERVIEW Negative Climb Rate After Takeoff Alert (NCR) FLIGHT INSTRUMENTS The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”) provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display.
SYSTEM OVERVIEW Hazard Avoidance System Status FLIGHT INSTRUMENTS During G1000 power-up, TAWS conducts a self-test of its aural and visual annunciations. The system test can also be manually initiated. An aural alert is issued at test completion. TAWS System Testing is disabled when ground speed exceeds 30 knots.
Hazard Avoidance SYSTEM OVERVIEW 6.4 Traffic Information Service (TIS) FLIGHT INSTRUMENTS WARNING: The Traffic Information Service (TIS) is intended for advisory use only. TIS is intended to help the pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic. NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar EICAS site.
SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS The altitude difference between the requesting aircraft and other intruder aircraft is displayed above/below the traffic symbol in hundreds of feet. If the other aircraft is above the requesting aircraft, the altitude separation appears above the traffic symbol; if below, the altitude separation appears below. Altitude trend is displayed as an up/down arrow (for speeds greater than 500 fpm in either direction) to the right of the target symbol.
Hazard Avoidance SYSTEM OVERVIEW Displaying traffic information (PFD Inset Map): 1) Select the INSET Softkey. 2) Select the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). FLIGHT INSTRUMENTS 3) Select the softkey again to display the traffic-only inset (TRFC-2). 4) Select the softkey again to remove traffic data. Customizing traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. EICAS 2) Press the MENU Key.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Figure 6-71 Navigation Map Page Menu Figure 6-72 Navigation Map Page Setup Menu Figure 6-73 Navigation Map Page Setup Menu, Traffic Group HAZARD AVOIDANCE The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of traffic. The setup menu also controls the map range settings above which traffic data (symbols and labels) are decluttered from the display.
Hazard Avoidance SYSTEM OVERVIEW 3) Confirm TIS is in Operating Mode: Select the OPERATE Softkey to begin displaying traffic. Or: FLIGHT INSTRUMENTS a) Press the MENU Key. b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT Key.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance AUDIO PANEL & CNS EICAS Inset Map Displays When TA is Detected Figure 6-75 Traffic Annunciation (PFD) A “TIS Not Available” (TNA) voice alert is generated when the TIS service becomes unavailable or is out of range.
Hazard Avoidance SYSTEM OVERVIEW System Status Traffic Map Page Annunciation NO DATA FAILED Description Data is not being received from the transponder* Data is being received from the transponder, but a failure is detected in the data stream* EICAS DATA FAILED FLIGHT INSTRUMENTS The G1000 performs an automatic test of TIS during power-up. If TIS passes the test, TIS enters Standby Mode (on the ground) or Operating Mode (in the air).
SYSTEM OVERVIEW Hazard Avoidance AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the ground, TIS automatically enters Standby Mode. If traffic is selected for display on another map while Standby Mode is selected, the traffic display enabled icon is crossed out (also the case whenever TIS has failed). Once the aircraft is airborne, TIS switches to Operating Mode and traffic information is displayed.
Hazard Avoidance SYSTEM OVERVIEW The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed (Table 6-13). Traffic Status Banner Annunciation TA X.
SYSTEM OVERVIEW Hazard Avoidance 6.5 Traffic Advisory System (TAS) FLIGHT INSTRUMENTS NOTE: TIS is disabled when Traffic Advisory System (TAS) is installed. Refer to the Honeywell® KTA 870 Pilot’s Guide for a detailed discussion of the KTA 870 TAS. TAS Symbology EICAS Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an onboard interrogator-processor and the Mode S transponder for the air-to-air traffic data link.
Hazard Avoidance SYSTEM OVERVIEW Operation The KTA 870 must be in Operating Mode for traffic to be displayed. The unit starts in Operating Mode upon power-up. FLIGHT INSTRUMENTS Selecting the STANDBY Softkey forces the unit into Standby Mode. Selecting the NORMAL Softkey allows the KTA 870 to switch from Standby Mode to Operating Mode as necessary.
SYSTEM OVERVIEW Hazard Avoidance Operating Mode Altitude Mode FLIGHT INSTRUMENTS Traffic Display Range Traffic Advisory, Aircraft is 400’ Below, Climbing AUDIO PANEL & CNS EICAS “Non-Bearing” Traffic (Bearing Undetermined), Distance 8.
Hazard Avoidance SYSTEM OVERVIEW Displaying traffic on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is now displayed on the map as shown in the figure.
SYSTEM OVERVIEW Hazard Avoidance 3) To return to the Traffic Page, select the BACK Softkey. Or: FLIGHT INSTRUMENTS 1) Press the MENU Key. EICAS 2) Turn the small FMS Knob to select one of the following: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) 3) Select the ENT Softkey. AUDIO PANEL & CNS Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time.
Hazard Avoidance SYSTEM OVERVIEW 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page. FLIGHT INSTRUMENTS EICAS Figure 6-79 Navigation Map Page Menu AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-81 Navigation Map Page Setup Menu, Traffic Group HAZARD AVOIDANCE Figure 6-80 Navigation Map Page Setup Menu The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map range settings.
SYSTEM OVERVIEW Hazard Avoidance TAS Alerts FLIGHT INSTRUMENTS NOTE: Refer to the KTA 870 documentation for information on alerts generated by the TAS equipment. When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A “Traffic, Traffic” voice alert is generated when the first TA is displayed.
Hazard Avoidance SYSTEM OVERVIEW If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance Blank Page 362 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Automatic Flight Control System SYSTEM OVERVIEW Section 7 Automatic Flight Control System FLIGHT INSTRUMENTS Note: The approved Airplane Flight Manual (AFM) always supersedes this Pilot’s Guide. The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G1000 System avionics architecture. The System Overview section provides a block diagram to support this system description.
SYSTEM OVERVIEW Automatic Flight Control System 7.1 AFCS Controls The AFCS Control Unit is positioned above the MFD, and has the following controls: FLIGHT INSTRUMENTS 1 2 3 Selects/deselects Heading Select Mode NAV Key FD Key Selects/deselects Navigation Mode Activates/deactivates the flight director only Pressing once turns on the selected flight director in the default vertical and lateral modes. Pressing again deactivates the flight director and removes the Command Bars.
Automatic Flight Control System SYSTEM OVERVIEW The following AFCS controls are located separately from the AFCS Control Unit: An AP DISC Switch is located on each control wheel. This switch may be used to acknowledge an autopilot disconnect alert and mute the associated aural tone.
SYSTEM OVERVIEW Automatic Flight Control System 7.2 Flight Director Operation FLIGHT INSTRUMENTS The flight director function provides pitch and roll commands to the AFCS and displays them on the PFDs. With the flight director active, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (±20°) and roll (30°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification.
Automatic Flight Control System SYSTEM OVERVIEW AFCS Status Box Lateral Modes Yaw Autopilot Damper Status Status FLIGHT INSTRUMENTS Flight director mode annunciations are displayed on the PFDs when the flight director is active. Flight director selection and autopilot and yaw damper statuses are shown in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left and vertical on the right. Armed modes are displayed in white and active in green.
SYSTEM OVERVIEW Automatic Flight Control System Flight Director Modes FLIGHT INSTRUMENTS 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 modes(s).
Automatic Flight Control System SYSTEM OVERVIEW Command Bars FLIGHT INSTRUMENTS Upon activation of the flight director, Command Bars are displayed in magenta on the PFDs as single cues or cross pointers. The Aircraft Symbol (in yellow) changes to accommodate the Command Bar format; the Command Bars do not override the Aircraft Symbol. The single-cue Command Bars (Figure 7-5) move together vertically to indicate pitch commands and bank left or right to indicate roll commands.
SYSTEM OVERVIEW Automatic Flight Control System 7.3 Vertical Modes FLIGHT INSTRUMENTS Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/DN Wheel can be used to change the vertical mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode.
Automatic Flight Control System SYSTEM OVERVIEW Pitch Hold Mode (PIT) FLIGHT INSTRUMENTS When the flight director is activated (the FD Key is pressed) or switched (the XFR Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active vertical mode by the ‘PIT’ annunciation. 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 Pitch Hold Mode is activated.
SYSTEM OVERVIEW Automatic Flight Control System Selected Altitude Capture Mode (ALTS) FLIGHT INSTRUMENTS Selected Altitude Capture Mode is automatically armed with activation of the following modes: • Pitch Hold • Go Around • Vertical Speed • Vertical Path Tracking (if the Selected Altitude is to be captured instead of the VNV Target Altitude) • Flight Level Change EICAS The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-7 for example).
Automatic Flight Control System SYSTEM OVERVIEW Altitude Hold Mode (ALT) FLIGHT INSTRUMENTS Altitude Hold Mode can be activated by pressing the ALT Key; the flight director maintains the current aircraft altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box.
SYSTEM OVERVIEW Automatic Flight Control System Vertical Speed Mode (VS) FLIGHT INSTRUMENTS In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference. Current aircraft vertical speed (to the nearest 100 fpm) becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation.
Automatic Flight Control System SYSTEM OVERVIEW Flight Level Change Mode (FLC) NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode. FLIGHT INSTRUMENTS Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the Airspeed Reference (in IAS or Mach) while climbing or descending to the Selected Altitude (shown above the Altimeter).
SYSTEM OVERVIEW Changing the Airspeed Reference FLIGHT INSTRUMENTS Automatic Flight Control System • Using the NOSE UP/DN Wheel The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be adjusted by: • Pressing the CWS Button, hand-flying the aircraft to attain a new Airspeed Reference, then releasing the CWS Button NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.
Automatic Flight Control System SYSTEM OVERVIEW Airspeed Reference units can be manually toggled between IAS and Mach units using the SPD Key. When the FLC Airspeed Reference is displayed in Mach, the Airspeed Reference Bug is displayed on the Airspeed Indicator at the IAS corresponding to the selected Mach target speed and the current Mach number is shown below the Airspeed Indicator.
SYSTEM OVERVIEW Automatic Flight Control System Vertical Navigation Modes (VPTH, ALTV) FLIGHT INSTRUMENTS Note: VNV is disabled when parallel track or Dead Reckoning Mode is active. Note: The Selected Altitude takes precedence over any other vertical constraints. EICAS Vertical Navigation (VNV) flight control is available for enroute/terminal cruise and descent operations any time that VNV flight planning is available.
Automatic Flight Control System SYSTEM OVERVIEW Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude by at least 75 feet.
SYSTEM OVERVIEW Automatic Flight Control System When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes active and tracks the descent profile (Figure 7-15). An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate.
Automatic Flight Control System SYSTEM OVERVIEW Automatic Reversion to Pitch Hold Mode Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: FLIGHT INSTRUMENTS • Vertical deviation exceeds 200 feet during an overspeed condition. • Vertical deviation experiences a discontinuity that both exceeds 200 feet in magnitude and results in the vertical deviation exceeding 200 feet in magnitude.
SYSTEM OVERVIEW Automatic Flight Control System VNV Target Altitude Capture Mode (ALTV) Note: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive. However, FLIGHT INSTRUMENTS Selected Altitude Capture Mode is armed implicitly (not annunciated) whenever VNV Target Altitude Capture Mode is armed.
Automatic Flight Control System SYSTEM OVERVIEW Glidepath Mode (GP) NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot FLIGHT INSTRUMENTS guides the aircraft back to the glidepath upon release of the CWS Button. Glidepath Mode is used to track the WAAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box.
SYSTEM OVERVIEW Automatic Flight Control System Glidepath Mode Active AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS GPS Approach Mode Active FLIGHT MANAGEMENT GPS is Selected LPV Approach Navigation Active Source Command Bars to Indicate Descent on Glidepath INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 7-19 Glidepath Mode Glidepath Indicator 384 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Automatic Flight Control System SYSTEM OVERVIEW Glideslope Mode (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot FLIGHT INSTRUMENTS guides the aircraft back to the glideslope upon release of the CWS Button. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director mode.
SYSTEM OVERVIEW Automatic Flight Control System Takeoff (TO) and Go Around (GA) Modes FLIGHT INSTRUMENTS Go Around and Takeoff modes are coupled pitch and roll modes and are annunciated as both the vertical and lateral modes when active. In these modes, the flight director commands a constant set pitch attitude and keeps the wings level. The GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground.
Automatic Flight Control System SYSTEM OVERVIEW 7.
SYSTEM OVERVIEW Automatic Flight Control System Roll Hold Mode (ROL) Note: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings FLIGHT INSTRUMENTS level. EICAS When the flight director is activated or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle condition.
Automatic Flight Control System SYSTEM OVERVIEW Heading Select Mode (HDG) FLIGHT INSTRUMENTS Heading Select Mode is activated by pressing the 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. Changing the Selected Heading Note: Pressing the HDG Knob synchronizes the Selected Heading to the current heading.
SYSTEM OVERVIEW Automatic Flight Control System Navigation Modes (GPS, VOR, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the FLIGHT INSTRUMENTS flight director to enter Navigation Mode. EICAS Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected navigation source.
Automatic Flight Control System SYSTEM OVERVIEW Changing the Selected Course FLIGHT INSTRUMENTS If the navigation source is VOR or localizer or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob corresponding to the selected flight director (CRS1 for the pilot side, CRS2 for the copilot side). Pressing the CWS Button and hand-flying the aircraft does not change the Selected Course while in Navigation Mode.
SYSTEM OVERVIEW Automatic Flight Control System Approach Modes (GPS, VAPP, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the FLIGHT INSTRUMENTS flight director to enter Approach Mode. EICAS Approach Mode is activated when the APR Key is pressed. Approach Mode acquires and tracks the selected navigation source (GPS, VOR, or LOC), depending on loaded approach.
Automatic Flight Control System SYSTEM OVERVIEW LOC Approach Mode allows the autopilot to fly a LOC/ILS approach with a glideslope. When LOC Approach Mode is armed, Glideslope Mode is also armed automatically. LOC captures are inhibited if the difference between aircraft heading and localizer course exceeds 105°. FLIGHT INSTRUMENTS Selecting LOC Approach Mode: 1) Ensure a valid localizer frequency is tuned.
SYSTEM OVERVIEW Backcourse Mode (BC) FLIGHT INSTRUMENTS Automatic Flight Control System Backcourse Mode captures and tracks a localizer signal in the backcourse direction. 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. If the CDI is less than one dot, Backcourse Mode is automatically captured when the BC Key is pressed.
Automatic Flight Control System SYSTEM OVERVIEW 7.5 Autopilot and Yaw Damper Operation NOTE: Refer to the AFM for specific instructions regarding emergency procedures. FLIGHT INSTRUMENTS The Cessna Citation Mustang’s autopilot and yaw damper operate the 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.
SYSTEM OVERVIEW Automatic Flight Control System Engagement NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use FLIGHT INSTRUMENTS the CWS Button to disengage the pitch and roll servos while the autopilot remains active. Note: The autopilot cannot be engaged if the yaw damper has failed.
Automatic Flight Control System SYSTEM OVERVIEW Disengagement FLIGHT INSTRUMENTS The autopilot is manually disengaged by pushing the AP Key on the AFCS Control Unit, the GA Switch, or the MEPT ARM Switch. Manual autopilot disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation and a three-second autopilot disconnect aural alert. Figure 7-33 Manual Autopilot Disengagement EICAS Pushing the AP DISC Switch or YD Key disengages both the yaw damper and the autopilot.
SYSTEM OVERVIEW Automatic Flight Control System 7.6 Example Flight Plan FLIGHT INSTRUMENTS Note: The following example flight plan and diagrams (not to be used for navigation) in this section are for instructional purposes only and should be considered not current. Numbered portions of accompanying diagrams correspond to numbered procedure steps.
Automatic Flight Control System SYSTEM OVERVIEW Departure Climbing to the Selected Altitude and flying an assigned heading: FLIGHT INSTRUMENTS 1) Before takeoff: a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet. b) Push the GA Switch to activate Takeoff Mode. The flight director Command Bars establish a pitch up attitude to follow. EICAS c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Automatic Flight Control System HD GM od EICAS e AUDIO PANEL & CNS TO M ode 3 Selected Altitude of 12,000 MSL ALT Mode 4 FLIGHT MANAGEMENT KMKC 2 1 VS e Mod ode M TO INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 7-37 Departure 400 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Automatic Flight Control System SYSTEM OVERVIEW Intercepting a VOR Radial FLIGHT INSTRUMENTS 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. In this scenario, VOR Navigation Mode is used for navigation to the first VOR waypoint in the flight plan.
SYSTEM OVERVIEW Automatic Flight Control System Flying a Flight Plan/GPS Course Note: Changing the navigation source cancels Navigation Mode and causes the flight director to revert FLIGHT INSTRUMENTS back to Roll Hold Mode (wings rolled level). As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is currently tracking inbound on Airway V4.
Automatic Flight Control System SYSTEM OVERVIEW Descent While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for descent: FLIGHT INSTRUMENTS • Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a constant airspeed. This descent method does not account for flight plan waypoint altitude constraints.
SYSTEM OVERVIEW Automatic Flight Control System Vertical Path Tracking descent to VNV Target Altitude: 1) Select VNV flight control: FLIGHT INSTRUMENTS a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT SEL Knob, set the Selected Altitude below the flight plan’s VNV Target Altitude of 10,000 feet.
Automatic Flight Control System SYSTEM OVERVIEW Non-path descent using Flight Level Change Mode: 1) Using Flight Level Change Mode, command a non-path descent to an intermediate altitude above the next VNV flight plan altitude: FLIGHT INSTRUMENTS a) Using the ALT SEL 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.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Automatic Flight Control System VP EICAS TH M od e ALT Mode AUDIO PANEL & CNS Planned TOD 2 BOD 1 FL C Pla nn M od e Selected Altitude of 9,400 MSL VNAV Target Altitude of 10,000 MSL 3 ed De sce nt ALT Mode Pa th TOD 4 VP TH Mo FLIGHT MANAGEMENT VNAV Target Altitude of 9,000 MSL de 5 BOD ALT Mode Selected Altitude 3 nm OPSHN HABUK INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 7-42 Non-path Descent 406
Automatic Flight Control System SYSTEM OVERVIEW Approach Flying an ILS approach: FLIGHT INSTRUMENTS 1) Transition from GPS Navigation Mode to Heading Select Mode. a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. Load and activate the approach into the flight plan. b) Use the HDG Knob to set the Selected Heading after getting vectors from ATC. c) Press the HDG Key. The autopilot turns the aircraft to the desired heading.
SYSTEM OVERVIEW Automatic Flight Control System Flying a RNAV GPS approach with vertical guidance: 1) Arm flight director modes for a RNAV GPS approach with vertical guidance: FLIGHT INSTRUMENTS 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. EICAS 2) Press the APR Key once clearance for approach has been received.
Automatic Flight Control System SYSTEM OVERVIEW Go Around/Missed Approach Note: As a result of calculations performed by the system while flying the holding pattern, the display may FLIGHT INSTRUMENTS re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and MFD. Flying a missed approach: EICAS 1) Push the GA Switch at the Decision height and apply go around power to execute a missed approach.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Automatic Flight Control System EICAS 4 FLIGHT MANAGEMENT GPS NAV Mode AUDIO PANEL & CNS MOGAL 3 2 HAZARD AVOIDANCE GA Mode KCOS AFCS 1 INDEX APPENDICES ADDITIONAL FEATURES Figure 7-45 Go Around/Missed Approach 410 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Automatic Flight Control System SYSTEM OVERVIEW 7.7 AFCS Annunciations and Alerts AFCS Status Alerts FLIGHT INSTRUMENTS The annunciations in Table 7-6 (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.
SYSTEM OVERVIEW Automatic Flight Control System Overspeed Protection FLIGHT INSTRUMENTS 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.
Additional Features SYSTEM OVERVIEW Section 8 Additional Features FLIGHT INSTRUMENTS NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts in electronic form, it is still advisable to carry another source of charts on board the aircraft.
SYSTEM OVERVIEW Additional Features 8.1 Synthetic Vision System (SVS) FLIGHT INSTRUMENTS Note: When Synthetic Vision System (SVS) is installed in the G1000 the X-Pointer Command Bars cannot be used when SVS is in use. Refer to the AFCS Section and Flight Instruments Section for more information. NOTE: SVS requires a terrain database that has a resolution of nine arc-seconds.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-1 Synthetic Vision Imagery SVS Operation HAZARD AVOIDANCE SVS is activated from the PFD using the softkeys located along the bottom edge of the display. Pressing the softkeys turns the related function on or off. When SVS is enabled, the pitch ladder increments are reduced to 10 degrees up and 7.5 degrees down. AFCS SVS functions are displayed on three levels of softkeys.
SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS PFD BACK SYN VIS Pressing the BACK Softkey returns to the top-level softkeys. EICAS PATHWAY BACK SYN TERR HRZN HDG APTSIGNS AUDIO PANEL & CNS Pressing the BACK Softkey returns to the previous level of softkeys. Figure 8-2 SVS Softkeys Activating and deactivating SVS: FLIGHT MANAGEMENT 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. The SVS display will cycle on or off with the SYN TERR Softkey.
Additional Features SYSTEM OVERVIEW SVS Features Airport Runway FLIGHT INSTRUMENTS Selected Altitude Traffic Command Bars Airplane Symbol EICAS Zero Pitch Line (ZPL) with Compass Heading Marks Pathways Flight Path Marker AUDIO PANEL & CNS Synthetic Terrain FLIGHT MANAGEMENT HAZARD AVOIDANCE SVS Softkeys Figure 8-3 SVS on the Primary Flight Display NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the CDI, VSI, and VDI.
SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS Selected Altitude FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Programmed Altitudes HAZARD AVOIDANCE Figure 8-4 Programmed and Selected Altitude AFCS Pathways provide supplemental glidepath information on an active ILS, LPV, LNAV/VNAV, and some LNAV approaches. Pathways are intended as an aid to situational awareness and should not be used independent of the CDI, VDI, glide path indicator, and glide slope indicator.
Additional Features SYSTEM OVERVIEW Descent and Approach FLIGHT INSTRUMENTS Pathways are shown descending only for a programmed descent (Figures 8-5, 8-6). When the flight plan includes programmed descent segments, pathways are displayed along the descent path provided that the selected altitude is lower than the programmed altitude. EICAS During a Vectors-to-Final (VTF) approach transition, pathways are displayed along the final approach course inbound to the Missed Approach Point (MAP).
SYSTEM OVERVIEW Additional Features Missed Approach FLIGHT INSTRUMENTS Upon activating the missed approach, pathways lead to the Missed Approach Holding Point (MAHP) and are displayed as a level path at the published altitude for the MAHP, or the selected altitude, whichever is the highest. If the initial missed approach leg is a Course-to-Altitude (CA) leg, the pathways boxes will be displayed level at the altitude published for the MAHP.
Additional Features SYSTEM OVERVIEW Flight Path Marker FLIGHT INSTRUMENTS The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed and direction relative to the three-dimensional terrain display. The FPM is always available when the Synthetic Terrain feature is in operation.
SYSTEM OVERVIEW Additional Features Zero Pitch Line FLIGHT INSTRUMENTS The Zero Pitch Line is drawn completely across the display and represents the aircraft attitude with respect to the horizon. It may not align with the terrain horizon, particularly when the terrain is mountainous or when the aircraft is flown at high altitudes. Horizon Heading EICAS The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass heading in 30‑degree increments on the Zero Pitch Line.
Additional Features SYSTEM OVERVIEW Runways FLIGHT INSTRUMENTS Runway data provides improved awareness of runway location with respect to the surrounding terrain. As runways are displayed, those within 45 degrees of the aircraft heading are displayed in white. Other runways will be gray in color. When an approach for a specific runway is active, that runway will appear brighter and be outlined with a white box, regardless of the runway orientation as related to aircraft heading.
SYSTEM OVERVIEW Additional Features TAWS Alerting FLIGHT INSTRUMENTS Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA). When an obstacle becomes a potential impact point the color of the obstacle matches the red or yellow X on the Inset map and MFD map displays. For more detailed information regarding TAWS, refer to the Hazard Avoidance Section.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols found on the Inset map and MFD maps and charts. Obstacle symbols appear in the perspective view with relative height above terrain and distance from the aircraft.
SYSTEM OVERVIEW Additional Features Field of View FLIGHT INSTRUMENTS The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a V‑shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD. Configuring field of view: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS 2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key.
Additional Features SYSTEM OVERVIEW The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEW turned on. FLIGHT INSTRUMENTS V-Shaped Lines Depict PFD Field of View EICAS Field of View on the MFD AUDIO PANEL & CNS SVS View on the PFD Figure 8-13 MFD and PFD Field of View Comparison FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Additional Features 8.2 SafeTaxi FLIGHT INSTRUMENTS SafeTaxi is an enhanced feature that gives greater map detail when viewing airports at close range. The maximum map ranges for enhanced detail are pilot configurable. When viewing at ranges close enough to show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport landmarks including ramps, buildings, control towers, and other prominent features.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS Taxiway Identification EICAS Aircraft Position Airport Hot Spot Outline AUDIO PANEL & CNS Airport Features HAZARD AVOIDANCE The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR -2, and DCLTR-3 each time the softkey is pressed for easy recognition of decluttering level. Pressing the DCLTR Softkey removes the taxiway markings and airport feature labels.
SYSTEM OVERVIEW Additional Features Configuring SafeTaxi range: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS 2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key. Figure 8-15 Navigation Map PAGE MENU, Map Setup Option 3) Turn the FMS Knob to select the Aviation Group and press the ENT Key.
Additional Features SYSTEM OVERVIEW SafeTaxi Cycle Number and Revision FLIGHT INSTRUMENTS SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the G1000, the Power-up Page indicates whether the databases are current, out of date, or not available. The Power-up Page shows the SafeTaxi database is current when the SafeTaxi Expires date is shown in white. When the SafeTaxi cycle has expired, the SafeTaxi Expires date appears in yellow.
SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page. SafeTaxi information appears in blue and yellow text. The EFFECTIVE date appears in blue when data is current and in yellow when the current date is before the effective date. The EXPIRES date appears in blue when data is current and in yellow when expired (Figures 8‑18 and 8‑19).
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS The other three possible AUX - System Status page conditions are shown here. The EFFECTIVE date is the beginning date for this database cycle. If the present date is before the effective date, the EFFECTIVE date appears in yellow and the EXPIRES date appears in blue. The EXPIRES date is the revision date for the next database cycle. NOT AVAILABLE indicates that SafeTaxi is not available on the database card or no database card is inserted.
SYSTEM OVERVIEW Additional Features 8.3 ChartView FLIGHT INSTRUMENTS ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the plan view of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta. The ChartView database subscription is available from Jeppesen, Inc.
Additional Features SYSTEM OVERVIEW ChartView Terminal Procedures Charts Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. EICAS 3) Press the ENT Key to display the chart.
SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner UNABLE TO DISPLAY CHART is then displayed. Figure 8-23 Unable To Display Chart Banner EICAS When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages.
Additional Features SYSTEM OVERVIEW Selecting a chart: 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey if the Approach Box is not currently shown).
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Selecting the CHRT Softkey switches between the ChartView diagram and the associated map in the WPT page group. In the example shown, the CHRT Softkey switches between the DeKalb Peachtree (KPDK) Airport Diagram and the navigation map on the WPT – Airport Information page.
Additional Features SYSTEM OVERVIEW Selecting the INFO Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO Softkey has no effect. FLIGHT INSTRUMENTS The aircraft position is shown in magenta on the ChartView diagrams when the location of the aircraft is within the chart boundaries. In the example shown, the aircraft is taxiing on Taxiway Alpha on the Charlotte, NC (KCLT) airport.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS In the example shown in Figure 8-26, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-27). HAZARD AVOIDANCE Figure 8-27 Airport Information Page, Class B Chart Selected from INFO View Selecting the DP Softkey displays the Departure Procedure Chart if available.
Additional Features SYSTEM OVERVIEW Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available. Chart Not To Scale FLIGHT INSTRUMENTS EICAS Change Range and Scroll Through the Chart With the Joystick AUDIO PANEL & CNS FLIGHT MANAGEMENT Aircraft Not Shown Icon Figure 8-29 Arrival Information Page HAZARD AVOIDANCE Selecting the APR Softkey displays the approach chart for the airport if available. AFCS ADDITIONAL FEATURES APPENDICES 190-00494-02 Rev.
SYSTEM OVERVIEW Additional Features EICAS FLIGHT INSTRUMENTS Selecting the WX Softkey shows the airport weather frequency information, and includes weather data such as METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only when an XM Data Link Receiver is installed and the XM Weather subscription is current.
Additional Features SYSTEM OVERVIEW NOTE: A subdued softkey label indicates the function is disabled. FLIGHT INSTRUMENTS Recent NOTAMS applicable to the current ChartView cycle are included in the ChartView database. Selecting the NOTAM Softkey shows the local NOTAM information for selected airports, when available. When NOTAMS are not available, the NOTAM Softkey label appears subdued and is disabled as shown in Figure 8-31.
SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Local NOTAM on This Airport FLIGHT MANAGEMENT NOTAM Softkey Selected Figure 8-33 Airport Information Page, Local NOTAMs Selecting the NOTAM Softkey again removes the NOTAMS information. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight Plan Page).
Additional Features SYSTEM OVERVIEW Chart Options Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-20). Selecting the ALL Softkey shows the entire approach chart on the screen. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS Entire Chart Shown FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-34 Approach Information Page, ALL View AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Additional Features EICAS FLIGHT INSTRUMENTS Selecting the HEADER Softkey shows the header view (approach chart briefing strip) on the screen. FLIGHT MANAGEMENT AUDIO PANEL & CNS Approach Chart Briefing Strip Figure 8-35 Approach Information Page, Header View ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selecting the PLAN Softkey shows the approach chart two dimensional plan view.
Additional Features SYSTEM OVERVIEW Selecting the PROFILE Softkey displays the approach chart descent profile strip. FLIGHT INSTRUMENTS EICAS Approach Chart Descent Profile Strip AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-37 Approach Information Page, Profile View, Full Screen Width HAZARD AVOIDANCE Selecting the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart.
SYSTEM OVERVIEW Additional Features AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS If the chart scale has been adjusted to view a small area of the chart, selecting the FIT WIDTH Softkey changes the chart size to fit the available screen width.
Additional Features SYSTEM OVERVIEW Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right. Selecting Additional Information: FLIGHT INSTRUMENTS 1) While viewing the Airport Taxi Diagram, select the FULL SCN Softkey to display the information windows (AIRPORT, INFO). 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or FREQUENCIES Box (INFO Box shown).
SYSTEM OVERVIEW Additional Features The full screen view can also be selected by using the page menu option. Selecting full screen On or Off: FLIGHT INSTRUMENTS 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options.
Additional Features SYSTEM OVERVIEW Day/Night View FLIGHT INSTRUMENTS ChartView can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the G1000 softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 8-43 Arrival Information Page, Day View INDEX Figure 8-44 Arrival Information Page, Night View 452 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Additional Features SYSTEM OVERVIEW ChartView Cycle Number and Expiration Date Power-up Page Display FLIGHT INSTRUMENTS The ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. ChartView is disabled 70 days after the expiration date and is no longer available for viewing upon reaching the disables date.
SYSTEM OVERVIEW Additional Features ChartView Database is Current and Available Chart Cycle has Expired, Next Cycle is Available Chart Cycle has Expired but is Still Viewable for 70 Days from Expiration Date Chart Cycle is No Longer Viewable INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Examples of four possible Power-up Page conditions are shown here.
Additional Features SYSTEM OVERVIEW NOTE: A subdued softkey label indicates the function is disabled. FLIGHT INSTRUMENTS The ChartView time critical information can also be found on the AUX - System Status page. The database CYCLE number, EXPIRES, and DISABLES dates of the ChartView subscription appear in either blue or yellow text. When the ChartView EXPIRES date is reached, ChartView becomes inoperative 70 days later. This is shown as the DISABLES date.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS The other three possible AUX - System Status page conditions are shown here. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable. REGION and CYCLE NOT AVAILABLE in blue, indicate that no ChartView data is available on the database card or no database card is inserted.
Additional Features SYSTEM OVERVIEW 8.4 FliteCharts • Departure Procedures (DP) FLIGHT INSTRUMENTS FliteCharts resemble the paper version of National Aeronautical Charting Office (NACO) terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. FliteCharts database subscription is available from Garmin.
SYSTEM OVERVIEW Additional Features FliteCharts Terminal Procedures Charts Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS 3) Press the ENT Key to display the chart.
Additional Features SYSTEM OVERVIEW If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner UNABLE TO DISPLAY CHART is then displayed. FLIGHT INSTRUMENTS Figure 8-51 Unable To Display Chart Banner EICAS When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages.
SYSTEM OVERVIEW Selecting a chart: FLIGHT INSTRUMENTS Additional Features 2) Press the FMS Knob to activate the cursor. 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. 3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey if the Approach Box is not currently shown).
Additional Features SYSTEM OVERVIEW Selecting the CHRT Softkey switches between the FliteCharts diagram and the associated map in the WPT page group. In the example shown, the CHRT Softkey switches between the Charlotte, NC (KCLT) Airport Diagram and the navigation map on the WPT – Airport Information page.
SYSTEM OVERVIEW Additional Features Selecting the INFO Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO Softkey has no effect. EICAS FLIGHT INSTRUMENTS Another source for additional airport information is from the INFO Box above the chart (Figure 8-53) or to the right of the chart (Figure 8-54) for certain airports. This information source is not related to the INFO Softkey.
Additional Features SYSTEM OVERVIEW In the example shown in Figure 8-54, ALTERNATE MINIMUMS is selected. Pressing the ENT Key displays the IFR Alternate Minimums Chart (Figure 8-55). FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-55 Airport Information Page, ALTERNATE MINIMUMS Selected from INFO View HAZARD AVOIDANCE Selecting the DP Softkey displays the Departure Procedure Chart if available.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available. Figure 8-57 Arrival Information Page APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selecting the APR Softkey displays the approach chart for the airport if available. INDEX Figure 8-58 Approach Information Page 464 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Additional Features SYSTEM OVERVIEW Selecting the WX Softkey shows the airport weather frequency information, when available, and includes weather data such as METAR and TAF from the XM Data Link Receiver. Weather information is available only when an XM Data Link Receiver is installed and the XM Weather subscription is current. FLIGHT INSTRUMENTS Selecting Additional Information: 1) While viewing the Airport Taxi Diagram, select the WX Softkey to display the information windows (AIRPORT, INFO).
SYSTEM OVERVIEW Additional Features Chart Options Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8‑48). EICAS FLIGHT INSTRUMENTS Selecting the ALL Softkey shows the entire chart on the screen.
Additional Features SYSTEM OVERVIEW Selecting the FIT WIDTH Softkey fits the width of the chart in the display viewing area. In the example shown, the chart at close range is replaced with the full width chart. FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Select FIT WDTH Softkey to Show Full Chart Width Figure 8-61 Approach Information Page, FIT WDTH Softkey Selected APPENDICES INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right.
Additional Features SYSTEM OVERVIEW The full screen view can also be selected by using the page menu option. Selecting full screen On or Off: FLIGHT INSTRUMENTS 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.
SYSTEM OVERVIEW Additional Features Day/Night View FLIGHT INSTRUMENTS FliteCharts can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the G1000 softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-65 Approach Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-66 Approach Information Page, Night View INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Additional Features FliteCharts Cycle Number and Expiration Date FLIGHT INSTRUMENTS FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. FliteCharts is disabled 180 days after the expiration date and are no longer available for viewing upon reaching the disables date. When turning on the G1000, the Power-up Page indicates any of five different possible criteria for chart availability.
Additional Features SYSTEM OVERVIEW Examples of four possible Power-up Page messages are shown here. FliteCharts Expires plus a date in white, indicates the chart database is current. Chart data is out of date! in yellow, indicates charts are still viewable, but approaching the disable date. FLIGHT INSTRUMENTS When the 180 day grace period has expired, Chart data is disabled. in yellow indicates that the FliteCharts database has expired and is no longer viewable.
SYSTEM OVERVIEW Additional Features NOTE: A subdued softkey label indicates the function is disabled. FLIGHT INSTRUMENTS FliteCharts time critical information can also be found on the AUX - System Status page. The FliteCharts database REGION, CYCLE number, EFFECTIVE, EXPIRES, and DISABLES dates of the subscription appear in either blue or yellow text. Dates shown in blue are current data. Dates shown in yellow indicate the data is not within the current subscription period.
Additional Features SYSTEM OVERVIEW The other three possible AUX - System Status page conditions are shown here. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable. REGION and CYCLE NOT AVAILABLE in blue, indicate that FliteCharts database is not available on the database card or no database card is inserted.
SYSTEM OVERVIEW Additional Features 8.5 XM Radio Entertainment FLIGHT INSTRUMENTS Note: Refer to the Hazard Avoidance Section for information about XM Weather products. The optional XM Radio entertainment feature of the GDL 69A Data Link Receiver is available for the passengers’ enjoyment. The GDL 69A can receive XM Satellite Radio® entertainment services at any altitude throughout the Continental U.S.
Additional Features SYSTEM OVERVIEW NOTE: The LOCK Softkey on the XM Information Page (AUX Page Group) is used to save GDL 69A activation FLIGHT INSTRUMENTS data when the XM services are initially set up. It is not used during normal XM Radio operation, but there should be no adverse effects if inadvertently selected during flight. Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev F or later) for further information.
SYSTEM OVERVIEW Additional Features Using XM Radio FLIGHT INSTRUMENTS The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. Selecting the XM Radio Page: 1) Turn the large FMS Knob to select the AUX Page Group. 2) Turn the small FMS Knob to select the displayed AUX - XM Information Page. EICAS 3) Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled.
Additional Features SYSTEM OVERVIEW Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel that the XM Radio is using. FLIGHT INSTRUMENTS The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category. Channels can be stepped through one at a time or may be selected directly by channel number. Selecting a channel from the channel list: 1) While on the XM Radio Page, select the CHNL Softkey.
SYSTEM OVERVIEW Additional Features Category FLIGHT INSTRUMENTS The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other contents. One of the optional categories is PRESETS to view channels that have been programmed. Selecting a category: 1) Select the CATGRY Softkey on the XM Radio Page.
Additional Features SYSTEM OVERVIEW Presets FLIGHT INSTRUMENTS Up to 15 channels from any category can be assigned a preset number. The preset channels are selected by selecting the PRESETS and MORE Softkeys. Then the preset channel can be selected directly and added to the channel list for the Presets category.
SYSTEM OVERVIEW Additional Features 8.6 Scheduler FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS The Scheduler feature can be used to enter and display reminder messages (e.g., Hot Section Inspection or Phase 1 Maintenance Check) in the Messages Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic).
Additional Features SYSTEM OVERVIEW 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. FLIGHT INSTRUMENTS c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message: 1) Select the AUX - Utility Page.
SYSTEM OVERVIEW Additional Features 8.7 Abnormal Operation FLIGHT INSTRUMENTS SVS Troubleshooting SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD display reverts to the standard blue-over-brown attitude display.
Additional Features SYSTEM OVERVIEW Unusual Attitudes FLIGHT INSTRUMENTS Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to correct the unusual attitude condition. The display shows either a brown or blue colored bar at the top or bottom of the screen to represent earth or sky. This is intended to prevent losing sight of the horizon during extreme pitch attitudes.
SYSTEM OVERVIEW Additional Features GDL 69/69A Data Link Receiver Troubleshooting Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure.
Additional Features SYSTEM OVERVIEW If a failure still exists, the following messages may provide insight as to the possible problem: NO SIGNAL LOADING OFF AIR --- Message Location XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Weather Datalink Page - center of page XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Description Data Link Receiver antenna error; service required Dat
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features Blank Page 488 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Appendix A SYSTEM OVERVIEW Annunciations and Alerts CAS Messages Inhibits CABIN ALT ENGINE FAIL L-R* FUEL BOOST L-R* FUEL FLTR BP L-R* GEN OFF L-R GEN OFF L-R* HYD PRESS LO HYD PUMP ON NOSE DOOR L-R* STALL WARN FAIL T2 HTR FAIL L-R* TAIL CONE BLD LK X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X *Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here display L-R for example.
EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix A Name Inhibit EMER ESI TOPI AIR LOPI ESDI GND Emergency Bus Mode Inhibit Engine Start Inhibit Takeoff Operation Phase Inhibit In-Air Inhibit Landing Operation Phase Inhibit Engine Shutdown Inhibit On-Ground Inhibit Red annunciation window text signifies warnings; yellow, cautions; and white, annunciation advisories. See the Airplane Flight Manual (AFM) for recommended pilot actions.
Appendix A SYSTEM OVERVIEW Reversionary Sensor Annunciations FLIGHT INSTRUMENTS Reversionary sensor selection is annunciated in the Reversionary Sensor Window, as shown in Figure A-2. These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey gives access to ADC1, ADC2, AHRS1, and AHRS2 Softkeys. These softkeys allow manual switching of sensors. In the case of certain types of sensor failures, the G1000 may make some sensor selections automatically.
SYSTEM OVERVIEW Appendix A NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to initialize. All windows should be operational within one minute of power-up. Should any window continue FLIGHT INSTRUMENTS to remain flagged, the G1000 system should be serviced by a Garmin-authorized repair facility.
Appendix A SYSTEM OVERVIEW System Annunciation Comment FLIGHT INSTRUMENTS Attitude and Heading Reference System is aligning. Display system is not receiving attitude information from the AHRS. EICAS AUDIO PANEL & CNS Indicates a configuration module failure. FLIGHT MANAGEMENT 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.
SYSTEM OVERVIEW Appendix A System Annunciation Comment FLIGHT INSTRUMENTS GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFM). EICAS Other Various Red X Indications A red “X” through any other display field (such as engine instrumentation display) indicates that the field is not receiving valid data.
Appendix A SYSTEM OVERVIEW MFD & PFD Message Advisories (Cont.) Comments The MFD configuration settings do not match backup configuration memory. The G1000 system should be serviced. The MFD and PFDs have different software versions installed. The G1000 system should be serviced. The MFD and/or PFDs have a software mismatch. A red ‘X’ will appear in the CAS display. The G1000 system should be serviced.
SYSTEM OVERVIEW Appendix A Database Message Advisories (Cont.) Comments The MFD and/or PFD detected a failure in the terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, The G1000 system should be serviced. The terrain database is present on another LRU, but is missing on the specified LRU. The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card.
Appendix A SYSTEM OVERVIEW Database Message Advisories (Cont.) Comments FLIGHT INSTRUMENTS Message MFD1 DB ERR – MFD1 Safe Taxi database error exists. PFD1 DB ERR – PFD1 Safe Taxi database error exists. PFD2 DB ERR – PFD2 Safe Taxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, The G1000 system should be serviced.
SYSTEM OVERVIEW Appendix A GMA 1347D Message Advisories (Cont.) EICAS FLIGHT INSTRUMENTS Message MANIFEST – GMA1 software mismatch, communication halted. MANIFEST – GMA2 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. GMA2 SERVICE – GMA2 needs service. Return unit for repair. Comments The audio panel has incorrect software installed. The G1000 system should be serviced. The audio panel self-test has detected a problem in the unit.
Appendix A SYSTEM OVERVIEW GIA 63W Message Advisories (Cont.) The system has detected an over temperature condition in COM1 and/or COM2. The transmitter is operating at reduced power. If the problem persists, the G1000 system should be serviced. 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. EICAS The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position.
SYSTEM OVERVIEW Appendix A GIA 63W Message Advisories (Cont.) FLIGHT INSTRUMENTS Message G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. EICAS G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Comments A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available.
Appendix A SYSTEM OVERVIEW GRS 77 Message Advisories AHRS2 TAS – AHRS2 not receiving valid airspeed. EICAS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE The #1 AHRS and #2 AHRS magnetic model database versions do not match. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The #2 AHRS earth magnetic field model is out of date. Update magnetic field model when practical.
SYSTEM OVERVIEW Appendix A GMU 44 Message Advisories EICAS FLIGHT INSTRUMENTS Message HDG FAULT – AHRS1 magnetometer fault has occurred. HDG FAULT – AHRS2 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. MANIFEST – GMU2 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. A fault has occurred in the #2 GMU 44.
Appendix A SYSTEM OVERVIEW GDC 74B Message Advisories Comments FLIGHT INSTRUMENTS GDC1 or GDC2 is reporting that the altitude error correction is unavailable. GDC1 or GDC2 is reporting that the airspeed error correction is unavailable. EICAS The GDC 74B has incorrect software installed. The G1000 system should be serviced. AUDIO PANEL & CNS Message ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC2 ALT EC – ADC2 altitude error correction is unavailable.
SYSTEM OVERVIEW Appendix A Miscellaneous Message Advisories Comments Upon power-up, the G1000 system detects that a stored flight plan waypoint is 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.
Appendix A SYSTEM OVERVIEW Miscellaneous Message Advisories (Cont.) The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint.
SYSTEM OVERVIEW Appendix A AFCS Alerts NOTE: Do not press the AP DISC switch during servo power-up and preflight system tests as this may cause FLIGHT INSTRUMENTS the preflight system test to fail or never to start (if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation. AUDIO PANEL & CNS EICAS System Status Field Figure A-5 AFCS System Status Field The following alert annunciations appear in the AFCS System Status field on the PFD.
Appendix A SYSTEM OVERVIEW TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SYSTEM OVERVIEW Appendix A 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 System Test in progress None “TAWS Not Available” None None None “TAWS System Test OK” EICAS FLIGHT INSTRUMENTS Alert Type System Test pass None AUDIO PANEL & CNS Other G1000 Aural Alerts Aural Alert Description “Minimums, minimu
Appendix B SYSTEM OVERVIEW SD Card Use FLIGHT INSTRUMENTS 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. CAUTION: Do not load Jeppesen navigation data (except ChartView) onto Garmin Supplemental Data Cards. EICAS Jeppesen Databases The Jeppesen aviation database is updated on a 28-day cycle.
SYSTEM OVERVIEW Appendix B 4) After the update completes, the PFD starts in normal mode. 5) Turn the G1000 System OFF and remove the SD card. FLIGHT INSTRUMENTS 6) Repeat steps 1 through 4 for the other PFD and the MFD. The MFD and PFD databases are now updated. Remove the SD card when finished. 7) Verify that the correct update cycle is loaded during startup of the MFD.
Appendix B SYSTEM OVERVIEW The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is very important to note that not all obstacles are necessarily charted and therefore may not be contained in the obstacle database. This database is updated on a 56-day cycle. Coverage of the obstacle database includes the United States and Europe.
EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix B AUDIO PANEL & CNS Figure B-4 Database Information on the Splash Screen 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 4) Turn the large FMS Knob to select the AUX Page group on the MFD. FLIGHT MANAGEMENT 5) Turn the small FMS Knob to select the System Status Page. 6) Select the DBASE Softkey to place the cursor in the ‘Database’ box.
Appendix C SYSTEM OVERVIEW Glossary ADDITIONAL FEATURES APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang AFCS 190-00494-02 Rev. B barometric altitude barometric setting battery backcourse HAZARD AVOIDANCE B ALT BARO BATT BC FLIGHT MANAGEMENT ATK AUTOSEQ AUX AWOS The compass direction from the present position to a destination waypoint.
SYSTEM OVERVIEW Appendix C FLIGHT INSTRUMENTS CVR CVRG CWS CYL Cockpit Voice Recorder coverage control wheel steering cylinder density altitude database decibels ‘Z’ (radar return) declutter decrease fuel degree de-icing departure The desired course between the active “from” and “to” waypoints.
Appendix C ADDITIONAL FEATURES APPENDICES key stuck kilogram Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang INDEX 190-00494-02 Rev.
SYSTEM OVERVIEW Appendix C kHz km kt kilohertz kilometer knot AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS L left, left runway LAT latitude LBL label lb pound LCD Liquid Crystal Display LCL local LED Light Emitting Diode Left Over Fuel On Board The amount of fuel remaining on board after the completion of one or more legs of a flight plan or direct-to.
Appendix C RAM REF REM REQ RES REV RF RMI RMT RNG RNWY ROL ROM rpm RST FUEL RSV RT RVRSNRY RX SID SIGMET 190-00494-02 Rev.
FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix C TRUNC TTL TURN TX truncated total procedure turn transmit UNAVAIL USR UTC UTM/UPS unavailable user Coordinated Universal Time Universal Transverse Mercator / Universal Polar Stereographic Grid WARN WGS-84 WPT WW WX warning (GPS position error) World Geodetic System - 1984 waypoint(s) world wide weather XFER, XFR XPDR XTALK XTK transfer transponder cross-talk cross-track APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MA
Appendix D SYSTEM OVERVIEW Frequently Asked Questions FLIGHT INSTRUMENTS If a particular aspect of G1000 operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized dealer. Garmin is dedicated to supporting its products and customers. What is WAAS? EICAS The Wide Area Augmentation System (WAAS) uses a system of ground stations to correct any GPS signal errors.
SYSTEM OVERVIEW Appendix D For RAIM to work correctly, the GPS receiver must track at least five satellites. A minimum of six satellites is required to allow RAIM to eliminate a single corrupt satellite from the navigation solution. FLIGHT INSTRUMENTS RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection limit (2.0 nm for oceanic and en route, 1.0 nm for terminal, and 0.3 nm for non-precision approaches).
Appendix D • Manual course change on HSI not possible • Manually select course to waypoint from HSI • Always navigates ‘TO’ the active waypoint • Indicates ‘TO’ or ‘FROM’ waypoint • Must be in this mode for final approach course • Cannot be set for final approach course or published holding patterns FLIGHT INSTRUMENTS OBS • Manual sequencing - ‘holds’ on selected waypoint SYSTEM OVERVIEW Normal (OBS not activated) • Automatic sequencing of waypoints EICAS When OBS mode is active, the G1000 allow
SYSTEM OVERVIEW Appendix D When does the CDI scale change? • When set to ‘Auto’ (default), the GPS CDI scale automatically adjusts to the desired limits based upon the current phase of flight. FLIGHT INSTRUMENTS • When a departure procedure is activated, the CDI is scaled for departure (0.3 nm). • The system switches from departure to terminal CDI scaling (1.
Appendix D SYSTEM OVERVIEW Why does the HSI not respond like a VOR when OBS mode is active? FLIGHT INSTRUMENTS Unlike a VOR, the CDI scale used on GPS equipment is based on the crosstrack distance to the desired course, not on the angular relationship to the destination. Therefore, the CDI deflection on the GPS is constant regardless of the distance to the destination and does not become less sensitive when further away from the destination.
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix D Blank Page 524 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Appendix E SYSTEM OVERVIEW General TIS Information Introduction FLIGHT INSTRUMENTS NOTE: Aircraft without an operating transponder are invisible to TIS. EICAS The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped aircraft. TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a specified service volume.
SYSTEM OVERVIEW Appendix E WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations FLIGHT INSTRUMENTS is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map. NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in mountainous regions. AUDIO PANEL & CNS EICAS TIS information is collected during a single radar sweep.
Appendix F SYSTEM OVERVIEW Display Symbols Airport Basemap Symbol Item Symbol Item Symbol FLIGHT INSTRUMENTS Item Interstate Highway Unknown Airport State Highway Non-towered, Non-serviced Airport EICAS US Highway Towered, Non-serviced Airport National Highway AUDIO PANEL & CNS Non-towered, Serviced Airport Small City or Town Medium City Restricted (Private) Airport Large City FLIGHT MANAGEMENT Towered, Serviced Airport Heliport Item Symbol Intersection HAZARD AVOIDANCE Traffic
SYSTEM OVERVIEW Appendix F Line Symbols Item Symbol FLIGHT INSTRUMENTS ICAO Control Area Class B Airspace Mode C Tower Area FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS Warning Area Alert Area Caution Area Danger Area Prohibited Area Restricted Area Training Area Unknown Area Class C Terminal Radar Service Area Mode C Area Military Operations Area (MOA) HAZARD AVOIDANCE State or Province Border International Border Road AFCS Railroad ADDITIONAL FEATURES Lattitude/Longitude Obstacle database INDE
Appendix F SYSTEM OVERVIEW Terrain Color Chart Potential Impact Point 100 ft Threshold Unlighted Obstacle FLIGHT INSTRUMENTS Terrain above or within 100 ft below the aircraft altitude Projected Flight Path 1000 ft EICAS Terrain Color Terrain Location Terrain between 100 ft and 1000 ft below the aircraftTerrain altitude Red (WARNING) above or within 100 ft below aircraft altitude Yellow (CAUTION) Terrain between 100 ft and 1000 ft of aircraft altitude Terrain more than 1000 ft below the aircraft alt
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix F Blank Page 530 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
Index Calibrated Airspeed-----------------------------------------241 Cargo---------------------------------------------------------246 CDI----------------------------------------------------- 131, 504 Chart Not Available---------------------------------- 451, 470 Chart options------------------------------------------- 46, 455 CHART SETUP box------------------------------------------453 ChartView----------------------------------------------------434 ChartView database------------------------------------
SYSTEM OVERVIEW Index EICAS FLIGHT INSTRUMENTS Modes, vertical------------------------------------ 387–412 Flight director (FD)----------------------------------- 370–384 Modes, vertical-------------------------------------------375 Flight plan Storing-----------------------------------------------------520 Flight timer---------------------------------------------------457 FliteCharts---------------------------------------------------474 FliteCharts cycle---------------------------------------------457
Index WAAS-------------------------------------------- 252, 398, 498 WAAS precision approach---------------------------------408 Warranty--------------------------------------------------------- i WATCH-------------------------------------------------------- 31 Waypoint Automatic sequencing----------------------------------521 Skipping---------------------------------------------------521 FLIGHT MANAGEMENT X XM XM weather products Activating---------------------------------------------------- 4 XM radio-
INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EICAS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Index Blank Page I-4 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev.
G1000 ® Integrated Flight Deck Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown 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:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Cessna Citation Mustang Garmin AT, Inc.
