Garmin G1000 Pilot’s Guide for Cessna Nav III

as well as FIS-B weather information. It broadcasts aircraft position, velocity, projected track, altitude, and flight identification to other equipped aircraft in the vicinity, as well as to FAA ground stations. The GDL 90 receives FIS-B weather information which is displayed on the MFD as NEXRAD radar and METARs. • GSA 81 (3), and GSM 85 (3) - The GSA 81 servos are used for the automatic control of roll, pitch, and pitch trim. These units interface with each GIA 63/63W. The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the mechanical flight-control surface linkage. Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. PFD GDU 1040 or GDU 1044B* GMA 1347 Audio Panel Reversionary 17 CASSANO Control イ Reversionary Control SYSTEM OVERVIEW MFD GDU 1040 or GDU 1044B* No. 1 GIA 63/63W Integrated Avionics Unit System Inegration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope GFC 700 Flight Director (172S, 182, & 206) GPS Output GDC 74A Air Data Computer OAT Airspeed Altitude Vertical Speed No. 2 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope GRS 77 AHRS Attitude Rate of Turn Slip/Skid GPS Output GMU 44 Magnetometer Heading GTX 33 Transponder Honeywell KAP 140 Autopilot GEA 71 Engine/Airframe Unit GSA 81 Pitch Servo Autopilot Calculations (172S/TD,182 & 206) GSA 81 Pitch Trim Autopilot Calculations (172S/TD,182 & 206) GSA 81 Roll Servo Autopilot Calculations (172S/TD,182 & 206) GTS 800 TAS or GDL 90 Data Link ADS-B Traffic Data * The GDU 1040 is available in systems not using the GFC 700 Automatic Flight Control System. The GDU 1044B is available in systems using the Garmin GFC 700 Automatic Flight Control System. Figure 1-1 Basic G1000 System 17 CRSBARO 190-00498-07 Rev. A Garmin G1000 Pilot's Guide for Cessna Nav III 5 SYSTEM FLIGHT EIS OVERVIEW INSTRUMENTS & CNS AUDIO PANEL MANAGEMENT FLIGHT AVOIDANCE HAZARD AFCS FEATURES ADDITIONAL APPENDICES INDEX INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL EIS & CNS FLIGHT INSTRUMENTS SYSTEM OVERVIEW SYSTEM OVERVIEW CRS-BANO CASSANO No. 1 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GFC 700 Flight Director No. 2 GIA 63/63W Integrated Avionics Unit System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope ELT Emergency Locator Transmitter L3 Stormscope Lightning Strike and Thunderstorm Detection Honeywell KR 87 ADF Receiver GDL 69/69A Data Link Weather Data Digital Audio Entertainment GARMIN Honeywell KN 63 CO Guardian DME Carbon Monoxide Detection Honeywell KTA 870 Traffic Avoidance System Figure 1-2 Additional Equipment Options 6 Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. 1.3 G1000 CONTROLS SYSTEM OVERVIEW NOTE: The Audio Panel (GMA 1347) and AFCS controls are described in the CNS & Audio Panel and AFCS sections respectively. The G1000 system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD/MFD CONTROLS PUSH VOLID 1 2 3 4 NAV PUSH 1-2 HDG PUSH HDG SYNC AP FD HDG ALT NAV VNV APR BC VS NOSE UP NOSE FLC DN ALT 17 5 6 7 8 9 EMERG COM PUSH VOL SQ PUSH 1-2 CRS BARO PUSH CRS CTR RANGE PUSH PAN -D▸> MENU FPL PROC CLR DFLT MAP FMS ENT PUSH CRSR 18 AP FD 24 10 -D▸ MENU 14 19 -HDG ALT 25 11 FPL PROC 15 20 NAV VNV 26 12 CLR ENT 16 (21) APR BC 27 DFLT MAP FMS 22 VS NOSE UP 28 13 23 FLC NOSE DN 29 PUSH CRSR 190-00498-07 Rev. A GFC 700 AFCS Only Figure 1-3 PFD/MFD Controls Garmin G1000 Pilot's Guide for Cessna Nav III SYSTEM OVERVIEW INSTRUMENTS FLIGHT AUDIO PANEL EIS & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD AFCS FEATURES ADDITIONAL APPENDICES INDEX 7 HAZARD FLIGHT AUDIO PANEL AFCS FLIGHT SYSTEM FEATURES AVOIDANCE MANAGEMENT EIS & CNS INSTRUMENTS OVERVIEW SYSTEM OVERVIEW PFD and MFD control functions are the same. ① NAV VOL/ID Knob - Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. GARMIN. 3 Dual NAV Knob - Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields. 4 Heading Knob - Turn to manually select a heading on the HSI. When pressed, it synchronizes the heading bug with the compass lubber line. Selected Heading provides the heading reference to the Flight Director while operating in Heading Select mode. 5 Joystick - Changes the map range (distance top to bottom of map display) when rotated. Activates the map pointer when pressed. 6 CRS/BARO Knob - The large knob sets the altimeter barometric pressure and the small knob adjusts the course. The course is only adjustable when the HSI is in VORI, VOR2, or OBS/SUSP mode. Pressing this knob centers the CDI on the currently selected VOR. Selected Course provides course reference to the Flight Director when operating in Navigation and Approach modes. - ⑦ Dual COM Knob - Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob toggles the tuning cursor (light blue box) between the COM1 and COM2 fields. 8 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field. 9 COM VOL/SQ Knob - Controls COM audio level. Audio volume level is shown in the field as a percentage. Pressing this knob turns the COM automatic squelch ON and OFF. 10 Direct-to Key - Allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by the identifier, chosen from the active route, or taken from the map pointer position). ⑲1 FPL Key - Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. ⑫2 CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). (13) Dual FMS Knob - Press to turn the selection cursor ON/OFF. Data Entry: With the cursor ON, turn to enter data in the highlighted field (large knob moves cursor location; small knob selects character for highlighted cursor location). When the cursor is turned ON while viewing the Active Flight Plan Page, the cursor is placed on the line below the Data Insertion Pointer see Figure 1-4. The pointer indicates data entered at the cursor will be inserted above the line selected. Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view. With cursor ON, turn large knob to scroll through the list. Page Selection: Turn knob on MFD to select the page to view (large knob selects a page group; small knob selects a specific page from the group) 14 MENU Key - Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. INDEX APPENDICES ADDITIONAL 8 Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. Data is Inserted Above the Cursor, Indicated by the Data Insertion Pointer ACTIVE FLIGHT PLANɲ KAEJ / KLXV DTK DIS ALT Enroute KAEJ .FT KLXV 337° 528NM FT Approach - KLXV-GPS 16GPS LNAV DAVVY iaf 344° 19.3NM FT LASCH 157° 5.9NM 14000FT INGRR faf 177° 5.0NM 13000FT SYSTEM OVERVIEW OVERVIEW SYSTEM INSTRUMENTS FLIGHT AUDIO PANEL EIS & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD AFCS FEATURES ADDITIONAL APPENDICES INDEX Figure 1-4 Data Insertion Pointer 15 PROC Key - Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. If a flight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARS) and approaches (IAPS) from the database and loads them into the active flight plan. 16 ENT Key - Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. 17 Dual ALT Knob - Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands (500m for metric), while the small knob selects the hundreds (50m for metric). Altitude Select is used by the Automatic Flight Control System in certain modes, in addition to the standard G1000 Altitude Alerter function. The following are only available with the GFC 700 AFCS. 18 AP Key - Engages/disengages the autopilot and flight director. Pressing the AP Key activates the flight director and engages the autopilot in the default pitch axis and roll axis modes. Pressing the AP Key again disengages the autopilot and deactivates the flight director. 19 HDG Key - Selects/deselects Heading Select Mode. 20 NAV Key - Selects/deselects Navigation Mode. 21 APR Key - Selects/deselects Approach Mode. 22 VS Key - Selects/deselects Vertical Speed Mode. 23 FLC Key - Selects/deselects Flight Level Change Mode. 24 FD Key - Activates/deactivates the flight director only. Pressing the FD Key turns on the flight director in the default pitch axis and roll axis modes. Pressing the FD Key again deactivates the flight director and removes the command bars, unless the autopilot is engaged. If the autopilot is engaged, the FD Key is disabled. 25 ALT Key - Selects/deselects Altitude Hold Mode. 26 VNV Key - Selects/deselects Vertical Navigation Mode. 27 BC Key - Selects/deselects Back Course Mode. - 28 29 NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes. 190-00498-07 Rev. A Garmin G1000 Pilot's Guide for Cessna Nav III 9 INDEX APPENDICES ADDITIONAL AFCS FEATURES HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS FLIGHT SYSTEM EIS INSTRUMENTS OVERVIEW 10 SYSTEM OVERVIEW AUDIO PANEL CONTROLS COM1 MIC COM1 2 3 COM2 MIC COM2 COM3 5 COM3 6 MIC COM 7 TEL 8 1/2 9 PA SPKR 10 11 MKR MUTE HI SENS 12 13 DME NAV1 14 15 ADF NAV2 16 17 AUX 18 MAN SQ PLAY 19 CREW 20 PILOT COPLT 21 ICS ISOLATION PILOT-PASS 22 VOL SQ DISPLAY BACKUP 23 24 Figure 1-5 Audio Panel Controls (GMA 1347) GARMIN. NOTE: When a key is selected, a triangular annunciator above the key is illuminated. ① COMI 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. COM2 receiver audio can be added by pressing the COM2 Key. (2) COMI - When selected, audio from the #1 COM receiver can be heard. 3 COM2 MIC - Selects the #2 transmitter for transmitting. COM2 is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM2 can be deselected by pressing the COM2 Key, or COM1 can be added by pressing the COM1 Key. 4 COM2 When selected, audio from the #2 COM receiver can be heard. COM3 MIC - Not used on Cessna Nav III aircraft. Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. SYSTEM OVERVIEW SYSTEM FLIGHT AUDIO PANEL EIS OVERVIEW INSTRUMENTS & CNS MANAGEMENT FLIGHT HAZARD AFCS AVOIDANCE FEATURES ADDITIONAL APPENDICES INDEX 6 COM3 Not used on Cessna Nav III aircraft. ⑦ COM 1/2 - Split COM is disabled on Cessna Nav III aircraft. 8 TEL Not used on Cessna Nav III aircraft. 9 PA - Selects the Passenger Address system. The selected COM transmitter is deselected when the PA Key is pressed. The Passenger Address system is disabled on the Cessna 172R/S. 10 SPKR - Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. ⑲1 MKR/MUTE – Mutes the currently received marker beacon receiver audio. Unmutes when new marker beacon audio is received. Also, stops play of the clearance recorder. 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. 14 NAVI - When selected, audio from the #1 NAV receiver can be heard. 15 ADF - Pressing turns on or off the audio from the ADF receiver. 16 NAV2 - When selected, audio from the #2 NAV receiver can be heard. (17) AUX - Not used on Cessna Nav III aircraft. 18 MAN SQ – Press to enable manual squelch for the intercom. When active, press the PILOT Knob to illuminate 'SQ'. Turn the PILOT/PASS Knobs to adjust squelch. 19 PLAY – Press once to play the last recorded audio. Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. Press the MKR/MUTE Key to stop play. 20 PILOT - Pressing selects the pilot intercom isolation. Press again to deselect pilot isolation. 21 COPLT - Pressing selects the copilot intercom isolation. Press again to deselect copilot isolation. 22 PILOT Knob - Press to switch between volume and squelch control as indicated by the 'VOĽ' or 'SQ' being illuminated. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 23 PASS Knob - Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 24 Reversionary Mode Button – Pressing manually selects Reversionary Mode. 190-00498-07 Rev. A Garmin G1000 Pilot's Guide for Cessna Nav III 11 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL FLIGHT SYSTEM EIS & CNS INSTRUMENTS OVERVIEW SYSTEM OVERVIEW GARMIN. 1.4 SECURE DIGITAL (SD) CARDS ✔ NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on loading database updates. The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. SD cards are used for storing the various databases and system software updates. Each display bezel is equipped with two SD card slots. The top slot is used for importing and exporting flight plans, Flight Data Logging, and loading navigation database updates. The bottom slot of each display contains a Garmin Supplemental Data Card which is used for storing the various databases. Not all SD cards are compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft manufacturer. Installing an SD card: 1) Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. 2) To eject the card, gently press on the SD card to release the spring latch. EMERG COM PUSH VOL SQ SD Card Slots PUSH 1-2 CRS-BARO PUSH CRS CTR RANGE Figure 1-6 Display Bezel SD Card Slots 12 Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. 1.5 SYSTEM POWER-UP SYSTEM OVERVIEW NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to Appendix A for system-specific annunciations and alerts. The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation. During system initialization, test annunciations are displayed, as shown in Figure 1-7. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel. On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up, the power-up screen (Figure 1-8) displays the following information: • System version • • Copyright • Land database name and version • Safe Taxi database information . • Terrain database name and version . Obstacle database name and version Navigation database name, version, and effective dates Airport Directory name, version and effective dates FliteCharts/ChartView database information SYSTEM OVERVIEW INSTRUMENTS FLIGHT AUDIO PANEL EIS & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD AFCS FEATURES ADDITIONAL APPENDICES INDEX Current database information includes database type, cycle number, or valid operating dates. Review the listed information for currency (to ensure that no databases have expired). Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to determine a position, the aircraft's current position is shown on the Navigation Map Page. NAV2 AFCS Dirt SHRSPEED DIS BRG TAMS TEST 988 AHRS ALIGN: Keep Wings Level HOG HDG 868 CRS 354 29.92 INSET PFD 0 GPS ENR INTEG 00 SKYHAWK CDI DHE XPDR IDENT XPOR FAIL THR/REF NRST ADVISORY GARMIN Figure 1-7 PFD Initialization G1000 Cessna 1723 Systen 0563.25 (2002-10 Garmin Ltd or subs DATABASE Checklist File: N/A Basemap Land 4.00 A SafeTaxi Expires 22-OCT-2011 Terroin 2.04 Airport Terrain 2.04 Obstocle Expires 22-OCT-2011 Navigation Expires 24-SEP-2011 Apt Directory Expires 14-OCT-2011 Chart Data: N/A All mop and terrain data provided is only to be used as a sereral reference to veur surrounding ard as an aid to situational overeness Press "ENT" or rightnost softkey to continue Figure 1-8 MFD Power-Up Screen (172R shown) 190-00498-07 Rev. A Garmin G1000 Pilot's Guide for Cessna Nav III 13 INDEX ADDITIONAL APPENDICES AFCS FEATURES HAZARD AVOIDANCE FLIGHT AUDIO PANEL FLIGHT SYSTEM EIS MANAGEMENT & CNS INSTRUMENTS OVERVIEW SYSTEM OVERVIEW GARMIN. 1.6 SYSTEM OPERATION NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In reversionary mode, it can be adjusted from the remaining display. The displays are connected together via a single Ethernet bus for high-speed communication. Each IAU is connected to a single display, as shown in Figure 1-1. This allows the units to share information, enabling true system integration.. This section discusses normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations. NORMAL DISPLAY OPERATION In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information). The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection. 188.00 117.95 188.00 117.95 KHEN-KIRA CON 165m 119.700124.15 com 136.975 118.000 co IWFX 138 20 20 128 1160 15 CRS&BARO 105) TRIL 2 867 RANGE SOUTH EP CDE DE XPON NRST ALERIS Figure 1-9 Normal Mode 118.75 112.00 H 120 T 068 112.4-117.58 TIM 874° HAP-NAVIGATION HAP 0126 113.700 124.150 com 135.675128.600 COM 2200 OIL TEMP 191 FUEL STY SAA ELECTRICAL COATE 328 vats 228 ENGINE 19001 HAYYOR 73\ CRS BARO XURO HODY 100er OCLTR RANGE REVERSIONARY DISPLAY OPERATION NOTE: The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A for further information regarding system-specific alerts. In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In reversionary mode, all important flight information is presented on the remaining display in the same format as in normal operating mode. 14 Garmin G1000 Pilot's Guide for Cessna Nav III 190-00498-07 Rev. A GARMIN. SYSTEM OVERVIEW If a display fails, the appropriate IAU Ethernet interface to the display is cut off. Thus, the IAU can no longer communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is completely automated for all LRUs and no pilot action is required. TE CRSBARO RANGE F P CHEN KINA 173 G 112.48 117.58 135.675 128.608 TINTTO COM 20 2200 140 1201 128 9200 9100 CRS BARO 9200 1TM 100 874 RANGE ON INS ELECTRICAL 328 VOLTS 328 BATT S +110 +118 ENGINE INSE 612 Mvt NAV 010125 CDENT THREF ARST ADVISORY PAN SYSTEM OVERVIEW INSTRUMENTS FLIGHT AUDIO PANEL EIS & CNS MANAGEMENT FLIGHT AVOIDANCE HAZARD AFCS FEATURES ADDITIONAL APPENDICES INDEX Figure 1-10 Reversionary Mode (Failed PFD) If the system fails to detect a display problem, reversionary mode may be manually activated by pressing the Audio Panel's red DISPLAY BACKUP button (refer to the Audio Panel and CNS Section for further details). Pressing this button again deactivates reversionary mode. Pressing the DISPLAY BACKUP button activates/deactivates reversionary mode DISPLAY BACKUP Figure 1-11 DISPLAY BACKUP Button AHRS OPERATION NOTE: Refer to Appendix A for specific AHRS alert information. NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy. The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs. Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts. Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red 'X' flags over the corresponding flight instruments). 190-00498-07 Rev. A Garmin G1000 Pilot's Guide for Cessna Nav III 15