Integrated Flight Deck Cockpit Reference Guide Beechcraft A36/G36
Copyright © 2005-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0464.08 or later for the Beechcraft A36/G36. 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. Tel: 503/391.
WARNINGS, CAUTIONS, & NOTES . WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight.
WARNINGS, CAUTIONS, & NOTES WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in the Beechcraft A36/G36 aircraft, has a very high degree of functional integrity.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00525-00 190-00525-01 Rev A Change Summary Initial release. Added GDU software version 6.13 parameters. Added TAWS Revision Date of Revision Affected Pages B 9/07 Copyright Page Description Changed system software number to 0464.08.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Backlighting ............................................................. 1-8 Database Updates ..................................
TABLE OF CONTENTS Flying a GPS Flight Plan............................................. 6-16 Flight Level Change (Descent).................................... 6-17 ILS Approach ............................................................. 6-18 Go-Around / Missed Approach................................... 6-19 SECTION 7: NAVIGATION .................................................. 7-1 7.1 Navigation Map Page ............................................ 7-1 Select the MAP Page Group........................
TABLE OF CONTENTS 9.2 Approaches .............................................................. 9-2 Load and/or Activate an Approach Procedure ............... 9-2 Activate An Approach in the Active Flight Plan ............. 9-3 Excessive Descent Rate Alert (EDR) .......................... 10-13 Negative Climb Rate After TakeoffAlert (NCR) .......... 10-13 “Five-Hundred” Aural Alert...................................... 10-13 Displaying Terrain and Obstacles on the Navigation Map ...........................
TABLE OF CONTENTS Blank Page iv Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide.
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Transfer Key – Switches the standby and active NAV frequencies.
SECTION 1 SYSTEM OVERVIEW (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 reference altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds.
SECTION 1 SYSTEM OVERVIEW BRG1 (bearing) – Press to cycle through the following information: NAV1 – Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 information window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG1 information window. OFF – Removes the BRG1 information window. BRG2 (bearing) – Press to cycle through the following information: NAV2 – Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 information window.
SECTION 1 SYSTEM OVERVIEW OBS – Press to select OBS mode on the CDI when navigating by GPS (only available with active leg). CDI – Press to change navigation mode on the CDI between GPS, VOR1, and VOR2. DME (optional) – Press to display the DME Tuning window. XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select standby mode. ON – Press to select mode A. ALT – Press to select altitude reporting mode. VFR – Press to automatically squawk 1200 (only in the U.S.A.
SECTION 1 SYSTEM OVERVIEW 1.3 MFD SOFTKEYS ENGINE – Pressing this softkey makes available the LEAN and SYSTEM Softkeys which in turn access the Lean Page and the System Page, respectively. MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/removes Traffic on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map.
SECTION 1 SYSTEM OVERVIEW 1.4 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-7. Nearest Group Auxiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group Figure 1-7 Page Group Icon 1.5 Selected Page BACKLIGHTING Manually adjust the backlight for the PFD and MFD: 1-8 1) Press the MENU Key on the PFD to display the PFD Setup Menu window.
SECTION 1 SYSTEM OVERVIEW 1.6 DATABASE UPDATES Aviation Database Update 7) Terrain and Obstacle Database Updates NOTE: The display downloads the aviation database and stores it internally. The aviation database SD card is not required to remain in the display after the update. 1) 2) 3) NOTE: The data contained in the terrain and obstacle databases comes from government agencies.
SECTION 1 SYSTEM OVERVIEW 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 4) At the MAP – NAVIGATION MAP page, select the MAP Softkey and check to make sure that the TOPO and TERRAIN softkeys are functional (not grayed out). 5) Power down the G1000.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 11 1 10 9 2 8 3 7 4 5 6 1 Traffic Annunciation 7 Alerts Window 2 Selected Heading Box 8 Selected Course Box 3 Inset Map 9 Annunciation Window 4 BRG1 Information Window 10 Vertical Deviation/Glideslope Indicator 5 DME Information Window 11 Marker Beacon Annunciation 6 BRG2 Information Window Figure 2-2 Additional PFD Information Distance to Next Waypoint Next Waypoint Desired Track to Next Waypoint Current Track Figure 2-3 PFD Navigation Status Wi
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Vspeed References Airspeed Trend Vector Actual Airspeed Speed Range (flap speed range) Vspeed References (best glide) True Airspeed Box Figure 2-4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Vspeed References are turned on or off in the Timer/References window. Press the TMR/REF Softkey to display the widow.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Alerting Altitude Reference Box Within 1000 ft Within 200 ft Deviation of ±200 ft Figure 2-8 Altitude Alerting Visual Annunciations Altitude Trend Vector Altitude Select Bug Current Altitude Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.
SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft 2.5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Barometric Minimum Bug Vertical Deviation/Glideslope Indicator Barometric Minimum Box Altitude Reached Figure 2-10 Marker Beacon and Vertical Deviation 2.6 VERTICAL SPEED INDICATOR Selected Vertical Speed Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS 2.7 HORIZONTAL SITUATION INDICATOR (HSI) 14 13 1 12 2 11 3 10 4 9 Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
SECTION 2 FLIGHT INSTRUMENTS Course Deviation Indicator (CDI) Distance to Bearing Source The CDI scale automatically adjusts to the current phase of flight (enroute 5.0 nm, terminal area 1.0 nm, or approach 0.3 nm). Scaling may be selected manually from the MFD System Setup Page. See System Setup in the G1000 Pilot’s Guide for more details.
SECTION 2 FLIGHT INSTRUMENTS • INTEG – GPS information is either not present or is invalid for navigation use • WARN – GPS detects a position error • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. Figure 2-20 GPS INTEG, GPS SUSP, LOC1 and VOR2 Enable/disable OBS mode while navigating with GPS: 1) Press the OBS Softkey to select OBS Mode. 2) Turn the CRS Knob to select the desired course TO/FROM the waypoint.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 3.2 LEAN ENGINE DISPLAY ENGINE DISPLAY In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys which in turn provide access to the Lean Page and the System Page, respectively.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 ENGINE SYSTEM DISPLAY If desired, use the DEC FUEL, INC FUEL and RST FUEL Softkeys to adjust the amount of fuel remaining for totalizer calculations. NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The Nav/Com controls and frequency windows are located on the Primary Flight Display and the MultiFunction Display in the same locations.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies. • Press to change tuning box positions.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD 4.7 TRANSPONDER Mode Selection The STBY, ON and ALT Softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-9 Nearest Airports Window (PFD) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn either FMS Knob to highlight the desired frequency.
SECTION 4 – NAV/COM & TRANSPONDER Following is a list of important codes: • 1200 – VFR code in the U.S. (please refer to the ICAO standards for VFR codes in other countries). • 7000 – VFR code commonly used in Europe (please refer to the ICAO standards). • 7500 – Hijack code. • 7600 – Loss of communication code. • 7700 – Emergency code. • 7777 – Military interceptor operations code (NEVER ENTER THIS CODE). • 0000 – Code for military use (in the U.S.).
SECTION 4 – NAV/COM & TRANSPONDER Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transceiver Audio (COM 3 is unavailable) Transmitters (COM3 MIC is unavailable) Split COM (Not recommended for use in the Beechcraft A36/G36) Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (DME optional, ADF & AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annun
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Outer Marker Annunciator Middle Marker Annunciator Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC Key, press the already selected COM1 or COM2 Key before pressing the other COM MIC Key.
SECTION 5 – AUDIO PANEL 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1. 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER AND PLAYBACK Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL In addition to the AFCS (Automatic Flight Control System) keys on the MFD, as discussed in the System Overview section, the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD. • AP DISC (Autopilot Disconnect) Button — Located on the pilot’s control wheel, pressing this button disengages the autopilot. Pressing it also acknowledges an autopilot disconnect.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Active Mode Yaw Damper Status Mode Reference Autopilot Status Armed Mode Armed Mode Active Mode Roll Axis Modes Pitch Axis Modes AFCS Status Bar System Status Field (see Annunciations & Alerts) Selected Altitude Box Aircraft Attitude Symbol Flight Director Command Bars Figure 6-3 PFD AFCS Display 6.2 OVERSPEED PROTECTION An overspeed annunciation (flashing inverse video) is displayed above the airspeed tape.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Automatic Disengagement Yaw Damper Automatic disengagement typically occurs due to a failure. Automatic disengagement is annunciated by a flashing ‘AP’, alternating red on white and white on red in the Autopilot Status field. Also, the autopilot disconnect aural alert will be heard. Both the annunciation and the aural alert will continue until acknowledged by pressing the AP DISC button or the MET ARM switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL AFCS Key FD/AP only ALT VS FLC APR GA AFCS Mode Annunciation Pitch Hold (Default) PIT Altitude Hold ALT nnnnn FT Vertical Speed VS nnnn FPM Flight Level Change FLC nnn KT Glideslope (vertical comGS ponent of Approach) Go Around GA The default pitch axis mode is Pitch Hold (PIT). When no other pitch axis modes are selected, this is the active pitch axis mode when the autopilot and/or flight director is engaged. Pitch Hold Mode (PIT) 1) Press the AP or FD Key.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Altitude Hold Mode (ALT) 3) 1) Press the ALT Key. The flight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode field with the current altitude displayed in the Altitude Reference field. 2) Pitch commands will be given to manually maintain the current altitude. Press the AP Key to engage the autopilot for maintaining the current altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change Mode (FLC) 1) 2) 3) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select box. This altitude must be selected first because Flight Level Change mode will only fly toward a selected altitude. Press the FLC Key. The flight director is activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode field and the Airspeed Bug will appear on the Airspeed Indicator.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around Mode (GA) Glideslope (GS) Pressing the GA button (not located on the MFD) engages the flight director in a wings level, 7 degree pitch up attitude. Go-Around mode disengages the autopilot, and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is also allowed. If the pitch attitude is changed manually (e.g with CWS button or the NOSE UP/NOSE DN Keys), Pitch and Roll Hold modes will automatically be selected.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 If the aircraft bank angle is < 6 degrees when the key is pressed, the aircraft will be maintained at wings level. If only the flight director is active, command bars give guidance to maintain wings level. ROLL AXIS MODES Mode annunciations for active roll axis modes are shown in green during normal operation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) 1) 2) 3) Turn the HDG Knob to move the heading bug on the HSI to the desired heading. When the knob is turned, the Selected Heading box will appear and remain for three seconds after the knob stops moving. The selected heading will be displayed in the Selected Heading box. With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode field.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. The Navigation mode acquires and tracks the selected navigation receiver on the HSI (e.g. GPS, VOR or LOC). GPS roll steering commands are followed when the HSI is in GPS mode, and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR, LOC, or BC (backcourse) modes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach Mode (GPS, VAPP or LOC) The Approach mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC). This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. The Approach mode provides greater sensitivity for VOR tracking than Navigation mode, and allows the autopilot to fly an ILS approach with a glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.7 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in the following examples are for instructional purposes only and may not be used for navigation. This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure 3) Activate Heading Select Mode while the autopilot is engaged in the climb. Climb to the selected altitude and fly an assigned heading: a) Use the HDG Knob to set the Selected Heading to 070°. 1) Upon takeoff, set the Selected Altitude to 7000 feet using the ALT Knob. b) Press the HDG Key. The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial NOTE: Changing the HSI mode cancels Navigation Mode and causes the flight director to revert to Roll Hold Mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V107 to Panoche VORTAC (PXN) should now be intercepted. 1) Tune the VOR frequency and activate Heading Select Mode. a) Use the CDI Softkey to set the HSI mode to VOR. c) Press the NAV Key to arm Navigation Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2) Transition from VOR to GPS Navigation Mode. a) Use the CDI Softkey to put the HSI in GPS mode. This cancels VOR mode on the HSI and the flight director loses the VOR signal. As a result, the VOR annunciation flashes yellow.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) While flying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. 1) Enter Flight Level Change Mode. a) Using the ALT Knob, set the Selected Altitude to 3000 feet. b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed, 142 knots.
SECTION 6 – AUTOMATIC FLIGHT CONTROL ILS Approach 3) In preparation for approach, tune the localizer frequency and select LOC mode on the HSI. 1) Transition from GPS Navigation Mode to Heading Select Mode. 4) Press the APR Key when cleared for approach to arm the Approach Mode. ‘LOC’ and ‘GS’ appear in the armed roll and pitch mode fields, respectively. The autopilot and flight director determine when to begin the turn to intercept the final approach course.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach 1) Push the GA button at the Decision Height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. Note that when the GA button is pushed, the autopilot disconnects and the ‘AP’ annunciation flashes yellow for five seconds 30 CZQ 27 9 24 4. 12 21 15 18 e od SM GP c) Press the NAV Key to have the autopilot fly to the hold.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-20 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1) Turn the large FMS Knob until MAP is highlighted in the page group window in the lower right of the MFD display. 2) Turn the small FMS Knob to select the first MAP page (indicated by a solid rectangular icon).
SECTION 7 – NAVIGATION 4) 5) Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport. Press the ENT Key to confirm the selection. Press ENT again to activate a Direct-to. Re-center the CDI (HSI) needle to the same destination waypoint: 1) ) Key, followed Press the Direct-to ( by pressing the ENT Key twice. NOTE: If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION 6) To remove the flashing cursor, press the FMS Knob. Access Runway Information 1) Press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the Runways field. 3) Turn the small FMS Knob to display the next runway for the selected airport. 4) Continue turning the small FMS Knob to select the desired runway. 5) To remove the flashing cursor, press the FMS Knob.
SECTION 7 – NAVIGATION 7.4 INTERSECTION INFORMATION 7.5 NDB INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the WPT page group. 2) Turn the small FMS Knob to select the second rectangular page icon. Figure 7-7 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the WPT page group.
SECTION 7 – NAVIGATION 7.6 VOR INFORMATION 7.7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.8 NEAREST AIRPORTS Figure 7-8 VOR Information Page Select the VOR Information Page 1) Turn the large FMS Knob to select the WPT page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION Access Runway Information for the Selected Airport 2) Press the ENT Key to display airport information. Press the ENT Key again (cursor is on ‘BACK’) to return to the list. 1) Press the RNWY Softkey located at the bottom of the display. 3) 2) Turn the small FMS Knob to select the desired runway. Load an Airport COM Frequency into the Active COM 1) Turn the large FMS Knob to place the cursor on the desired airport frequency shown in the window.
SECTION 7 – NAVIGATION 2) Turn the small FMS Knob to select the second rectangular page icon. View Information on the Nearest Intersection 1) 2) Press the FMS Knob to activate the cursor. Turn either FMS Knob to select the desired intersection. Press the ENT Key. 7.10 NEAREST NDB on the Nearest NDB Page pertains to the selected NDB. 7.11 NEAREST VOR Select the Nearest VOR Page 1) Turn the large FMS Knob to select the NRST page group.
SECTION 7 – NAVIGATION Select and Load a VOR Frequency 1) With the Nearest VOR Page selected, press the FREQ Softkey to highlight the VOR frequency for the selected VOR. 2) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. OR Press the MENU Key. Select the Select Frequency Window option and press the ENT Key. Press the ENT Key again when the frequency field is highlighted to place the selected VOR frequency in the NAV standby field.
SECTION 7 – NAVIGATION Select and Load the Nearest ARTCC, FSS, or Weather Frequency 1) With the Nearest Frequencies Page selected, press the ARTCC, FSS, or Wx Softkey. 2) Turn the large FMS Knob to select the frequency. 3) Press the ENT Key to load the frequency into the ‘COM’ frequency standby field. 7.14 NEAREST AIRSPACES • If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside, ‘Ahead < 2 nm’ is displayed.
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SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 3) Turn the large FMS Knob to highlight the latitude/longitude field or the Reference Waypoints field, depending on how the waypoint is to be defined. 4) Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint. 5) Press the ENT Key to accept the new waypoint. 6) Press the FMS Knob to remove the flashing cursor.
SECTION 8 – FLIGHT PLANNING Modify a User Waypoint 1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes. 3) Press the ENT Key to accept the changes. 4) Press the FMS Knob to remove the flashing cursor. Delete a User Waypoint 1) 2) 8.
SECTION 8 – FLIGHT PLANNING 8.4 1) 2) ACTIVATE A FLIGHT PLAN LEG From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. Press the ACT LEG Softkey (using MFD only). OR 3) 4) flight plan, only the active flight plan. Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key. This step must be used when activating a leg from the PFD.
SECTION 8 – FLIGHT PLANNING 2) Press the NEW Softkey to display a blank flight plan page for the first empty storage location. Figure 8-10 Create FPL on MFD 3) Turn the small FMS Knob to display the Waypoint Information Page. Turn the small FMS Knob to enter the first character of the identifier of the departure waypoint. Turn the large FMS Knob to move the cursor to the next character field. Repeat using the FMS Knobs until the desired identifier has been entered.
SECTION 8 – FLIGHT PLANNING 8.10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures. 8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN 1) 2) 3) With the Active or Stored Flight Plan Page displayed, press the small FMS Knob to activate the cursor. Turn the large FMS Knob to highlight the title for the approach, departure or arrival to be deleted. Titles appear in white directly above the procedure’s waypoints.
SECTION 8 – FLIGHT PLANNING 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired flight plan and press the MENU Key to display the Page Menu options. 3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’ and press the ENT Key. The original flight plan remains intact in its flight plan catalog storage location.
SECTION 8 – FLIGHT PLANNING 8.19 TRIP PLANNING 1) Turn the large FMS Knob to select the AUX page group. 2) Turn the small FMS Knob to select the first rectangular page icon. 3) The current page mode is displayed at the top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey. the ENT Key to accept the waypoint. The flashing cursor moves to the ‘to’ waypoint.
SECTION 8 – FLIGHT PLANNING 8.20 VERTICAL NAVIGATION (VNAV) PAGE 5) Press the ENT Key. The cursor is now positioned over the ‘Before’ and ‘After’ field. NOTE: An active flight plan or Direct-to must be entered in order to utilize VNAV. 6) Turn the small FMS Knob to select whether the previously set distance is ‘Before’ or ‘After’ the endpoint. NOTE: VNAV is advisory only and cannot be coupled to the autopilot. 7) Press the ENT Key. The cursor is now placed over the VNAV profile endpoint field.
SECTION 8 – FLIGHT PLANNING the target altitude. If the selected altitude is above the current aircraft altitude, a profiled climb is created. If the selected altitude is below the current aircraft altitude, a profiled descent will be created. 11) Press the ENT Key. The cursor is now placed in the ‘TARGET VERTICAL SPEED’ field. The default profile utilizes a 400 foot-per-minute descent rate. 12) To change the vertical speed, turn the FMS Knobs to enter the desired vertical speed. Press the ENT Key when finished.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) With the Navigation Map Page displayed, press the FPL Key. 2) Press the LD DP Softkey. If a flight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. 3) If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 6) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. will not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS).
SECTION 9 – PROCEDURES 6) The cursor will move to the TRANSITIONS field. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key. (The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course.) Figure 9-7 Selecting an Approach Transition 7) Turn the large FMS Knob to highlight ‘Activate?’ and press the ENT Key to activate the approach.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: The Stormscope system is not intended to be used for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation. 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) 2) 3) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Stormscope Page 1) Turn the large FMS Knob until the Map Page group is selected. 2) Turn the small FMS Knob until the Stormscope Page is selected. This is the third rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE Change the viewing mode between 360˚ and 120˚: 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. Press the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. 3) Press the available softkeys to select the desired XM weather product. 4) Press the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – Pressing the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – Press the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • • • • • Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range NOTE: If the G1000 is configured to use the optional Skywatch Traffic Advisory System, TIS will not be available for use. NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
SECTION 10 – HAZARD AVOIDANCE 10.5 SKYWATCH TRAFFIC ADVISORY SYSTEM (TAS)(OPTIONAL) Traffic Advisory, aircraft is 400’ below Traffic Mode Altitude Mode & climbing Traffic, Out of Range Refer to the SkyWatch pilot’s guide for a detailed discussion of the SkyWatch system. Displaying Traffic on the Traffic Map Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the second rectangular page icon. 3) Press the OPERATE Softkey to begin displaying traffic.
SECTION 10 – HAZARD AVOIDANCE 4) Traffic Advisory Non-Bearing Traffic Off Scale Traffic Advisories Banner Rotate the JOYSTICK clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Non-Threat Traffic Figure 10-13 TAS Traffic on Navigation Map 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Unlighted Obstacle (Height is less than 1000’ AGL) Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Figure 10-15 Obstacle Symbols 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Suggested Pilot Response Terrain/Obstacle at or within 100’ below or above aircraft altitude. Red Initiate climb and/or turn away from terrain/obstacle. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Be aware of surroundings. Be prepared to take action. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. No action required.
SECTION 10 – HAZARD AVOIDANCE Manual System Test A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” will be heard. The system test may also be initiated manually, but only when the aircraft is on the ground. To manually verify proper operation of the aural and visual annunciations of the system, perform the following steps. 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select ‘Test TAWS’.
SECTION 10 – HAZARD AVOIDANCE Excessive Descent Rate Alert (EDR) The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 10-20 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up).
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1) 2) With the Navigation Map displayed, press the MAP Softkey. Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established.
SECTION 11 – ABNORMAL OPERATION SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display.
SECTION 11 – ABNORMAL OPERATION 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.500 MHz) automatically becomes the active frequency to the pilot through the pilot headset. 11.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Beechcraft A36/G36 Pilot’s Operating Handbook (POH) supersedes information found in this document.
SECTION 12 – ANNUNCIATIONS & ALERTS detects invalid data. A red ‘X’ is accompanied by an alert message in the Alerts Window. • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Beechcraft A36/G36 aircraft, uses four alert levels. • WARNING: This level of alert is time critical and requires immediate pilot attention.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 A36/G36 AIRCRAFT ANNUNCIATIONS & ALERTS The following alert annunciations are configured specifically for the Beechcraft A36/G36 aircraft. See the Beechcraft A36/G36 Pilot’s Operating Handbook (POH) for information regarding pilot responses. WARNING Annunciation Annunciation Window Text GEAR UP ALT 1 INOP ALT 2 INOP ALT 1-2 INOP Alerts Window Message Gear up. Alternator 1 offline. Alternator 2 offline. Alternators 1 and 2 offline.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 AFCS ALERTS System Status Field System Status Field The following AFCS alert annunciations appear in the AFCS System Status field on the PFD. • WARNING: Red annunciation is time critical and indicates an abnormal AFCS condition requiring immediate pilot attention. • CAUTION: Yellow annunciation indicates the existence of abnormal AFCS conditions that may require pilot intervention.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Attitude and Heading Reference System is aligning. Display system is not receiving attitude information from the AHRS. Display system is not receiving airspeed input from air data computer. Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS.
SECTION 12 – ANNUNCIATIONS & ALERTS Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. 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 POH). Display is not receiving valid transponder information.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs. GIA 63 Integrated Avionics Units GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS OR GMU 44 Magnetometer GEA 71 Engine Airframe Unit OR GIA 63 Integrated Avionics Unit GIA 63 Integrated Avionics Units GDC 74A Air Data Computer Figure 12-6 G1000 System Failure Annunciations 12.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. PFD1 CONFIG – PFD1 configuration error. Config service req’d. MFD1 CONFIG – MFD1 configuration error. Config service req’d. SW MISMATCH – GDU software mismatch. Xtalk is off.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, the G1000 system should be serviced. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. The MFD and/or PFD detected a failure in the basemap database.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Alerts Window Message DB MISMATCH – Airport Terrain database mismatch. Xtalk is off Comments The PFD and MFD have different airport terrrain databases installed. Crossfill is off. Install correct airport terrain database in both displays. GMA 1347 Message Advisories Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. There is a hardware mismatch between GIA1 and GIA2. The G1000 system should HW MISMATCH – GIA hardware be serviced. mismatch. Communication halted.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS ACC – GPS position GPS position accuracy has been degraded and RAIM is not available. accuracy degraded & RAIM unavailable. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced. GPS2 FAIL – GPS2 is inoperative. GPS1 SERVICE – GPS1 needs service. Return unit for repair.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch. Communication halted. BACKUP PATH – XPDR1 using backup data path. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Alerts Window Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch. Communication halted. Comments A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the aircraft position. ahead. ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. LEG UNSMOOTH – Flight plan leg will The approaching flight plan waypoints are too close to allow for smooth turns. not be smooth.
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 Advisory 12-1, 12-2 AFCS 1-3, 6-1, 6-2, 6-4, 6-6, 6-7, 6-9, 6-11, 6-12, 6-13, 12-4 Age 10-6 AHRS 12-15 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-6 Airport information 7-3 Airspace alerts 7-9 Airspeed indicator 2-3 Airspeed trend vector 2-3 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Alert Message 12-2 Alert message 12-1 Alert Pop-Up 10-14 Altitude hold 1-4, 6-4 – 6-8, 6-10 Altitude trend vector 2-4 ALT knob
INDEX Horizontal situation indicator 2-6 Hurricanes 10-5 I ICAO 4-5 ID 4-3 IDENT function 4-5 Imminent Terrain Impact 10-12 Impact point 10-12 Inhibit 10-11 Inhibit TAWS 10-11 INTEG 2-8 Interrogations 4-4 IOI 10-12, 10-15, 12-5 ITI 10-12 K N Nav/Com controls 4-1 NAV1 5-2 NAV2 5-2 NAVAIDS iii Navigation 7-1 Navigation Mode 6-11 Navigation status window 2-2 NAV Frequency Window 4-1 NCR 10-13 Nearest Airports Page 7-3, 7-5 – 7-9, 8-1 Nearest ARTCC & FSS frequencies 7-8 Negative Climb Rate After Takeoff 10-1
INDEX Tornado 10-5 Traffic Advisory 10-7, 10-8, 10-9, 12-6 Traffic advisory 10-16 Traffic map page 10-7, 10-8, 10-9, 10-14 Transponder 4-4 Transponder Status bar 4-4 Tropical storms 10-5 TX 4-3 Y Yaw Damper 1-4, 6-2, 6-3, 12-4 Yaw damper 1-4, 6-2, 6-3, 12-4 YD 1-4 U Unlighted obstacle 10-14 V Vertical Deviation/Glideslope indicator 2-5 Vertical navigation profile 8-8 Vertical speed 1-4, 2-1, 2-5, 6-4, 6-6, 12-1 Vertical Speed Bug 2-5 Vertical Speed Mode 6-6 VFR code 4-5 VHF 4-1 Voice Alerts 12-6 Voice alerts
INDEX Blank Page Index-4 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
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