G1000 TM Cockpit Reference Guide for the Beechcraft 58/G58
Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0500.00 or later for the Beechcraft 58/G58. 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. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. WARNING: The Garmin G1000, as installed in the Beechcraft 58/G58 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 190-00526-00 Change Summary Initial release.
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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 4.7 Transponder ..................................
TABLE OF CONTENTS 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......................................... 7-1 7.2 Direct-to Navigation ............................
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 SECTION 10: HAZARD AVOIDANCE ........................... 10-1 10.1 Customizing the Hazard Displays on the Navigation Map .................................................... 10-1 10.2 STORMSCOPE® (Optional)..................................
TABLE OF CONTENTS GIA 63 Alert Messages ............................................ 12-11 GEA 71 Alert Messages ........................................... 12-13 GTX 33 Alert Messages ........................................... 12-14 GRS 77 Alert Messages ........................................... 12-14 GMU 44 Alert Messages.......................................... 12-15 GDL 69 Alert Messages ........................................... 12-15 GDC 74A Alert Messages ........................................
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 Functionality of the PFD and MFD controls are the same with the exception of the dedicated autopilot keys located only on the MFD bezel. (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 Toggle Key – Toggles the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver.
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 IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC).
SECTION 1 SYSTEM OVERVIEW 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 To 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. 2.
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 Actual Airspeed Speed Range (flaps 30 speed range) Vspeed References Flap Extension Speed Airspeed Trend Vector 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 Barometric Setting Box Altitude Reference Box To set barometric pressure, turn the BARO knob to select the desired setting. 2.4 Altitude Trend Vector Current Altitude The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV field. 2.
SECTION 2 FLIGHT INSTRUMENTS 2.6 VERTICAL SPEED INDICATOR 2.7 HORIZONTAL SITUATION INDICATOR (HSI) Selected Vertical Speed 14 13 1 Vertical Speed Bug Vertical Speed Pointer 12 2 11 3 10 4 9 8 5 Figure 2-9 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer. Pressing the VS key will display the Vertical Speed Bug. Press the NOSE UP or NOSE DN key to adjust.
SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Bearing Pointers and Information Windows Each tick mark is at 9 (half standard rate tick mark) and 18 (standard rate tick mark) degrees to the left and right of the lubber line. A wide magenta line displays the current turn rate, up to 24 degrees. A magenta arrowhead appears at 25 degrees. This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate.
SECTION 2 FLIGHT INSTRUMENTS DME Radio (optional) To display the DME Information Window, press the PFD softkey followed by the DME softkey. Figure 2-17 DME Information Window Navigation Source To change between navigation sources: 1. Press the CDI softkey to change from GPS to VOR1/LOC1. 2. Press the CDI softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3. Press the CDI softkey a third time to return to GPS.
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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, 166 GAL, and 194 GAL 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 NAV Frequency Navigation Status Window Selected COM Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Toggle Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Toggle Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Toggle Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • TX – When a COM radio is keyed, a white TX indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ID indication appears to the left of the corresponding active NAV frequency. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. 4.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD 4.7 TRANSPONDER Mode Selection The STBY, ON and ALT softkeys can be accessed by pressing the XPDR softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-9 Nearest Airports Window (PFD) 1. Press the NRST softkey to display the Nearest Airports Window. 2. Turn either FMS knob to highlight the desired frequency. 3.
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.).
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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 58/G58 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 Annunci
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Marker Beacon Signal Sensitivity 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 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ key to light the annunciator. Figure 5-5 Navigation Radios 5.4 INTERCOM SYSTEM (ICS) ISOLATION Pressing the small VOL/SQ knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively. Press the PILOT and/or COPLT key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY 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 If only the flight director is engaged, pitch and roll commands are given to manually maintain the selected altitude. If no altitude has been selected, Altitude Hold will not become active and the current pitch attitude will be maintained. Altitude Hold Mode (ALT) 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.
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 and roll 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. 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. Pitch and roll commands are given to manually maintain airspeed.
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 cancels all armed modes including Altitude Hold. Other roll axis modes may be selected after Go-Around mode engagement. Subsequent autopilot engagement is also allowed. If the pitch attitude is changes manually (e.
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 current. 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 4. With the autopilot engaged in a climb, set Selected Heading to 070 degrees using the HDG knob, then press the HDG key. The autopilot turns the aircraft to the desired heading. 5. As the aircraft climbs to the selected altitude, the autopilot changes from Vertical Speed mode to Altitude Hold mode. This is annunciated by the green ‘ALT’ flashing for ten seconds. 6.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial 3. The system calculates the point at which the autopilot changes from Heading mode to Navigation mode. When the aircraft reaches this point, ‘VOR’ flashes green in the active mode field. The autopilot begins turning to intercept the selected course. 4. The autopilot continues the turn until the aircraft is established on the selected course.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan / GPS Course 3. 1. The aircraft is currently tracking inbound on the 116 degree radial of Panoche VORTAC. Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2. With the flight plan activated, press the CDI softkey to set the CDI to GPS. This cancels VOR mode, and the autopilot loses the VOR signal.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) 3. 1. In preparation for the approach to KFAT, set Selected Altitude to 3,000 feet using the ALT knob. Press the FLC key. ‘FLC’ is annunciated with the airspeed reference, which defaults to the current aircraft airspeed. Altitude Hold mode is armed automatically. The current cruise speed of 142 knots will be used for the descent. 2. To allow the aircraft to descend, power must be reduced.
SECTION 6 – AUTOMATIC FLIGHT CONTROL ILS Approach 1. 2. Load the Runway 29R ILS approach for KFAT into the flight plan. ‘Vectors to Final’ is selected for the transition. Upon being given vectors from ATC, set the Selected Heading to the heading given by ATC. and press the HDG key. The autopilot turns the aircraft to the desired heading. Turn the HDG knob to set the Heading Bug to comply with ATC vectors, as requested. 3.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach 30 27 6 9 24 CZQ 21 15 18 e d Mo Upon reaching the holding pattern, set the Selected Heading to 307 degrees using the HDG knob and press the HDG key. The HDG knob is used for the remainder of the hold to guide the aircraft. 4. S GP 4. During the climb, set a desired hold altitude in the Selected Altitude box by turning the ALT knob. The CWS button may be used to manually set a new pitch attitude.
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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). 3.
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. 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 7. 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. 2.
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. 2.
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. Figure 8-3 Active Flight Plan Window on the PFD 8.3 1.
SECTION 8 – FLIGHT PLANNING 2. Press the ACT LEG softkey (using MFD only). OR 3. 4. 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. With ‘Activate’ highlighted, press the ENT key. 8.6 INVERT ACTIVE FLIGHT PLAN 1. From the Active Flight Plan Page, press the MENU key to display the Page Menu. 2. Turn the large FMS knob to highlight ‘Invert Flight Plan’ and press the ENT key.
SECTION 8 – FLIGHT PLANNING 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. 1. Press the FPL key and press the small FMS knob to activate the cursor. 2.
SECTION 8 – FLIGHT PLANNING 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. Press the CLR key to display a confirmation window. With ‘OK’ highlighted, press the ENT key to remove the selected procedure. 8.
SECTION 8 – FLIGHT PLANNING 3. 4. 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. 2. Press the MENU key to display the Flight Plan Catalog options. 3. Turn the large FMS knob to highlight ‘Delete Flight Plan’ and press the ENT key. With ‘OK’ highlighted, press the ENT key to invert the flight plan. 4. A ‘Delete flight plan?’ confirmation window is displayed.
SECTION 8 – FLIGHT PLANNING 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. Figure 8-16 Trip Planning Page 4. 5. For Direct-to planning, press the WPTS softkey and verify that the ‘from’ waypoint field indicates P.POS (present position). If necessary, press the MENU key and select ‘Set WPT to Present Position’ to display P.POS. Press the ENT key and the flashing cursor moves to the ‘to’ waypoint field.
SECTION 8 – FLIGHT PLANNING Figure 8-17 Vertical Navigation (VNAV) Page To create a vertical navigation profile: 8-8 1. Select the Vertical Navigation Page. 2. Press the FMS knob to activate the cursor. 3. With the ‘TARGET ALTITUDE’ field highlighted, turn the small and large FMS knobs to select the target altitude and press the ENT key. 4. Turn the small FMS knob to select ‘Above Wpt’ (AGL) or ‘MSL’, and press the ENT key. ‘Above Wpt’ uses the altitude of a destination airport.
SECTION 8 – FLIGHT PLANNING With the profile set, the vertical speed required (VSR) is displayed. Expect the following to occur when using the vertical navigation feature: At one minute prior to reaching the initial descent point, the message ‘APPR VPROF - Approaching VNAV Profile’ is displayed as a PFD alert. The descent (or climb) angle also locks to prevent changes in speed from altering the profile.
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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. 4.
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. 9.2 Load and/or Activate an Approach Procedure 1. With the Navigation Map Page displayed, press the FPL key. 2. Press the LD APR softkey. If a flight plan is active, the destination airport will be displayed as the default. A list of available approaches is also displayed. 3.
SECTION 9 – PROCEDURES 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. Selecting ‘Load?’ will add the procedure to the flight plan without immediately using it for navigation guidance. Activate An Approach in the Active Flight Plan 1. With the Navigation Map Page displayed, press the PROC key. 2. Turn the large FMS knob to highlight ‘ACTIVATE APPROACH’. 3. Press the ENT key.
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SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: Use of the Stormscope system for hazardous thunderstorm penetration is prohibited. 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.
SECTION 10 – HAZARD AVOIDANCE To 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 are 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: Use of XM weather for hazardous weather penetration is not recommended.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page To 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 Weather Data Link Page. 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. Displaying Traffic on the Traffic Map Page 1.
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 Traffic Map Page. 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. Displaying Terrain and Obstacles on the Terrain Proximity Page 1.
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 Maximum elevation of topography presently displayed on-screen Minimum elevation of topography presently displayed on-screen Displaying Terrain on the TAWS Page 1. Turn the large FMS knob to select the Map Page Group. 2.
SECTION 10 – HAZARD AVOIDANCE Enable/Disable Aviation Data 1. While the TAWS Page is displayed, press the MENU key. 2. Turn the small FMS knob to select “Show (or Hide) Aviation Data”. 3. Press the ENT key. Figure 10-18 TAWS Page (ARC View) Figure 10-19 TAWS Page Menu Color Alert Level Suggested Pilot Response Terrain/Obstacle at or within 100’ below current aircraft altitude. WARNING Initiate climb and/or turn away from terrain/obstacle.
SECTION 10 – HAZARD AVOIDANCE TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled. To Inhibit TAWS: 1. While the TAWS Page is displayed, press the MENU key. 2. Turn the small FMS knob to select‘Inhibit TAWS’. 3. Press the ENT key. To Enable TAWS: 1. While the TAWS Page is displayed, press the MENU key. 2. Turn the small FMS knob to select ‘Enable TAWS’. 3. Press the ENT key.
SECTION 10 – HAZARD AVOIDANCE Final Approach Fix 200' below FAF Altitude Runway Threshold CAUTION 0. 5 n m Glideslope Intercept Final Approach Fix 200' below FAF Altitude Runway Threshold 0.5 nm CAUTION PDA Alert is 0.7 Below Glideslope 15 nm Figure 10-21 ILS Approach PDA Alert Threshold 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.
SECTION 10 – HAZARD AVOIDANCE Negative Climb Rate After Takeoff Alert (NCR) Maximum elevation of topography presently displayed on-screen The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that 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.
SECTION 10 – HAZARD AVOIDANCE Pop-up Alerts When a terrain or obstacle alert is issued, a pop-up window is displayed on the MFD with the appropriate alert. Figure 10-25 Alert Pop-Up Press the ENT key to display the TAWS Page, or press the CLR key to remain on the existing page.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued.
SECTION 10 – HAZARD AVOIDANCE 10.8 AIRBORNE WEATHER RADAR Displaying Weather on the Weather Radar Page 1. Turn the large FMS knob to select the Map Page Group. 2. Turn the small FMS knob to select the Weather Radar Page. 3. Press the MODE softkey. 4. If the aircraft is on the ground, press the STANDBY softkey to initiate the one minute warm-up period. After the warm-up is complete, the radar will enter the standby mode. After the aircraft is airborne, press the WEATHER softkey. 4.
SECTION 10 – HAZARD AVOIDANCE On the Vertical Scan Display 1. Scan Line Bearing Line Press the TILT softkey to activate the cursor in the TILT field and display the Tilt Line. 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 will be implemented when Horizontal Scan is again selected. Vertically Scan a Storm Cell 1.
SECTION 10 – HAZARD AVOIDANCE Adjusting Gain 1. Press the GAIN softkey to activate the cursor in the GAIN field. 2. Turn the small FMS knob to adjust the gain for the desirable level. The gain setting is visible in the gain field as a movable horizontal bar in a flashing box. The line pointer is a reference depicting the calibrated position. 3. Press the FMS knob to remove the cursor. 4. Press the GAIN softkey again to recalibrate the gain. CALIBRATED will be displayed in the GAIN field.
SECTION 10 – HAZARD AVOIDANCE Figure 10-35 40˚ Sector Scan Figure 10-34 Selecting Sector Scan Position 3. 4. 5. 6. 7. Turn the small FMS knob to place the Bearing Line in the desired position. The location of the Bearing Line will become the center point of the Sector Scan. Turn the large FMS knob to place the cursor in the SECTOR SCAN field. Turn the small FMS knob to select FULL, 60˚, 40˚, or 20˚ scan.
SECTION 10 – HAZARD AVOIDANCE To activate or deactivate the Watch feature, press the WATCH softkey. Figure 10-36 Horizontal Scan Without WATCH Displayed intensity is questionable. Potentially stronger than displayed.
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 58/G58 Pilot’s Operating Handbook (POH) supersedes information found in this document. The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation window displays abbreviated annunciation text.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Beechcraft 58/G58 aircraft, uses four alert levels. • WARNING: This level of alert is time critical and requires immediate pilot attention. A warning annunciation is displayed in the Annunciation Window as red text. A warning annunciation is also accompanied by a flashing red WARNING softkey label, as shown in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 BEECHCRAFT 58/G58 ANNUNCIATIONS & ALERTS See the Beechcraft 58/G58 Pilot’s Operating Handbook (POH) for information regarding pilot responses. WARNING Annunciation Annunciation Window Text GEAR UP Alerts Window Message Gear up. L ALT INOP R ALT INOP L-R ALT INOP Left alternator offline. Right alternator offline. Right and Left alternators 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” 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 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. GPS information is either not present or is invalid for navigation use.
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 Alert Messages 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. MANIFEST – PFD1 software mismatch.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Alert Messages 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 GMA 1347 Alert Messages Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. GMA1 CONFIG – GMA1 configuration The audio panel configuration settings do not match backup configuration memory. error. Config service req’d. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Alert Messages (Cont.) Alerts Window Message Comments MANIFEST – GIA1 software mismatch. Communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch. be serviced. Communication halted. COM1 TEMP – COM1 over temp. The system has detected an over temperature condition in COM1 and/or COM2. The Reducing transmitter power. transmitter will operate at reduced power.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Alert Messages (Cont.) Alerts Window Message Comments GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still GPS2 SERVICE – GPS2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. A failure has been detected in the NAV1 and/or NAV2 receiver.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Alert Messages 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 Alert Messages 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 Alert Messages 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 Alert Messages (Cont.) Alerts Window Message Comments LOCKED FPL – Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan. locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. -[xxxx] STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead.
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INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-2 Active flight plan 8-2 ADVISORY 12-1 Advisory 12-2 AFCS 1-1, 6-1, 6-2, 6-4, 6-6, 6-7, 6-9, 6-11, 6-12, 6-13, 12-4 Age 10-6 AHRS 12-14 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 messages 12-8 – 12-17 Alert Pop-Up 10-15 Altitude Hold 1-4 Altitude hold 1-4, 6-4 – 6-8, 6-10
INDEX H HDG key 6-10, 6-14, 6-18, 6-19 Heading hold 6-9 Heading indication 2-6 Heading Select 1-3, 1-4, 6-9, 6-10 Heading Select Mode 6-10 Headset(s) 5-2 Hijack code 4-5 Horizontal scan 10-18, 10-19, 10-22 Horizontal situation indicator 2-5 Hurricanes 10-5 I ICAO 4-5 ID 4-3 IDENT function 4-5 Imminent Terrain Impact 10-12 Impact point 10-12 Inhibit 10-12 Inhibit TAWS 10-12 INTEG 2-7 Interrogations 4-4 IOI 10-12, 10-16, 12-5 ITI 10-12 K Key(s) 1-4 L Lighted obstacle 10-14 Lightning 1-4, 1-7, 10-2, 10-3, 1
INDEX T W TA 10-7, 12-6 TAF 10-3 TAS 10-8, 10-9, 10-18 – 10-21, 12-6, 12-14 TAWS 10-10 – 10-12, 10-14 – 10-17, 12-5, 12-6 TAWS-B 10-10 TAWS system test 10-12 Terrain 10-9, 10-10, 10-15, 10-17, 12-10 Terrain separation ii Tilt 10-18, 10-19 Tilt line 10-18, 10-19 TIS 12-17 Tornado 10-5 Trademark i Traffic advisory 10-7, 10-8, 10-9, 10-17, 10-18, 12-6 Traffic map page 10-7, 10-8, 10-9, 10-14 Transponder 4-4 Transponder Status bar 4-4 Trend vector 2-6 Tropical storms 10-5 Turn rate indicator 2-6 TX 4-3 WARN 2-
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