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Garmin G1000:Beechcraft Baron 58/G58, User Manual


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190-00663-00  Rev. A

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT

A-9

APPENDIX A

MFD & PFD MESSAGE ADVISORIES (CONT.)

Message

Comments

MFD1 CONFIG

 – MFD1 configuration 

error.  Config service req’d.

The MFD configuration settings do not match backup configuration memory.  The 
G1000 system should be serviced.

SW MISMATCH

 – GDU software 

version mismatch.  Xtalk is off.

The MFD and PFD have different software versions installed.  The G1000 system 
should be serviced.

PFD1 COOLING 

– PFD1 has poor 

cooling.  Reducing power usage.

The PFD and/or MFD is overheating and is reducing power consumption by dimming 
the display.   If problem persists, the G1000 system should be serviced.

PFD2 COOLING 

– PFD2 has poor 

cooling.  Reducing power usage.

MFD1 COOLING

 – MFD1 has poor 

cooling.  Reducing power usage. 

PFD1 KEYSTK

 – PFD1 [key name] Key 

is stuck.

A key is stuck on the PFD and/or MFD bezel.  Attempt to free the stuck key by 
pressing it several times.  The G1000 system should be serviced if the problem 
persists.

PFD2 KEYSTK

 – PFD2 [key name] Key 

is stuck

MFD1 KEYSTK

 – MFD1 [key name] Key 

is stuck.

CNFG MODULE

 – PFD1 configuration 

module is inoperative.

The PFD1 configuration module backup memory has failed.  The G1000 system 
should be serviced.

PFD1 VOLTAGE

 – PFD1 has low 

voltage.  Reducing power usage.

The PFD1 voltage is low.  The G1000 system should be serviced.

PFD2 VOLTAGE

 – PFD2 has low 

voltage.  Reducing power usage.

The PFD2 voltage is low.  The G1000 system should be serviced.

MFD1 VOLTAGE

 – MFD1 has low 

voltage.  Reducing power usage.

The MFD voltage is low.  The G1000 system should be serviced.

DATABASE MESSAGE ADVISORIES

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.

PFD2 DB ERR

 – PFD2 aviation 

database error exists.

MFD1 DB ERR

 – MFD1 basemap 

database error exists.

The MFD and/or PFD detected a failure in the basemap database.  The G1000 
system should be serviced.

PFD1 DB ERR

 – PFD1 basemap 

database error exists.

PFD2 DB ERR

 – PFD2 basemap 

database error exists.

Summary of Contents for G1000:Beechcraft Baron 58/G58

Page 1: ...Hawker Beechcraft C90A GT...

Page 2: ...of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permis...

Page 3: ...TY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE STATUTORY OR OTHERWISE THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE IN NO EVENT...

Page 4: ...e used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G...

Page 5: ...Airplane Flight Manual Thoroughly practice basic operation prior to actual use During ight operations carefully compare indications from the G1000 to all available navigation sources including the in...

Page 6: ...current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE Thisdevicecomplieswithpart15oftheFCCRules Operationissubjecttothefollowingtwocon...

Page 7: ...3 00 Rev A Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT v REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190 00663 00 A 9 21 07 i I 6 Initial...

Page 8: ...ions 2 29 G1000 Alerting system 2 29 Marker Beacon Annunciations 2 31 Traf c Annunciation 2 31 TAWS Annunciations Optional 2 32 Altitude Alerting 2 32 Low Altitude Annunciation 2 33 Minimum Descent Al...

Page 9: ...to Navigation 5 53 5 6 Flight Planning 5 59 Flight Plan Creation 5 60 Adding Waypoints To An Existing Flight Plan 5 63 Adding Airways to a Flight Plan 5 65 Adding Procedures To A Stored Flight Plan 5...

Page 10: ...ode FLC 7 13 Vertical Navigation Modes VPTH ALTV 7 15 Glidepath Mode GP 7 21 Glideslope Mode GS 7 22 Takeoff TO and Go Around GA Modes 7 23 7 4 Lateral Modes 7 24 Roll Hold Mode ROL 7 25 Low Bank Mode...

Page 11: ...A 1 Comparator Annunciations A 4 Reversionary Sensor Annunciations A 5 G1000 System Annunciations A 5 G1000 System Message Advisories A 8 AFCS Alerts A 20 TAWS ALERTS A 21 Other G1000 Aural Alerts A 2...

Page 12: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A x TABLE OF CONTENTS BLANK PAGE...

Page 13: ...y MFD GIA 63W Integrated Avionics Unit GDC 74B Air Data Computer ADC GEA 71 Engine Airframe Unit GRS 77 Attitude and Heading Reference System AHRS GMU 44 Magnetometer GMA 1347D Dual Audio System with...

Page 14: ...e MFD and with the on side GIA 63W Integrated Avionics Unit through a High Speed Data Bus HSDB connection GDU 1500 1 Features a 15 inch LCD with 1024 x 768 resolution and is con gured as an MFD This u...

Page 15: ...s from the engine and airframe sensors This unit communicates with both GIA 63Ws using an RS 485 digital interface GRS 77 2 Provides aircraft attitude and heading information via ARINC 429 to both the...

Page 16: ...at provide Modes A C and S capability Both transponders can be controlled from either PFD and only one transponder can be active at a time Each transponder communicates with the on side GIA 63W throug...

Page 17: ...erface allowing communication with both PFDs GTP 59 2 Provides Outside Air Temperature OAT data to the on side GDC 74B GSA 80 3 GSA 81 1 and GSM 85A 4 The GSA 80 servos are used for the automatic cont...

Page 18: ...SA 81 Pitch Trim GRS 77 1 GIA 63W 1 GMC 710 GMU 44 1 GEA 71 2 GEA 71 1 GDC 74B 1 GTP 59 1 GMA 1347D 2 GMA 1347D 1 GTX 33 GTX 33 GCU 475 GWX 68 GDL 69A GRS 77 2 GMU 44 2 GDC 74B 2 GTP 59 2 VHF COM VHF...

Page 19: ...ntrols GMC 710 are described in the CNS Audio Panel and AFCS sections respectively The G1000 system controls are located on the PFD and MFD bezels MFD Control Unit AFCS Control Unit and audio panel Th...

Page 20: ...cy eld as a percentage Press to turn the COM automatic squelch ON and OFF 9 Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination the...

Page 21: ...in the applicable window by turning the small and large knobs In this case the large knob moves the cursor on the page while the small knob selects individual characters for the highlighted cursor lo...

Page 22: ...alidates or con rms a menu selection or data entry 12 CLR Key Erases information cancels entries or removes page menus Pressing and holding this key displays the Navigation Map Page automatically 13 S...

Page 23: ...mode reference for the Pitch Vertical Speed and Flight Level Change modes 12 VNV Key Selects deselects Vertical Navigation mode 13 ALT SEL Knob Sets the selected altitude in the Selected Altitude Box...

Page 24: ...eceive is simultaneously selected when this key is pressed allowing received audio from the 1 COM receiver to be heard COM2 receiver audio can be added by pressing the COM2 Key 2 COM1 When selected au...

Page 25: ...io on or off 14 NAV1 When selected audio from the 1 NAV receiver can be heard 15 ADF Pressing turns on or off the audio from the optional ADF receiver 16 NAV2 When selected audio from the 2 NAV receiv...

Page 26: ...wo SD card slots SD cards are used for aviation database and system software updates as well as terrain database storage Install an SD card Insert the SD card in the SD card slot pushing the card in u...

Page 27: ...the control units and the display bezels On the PFD the AHRS begins to initialize and displays AHRS ALIGN Keep Wings Level The AHRS should display valid attitude and heading elds typically within one...

Page 28: ...rs control for COM and NAV frequency selection MFD In normal mode the right portion of the MFD displays a full color moving map with navigation information while the left portion of the MFD is dedicat...

Page 29: ...e in reversionary mode as follows PFD1 By pressing the DISPLAY BACKUP button on the left audio panel MFD By pressing the DISPLAY BACKUP button on the left or the right audio panel PFD2 By pressing the...

Page 30: ...ble u n a v a i l a b l e available unavailable unavailable available Air Data Magnetometer Data unavailable available GPS Data Magnetometer Data Air Data Figure 1 13 AHRS Operation GPS INPUT FAILURE...

Page 31: ...iption of all annunciations and alerts refer to Appendix A Refer to the AFM POH for additional information regarding pilot responses to these annunciations When an LRU or an LRU function fails a large...

Page 32: ...nd automatically switch back to white text on black background when selected If messages remain after acknowledgement the ALERTS Softkey is black on white The PFD softkeys provide control over ight ma...

Page 33: ...e information and ADF frequency HSI FRMT Displays the softkeys for selecting the two HSI formats 360 HSI Displays HSI as a 360 compass rose ARC HSI Displays HSI as a 140 viewable arc BRG2 Cycles the B...

Page 34: ...cally enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time IDENT Activates the Spec...

Page 35: ...elect the BACK Softkey to return to the top level softkeys BACK ADC2 ADC1 AHRS1 AHRS2 ALERTS ALERTS optional Figure 1 19 PFD Con guration Softkeys Select the BACK Softkey to return to the top level so...

Page 36: ...on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are di...

Page 37: ...oupled to both PFDs BOTH ON GPS 1 or BOTH ON GPS 2 is displayed in the Reversionary Sensor Window see Appendix A indicating which GPS receiver is being used Both GPS receivers are still functioning pr...

Page 38: ...r SBAS Selected Satellite Signal Strength Bars Satellite Constellation Diagram Satellite Signal Information Status RAIM Availability Prediction GPS Receiver Status SBAS Selected RAIM Softkey Selected...

Page 39: ...dicated as the solution until a suf cient number of satellites have been acquired for computing a solution When the receiver is in the process of acquiring a 3D differential GPS solution 3D NAV is ind...

Page 40: ...ENT Key to accept the waypoint entry 6 Use the FMS Knob to enter an arrival time and press the ENT Key 7 Use the FMS Knob to enter an arrival date and press the ENT Key 8 With the cursor highlighting...

Page 41: ...er 01 32 or 120 138 for WAAS below each bar The progress of satellite acquisition is shown in three stages as indicated by signal bar appearance No bar Receiver is looking for the indicated satellite...

Page 42: ...the FMS Knob also removes the displayed menu Figure 1 23 Page Menu Examples No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed MFD PAGE GROUPS NOTE Refer to the GPS Na...

Page 43: ...roup is selected 2 Turn the small FMS Knob until the desired page is selected There are also several pages Airport Information and XM Information pages which are selected rst from within a main page g...

Page 44: ...ey Departure Information DP Softkey Arrival Information STAR Softkey Approach Information APR Softkey Weather Information WX Softkey Intersection Information NDB Information VOR Information User Waypo...

Page 45: ...sed exclusively using the FMS Knobs there are pages for ight planning FPL and loading procedures PROC which are accessed by a dedicated key In some instances softkeys may be used to access the Procedu...

Page 46: ...ains the same MFD SYSTEM PAGES In the Auxiliary AUX Page Group there are two system pages System Setup page 5 of 7 and System Status page 7 of 7 The System Setup Page allows management of various syst...

Page 47: ...or the Hawker Beechcraft C90A GT 1 35 SYSTEM OVERVIEW Restoring system setup defaults 1 Select the AUX System Setup Page 2 Press the DFLTS Softkey or press the MENU Key highlight Restore Defaults and...

Page 48: ...l 24 hr or UTC Local time is set by adding subtracting an offset hours minutes to from UTC Figure 1 33 System Time Local 24 hr Format Con guring the system time 1 Select the AUX System Setup Page 2 Pr...

Page 49: ...d Figure 1 35 Display Unit Settings System Setup Page Creating a pro le 1 Select the AUX System Setup Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to h...

Page 50: ...ng a pro le 1 Select the AUX System Setup Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight RENAME in the Pilot Pro le Box 4 Press the ENT Key...

Page 51: ...ector Map range Traf c Page Terrain Proximity TAWS Page CDI scaling System Setup Fuel range calculation EIS Altitude and Vertical Speed Feet All altitudes on MFD All elevations on MFD Altimeter Vertic...

Page 52: ...ily to activate the ashing cursor 3 Turn the large FMS Knob to select the ON OFF eld in the Arrival Alert Box 4 Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to t...

Page 53: ...ctive LRUs are indicated by green check marks and failed LRUs are indicated by red X s Failed LRUs should be noted and a service center or Garmin dealer informed Figure 1 37 Example System Status Page...

Page 54: ...set Refer to the Additional Features section for a dicussion on the Scheduler feature Figure 1 38 Utility Page TIMERS The G1000 timers available include Stopwatch like generic timers available from th...

Page 55: ...and the digits are reset 9 To remove the window press the CLR Key or the TMR REF Softkey Figure 1 39 Generic Timer PFD Timer References Window Setting the generic timer MFD AUX Utility Page 1 Use the...

Page 56: ...ey Resetting the ight timer 1 Use the FMS Knob to select the AUX Utility Page 2 Press the MENU Key 3 With Reset Flight Timer highlighted press the ENT Key The G1000 records the time at which departure...

Page 57: ...dspeed Maximum groundspeed for the period of time since the last reset is also displayed Resetting trip statistics readouts 1 Use the FMS Knob to select the AUX Utility Page 2 Press the MENU Key The f...

Page 58: ...duler Utility Page Entering a scheduler message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the rst empty schedu...

Page 59: ...lity Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the name eld of the scheduler message to be deleted 4 Press the CLR Key to clear the mes...

Page 60: ...b to select AUTO next to MFD DSPL or PFD2 DSPL 2 Turn the small FMS Knob to select MANUAL and press the ENT Key The intensity value is now highlighted 3 Use the FMS Knob to enter the desired backlight...

Page 61: ...al speed and course deviation information In addition to the ight instruments navigation communication terrain traf c and weather information are also presented on the PFD and explained in other secti...

Page 62: ...ading 6 Horizontal Situation Indicator HSI 7 Outside Air Temperature OAT 8 Softkeys 9 System Time 10 Transponder Data Box 11 Selected Heading Bug 12 Turn Rate Indicator 13 Altimeter Barometric Setting...

Page 63: ...cted Heading 3 Wind Data 4 Inset Map 5 DME Information Window optional 6 Bearing Information Windows 7 Minimum Descent Altitude Decision Height 8 Flight Plan Window 9 Selected Course 10 Vertical Speed...

Page 64: ...it turns red Figure 2 4 Red Pointer Showing Airspeed Above VMO Figure 2 3 Airspeed Indicator Actual Airspeed Airspeed Trend Vector True Airspeed Color coded Speed Tape Vspeed References VMCA Red Line...

Page 65: ...eoff or landing Takeoff Vspeed ags are automatically turned off when airspeed reaches 160 knots The order in which the categories are displayed is determined by whether the aircraft is on the ground o...

Page 66: ...he large FMS Knob to highlight the ON OFF eld 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey Figure 2 7 Takeoff an...

Page 67: ...pearance based on selection of AFCS ight director Command Bar format see the AFCS Section for details Both PFDs show the same Command Bar format and Aircraft Symbol Command Bar format may only be chan...

Page 68: ...inor pitch marks occur every 2 5 The inverted white triangle indicates zero on the roll scale Major tick marks at 30 and 60 and minor tick marks at 10 20 and 45 are shown to the left and right of the...

Page 69: ...d Altitude Setting the Selected Altitude Turn the ALT SEL Knob to set the SelectedAltitude in 100 ft increments if baro min reference is set the selected altitude can be set in 10 feet increments to m...

Page 70: ...ents it may take several minutes for the aircraft to re establish on the descent path If the change is made while nearing a waypoint with a VNV Target Altitude the aircraft may not re establish on the...

Page 71: ...System Setup Page Barometric Pressure Synchronization VERTICAL SPEED INDICATOR VSI The Vertical Speed Indicator VSI displays the aircraft vertical speed using a non moving tape labeled at 2000 and 40...

Page 72: ...LS frequency is tuned in the active NAV eld and the heading is less than 105 from the inbound course A green diamond acts as the Glideslope Indicator like a glideslope needle on a conventional indicat...

Page 73: ...SI display format 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI or ARC HSI Softkey The 360 HSI contains a Course Deviation Indicator CDI with a Course Pointer To From Indica...

Page 74: ...er being adjusted The light blue bug on the compass rose corresponds to the Selected Heading While the HSI is displayed as an arc if the Selected Heading Bug is adjusted off the shown portion of the c...

Page 75: ...e navigation angle setting to True at the appropriate time Figure 2 22 Heading and Course Indications True Changing the navigation angle setting 1 Use the FMS Knob to select the AUX System Setup Page...

Page 76: ...te Arrow Shown for Turn Rate 4 Degrees per Second Figure 2 24 Turn Rate Indicator and Trend Vector BEARING POINTERS AND INFORMATION WINDOWS NOTE When the Arc HSI is displayed the Bearing Information w...

Page 77: ...O DATA is displayed in the information window if The NAV radio is not receiving the tuned VOR station GPS is the bearing source and an active waypoint is not selected Selecting bearing display and cha...

Page 78: ...ed Figure 2 26 Course Deviation Indicator 360 HSI Scale Crosstrack Error Flight Phase CDI Navigation Source Arc HSI CDI Navigation Source CDI Scale Flight Phase Crosstrack Error The CDI can display tw...

Page 79: ...NAV1 standby frequency in the upper left corner of the PFD 2 Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequ...

Page 80: ...p Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the CDI Sync in the Synchronization box 4 Turn the small FMS Knob clockwise to ON or counterclockwi...

Page 81: ...is annunciated in magenta beneath the aircraft symbol The current GPS CDI scale setting is displayed as System CDI on the AUX System Setup Page and the full scale de ection setting may also be change...

Page 82: ...om the departure airport or the leg after the last departure waypoint has been activated or a direct to waypoint is activated If after completing the departure procedure the nearest airport is more th...

Page 83: ...system automatically switches back to terminal scaling under the following conditions The next leg in the missed approach procedure is not aligned with the nal approach path The next leg in the misse...

Page 84: ...o the lower right of the aircraft symbol when OBS Mode is selected see Figure 2 34 While OBS Mode is enabled a course line is drawn through the active to waypoint on the moving map If desired the cour...

Page 85: ...synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to return to automatic waypoint sequencing As the aircraft crosses the missed approach point in ap...

Page 86: ...ata display In addition to the ight instruments the PFD also displays various supplemental information including temperatures wind data and Vertical Navigation VNV indications TEMPERATURE DISPLAYS The...

Page 87: ...shows NO WIND DATA Wind data can be displayed in three different ways Figure 2 37 Wind Data No Data Option 2 Option 1 Option 3 Displaying wind data 1 Press the PFD Softkey 2 Press the WIND Softkey to...

Page 88: ...is Selected Navigation Source Enroute Phase of Flight Criteria VNV Indication Removed Required Vertical Speed RVSI Vertical Deviation VDI VNV Target Altitude Aircraft 1 min before the next TOD and not...

Page 89: ...y open when a new message is generated selecting the ALERTS Softkey to acknowledge the message causes it to turn gray The Annunciation Window appears to the right of the Vertical Speed Indicator and d...

Page 90: ...ce of a message advisory The ashing ADVISORY Softkey annunciation continues to ash until acknowledged by pressing the ADVISORY Softkey Figure 2 40 Softkey Annunciation ALERTS Softkey Labels Critical v...

Page 91: ...MFD and various other MFD page maps Refer to the Hazard Avoidance Section and Appendix E for more details about the Traf c Information Service TIS and optional Traf c Advisory Systems TAS When a traf...

Page 92: ...Alerter is independent of the GFC 700 AFCS but alerting tones are generated only when the GFC 700 is installed The following occur when approaching the Selected Altitude Upon passing through 1000 fee...

Page 93: ...CISION HEIGHT ALERTING For altitude awareness a barometric Minimum Descent Altitude MDA or Decision Height DH can be set in the Timer References Window and is reset when the power is cycled When activ...

Page 94: ...rn the large FMS Knob to highlight the next eld 4 Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet 5 To remove the window press the CLR Key or the TMR REF Softkey Barometr...

Page 95: ...e GPS position errors INTEG OK Lower left of aircraft symbol Integrity OK GPS integrity has been restored to within normal limits annunciation displayed for 5 seconds DR Upper right of aircraft symbol...

Page 96: ...in on the display and the Bearing Information Alerts and Annunciation windows can be displayed during such situations The following information is removed from the PFD and corresponding softkeys are d...

Page 97: ...outs Green ranges on the instrument scales indicate normal ranges of operation yellow and red bands indicate caution and warning respectively White or uncolored bands indicate areas outside of normal...

Page 98: ...transitioning to an arrowhead The arrowhead points towards the propeller turning at a higher speed 5 Turbine Speed RPM Displays turbine speed in a percentage of the revolutions per minute rpm 6 Fuel...

Page 99: ...190 00663 00 Rev A Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 3 3 ENGINE INDICATION SYSTEM Figure 3 2 EIS Display C90A GT Baseline Con guration 8 5 4 3 2 1 6 7...

Page 100: ...start and running conditions Values between 200 and 1200 degrees Celsius C are shown at engine start values change to 200 to 800 C once the engine has stabilized A red triangle is displayed at 1090 C...

Page 101: ...tick mark The Tachometer is equipped with a propeller sync indicator which points towards the higher speed propeller The indicator changes linearly with RPM difference between the left and right prope...

Page 102: ...Speed Gauge is located beneath the Tachometer Turbine speed is indicated as a percentage of the maximum operating speed rpm from 0 to 110 Figure 3 8 Turbine Speed Gauge FUEL FLOW The Fuel Flow Gauge i...

Page 103: ...s per square inch psi from 0 to 200 psi Safe operating pressure is more than 80 psi and less than 100 psi A red triangle represents the maximum oil pressure 200 psi Figure 3 10 Oil Pressure Gauge OIL...

Page 104: ...htforward for the pilot for ight parameters are presented in the same format as in normal mode refer to the System Overview for information about display Reversionary Mode Figure 3 12 Reversionary Mod...

Page 105: ...ave a different shape and share one title i e ITT FFLOW for each pair of gauges NOTE The gauges displayed and the values shown in this section are taken from the Hawker Beechcraft C90A GT baseline con...

Page 106: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 3 10 ENGINE INDICATION SYSTEM BLANK PAGE...

Page 107: ...n no audio is detected MASQ processing further reduces the amount of background noise from the radios The Mode S Transponders are controlled with softkeys and the FMS Knob located on the Primary Fligh...

Page 108: ...Garmin G1000 Pilot s Guide for the Beechcraft C90A GT 4 2 AUDIO PANEL AND CNS PFD CONTROLS AND FREQUENCY DISPLAY Figure 4 1 PFD Controls NAV COM Frequency Tuning Boxes and DME Tuning Window 12 2 1 6...

Page 109: ...small knob for kHz Press to move the tuning box light blue box and Frequency Transfer Arrow between COM1 and COM2 7 COM Frequency Transfer Key Transfers the standby and active COM frequencies Press a...

Page 110: ...s simultaneously selected when this key is pressed allowing received audio from the 1 COM receiver to be heard COM2 receive can be added by pressing the COM2 Key 2 COM1 When selected audio from the 1...

Page 111: ...n selected audio from the 2 NAV receiver can be heard 17 AUX Not used in Beechcraft C90A GT aircraft 18 REC Press to enable the recording of up to 2 5 minutes of COM receiver audio When no audio is be...

Page 112: ...r is selected for transmitting by pressing the COM MIC Keys on the Audio Panel During reception of audio from the COM radio selected for transmission audio from the other COM radio is muted An active...

Page 113: ...elected on both Audio Panels the pilot has transmit priority on COM1 the copilot has transmit priority on COM2 COM TRANSCEIVER MANUAL TUNING The COM frequency controls and frequency boxes are on the r...

Page 114: ...Boxes Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other QUICK TUNING AND ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Transfer Key for two seconds automatica...

Page 115: ...ncy is entered it becomes a standby frequency Pressing the Frequency Transfer Key places this frequency into the COM Active Frequency Field Auto tuning a COM frequency for a nearby airport from the PF...

Page 116: ...uency can be auto tuned activate the cursor by pressing the FMS Knob on the MFD control unit or selecting the appropriate softkey 2 Turn the FMS Knob to place the cursor on the desired COM frequency F...

Page 117: ...menu options 3 Press the ENT Key to place the cursor on the desired selection 4 Scroll through the frequency selections with the FMS Knob or the ENT Key 5 Press the ENT Key to load the COM frequency i...

Page 118: ...ing the FMS Knob and scrolling through the list The frequency is transferred to the COM Standby Field with the ENT Key Press ENT Key to load frequency into PFD1 COM Standby Field Cursor then advances...

Page 119: ...ies can also be auto tuned from the NRST Nearest Airspaces NRST Nearest Frequencies and NRST Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key the FMS Kn...

Page 120: ...the System Setup Page of the AUX Page Group Figure 4 13 COM Channel Spacing 25 kHz Channel Spacing 8 33 kHz Channel Spacing Changing COM frequency channel spacing 1 Select the AUX System Setup Page 2...

Page 121: ...Knob again enables Automatic Squelch When Automatic Squelch is disabled a white SQ appears next to the COM frequency Figure 4 15 Overriding Automatic Squelch Squelch Indication Press the COM VOL SQ K...

Page 122: ...and the Frequency Transfer Arrow are placed in the active NAV Frequency Field and the active NAV frequency color changes to green The three navigation modes that can be cycled through are VOR1 or LOC1...

Page 123: ...The NAV frequency controls and frequency boxes are on the left side of the PFDs Manually tuning a NAV frequency 1 Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box 2 Press the Fre...

Page 124: ...the NAV1 or NAV2 Key on the Audio Panel Pressing the VOL ID Knob turns off the Morse code audio only in the radio with the NAV Tuning Box To turn off both NAV IDs transfer the NAV Tuning Box between...

Page 125: ...Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key Figures 4 23 4 24 and 4 25 Auto tuning a NAV frequency from the WPT and NRST Pages 1 From any page...

Page 126: ...roll through the menu options 3 Press the ENT Key to place the cursor in the desired window 4 Scroll through the frequency selections with the FMS Knob or the ENT Key 5 Press the ENT Key to load the N...

Page 127: ...is used to scroll through the list The cursor is placed on the frequency with the FREQ Softkey and loaded into the NAV Tuning Box with the ENT Key Select the FREQ Softkey to Place the Cursor on the VO...

Page 128: ...e auto tuned from the NRST Nearest Airports WPT Airport Information WPT VOR Information and NRST Nearest Frequencies Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key the...

Page 129: ...vation on both PFD1 and PFD2 When loading or activating a VOR or ILS LOC approach the approach frequency is automatically transferred to a NAV frequency eld as follows If the current CDI navigation so...

Page 130: ...On Muted and Deselected Pressing the MKR MUTE Key selects and deselects marker beacon audio The key annunciator indicates when marker beacon audio is selected During marker beacon audio reception pres...

Page 131: ...ME Tuning Window Pressing the DME Softkey switches the DME Tuning Window on and off Figure 4 29 DME Tuning Window DME Modes The following DME transceiver pairing can be selected NAV1 Pairs the DME fre...

Page 132: ...lective interrogation The Hazard Avoidance Section provides more details on traf c avoidance systems TRANSPONDER CONTROLS Transponder function is displayed on three levels of softkeys on the PFD Top l...

Page 133: ...activate the other transponder When turning on the G1000 for use the system activates Transponder 1 as the default unit regardless of which transponder was active prior to shutdown When switching betw...

Page 134: ...an be returned to Ground Mode by selecting the GND Softkey GND Mode Figure 4 31 Ground Mode STANDBY MODE MANUAL NOTE In Standby Mode the IDENT function is inhibited Standby Mode can be selected at any...

Page 135: ...Mode is selected a green ALT indication and transponder code appear in the mode eld of the Transponder Data Box and all transponder replies requesting altitude information are provided with pressure a...

Page 136: ...entered the transponder code becomes active Entering a Code Figure 4 36 Entering a Code Entering a transponder code with the PFD FMS Knob 1 Select the XPDR and the CODE Softkeys as in the previous pro...

Page 137: ...enter for con guration Figure 4 38 VFR Code VFR Code IDENT FUNCTION NOTE In Standby Mode the IDENT Softkey is inoperative Selecting the IDENT Softkey sends an ID indication to Air Traf c Control ATC T...

Page 138: ...nly the left channel in both ears If a monaural headset is used at one of the passenger positions any other passenger using a stereo headset hears audio in the left ear only SPEAKER NOTE When the oxyg...

Page 139: ...ual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob toggles between volume and squelch adjustment lighting the associated annunciator beneath...

Page 140: ...eadphones When PA is selected on the Audio Panel the annunciator ashes about once per second while pressing the PTT the COM MIC annunciator is no longer lit and the active COM frequency for that Audio...

Page 141: ...corded The PLAY Key controls the play function The PLAY annunciator indicates when play is in progress The PLAY annunciator turns off after playback is nished Pressing the PLAY Key once plays the late...

Page 142: ...induced issues These pre ight procedures should be performed each time a ight crew boards the aircraft to insure awareness of all audio levels in the Audio Panels and radios Figure 4 44 Audio Panel C...

Page 143: ...me least amount of attenuation 4 Adjust radio volume levels COM NAV etc to a suitable level 5 Adjust the ICS volume Knob on each Audio Panel to the desired intercom level Once this procedure has been...

Page 144: ...s stuck the COM transmitter stops transmitting after 35 seconds of continuous operation An alert appears on the PFD to advise the crew of a stuck microphone The COM1 MIC or COM2 MIC Key Annunciator on...

Page 145: ...requency is not shown The COM1 emergency frequency is available to both the copilot and pilot Figure 4 54 Frequency Section of MFD Display after PFD1 Failure Emergency Channel Loaded Automatically If...

Page 146: ...ctly to the COM2 transceiver Audio is not available on the speakers If there is a failure of one Audio Panel the remaining one does not have access to the others side s COM and NAV For example if the...

Page 147: ...ing the OFF Softkey removes the Inset Map The Navigation Map displays aviation data e g airports VORs airways airspaces geographic data e g cities lake highways borders topographic data map shading in...

Page 148: ...t Plan Window Procedures Window Nearest Airports Window Inset Map Navigation Status Box Navigation Mode Figure 5 2 GPS Navigation Information on the MFD Navigation Page Active Flight Plan Leg Navigati...

Page 149: ...eft DME Arc The Navigation Status Box located at the top of the MFD contains four data elds each displaying one of the following items Bearing BRG Distance DIS Desired Track DTK Enroute Safe Altitude...

Page 150: ...Map range Wind direction and speed Map orientation Icons for enabled map features Aircraft icon representing present position Nav range ring Flight plan legs User waypoints Track vector Topography sc...

Page 151: ...ewing active ight plan legs in a non North Up orientation the map does not show the map orientation nor the wind direction and speed NOTE Map orientation can only be changed on the Navigation Map Page...

Page 152: ...e MAP RANGE There are 28 different map ranges available from 500 feet to 2000 nm The current range is indicated in the lower right corner of the map and represents the top to bottom distance covered b...

Page 153: ...the Map Group These settings determines the minimum and maximum distance to display based upon the aircraft s ground speed Waypoints that are long distances apart cause the map range to increase to a...

Page 154: ...Page displayed The cursor ashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed 3 Select the Map group 4 Press the ENT Key 5 Highlight the AUTO ZOOM eld 6 Select Off MFD On...

Page 155: ...s selected by pressing the Joystick the Map Pointer ashes on the map display A window also appears at the top of the map display showing the latitude longitude position of the pointer the bearing and...

Page 156: ...placed on an object the name of the object is highlighted even if the name was not originally displayed on the map When any map feature or object is selected on the map display pertinent information...

Page 157: ...formation includes the name and class of airspace the ceiling in feet above Mean Sea Level MSL and the oor in feet MSL Figure 5 10 Navigation Map Map Pointer on Airspace Map Pointer on Airspace Inform...

Page 158: ...Place the Map Pointer on a waypoint 2 Press the ENT Key to display the Waypoint Information Page for the selected waypoint 3 Press the GO BACK Softkey the CLR Key or the ENT Key to exit the Waypoint I...

Page 159: ...er on an open area within the boundaries of an airspace 2 Press the ENT Key to display an options menu 3 Review Airspace should already be highlighted if not select it Press the ENT Key to display the...

Page 160: ...the navigation map Measuring bearing and distance between any two points 1 Press the MENU Key with the Navigation Map Page displayed 2 Highlight the Measure Bearing Distance eld 3 Press the ENT Key A...

Page 161: ...ving topographic data on all pages displaying navigation maps 1 Press the MAP Softkey the INSET Softkey for the PFD Inset Map 2 Press the TOPO Softkey 3 Press the TOPO Softkey again to remove topograp...

Page 162: ...et Map removes the same item at 50 nm Selecting a topographical data range TOPO DATA 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option 2 Press the EN...

Page 163: ...er is displayed Range of Displayed Elevations Displaying removing the topographic scale TOPO SCALE 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option...

Page 164: ...llowing items are con gured on the land menu Land Symbols Text label size can be None Small Medium Med or Large Lrg Symbol Default Range nm Maximum Range nm Latitude Longitude LAT LON Off 2000 Highway...

Page 165: ...ports NAVAIDs 2000 2000 Large Airports LARGE APT 250 500 Medium Airports MEDIUM APT 150 300 Small Airports SMALL APT 50 100 Taxiways SAFETAXI See Section 8 3 20 Runway Extension RWY EXTENSION N A Off...

Page 166: ...f 5 Press the FMS Knob to return to the Navigation Map Page Figure 5 18 Navigation Map Setup Menu TOPO SCALE Setup LAND DATA On Off The label size TEXT sets the size at which labels appear on the disp...

Page 167: ...ge Text Label Size Off Small Med or Lrg Figure 5 20 Navigation Map Setup Menu AVIATION GROUP Setup Maximum Display Range Text Label Size Off Small Med or Lrg NOTE Since the PFD Inset Map is much small...

Page 168: ...Declutter Level Navigation Map Page Menu DCLTR Softkey Decluttering the map Select the DCLTR Softkey with the Navigation Map Page displayed The current declutter level is shown With each softkey selec...

Page 169: ...X X International Borders X X X X Track Vector X X X X Navigation Range Ring X X X X Fuel Range Ring X X X X Terrain Data X X X X Traf c X X X X NEXRAD X X X XM Lightning Data X X X Airports X X X Run...

Page 170: ...or Airways since they run primarily between VORs High Altitude Airways or Jet Routes primarily serve airliners jets turboprops and turbocharged piston aircraft operating above 18 000 feet MSL Jet Rout...

Page 171: ...2 Press the ENT Key The Map Setup Menu is displayed 3 Turn the small FMS Knob to select the Airways group and press the ENT Key 4 Turn the large FMS Knob to highlight the AIRWAYS eld 5 Turn the FMS Kn...

Page 172: ...ircraft track The track vector look ahead time is selectable 30 sec 60 sec default 2 min 5 min 10 min 20 min and determines the length of the track vector The arrowhead is continuously pointing to the...

Page 173: ...d as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than or equal to 1 kt Figure 5 26 Navigation Map Wind Vector Wind Direction Wind Speed NOTE The wind ve...

Page 174: ...OTE The Nav Range Ring is not displayed on the Waypoint Information pages Nearest pages or Direct to Window map Displaying removing the Nav Range Ring 1 Press the MENU Key with the Navigation Map Page...

Page 175: ...Ring Displaying removing the fuel range ring and selecting a fuel range time 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option 2 Press the ENT Key T...

Page 176: ...view section for detailed instructions on entering data in the G1000 As a waypoint identi er facility name or location is entered the G1000 s Spell N Find feature scrolls through the database displayi...

Page 177: ...uencies COM NAV and lighting review runways and review instrument procedures that may be involved in the ight plan See the Audio Panel and CNS Section for more information on loading frequencies auto...

Page 178: ...vel Dirt Soft Unknown or Water Runway lighting type No Lights Part Time Full Time Unknown or PCL Freq for pilot controlled lighting COM Availability TX transmit only RX receive only PT part time i add...

Page 179: ...ach can be loaded using the softkeys on the Airport Information Page See the procedures section for details METARs or TAFs applicable to the selected airport can be selected for display see the Hazard...

Page 180: ...on the MFD is rst in the group of NRST pages because of its potential use in the event of an in ight emergency In addition to displaying a map of the currently selected airport and surrounding area th...

Page 181: ...BACK or press the CLR Key The cursor is now on the next airport in the nearest airports list Repeatedly pressing the ENT Key moves through the airport list alternating between the Nearest Airports Win...

Page 182: ...s that are not appropriately surfaced from being displayed Default settings are 0 feet or meters for runway length and ANY for runway surface type Selecting nearest airport surface matching criteria 1...

Page 183: ...ree boxes labeled INTERSECTION INFORMATION and NEAREST VOR Figure 5 36 Intersection Information Page Selected Intersection Navigation Map Showing Selected Intersection Intersection Identi er Nearest V...

Page 184: ...ed intersection is indicated by a white arrow Up to seventeen intersections are visible at a time If there are more than can be shown the list can be scrolled If there are no items for display text in...

Page 185: ...Bearing Distance to Airport NDB Information Type Region Lat Long NDB Frequency NOTE Compass locator LOM a low power low or medium frequency radio beacon installed in conjunction with the instrument la...

Page 186: ...enti er indicates the selected NDB Up to seventeen NDBs are visible at a time If there are more than can be shown each list can be scrolled The list only includes waypoints that are within 200nm If th...

Page 187: ...xes labeled VOR INFORMATION FREQUENCY and NEAREST AIRPORT Figure 5 40 VOR Information Page Selected VOR Navigation Map Showing Selected VOR VOR Identi er Type Facility Name Nearest City Nearest Airpor...

Page 188: ...in three boxes labeled NEAREST VOR INFORMATION and FREQUENCY The list only includes waypoints that are within 200 nm A white arrow before the VOR identi er indicates the selected VOR Up to seventeen...

Page 189: ...the map using the Joystick or from the User Waypoint Information Page by referencing a bearing distance from an existing waypoint or bearing from two existing waypoints Once a waypoint has been create...

Page 190: ...racters 3 Press the ENT Key The current aircraft position is the default location of the new waypoint 4 If desired highlight the Information Box and enter the latitude and longitude for the waypoint o...

Page 191: ...ce between Review Airspaces or Create User Waypoint or 3 a new waypoint is initiated with the default name being the selected map item 3 Enter a user waypoint name up to six characters 4 Press the ENT...

Page 192: ...1 Enter a waypoint name or select the waypoint in the User Waypoint List then press the ENT Key 2 Press the MENU Key 3 Select Use Present Position 4 Press the ENT Key twice The new waypoint s locatio...

Page 193: ...ress the ENT Key 4 Press the FMS Knob to remove the ashing cursor Or 1 Highlight a User Waypoint in the User Waypoint List or enter a waypoint in the User Waypoint eld 2 Press the MENU Key 3 Select De...

Page 194: ...0 can display the following types of airspaces Class B TMA Class C TCA Class D Restricted MOA Military Other Airspace Air Defense Interdiction Zone ADIZ and Temporary Flight Restriction TFR Figure 5 4...

Page 195: ...eet and the aircraft is more than 500 feet above below an airspace an alert message is not generated but if the aircraft is less than 500 feet above below an airspace and projected to enter it the pil...

Page 196: ...Airspace Alerts DFLTS Softkey Airspace Alerts Box Airspace Altitude Buffer Alert On Off Default Settings Shown Map ranges for the airspace boundaries are selected from the Aviation Group in the Map S...

Page 197: ...ercept only if Ahead or Ahead 2nm Airspace Vertical Limits Ceiling Floor Airspace Agency Info Airspace Type Controlling Agency Softkeys Airspace 1 Associated Frequencies Type Availability Info Frequen...

Page 198: ...ents INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft penetrates the airspace wit...

Page 199: ...d with a new direct to or ight plan or cancelled A vertical navigation VNV direct to creates a descent path and provides guidance to stay on the path from the current altitude to a selected altitude a...

Page 200: ...press the CLR Key to remove it or turn the large FMS Knob to select the facility name or city eld and turn the small FMS Knob to begin entering a facility name or city If duplicate entries exist for...

Page 201: ...s the FPL list is populated only when navigating a ight plan 3 Turn the small FMS Knob clockwise to display the NRST or RECENT waypoints 4 Turn the large FMS Knob clockwise to select the desired waypo...

Page 202: ...splay the pointer 2 Move the Joystick to place the pointer at the desired destination location 3 If the pointer is placed on an existing airport NAVAID or user waypoint the waypoint name is highlighte...

Page 203: ...on the path from the aircraft s current altitude to the altitude of the direct to waypoint The altitude is reached at the waypoint or at the speci ed distance along the ight path if an offset distance...

Page 204: ...NAGEMENT Removing a VNV altitude constraint 1 Press the Direct to Key to display the Direct to Window 2 Press the MENU Key 3 With Clear Vertical Constraints highlighted press the ENT Key Figure 5 52 D...

Page 205: ...departure or arrival the G1000 uses the waypoint information from the current database to de ne the waypoints If the database is changed or updated the G1000 automatically updates the information if...

Page 206: ...AN CREATION There are three methods to create or modify a ight plan Active Flight Plan Page on the MFD create modify the active ight plan Active Flight Plan Window on the PFD create modify the active...

Page 207: ...Waypoint Destination Waypoint Total Flight Plan Distance Enroute Safe Altitude Catalog Contents Used Empty Softkeys Selected Flight Plan Map The active ight plan is listed on the active Flight Plan Pa...

Page 208: ...cursor Creating a stored ight plan 1 Press the FPL Key 2 Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Select the NEW Softkey or press the MENU Key highlight Create New...

Page 209: ...ans are limited to 99 waypoints including waypoints within airways and procedures If the number of waypoints in the ight plan exceeds 99 the message Flight plan is full Remove unnecessary waypoints ap...

Page 210: ...as duplicates a Duplicate Waypoint Window is displayed Use the FMS Knob to select the correct waypoint Figure 5 58 Duplicate Waypoints Window Adding a waypoint to the active ight plan 1 Press the FPL...

Page 211: ...hoose a ight plan add the desired airway entry point if not already in the ight plan select the waypoint after the desired airway entry point select the airway and it is added in front of the selected...

Page 212: ...cursor position 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown rst in the list followed by all altitude airways and then high altit...

Page 213: ...DEVAL Airway UR975 in North Africa has more complicated directional restrictions within the list of airway waypoints AMANO VAKOR LIBRO NELDA DIRKA GZO KOSET and SARKI Starting from AMANO the airway c...

Page 214: ...rocedures from the navigation database into a ight plan The procedures are designed to facilitate routing of traf c leaving an airport departure arriving at an airport arrival and landing at an airpor...

Page 215: ...oint Sequence Preview of Selected Departure Loading a departure procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Page 2 Select the EDIT Softkey or press the M...

Page 216: ...ure Airport Selected Departure Departure Transition Points Available Selected Runway Selected Departure End Point Preview of Selected Departure Selected Transition Figure 5 65 Stored Flight Plan Page...

Page 217: ...nt Sequence Preview of Selected Arrival Selected Runway Loading an arrival procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Page 2 Select the EDIT Softkey or...

Page 218: ...cting the Transition Destination Airport Selected Arrival Transitions Available with DBRY1 Arrival Waypoint Sequence Preview of Selected Arrival Selected Transition Figure 5 68 Stored Flight Plan Page...

Page 219: ...h Approaches Available at KCOS Approach Waypoint Sequence Preview of Selected Approach Loading an approach procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Pa...

Page 220: ...h Load Approach Selected Transition Figure 5 71 Stored Flight Plan Page Approach Inserted Inserted Approach Header Approach Identi er approach airport runway and approach type e g KCOS RNAV 35RGPS LPV...

Page 221: ...d Flight Plan 5 Press the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the ight plan 6 Press the FMS Knob to exit the Stored Flight Plan Page Figure 5 72 Stored Flight Pl...

Page 222: ...ress the MENU Key highlight Activate Flight Plan and press the ENT Key The Activate Stored Flight Plan window is displayed 4 With OK highlighted select the ENT Key To cancel the request press the CLR...

Page 223: ...ss the CLR Key or highlight CANCEL and press the ENT Key Deleting all stored ight plans 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the MENU Key 3 H...

Page 224: ...t the white header of the airway to be deleted 3 Press the CLR Key The Remove airway name window is displayed 4 With OK highlighted press the ENT Key To cancel the request press the CLR Key or highlig...

Page 225: ...dow is displayed 7 With OK highlighted press the ENT Key To cancel the request press the CLR Key or highlight CANCEL and press the ENT Key Deleting an entire procedure from a stored ight plan 1 Press...

Page 226: ...s to edit the comment 7 Press the ENT Key to accept the changes ALONG TRACK OFFSETS A waypoint having an along track offset distance from an existing waypoint can be entered into a ight plan Along tra...

Page 227: ...ss the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highli...

Page 228: ...esult of the course change NOTE Vertical navigation is unavailable while the Parallel Track feature is active Figure 5 74 Active Flight Plan Window Selecting Parallel Track Selecting Parallel Track Ac...

Page 229: ...lel Track Active Parallel Track Waypoints TIFTO p TOP p SLN p HYS p LAA p Activating Parallel Track affects the entire active ight segment e g enroute Parallel Track Original Track If the parallel tra...

Page 230: ...h Leg Active If the offset direction and distance results in an unreasonable route geometry the status indicates that the system is unable to activate the parallel track because of invalid geometry Fi...

Page 231: ...or navigation guidance Activating a ight plan leg 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not re...

Page 232: ...3 Select OK 4 Press the ENT Key to invert and activate the active ight plan To cancel press the CLR Key or highlight CANCEL and press the ENT Key Inverting and activating a stored ight plan 1 Press th...

Page 233: ...FD to display the Active Flight Plan Page 2 Press the VIEW Softkey to display the CUM and LEG LEG Softkeys 3 Press the CUM Softkey to view cumulative waypoint distance or press the LEG LEG Softkey to...

Page 234: ...ading When airways are collapsed leg to leg computed values such as DIS or ETE shown for the exit waypoint re ects the total of all the legs on the airway that have been hidden in the collapsed displa...

Page 235: ...s a reference waypoint and creates a new user waypoint along the ight plan at the location closest to a chosen reference waypoint Determining the closest point along the active ight plan to a selected...

Page 236: ...th The desired path is de ned by a line joining two waypoints with speci ed altitudes or as a vertical angle from a speci ed waypoint altitude The vertical waypoints are integrated into the active igh...

Page 237: ...a vertical navigation direct to to any waypoint in the active ight plan with an altitude constraint designated for vertical guidance Selecting the VNV Direct to Softkey on the Active Flight Plan Page...

Page 238: ...VS TGT and FPA 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Press the VNV PROF Softkey or press the MENU Key highlight SelectVNV Pro leWindow and press the ENT key The curso...

Page 239: ...played as blue text up to but not including the FAF The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case th...

Page 240: ...ccept the altitude constraint if the selected waypoint is an airport an additional choice is displayed Turn the small FMS Knob to choose MSL or AGL and press the ENT Key to accept the altitude Altitud...

Page 241: ...Revert to published VNV altitude of nnnnnFT con rmation window is displayed 4 Select REVERT and press the ENT Key The altitude is changed to the navigation database value Modifying a system calculated...

Page 242: ...intermediate waypoints in the original ight plan but keeps the procedure available on the Active Flight Plan Page for quick activation when needed Activating also adds the procedure to the end of the...

Page 243: ...C90A GT 5 97 FLIGHT MANAGEMENT Figure 5 87 Departure Selection Departure Airport Departure Preview Available Procedure Actions Departure Choices Loaded Procedures Procedure Loading Page Selection Sof...

Page 244: ...iew the available transitions Press the ENT Key to select the transition The cursor moves to the Sequence box The departure is previewed on the map 7 Select the INFO Softkey to return to the Airport I...

Page 245: ...n waypoints and a runway LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN Loading an arrival into the active ight plan using the PROC Key 1 Press the PROC Key The Procedures Window is displayed 2 Highli...

Page 246: ...cility name city and press the ENT Key 3 Press the FMS Knob then turn the large FMS Knob to highlight the Arrival The arrival is previewed on the map 4 Turn the small FMS Knob to view the available ar...

Page 247: ...instrument approach procedures Only one approach can be loaded at a time in a ight plan If an approach is loaded when another approach is already in the active ight plan the new approach replaces the...

Page 248: ...roach using published LNAV VNAV minima LPV GPS approach using published LPV minima Table 5 9 Approach Types LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN Loading an approach into the active ight pla...

Page 249: ...FLIGHT MANAGEMENT Figure 5 91 Approach Selection Destination Airport Approach Preview Available Procedure Actions Approach Choices Loaded Procedures Figure 5 92 Approach Loading Loaded Approach Selec...

Page 250: ...ight plan from the Nearest Airport Page 1 Select the Nearest Airports Page 2 Press the FMS Knob then turn the large FMS Knob to highlight the desired nearest airport The airport is previewed on the m...

Page 251: ...ourse of the approach REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN When plans change while ying IFR approaches can be easily removed from the Active Flight Plan Removing an approach from the activ...

Page 252: ...ect to is established to this x until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published x in this case MOGAL If the aircraft altitude is above the...

Page 253: ...Departure Time local Ground Speed Fuel Flow Fuel On Board Aircraft Calibrated Airspeed Indicated Altitude Barometric Pressure Total Air Temperature Softkeys Automatic Manual Page Mode Flight Plan Wayp...

Page 254: ...ght plan these default to the endpoints of the active leg Some of the calculated trip statistics are dashed when the selected leg of the active ight plan has already been own Desired Track DTK DTK is...

Page 255: ...rip FUEL REQ This value is calculated by multiplying the time to go by the fuel ow Total range at entered fuel ow TOTAL RANGE This value is calculated by multiplying the time of fuel endurance by the...

Page 256: ...ys the selected data Selecting waypoints for waypoint mode 1 Select the WPTS Softkey or press the MENU Key highlight Waypoints Mode and press the ENT Key The cursor is positioned in the waypoint eld d...

Page 257: ...Empty Weight Softkey selects Basic Empty Weight Entering basic empty weight 1 Select the EMPTY WT Softkey or press the MENU Key highlight Set Basic Empty Weight and press the ENT Key to select the BAS...

Page 258: ...O FUEL WEIGHT is calculated by adding the basic empty pilot and stores passenger and cargo weights Entering a fuel on board weight 1 Press the FMS Knob to activate the cursor and highlight the FUEL ON...

Page 259: ...ht then the aircraft weight is displayed in amber If the estimated landing weight is greater than the maximum allowable landing weight then the estimated landing weight is displayed in amber If the es...

Page 260: ...y be times when RAIM is not available RAIM prediction must be initiated manually if there is concern over WAAS coverage at the destination or some other reason that compromises navigation precision If...

Page 261: ...ghted 3 Press the MENU Key highlight Set WPT to Present Position and press the ENT Key 4 Press the ENT Key to accept the waypoint entry 5 Turn the FMS Knobs to enter an arrival time and press the ENT...

Page 262: ...the Hawker Beechcraft C90A GT 190 00663 00 Rev A 5 116 FLIGHT MANAGEMENT Figure 5 99 SBAS Display Active SBAS Softkey displays SBAS Selection SBAS SELECTION Box WAAS Enable Disable RAIM Softkey displa...

Page 263: ...Select the AUX GPS Status Page 2 Press the FMS Knob The SBAS SELECTION WAAS eld is highlighted 3 Press the ENT Key to disable SBAS Press the ENT Key again to enable SBAS Figure 5 100 SBAS Display Disa...

Page 264: ...from KMKC to KCOS led using the TIFTO2 departure various Victor Airways and the DBRY1 arrival with the transition at TBE The ight plan includes an enroute altitude of 12 000 feet an LPV WAAS approach...

Page 265: ...GT 5 119 FLIGHT MANAGEMENT 3 ATC now assigns routing to joinV4 A heading of 290 is assigned to interceptV4 The aircraft turns to heading 290 as seen in Figure 5 102 Figure 5 102 Assigned Heading of 2...

Page 266: ...e desired ight plan insertion point SLN as shown in Figure 5 103 When the V4 entry point TOP is inserted it is placed immediately above the highlighted waypoint SLN Figure 5 103 Begin Adding V4 to the...

Page 267: ...the Flight Plan e With SLN still highlighted as in Figure 5 105 turn the small FMS Knob clockwise The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available f Select the LD...

Page 268: ...now displayed as in Figure 5 107 Figure 5 107 List of Available Exits for V4 i If necessary turn either FMS Knob to select the desired exit In this case Salina VOR SLN is selected as in Figure 5 107 j...

Page 269: ...aded in the Flight Plan 5 Making V4 the active leg of the ight plan a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight SLN The TO waypoint of the leg is selected in ord...

Page 270: ...plan leg Note the phase of ight remained in Terminal TERM mode up to this point because a departure leg was active Since a leg after the departure is now active the current CDI ight phase is ENR Enro...

Page 271: ...ENT 7 As the CDI approaches center the aircraft turns onto the active leg as seen in Figure 5 112 Figure 5 112 Turn on to Active Leg 8 At SLN Victor Airway 244 V244 is intercepted Turn prompts are dis...

Page 272: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 5 126 FLIGHT MANAGEMENT 9 As seen in Figure 5 114 V244 is now the active ight plan leg Figure 5 114 V244 Now Active Leg...

Page 273: ...Active 11 ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure ATC advises to expect an altitude of 10 000 feet at OPSHN a Press the FMS Knob to activate the...

Page 274: ...10 000 feet is entered as requested by ATC f Press the ENT Key The cursor is now displayed in the VNV offset eld as shown in Figure 5 118 Figure 5 118 Enter VNV Offset Distance g Enter the offset or...

Page 275: ...OPSHN Note the Direct to waypoint is within the loaded arrival procedure therefore phase of ight scaling for theCDI changes to Terminal Mode and is annunciated by displaying TERM on the HSI NOTE If t...

Page 276: ...ACH should be highlighted as shown in Figure 5 120 Figure 5 120 Proceudures Window c Press the ENT Key A list of available approaches for the destination airport is displayed as in Figure 5 121 Figure...

Page 277: ...ed approach is displayed as in Figure 5 122 Figure 5 122 List of Available Transitions f Turn either FMS Knob to select the desired transition In this case the Initial Approach Fix IAF at HABUK is use...

Page 278: ...g a Press the FMS Knob to activate the cursor b Turn the small FMS Knob to highlight the desired altitude c Press the CLR Key d Press the FMS Knob to deactivate the cursor After making the altitude no...

Page 279: ...ical speed eld VS TGT as shown in Figure 5 125 b At this point the descent vertical speed can be selected or the FPA can be selected Turn the large FMS Knob to select the desired selection eld then tu...

Page 280: ...ertical speed required to reached the selected altitude TheVertical Deviation Indicator VDI and the RequiredVertical Speed Indicator RVSI are now displayed on the PFD as shown in Figure 5 127 Figure 5...

Page 281: ...Figure 5 128 Figure 5 128 VDI RVSI Showing Correctly Established Descent Align Actual Vertical Speed with Required Vertical Speed Keep Vertical Deviation Pointer Centered 17 When the aircraft is one...

Page 282: ...pproaching OPSHN The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5 130 Initiate the turn and maneuver the aircraft on a track through the turn radius to...

Page 283: ...ocedure is now active Figure 5 131 Tracking the OPSHN to FSHER Leg 20 The ight continues through the arrival procedure to PYNON see Figure 5 132 At a point 31 nm from the destination airport the phase...

Page 284: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 5 138 FLIGHT MANAGEMENT Figure 5 132 Approaching PYNON...

Page 285: ...has progressed through the nal waypoint of the arrival and the ight plan has automatically sequenced to the IAF as the active leg activating the approach procedure see Figure 5 133 Figure 5 133 Approa...

Page 286: ...663 00 Rev A 5 140 FLIGHT MANAGEMENT 22 The IAF is the next waypoint At the TOD establish a descent vertical speed as previously discussed in Step 16 The aircraft altitude is 9 000 feet upon reaching...

Page 287: ...dingly and is used much like a localizer when ying an ILS approach The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator as shown in Figure 5 136 when the nal approach course...

Page 288: ...ltitude 6 368 feet after crossing the MAP a direct to is established to this x until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published x in this c...

Page 289: ...quencing is suspended past the MAP Select the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure A direct to is initiated to MOGAL which is the Misse...

Page 290: ...ft continues climbing to AT or ABOVE 10 000 feet at MOGAL A holding pattern is established at the MAHP MOGAL as shown in Figure 5 139 Figure 5 139 Establishing the Holding Pattern 27 The aircraft main...

Page 291: ...no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to dete...

Page 292: ...earing GPS Navigation Lost Message Dead Reckoning Annunciaion Dead Reckoning Annunciation Subdued Aircraft Symbol Nav Data Bar All data except Active Leg TAS and DTK are in yellow Wind Data Wind Data...

Page 293: ...r traf c This section is divided into the following groups Weather GDL 69 69A XM Satellite Weather GWX 68 Airborne Color Weather Radar L 3 STORMSCOPE WX 500 Series II Weather Mapping Sensor Optional T...

Page 294: ...9A XM Satellite Radio and XM Satellite Weather services each have coded IDs The Data and Audio Radio IDs must be provided to XM Satellite Radio to activate the weather service and entertainment subscr...

Page 295: ...RD AVOIDANCE Select INFO Softkey to Display XM Information Page Weather Products Available Products for Service Class Indicated in Green Select LOCK Softkey to Lock Subscription Information Figure 6 2...

Page 296: ...Display Enabled When a weather product is active on the Weather Data Link Page or the Navigation Map Page the age of the data is displayed on the screen The age of the product is based on the time dif...

Page 297: ...ather data is refreshed at intervals that are de ned and controlled by XM Satellite Radio and its data vendors Weather Product Symbol Expiration Time Minutes Refresh Rate Minutes NEXRAD 30 5 Cloud Top...

Page 298: ...tion Map Page Weather Data Link Page Weather Information Page AUX Trip Planning Page Nearest Page Group Flight Plan Pages NEXRAD Cloud Top CLD TOP Echo Top ECHO TOP XM Lightning LTNG Cell Movement CEL...

Page 299: ...MOV SIG AIR METAR LEGEND SFC OFF CYCLONE 24 HR 36 HR 12 HR BACK LEGEND CURRENT 48 HR OFF 9000 12000 6000 BACK LEGEND 3000 15000 SFC PREV OFF NEXT 27000 30000 24000 BACK LEGEND 21000 33000 18000 PREV O...

Page 300: ...duct selections 5 Turn the small FMS Knob to scroll though options for each product ON OFF range settings etc 6 Press the ENT Key to select an option 7 Press the FMS Knob or CLR Key to return to the W...

Page 301: ...s the ENT Key Figure 6 6 4 Turn the small FMS Knob to select the Weather Group and press the ENT Key Figure 6 7 5 Turn the large FMS Knob or press the ENT Key to scroll though product selections Figur...

Page 302: ...rough the legends if more are available than t in the window 4 To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Additional information about the follo...

Page 303: ...NEXRAD network provides important information about severe weather for air traf c safety NEXRAD data is not real time The lapsed time between collection processing and dissemination of NEXRAD images c...

Page 304: ...individual radar sweeps The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the Weather Data Link Page For the NEXRAD leg...

Page 305: ...relative to re ectivity Z NEXRAD measures the radar re ectivity ratio or the energy re ected back to the radar receiver designated by the letter Z The value of Z increases as the returned signal stren...

Page 306: ...dings or mountains which may cause shadows Metallic dust from military aircraft which can cause alterations in radar scans ECHO TOPS NOTE Display of Echo Tops is mutually exclusive with Cloud Tops and...

Page 307: ...oud Tops use the same color scaling to represent altitude display of these weather products is mutually exclusive When Echo Tops is activated NEXRAD and Cloud Tops data are removed Figure 6 14 ECHO TO...

Page 308: ...gure 6 15 Cloud Tops Data Displaying Cloud Tops information 1 Select the Weather Data Link Page with the FMS Knob 2 Select the CLD TOP Softkey To display the Cloud Tops legend select the LEGEND Softke...

Page 309: ...a shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has occurred within a two kilometer region The exact location of the lightning strike is no...

Page 310: ...ey when XM Lightning is selected for display Figure 6 18 Lightning Legend CELL MOVEMENT Cell Movement data shows the location and movement of storm cells as identi ed by the ground based system Cells...

Page 311: ...the Navigation Map Setup Menu see Setting Up XM Satellite Weather To display the Cell Movement legend on the Weather Data Link Page select the LEGEND Softkey when Cell Movement is selected for display...

Page 312: ...lect the SIG AIR Softkey 3 To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon 4 Press the ENT key The gure below shows a sample of SIGMET text To disp...

Page 313: ...METARs are shown as colored ags at airports that provide them Figure 6 23 METAR Flags on the Weather Data Link Page Instructions for Viewing METAR and TAF Text Selected Airport TAF Terminal Area Forec...

Page 314: ...y to select the Weather Information Page 3 Press the FMS Knob to display the cursor 4 Using the FMS Knob enter the desired airport and press the ENT Key 5 Scroll through the METAR and TAF text with th...

Page 315: ...Forecast information is available for current and forecast weather conditions Forecasts are available for intervals of 12 24 36 and 48 hours Figure 6 26 Surface Analysis Data 36 Hour Displaying Surfa...

Page 316: ...cast are selected for display Figure 6 27 Surface Analysis Legend FREEZING LEVEL Freezing Level data shows the color coded contour lines for the altitude and location at which the rst isotherm is foun...

Page 317: ...layed Figure 6 29 Freezing Level Legend WINDS ALOFT Winds Aloft data shows the forecast wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3000 foot increme...

Page 318: ...Beechcraft C90A GT 190 00663 00 Rev A 6 26 HAZARD AVOIDANCE Figure 6 30 Winds Aloft at 27 000 Feet To display the Winds Aloft legend select the LEGEND Softkey when Winds Aloft is selected for display...

Page 319: ...res tornadoes severe thunderstorms ood conditions and other natural disasters Figure 6 32 County Flood and Thunderstorm Warnings Thunderstorm Warnings Flood Warnings Displaying County Warning informa...

Page 320: ...hurricanes and their projected tracks Figure 6 34 Cyclone Data Selected for Display Cyclone Displaying cyclone hurricane track information 1 Select the Weather Data Link Page with the FMS Knob 2 Selec...

Page 321: ...ect the weather behind a storm Weather Alert that looks ahead for intense cell activity in the 80 320 nm range even if these ranges are not being monitored PRINCIPLES OF PULSED AIRBORNE WEATHER RADAR...

Page 322: ...radar is only capable of seeing what is inside the boundaries of the beam The gure below depicts a radar beam s characteristics The gure illustrates vertical dimensions of the radar beam although the...

Page 323: ...portion of the radar energy is re ected back to the antenna However much of the energy is absorbed If precipitation is very heavy or covers a large area the signal may not reach completely through the...

Page 324: ...ectors are raindrops wet snow or wet hail The larger the raindrop the better the re ectivity The size of the precipitation droplet is the most important factor in radar re ectivity Because large drop...

Page 325: ...n the display However rough or choppy water is a better re ector and provides stronger returns from the downwind sides of the waves Mountains also provide strong return signals to the antenna but also...

Page 326: ...d 11 for 12 antenna MPEL Boundary Figure 6 40 MPEL Boundary BASIC ANTENNA TILT SETUP The following discussion is a simple method for setting up the weather radar antenna tilt for most situations It is...

Page 327: ...isplayed range to 60 miles may be more helpful Closely monitor anything that enters the display Also after setting up the antenna tilt angle as described previously ground returns can be monitored for...

Page 328: ...d downdrafts in thunderstorms carry water through the cloud The more severe the drafts the greater the number and size of the precipitation droplets With this in mind the following interpretations can...

Page 329: ...the target return may also indicate turbulence appearing as hooks ngers or scalloped edges These irregularities may be present in green areas with no yellow red or magenta areas and should be treated...

Page 330: ...ost often have not shown shapes different from those of a normal thunderstorm display HAIL Hail results from updrafts carrying water high enough to freeze Therefore the higher the top of a thunderstor...

Page 331: ...the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby mode the antenna is parked at the center line It is always a good idea to put the radar in Standby mode b...

Page 332: ...e radar enters the Standby Mode a Select the WEATHER Softkey A con rmation window is displayed Figure 6 46 Con rming Activating Radar b Turn the small FMS Knob to highlight YES and press the ENT Key t...

Page 333: ...e Press the ENT Key 2 Press the ENT Key 3 Turn the small FMS Knob to place the Bearing Line on the desired storm cell or other area to be vertically scanned Figure 6 47 Bearing Line on Horizontal Scan...

Page 334: ...the freezing level of the storm The best way to nd this point is to use the Vertical Scan feature The antenna tilt angle can be centered on the strongest return area in the vertical scan to get a more...

Page 335: ...ILT eld and display the Tilt Line If theTilt Line is not displayed press the MENU Key and turn the large FMS Knob to select ShowTilt Line Press the ENT Key 2 Turn the small FMS Knob to adjust the ante...

Page 336: ...intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN eld 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the GAIN...

Page 337: ...Press the ENT Key Figure 6 51 Selecting Sector Scan Position 3 Turn the small FMS Knob to place the Bearing Line in the desired position The location of the Bearing Line becomes the center point of t...

Page 338: ...0 Sector Scan ANTENNA STABILIZATION 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF...

Page 339: ...lso attenuates the radar energy All these factors have an effect on the return intensity The more energy that dissipates the lesser the displayed intensity of the return Accuracy of the displayed inte...

Page 340: ...pproximate azimuth of the detected returns If a Weather Alert is detected within 10 of the aircraft heading an alert is displayed on the PFD in the Messages Window If the antenna tilt is adjusted too...

Page 341: ...nd targets can be recognized more easily As previously discussed the type and orientation of the target in relation to the aircraft affects the intensity displayed When the weather radar system is in...

Page 342: ...ftkey or the INSET Softkey for the PFD Inset Map then press the STRMSCP Softkey These pages can also display cell or strike data using the yellow lightning strike symbology shown in Table 6 5 Lightnin...

Page 343: ...s the display of Stormscope data on or off STRMSCP MODE Selects the CELL or STRIKE mode of lightning activity Cell mode identi es clusters or cells of electrical activity Strike mode indicates the app...

Page 344: ...ey 3 Select the Weather group 4 Press the ENT Key The cursor ashes on STRMSCP LTNG 5 Turn the large FMS Knob to select STRMSCP MODE 6 Turn the small FMS Knob to change between CELL and STRIKE options...

Page 345: ...vigation Map Page However in Track Up orientation at the 500 nm range a portion of Stormscope lightning data can be behind the aircraft and therefore not visible on the Navigation Map Since the range...

Page 346: ...ss the FMS Knob to return to the Navigation Map Page To change the display range on the Navigation Map Page turn the RANGE Knob clockwise to zoom out or counter clockwise to zoom in SELECTING THE STOR...

Page 347: ...the Stormscope Page Or 1 Select the Stormscope Page 2 Press the MENU Key 3 Turn the small FMS Knob to choose between CELL and STRIKE options 4 When an item is selected press the ENT Key If heading inp...

Page 348: ...IEW Softkey The 360 and ARC softkeys are displayed 3 Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area 4 Press the BACK Softkey to return to th...

Page 349: ...uses information provided from the GPS receiver to provide a horizontal position and altitude GPS altitude is derived from satellite measurements GPS altitude is converted to a mean sea level MSL bas...

Page 350: ...le is between 100 and 1000 below current aircraft altitude Table 6 6 TAWS Obstacle Colors and Symbology TAWS information can be displayed on the following maps PFD Inset Map Navigation Map Page TAWS P...

Page 351: ...Customizing terrain and obstacle display on the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key Figure 6 64 4 Turn the small F...

Page 352: ...d heading Two views are available relative to the position of the aircraft the 360 default display and the radar like ARC 120 display Map range is adjustable with the RANGE Knob from 1 to 200 nm as in...

Page 353: ...ning Terrain Above or Within 100 Below the Aircraft Altitude Black Terrain Terrain More than 1000 Below the Aircraft Altitude Terrain Legend Map Range Yellow Terrain Caution Terrain Between 100 and 10...

Page 354: ...y issued Table 6 7 shows TAWS alert types with corresponding annunciations and aural messages When an alert is issued annunciations appear on the PFD and MFD The TAWS Alert Annunciation is shown to th...

Page 355: ...190 00663 00 Rev A Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 6 63 HAZARD AVOIDANCE Figure 6 71 TAWS PULL UP Alert Annunciation on the MFD Alert Annunciation Potential Impact Point...

Page 356: ...ed TAWS Inhibited Annunciation Inhibiting enabling TAWS alerting 1 Select the TAWS Page 2 Press the MENU Key 3 Select Inhibit TAWS or Enable TAWS depending on the current state and press the ENT Key O...

Page 357: ...l Up or Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution RTC or Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI or Terrai...

Page 358: ...itable noti cation when the aircraft is determined to be closing descending upon terrain at an excessive speed The following gure shows the parameters for the alert as de ned by TSO C151b 6000 5500 50...

Page 359: ...CLE IMPACT Imminent Terrain Impact ITI and Imminent Obstacle Impact IOI alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the aircraft s projected path ITI an...

Page 360: ...he threshold During the nal descent algorithms set a threshold for alerting based on speed distance and other parameters 700 600 500 400 300 200 100 Height Above Terrain Feet Distance From Destination...

Page 361: ...display NCR alerting is only active when departing from an airport and when the following conditions are met Height above the terrain is less than 700 feet Distance from the departure airport is 2 nm...

Page 362: ...age Menu TAWS continually monitors several system critical items such as database validity hardware status and GPS status If the terrain obstacle database is not available the aural message TAWS Syste...

Page 363: ...ltitude separation data or climb descent indication NOTE TIS is disabled when a Traf c Advisory System TAS is installed The type of traf c system that is installed is determined by the traf c page sof...

Page 364: ...S also provides a vector line showing the direction in which the traf c is moving to the nearest 45 Traf c information for which TIS is unable to determine the bearing non bearing traf c is displayed...

Page 365: ...traf c is selected on maps other than the Traf c Map Page the traf c icon is shown to indicate the feature is enabled for display Figure 6 78 TIS Traf c on the Navigation Map Page Traf c Advisory Tra...

Page 366: ...MODE Selects the traf c mode for display select from All Traf c Displays all traf c TA PA Displays Traf c Alerts and Proximity Advisories TA ONLY Displays Traf c Alerts only TRAFFIC SMBL Selects the m...

Page 367: ...ode and the G1000 begins to display traf c information Refer to the System Status discussion for more information Displaying traf c on the Traf c Map Page 1 Turn the large FMS Knob to select the Map P...

Page 368: ...itially decreases and then subsequently increases another voice alert is generated Figure 6 83 Traf c Annunciation PFD Inset Map Displays When TA is Detected A Traf c Not Available TNA voice alert is...

Page 369: ...performs an automatic test of TIS during power up If TIS passes the test TIS enters Standby Mode on the ground or Operating Mode in the air If TIS fails the power up test an annunciation is shown in t...

Page 370: ...cted for display on another map while Standby Mode is selected the traf c display enabled icon is crossed out also the case when TIS has failed Once the aircraft is airborne TIS switches to Operating...

Page 371: ...rmine bearing of Traf c Advisory Annunciation indicates distance in nm altitude separation in hundreds of feet and altitude trend arrow climbing descending AGE MM SS Appears if traf c data is not refr...

Page 372: ...k Traf c is displayed according to TCAS symbology using four different symbols TAS Symbol Description Non Threat Traf c Proximity Advisory PA Traf c Advisory TA Traf c Advisory Off Scale Table 6 15 TA...

Page 373: ...st 1 Set the range to 2 6 nm 2 Press the STANDBY Softkey 3 Press the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traf c symbols are displayed and...

Page 374: ...om 2 to 40 nm as indicated by the map range rings The traf c mode and altitude display mode are annunciated in the upper left corner DISPLAYING TRAFFIC DATA Traf c information can be displayed on the...

Page 375: ...chcraft C90A GT 6 83 HAZARD AVOIDANCE 2 Select the TRAFFIC Softkey Traf c is now displayed on the map as shown in the gure Proximity Traf c Figure 6 87 TAS Traf c on Navigation Map Traf c Advisory TA...

Page 376: ...altitude display mode 1 On the Traf c Page select the ALT MODE Softkey 2 Press one of the following Softkeys BELOW NORMAL ABOVE UNREST unrestricted 3 To return to the Traf c Page select the BACK Softk...

Page 377: ...ta on or off TRAFFIC MODE Selects the traf c mode for display select from All Traf c Displays all traf c TA PA Displays Traf c Alerts and Proximity Advisories TA ONLY Displays Traf c Alerts only TRAFF...

Page 378: ...g for 5 seconds and remaining displayed until no TAs are detected in the area The PFD Inset Map is automatically displayed with TA traf c Figure 6 91 Traf c Annunciation PFD Inset Map Displays When TA...

Page 379: ...information appear in a banner at the lower left corner of maps on which traf c can be displayed Traf c Status Banner Annunciation Description TA OFF SCALE A Traf c Advisory is outside the selected d...

Page 380: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 6 88 HAZARD AVOIDANCE BLANK PAGE...

Page 381: ...700 AFCS can be divided into these main operating functions Flight Director FD The Hawker Beechcraft C90A GT has two ight directors each operating within an IAU and referred to as pilot side and copil...

Page 382: ...ntal Situation Indicator HSI of the corresponding PFD Press to re center the Course Deviation Indicator CDI and return course pointer directly TO the bearing of the active waypoint station 10 SPD Key...

Page 383: ...ctions of this manual GA Switch Go Around Disengages the autopilot and selects ight director Takeoff on ground or Go Around in air Mode If an approach procedure is loaded this switch also activates th...

Page 384: ...e autopilot is engaged Control Pressed Modes Selected Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold defa...

Page 385: ...uses are shown in the center of the AFCS Status Box Lateral ight director modes are displayed on the left and vertical on the right Armed modes are displayed in white and active in green Figure 7 2 PF...

Page 386: ...light indicate loss of sensor ADC or navigation data VOR LOC GPS VNV WAAS required to compute commands When such a loss occurs the system automatically begins to roll the wings level enters Roll Hold...

Page 387: ...ndently to indicate pitch horizontal bar and roll vertical bar commands Both PFDs show the same Command Bar format Command Bar format may only be changed while on the ground Figure 7 5 Single cue Comm...

Page 388: ...rtical speed may be used to climb descend to the Selected Altitude VS Key VS nnnn FPM 4000 to 4000 fpm 100 fpm Flight Level Change IAS Hold Maintains the current aircraft airspeed in IAS or Mach while...

Page 389: ...old Mode the ight director maintains a constant pitch attitude the pitch reference The pitch reference is set to the aircraft pitch attitude at the moment of mode selection If the aircraft pitch attit...

Page 390: ...for up to 10 seconds and the appearance of the white ALT annunciation The Selected Altitude is shown as the Altitude Reference beside the ALTS annunciation At 50 feet from the Selected Altitude the i...

Page 391: ...e Mode see Figure 7 8 Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude error is less than 50 feet In this case the Selected Altitude becomes the ight di...

Page 392: ...yed above the Vertical Speed Indicator A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator CHANGING THE VERTICAL SPEED REFERENCE The Vertical Speed R...

Page 393: ...Level Change Mode is indicated by a green FLC annunciation beside the Airspeed Reference in the AFCS Status Box The Airspeed Reference is also displayed directly above the Airspeed Indicator along wit...

Page 394: ...rence IAS or Mach automatic switching does not occur For descent if Mach airspeed reference is selected above 16 000 ft the aircraft descends in Mach until the indicated airspeed reaches 220 KIAS at w...

Page 395: ...or vertical direct to is active VNV is enabled VNV ENBL Softkey pressed on the MFD Crosstrack error is valid and within certain limits Desired actual track are valid or track angle error is within cer...

Page 396: ...des If applicable the appropriate altitude capture mode is armed for capture of the next VNV Target Altitude ALTV or the Selected Altitude ALTS whichever is greater Figure 7 13 Vertical Path Tracking...

Page 397: ...ge VNV indications VNV Target Altitude vertical deviation and vertical speed required appear on the PFDs in magenta Figure 7 14 Selected Altitude Below VNV Target VNV Target Altitude Required Vertical...

Page 398: ...V Target Altitude Capture Armed Vertical Path Tracking Active If the altimeter barometric setting is adjusted while Vertical Path Tracking is active the ight director increases decreases the descent r...

Page 399: ...ve vertical direct to Unless VNV is disabled Vertical Path Tracking Mode and the appropriate altitude capture mode become armed following the reversion to Pitch Hold Mode to allow for possible pro le...

Page 400: ...The VNV Target Altitude is shown as the Altitude Reference beside the ALTV annunciation and remains displayed above the Vertical Speed Indicator The Required Vertical Speed Indication RSVI is removed...

Page 401: ...o a waypoint not in the ight plan 2 Ensure that GPS is the selected navigation source use the CDI Softkey to cycle through navigation sources if necessary 3 Press the APR Key Upon reaching the glidepa...

Page 402: ...e use the CDI Softkey to cycle through navigation sources if necessary 3 Press the APR Key Or 1 Ensure that GPS is the selected navigation source use the CDI Softkey to cycle through navigation source...

Page 403: ...mode can be selected only while on the ground by pushing the GA Switch The ight director Command Bars assume a wings level pitch up attitude Pressing the GA Switch while in the air activates the ight...

Page 404: ...Track No Glideslope LOC 25 Backcourse Arm Capture Track Captures and tracks a localizer signal for backcourse approaches BC Key BC 25 Approach GPS Arm Capture Track Captures and tracks the selected na...

Page 405: ...ll Hold Mode Responses Figure 7 24 Roll Hold Mode Annunciation CHANGING THE ROLL REFERENCE The roll reference can be changed by pressing the CWS Button establishing the desired bank angle then releasi...

Page 406: ...he Selected Heading is adjusted using the HDG Knob on either PFD Pressing the CWS Button and hand ying the aircraft does not change the Selected Heading The autopilot guides the aircraft back to the S...

Page 407: ...s pressed the selected mode is armed If the CDI shows less than one dot Navigation Mode is automatically captured when the NAV Key is pressed The armed annunciation appears in white to the left of the...

Page 408: ...ector CRS1 for the pilot side CRS2 for the copilot side Pressing the CWS Button and hand ying the aircraft does not change the Selected Course while in Navigation Mode The autopilot guides the aircraf...

Page 409: ...he active lateral mode If the CDI is less the 1 dot the LOC is automatically captured when the APR Key is pressed VOR Approach Mode VAPP provides greater sensitivity for signal tracking than VOR Navig...

Page 410: ...the active ight plan 3 Ensure the corresponding LOC frequency is tuned 4 Press the APR Key If the following occurs the ight director reverts to Roll Hold Mode wings rolled level Approach Mode is acti...

Page 411: ...Key is pressed The ight director creates roll steering commands from the Selected Course and deviation when in Backcourse Mode Pitch Hold Mode Active Backcourse Mode Active LOC2 is Selected Navigation...

Page 412: ...p clutches set to certain values This allows the servos to be overridden in case of an emergency PITCH AXIS AND TRIM The autopilot pitch axis uses pitch rate to stabilize the aircraft pitch attitude d...

Page 413: ...e autopilot and the yaw damper annunciator light is illuminated Autopilot and yaw damper status are displayed in the center of the AFCS Status Box Engagement is indicated by green AP and YD annunciati...

Page 414: ...lert may be cancelled by pushing the MEPT ARM or AP YD DISC Switch AP YD DISC Switch also cancels the ashing AP annunciation Automatic autopilot disengagement is indicated by a ashing red and white AP...

Page 415: ...during a ight In this scenario the aircraft departs Charles B Wheeler Downtown Airport KMKC enroute to Colorado Springs Airport KCOS After departure the aircraft climbs to 12 000 ft and airway V4 is i...

Page 416: ...tical Speed Mode The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP DN Wheel or pushing the CWS Button while hand ying the aircraft to establish a new...

Page 417: ...90 00663 00 Rev A Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 7 37 AFCS Figure 7 37 Departure Selected Altitude of 12 000 MSL 1 2 3 4 HDG Mode VS Mode ALT Mode TO Mode T O M o d e KMK...

Page 418: ...ation source to VOR c Use the CRS1 or CRS2 Knob to set the Selected Course to the desired value 255 Note that at this point the ight director is still in Heading Select Mode and the autopilot continue...

Page 419: ...n from VOR to GPS Navigation Mode a Press the CDI Softkey until GPS is the selected navigation source b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft along the ac...

Page 420: ...Change Mode is used in the example Flight Level Change descent 1 Select Flight Level Change Mode a Using the ALT SEL Knob set the Selected Altitude to 10 000 feet b Press the FLC Key to activate Fligh...

Page 421: ...egins ashing do one of the following Press the VNV Key Turn the ALT SEL Knob to adjust the Selected Altitude If the descent is not con rmed by the time of interception Vertical Path Tracking Mode rema...

Page 422: ...tains the Airspeed Reference 3 As the aircraft nears the Selected Altitude the ight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation ashing for up to 10...

Page 423: ...3 AFCS Figure 7 42 Non path Descent HABUK VNAV Target Altitude of 10 000 MSL VNAV Target Altitude of 9 000 MSL ALT Mode Planned Descent Path Selected Altitude of 9 400 MSL ALT Mode VPTH M ode 1 2 3 FL...

Page 424: ...s a Ensure the appropriate localizer frequency is tuned b Press the APR Key when cleared for approach to arm Approach and Glideslope modes LOC and GS appear in white as armed mode annunciations c The...

Page 425: ...ch into the ight plan 2 Press the APR Key once clearance for approach has been received GPS Approach Mode is activated and Glidepath Mode is armed 3 Once the glidepath is captured Glidepath Mode becom...

Page 426: ...ed approach is activated and the autopilot disconnects indicated by the AP annunciation ashing yellow for 5 seconds and the autopilot disconnect aural alert Flashes 5 sec 2 Start the climb to the pres...

Page 427: ...hcraft C90A GT 7 47 AFCS 4 The autopilot ies the holding pattern after the missed approach is activated Annunciations are displayed in the Navigation Status Box above the AFCS Status Box Figure 7 45 G...

Page 428: ...own Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure or stuck MEPT Switch If AP engaged take control of the aircraft and disengage AP If AP disen...

Page 429: ...n becomes active Overspeed protection is provided in situations where the ight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certi ed max...

Page 430: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A 7 50 AFCS BLANK PAGE...

Page 431: ...channels of music news and sports XM Radio offers more entertainment choices and longer range coverage than commercial broadcast stations The Scheduler feature can be used to enter and display short...

Page 432: ...KSFO airport Airport Hot Spots are outlined in magenta When panning over the airport features such as runway holding lines and taxiways are shown at the cursor Figure 8 1 SafeTaxi Depiction on the Na...

Page 433: ...U Map Setup Option 3 Turn the FMS Knob to select the Aviation Group and press the ENT Key 4 Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI 5 Turn the small FMS Knob t...

Page 434: ...icates whether the databases are current out of date or not available The Power up Page shows the SafeTaxi database is current when the SafeTaxi Expires date is shown in white When the SafeTaxi cycle...

Page 435: ...s never disabled Select the DBASE Softkey for scrolling through the database information Scroll through the database with the FMS knob or ENT Key The SafeTaxi database cycle number shown in the gure 0...

Page 436: ...he EFFECTIVE date is the beginning date for this database cycle EXPIRES date is the revision date for the next database cycle NOT AVAILABLE indicates that SafeTaxi is not available on the database car...

Page 437: ...age selecting the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys CHRT OPT CHRT INFO DP STAR APR WX NOTAM and GO BACK The chart selection s...

Page 438: ...ll through the OPTIONS Menu to Show Chart 3 Press the ENT Key to display the chart Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8 8 Option Menus When no termi...

Page 439: ...the WPT Pages or Flight Plan Pages If a chart is available for the destination airport or the airport selected in the active ight plan the chart appears on the screen When no ight plan is active or wh...

Page 440: ...on choices 8 Turn either FMS Knob to scroll through the available charts 9 Press the ENT Key to complete the chart selection Select Desired Approach Chart from Menu Scroll Through Entire Chart With th...

Page 441: ...hartView diagram and the associated map in the WPT page group In the example shown the CHRT Softkey switches between the Gainesville FL KGNV Airport Diagram and the navigation map on the WPT Airport I...

Page 442: ...to Taxiway Bravo on the Charlotte NC KCLT airport Another source for additional airport information is from the INFO Box above the chart for certain airports This information source is not related to...

Page 443: ...Class B Chart is selected Pressing the ENT Key displays the Charlotte Class B Airspace Chart Figure 8 14 Figure 8 14 Airport Information Page Class B Chart Selected from INFO View Selecting the DP Sof...

Page 444: ...ey displays the Standard Terminal Arrival Chart if available Figure 8 16 Arrival Information Page Aircraft Not Shown Icon Change Range and Scroll Through the Chart With the Joystick Chart Not To Scale...

Page 445: ...irport weather frequency information and includes weather data such as METAR and TAF from the XM Data Link Receiver when available Weather information is available only when an XM Data Link Receiver i...

Page 446: ...ncluded in the ChartView database Selecting the NOTAM Softkey shows the local NOTAM information for selected airports when available When NOTAMS are not available the NOTAM Softkey label appears subdu...

Page 447: ...FEATURES Figure 8 20 Airport Information Page Local NOTAMs Local NOTAM on This Airport NOTAM Softkey Selected Selecting the NOTAM Softkey again removes the NOTAMS information Selecting the GO BACK So...

Page 448: ...8 ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys the chart options level Figure 8 7 Selecting the ALL Softkey shows the entire approach chart on t...

Page 449: ...HEADER Softkey shows the header view approach chart brie ng strip on the screen Approach Chart Brie ng Strip Figure 8 22 Approach Information Page Header View Selecting the PLAN Softkey shows the app...

Page 450: ...escent pro le strip Approach Chart Descent Pro le Strip Figure 8 24 Approach Information Page Pro le View Full Screen Width Selecting the MINIMUMS Softkey displays the minimum descent altitude visibil...

Page 451: ...ONAL FEATURES If the chart scale has been adjusted to view a small area of the chart selecting the FIT WIDTH Softkey changes the chart size to t the available screen width Select FIT WDTH Softkey to S...

Page 452: ...n the large FMS Knob to highlight the AIRPORT INFO or FREQUENCIES Box INFO Box shown 4 Turn the small FMS Knob to select the INFO Box choices If multiple choices are available scroll to the desired ch...

Page 453: ...While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to...

Page 454: ...d press the ENT Key Figure 8 29 Waypoint Information Page OPTIONS Menu 3 Turn the large FMS Knob to move to the COLOR SCHEME Option Figure 8 30 4 Turn the small FMS Knob to choose between Day Auto and...

Page 455: ...Garmin G1000 Pilot s Guide for the Beechcraft C90A GT 190 00663 00 Rev A 8 25 ADDITIONAL FEATURES Figure 8 30 Arrival Information Page Day View Figure 8 31 Arrival Information Page Night View...

Page 456: ...Garmin authorized service center for con guration System is con gured for ChartView but no chart database is installed Contact Jeppesen for a ChartView database Normal operation ChartView database is...

Page 457: ...s the chart data cycle has expired within the past week and the next chart cycle is available Chart data is out of date in yellow indicates charts are still viewable but approaching the disable date C...

Page 458: ...ed and is disabled until a revised issue of ChartView is installed Select the DBASE Softkey for scrolling through the database information Scroll through the database with the FMS knob or ENT Key The...

Page 459: ...is the date that this database cycle is no longer viewable REGION and CYCLE NOT AVAILABLE in blue indicate that no ChartView data is available on the database card or no database card is inserted Fig...

Page 460: ...he chart selection level of softkeys CHRT OPT CHRT INFO DP STAR APR WX and GO BACK The chart selection softkeys appear on the Airport Information Page Selecting the GO BACK Softkey reverts to the top...

Page 461: ...large FMS Knob to scroll through the OPTIONS Menu to Show Chart 3 Press the ENT Key to display the chart Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8 36 Opt...

Page 462: ...the WPT Pages or Flight Plan Pages If a chart is available for the destination airport or the airport selected in the active ight plan the chart appears on the screen When no ight plan is active or w...

Page 463: ...the large FMS Knob to select the Approach Box 7 Turn the small FMS Knob to show the approach chart selection choices 8 Turn either FMS Knob to scroll through the available charts 9 Press the ENT Key t...

Page 464: ...e FliteCharts diagram and the associated map in the WPT page group In the example shown the CHRT Softkey switches between the Gainesville FL KGNV Airport Diagram and the navigation map on the WPT Airp...

Page 465: ...l airport information is from the INFO Box above the chart Figure 8 39 or to the right of the chart Figure 8 41 for certain airports This information source is not related to the INFO Softkey When the...

Page 466: ...in Figure 8 41 ALTERNATE MINIMUMS is selected Pressing the ENT Key displays the IFR Alternate Minimums Chart Figure 8 42 Figure 8 42 Airport Information Page ALTERNATE MINIMUMS Selected from INFO Vie...

Page 467: ...A 8 37 ADDITIONAL FEATURES Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available Figure 8 44 Arrival Information Page Selecting the APR Softkey displays the approach ch...

Page 468: ...the WX Softkey to display the information windows AIRPORT INFO 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the INFO Box 4 Turn the small FMS Knob to select the I...

Page 469: ...9 ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys the chart options level Figure 8 35 Selecting the ALL Softkey shows the entire chart on the scree...

Page 470: ...EATURES Selecting the FIT WIDTH Softkey ts the width of the chart in the display viewing area In the example shown the chart at close range is replaced with the full width chart Figure 8 48 Approach I...

Page 471: ...tkey alternates between removing and replacing the data window to the right Figure 8 49 Airport Information Page Full Screen and Info Window Select FULL SCN Softkey to Switch Between Chart on Full Scr...

Page 472: ...While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to...

Page 473: ...nd press the ENT Key Figure 8 51 Waypoint Information Page OPTIONS Menu 3 Turn the large FMS Knob to move to the COLOR SCHEME Option Figure 8 52 4 Turn the small FMS Knob to choose between Day Auto an...

Page 474: ...Garmin G1000 Pilot s Guide for the Beechcraft C90A GT 190 00663 00 Rev A 8 44 ADDITIONAL FEATURES Figure 8 52 Approach Information Page Day View Figure 8 53 Approach Information Page Night View...

Page 475: ...ilable current out of date or disabled See the table below for the various FliteCharts Power up Page displays and the de nition of each Power up Page Display De nition Blank Line G1000 system is not c...

Page 476: ...approaching the disable date When the 180 day grace period has expired Chart data is disabled in yellow indicates that the FliteCharts database has expired and is no longer viewable Chart Data N A app...

Page 477: ...y label appears subdued and is unavailable until a revised issue of FliteCharts is installed Select the DBASE Softkey for scrolling through the database information Scroll through the database with th...

Page 478: ...te that this database cycle is no longer viewable REGION and CYCLE NOT AVAILABLE in blue indicate that FliteCharts database is not available on the database card or no database card is inserted Figure...

Page 479: ...For more information on speci c service packages visit www xmradio com ACTIVATING XM SATELLITE RADIO SERVICES The service is activated by providing XM Satellite Radio with either one or two coded IDs...

Page 480: ...d on the website Follow the instructions provided by XM Satellite Radio services 2 Select the Auxiliary Page Group 3 Select the next to last page in the AUX Page Group 4 Select the INFO Softkey to dis...

Page 481: ...entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Infor...

Page 482: ...el list 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or 1 Press the FMS Knob to h...

Page 483: ...nnels for a type of music or other contents One of the optional categories is PRESETS to view channels that have been programmed Selecting a category 1 Select the CATGRY Softkey on the XM Radio Page 2...

Page 484: ...umber to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Figure 8 60 Accessing and Selecting XM Preset Channels Select PRESETS to Access the P...

Page 485: ...Scheduler Utility Page Entering a scheduler message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the rst empty s...

Page 486: ...Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the name eld of the scheduler message to be deleted 4 Press the CLR Key to clear the message text I...

Page 487: ...n activated Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver For troubleshooting purposes check the LRU Information Box on the AUX System Status...

Page 488: ...de NO SIGNAL XM Radio Page active channel eld Weather Datalink Page center of page Loss of signal signal strength too low for receiver LOADING XM Radio Page active channel eld Acquiring channel audio...

Page 489: ...rough the alert message list Softkey Annunciation During certain alerts the ALERTS Softkey may appear as a ashing annunciation to accompany an alert The ALERTS Softkey assumes a new label consistent w...

Page 490: ...Level De nitions Section for more information The annunciation tone may be tested from the AUX System Status Page Testing the system annunciation tone 1 Use the FMS Knob to select the AUX System Statu...

Page 491: ...general information An annunciation alert is accompanied by a ashing ADVISORY Softkey annunciation see Figure A 3 Pressing the ADVISORY Softkey acknowledges the presence of the annunciation alert Mes...

Page 492: ...lues generated by redundant sensors If differences in the sensors exceed a speci ed amount this discrepency is annunciated in the Comparator Window as a MISCOMP miscompare as seen in Figure A 1 If one...

Page 493: ...ADC The PFDs are displaying data from the cross side Air Data Computer XSIDE AHRS The PFDs are displaying data from the cross side Attitude Heading Reference System G1000 SYSTEM ANNUNCIATIONS When a...

Page 494: ...em Annunciation Red X Figure A 4 G1000 System Failure Annunciations GDC 74B Air Data Computer GTX 33 Transponder Or GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GEA 71 Engine Airframe U...

Page 495: ...a Garmin authorized repair facility System Annunciation Comment Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS Display system is n...

Page 496: ...ge Always use sound pilot judgment The AFM POH takes precedence over any con icting guidance found in this section MFD PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Rech...

Page 497: ...m persists PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD1 key name Key is stuck CNFG MODULE PFD1 con guration module is inoperative The PFD1 con guration module backup memory has failed The G...

Page 498: ...the G1000 system should be serviced PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists MFD1 DB ERR MFD1 obstacle database missing The obstacle database is...

Page 499: ...a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced DB MISMATCH Aviation da...

Page 500: ...may still be available and the audio panel may still be usable The G1000 system should be serviced when possible GMA2 SERVICE GMA2 needs service Return unit for repair GIA 63W MESSAGE ADVISORIES Mess...

Page 501: ...TT COM1 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists...

Page 502: ...e transfer key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S2 FAIL G S2 is inoperative G S1 SERV...

Page 503: ...information to augment the lack of airspeed The G1000 system should be serviced AHRS2 TAS AHRS2 not receiving airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS rel...

Page 504: ...has incorrect software installed The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 He...

Page 505: ...on guration settings do not match those of backup con guration memory The G1000 system should be serviced GCU FAIL GCU is inoperative A failure has been detected in the GCU 475 The GCU 475 is unavaila...

Page 506: ...e to a new aviation database update Verify that stored ight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system noti es the pilot that the timer has expired DB CHANGE Da...

Page 507: ...plan The lateral ight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unav...

Page 508: ...ide a sustained force Be prepared to apply nose down control wheel force upon autopilot disconnect Aileron Mistrim Left A condition has developed causing the roll servo to provide a sustained left for...

Page 509: ...e Pull Up Pull Up or ObstacleAhead Pull Up ObstacleAhead Pull Up Imminent Obstacle ImpactWarning IOI or ObstacleAhead Pull Up ObstacleAhead Pull Up or Obstacle Obstacle Pull Up Pull Up Reduced Require...

Page 510: ...e No GPS position or excessively degraded GPS signal None TAWS Not Available TAWS Available is heard when suf cient GPS signal is re established System Test in progress None None System Test pass None...

Page 511: ...he MFD The aviation database may be installed from the Jeppesen supplied SD data card or copied to one of the Garmin supplied Supplemental Data Cards Contact Jeppesen www jeppesen com for subscription...

Page 512: ...se products will be downloaded to three Supplemental Data Cards with the exception of FliteCharts which is loaded on only one card Insert each Supplemental Data Card into the correct location shown in...

Page 513: ...n Databases section of the Garmin website www garmin com Once the updated les have been downloaded from the website a PC equipped with an appropriate SD card reader is used to unpack and program the n...

Page 514: ...by pressing the ENT Key or the right most softkey 4 Turn the large FMS Knob to select the AUX Page group on the MFD 5 Turn the small FMS Knob to select the System Status Page 6 Press the DBASE Softke...

Page 515: ...upport Branch ASOS Automated Surface Observing System ATC Air Traf c Control ATCRBS ATC Radar Beacon System ATIS Automatic Terminal Information Service ATK along track AUTOSEQ automatic sequence AUX a...

Page 516: ...desired course between the active from and to waypoints DEST destination DF Direct to Fix DFLT default DGRD degrade DH decision height Dilution of Precision A measure of GPS satellite geometry qualit...

Page 517: ...IS B Flight Information Services Broadcast FISDL Flight Information Service Data Link FL ight level FLC Flight Level Change FM Course From Fix to Manual Termination FMS Flight Management System FOB Fu...

Page 518: ...e Identi er IDENT IDNT identi cation IF Initial Fix IFR Instrument Flight Rules IG Imperial gallon ILS Instrument Landing System IMC Instrument Meteorological Conditions in inch INACTV inactive INC FU...

Page 519: ...afe Altitude Uses Grid MORAs to determine a safe altitude within ten miles of the aircraft present position MKR marker beacon MOA Military Operations Area MOV movement mpm meters per minute MSA Minimu...

Page 520: ...ature SBAS Satellite Based Augmentation System SCIT Storm Cell Identi cation and Tracking SD Secure Digital sec second s SEL SLCT select SFC surface SIAP Standard Instrument Approach Procedures SID St...

Page 521: ...t VERT vertical Vertical Figure of Merit A measure of the uncertainty in the aircraft s vertical position Vertical Speed Required The vertical speed necessary to descend climb from a current position...

Page 522: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A C 8 APPENDIX C BLANK PAGE...

Page 523: ...ATIONS Both LNAV VNAV and LPV approaches use the accuracy of WAAS to include vertical glide path guidance capability The additional accuracy and vertical guidance capability allows improved instrument...

Page 524: ...cedure The original en route portion of the ight plan remains active unless the instrument procedure is activated This may be done either when the procedure is loaded or at a later time Flight plans c...

Page 525: ...s enabled i e no OBS or SUSP annunciation For automatic sequencing to occur the aircraft must also cross the bisector of the turn being navigated The bisector is a line passing through the waypoint co...

Page 526: ...approach procedure has not yet commenced the CDI is scaled for oceanic ight 2 0 nm Within 31 nm of the destination airport terminal area the CDI scale gradually ramps down from 2 0 nm to 1 0 nm over...

Page 527: ...HOW CAN A NEW APPROACH BE ACTIVATED NOTE Do not attempt to reactivate the current approach prior to crossing the missed approach point MAP If an attempt to do so is made an alert message Are you sure...

Page 528: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A D 6 APPENDIX D BLANK PAGE...

Page 529: ...DB non directional radio beacon VOR VOR DME VOR ILS VORTAC TACAN LINE SYMBOLS Item Symbol ICAO Control Area Class B Airspace Mode C Tower Area Warning Area Alert Area Caution Area Danger Area Prohibit...

Page 530: ...af c Enabled User Waypoint Vertical Navigation Along Track Waypoint Parallel Track Waypoint Unanchored Flight Path Waypoint Top of Descent TOD Bottom of Descent BOD Navigating using Dead Reckoning STO...

Page 531: ...aircraft altitude Black Terrain more than 1000 ft below the aircraft altitude Figure E 1 TAWS Color Chart Figure E 2 TAWS Potential Impact Points Unlighted Obstacle Lighted Obstacle Obstacle Color Obs...

Page 532: ...lay enabled Stormscope display enabled NEXRAD display enabled Cloud Top display enabled Echo Top display enabled XM Lightning display enabled Cell Movement display enabled SIGMETs AIRMETs display enab...

Page 533: ...ing 5 105 WAAS 7 45 Approach Mode 7 29 7 44 7 45 APR softkey 5 104 5 110 Arc HSI 2 14 Arrival procedure5 59 5 71 5 99 5 101 5 102 5 104 5 127 5 129 5 137 Attitude 1 1 Attitude Heading Reference System...

Page 534: ...5 143 Display backup 1 17 4 5 DME audio 4 17 DME Information Window 2 17 DME tuning 4 25 E Emergency frequency 4 38 Engine Indication System EIS 3 1 3 10 Entering Flight ID 4 26 Estimated Landing Fue...

Page 535: ...con Annunciations 2 31 MASQ processing 4 1 Measurement units changing displayed 1 39 Menus 1 29 Messages Reminder 1 46 Message advisoriesA 3 A 8 A 9 A 10 A 11 A 12 A 14 A 15 A 16 A 17 A 18 A 19 MET A...

Page 536: ...4 SafeTaxi database 8 5 SBAS 5 114 5 116 5 117 Scheduler 1 46 1 47 8 1 8 2 8 55 SD card 1 14 Sector scan 6 45 Secure Digital SD card B 1 Selected Altitude 2 2 2 9 2 32 7 9 7 10 7 12 7 13 7 15 7 20 Sel...

Page 537: ...2 Vertical navigation 5 92 Direct to 5 91 5 92 Vertical Navigation ight control 7 15 7 19 Vertical Path Tracking Mode 7 16 7 17 7 41 Vertical scan 6 42 6 43 Vertical speed guidance 5 93 Vertical Speed...

Page 538: ...Garmin G1000 Pilot s Guide for the Hawker Beechcraft C90A GT 190 00663 00 Rev A I 6 INDEX BLANK PAGE...

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