Page 1 Hawker Beechcraft C90A/GT...
Page 2 Except as expressly provided herein, no part 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 permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Page 3 Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole discretion.
Page 4 Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be WARNING: relied upon as the sole source of obstacle and terrain avoidance information.
Page 5 The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.
Page 6 WARNINGS, CAUTIONS, AND NOTES The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by CAUTION: an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.
Page 7 REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00663-00 9/21/07 i – I-6 Initial Release 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 8: Table Of Contents
Transponder Controls ..........2-29 G1000 Alerting system ........4-27 Transponder Mode Selection ........2-31 Marker Beacon Annunciations ........4-30 Entering a Transponder Code ..........2-31 Trafﬁc Annunciation ............4-31 IDENT Function ........2-32 TAWS Annunciations (Optional) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 9 Safe Operating Distance s..............5-41 ...........6-34 Basic Antenna Tilt Setup ............5-43 User Waypoints ......6-36 Weather Mapping and Interpretation 5.4 Airspaces .............5-48 ......6-49 Ground Mapping and Interpretation 5.5 Direct-to-Navigation .........5-53 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 10 Glideslope Mode (GS) ............8-51 Using XM Radio ....7-23 Takeoff (TO) and Go Around (GA) Modes 8.5 Scheduler.............8-55 7.4 Lateral Modes.............7-24 8.6 Abnormal Operation ..........8-57 ..........7-25 Roll Hold Mode (ROL) viii Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 11 TAWS ALERTS .........A-22 Other G1000 Aural Alerts SD Card Use ..............B-1 ...........B-1 Jeppesen Databases .............B-2 Garmin Databases Glossary................C-1 Frequently Asked Questions .........D-1 Map Symbols ..............E-1 INDEX Index ................I-1 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 12 TABLE OF CONTENTS LANK Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 13: Section 1 System Overview
In the Hawker Beechcraft C90A/GT, the GFC 700 Automated Flight Control System (AFCS) provides the ﬂight director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 14: Line Replaceable Units (Lru)
Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA 63Ws are not paired together and do not communicate with each other directly. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 15 • GMU 44 (2) – Measures local magnetic ﬁeld. Data is sent to the GRS 77 for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77, using an RS-485 digital interface. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 16 MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the GDL 69A capability. • GWX 68 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A, via HSDB connection. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 17 GIA 63W. The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to the mechanical ﬂight-control surface linkage. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 18 GSA 80 Servo Management Servo Management (Pitch) GSA 80 (Roll) GTX 33 GTX 33 GSA 80 (Yaw) GEA 71 #1 GEA 71 #2 Figure 1-1 G1000 System (LRU Conﬁguration) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 19: G1000 Controls
The G1000 system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD CONTROLS Figure 1-2 PFD Controls Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 20 If a ﬂight plan is not used, both the desired airport and the desired procedure may be selected. ENT Key – Validates or conﬁrms a menu selection or data entry. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 21: Controls Associated With The Mfd
Theses procedures can then be loaded into the active ﬂight plan. If a ﬂight plan is not used, both the desired airport and the desired procedure may be selected. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 22: Afcs Controls
The GFC 700 AFCS is mainly controlled through the GMC 710 AFCS Control Unit. The AFCS Control Unit consists of the following controls: HDG Key – Selects/deselects Heading Select Mode. APR Key – Selects/deselects Approach Mode. NAV Key – Selects/deselects Navigation Mode. 1-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 23 Switch, and MEPT (Manual Electric Pitch Trim) Switch are additional AFCS controls and are located in the cockpit, separately from the AFCS Control Unit. These are discussed in detail in the AFCS section. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 24: Audio Panel Controls
COM2 Key, or COM1 can be added by pressing the COM1 Key. COM2 – When selected, audio from the #2 COM receiver can be heard. 1-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 25 MSTR Knob – The Master Volume Control adjusts volume for the blended NAV, COM, and intercom audio. Reversionary Mode Button – Pressing manually selects Reversionary Mode. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-13...
Page 26: Secure Digital Cards
Figure 1-6 Display Bezel SD Card Slots 1.5 SYSTEM POWER-UP Refer to the Appendices for AHRS initialization bank angle limitations. NOTE: See the Appendices for additional information regarding system-speciﬁc annunciations and alerts. NOTE: 1-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 27 (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information and displays the Auxiliary (AUX) Weight Planning Page. Figure 1-7 PFD Initialization Figure 1-8 MFD Power-up Page Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-15...
Page 28: System Operation
(see Figure 1-10). Transition to reversionary mode should be straightforward for the pilot, for ﬂight parameters are presented in the same format as in normal mode. 1-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 29: Ahrs Operation
Figure 1-12 Inoperative Input (NAV1 Shown) AHRS OPERATION Refer to the Appendices for speciﬁc AHRS alert information. NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy. NOTE: Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-17...
Page 30 GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both GPS inputs fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer inputs are available and valid. 1-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 31: G1000 System Annunciations
(Figure 1-14 displays all possible ﬂags and responsible LRUs). Upon G1000 power-up, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of power-up. If any window remains ﬂagged, the G1000 system should be serviced by a Garmin- authorized repair facility.
Page 32: Softkey Function
Displays Stormscope information on Inset Map (optional) STRMSCP Displays NEXRAD weather and coverage on Inset Map (optional) NEXRAD Displays XM lightning information on Inset Map (optional) XM LTNG 1-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 33 Selects the #1 transponder as active XPDR1 Selects the #2 transponder as active XPDR2 Selects standby mode (transponder does not reply to any interrogations) STBY Selects Mode A (transponder replies to interrogations) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-21...
Page 34 Figure 1-16 Top Level PFD Softkeys (optional) ALERTS (optional) (optional) (optional) STRMSCP ALERTS Select the BACK Softkey to return to the top-level softkeys. Figure 1-17 INSET Softkeys 1-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 35 Select the BACK Softkey to return to the top-level softkeys METERS ALERTS 360 HSI ARC HSI ALERTS ALERTS SNGL CUE X POINTR ALERTS Figure 1-19 PFD Conﬁguration Softkeys Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-23...
Page 36 DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active ﬂight plan When available, displays optional airport and terminal procedure charts SHW CHRT When available, displays optional checklists CHKLIST 1-24 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 37: Gps Receiver Operation
1) Use the large FMS Knob to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-25...
Page 38 45° above the horizon, and the center point showing the position directly overhead. 1-26 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 39 “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be ﬂown. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 40 8) Use the FMS Knob to enter an arrival date and press the ENT Key. 9) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: 1-28 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 41: Accessing G1000 Functionality
The main controls used in association with all window/page group operations are described in section 1.3. Softkey selection does not display menus or submenus. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 42: Mfd Page Groups
In the bottom right corner of the screen, the current page group, number of pages available in the group, and placement of the current page within the group are indicated. Page Groups Pages in Current Group Selected Page Figure 1-25 Page Group Icons 1-30 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 43 Map Pages (MAP) Navigation Map Trafﬁc Map Weather Radar Stormscope®(optional) Weather Data Link (service optional) Terrain Proximity Figure 1-26 Map Pages Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-31...
Page 44 Trip Planning Utility GPS Status System Setup XM Satellite pages - XM Information Satellite (INFO Softkey) Pages - XM Radio (RADIO Softkey) System Status Figure 1-28 Auxiliary Pages 1-32 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 45 Active Flight Plan - Wide View, Narrow View (VIEW Softkey) Flight Plan Catalog Stored Flight Plan (NEW Softkey) Narrow and Wide View Figure 1-30 Flight Plan Pages Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-33...
Page 46: Mfd System Pages
(see the Audio Panel and CNS Section) • Arrival alerts (see the Flight Management Section) • Criteria for displaying nearest airports (see the Flight Management Section) • Audio alerts 1-34 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 47 1) Select the AUX - System Setup Page. 2) Press the DFLTS Softkey; or press the MENU Key, highlight ‘Restore Defaults’, and press the ENT Key. Figure 1-32 System Setup Page Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-35...
Page 48 5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to conﬁrm selection. Figure 1-34 Date/Time Settings (System Setup Page) 1-36 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 49 6) In the next ﬁeld, use the small FMS Knob to select the desired settings upon which to base the new proﬁle. Proﬁles can be created based on Garmin factory defaults, default proﬁle settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings.
Page 50 6) Press the ENT Key. 7) With ‘DELETE’ highlighted, press the ENT Key. 8) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. 1-38 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 51 HDDD°MM’SS.S” MGRS UTM/UPS * Default setting ** Contact a Garmin-authorized service center to change this setting *** Not conﬁgurable Table 1-1 Display Units Settings (System Setup Page) Changing a display unit setting 1) While on the System Setup Page, press the FMS Knob momentarily to activate the ﬂashing cursor.
Page 52 2) Turn the large FMS Knob to highlight the voice in the Audio Alert Box. 3) Turn the small FMS Knob to display and highlight the desired voice and press the ENT Key. 1-40 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 53 The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and a service center or Garmin dealer informed.
Page 54 If the timer is reset before reaching zero on a countdown, the digits are reset to the initial value. If the timer is counting up when reset, the digits are zeroed. 1-42 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 55 6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The ﬁeld changes to ‘RESET?’. 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The ﬁeld changes back to ‘START?’ and the digits are reset. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-43...
Page 56 3) Turn the large FMS Knob to highlight the ﬁeld next to the departure time. 4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and pr ess the ENT Key. 1-44 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 57 2) Use the FMS Knob to highlight the desired reset option and pr ess the ENT Key. The selected parameters are reset to zero and begin to display data from the point of reset. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 58 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next ﬁeld. 8) For periodic and one-time message, use the FMS Knob to enter the timer value (HHH:MM:SS) from which to countdown and press the ENT Key. 1-46 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 59 The softkey reverts to the ‘ALERTS’ label and when pressed, the Alerts Window is removed from the display and the scheduler message is deleted from the message queue. Figure 1-42 PFD Alerts Window Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A 1-47...
Page 60: Display Backlighting
6) Use the FMS Knob to enter the desired backlighting and press the ENT Key. 7) To remove the menu, press the CLR or MENU Key. Figure 1-43 PFD Setup Menu 1-48 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 61: Section 2 Flight Instruments
• System time – Selected Altitude • Wind data • Vertical Deviation, Glideslope, and • Vertical Navigation indications Glidepath Indicators The PFDs also display various alerts and annunciations. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 62 COM Frequency Box Softkeys AFCS Status Box System Time Navigation Status Box Transponder Data Box Slip/Skid Indicator Selected Heading Bug Attitude Indicator Figure 2-1 Primary Flight Display (Default) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 63 Vertical Deviation Indicator (VDI) DME Information Window (optional) Comparator Window Bearing Information Windows Current VNV Target Altitude Minimum Descent Altitude/ AFCS Status Annunciation Decision Height Figure 2-2 Additional PFD Information 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 64: Airspeed Indicator
, the text of the actual airspeed readout changes to yellow while the pointer remains black. The trend vector is absent if the speed remains constant or if any data needed to calculate airspeed is not available due to a system failure. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 65 The maximum speed with approach ﬂaps is displayed as a solid white triangle to the right of the airspeed scale. This indication is always displayed and cannot be turned off by the pilot. Figure 2-6 Maximum Flaps Extended Speed Reference 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 66 3) Turn the FMS Knob to highlight the desired selection. 4) Press the ENT Key. 5) To remove the window, press the CLR Key or the TMR/REF Softkey. Figure 2-8 Page Menu (Timer/References Window) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 67: Attitude Indicator
Or : Press the X POINTR Softkey to display Command Bars as a cross pointer (Aircraft Symbol in Figure 2-11). Figure 2-10 Aircraft Symbol for Single Cue Command Bars 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 68 Slip/skid is indicated by the location of the bar relative to the pointer. One bar displacement is equal to one ball displacement on a traditional Slip/Skid Indicator. Figure 2-12 Slip/Skid Indication Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 69: Altimeter
2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to turn on metric altitude readouts. 4) Press the BACK Softkey to return to the top-level softkeys. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 70 Or, press the HPA Softkey to display the barometric pressure setting in hectopascals (hPa; see Figure 2-14). 4) Press the BACK Softkey to return to the top-level softkeys. 2-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 71: Vertical Speed Indicator (Vsi)
Target Altitude once the “TOD [Top of Descent] within 1 minute” alert has been generated. See the Flight Management Section for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information about VNV indications on the PFD. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-11...
Page 72: Vertical Deviation
Indicator Deviation Speed Indicator Indicator Pointer Required Vertical Speed Figure 2-17 Glideslope Indicator Figure 2-18 Glidepath Indicator Figure 2-16 Vertical Speed and Deviation Indicators (VSI and VDI) 2-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 73: Horizontal Situation Indicator (Hsi)
Flight Phase Aircraft Symbol Lubber Line Course Deviation Indicator Turn Rate/Heading (CDI) Trend Vector Current Heading Rotating Compass Rose OBS Mode Active Figure 2-19 Horizontal Situation Indicator (HSI) 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-13...
Page 74 (see OBS Mode for adjusting a GPS course). Current Track Bug Current Heading Selected Heading Selected Course Selected Heading Bug Figure 2-21 Heading and Course Indications 2-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 75 • TRUE - References angles to true north (denoted with ‘T’) • MAGNETIC - Angles corrected to the computed magnetic variation (‘Mag Var’) Figure 2-23 System Setup Page, Navigation Angle Settings 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-15...
Page 76 Bearing Source Identiﬁer Selected Bearing Pointer Pointer Bearing Source Icon Icon Source Bearing 1 Information Window Bearing 2 Information Window Figure 2-25 HSI with Bearing and DME Information 2-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 77 2) Press the DME Softkey to display the DME Information Window above the BRG1 Information Window. 3) To remove the DME Information Window, press the DME Softkey again. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-17...
Page 78: Course Deviation Indicator (Cdi)
CDI. If the CDI exceeds the maximum deviation on the scale (two dots) while displaying GPS, the crosstrack error (XTK) is displayed below the white aircraft symbol. Navigation Source Selected on Both PFDs Figure 2-27 Navigation Sources 2-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 79 3) Select the CDI Softkey a third time to return to GPS. NAV1 Selected NAV2 Selected for Tuning for Tuning LOC1 VOR2 Selected Selected Selected CDI Softkey Cycles Through Navigation Sources Figure 2-28 Selecting a Navigation Source 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-19...
Page 80 • The ﬁnal approach ﬁx (FAF) is the active waypoint, the FAF is less than 15 nm away, and the aircraft is moving toward the FAF • A valid localizer frequency has been tuned • The GPS CDI deviation is less than 1.2 times full-scale deﬂection 2-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 81 When set to ‘Auto’ (default), the GPS CDI scale automatically adjusts to the desired limits based upon the current phase of ﬂight (Figure 2-31, 2-32, 2-33, Table 2-2). 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-21...
Page 82 - If the active waypoint is part of the missed approach procedure, the active leg and preceding missed approach legs must be aligned with the ﬁnal approach segment course and the aircraft must not have passed the turn initiation point. 2-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 83 1.0 nm decreasing to a speciﬁed course width, then 0.3 nm, depending on variables (see Figure 2-31) Approach (LPV) Missed Approach MAPR 0.3 nm Table 2-2 Automatic GPS CDI Scaling 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-23...
Page 84 Extended Course Line Mode Enabled Pressing the OBS Pressing the OBS Softkey Again Returns Softkey Suspends to Normal Operation Waypoint Sequencing Figure 2-34 Omni-bearing Selector (OBS) Mode 2-24 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 85 ‘SUSP’ appears on the HSI (to the lower right of the aircraft symbol) in place of ‘OBS’ and the OBS Softkey label changes to SUSP. SUSP Softkey Suspends SUSP Waypoint Sequencing Annunciation Figure 2-35 Suspending Automatic Waypoint Sequencing 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-25...
Page 86: Supplemental Flight Data
The Outside Air Temperature (OAT) is displayed in degrees Celsius (°C) by default in the lower left of the PFD under normal display conditions, or below the true airspeed in reversionary mode. Normal Display Reversionary Mode Figure 2-36 Outside Air Temperature 2-26 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 87: Wind Data
• OPTN 2: Total wind direction and speed • OPTN 3: Total wind direction with head and crosswind speed components 4) To remove the window, press the OFF Softkey. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-27...
Page 88: Vertical Navigation (Vnv) Indications
Active altitude-constrained waypoint can not be reached within maximum allowed ﬂight path angle and vertical speed Last altitude-constrained waypoint in active ﬂight plan reached (30 sec before) Table 2-3 VNV Indication Removal Criteria 2-28 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 89: Pfd Annunciations And Alerting Functions
ﬂashes and the appropriate aural alert sounds until acknowledged by pressing the softkey. The softkey then reverts to the ALERTS Softkey label, and when selected again opens the Alerts Window to display a descriptive message of the alert. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-29...
Page 90 PFD. With certain types of sensor failures, the G1000 may make some sensor selections automatically. The GPS sensor cannot be switched manually. Figure 2-42 Reversionary Sensor Window 2-30 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 91: Marker Beacon Annunciations
TAS documentation for alerts generated by TAS equipment) If additional TAs appear, new aural and visual alerts are generated. Trafﬁc Symbols Figure 2-44 Inset Map with Trafﬁc Displayed 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-31...
Page 92: Taws Annunciations (Optional)
Altitude), the Selected Altitude changes to yellow text on a black background, ﬂashes for 5 seconds, and an aural tone is generated. Within 1000 ft Within 200 ft Deviation of ±200 ft Figure 2-46 Altitude Alerting Visual Annunciations 2-32 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 93: Low Altitude Annunciation
• Once the aircraft reaches the MDA/DH, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated. Within 2500 feet Within 100 feet Altitude Reached MDA/DH Bug MDA/DH Setting Figure 2-48 Minimum Descent Altitude/Decision Height Alerting Visual Annunciations 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-33...
Page 94 Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the setting for the alert. If the aircraft proceeds to climb after having reached the MDA/DH, once it reaches 50 feet above the MDA/DH, alerting is disabled. 2-34 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 95: Abnormal Operations
• Wind Data (calculated based on GPS information) • Distances in the Bearing Information windows • GPS bearing pointers These items should be veriﬁed when operating in Dead Reckoning Mode. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 2-35...
Page 96: Unusual Attitudes
• DME Information Window • VNV Target Altitude (optional) – Alerts • Wind data – Procedures • Transponder Status Box – DME Tuning (optional) • System Time 2-36 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 97: Section 3 Engine Indication System
If the sensor data for a parameter becomes invalid or unavailable, a red “X” is displayed across the indicator and/or readout. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 98: Eis Display
The gauges displayed and the values shown in this section are taken from the Hawker Beechcraft NOTE: C90A/GT baseline conﬁguration. Refer to the Pilot’s Operating Handbook (POH) and FAA Approved Airplane Flight Manual (AFM) for speciﬁc values and operating limitations. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 99 ENGINE INDICATION SYSTEM C90A/GT Baseline Conﬁguration Figure 3-2 EIS Display 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 100: Interstage Turbine Temperature
0 FT-LB to 1600 FT-LB If the torque remains above 1315 FT-LB for more than 2 seconds or exceeds the value indicated by the red tick mark, a warning condition occurs. Figure 3-4 Torque Gauge Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 101: Tachometer (Rpm)
Figure 3-5 Tachometer with Propellers Synchronized Figure 3-6 Tachometer with Propellers Out of Sync (less than 50 rpm) Figure 3-7 Tachometer with Propellers Out of Sync (greater than or equal to 50 rpm) 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 102: Turbine Speed
The Fuel Flow Gauge is displayed beneath the Turbine Speed gauge. Fuel Flow is displayed in pounds per hour (pph) from 0 to 600 pph. Figure 3-9 Fuel Flow Gauge Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 103: Oil Pressure
The Oil Temperature Gauge is located beneath the Oil Pressure gauge. Oil temperature is displayed in degrees Celsius (°C). Safe operating range for oil temperature is 0 to 99° C Figure 3-11 Oil Temperature Gauge 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 104: Eis Display In Reversionary Mode
• PFD2 failure – Press the Display Backup button on the right Audio Panel. MFD enters reversionary mode; PFD1 remains in normal mode. Figure 3-13 Display Backup Button Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 105: Reversionary Display
C90A/GT baseline conﬁguration. Refer to the Pilot’s Operating Handbook (POH) and FAA Approved Airplane Flight Manual (AFM) for speciﬁc values and operating limitations. C90A/GT Baseline Conﬁguration Figure 3-14 EIS Reversionary Mode Display 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 106 ENGINE INDICATION SYSTEM LANK 3-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 107: Section 4 Audio Panel And Cns
Audio Panel for the respective crew position. In addition, the master volume control for each Audio Panel affects all other system audio output to its designated crew position headset much like volume adjustments found on many aviation headsets. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 108: Pfd Controls And Frequency Display
AUDIO PANEL AND CNS PFD CONTROLS AND FREQUENCY DISPLAY Figure 4-1 PFD Controls, NAV/COM Frequency Tuning Boxes, and DME Tuning Window Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 109 The large knob moves the cursor in the window. The small knob selects individual characters for the highlighted cursor location. Transponder Data Box – Indicates the selected transponder code, operating mode, reply, and ident status for the applicable transponder. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 110: Audio Panel Controls
#2 COM receiver to be heard. COM1 receive can be added by pressing the COM1 Key. COM2 – When selected, audio from the #2 COM receiver can be heard. COM3 MIC – Reserved for optional COM radio. Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 111 VOL or SQ. The MAN SQ Key must be selected to allow squelch adjustment. MSTR Knob – The Master Volume Control adjusts volume for the blended NAV, COM, intercom audio, and alert warnings. DISPLAY BACKUP Button – Manually selects Reversionary Mode. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 112: Com Operation
Audio Panel Tuning Box COM2 Radio is Selected on the Audio Panel Figure 4-3 Selecting a COM Radio for Transmit COM3 is reserved for an optional COM radio. Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 113: Com Transceiver Manual Tuning
Automatic Squelch On or Off Key to Transfer COM Frequencies Between Active and Standby Frequency Boxes Turn the COM Knob to Tune the Frequency in the Tuning Box Figure 4-5 COM Frequency Tuning 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 114: Quick-Tuning And Activating 121.500 Mhz
In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver. Press for Two Seconds to Load 121.500 MHz Figure 4-7 Quickly Tuning 121.500 MHz Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 115: Auto-Tuning The Com Frequency
4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Select the NRST Softkey to Open the Nearest Airports Window Figure 4-8 Nearest Airports Window (PFD) 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 116 Knob to Scroll Press the ENT Key to Load a Through a List Highlighted Frequency into the of Frequencies. COM Standby Frequency Box. Figure 4-9 Frequency Auto-Tuning from the MFD 4-10 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 117 6) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Nearest Airports Menu Nearest Frequencies Menu Nearest Airspaces Menu Figure 4-10 Nearest Pages Menus 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-11...
Page 118 PFD1 COM Standby Field. Cursor then advances to the next frequency. Select INFO Softkey for AIRPORT, RUNWAYS, and FREQUENCIES Windows Figure 4-11 WPT – Airport Information Page 4-12 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 119 NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key. Figure 4-12 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-13...
Page 120: Frequency Spacing
While the COM CONFIG Window is selected, the G1000 softkeys are blank. Select 8.33-kHz or 25.0-kHz COM Frequency Channel Spacing AUX - SYSTEM SETUP PAGE Figure 4-14 AUX – System Setup Page 4-14 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 121: Automatic Squelch
Volume level indication remains for two seconds after the change. COM Volume Level Remains for Two Seconds Figure 4-16 COM Volume Level 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-15...
Page 122: Nav Operation
Figure 4-17 Selecting a NAV Radio for Navigation See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR or ADF as the source for the bearing pointer. 4-16 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 123: Nav Receiver Manual Tuning
Press the Frequency Transfer Key to Transfer NAV Frequencies Between Active and Standby Frequency Fields Turn the NAV Knob to Tune the Frequency in the Tuning Box Figure 4-19 NAV Frequency Tuning 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-17...
Page 124 When adjusting, the level is displayed in place of the standby frequencies. Volume level indication remains for two seconds after the change. NAV Volume Level Remains for Two Seconds Figure 4-22 NAV Volume Level 4-18 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 125: Auto-Tuning A Nav Frequency From The Mfd
Press the ENT Key to Load a Through a List Highlighted Frequency into the of Frequencies. NAV Standby Frequency Box. Figure 4-23 NAV Frequency Auto-Tuning from the MFD 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-19...
Page 126 5) Press the ENT Key to load the NAV frequency into the standby ﬁeld of the selected NAV radio. 6) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. Nearest Airports Menu Nearest VOR Menu Figure 4-24 Nearest Pages Menus 4-20 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 127 Place the Cursor on to Place the Cursor on the VOR Frequency the VOR Identiﬁer Figure 4-25 Loading the NAV Frequency from the NRST – Nearest VOR Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-21...
Page 128 MENU Key, the FMS Knob, and the ENT Key. Figure 4-26 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and NRST – Nearest Airports Pages 4-22 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 129 NAV2 standby frequency ﬁeld, the standby frequency is transferred to active. • If the current CDI navigation source is NAV1 or NAV2, the approach frequency is transferred to the standby frequency ﬁelds of the selected CDI NAV radio. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-23...
Page 130: Marker Beacon Receiver
(annunciator illuminated) is used to provide an earlier indication when nearing a marker during an approach. The LO SENS function (annunciator extinguished) results in a narrower marker dwell while over a station. 4-24 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 131 DME tuning state. Pressing the FMS Knob activates/deactivates the cursor in the DME Tuning Window. See the Flight Instruments Section for displaying the DME information window. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-25...
Page 132: Gtx 33 Mode S Transponders
Selecting the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the top-level softkeys. After 45 seconds of transponder control inactivity, the system reverts back to the top-level softkeys. 4-26 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 133: Transponder Mode Selection
The STBY, ON , and ALT Softkeys can be accessed by selecting the XPDR Softkey. Selecting a transponder mode: 1) Select the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Select the desired softkey to activate the transponder mode. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-27...
Page 134 Mode C altitude reporting is inhibited. In ON Mode, a green ON indication and transponder code appear in the mode ﬁeld of the Transponder Data Box. ON Mode (No Altitude Reporting) Figure 4-33 ON Mode 4-28 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 135 When the transponder sends replies to interrogations, a white R indication appears momentarily in the reply status ﬁeld of the Transponder Data Box. Reply to Interrogation Figure 4-35 Reply Indication 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-29...
Page 136: Entering A Transponder Code
Turn the Large Enter Two Code FMS Knob Digits at a Time to Move the Cursor to the Next Code Field Figure 4-37 Entering a Code with the FMS Knob 4-30 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 137: Ident Function
After the IDENT Softkey is selected while in Mode or Code Selection, the system reverts to the top-level softkeys. IDNT Indication Select the IDENT Softkey to Initiate the ID Function Figure 4-39 IDENT Softkey and Indication 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-31...
Page 138: Additional Audio Panel Functions
Aural alerts are always present on the headset and are on the speaker when the SPKR is selected. These warnings and the aircraft radios are not heard on the passenger headphones. 4-32 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 139: Intercom
Turn to adjust Squelch Control for Pilot when SQ Annunciation Side or Copilot is lit, Volume when Side VOL Annunciation is lit. Volume Annunciation Squelch Annunciation Figure 4-41 Intercom Controls 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-33...
Page 140: Passenger Address (Pa) System
COM MIC Annunciator ﬂashes when either pilot’ s microphone PTT is pressed. If both pilots select the same COM radio, the pilot has priority on COM1 and the copilot has priority on COM2. 4-34 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 141: Clearance Recorder And Player
Each subsequent two presses of the PLAY Key within one-half second backtrack through the recorded memory blocks to reach and play any recorded block. Powering off the unit automatically clears all recorded blocks. Figure 4-43 Record and Playback Key 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-35...
Page 142: Audio Panels Preﬂight Procedure
Audio Panel for the respective crew position. The master volume control for each Audio Panel affects all other system audio output for the pilot or copilot headset. 4-36 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 143 Knobs Adjust Radio Level COM Radio Master Volume Audio Knobs Adjust Headphone Volume Level NAV Radio Audio Copilot Master Volume Control Figure 4-45 Radio and Headphone Volume Controls 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-37...
Page 144: Abnormal Operation
In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is automatically tuned in the radio in which the tuning failure occurred. Emergency Channel Loaded Automatically Figure 4-47 COM Tuning Failure 4-38 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 145: Pfd Failure, Dual System
121.500 MHz, but the frequency is not shown. The COM2 emergency frequency is available to both the copilot and pilot. Figure 4-55 PFD1 Display after PFD2 Failure 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 4-39...
Page 146: Audio Panel Fail-Safe Operation
COM1 and NAV1. REVERSIONARY MODE The red DISPLAY BACKUP Button selects the Reversionary Mode. See the System Overview Section for more information on Reversionary Mode. Figure 4-48 Reversionary Mode Button 4-40 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 147: Section 5 Flight Management
The Direct-to Window, the Flight Plan Window, the Procedures Window, and the Nearest Airports Window can be displayed in the lower right corner of the PFD. Details of these windows are discussed in detail later in the section. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 148: Flight Plan Window
- Topographic Data - Hazard Data Flight Plan Leg Aircraft Icon Active Flight Plan Leg at Present Position Map Range Figure 5-2 GPS Navigation Information on the MFD Navigation Page Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 149: Navigation Status Box
2) Press the FMS Knob momentarily to activate the ﬂashing cursor. 3) Turn the large FMS Knob to highlight the desired ﬁeld number in the MFD Data Bar Fields Box. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 150: Using Map Displays
(track up, desired track up, or heading up). The map orientation is shown in the upper right corner of the map. Figure 5-3 Map Orientation Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 151 2) Select the ENT Key to display the Map Setup Window. 3) Turn the large FMS Knob, or select the ENT Key once, to select the ‘ORIENTATION’ ﬁeld. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 152: Map Range
To change the map range turn the Joystick counter-clockwise to decrease the range, or clockwise to increase the range. Range Overzoom Figure 5-6 Map Range Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 153 • When the maximum ‘look forward’ time is set to zero, the upper limit becomes the maximum range available (2000 nm). • When the minimum ‘look forward’ time is set to zero, the lower limit becomes 1.5 nm. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 154 9) Repeat step 8 for ‘MIN LOOK FWD’ (zero-99 minutes) and ‘MAX LOOK FWD’ (zero to 999 minutes). 10) Press the FMS Knob to return to the Navigation Map Page. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 155: Map Panning
The map is normally centered on the aircraft’s position. If the map has been panned and there has NOTE: been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position and the ﬂashing pointer is removed. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 156 When any map feature or object is selected on the map display, pertinent information is displayed. Information about Point of Interest Map Pointer on Figure 5-9 Navigation Map - Map Pointer on Point of Interest 5-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 157 2) Move the Joystick to move the Map Pointer around the map. 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-11...
Page 158 3) Press the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page and return to the Navigation Map showing the selected waypoint. NAVAID Information GO BACK Softkey Figure 5-11 Navigation Map - Information Window - NAVAID 5-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 159 Information Page for the selected airspace. 4) Press the CLR or ENT Key to exit the Airspace Information Page. Airspace Information Figure 5-12 Navigation Map - Information Window - Airspace 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-13...
Page 160: Measuring Bearing And Distance
5) To exit the Measure Bearing/Distance option, press the Joystick; or select ‘Stop Measuring’ from the Page Menu and press the ENT Key. Measurement Pointer Lat/Long Information Measurement Line Figure 5-13 Navigation Map - Measuring Bearing and Distance 5-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 161: Topography
4) Press the ENT Key. 5) Highlight the ‘TOPO DATA’ ﬁeld. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-15...
Page 162 In addition, the Navigation Map can display a topographic scale (located in the lower right hand side of the map) showing a scale of the terrain elevation and current elevation values as shown following. 5-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 163 5) Select ‘On’ or ‘Off’. 6) Press the FMS Knob to return to the Navigation Map Page. TOPO SCALE On/Off Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-17...
Page 164: Map Symbols
LARGE CITY (> 200,000) 1500 MEDIUM CITY (> 50,000) SMALL CITY (> 5,000) States and Provinces (STATE/PROV) 1500 Rivers and Lakes (RIVER/LAKE) USER WAYPOINT Table 5-1 Land Symbol Information 5-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 165 Class D Airspace (CLASS D) Restricted Area (RESTRICTED) Military Operations Area [MOA(MILITARY)] Other/Air Defense Interdiction Zone (OTHER/ADIZ) Temporary Flight Restriction (TFR) 2000 Table 5-2 Aviation Symbol Information 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-19...
Page 166 5) Select the desired land option. 6) Select the desired text size. 7) Press the ENT Key to accept the selected size. 6) Select the desired range. 5-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 167 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map removes the same item at 50 nm). 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-21...
Page 168 Decluttering the PFD Inset Map: 1) Press the INSET Softkey. 2) Select the DCLTR Softkey. The current declutter level is shown. With each selection, another level of map information is removed. 5-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 169 Class C Airspaces/TCA Class D Airspaces Other Airspaces/ADIZ TFRs Obstacles Airways Land/Country Text Cities Roads Railroads State/Province Boundaries River/Lake Names Table 5-3 Navigation Map Items Displayed by Declutter Level 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-23...
Page 170: Airways
When airways are selected for display on the map, the airway waypoints (VORs, NDBs and Intersections) are also displayed. Low Altitude Airway (Victor Airway) High Altitude Airway (Jet Route) Figure 5-22 Airways on MFD Navigation Page 5-24 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 171 7) Select the desired range using the small FMS Knob. 8) Press the ENT Key. 9) Press the FMS Knob to return to the Navigation Map Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-25...
Page 172: Track Vector
ﬁeld. Use the FMS Knob to select the desired time. Press the ENT Key. 7) Press the FMS Knob to return to the Navigation Map Page. 5-26 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 173: Wind Vector
4) Press the ENT Key. 5) Highlight the ‘WIND VECTOR’ ﬁeld. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-27...
Page 174: Nav Range Ring
7) Press the FMS Knob to return to the Navigation Map Page. The Nav Range Ring is referenced to either magnetic or true north, based on the selection on the AUX NOTE: - System Setup Page. 5-28 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 175: Fuel Range Ring
8) To change the reserve fuel time, enter a time (00:00 to 23:59; hours:minutes). The default setting is 00:45 minutes. 9) Press the ENT Key. 10) Press the FMS Knob to return to the Navigation Map Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-29...
Page 176: Waypoints
FMS Knob during the selection process. If duplicate entries exist for an identiﬁer, a Duplicate Waypoints Window is displayed when the ENT Key is pressed. 5-30 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 177: Airports
In addition to displaying a map of the currently selected airport and surrounding area, the Airport Information Page displays airport information in three boxes labeled ‘AIRPORT’, ‘RUNWAYS’, and ‘FREQUENCIES’. For airports with multiple runways, information for each runway is available. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-31...
Page 178 3) Turn the small FMS Knob to display the desired runway (if more than one) for the selected airport. 4) To remove the ﬂashing cursor, press the FMS Knob. 5-32 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 179 Approach Available Type Length of Longest Runway COM Freq. Info. - Identiﬁcation - Frequency Additional Airports (within 200 nm) NRST Softkey Figure 5-32 Nearest Airports Window on PFD 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-33...
Page 180 If there are no items for display in a boxed area, text indicating that fact is displayed. The currently selected airport remains in the list until it is unselected. 5-34 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 181 4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport) 5) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-35...
Page 182 4) Use the FMS Knob to enter the minimum runway length (zero to 99,999 feet) and press the ENT Key. Nearest Airport Criteria - Type of Runway Surface - Minimum Runway Length Figure 5-35 System Setup Page - Nearest Airport Selection Criteria 5-36 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 183: Intersections
2) Press the ENT Key or turn either FMS Knob to select an identiﬁer in the Nearest Intersection Box. 3) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-37...
Page 184 Intersection aircraft position Intersection Lat/Long Reference VOR Info Nearest Intersection - Identiﬁer/Type (symbol) - VOR Frequency - Bearing/Distance to VOR Figure 5-37 Nearest Intersections Page 5-38 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 185: Ndbs
1) With the Nearest NDB Page displayed, enter an identiﬁer, the name of the NDB, or the city in which it’s located in the NDB Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-39...
Page 186 - Bearing/Distance to Showing Selected NDB from aircraft position Nearest NDB NDB Information - Facility Name/City - Type - Lat/Long NDB Frequency Figure 5-39 Nearest NDB Page 5-40 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 187: Vors
2) Highlight ‘SELECT VOR WINDOW’, and press the ENT Key. 3) Enter an identiﬁer, the name of the VOR, or the city in which it’s located in the VOR Box. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-41...
Page 188 - Bearing/Distance to VOR Showing Nearest from aircraft position VOR Information - Facility Name/City - Class/Magnetic Variation - Lat/Long Nearest VOR VOR Frequency Figure 5-41 Nearest VOR Page 5-42 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 189: User Waypoints
Reference Wpt Info - Identiﬁer - Radial/Distance Selected User User Waypoint List Waypoint - Identiﬁer - Comment # User Wpts Used Softkeys Figure 5-42 User Waypoint Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-43...
Page 190 5) Highlight the Information Box and enter the latitude and longitude for the waypoint or highlight the Reference Waypoints Box to enter a bearing and distance from another waypoint or the bearing from two other waypoints to deﬁne the new waypoint location. 5-44 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 191 3) Turn the small FMS Knob to make any changes. 4) Press the ENT Key to accept the changes. 5) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-45...
Page 192 2) Press the MENU Key. 3) Select ‘Auto Comment’. 4) Press the ENT Key. The generated comment is based on the reference point used to deﬁne the waypoint. 5-46 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 193 2) Press the MENU Key. 3) Select ‘Delete All User Waypoints’ 4) Press the ENT Key twice to conﬁrm the selection.. 5) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-47...
Page 194: Airspaces
(Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR). Class D Airspace MOA (Military) Class B Airspace Restricted Area Alert Area Class C Airspace ADIZ Warning Area Figure 5-45 Airspaces 5-48 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 195 3) Turn the large FMS Knob to highlight the desired ﬁeld in the Airspace Alerts Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-49...
Page 196 Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu: See Table 5-2 for the default and maximum ranges for each type of airspace and the symbol used to deﬁne the airspace area. 5-50 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 197 ENT Key. The cursor is placed in the ‘AIRSPACE ALERTS’ Box. 3) Select the desired airspace. 4) Press the FMS Knob to remove the ﬂashing cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-51...
Page 198 ARSPC NEAR – Airspace near – Special use airspace is within 2 nm of the aircraft position. less than 2 nm. Table 5-6 PFD Airspace Alert Messages 5-52 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 199: Direct-To-Navigation
- City - Altitude at Arrival - Along Track Offset Map of Selected Point Location of Destination - Bearing/Distance Desired Course Figure 5-48 Direct-to Window - MFD 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-53...
Page 200 Selecting an active ﬂight plan waypoint as a direct-to destination: 1) While navigating an active ﬂight plan, press the Direct-to Key. The Direct-to Window is displayed with the active ﬂight plan waypoint as the default selection. 5-54 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 201 1) Select the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page. 2) Select the desired airport (the nearest one is already selected). 3) Press the Direct-to Key. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-55...
Page 202 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a ﬂight plan is still active, the G1000 resumes navigating the ﬂight plan along the closest leg. Page Menu - Cancel Direct-To Navigation Figure 5-51 Direct-to Window - Cancelling Direct-to Navigation 5-56 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 203 7) Enter the desired distance along-track before (-) or after (+) the offset waypoint. 8) Press the ENT Key. The ‘Activate?’ ﬁeld is highlighted. 9) Press the ENT Key to activate. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-57...
Page 204 2) Press the MENU Key. 3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key. Page Menu - Clear Vertical Navigation Constraints Figure 5-52 Direct-to Window - Clearing Vertical Constraints 5-58 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 205: Flight Planning
If that happens, the airway waypoints are changed to regular (non-airway) ﬂight plan waypoints, and an alert is displayed (see Miscellaneous System Messages). 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-59...
Page 206: Flight Plan Creation
- Flight Path Angle - Vertical Speed Target - Time to Top of Descent Non-Active, - Vertical Deviation Flight Plan Leg Figure 5-53 Active Flight Plan Page 5-60 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 207 (becomes the active ﬂight plan). Creating an active ﬂight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (only on MFD). 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-61...
Page 208 7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new ﬂight plan is now in the list. 5-62 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 209: Adding Waypoints To An Existing Flight Plan
- Distance to Waypoint - Waypoint Altitude Constraint Softkeys Figure 5-56 Stored Flight Plan Page Flight Plan Full Message Figure 5-57 Active Flight Plan Page - FPL Full 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-63...
Page 210 5) Enter the identiﬁer, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active ﬂight plan is modiﬁed as each waypoint is entered. 5-64 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 211: Adding Airways To A Flight Plan
2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-65...
Page 212 Airway Entry Waypoint Selected Airway Selected Exit Point Preview of Selected Airway Airway Exit Points Selected Airway Exit Available Point Figure 5-60 Select Airway Page - Selecting Exit Point 5-66 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 213 The system only allows correct airway sequences to be inserted. If the pilot subsequently inverts the ﬂight plan, the system inverts the airway waypoint sequence and removes the airway header. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-67...
Page 214: Adding Procedures To A Stored Flight Plan
(arrival), and landing at an airport (approach). See the procedures section for more details. Flight Plan Name Flight Plan Waypoint List Softkeys Load Departure - Load Arrival - Load Approach - Activate Flight Plan Figure 5-62 Stored Flight Plan Page 5-68 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 215 5) Select a transition for the selected departure. Press the ENT Key. 6) Select a runway served by the selected departure, if required. Press the ENT Key. 7) Press the ENT Key to load the selected departure procedure. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-69...
Page 216 Figure 5-64 Departure Loading Page - Selecting Transition Inserted Departure Header - Departure Identiﬁer: [departure airport]-[departure runway]. [departure transition]. [departure end point] (e.g., KMKC-ALL.WLDCT2.SLN) Figure 5-65 Stored Flight Plan Page - Departure Inserted 5-70 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 217 5) Select a transition for the selected arrival. Press the ENT Key. 6) Select a runway served by the selected arrival, if required. Press the ENT Key. 7) Press the ENT Key to load the selected arrival procedure. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-71...
Page 218 Figure 5-67 Arrival Loading Page - Selecting the Transition Inserted Arrival Header - Arrival Identiﬁer: [arrival airport]-[arrival transition]. [arrival].[arrival runway] (e.g., KCOS-TBE.DBRY1.ALL) Figure 5-68 Stored Flight Plan Page - Arrival Inserted 5-72 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 219 4) Select an approach. Press the ENT Key. 5) Select a transition for the selected arrival. Press the ENT Key. 6) Press the ENT Key to load the selected approval procedure. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-73...
Page 220: Flight Plan Storage
G1000 is powered off or when another ﬂight plan is activated. Details about each stored ﬂight plan can be viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page. 5-74 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 221 4) With ‘OK’ highlighted, press the ENT Key. The ﬂight plan is stored in the next available position in the ﬂight plan list on the Flight Plan Catalog Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-75...
Page 222 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired ﬂight plan. 5-76 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 223: Flight Plan Editing
3) With ‘OK’ highlighted, press the ENT Key to delete the active ﬂight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-77...
Page 224 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 5-78 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 225 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-79...
Page 226: Along Track Offsets
An along track offset distance cannot be modiﬁed once entered. If the along track offset distance must be changed, the existing along track offset waypoint must be deleted and a new one created with the new offset distance. 5-80 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 227 4) Enter a positive or negative offset distance in the range of +/- 1 to 99 nm. 5) Press the ENT Key to create the offset waypoint. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-81...
Page 228: Parallel Track
4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL TRACK’ is highlighted. 5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track activation. 5-82 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 229 If the parallel track proposed by the offset direction and distance is not allowed by the system, the activation prompt is displayed, but disabled. Parallel Track cannot be activated if a course is set using direct-to or if the 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-83...
Page 230 Offset Direction & Distance Subdued (Unavailable) Cancel Prompt Active Status Figure 5-78 Cancelling Parallel Track 5-84 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 231: Activating A Flight Plan Leg
4) Press the ENT Key to activate the ﬂight plan leg. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Current Active Leg Selected Destination Waypoint Activate Leg Softkey Figure 5-79 Active Flight Plan Page - Selecting the Leg Destination Waypoint 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-85...
Page 232: Inverting A Flight Plan
6) Press the ENT Key to invert and activate the stored ﬂight plan. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5-86 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 233: Flight Plan Views
3) Press the WIDE Softkey to display the wide view, or press the NARROW Softkey to display the narrow view. 4) Press the BACK Softkey to return to the top level active ﬂight plan softkeys. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-87...
Page 234 “To” or the “Next” waypoint is automatically expanded. When an airway is loaded, airways are automatically expanded to facilitate ﬂight plan review. 5-88 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 235: Closest Point Of Fpl
(DIS) to the closest point along the ﬂight plan to the selected reference waypoint and creates a user waypoint at this location. The name for the new user waypoint is derived from the identiﬁer of the reference waypoint. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-89...
Page 236: Vertical Navigation
CURRENT VNV PROFILE box (defaults ﬁrst waypoint in the active ﬂight plan with an altitude enabled for vertical navigation (e.g., HABUK)). 5-90 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 237 (TOD) point is computed based on the default ﬂight path angle; descent begins once the TOD is reached. Current Vertical Navigation Proﬁle Current Vertical Navigation Proﬁle Prior to VNV Direct-to After VNV Direct-to VNV Direct-To Softkey VNV PROF Softkey Figure 5-85 Vertical Navigation Direct-To 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-91...
Page 238: Altitude Constraints
Small Light Blue Text Cross AT Small Light Blue or BELOW Subdued Text 3,000 ft Altitude Constraint Small White Text with Examples Altitude Restriction Bar Figure 5-86 Waypoint Altitude Constraints 5-92 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 239 (only before the FAF). When a database altitude restriction of type “AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to deﬁne the vertical proﬁle. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-93...
Page 240 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ conﬁrmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available). 5-94 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 241 3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ conﬁrmation window is displayed. 4) Select ‘EDIT’ and press the ENT Key. 5) Edit the value using the FMS Knobs, and press the ENT Key. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-95...
Page 242: Procedures
6) Select a runway (if required) and press the ENT Key. 7) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the departure procedure. 5-96 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 243 Available Procedure Actions Departure Airport Loaded Procedures Departure Preview Departure Choices Figure 5-87 Departure Selection Selected Departure Loaded Departure Procedure Loading Page Selection Softkeys Figure 5-88 Departure Loading 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-97...
Page 244 3) Press the CLR Key. A conﬁrmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 5-98 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 245: Arrivals
7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the arrival procedure. Available Procedure Actions Destination Airport Loaded Procedures Arrival Preview Arrival Choices Figure 5-89 Arrival Selection 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-99...
Page 246 6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Sequence box. The arrival is previewed on the map. 7) Select the INFO Softkey to return to the Airport Information Page. 5-100 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 247: Approaches
The G1000 WAAS GPS allows for ﬂying LNAV, LNAV/VNAV, and LPV approaches according to the published chart. LNAV+V is a standard LNAV approach with advisory vertical guidance provided for assistance in 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-101...
Page 248 FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to ﬂy the ﬁnal course of the approach. 5-102 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 249 Loaded Procedures Approach Preview Approach Choices Figure 5-91 Approach Selection Selected Approach Loaded Approach Procedure Loading Page Selection Softkeys LOAD or ACTIVATE? Annunciation Figure 5-92 Approach Loading 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-103...
Page 250 Activating a previously loaded approach: 1) Press the PROC Key. The Procedures Window is displayed with ‘Activate Approach’ highlighted. 2) Press the ENT Key to activate the approach. 5-104 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 251 1) Press the PROC Key. 2) Turn the FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. The aircraft automatically sequences to the MAHP. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-105...
Page 252 ﬁx when the missed approach procedure is activated. Course to Fix Waypoint Figure 5-93 Course to Fix 5-106 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 253: Trip Planning
• Departure time (DEP TIME) - This defaults to the current time in automatic page mode. The computations are from the aircraft present position, so the aircraft is always just departing. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-107...
Page 254 • Enroute safe altitude (ESA) - The ESA is shown as nnnnnFT • Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes and are the local time at the destination. 5-108 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 255 Starting and Ending Waypoint of - NN: Pres. Pos. to End of Selected Leg Selected Flight Plan Segment Figure 5-95 Trip Planning Page - Flight Plan Mode 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-109...
Page 256 2) Turn the FMS Knobs to move the cursor onto the DEP TIME ﬁeld and enter the desired value. Press the ENT Key. The statistics are calculated using the new value and the cursor moves to the next entry ﬁeld..Repeat until all desired values have been entered. 5-110 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 257: Weight Planning
1) Press the FMS Knob to activate the cursor and highlight the ‘PASSENGERS #’ ﬁeld. 2) Turn the small FMS Knob to enter the number of passengers. 3) Press the ENT Key to conﬁrm the entry. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-111...
Page 258 If the aircraft is on the ground or a destination waypoint has not been entered, the following ﬁelds display invalid values consisting of six dashes: • Estimated landing weight • Estimated landing fuel weight • Excess fuel weight 5-112 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 259: Weight Caution And Warning Conditions
If the estimated landing fuel weight is zero or negative, then the following values are displayed in red: • Estimated fuel at landing weight • Excess fuel weight 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-113...
Page 260: Raim Prediction
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active ﬂight plan, nearest, recent, or airway waypoints). 5-114 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 261 • ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable. The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS can be enabled or disabled manually on the GPS Status Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-115...
Page 262 FLIGHT MANAGEMENT SBAS Status SBAS SELECTION Box - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays RAIM (displays SBAS Selection) PREDICTION) Figure 5-99 SBAS Display - Active 5-116 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 263 3) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS. SBAS Status SBAS SELECTION Box - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays RAIM (displays SBAS Selection) PREDICTION) Figure 5-100 SBAS Display - Disabled 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-117...
Page 264: Navigating A Flight Plan
2) Figure 5-101 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI ﬂight phase displayed on the HSI indicating 1.0 nm CDI scaling. Figure 5-101 Assigned Heading of 240º 5-118 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 265 290° as seen in Figure 5-102. Figure 5-102 Assigned Heading of 290º 4) Enter V4 into the ﬂight plan. a) Press the FMS Knob to activate the cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-119...
Page 266 Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4, Topeka VOR (TOP), as shown in Figure 5-104. Figure 5-104 Entering V4 Entry Point 5-120 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 267 Select the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-106. Figure 5-106 List of Available Airways for TOP g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-106. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-121...
Page 268 Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in Figure 5-108. Figure 5-108 Ready to Load V4 k) Press the ENT Key. 5-122 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 269 Select the ACT LEG Softkey. The conﬁrmation window is now displayed as in Figure 5-110. Note the TOP to SLN leg is actually part of V4. Figure 5-110 Comﬁrm Active Leg 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-123...
Page 270 6) The aircraft continues on heading 290º. When crosstrack distance is less than 2.0 nm, the XTK disappears from the HSI and the CDI is positioned on the last dot indicating a 2.0 nm distance from the centerline of the next course. 5-124 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 271 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-113. Figure 5-113 Turn to Intercept V244 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-125...
Page 272 FLIGHT MANAGEMENT 9) As seen in Figure 5-114, V244 is now the active ﬂight plan leg. Figure 5-114 V244 Now Active Leg 5-126 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 273 Turn the large FMS Knob to select OPSHN in the ﬂight plan list. c) Press the Direct-to ( ) Key. The Direct-to Window is now displayed as shown in Figure 5-116. Figure 5-116 Direct To OPSHN 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-127...
Page 274 OPSHN is entered. In other words, the G1000 gives vertical guidance so the aircraft arrives at an altitude of 10,000 feet three miles prior to OPSHN. 5-128 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 275 12) The aircraft is proceeding to OPSHN. The expected approach is the RNAV LPV approach to runway 35R, so it is selected. a) Press the PROC Key to display the Procedures Window. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-129...
Page 276 Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-121. Figure 5-121 List of Available Approaches d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-121. 5-130 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 277 With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the ﬂight plan as seen in Figure 5-123. Figure 5-123 Loaded Approach 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-131...
Page 278 Vertical guidance to the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS altitude source, therefore, the displayed altitude values are for reference only. Figure 5-124 Vertical Guidance is Active to the FAF 5-132 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 279 TOD that results in a -3.0 degree FPA descent to an altitude of 10,000 feet upon reaching the offset waypoint. Figure 5-125 Adjusting the Descent c) Press the ENT Key. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-133...
Page 280 Figure 5-126 Approaching Top of Descent (TOD) Target Altitude Vertical Deviation Indicator (VDI) Required Vertical Speed Indicator (RVSI) Figure 5-127 VDI & RVSI Upon Reaching Top of Descent (TOD) 5-134 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 281 17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 5-129. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet. Figure 5-129 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-135...
Page 282 PFD as seen in Figure 5-130. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI. Figure 5-130 Turn to intercept OPSHN to FSHER Leg 5-136 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 283 A descent to HABUK is in the next leg. Note the TOD point on the map. Annunciations for the upcoming turn and descent, as well as the VDI and RVSI, appear on the PFD as the ﬂight progresses. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-137...
Page 284 FLIGHT MANAGEMENT Figure 5-132 Approaching PYNON 5-138 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 285 Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 5-134. c) Press the ENT Key to activate the approach. Figure 5-134 Manually Activate Approach 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-139...
Page 286 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude is 9,000 feet upon reaching HABUK. Figure 5-135 Descending Turn to the Initial Approach Fix (IAF) 5-140 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 287 “AT” 7,800 feet at the FAF. Note the altitude restriction lines over and under (At) the altitude in the ‘ALT’ ﬁeld in Figure 5-136. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-141...
Page 288 In this case, the altitude ﬁx would be labeled ‘5500 ’. Again, if the aircraft altitude is lower than this prescribed altitude, a direct-to is established to this ﬁx when the missed approach procedure is activated. 5-142 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 289 The aircraft is climbing to 10,000 feet. The CDI ﬂight phase now changes from LPV to MAPR as seen on the HSI. Figure 5-138 Missed Approach Active 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-143...
Page 290 Figure 5-139 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-140. Figure 5-140 Hold Established 5-144 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 291: Abnormal Operation
Also, while the G1000 is in DR Mode, the autopilot does not couple to GPS, and both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 5-145...
Page 292 The Inset Map is removed from the PFD any time aircraft pitch is greater than +30° or less than –20°, NOTE: or when a 65° bank angle is reached. 5-146 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 293: Section 6 Hazard Avoidance
• L-3 SKYWATCH ® HP (SKY899) Trafﬁc Advisory System (Optional) Determine what type of trafﬁc system is installed by looking at the Trafﬁc Page softkeys. Figure 6-1 Trafﬁc Softkeys 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 294: Xm Satellite Weather
• The label on the back of the Data Link Receiver • The XM Information Page on the MFD • The XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N 190-00355-04) Contact the installer if the Audio and Data Radio IDs cannot be located.
Page 295 (Available Products for Service Class Indicated in Green) Select INFO Select LOCK Softkey to Softkey to Lock Display XM Subscription Information Page Information Figure 6-2 XM Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 296: Using Xm Satellite Weather Products
XM Satellite Radio services. If more than half of the expiration time has elapsed, the color of the product age displayed changes to yellow. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 297 Winds Aloft (WIND) County Warnings (COUNTY) Cyclone Warnings (CYCLONE) Radar Coverage No product image TFRs No product image TAFs No product image Table 6-1 Weather Product Symbols and Data Timing 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 298 City Forecast (CITY) Surface Analysis (SFC) Freezing Levels (FRZ LVL) Winds Aloft (WIND) County Warnings (COUNTY) Cyclone Warnings (CYCLONE) Radar Coverage TFRs TAFs Table 6-2 Weather Product Display Maps Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 299: Weather Softkeys On The Weather Data Link Page
The menus also provide a means in addition to the softkeys for enabling/disabling display of weather products. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 300 3) With Weather Setup highlighted, press the ENT Key. 4) Press the MENU Key. 5) Highlight the desired default(s) to restore (all or for selection) and press the ENT Key. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 301 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-6 Navigation Map Page Menu Figure 6-7 Navigation Map Page Setup Menu Figure 6-8 Navigation Map Page Setup Menu, Weather Group 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 302 RANGE Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer. Additional Information on Weather Feature Selected with Map Pointer Tornado Warning Selected With Map Pointer Figure 6-9 Panning on the Weather Data Link Page 6-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 303 • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Weather Data Link Page • Flight Plan Pages • Airport Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-11...
Page 304 NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in grayish-purple. Radar capability exists in these areas, but it is not active or is off-line. 6-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 305 The intensity level reﬂected by each square represents the highest level of NEXRAD data sampled within the area. Each block covers an Area of 4 sq. km Figure 6-12 NEXRAD Data - Zoomed 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-13...
Page 306 Information is derived from NEXRAD data. Figure 6-13 Echo Tops Data 6-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 307 NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in grayish-purple. Radar capability exists in these areas, but it is not active or is off-line. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-15...
Page 308 Since Cloud Tops and Echo Tops use the same color scaling to represent altitude, display of these weather products is mutually exclusive. When Cloud Tops is activated, Echo Tops data is removed. Figure 6-16 Cloud Tops Legend 6-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 309 XM Lightning data displays on the following maps: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Weather Data Link Page • Flight Plan Pages 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-17...
Page 310 Data Link Page, Cell Movement data can be selected independently. Cell Movement data can be displayed on the following maps: • PFD Inset Map • AUX - Trip Planning Page •Navigation Map • Nearest Pages 6-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 311 SIGMET is issued for hazardous convective weather. A localized SIGMET is a signiﬁcant weather condition occurring at a localized geographical position. Convective Sigmet Figure 6-21 SIGMET/AIRMET Data 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-19...
Page 312 To display the SIGMET and AIRMET legend, select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Sample SIGMET Text SIGMET/AIRMET Legend Figure 6-22 SIGMET/AIRMET Text and Legend 6-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 313 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text is placed ahead of the TAF text. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-21...
Page 314 Figure 6-24 METAR with Text To display the METAR legend on the Weather Data Link Page, select the LEGEND Softkey when METARs are selected for display. Figure 6-25 METAR Legend 6-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 315 3) Select the SFC Softkey. 4) Select the forecast time: CURRENT, 12 HR, 24 HR, 36 HR, or 48 HR. The SFC Softkey label changes to reﬂect the forecast time selected. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-23...
Page 316 When no data is displayed for a given altitude, the data for that altitude has not been received, or is out of date and has been removed from the display. New data appears at the next update. Figure 6-28 Freeze Level Data 6-24 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 317 4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reﬂect the altitude selected. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-25...
Page 318 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. Figure 6-31 Winds Aloft Data with Legend 6-26 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 319 3) Select the COUNTY Softkey. To display the County Warnings legend, select the LEGEND Softkey when County Warnings are selected to be displayed. Figure 6-33 County Warnings Legend 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-27...
Page 320 2) Select the MORE WX Softkey. 3) Select the CYCLONE Softkey. To display the Cyclone legend, select the LEGEND Softkey when Cyclones are selected to be displayed. Figure 6-35 Cyclone Legend 6-28 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 321: Airborne Color Weather Radar
6.2 AIRBORNE COLOR WEATHER RADAR SYSTEM DESCRIPTION The Garmin GWX 68 Airborne Color Weather Radar is a four-color digital pulsed radar with 6.5 kilowatts of output power. It combines excellent range and adjustable scanning proﬁles with a high-deﬁnition target display. The pulse width is four microseconds (µs) on all ranges except the 2.5 nm range. The GWX 68 uses a one µs pulse width at this range to reduce the targets smearing together on the display for better target deﬁnition...
Page 322 Both systems use colors to identify the different echo intensities, but the colors are not interchangeable. Airborne color radar values used by Garmin Airborne Color Weather Radar should not be confused with NEXRAD radar values. ANTENNA BEAM ILLUMINATION The radar beam is much like the beam of a spotlight.
Page 323 Attenuation can also be due to poor maintenance or degradation of the radome. Even the smallest amount of wear and scratching, pitting, and pinholes on the radome surface can cause damage and system inefﬁciency. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-31...
Page 324 Additionally, a cloud that contains only small raindrops, such as fog or drizzle, does not reﬂect enough radar energy to produce a measurable target return. Figure 6-38 Precipitation Type and Reﬂectivity 6-32 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 325 Since more radar energy is reﬂected back to the antenna with a low incident angle, the resulting detectable range is increased for mountainous terrain. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-33...
Page 326: Safe Operating Distance
14 nautical miles. Note this antenna tilt angle setting. Now, raise the antenna tilt 6 degrees above this setting. The bottom of the radar beam is now angled down 4º from parallel with the ground. 6-34 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 327 This setup provides a good starting point for practical use of the GWX 68. There are many other factors to consider in order to become proﬁcient at using weather radar in all situations. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-35...
Page 328: Weather Mapping And Interpretation
• Areas that show red or magenta are associated with hail or turbulence, as well as heavy precipitation. Vertical scanning and antenna tilt management may be necessary to identify areas of maximum intensity. 6-36 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 329 Figure 6-43 The Blind Alley - Horizontal Scan 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-37...
Page 330 In the upper regions of a cell where ice particles are dry (no liquid coating), target returns are less intense. 6-38 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 331 Standby mode until both displays are restored. In Reversionary mode, the weather radar system cannot be controlled. Radar Mode Scan Line Antenna Stabilization Status Figure 6-45 Horizontal Scan Display 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-39...
Page 332 4) Turn the RANGE Knob to select the desired map range. 5) The horizontal scan is initially displayed (Figure 6-45). If desired, select the VERTICAL Softkey to change to vertical scanning. 6-40 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 333 8) To select a new area to be vertically scanned, select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps. The RANGE Knob can also be used to adjust bearing from left to right. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-41...
Page 334 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. The RANGE Knob can also be used to adjust tilt up and down. 6-42 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 335 2) Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is again selected. The RANGE Knob can also be used to adjust tilt. Tilt Line Scan Line Figure 6-49 Adjusting Tilt on Vertical Scan Display 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-43...
Page 336 4) Select the GAIN Softkey again to recalibrate the gain. CALIBRATED is displayed in the GAIN ﬁeld. Manual Gain Set Below Calibrated Calibrated Gain Figure 6-50 Gain Calibration 6-44 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 337 6) If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan. 7) Select the BRG Softkey again to remove the Bearing Line and cursor. The bearing reference is reset to 0º. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-45...
Page 338 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. 6-46 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 339 Displayed intensity is questionable. Areas of Potentially stronger than displayed. Attenuated Signal Horizontal Scan Without WATCH™ Horizontal Scan With WATCH™ Figure 6-53 Horizontal Scan Without and With WATCH™ 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-47...
Page 340 To activate or deactivate Weather Alerts, select the WX ALRT Softkey. Activating and deactivating also enables or inhibits the alert on the PFD. Figure 6-55 Weather Alert on PFD 6-48 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 341: Ground Mapping And Interpretation
6) Adjust the antenna tilt angle by turning the small FMS Knob to display ground returns at the desired distance. 7) Press the FMS Knob to remove the cursor. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-49...
Page 342: Stormscope Wx-500 Series Ii (Optional)
4) Turn the large FMS Knob to highlight and move between the product selections. 5) When an item is highlighted, turn the small FMS Knob to select the option. 6-50 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 343 • STRMSCP SMBL – Selects the range at which Stormscope data displays. Stormscope data is removed when a map range greater than the STRMSCP SMBL value is selected (Figure 6-57). Figure 6-56 Page Menu Figure 6-57 Map Setup Menu 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-51...
Page 344 If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn (Figure 6-59). This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. 6-52 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 345 Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner (Figure 6-60). Figure 6-60 Lightning Display Range Annunciation 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-53...
Page 346: Selecting The Stormscope Page
2) Turn the small FMS Knob to select the Stormscope Page. 3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in. Figure 6-61 Stormscope Page 6-54 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 347 3) Select ‘Clear Stormscope Lightning’. 4) Press the ENT Key. Or : 1) Select the Stormscope Page. 2) Press the CLEAR Softkey. Figure 6-62 Navigation Map Page Options Menu 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-55...
Page 348 2) Press the MENU Key. 3) Turn the small FMS Knob to choose between ‘View Arc’ and ‘View 360˚ options. 4) When an item is selected, press the ENT Key. 6-56 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 349: Terrain Awareness & Warning System (Taws)
Individual obstructions may be shown if available in the database. The data undergoes veriﬁcation by Garmin to conﬁrm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data may be inaccurate.
Page 350: Displaying Taws Data
The setup menu also controls the map range settings above which terrain and obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. 6-58 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 351 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-64 Navigation Map Page Menu Figure 6-65 Navigation Map Page Setup Menu Figure 6-66 Navigation Map Page Setup Menu, Map Group 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-59...
Page 352: Taws Page
Showing/hiding aviation information on the TAWS Page: 1) Press the MENU Key. 2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’, dependent on current state, and press the ENT Key. 6-60 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 353 1000’ Below the Aircraft Altitude) Yellow Terrain (Caution - Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Terrain Legend Figure 6-68 TAWS Page (ARC View) 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-61...
Page 354: Taws Alerts
• Press the CLR Key (returns to the currently viewed page), or • Press the ENT Key (accesses the TAWS Page) Alert Annunciation Figure 6-69 Alert Annunciation on the PFD Figure 6-70 Alert Pop-up on the MFD 6-62 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 355 HAZARD AVOIDANCE Potential Impact Point Alert Annunciation Figure 6-71 TAWS PULL UP Alert Annunciation on the MFD 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-63...
Page 356 LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for details. 6-64 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 357 “Too Low, Terrain” * Alerts with multiple messages are conﬁgurable at installation and are installation-dependent. Alerts for the default conﬁguration are indicated with asterisks. Table 6-7 TAWS Alerts Summary 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-65...
Page 358 4000 3500 3000 2500 2000 1500 "PULL UP" "PULL UP" 1000 2000 4000 6000 8000 10000 12000 Descent Rate (FPM) Figure 6-73 Excessive Descent Rate Alert Criteria 6-66 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 359 During ﬁnal approach, FLTA alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or below 125 feet AGL while within 1.0 nm of the runway threshold. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-67...
Page 360 500 feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “ﬁve-hundred” is generated. There are no display annunciations or pop-up alerts that accompany the aural message. 6-68 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 361 Altitude Loss (Feet) 1000 “DON’T SINK” “DON’T SINK” 1000 1500 2000 2500 3000 3500 4000 Sink Rate (Feet Per Minute) Figure 6-75 Negative Climb Rate (NCR) Alert Criteria 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-69...
Page 362: System Status
Annunciation Annunciation No GPS position NO GPS POSITION “TAWS Not Available” Excessively degraded GPS signal GPS signal re-established None None “TAWS Available” Table 6-10 TAWS Status Annunciations 6-70 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 363: Trafﬁc Information Service (Tis)
3500 feet above the requesting aircraft. Trafﬁc is displayed according to TCAS symbology using four different symbols. TIS Symbol Description Non-Threat Trafﬁc Proximity Advisory (PA) Trafﬁc Advisory (TA) Trafﬁc Advisory Off Scale Table 6-11 TIS Trafﬁc Symbols 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-71...
Page 364 (for speeds greater than 500 fpm in either direction) to the right of the target symbol. Trafﬁc symbols for aircraft without altitude reporting capability appear without altitude separation or climb/descent information. 6-72 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 365 If a map range larger than the map range setting is selected, the data is removed from the map. Maps other than the Trafﬁc Map Page use settings based on those selected for the Navigation Map Page. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-73...
Page 366 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-79 Navigation Map Page Menu Figure 6-80 Navigation Map Page Setup Menu Figure 6-81 Navigation Map Page Setup Menu, Trafﬁc Group 6-74 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 367: Trafﬁc Map Page
Non-Bearing Trafﬁc (System is Unable to is 400’ Below and Determine Bearing), Aircraft Distance is 8.0 Climbing nm, 1100’ Above and Descending Figure 6-82 Trafﬁc Map Page - Advisories 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-75...
Page 368: Tis Alerts
The “Trafﬁc Not Available” (TNA) voice alert can be manually muted to reduce nuisance alerting. TNA muting status is shown in the upper left corner of the Trafﬁc Map Page. 6-76 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 369: System Status
The transponder has failed UNAVAILABLE TIS is unavailable or out of range * Contact a service center or Garmin dealer for corrective action Table 6-12 TIS Failure Annunciations 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 370 TIS Operating STANDBY TIS Standby (Also shown in white in center of page) FAIL TIS Failed* * See Table 6-14 for additional failure annunciations Table 6-13 TIS Modes 6-78 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 371 The trafﬁc service is unavailable or out of range *Shown as symbol on Trafﬁc Map Page **Shown in center of Trafﬁc Map Page Table 6-14 TIS Trafﬁc Status Annunciations 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-79...
Page 372: Skywatch Hp (Sky899) Tas (Optional)
TA criteria. A Trafﬁc Advisory that is beyond the selected display range is indicated by a half TA symbol at the edge of the screen at the relative bearing of the intruder. 6-80 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 373: Operation
4) Select the STANDBY Softkey to place the system in the Standby mode. STANDBY is displayed in the Trafﬁc mode ﬁeld. 5) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-81...
Page 374 When trafﬁc is selected on maps other than the Trafﬁc Map Page, a trafﬁc icon is shown to indicate TAS is enabled for display. Displaying trafﬁc on the Navigation Map 1) Ensure that the TAS system is operating. With the Navigation Map displayed, select the MAP Softkey. 6-82 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 375 2) Select the TRAFFIC Softkey. Trafﬁc is now displayed on the map as shown in the ﬁgure. Trafﬁc Advisory Proximity Trafﬁc Non-Threat Trafﬁc TA Off Scale Banner Non-Bearing Trafﬁc Advisories Figure 6-87 TAS Trafﬁc on Navigation Map 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-83...
Page 376: Altitude Display
2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm • 12 and 24 nm • 24 and 40 nm 6-84 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 377 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page. Figure 6-88 Navigation Map Page Menu Figure 6-89 Navigation Map Page Setup Menu Figure 6-90 Navigation Map Page Setup Menu, Trafﬁc Group 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-85...
Page 378: Tas Alerts
TAS Operating STANDBY TAS Standby (also shown in white in center of page) TAS Failed* FAIL * See Table 6-17 for additional failure annunciations Table 6-16 TAS Modes 6-86 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 379 Data is not being received from the TAS unit *Shown as symbol on Trafﬁc Map Page **Shown in center of Trafﬁc Map Page Table 6-18 TAS Trafﬁc Status Annunciations 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 6-87...
Page 380 HAZARD AVOIDANCE LANK 6-88 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 381: Section 7 Automatic Flight Control System
• Manual Electric Pitch Trim (MEPT) — The pitch trim servo provides manual electric pitch trim capability when the autopilot is not engaged. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 382 Adjusts the Selected Heading and bug in 1° increments on the HSI (both PFDs) Press to synchronize the Selected Heading to the current heading on the pilot-side PFD Annunciator Light Figure 7-1 GMC 710 AFCS Control Unit Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 383: Additional Afcs Controls
MEPT function is disabled and ‘PTRM’ is displayed as the AFCS Status Annunciation on the PFDs. The function remains disabled until both sides of the switch are inactivated. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 384: Flight Director Operation
NAV or APR Key press activates ﬂight director. ***The selected navigation receiver must have a valid LOC signal before BC Key press activates ﬂight director. Table 7-1 Flight Director Activation Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 385: Afcs Status Box
Flight Director Active Mode Armed Indicator Arrow Reference AFCS Status Box Selected Altitude Vertical Speed Reference Command Bars GPS is Selected Navigation Source Figure 7-2 PFD AFCS Display 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 386: Flight Director Modes
XFR Key. When the ﬂight directors are switched, the vertical and lateral modes revert to default. Pilot-side Flight Director Selected Copilot-side Flight Director Selected Figure 7-4 Flight Director Selection Indications Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 387: Command Bars
If the attitude information being sent to the ﬂight director becomes invalid or unavailable, the Command Bars are removed from the display. The ﬂight director Command Bars also disappear if the pitch exceeds +30˚/-20˚ or bank exceeds 65˚. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 388: Vertical Modes
VNV Target Altitude ** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude Table 7-2 Flight Director Vertical Modes Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 389: Pitch Hold Mode (Pit)
• Pressing the CWS Button, hand-ﬂying the aircraft to establish a new pitch reference, then releasing the CWS Button Pitch Hold Selected Altitude Mode Active Capture Mode Armed Selected Altitude Command Bars Maintain Desired Pitch Reference Figure 7-7 Pitch Hold Mode 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 390: Selected Altitude Capture Mode (Alts)
Use of the ALT SEL Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes the ﬂight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new Selected Altitude. 7-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 391: Altitude Hold Mode (Alt)
CWS Button is released at the desired altitude, the new altitude is established as the Altitude Reference. Altitude Hold Altitude Mode Active Reference Selected Altitude Command Bars Selected Hold Pitch Altitude Attitude to Maintain Altitude Reference Figure 7-9 Altitude Hold Mode 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-11...
Page 392: Vertical Speed Mode (Vs)
Mode Active Reference Mode Armed Selected Altitude Vertical Speed Reference Command Vertical Bars Indicate Speed Climb to Attain Reference Vertical Speed Reference Figure 7-10 Vertical Speed Hold Mode 7-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 393: Flight Level Change Mode (Flc)
Selected Altitude. Flight Level Selected Change Mode Airspeed Altitude Capture Active Reference Mode Armed Airspeed Reference Airspeed Reference Figure 7-11 Flight Level Change Mode (IAS) 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-13...
Page 394 Indicator at the IAS corresponding to the selected Mach target speed and the current Mach number is shown only in the AFCS Status Box. Flight Level Airspeed Selected Change Mode Reference Altitude Capture Active (Mach) Mode Armed Figure 7-12 Flight Level Change Mode (Mach) 7-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 395: Vertical Navigation Modes (Vpth, Altv)
ﬂight director to follow the path deﬁned by the vertical proﬁle. Upon reaching the last waypoint in the VNV ﬂight plan, the ﬂight director transitions to Altitude Hold Mode and cancels any armed VNV modes. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-15...
Page 396 If the descent is not conﬁrmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured. 7-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 397 Altitude Selected Altitude Below VNV Target Vertical Deviation Indicator Required Vertical Speed Bug GPS is Enroute Selected Phase of Navigation Flight Source Figure 7-14 Vertical Path Capture 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-17...
Page 398 If the change is made while nearing a waypoint with a VNV Target Altitude, the aircraft may not re-establish on the descent path in time to meet the vertical constraint. 7-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 399 • Vertical deviation from the proﬁle has exceeded 250 feet, but is now less than 200 feet Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate proﬁle re-capture. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-19...
Page 400 ﬁrst. VNV target altitudes can be changed while editing the active ﬂight plan (see the GPS Navigation Section for details). 7-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 401: Glidepath Mode (Gp)
• Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI) GPS Approach Glidepath Mode Active Mode Active Glidepath Indicator Command Bars Indicate Descent on Glidepath GPS is Selected Approach Navigation Active Source Figure 7-19 Glidepath Mode 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-21...
Page 402: Glideslope Mode (Gs)
Mode Active Mode Active Active ILS Frequency Tuned Command Glideslope Bars Indicate Indicator Descent on Localizer/ Glideslope Path NAV2 (localizer) is Selected Navigation Source Figure 7-21 Glideslope Mode 7-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 403: Takeoff (To) And Go Around (Ga) Modes
Go Around Mode Active Autopilot Disconnect Annunciation Flashes Yellow for 5 seconds Command Bars Indicate Climb Figure 7-22 Go Around Mode Takeoff Mode Active Figure 7-23 Takeoff Mode 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-23...
Page 404: Lateral Modes
The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach Mode. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS Button. 7-24 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 405: Roll Hold Mode (Rol)
Low Bank Mode when descending through 20,500 feet. The annunciator light next to the BANK Key illuminates while Low Bank Mode is selected. Figure 7-25 Low Bank Mode Limits 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-25...
Page 406 330° at a time result in turn reversals. Heading Select Pitch Hold Mode Active Mode Active Command Bars Track Selected Heading Selected Heading Selected Heading Figure 7-26 Heading Select Mode 7-26 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 407: Navigation Mode (Gps, Vor, Loc)
• Navigation source manually switched (with the CDI Softkey) • During a LOC/ILS approach, the FAF is crossed while in GPS Navigation Mode after the automatic navigation source switch from GPS to LOC 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-27...
Page 408 Mode Active Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude Selected Course GPS is Selected Navigation Source Figure 7-28 Navigation Mode 7-28 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 409: Approach Mode (Gps, Vapp, Loc)
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. Figure 7-29 GPS Approach Mode Armed 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-29...
Page 410 Pressing the CWS Button and hand-ﬂying the aircraft does not change the Selected Course while in Approach Mode. The autopilot guides the aircraft back to the Selected Course (or GPS ﬂight plan) when the CWS Button is released. 7-30 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 411: Backcourse Mode (Bc)
Pressing the CWS Button and hand-ﬂying the aircraft does not reset any reference data while in Backcourse Mode. The autopilot guides the aircraft back to the Selected Course when the CWS Button is released. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-31...
Page 412: Autopilot And Yaw Damper Operation
YAW AXIS The yaw damper uses yaw rate and roll attitude to dampen the aircraft’ s natural Dutch roll response. It also uses lateral acceleration to coordinate turns. 7-32 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 413: Engagement
In most scenarios, releasing the CWS Button reengages the autopilot with a new reference. Refer to ﬂight director mode descriptions for speciﬁc CWS behavior in each mode. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-33...
Page 414: Disengagement
A localized failure in the yaw damper system or invalid sensor data also cause yaw damper disengagement. Figure 7-35 Automatic Autopilot and Yaw Damper Disengagement 7-34 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 415: Example Flight Plan
The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed. KMKC KCOS Figure 7-36 Flight Plan Overview 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-35...
Page 416: Departure
At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation ﬂashes for up to 10 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 7-36 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 417 AFCS Selected Altitude of 12,000 MSL ALT Mode KMKC Figure 7-37 Departure 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-37...
Page 418: Intercepting A Vor Radial
Mode and the ‘VOR’ annunciation ﬂashes green. The autopilot begins turning to intercept the Selected Course. 3) The autopilot continues the turn until the aircraft is established on the Selected Course. Figure 7-38 Intercepting a VOR Radial 7-38 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 419: Flying A Flight Plan/Gps Course
3) Following the ﬂight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS Navigation Mode, course changes deﬁned by the ﬂight plan are automatically made without pilot action required. Figure 7-39 Transition to GPS Flight Plan 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-39...
Page 420: Descent
Altitude Hold Mode and levels the aircraft. Cruise Altitude of 12,000 MSL ALT Mode Selected Altitude of 10,000 MSL ALT Mode Figure 7-40 FLC Descent 7-40 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 421 ALT Mode VNAV Target Altitude of 10,000 MSL Selected Altitude (set below VNAV Target Altitude) Along-track Offset, 3 nm before OPSHN 3 nm Figure 7-41 VPTH Descent 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-41...
Page 422 The green ‘ALT’ annunciation ﬂashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint. 7-42 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 423 ALT Mode ALT Mode Selected Altitude of 9,400 MSL ALT Mode VNAV Target Altitude of 9,000 MSL Selected Altitude OPSHN HABUK 3 nm Figure 7-42 Non-path Descent 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-43...
Page 424: Approach
• Push the AP/YD DISC Switch at the decision • Use the GA Switch to execute a missed approach. height and land the aircraft. KCOS PETEY PYNON Figure 7-43 ILS Approach to KCOS 7-44 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 425 • Push the AP/YD DISC Switch at the decision • Use the GA Switch to execute a missed approach. height and land the aircraft. KCOS CEGIX FALUR HABUK PYNON Figure 7-44 LPV Approach to KCOS 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-45...
Page 426: Go Around/Missed Approach
The green ‘ALT’ annunciation ﬂashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 7-46 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 427 4) The autopilot ﬂies the holding pattern after the missed approach is activated. Annunciations are displayed in the Navigation Status Box, above the AFCS Status Box. MOGAL KCOS Figure 7-45 Go Around/Missed Approach 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-47...
Page 428: Afcs Annunciations And Alerts
Power must be cycled to the servos to remedy the situation. Preﬂight system test failed; aural alert sounds at failure Table 7-5 AFCS Status Alerts 7-48 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 429: Overspeed Protection
Indicator, ﬂashing a yellow ‘MAXSPD’ annunciation. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. Airspeed Indicator Figure 7-47 Overspeed Annunciation 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 7-49...
Page 430 AFCS LANK 7-50 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 431: Section 8 Additional Features
Airport Hot Spots are outlined to caution pilots of areas on an airport surface where positional awareness confusion or runway incursions happen most often. Hot Spots are deﬁned with a magenta circle or outline around the region of possible confusion. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 432 Selecting the DCLTR-3 Softkey cycles back to the original map detail. Refer to Map Declutter Levels in the Flight Management Section. Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 433 7) Press the ENT Key to complete the selection. 8) Press the FMS Knob to return to the Navigation Map Page. SAFETAXI Option SafeTaxi Range Options Figure 8-3 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 434: Safetaxi Cycle Number And Revision
N/A appears in white if no SafeTaxi data is available on the database card. SafeTaxi Database is Current SafeTaxi Database has Expired SafeTaxi Database Not Available Figure 8-4 Power-up Page, SafeTaxi Database Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 435 DBASE Softkey Selected Figure 8-5 AUX – System Status Page, SafeTaxi Current Information The SafeTaxi database is provided by Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 436 AVAILABLE indicates that SafeTaxi is not available on the database card or no database card is inserted. SafeTaxi Database Not Installed SafeTaxi Database has Expired Figure 8-6 AUX – System Status Page, SafeTaxi Expired, SafeTaxi Not Available Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 437: Chartview
PLAN PROFILE MINIMUMS FIT WDTH FULL SCN BACK Selecting the BACK Softkey returns to the Chart Selection Softkeys. Figure 8-7 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 438: Terminal Procedures Charts
CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the Jeppesen subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport. Figure 8-9 Chart Not Available Banner Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 439 Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 440 (Figure 8-15). If the Chart Scale Box displays a banner CHART NOT TO SCALE, the aircraft symbol is not shown. The Aircraft Not Shown Icon may appear at certain times, even if the chart is displayed to scale. 8-10 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 441 Diagram and the navigation map on the WPT – Airport Information page. Select CHRT Softkey to Switch Between ChartView and WPT - Airport Information Page Figure 8-12 CHRT Softkey, Airport Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-11...
Page 442 Airport Diagram, Take-off Minimums, Class B Airspace, Airline Parking Gate Coordinates, and Airline Parking Gate Location. (The numbers in parentheses after the chart name are Jeppesen designators.) Aircraft Current Position Figure 8-13 Airport Information Page, INFO View, Full Screen Width 8-12 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 443 Figure 8-14 Airport Information Page, Class B Chart Selected from INFO View Selecting the DP Softkey displays the Departure Procedure Chart if available. Chart Not To Scale Aircraft Not Shown Icon Figure 8-15 Departure Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-13...
Page 444 Joystick Aircraft Not Shown Icon Figure 8-16 Arrival Information Page Selecting the APR Softkey displays the approach chart for the airport if available. Figure 8-17 Approach Information Page 8-14 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 445 METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only when an XM Data Link Receiver is installed and the XM Weather subscription is current. WX Info When Available WX Softkey Selected Figure 8-18 Weather Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-15...
Page 446 NOTAM Softkey label appears subdued and is disabled as shown in Figure 8-18. The NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections. NOTAM Softkey Appears for Selected Airports Figure 8-19 NOTAM Softkey Highlighted 8-16 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 447 Selecting the NOTAM Softkey again removes the NOTAMS information. Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight Plan Page). 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-17...
Page 448: 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 the screen. Entire Chart Shown Figure 8-21 Approach Information Page, ALL View 8-18 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 449 Figure 8-22 Approach Information Page, Header View Selecting the PLAN Softkey shows the approach chart two dimensional plan view. Approach Chart Plan View Figure 8-23 Approach Information Page, Plan View 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-19...
Page 450 Selecting the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart. Minimum Descent Altitude/ Visibility Strip Figure 8-25 Approach Information Page, Minimums View, Full Screen Width 8-20 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 451 ﬁt the available screen width. Select FIT WDTH Softkey to Show Full Chart Width Figure 8-26 Airport Information Page, FIT WDTH Softkey Selected 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-21...
Page 452 Screen and Chart with Info Window Figure 8-27 Airport Information Page, Full Screen and Info Window Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. 8-22 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 453 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. Chart Setup Option Full Screen On/Off Selection Figure 8-28 Page Menus 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-23...
Page 454: Day/Night View
The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. 6) Press the FMS Knob when ﬁnished to remove the Chart Setup Menu. 8-24 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 455 ADDITIONAL FEATURES Figure 8-30 Arrival Information Page, Day View Figure 8-31 Arrival Information Page, Night View 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-25...
Page 456: Chartview Cycle Number And Expiration Date
System is verifying chart database when new cycle is installed for the ﬁrst time. After verifying, chart database is found to be corrupt. ChartView is not available. Table 8-1 ChartView Power-up Page Annunciations and Deﬁnitions 8-26 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 457 Chart Cycle has Expired but is Still Viewable Chart Cycle is No for 70 Days from Expiration Date Longer Viewable Figure 8-32 Examples of Power-up Page, ChartView Database 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-27...
Page 458 Figure 8-33 AUX – System Status Page, ChartView Current and Available The ChartView database is provided directly from Jeppesen. Refer to Updating Jeppesen Databases in Appendix B for instructions on revising the ChartView database. 8-28 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 459 System is Conﬁgured for ChartView but Database is not Available ChartView Database is Not Available Figure 8-34 AUX – System Status Page, ChartView Expired, ChartView Disabled, ChartView Not Available 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-29...
Page 460: Flitecharts
FliteCharts resemble the paper version of National Aeronautical Charting Ofﬁce (NACO) terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. FliteCharts database subscription is available from Garmin. Available data includes: • Arrivals (STAR) • Approaches •...
Page 461: Terminal Procedures Charts
The CHART NOT AVAILABLE banner does not refer to the FliteCharts subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport. Figure 8-37 Chart Not Available Banner 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-31...
Page 462 Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown. 8-32 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 463 The aircraft symbol is not shown on FliteCharts. The Chart Scale Box displays a banner CHART NOT TO SCALE, and the Aircraft Not Shown Icon is displayed in the lower right corner of the screen. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-33...
Page 464 Diagram and the navigation map on the WPT – Airport Information page. Select CHRT Softkey to Switch Between Navigation Map Page and FliteCharts Figure 8-40 CHRT Softkey, Airport Information Page 8-34 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 465 Peachtree Airport has three additional charts offering information; the Airport Diagram, Alternate Minimums, and Take-off Minimums. Info Box Selected Figure 8-41 Airport Information Page, INFO View with Airport Information 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-35...
Page 466 IFR Alternate Minimums Chart (Figure 8-42). Figure 8-42 Airport Information Page, ALTERNATE MINIMUMS Selected from INFO View Selecting the DP Softkey displays the Departure Procedure Chart if available. Figure 8-43 Departure Information Page 8-36 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 467 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 chart for the airport if available. Figure 8-45 Approach Information Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-37...
Page 468 When Available Chart Not To Scale Figure 8-46 Weather Information Page Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page). 8-38 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 469: 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 screen. Entire Chart Shown Figure 8-47 Airport Information Page, ALL View Selected 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-39...
Page 470 Select FIT WDTH Softkey to Show Full Chart Width Figure 8-48 Approach Information Page, FIT WDTH Softkey Selected 8-40 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 471 Info Window Figure 8-49 Airport Information Page, Full Screen and Info Window Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-41...
Page 472 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. Chart Setup Option Full Screen On/Off Selection Figure 8-50 Page Menus 8-42 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 473: Day/Night View
The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. 6) Press the FMS Knob when ﬁnished to remove the Chart Setup Menu. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-43...
Page 474 ADDITIONAL FEATURES Figure 8-52 Approach Information Page, Day View Figure 8-53 Approach Information Page, Night View 8-44 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 475: Flitecharts Cycle Number And Expiration Date
Blank Line. G1000 system is not conﬁgured for FliteCharts. Contact a Garmin-authorized service center for conﬁguration. System is conﬁgured for FliteCharts but no chart database is installed. Refer to Updating Garmin Databases in Appendix B for the FliteCharts database Normal operation. FliteCharts database is valid and within current cycle.
Page 476 FliteCharts Database is Current FliteCharts Database is and Available Expired but Still Available FliteCharts Database is Disabled FliteCharts Database is Not Available Figure 8-54 FliteCharts Power-up Page Messages 8-46 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 477 DBASE Softkey Selected Figure 8-55 AUX – System Status Page, FliteCharts Current and Available The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT...
Page 478 System is Conﬁgured for FliteCharts but Database is not Installed FliteCharts Database is Not Available Figure 8-56 AUX – System Status Page, FliteCharts Expired, FliteCharts Disabled, FliteCharts Not Available 8-48 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 479: Xm Radio Entertainment (Optional)
• On the label on the back of the Data Link Receiver • On the XM Information Page on the MFD (Figure 8-57) • On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N 190-00355-04) Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located.
Page 480 Page and a yellow Activation Required message is displayed in the center of the Weather Data Link Page (Map Page Group). The Service Class refers to the groupings of weather products available for subscription. 8-50 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 481: Using Xm Radio
2) Turn the small FMS Knob to select the displayed AUX - XM Information Page. 3) Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. Active Channels Channel List Categories Field Figure 8-58 XM Radio Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-51...
Page 482 3) Select the numbered softkeys located on the bottom of the display to directly select the desired channel number. 4) Press the ENT Key to activate the selected channel. 8-52 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 483 Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob and press the ENT Key. Selecting All Categories places all channels in the list. Figure 8-59 Categories List 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-53...
Page 484 Softkey is selected, the volume can also be adjusted using the small FMS Knob.) 3) Select the MUTE Softkey to mute the audio. Select the MUTE Softkey again to unmute the audio. Figure 8-61 Volume Control 8-54 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 485: Scheduler
7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next ﬁeld. 8) For periodic and one-time messages, use the FMS Knob to enter the timer value (HH:MM:SS) from which to countdown and press the ENT Key. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-55...
Page 486 The softkey label reverts to ALERTS when pressed, the Alerts Window is removed from the display, and the scheduler message is deleted from the message queue. Figure 8-63 PFD Alerts Window 8-56 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 487: Abnormal Operation
2) Turn the small FMS Knob to select the System Status Page (the last page in the AUX Page Group). Figure 8-64 LRU Information Window on System Status Page 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 8-57...
Page 488 Weather Datalink Page - center of page within last 5 minutes ACTIVATION REQUIRED Weather Datalink Page - center of page XM subscription is not activated Table 8-3 GDL 69/69A Data Link Receiver Error Messages 8-58 Garmin G1000 Pilot’s Guide for the Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 489: Annunciations And Alerts
Line Replaceable Unit (LRU). See the G1000 System Annunciations Section for more information. System Annunciation (Red ‘X’) Alerts Window Softkey Annunciation Figure A-1 G1000 Alerting System 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 490 Press the MENU Key. b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key. Press to Test Annunciation Tone Figure A-2 System Status Page, Annunciation Tone Testing Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 491 MFD FAN FAIL – MFD cooling fan is inoperative.. None AVN FAN 1 FAIL – Avionics cooling fan #1 is inoperative. None AVN FAN 2 FAIL – Avionics cooling fan #2 is inoperative. None 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 492: Comparator Annunciations
The following audio alerts are announced by the system using a voice of male or female gender (see the AUX - System Setup Page for the default conﬁgured voice gender; contact a Garmin-authorized service center to change the audio alert voice). If the optional Terrain Awareness and Warning System is installed, voice alerts are also generated (refer to the TAWS Alerts section).
Page 493: Reversionary Sensor Annunciations
NOTE: initialize. All windows should be operational within one minute of power-up. Should any window continue to remain ﬂagged, the G1000 system should be serviced by a Garmin-authorized repair facility. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 494 Integrated Avionics Unit GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GTX 33 Transponder Or GIA 63W Integrated Avionics Units Figure A-4 G1000 System Failure Annunciations Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 495 Upon power-up, certain windows remain invalid as G1000 equipment begins to initialize. All windows NOTE: should be operational within one minute of power-up. If any window continues to remain ﬂagged, the G1000 System should be serviced by a Garmin-authorized repair facility. System Annunciation Comment Attitude and Heading Reference System is aligning.
Page 496: G1000 System Message Advisories
Conﬁg service req’d. The PFD conﬁguration settings do not match backup conﬁguration memory. The G1000 system should be serviced. PFD2 CONFIG – PFD2 conﬁguration error. Conﬁg service req’d. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 497 The MFD and/or PFD detected a failure in the basemap database. The G1000 database error exists. system should be serviced. PFD2 DB ERR – PFD2 basemap database error exists. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 498 LRU. Ensure that the terrain card is properly inserted in the speciﬁed display. database missing. Replace terrain card. If problem persists, the G1000 system should be serviced. PFD2 DB ERR – PFD2 airport terrain database missing. A-10 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 499 DB MISMATCH – Airport Terrain The PFD and MFD have different airport terrrain databases installed. Crossﬁll is off. database mismatch. Install correct airport terrain database in both displays. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-11...
Page 500 The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. A-12 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 501 TRUE APR – True north approach. Displayed after passing the ﬁrst waypoint of a true north approach when the nav angle is Change HDG refereence to TRUE. set to ‘AUTO’. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-13...
Page 502 The #1 GEA 71 has incorrect software installed. The G1000 system should be mismatch, communication halted. serviced. MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed. The G1000 system should be mismatch, communication halted. serviced. A-14 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 503 AHRS2 GPS – AHRS2 operating The #2 AHRS is operating exclusively in no-GPS mode. The G1000 system should be exclusively in no-GPS mode. serviced. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-15...
Page 504 A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The G1000 system should be serviced. communication halted. A-16 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 505 A key is stuck on the GCMC 710 bezel. Attempt to free the stuck key by pressing it is stuck several times. The G1000 system should be serviced if the problem persists. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-17...
Page 506 ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the special use than 10 minutes. airspace within 10 minutes. A-18 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 507 UPDT BARO – Transition altitude The aircraft has climbed or descended through 18,000 feet and the altimeter setting crossed. Update baro setting. has not been adjusted accordingly. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-19...
Page 508: Afcs Alerts
(if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation. A-20 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 509: Taws Alerts
Premature Descent Alert Caution (PDA) “Too Low, Terrain” Altitude Callout “500” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) “Don’t Sink” “Too Low, Terrain” 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT A-21...
Page 510: Other G1000 Aural Alerts
The aircraft has descended below the preset barometric minimum descent altitude. “Vertical track” The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. A-22 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 511: Sd Card Use
Garmin supplied Supplemental Data Card which will reside in the bottom card slot on the 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 and update information.
Page 512: Garmin Databases
Remove the SD card when ﬁnished. 7) Verify that the correct update cycle is loaded during startup of the MFD. GARMIN DATABASES The following G1000 databases are stored on Supplemental Data Cards provided by Garmin: • Expanded basemap • Obstacle •...
Page 513 • Existing 010-00330-42 Supplemental Database SD Cards from both PFD and MFD In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional. It may also be necessary to have the system conﬁgured by a Garmin authorized service facility in order to use some database features.
Page 514 7) Turn either FMS Knob to scroll through the database list and check that all databases are current and there are no errors. 8) Power down the G1000. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 515: Glossary
Surveillance Air Trafﬁc Control carbon monoxide ATCRBS ATC Radar Beacon System communication radio ATIS Automatic Terminal Information Service CONFIG conﬁguration along-track COOL coolant AUTOSEQ automatic sequence COPLT co-pilot 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 516 The recommended minimum altitude Direct to Fix Altitude within ten miles left or right of the desired course on an active ﬂight plan DFLT default or direct-to. DGRD degrade Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 517 Flight Level Change travelling relative to a ground position. Course From Fix to Manual Termination Ground Track see Track Flight Management System Garmin Reference System Fuel On Board Ground speed 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 518 The portion of a ﬂight plan between Initial Fix two waypoints. Instrument Flight Rules LIFR Low Instrument Flight Rules Imperial gallon LNAV Lateral Navigation Instrument Landing System Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 519 P. POS Present Position Military Operations Area PRES, PRESS pressure movement PROC procedure(s), procedure turn meters per minute pounds per square inch Minimum Safe Altitude Procedure Turn 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 520 Static Air Temperature Terminal Control Area SBAS Satellite-Based Augmentation System TCAS Trafﬁc Collision Avoidance System SCIT Storm Cell Identiﬁcation and Tracking telephone Secure Digital TEMP temperature second(s) TERM terminal Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 521 VERT vertical XFER, XFR transfer Vertical Figure A measure of the uncertainty in the XPDR transponder of Merit aircraft’s vertical position. XTALK cross-talk cross-track 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 522 APPENDIX C LANK Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 523: Frequently Asked Questions
If a particular aspect of G1000 operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized dealer. Garmin is dedicated to supporting its products and customers.
Page 524 ﬂight plan. When OBS mode is cancelled, automatic waypoint sequencing is continued, and the G1000 automatically activates the next waypoint in the ﬂight plan once the aircraft has crossed the present active waypoint. Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 525 HSI (GPS mode) automatically sequences to the next DTK or HDG value. • The To/From indicator on the HSI ﬂips momentarily to indicate that the midpoint of the turn has been crossed. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 526 - The next leg in the missed approach procedure is not CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF - After any leg in the missed approach procedure that is not CA or FA Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 527 FMS Knobs. Press the ENT Key to accept the selected airport, then follow the steps in the preceding paragraph to select an approach for the new airport. 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 528 APPENDIX D LANK Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 529: Map Symbols
State or Province Border Heliport International Border NAVAIDS Road Item Symbol Railroad Intersection Latitude/Longitude LOM (compass locator at outer marker) NDB (non-directional radio beacon) VOR/DME VOR/ILS VORTAC TACAN 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 530 Trafﬁc 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 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 531 Obstacle within 100 ft of (WARNING) or above aircraft altitude Yellow Obstacle within 1000 ft of (CAUTION) aircraft altitude Obstacle more than 1000 Gray ft below aircraft altitude Obstacle Symbols and Colors 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 532 County Warnings display enabled Cyclone Warnings display enabled Loss of hazard avoidance feature (a white X is shown over the symbol to indicate not available; e.g., trafﬁc symbol) Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 533: Index
Chart Not Available--------------------------------- 8-8, 8-31 Missed ---------------------------------------------------7-46 Chart options -------------------------------------- 8-18, 8-39 Removing---------------------------------------------- 5-105 CHART SETUP Box -------------------------------- 8-24, 8-43 WAAS ----------------------------------------------------7-45 Clearance Recorder---------------------------------------4-35 Approach Mode---------------------------- 7-29, 7-44, 7-45 Closest Point-----------------------------------------------5-89 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 534 Navigation -------------------------------------5-53–5-146 Estimated Landing Fuel -------------------------------- 5-112 Receiver information--------------------------- 1-26–1-28 Estimated Position Error (EPE) --------------------------1-27 GMA 1347------------------------------------------- 1-1, 1-15 Excess Fuel Weight ---------------------------- 5-112, 5-113 GMU 44 ----------------------------------------------------- 1-1 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 535 Normal operating mode ---------------------------------1-16 NO COMP--------------------------------------------------- A-4 Magnetometer -------------------------------------- 1-1, 1-19 Pages-----------------------------------------------------1-31 Panning --------------------------------------------------- 5-9 Obstacles------------------------------------------- A-11, A-13 OBS Mode ----------------------------------------- 2-24–2-25 Symbols--------------------------------------------------- E-1 Marker beacon --------------------------------------------4-24 Odometer --------------------------------------------------1-45 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 536 RX indicator------------------------------------------------- 4-7 Timer Departure------------------------------------------------1-44 Flight -----------------------------------------------------1-44 SafeTaxi------------------------------------------- 8-1, 8-2, 8-4 Timer, PFD generic ----------------------------------------1-42 SafeTaxi database------------------------------------------ 8-5 TOD ------------------------------------- 5-133, 5-134, 5-140 SBAS ------------------------------------ 5-114, 5-116, 5-117 Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...
Page 537 Vertical Speed Reference --------------------------------7-12 Vertical track---------------------------------------------- A-22 VFR code ---------------------------------------------------4-31 VNAV ----------------------------------------------- 5-57, A-19 VNAV Target Altitude----------------------------- 7-16–7-19 VNAV Target Altitude Capture Mode ------------------7-20 VNV ------------------------------------------------- 5-133, C-7 190-00663-00 Rev. A Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT...
Page 538: Index
INDEX LANK Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT 190-00663-00 Rev. A...

This manual is also suitable for:

G1000:beechcraft bonanza G1000

Garmin G1000:Beechcraft Baron 58/G58 User Manual

Revision Information

System Description

Line Replaceable Units (LRU)

G1000 Controls

Secure Digital Cards

System Power-Up

System Operation

Accessing G1000 Functionality

Display Backlighting

Flight Instruments

Flight Instruments

Supplemental Flight Data

PFD Annunciations and Alerting Functions

1 TrafﬁC Annunciation

Abnormal Operations

3 Wind Data

5 DME Information Window (Optional)

7 Minimum Descent Altitude

Section 3 Engine Indication System

EIS Display

EIS Display in Reversionary Mode

Overview

COM Operation

NAV Operation

GTX 33 Mode S Transponders

Additional Audio Panel Functions

Audio Panels Preﬂight Procedure

Abnormal Operation

Section 5 Flight Management

Introduction

Using Map Displays

Aviation Symbols

Waypoints

Airspaces

Direct-To-Navigation

Flight Planning

Vertical Navigation

Procedures

Trip Planning

RAIM Prediction

Navigating a Flight Plan

Abnormal Operation

Section 6 Hazard Avoidance

XM Satellite Weather

Airborne Color Weather Radar

Stormscope WX-500 Series II (Optional)

Terrain Awareness & Warning System (TAWS)

TrafﬁC Information Service (TIS)

Skywatch HP (SKY899) TAS (Optional)

Section 7 Automatic Flight Control System

AFCS Overview

Flight Director Operation

Vertical Modes

Lateral Modes

Autopilot and Yaw Damper Operation

Example Flight Plan

AFCS Annunciations and Alerts

Safetaxi

Chartview

Flitecharts

XM Radio Entertainment (Optional)

Scheduler

Abnormal Operation

Annunciations and Alerts

SD Card Use

Glossary

Frequently Asked Questions

Map Symbols

Index

Index

Quick Links

Chapters

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Summary of Contents for Garmin G1000:Beechcraft Baron 58/G58