Page 1 Beechcraft A36/G36...
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 Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
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 REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00595-00 10/16/06 Initial release Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 7: Table Of Contents
Alerts Window ........4-35 ..........2-22 Clearance Recorder and Player Annunciation Window ...............4-35 ............2-23 Split COM Altitude Alerting ..........4-36 ........2-23 Entertainment Inputs Marker Beacon Annunciations ..........4-37 Reversionary Mode ..........2-24 Trafﬁc Annunciation 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 8 SECTION 6 HAZARD AVOIDANCE ............7-19 Flight Control ....7-20 6.1 XM WX Satellite Weather ........6-1 Engaging the Autopilot and Yaw Damper ..........7-20 Control Wheel Steering ....6-1 Activating XM Weather and Radio Services Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 9 ........A-10 G1000 System Alert Messages SD Card Use ..............B-1 Glossary................C-1 Frequently Asked Questions .........D-1 G1000 Map Datums............E-1 General TIS Information ..........F-1 Map Symbols ..............G-1 INDEX Index.................I-1 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 10 TABLE OF CONTENTS LANK viii Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 11: Section 1 System Overview
Refer to Section 7 for a description of the GFC 700 AFCS. NOTE: The G1000 is an integrated ﬂight deck system that presents ﬂight instrumentation, position, navigation, communication, and identiﬁcation information to the pilot using ﬂat-panel color displays. The system consists of the following Line Replaceable Units (LRUs): •...
Page 12: Line Replaceable Units
NAV/GS) receivers and system integration microprocessors and is paired with the on-side display via an HSDB connection. The IAUs are not paired together and do not communicate with each other directly. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 13 GDC 74 – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.
Page 14 • GSA 81 and GSM 85 – The GSA 81 servos are used for automatic control of pitch, pitch trim, and roll. These units interface with each IAU. The GSM 85 servo mounts are responsible for transferring the output torque of the servo actuators to the mechanical ﬂight-control surface linkages. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 15 �� Figure 1-1 Basic G1000 System Block Diagram 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 16 �� Figure 1-2 G1000 System Block Diagram With Options For information on additional equipment shown in Figure 1-2, consult the applicable optional interface NOTE: user’s guide. This document assumes that the reader is already familiar with the operation of this additional equipment.
Page 17: Secure Digital (Sd) Cards
SYSTEM OVERVIEW 1.3 SECURE DIGITAL (SD) CARDS Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to Appendix B for instructions on updating the aviation database. NOTE: The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels.
Page 18: System Power-Up
Refer to Appendix A for system-speciﬁc annunciations and alerts. NOTE: The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation.
Page 19: System Operation
(EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection. Figure 1-6 G1000 Normal Operation REVERSIONARY DISPLAY OPERATION The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A NOTE: for further information regarding system-speciﬁc alerts.
Page 20: G1000 System Annunciations
Upon G1000 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up. If any instrument remains ﬂagged, the G1000 should be serviced by a Garmin-authorized repair facility.
Page 21: Ahrs Operation
The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs.
Page 22: G1000 Controls
SYSTEM OVERVIEW 1.6 G1000 CONTROLS The G1000 controls have been designed to simplify operation of the system and minimize workload and the time required to access sophisticated functionality. Controls are located on the PFD and MFD bezels and Audio Panel. PFD and MFD controls and softkeys are discussed in this section. See the Audio Panel and CNS Section for more information about Audio Panel and NAV/COM controls.
Page 23 Press to select softkey shown above the bezel key on the PFD/MFD display Keys ALT Knob Sets the Selected Altitude, shown above the Altimeter (the large knob selects the thousands, the small knob selects the hundreds) 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-13...
Page 24: Softkey Function
Figure 1-13 Top-level PFD Softkeys INSET (optional) (optional) DCLTR TRAFFIC TOPO TERRAIN NEXRAD XM LTNG BACK ALERTS Press the OFF or BACK Softkey to 1-14 DCLTR-1 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A return to the top-level softkeys. DCLTR-2...
Page 25 ARC HSI Displays the HSI as a 140° viewable arc (Bearing Information Windows unavailable) STBY CODE IDENT BACK ALERTS Press the BACK Softkey to return to the top-level softkeys. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-15...
Page 26 ATC screen • TMR/REF Displays/removes Timer/References Window • NRST Displays/removes Nearest Airports Window • ALERTS Displays/removes Alerts Window 1-16 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 27 XM LTNG Displays/removes XM lightning information on Navigation Map Page (optional) BACK Returns to top-level softkeys (optional) (optional) TRAFFIC TOPO TERRAIN NEXRAD XM LTNG BACK Press the BACK Softkey to 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-17 return to the top-level softkeys.
Page 28 The DONE Softkey label changes to UNDO The DONE Softkey label changes to UNDO when the checklist item is already checked. CHKLIST when the checklist item is already checked. CHKLIST Figure 1-20 Checklist Softkeys 1-18 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 29: Accessing G1000 Functionality
G1000 In some instances, such as when entering an identiﬁer, the G1000 will try to predict the desired identiﬁer based on the characters being entered. In this case, if the desired identiﬁer appears, use the ENT Key to conﬁrm the entry without entering the rest of the identiﬁer manually.
Page 30: Page Groups
Selecting a page using the FMS Knob: 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob until the desired page is selected. 1-20 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 31 - Approach Information (APR Softkey) - Weather Information (optional) (WX Softkey) Intersection Information NDB Information Airport/Procedures/ Weather Information VOR Information Pages User Waypoint Information Figure 1-24 Waypoint Pages 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-21...
Page 32 FMS Knob, then with the appropriate softkey at the bottom of the page. In this case, the page remains set to the selected page until a different page softkey is pressed, even if a different page group is selected. 1-22 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 33 Figure 1-28 Procedure Loading Pages Information on optional electronic checklist pages is offered later in this section. Checklist pages may be accessed from any page on the MFD using the CHKLIST Softkey. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-23...
Page 34: System Setup And Status
• Map datum • GPS Course Deviation Indicator (CDI) settings • Airspace alerts • COM transceiver channel spacing • Arrival alert • Displayed nearest airports Figure 1-29 System Setup Page 1-24 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 35 ILOT ROFILES System settings conﬁgured on the System Setup Page may be saved under a pilot proﬁle. The G1000 can store up to 25 proﬁles; the currently active proﬁle, the amount of memory used, and the amount of memory available are shown at the top of the System Setup Page in the box labeled ‘Pilot Proﬁle’. From here, pilot proﬁles may be created, selected, renamed, or deleted.
Page 36 2) Press the FMS Knob momentarily to activate the ﬂashing cursor. 3) Turn the large FMS Knob to highlight the time offset ﬁeld in the Date/Time Box. 4) Enter the time offset and press the ENT Key. 1-26 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 37 For use outside the U.S., select the geodetic datum required by that country. If charts based on another datum are being used, the G1000 should be set to use the same datum. Using a map datum that does not match the paper charts can result in signiﬁcant differences in position information. If paper charts are being used for reference only, the G1000 still provides correct navigation guidance to the waypoints contained in the database, regardless of the datum selected.
Page 38 ﬁnal destination (the direct-to waypoint or the last waypoint in a ﬂight plan). Once the set distance (up to 99.9 units) has been reached, an “Arrival at [waypoint]” message is displayed in the PFD Navigation Status Box. 1-28 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 39 • Enroute Safe Altitude (ESA) • Track (TRK) • Estimated Time of Arrival (ETA) • Vertical Speed Required (VSR) • Estimated Time Enroute (ETE) • Crosstrack Error (XTK) 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-29...
Page 40 If a lower CDI range setting is selected (i.e., 1.0 or 0.3 nm), the higher range settings are not selected during any phase of ﬂight. For example, if 1.0 nm is selected, the G1000 uses this for enroute and terminal phases and ramps down to 0.3 nm during an approach.
Page 41 3) Turn the large FMS Knob to highlight the minimum length ﬁeld in the Nearest Airport Box. 4) Enter the minimum runway length (zero to 99,999 feet) and press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-31...
Page 42 The cursor can also be placed in the desired box using the System Status Page Menu. The ANN TEST Softkey, when depressed, causes an annunciation test tone to be played. 1-32 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 43: Electronic Checklists (Optional)
The user cannot edit the checklists. The MFD is able to display electronic checklists customized for the Beechcraft A36/G36. The G1000 accesses the checklists from an SD card inserted into the bezel slot (see Figure 1-3). Selecting the CHKLIST Softkey allows access to all checklists.
Page 44 10) To select a checklist item that is highlighted, press the ENT Key or DONE Softkey. Selected items turn green and checkmarks are placed in the boxes next to the item. After an item is selected, the next item is automatically highlighted for selection. Figure 1-32 Sample Checklist 1-34 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 45: Display Backlighting
9) Turn the small FMS Knob in the direction of the green arrowhead to display ‘MFD KEY’ and repeat steps 4-7. 10) To remove the menu, press the CLR or MENU Key. Figure 1-33 PFD Setup Menu 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1-35...
Page 46 SYSTEM OVERVIEW LANK 1-36 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 47: Section 2 Flight Instruments
AFCS modes. The G1000 System controls were designed so that regardless of which seat the pilot is ﬂying from, the aircraft can be ﬂown with one hand and the controls manipulated with the other hand. Increased situational awareness is provided by replacing the traditional instrument “six-pack”...
Page 48 COM Frequency Box Softkeys AFCS Status Box System Time Navigation Status Box Transponder Data Box Slip/Skid Indicator Selected Heading Bug Attitude Indicator Turn Rate Indicator Figure 2-1 Primary Flight Display (Default) Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 49 Barometric Minimum Descent Altitude Inset Map Annunciation Window DME Information Window Vertical Deviation/Glideslope Indicator Bearing Information Windows Marker Beacon Annunciation Selected Course AFCS Status Annunciation Figure 2-2 Additional PFD Information 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 50: Airspeed Indicator
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 Beechcraft A36/G36 190-00595-00 Rev. A...
Page 51 4) To remove all Vspeed ﬂags, turn the FMS Knob to highlight ‘All References Off’ and press the ENT Key. Restoring all Vspeed defaults: 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight ‘Restore Defaults’ and press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 52: Attitude Indicator
Red extreme pitch warning chevrons pointing toward the horizon are displayed, starting at 50˚ above and 30˚ below the horizon line. Nose High Nose Low Figure 2-8 Pitch Attitude Warnings Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 53: Altimeter
6 seconds at the current vertical speed. The trend vector is not shown if altitude remains constant or if data needed for calculation is not available due to a system failure. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 54 2) Press the STD BARO Softkey. SELECTED ALTITUDE See the AFCS Section for more information about how the G1000 uses the Selected Altitude. NOTE: The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol. A bug corresponding to this altitude is shown on the tape;...
Page 55: Vertical Deviation/Glideslope Indicator
If the rate of ascent/descent exceeds 2000 fpm, the pointer appears at the corresponding edge of the tape and the rate appears inside the pointer. Marker Beacon Annunciation Vertical Speed Vertical Pointer Deviation/ Glideslope Indicator Figure 2-12 Vertical Deviation/Glideslope Indicator Figure 2-13 Vertical Speed Indicator 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 56: Horizontal Situation Indicator (Hsi)
(GPS, VOR, OBS) or a diamond (LOC). Course Pointer Flight Phase Navigation Source Annunciation Course Deviation and Lateral Deviation Scale To/From Indicator Figure 2-15 Arc HSI 2-10 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 57 Turn Rate Arrow Shown Std Turn Rate Trend Vector for Turn Rate > 4 deg/sec Figure 2-18 Standard-Rate Turn Indication Figure 2-17 Turn Rate Indicator and Trend Vector 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-11...
Page 58 3) Press the CDI Softkey a third time to return to GPS. NAV1 Selected for Tuning NAV2 Selected for Tuning VOR2 LOC1 Selected Selected Selected Pressing the CDI Softkey Cycles through Navigation Sources Figure 2-20 Selecting a Navigation Source 2-12 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 59 3) Turn the large FMS Knob to highlight the ‘ILS CDI Capture’ ﬁeld in the ‘GPS CDI’ Box (Figure 2-21). 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. Figure 2-21 System Setup Page, ILS CDI Capture Setting 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-13...
Page 60 OBS Softkey label changes to SUSP. Selecting the SUSP Softkey resumes automatic of approach waypoints. SUSP Annunciation Pressing the SUSP Softkey Suspends Automatic Waypoint Sequencing Figure 2-23 Suspending Automatic Waypoint Sequencing 2-14 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 61 ﬂight and the selected setting is displayed instead of the ﬂight phase annunciation. For example, if 1.0 nm is selected, the G1000 uses this for enroute and terminal phases and ramps down to 0.3 nm during an approach. Receiver Autonomous Integrity Monitoring (RAIM) protection limits follow the selected CDI scale and corresponding ﬂight phases.
Page 62 “NO DATA”. When NAV1 or NAV2 is the selected bearing source, the frequency is replaced by the station identiﬁer when the station is within range. 2-16 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 63 Bearing Source Identiﬁer Selected Bearing Pointer Bearing 1 Bearing 2 Pointer Bearing Source Icon Information Information Icon Source Window Window Figure 2-26 HSI with Bearing and DME Information 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-17...
Page 64: Supplemental Flight Data
REF Softkey. This window provides access to the following settings: • Generic Timer • Vspeed values and ﬂags • Barometric minimum descent altitude (MDA, DH) Figure 2-27 Timer/References Window 2-18 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 65: Outside Air Temperature
3) Turn the large FMS Knob to highlight the ‘Temp’ ﬁeld (Figure 2-30). 4) Turn the small FMS Knob to select the desired unit. 5) Press the ENT Key to conﬁrm selection. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-19...
Page 66: System Time
5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to conﬁrm selection. Figure 2-31 System Setup Page, Date/Time Settings Figure 2-30 System Setup Page, Display Units Settings 2-20 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 67: Pfd Annunciations And Alerting Functions
ADVISORY Softkey annunciation (no aural tone) is used to alert the pilot of any message advisories. The ﬂashing ADVISORY annunciator continues to ﬂash until acknowledged by the pilot (by pressing the ADVISORY Softkey). Figure 2-32 Softkey Annunciation (ALERTS Softkey labels) 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-21...
Page 68: Alerts Window
G1000 message advisory occurs. System alert messages are provided to make the pilot aware of G1000 system problems or status and may not require pilot action. The Alerts Window allows system alerts to be displayed simultaneously. The FMS Knob can be used to scroll through the alert messages.
Page 69: Altitude Alerting
Refer to the Audio Panel and CNS Section for more information on Marker Beacon Annunciations. Outer Marker Middle Marker Inner Marker Altimeter Figure 2-35 Marker Beacon Annunciations 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-23...
Page 70: Trafﬁc Annunciation
FLIGHT INSTRUMENTS TRAFFIC ANNUNCIATION The G1000 System displays trafﬁc symbolically on the Inset Map (PFD), the Navigation Map Page (MFD), and various other MFD page maps. Refer to the Hazard Avoidance Section and Appendix E for more details about the Trafﬁc Information Service (TIS) and optional Trafﬁc Advisory Systems (TAS). When a trafﬁc advisory (TA) is detected, the following automatically occurs: •...
Page 71: Barometric Minimum Descent Altitude
If the aircraft proceeds to climb after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. Within 2500 ft Within 100 ft Altitude Reached Barometric Minimum Bug Barometric Minimum Box Figure 2-38 Barometric Minimum Descent Altitude Alerting Visual Annunciations 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 2-25...
Page 72 FLIGHT INSTRUMENTS LANK 2-26 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 73: Section 3 Engine Indication System (Eis)
Refer to the Pilot’s Operating Handbook (POH) for limitations. NOTE: The G1000 Engine Indication System (EIS) for the Beechcraft A36/G36 displays critical engine, electrical, fuel, and other system parameters on the left side of the Multi Function Display (MFD) during normal operations. In Reversionary Mode, the display unit is re-conﬁgured to present Primary Flight Display (PFD) symbology together...
Page 74: Engine Display
EIS display is currently shown. Beneath the dial gauges are horizontal bar indicators for fuel ﬂow, cylinder head temperature, oil temperature and pressure, alternator load, bus voltage, and fuel quantity. Fuel Flow Leaning Pointer Figure 3-2 Engine Display Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 75 Displays the primary bus voltages for buses 1 and 2 (BUS VOLTS) Fuel Quantity Indicator Displays the amount of fuel in gallons (gal) for each tank (L and R) (FUEL QTY GAL) 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 76: Lean Display
By default, the cylinder with the hottest EGT and CHT is selected (bar indicated in light blue) when the LEAN Softkey is pressed. The readouts below the bar graphs correspond to the selected cylinder. Figure 3-3 Lean Display Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 77 From the Lean Display, press the ASSIST Softkey to identify the peak. The peak temperature for the selected cylinder is indicated with a hollow block on the EGT Bar Graph and the temperature deviation from peak is shown underneath the EGT Bar Graph. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 78: System Display
The System Display is accessed by pressing the ENGINE Softkey followed by the SYSTEM Softkey. Readouts below the Engine Manifold Pressure Gauge and Tachometer are grouped into three categories: System (Oil), Fuel Calculations, and Electrical. Figure 3-4 System Display Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 79 From the System Display, press the DEC FUEL or INC FUEL Softkey to obtain the desired number of gallons remaining (GAL REM). Resetting the fuel totalizer: From the System Display, press the RST FUEL Softkey. This also resets the displayed fuel remaining (GAL REM) to zero. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 80 LANK Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 81: Section 4 Audio Panel And Cns
The Transponder Data Box is located to the left of the System Time Box. The data box displays a four-digit code ﬁeld, a mode ﬁeld, and a reply status indicator (Figure 4-1). 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 82: Pfd/Mfd Controls And Frequency Display
AUDIO PANEL AND CNS PFD/MFD CONTROLS AND FREQUENCY DISPLAY Figure 4-1 PFD/MFD Controls, COM/NAV Frequency Tuning Boxes, and DME Tuning Window (PFD Shown) Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 83 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 transponder. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 84: 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 – Not used in A36/G36 aircraft. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 85 PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. Reversionary Mode Button – Pressing manually selects Reversionary Mode. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 86: Com Operation
During PA Mode, the COM MIC annunciator is extinguished and the COM active frequency color is NOTE: white, indicating that the COM transmitter is inactive. When turning on the G1000 for use, the system remembers the last frequencies used and the active NOTE: COM transceiver state prior to shutdown.
Page 87: Stuck Microphone
An alert appears on the PFD to advise the crew of a stuck microphone. The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel continues to ﬂash as long as the PTT Key remains stuck. Figure 4-5 Stuck Microphone Alert 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 88: Com Transceiver Manual Tuning
ﬁelds. Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other Figure 4-7 Switching COM Tuning Boxes Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 89: Com Tuning Failure
In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver. Press for Two Seconds to Load 121.500 MHz Figure 4-9 Quickly Tuning 121.500 MHz 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 90: Auto-Tuning The Com Frequency
4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Press the NRST Softkey to Open the Nearest Airports Window Figure 4-10 Nearest Airports Window (PFD) 4-10 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 91 9) Press the ENT Key to load the COM frequency into the standby ﬁeld of the selected COM radio. 10) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Figure 4-12 Nearest Pages PAGE MENU 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-11...
Page 92 Press ENT Key to Load Frequency into COM Standby Field. Cursor then Advances to Next Frequency. Press INFO Softkey for AIRPORT, RUNWAYS, and FREQUENCIES Figure 4-13 WPT – Airport Information Page Windows 4-12 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 93 NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key and the FMS Knob. Figure 4-14 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-13...
Page 94: Frequency Spacing
AUDIO PANEL AND CNS FREQUENCY SPACING The G1000 COM radios can tune either 25 kHz spacing (118.000 to 136.975 MHz) or 8.33 kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel conﬁguration. When 8.33 kHz channel spacing is selected, all of the 25 kHz channel spacing frequencies are also available in the complete 3040 channel list.
Page 95: Automatic Squelch
Volume level indication remains for two seconds after the change. COM Volume Level Remains for Two Seconds Figure 4-18 COM Volume Level 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-15...
Page 96: Nav Operation
Figure 4-19 Selecting a NAV Radio for Navigation See the Flight Instruments Section for selecting the bearing information windows (VOR) and using VOR as the source for the bearing pointer. 4-16 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 97: 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 4-21 NAV Frequency Tuning 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-17...
Page 98 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 4-24 NAV Volume Levels 4-18 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 99: Auto-Tuning The Nav Frequency
Highlighted Frequency into the NAV Standby Turn the FMS Frequency Box Knob to Scroll Through a List of Frequencies Figure 4-25 NAV Frequency Auto-Tuning from the MFD 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-19...
Page 100 10) Press the ENT Key to load the COM frequency into the standby ﬁeld of the selected COM radio. 11) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Figure 4-26 Nearest Pages PAGE MENU 4-20 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 101 Press the FREQ Softkey to Place Softkey to Place the Cursor on the the Cursor on the VOR Identiﬁer VOR Frequency Figure 4-27 NRST – Nearest VOR Page 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-21...
Page 102 MENU Key, the FMS Knob, and the ENT Key. Figure 4-28 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and NRST – Nearest Airports Pages 4-22 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 103 ﬁeld, the standby frequency is transferred to active. • If the current CDI source is NAV1 or NAV2, the approach frequency is transferred to the standby frequency ﬁelds of the selected CDI NAV radio. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-23...
Page 104: Marker Beacon Receiver
HI SENS function (annunciator illuminated) is used to receive 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 A36/G36 190-00595-00 Rev. A...
Page 105: Dme Tuning (Optional)
NAV2, or HOLD state prior to shutdown. The G1000 System tunes the optional DME transceiver. The UHF DME frequency is tuned by pairing with a VHF NAV frequency. DME frequency pairing is automatic and only the VHF NAV frequency is shown.
Page 106: Gtx 33 Mode S Transponder
Pressing 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 softkey inactivity, the system reverts back to the top-level softkeys. 4-26 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 107: Transponder Mode Selection
Transponder Data Box. In Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations. Mode Figure 4-33 Ground Mode 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-27...
Page 108 If Altitude Mode is selected, a green ‘ALT’ indication and transponder code appear in the mode ﬁeld of the Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure altitude information. ALT Mode (Mode C Altitude Reporting) Figure 4-36 Altitude Mode 4-28 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 109 VFR Softkey. When the VFR Softkey is pressed, the pre-programmed VFR code is automatically displayed in the code ﬁeld of the Transponder Data Box. Pressing the VFR Softkey again restores the previous identiﬁcation code. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-29...
Page 110 ‘IDENT’ indication is displayed in the mode ﬁeld of the Transponder Data Box for a duration of 18 seconds. When the IDENT Softkey is pressed while in Mode or Code Selection, the system reverts to the top-level softkeys. IDNT Indication Figure 4-39 IDENT Indication 4-30 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 111: Flight Id Reporting
AUDIO PANEL AND CNS FLIGHT ID REPORTING If the Flight ID is required but the system is not conﬁgured for it, contact a Garmin-authorized service NOTE: center for conﬁguration. When the ﬂight crew must enter the Flight ID before ﬂight operation, the number is entered in the Timer/ References Window.
Page 112: Additional Audio Panel Functions
Speaker audio is muted when the PTT is pressed. Certain aural alerts and warnings (autopilot, trafﬁc, altitude) are always heard on the speaker, even when the speaker is not selected. The speaker volume is adjustable within a nominal range. Contact a Garmin-authorized service center for volume adjustment.
Page 113: Intercom
The passengers are isolated from the pilot and copilot but can communicate with each other. When both the PILOT and the COPLT Annunciators are extinguished, everyone hears the selected radios and is able to communicate with everyone else. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-33...
Page 114: Passenger Address (Pa) System
When PA is selected on the Audio Panel, the COM MIC Annunciator is extinguished, and the active COM frequency changes to white, indicating that there is no COM selected. The PA Annunciator ﬂashes about once per second while the PTT is depressed. 4-34 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 115: Clearance Recorder And Player
When Split COM Operation is selected, COM1 is used by the pilot and COM2 is used by the copilot. The COM1 MIC Annunciator ﬂashes when the pilot’ s microphone PTT is pressed. The COM2 MIC Annunciator ﬂashes when the copilot’ s microphone PTT is pressed. 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-35...
Page 116: Entertainment Inputs
For example, if passengers prefer their own music while the pilot listens to the Data Link Receiver, the entertainment audio should be connected to the MUSIC 2 jack. 4-36 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 117: Reversionary Mode
ﬂight and engine information on both the PFD and MFD, in case of display failure. See the System Overview Section for more information. Figure 4-45 Reversionary Mode Button 190-00595-00 Rev A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 4-37...
Page 118 ICS system as well as during COM transmissions. After powering up the G1000 System, the following steps will aid in maximizing the use of the Audio Panel as well as prevent pilot and copilot induced issues. These preﬂight procedures should be performed each time a pilot boards the aircraft to insure awareness of all audio levels in the Audio Panel and radios.
Page 119: Section 5 Gps Navigation
SECTION 5 GPS NAVIGATION 5.1 INTRODUCTION This section of the Pilot’ s Guide provides GPS navigation operating procedures for the G1000 installed in the Beechcraft A36/G36 aircraft. Some prior knowledge of the other sections of the G1000 Pilot’ s Guide, especially the “how-to”...
Page 120: Navigation Map (Mfd)
NAVIGATION MAP PAGE Figure 5-1 Navigation Map Page (not all map display items shown) The Navigation Map can be quickly displayed from any page in the G1000 by pressing and momentarily NOTE: holding the CLR key. The Navigation Map Page (Figure 5-3) is the ﬁrst page in the Map Page Group and provides the following GPS Navigation display capability: •Map display showing airports, NAVAIDS, airspaces, land data (highways, cities, lakes, rivers, borders, etc.)
Page 121 Within the Map Setup Option there are ﬁve setup groups (Figure 5-3): • Map • Weather (refer to the Hazard Awareness Section) • Trafﬁc (refer to the Hazard Awareness Section) • Aviation • Land 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 122 • Desired Track Up (DTK up) ﬁxes the top of the map display to the desired course. • Heading Up (HDG up) ﬁxes the top of the map display to the current aircraft heading. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 123 3) Select the ‘Map’ group. 4) Press the ENT Key. 4) Highlight the ‘LAND DATA’ ﬁeld. 5) Select ‘On’ or ‘Off.’. 6) Press the FMS Knob to return to the Navigation Map Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 124 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TRACK VECTOR’ ﬁeld. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 125 The Nav Range Ring (Figure 5-6) shows the direction of travel (ground track) on a rotating compass card. The range of the Nav Ring is determined by the map range: 125 feet (500 feet map range) to 500 nm (2000 nm map range). 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 126 5) Highlight the range ﬁeld. TOPO ranges are from Off to 2000 nm. 6) To change the TOPO range setting, turn the small FMS Knob to display the range list. 7) Select the desired range. 8) Press the ENT Key. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 127 Obstacle Data Obstacles Figure 5-7 Obstacle Data Refer to the Hazard Awareness Section for a complete description of obstacle data including how to display it on the Navigation Map Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 128 Refer to the Hazard Awareness Section for information pertaining to the setup and display of the Weather group options. RAFFIC ROUP Refer to the Hazard Awareness Section for information pertaining to the setup and display of the Trafﬁc group options. 5-10 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 129 • Small: off - 100 nm • Runway Extension (RWY EXTENSION) - The zoom range sets the maximum range at which runway extensions appear on the display: • Off - 100 nm 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-11...
Page 130 6) Select the desired text size. 7) Press the ENT Key to accept the selected text size. 8) Press the FMS Knob to return to the Navigation Map Page. 5-12 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 131 6) Select the desired range (RNG). 7) Press the ENT Key to accept the selected option. 8) Press the FMS Knob to return to the Navigation Map Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-13...
Page 132 • LARGE CITY (approximate populations greater than 200,000): off - 1500 nm • MEDIUM CITY (approximate populations greater than 50,000): off - 200 nm • SMALL CITY (approximate populations greater than 5,000): off - 50 nm 5-14 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 133 5) Select the desired land option. 6) Select the desired range. 7) Press the ENT Key to accept the selected option. 8) Press the FMS Knob to return to the Navigation Map Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-15...
Page 134 Navigation Map Page and represents the top-to- bottom distance covered by the map . To change the map range turn the JOYSTICK counter-clockwise to zoom in, or clockwise to zoom out. 5-16 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 135 SUA Group 5 Trafﬁc Symbols Local Roads SUA Group 6 Trafﬁc Labels Local Road Labels SUA Group 7 Railroads Obstacles Major Political Boundaries Table 5-1 Map Declutter Levels 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-17...
Page 136 3) Push in the JOYSTICK to remove the arrow and return to the present position. 5-18 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 137 5) If desired, enter the identiﬁer of the reference waypoint and the radial and distance to the reference waypoint. 6) Press the ENT Key to accept. 7) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-19...
Page 138 GPS NAVIGATION ISPLAYING OPOGRAPHIC ATA ON THE 5-20 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 139 • True Airspeed (TAS) • Track angle error (TKE) • Track angle (TRK) • Vertical speed required (VSR) • Cross track error (XTK) • Currently selected MFD page title 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-21...
Page 140 Navigation Map. Pressing the ENT Key at any location with the ‘Measure’ option enabled allows bearing and distance from the newly selected position to be acquired. 5-22 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 141 5) To exit the Measure Bearing/Distance option, push in the joystick or select ‘Stop Measuring’ from the page menu. 6) Press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-23...
Page 142: Pfd Inset Map And Windows
• Aircraft icon • TOPO data • Trafﬁc data • Weather data • Terrain data • Indication of which map features are enabled • Active navigation ﬂight plan 5-24 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 143: Pfd Windows
GPS navigation: • Nearest Airports • Direct-to • Flight Plan • Procedures Window Location Figure 5-17 PFD Window Location 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-25...
Page 144 This feature applies to everything displayed on the map except for route lines. 3) Push in the JOYSTICK to cancel the panning function and return to the present position on the map. 5-26 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 145: Direct-To-Navigation (Mfd)
The “direct-to” navigation feature provides a quick method of setting a GPS course to a destination waypoint. Once a direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the selected direct-to destination. Course guidance is provided until the direct-to is cancelled or replaced by a new destination.
Page 146 3) Enter the facility or city location of the desired waypoint. If duplicate entries exist for the entered facility or city name, additional entries can be viewed by turning the small FMS Knob during the selection process. 5-28 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 147 SPECIFYING A COURSE TO A WAYPOINT When navigating a direct-to, the G1000 sets a direct great circle course to the selected destination. The course to a destination can also be manually selected using the course ﬁeld (‘COURSE’) on the Direct-to Waypoint Window.
Page 148 Once a direct-to is activated, the G1000 provides navigation guidance to the selected destination until the direct-to is either replaced with a new direct-to or ﬂight plan, cancelled, or when the G1000 is powered off. Figure 5-23 Cancel Direct-to Option Cancelling a direct-to: 1) Press the Direct-to Key to display the Direct-to Window.
Page 149 5) If the map pointer is placed on an open location, press the Direct-to Key. 6) Press the ENT Key twice to create a ‘MAPWPT’ waypoint and then navigate to it (Figure 5-24). 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-31...
Page 150: Direct-To Navigation Shortcuts Using The Fms Knob
4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to. 5-32 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 151 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-33...
Page 152: Direct-To-Navigation (Pfd)
3) Turn the small FMS Knob to begin selecting the desired identiﬁer, location, etc. 4) Press the ENT Key. 5) The cursor is now ﬂashing on ‘ACTIVATE?’. If no altitude constraint or course is desired, press the ENT Key to activate. 5-34 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 153 3) Turn the small FMS Knob to display a selection window showing all waypoints in the active ﬂight plan. 4) Scroll through the list and highlight the desired waypoint. 5) Press the ENT Key twice to activate the direct-to. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-35...
Page 154 1) Press the Direct-to Key. 2) Press the MENU Key to display the Direct-to Menu. 3) Press the ENT Key to cancel direct-to navigation. If a ﬂight plan is still active, the G1000 resumes navigating the ﬂight plan along the closest leg of ﬂight.
Page 155: Airport Information (Mfd)
2) Select the identiﬁer, facility name or city location ﬁeld. 3) Enter the desired identiﬁer, facility name, or city location. 4) Press the ENT Key. 5) To remove the ﬂashing cursor, press the FMS Knob . 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-37...
Page 156 GPS NAVIGATION DUPLICATE WAYPOINTS As an identiﬁer, facility name or location is entered, the G1000’ s Spell’N’Find™ feature scrolls through the database, displaying those waypoints matching the characters which have been entered to that point. If duplicate entries exist for the entered facility name or location, additional entries may be viewed by continuing to turn the small FMS Knob during the selection process.
Page 157 ASOS Class B AWOS Class C Center Clearance Departure Gate Control Terminal Ground TRSA Helicopter Multicom Pre-Taxi Radar Ramp Other Tower Unicom Table 5-2 Frequency Descriptions and Abbreviations 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-39...
Page 158 Airport Information Window. The map image range is displayed in the lower left corner and is adjustable using the joystick. For airports with multiple runways, information for each runway is available. 5-40 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 159 5) If desired, enter the identiﬁer of the reference waypoint and the radial and distance to the reference waypoint. 6) Press the ENT Key to accept. 7) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-41...
Page 160: Intersection Information (Mfd)
1) With the Intersection Information Page displayed, press the FMS Knob to activate the cursor. 2) Enter a name for the identiﬁer. 3) Press t he ENT Key. 4) Press the FMS Knob to remove the ﬂashing cursor. 5-42 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 161: Ndb Information (Mfd)
2) Highlight the desired selection ﬁeld (identiﬁer, name or closest city). 3) Enter an identiﬁer, name or city. 4) Press t he ENT Key. 5) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-43...
Page 162: Vor Information (Mfd)
2) Highlight the desired selection ﬁeld (identiﬁer, name or closest city). 3) Enter an identiﬁer, name or city. 4) Press t he ENT Key. 5) Press the FMS Knob to remove the ﬂashing cursor. 5-44 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 163: User Waypoint Information (Mfd)
5) Highlight the latitude/longitude ﬁeld or the Reference Waypoints ﬁeld, depending on how the waypoint is to be deﬁned. 6) Enter the position coordinates or the radial and distance from the reference waypoint. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-45...
Page 164 3) Turn the small FMS Knob to make changes. 4) Press the ENT Key to accept the changes. 5) Press the FMS Knob to remove the ﬂashing cursor. 5-46 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 165 1) Select the User Waypoint Information Page and press the MENU Key. 2) Ensure waypoint is selected. 3) Select ‘Use Present Position’. 4) Press the ENT Key. 5) Highlight the position and press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-47...
Page 166 3) The user waypoint ﬁeld is highlighted. Rename the user waypoint. 4) Press the ENT Key. 5) The message ‘Would you like to rename the user waypoint’ is displayed. Select ‘YES’ to rename the new user waypoint. 5-48 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 167: Nearest Airports (Mfd)
Runway (or soft surface, if no hard surface runway exists) Primary Communications Frequency and Type Nearest Airport Displayed on Map Most Precise Approaches Available Figure 5-37 Nearest Airports Page 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-49...
Page 168 3) Press the ENT Key. The selected frequency is placed in the COM standby frequency tuning box. 4) Press the F REQUENCY TRANSFER Key to place the frequency in the active ﬁeld. 5) Press the FMS Knob to remove the ﬂashing cursor. 5-50 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 169 5) Press the FREQUENCY TRANSFER Key to place the frequency in the active ﬁeld. 6) Press the FMS Knob to remove the ﬂashing cursor. Figure 5-38 Nearest Airport Page Menu 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-51...
Page 170: Nearest Intersections (Mfd)
Selecting a nearest intersection from the Nearest Intersections Page: 1) Press the FMS Knob to activate the cursor. 2) Select the desired intersection. The information on the Nearest intersection Page pertains to the selected intersection. 5-52 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 171: Nearest Ndb (Mfd)
Selecting an NDB from the Nearest NDB Page: 1) Press the FMS Knob to activate the cursor. 2) Select the desired NDB. The information on the Nearest NDB Page pertains to the selected NDB. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-53...
Page 172: Nearest Vor (Mfd)
1) With the Nearest VOR Page displayed, press the VOR Softkey to place the cursor in the ‘NEAREST VOR’ window. 2) Turn the FMS Knob to select a VOR. 3) Press the FMS Knob to remove the ﬂashing cursor. 5-54 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 173 2) Select the option ‘Select Frequency Window’ and press the ENT Key. The cursor is placed in the ‘FREQUENCY’ ﬁeld. 3) Select the desired frequency. 4) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-55...
Page 174: Nearest User Waypoint (Mfd)
A map of the currently selected user waypoint and surrounding data is displayed which at a minimum shows the selected user waypoint and the current aircraft position. A line is drawn between the current position and the selected user waypoint. 5-56 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 175 2) Turn the FMS Knob to select the desired waypoint. The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint. 3) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-57...
Page 176: Nearest Frequencies (Mfd)
If there is no database loaded or if there are no stations in range, then any or all of the lists may be empty with the display indicating as such. 5-58 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 177 4) Turn the large FMS Knob to select the desired ARTCC frequency. 5) Press the ENT Key to load the frequency into the COM frequency standby ﬁeld. Figure 5-45 Nearest Frequencies Page Menu 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-59...
Page 178 3 ) Turn the FMS Knob to select the desired nearest WX frequency. 4 ) Press the ENT Key to load the WX frequency into the COM frequency standby ﬁeld. 5) Press the FMS Knob to remove the ﬂashing cursor. 5-60 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 179: Nearest Airspaces (Mfd)
5.17 NEAREST AIRSPACES (MFD) The G1000 alerts the pilot to as many as nine controlled or special use airspaces (three at the most at one time) near or in the ﬂight path. The airspace name, class, controlling agency, vertical limits and associated frequencies are displayed for the selected airspace.
Page 180 Ahead, or Ahead < 2nm, otherwise “__:__:__” is used) is displayed. If there are more than three airspace alerts they are displayed in a scrollable list box with only three visible at one time. 5-62 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 181 An altitude buffer is also provided on the System Setup Page to provide an extra margin of safety above or below the published limits. See the System Overview Section for additional details. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-63...
Page 182 If there are more than three frequencies for an airport waypoint index then they are displayed in a scrollable list box with only three visible at a time. 5-64 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 183: Nearest Airports (Pfd)
Facility Name City, State Airport Usage Type (e.g. public, private, military, heliport) Elevation Region Fuel Types Available (AV Gas, Jet) Position Field UTC Time Figure 5-48 Airport Information Window 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-65...
Page 184 From the Nearest Airports Window, highlight the desired frequency, then press the ENT Key. The frequency is placed in the standby COM frequency ﬁeld in the COM Tuning Box. COM Frequency Figure 5-50 COM Frequency 5-66 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 185: Flight Planning (Mfd)
6) Enter the identiﬁer for each additional ﬂight plan waypoint. 7) Once all waypoints have been entered, press the FMS Knob to store the ﬂight plan and return to the Flight Plan Catalog Window. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-67...
Page 186 Flight Plan (Figure 5-52). Direct-To Waypoint Identiﬁer, Facility, Symbol, City Departure Waypoint Destination Waypoint Total Flight Plan Distance Enroute Safe Altitude Figure 5-52 Flight Plan Information 5-68 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 187 1) Press the FMS Knob from the Active Flight Plan Page. 2) Highlight the Flight Plan Title Field. 3) Turn the FMS Knobs to change/edit the title (Figure 54). 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-69...
Page 188 2) Press the MENU Key. 3) Select ‘Activate Leg’ (Figure 5-56). 4) Press the ENT Key. An ‘Activate’ window is displayed. 5) With ‘Activate’ highlighted, press the ENT Key. 5-70 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 189 ﬂight plan is activated. When storing ﬂight plans with an approach, departure or arrival, the G1000 uses the waypoint information from the current database to deﬁne the waypoints. If the database is changed or updated, the G1000 automatically updates the information if the procedure has not been modiﬁed.
Page 190 5) Press the ENT Key. 6) The G1000 displays the location, lat/lon, bearing (BRG), and distance (DIST) to the closest point along the ﬂight plan from the selected reference waypoint. To create a user waypoint at this location and add it to the ﬂight plan, highlight ‘LOAD’...
Page 191 4) With ‘OK’ highlighted, press the ENT Key to copy the ﬂight plan. To cancel, highlight ‘CANCEL’ and press the ENT Key. Figure 5-58 Copy a Flight Plan 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-73...
Page 192 2) Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all ﬂight plans?’ conﬁrmation window is displayed. 3) With ‘OK’ highlighted, press the ENT Key to delete all ﬂight plans. To cancel, highlight ‘CANCEL’ and press the ENT Key. 5-74 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 193 5) If desired, enter the identiﬁer of the reference waypoint and the radial and distance to the reference waypoint. 6) Press the ENT Key to accept. 7) Press the FMS Knob to remove the ﬂashing cursor. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-75...
Page 194: Vertical Navigation
6) Select whether the previously set distance is ‘Before’ or ‘After’ the endpoint. 7) Press the ENT Key. The cursor is now placed over the VNAV proﬁle endpoint ﬁeld. 5-76 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 195 The VNAV mesages (Figures 5-60 and 5-61) will only be displayed if the VNAV messages are enabled. NOTE: Press the MENU key on the VNAV Page to enable or disable the messages. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-77...
Page 196 To view the vertical speed required on any MFD Page, a ﬁeld in the Navigation Status Bar must be conﬁgured to display VSR (Figure 5-63, see the System Setup Page Instructions for details). Figure 5-63 Vertical Navigation Page Menu 5-78 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 197: Flight Planning (Pfd)
• Store, invert, or delete ﬂight plan • Load or remove departure, arrival, or approach • Closest Point of FPL • Restore defaults • Parallel track Figure 5-65 Flight Plan Page Menu 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-79...
Page 198 2) Highlight the desired destination waypoint. 3) Press the MENU Key. 4) Highlight ‘Activate Leg’. 5) Press the ENT Key. A conﬁrmation window is displayed with ‘ACTIVATE’ highlighted. 6) Press the ENT Key. 5-80 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 199 GPS NAVIGATION STORE FLIGHT PLAN The active ﬂight plan is erased when the G1000 is powered off or when another ﬂight plan is activated. When storing ﬂight plans with an approach, departure or arrival, the G1000 uses the waypoint information from the current database to deﬁne the waypoints in the ﬂight plan.
Page 200 3) Press the ENT Key. A window appears with the reference waypoint ﬁeld highlighted. 4) Enter the identiﬁer of the reference waypoint. 5) Press the ENT Key. The G1000 displays the bearing (BRG) and distance (DIS) to the closest point along the ﬂight plan from the selected reference waypoint.
Page 201: Procedures (Mfd)
10) With ‘LOAD’ highlighted, press the ENT Key. The departure procedure is displayed as part of the overall ﬂight plan and is placed in front of the enroute ﬂight plan. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-83...
Page 202 10) Press the FMS Knob to remove the cursor. Identiﬁer Facility Name Location Available Departures Available Runways Available Transitions List of Legs in Departure Sequence Figure 5-67 Departure Loading Page 5-84 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 203 3) Highlight ‘View Departure Airport’. 4) Press the ENT Key. The Departure Information Page is displayed. 5) Enter an identiﬁer, facility, or city name for the departure airport. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-85...
Page 204 9) With ‘LOAD’ highlighted, press the ENT Key. The arrival procedure is displayed as part of the overall ﬂight plan and is placed at the end of the enroute ﬂight plan. 5-86 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 205 3) Press the ENT Key. A conﬁrmation window is displayed listing the procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-87...
Page 206 ‘ACTIVATE?’ will enter the selected approach procedure into the active ﬂight plan and make it immediately active. 8) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’. 9) Press the ENT Key. 5-88 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 207 7) Press the ENT Key. The ‘LOAD?’ ﬁeld is highlighted. 8) Press the ENT Key to load the approach. If navigating a ﬂight plan previous to loading this approach, the G1000 will continue navigating the ﬂight plan until the approach is activated.
Page 208 1) Press the PROC Key. 2) Highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. A conﬁrmation window will be displayed. 4) With ‘ACTIVATE’ highlighted, press the ENT Key. 5-90 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 209: Procedures (Pfd)
SELECT DEPARTURE ‘Select Departure’ selects a published standard instrument departure (SID) for the departure airport or replaces the current departure with a new selection. When using a direct-to, the G1000 uses the nearest airport as a reference when displaying available departures.
Page 210 ‘SELECT ARRIVAL’ selects a published standard terminal arrival route (STAR) for the destination airport or replaces a current arrival with a new selection. Available Transitions Available Arrivals Figure 5-73 Selecting an Arrival 5-92 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 211 9) Pr ess the ENT Key. A window appears listing the available runways for the arrival. 10) Select the desired runway. 11) Wi th ‘LOAD?’ highlighted, press the ENT Key to load the arrival. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-93...
Page 212 NOTE: If the approach is not approved for GPS, a ‘NOT APPROVED FOR GPS’ message is displayed with ‘YES’ highlighted. Press the ENT Key to acknowledge the message. To cancel the approach, select ‘NO’ and press the ENT Key. 5-94 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 213 Activating the approach with vectors to ﬁnal: 1) From an active ﬂight plan, press the PROC Key to display the Procedures Options Window. 2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’. 3) Press the ENT Key. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 5-95...
Page 214 GPS NAVIGATION Blank Page 5-96 Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 215: Section 6 Hazard Avoidance
HAZARD AVOIDANCE SECTION 6 HAZARD AVOIDANCE The hazard avoidance features available for the G1000 system are designed to aid situational awareness and provide advisory information with regard to potential hazards to ﬂight safety associated with weather, terrain, and air trafﬁc.
Page 216 6) Press the DONE Softkey. 7) Turn the large FMS Knob to highlight ‘YES’. 8) To complete activation, press the ENT Key. XM Satellite Radio activation instructions are also available at www.garmin.com (P/N 190-00355-04). Data Audio Radio ID (for XM...
Page 217: Using Xm Wx Satellite Weather Products
The Weather Data Link Page is in the Map group of pages. It is the primary starting point for viewing weather data because it can display all available XM weather products. No other G1000 page can display all XM weather products.
Page 218 It does not represent the rate at which weather data is updated or new content is received by the Data Link Receiver. Weather data is updated at intervals that are deﬁned and controlled by XM Satellite Radio and its data vendors. Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 219: Weather Softkeys On The Weather Data Link Page
When a weather product is selected for display, the corresponding softkey label changes to gray. This indicates that the product is enabled. Unavailable weather products have dimmed (disabled) softkey labels. Figure 6-3 Weather Softkeys 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 220 Never use NEXRAD data or any radar data to penetrate hazardous weather. Rather, use it in an early-warning capacity of pre- departure and enroute evaluation. Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 221 Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reﬂectivity from the individual radar sweeps. The display of the information is color-coded to indicate the weather severity level. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 222 (designated by the letter Z). The value of Z increases as the returned signal strength increases. Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 223 • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows • Metallic dust from military aircraft, which can cause alterations in radar scans 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 224 When Echo Tops is activated, NEXRAD and Cloud Tops are removed. Displaying Echo Tops information: 1) Select the Weather Data Link Page. 2) Press the ECHO TOPS Softkey. Echo Tops data displays only on the Weather Data Link Page. 6-10 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 225 Cloud Tops data (Figure 6-9) shows the altitude at the top of the clouds. This is determined from satellite imagery. Figure 6-9 Cloud Tops Data Displaying Cloud Tops information: 1) Select the Weather Data Link Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-11...
Page 226 • PFD Inset Map • Nearest Pages • Weather Data Link Page • AUX - Trip Planning Page • Navigation Map • Flight Plan Pages (except VNAV) 6-12 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 227 Press the CELL MOV Softkey to show the storm cells on the Weather Data Link Page. Using the Map Setup Window, Cell Movement data displays on the following maps: 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-13...
Page 228 Convective SIGMET is issued for hazardous convective weather. A localized SIGMET is a signiﬁcant weather condition occurring at a localized geographical position. SIGMET AIRMET Figure 6-15 SIG/AIR Data SIGMET and AIRMET data display on the Weather Data Link Page (Figure 6-15). 6-14 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 229 To display the SIGMET and AIRMET legend (Figure 6-16), select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Figure 6-16 SIGMET/AIRMET Legend Figure 6-17 shows sample SIGMET text. Figure 6-17 Sample SIGMET Text 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-15...
Page 230 TAF text. 3) Press the FMS Knob or the CLR Key to return to the Weather Data Link Page if the airport was selected by panning from this page. 6-16 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 231 Figure 6-18 METAR and TAF Text on the Weather Information Page To display the METAR legend (Figure 6-19), press the LEGEND Softkey when METARs are selected for display. Figure 6-19 METAR Legend 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-17...
Page 232 3) Press 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. 6-18 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 233 Figure 6-25 Freeze Level Data Displaying Freeze Level information: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the FRZ LVL Softkey. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-19...
Page 234 HAZARD AVOIDANCE Freeze Level data displays on the Weather Data Link page only. It does not display on other G1000 maps. To display the Freeze Level legend (Figure 6-26), press the LEGEND Softkey when Freeze Level is selected to be displayed.
Page 235 Figure 6-27 Winds Aloft Data at 27,000 Feet To display the Winds Aloft legend (Figure 6-28), select the LEGEND Softkey when Winds Aloft is selected for display. Figure 6-28 Winds Aloft Data with Legend 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-21...
Page 236 2) Press the MORE WX Softkey. 3) Press the COUNTY Softkey. County warnings display only on the Weather Data Link Page. They do not display on other G1000 maps. To display the County legend (Figure 6-30), press the LEGEND Softkey when County warnings are selected to be displayed.
Page 237: Setting Up The Weather Data Link Page
3) Press the CYCLONE Softkey. Cyclone data displays only on the Weather Data Link Page. It does not display on other G1000 maps. To display the Cyclone legend (Figure 6-31), press the LEGEND Softkey when Cyclones are selected to be displayed.
Page 238 Figure 6-33 shows the Data Link Setup Window. The ‘ON’ and ‘OFF’ settings control the display of weather products the same way that softkeys do. Winds Aloft Data Selected Figure 6-33 Data Link Setup Window 6-24 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 239 4) Turn the small FMS Knob to move between the options for each product (for example, ‘Yes’, ‘No’, or Map Range). 5) Press the ENT Key to select an option. 6) Press the MENU Key to restore the default settings. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-25...
Page 240 AIRMETs, County Warnings, TFRs (Temporary Flight Restrictions), Echo Tops, METARs, SIGMETs, and Cell Movement displays text information for the selection. This information is displayed in the same location as the map pointer information on the Navigation Map Page. 6-26 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 241: Setting Up Xm Weather On The Navigation Map
NAVAIDS, obstacles, and other ground references. NEXRAD Weather NEXRAD and XM Lightning Icons, 500 nm Map Range Figure 6-35 Navigation Map Page Displaying NEXRAD Weather 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-27...
Page 242 Use the Map Setup Window (Figure 6-36) to customize the display of weather data on the Navigation Map Page. The Map Setup Window settings control the display of weather data on all G1000 pages except the Weather Data Link Page.
Page 243: Stormscope (Wx-500)
The Stormscope system is not intended for hazardous thunderstorm penetration. Weather information NOTE: on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 User’s Guide for a detailed description of Stormscope operation. The following pages can display Stormscope data: •...
Page 244 Strike mode indicates the approximate location of lightning strikes. • STRMSCP SMBL – Selects the range at which Stormscope data displays. Figure 6-37 Page Menu Figure 6-38 Map Setup Menu 6-30 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 245 If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn (Figure 6-40). This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-31...
Page 246 Figure 6-41 Lightning Display Range Annunciation The maximum zoom range can also be set on the Navigation Map. Note that Stormscope data above the selected maximum zoom range is decluttered. 6-32 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 247: Selecting The Stormscope Page
Adjusting the Stormscope Map Range: 1) Select the Stormscope Page. 2) To change the map range, turn the Joystick clockwise to zoom out or counter-clockwise to zoom in. Figure 6-42 Stormscope Page 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-33...
Page 248 3) Select ‘Clear Stormscope Lightning’. 3) Press the ENT Key. OR : 1) Select the Stormscope Page. 2) Press the CLEAR Softkey. Figure 6-43 Navigation Map Page Options Menu 6-34 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 249 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. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-35...
Page 250: Terrain Proximity
3-D GPS position. GPS POSITION AND GPS-MSL ALTITUDE The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite position. GPS altitude is then converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used to determine terrain and obstacle proximity.
Page 251: Displaying Terrain Proximity Data
Obstacle above or within 100 ft below the aircraft altitude Obstacle between 100 ft and 1000 ft below the aircraft altitude Table 6-5 Terrain Proximity Terrain/Obstacle Colors and Symbology 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-37...
Page 252 Obstacles with heights greater than 200 feet above ground level (AGL) are displayed in three color levels (Table 6-5). The G1000 adjusts colors automatically as the aircraft altitude changes. Terrain Proximity may also be deselected from the Inset Map without affecting the terrain display on the MFD maps.
Page 253: Terrain Proximity Page
Yellow Terrain (Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Red Terrain (Terrain Above or Within 100’ Below the Terrain Aircraft Altitude) Legend Figure 6-45 Terrain Proximity Page 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-39...
Page 254 Other aviation information such as airports, VORs, and other NAVAIDS can be displayed on the Terrain Proximity Page. Showing or hiding aviation information: 1) Press the MENU Key. 2) Select ‘Show (or Hide) Aviation Data’. 3) Press the ENT Key. 6-40 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 255: Navigation Map Page
Area (Between 100’ and 1000’ Below Aircraft Altitude) Aircraft Symbol Cursor Placed on Lighted Obstacle Terrain Legend Terrain Symbol and Range Figure 6-47 Terrain Information on the Navigation Map Page 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-41...
Page 256 6) Turn the small FMS Knob to scroll through the ranges and press the ENT Key. Map Zoom Range at Which Data Begins to Display Figure 6-48 Map Setup Window Refer to Table 6-5 for the altitudes associated with obstacle and terrain colors. 6-42 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 257: Taws
TAWS uses terrain and obstacle information supplied by government sources. 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. TAWS ALERTING USING GPS POSITION/GPS MSL ALTITUDE TAWS uses information provided from the GPS receiver to provide a horizontal position and altitude.
Page 258: Using Taws
USING TAWS During G1000 power-up, the terrain/obstacle database versions are displayed along with a disclaimer to the pilot. At the same time, TAWS self-test begins. One of the following aural messages is generated: •...
Page 259 • 360˚ View—Displays surrounding terrain on all sides of aircraft (Figure 6-49). • ARC (120˚) View—Displays terrain ahead of and 60˚ to either side of the aircraft ﬂight path (Figure 6-50). 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-45...
Page 260 Between 100’ and 1000’ Below the Aircraft Altitude) Black Terrain (No Danger - Terrain More than 1000’ Below the Terrain Legend Aircraft Altitude) Figure 6-50 TAWS Page (120˚ View) 6-46 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 261 One of the following aural messages is generated: • “TAWS System Test, OK” • “TAWS System Failure” TAWS TEST is annunciated in yellow on the TAWS Page and in white on the PFD. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-47...
Page 262: Taws Symbols
TAWS alerts typically employ either a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed. Aural alerts are simultaneously issued. 6-48 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 263 Press the CLR Key. This acknowledges the pop-up alert and returns to the currently viewed page. • Press the ENT Key. This acknowledges the pop-up alert and accesses the TAWS Page. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-49...
Page 264 None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) “Don’t Sink” “Too Low, Terrain” Indicates the default conﬁguration Table 6-8 TAWS Alerts Summary 6-50 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 265 During the ﬁnal approach phase of ﬂight, 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. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-51...
Page 266 3) Press the ENT Key. The TAWS system is inhibited or enabled, depending on the previous status. The annunciation is displayed in the terrain annunciator ﬁeld whenever terrain is inhibited. 6-52 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 267 • The distance from the departure airport is 2 nm or less. • The heading change from the heading at the time of departure is less than 110 degrees. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-53...
Page 268 TAWS continually monitors several system-critical items such as database validity, hardware status, and GPS status. If the terrain/obstacle database is not available, the aural message “TAWS System Failure” is generated along with a ‘TAWS FAIL’ annunciation. 6-54 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 269: Trafﬁc Information Service (Tis)
TIS uses the Mode S transponder for the trafﬁc data link. TIS receives trafﬁc information from ground stations and provides a ﬁve-second update rate. The G1000 displays up to eight trafﬁc targets within a 7.5 nm radius, from 3000 feet below to 3500 feet above the requesting aircraft.
Page 270 • Trafﬁc display banner of all possible system statuses • AGE MM:SS • TRFC COAST • TA OFF SCALE • TRFC RMVD • TRFC FAIL • NO TRFC DATA • TRFC UNAVAIL • TRAFFIC 6-56 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 271 Alternatively, press the STANDBY Softkey to place the system in the Standby mode. ‘TIS STANDBY’ displays in the upper left corner of the page. 4) Turn the Joystick clockwise to display a larger area or counter-clockwise to display a smaller area 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-57...
Page 272 • Navigation Map • AUX - Trip Planning Page • WPT - VOR Information Page • Nearest Pages • PFD Inset Map • FPL - Active Flight Plan Page 6-58 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 273: Tis Power-Up Test
• FAILED - Indicates that the transponder has failed. Contact the service center or Garmin dealer for corrective action for these messages. To change the map range, turn the Joystick clockwise to zoom out or counter-clockwise to zoom in. Map ranges are 2 nm, 6 nm, and 12 nm.
Page 274: Operating Modes
HAZARD AVOIDANCE OPERATING MODES Once the aircraft is airborne, the system switches from Standby mode to Operating mode. The G1000 displays ‘TIS OPERATING’ in the upper left-hand corner and begins to display trafﬁc on the Trafﬁc Map Page. The TIS Trafﬁc Advisory (TA) alerts the crew to intruding aircraft.
Page 275 • TA OFF SCALE - Indicates that a trafﬁc advisory is outside the selected display range. The off range banner is removed when the trafﬁc comes within the selected display range. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-61...
Page 276: Skywatch (Sky497)
5) If the self-test fails again, refer to the L-3 Skywatch Pilot’s Guide. Figure 6-62 shows the Trafﬁc Map symbols that display when a user-initiated test is completed successfully: Figure 6-62 User-Initiated Test Results 6-62 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 277: Skywatch Tas Symbology
3) If ‘Operating Mode’ is selected from the FMS menu, press the ENT Key to conﬁrm and place SKYWATCH in operating mode. 4) To switch to Standby Mode from the Trafﬁc Page, press the STANDBY Softkey. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-63...
Page 278 6) Press the STANDBY Softkey to place the system in the Standby mode. ‘TAS STANDBY’ displays in the upper left corner of the page. 7) Turn the Joystick clockwise to display a larger area or counter-clockwise to display a smaller area. 6-64 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 279 SKYWATCH altitude display range is indicated in hundreds of feet relative to the aircraft. In Figure NOTE: 6-63, SKYWATCH indicates that the non-bearing intruder aircraft is at 1100 feet above the aircraft and descending. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 6-65...
Page 280 3) Press the TRAFFIC Softkey. Trafﬁc displays on the Navigation Map (Figures 6-64). Trafﬁc Advisory BLANK PAGE Non-Bearing Trafﬁc Off Non-Threat Trafﬁc Advisories Scale Banner Trafﬁc Figure 6-64 TAS Trafﬁc on Navigation Map 6-66 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev A...
Page 281: Section 7 Automatic Flight Control System
Any IAU failure results in loss of the autopilot and manual electric trim. The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G1000 System avionics architecture. Refer to Figure 1-1 in the System Overview for a block diagram supporting this system description.
Page 282: Afcs Controls On The Mfd
APR Key Selects/deselects Approach Mode NOSE UP/NOSE Control the active mode reference in Pitch Hold, Vertical Speed, and Flight Level DN Keys Change modes Figure 7-1 Dedicated MFD AFCS Controls Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 283: Additional Afcs Controls
3 seconds, MET function is disabled and ‘PTRM’ is displayed as the AFCS Status Annunciation on the PFD. The function remains disabled until both sides of the switch are inactivated. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 284: Flight Director Operation
If the attitude information sent to the ﬂight director becomes invalid or unavailable, the Command Bars are removed from the display. The Command Bars do not override the aircraft symbol. Figure 7-2 Command Bars Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 285: Afcs Status Box
Yaw Damper Roll Modes Pitch Modes Status Status Armed Active Active Mode Armed Reference AFCS Status Box Selected Altitude Command Bars GPS is Selected Navigation Source Figure 7-3 PFD AFCS Display 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 286: Flight Director Modes
After 10 seconds, if no action is taken, the ﬂashing annunciation stops. Figure 7-4 Loss of VOR Signal The ﬂight director is automatically disabled if the attitude information required to compute the default ﬂight director modes becomes invalid or unavailable. Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 287: Pitch Modes
-3000 to +1500 fpm 100 fpm FLC Key Flight Level Change 80 to 190 kt 1 kt Glideslope Arm/Capture/Track APR Key GA Button Go Around Table 7-1 Pitch Modes 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 288 • Pressing the CWS Button, hand-ﬂying the aircraft to establish a new pitch reference, then releasing the CWS Button Pitch Hold Mode Active Altitude Hold Mode Armed Command Bars Maintain Desired Pitch Reference Figure 7-5 Pitch Hold Mode Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 289 Altitude Reference in this case, the CWS Button must be pressed again after the Selected Altitude is captured. Altitude Hold Flight Director Mode Active Altitude Reference Selected Altitude Selected Altitude Bug Command Bars Hold Pitch Attitude to Maintain Altitude Reference Figure 7-6 Altitude Hold Mode 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36...
Page 290 Vertical Vertical Speed Altitude Hold Speed Mode Active Mode Armed Reference Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb Figure 7-7 Vertical Speed Mode 7-10 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 291 • Pressing the CWS Button, hand-ﬂying the aircraft to a new airspeed, then releasing the CWS Button to establish the new Airspeed Reference Flight Level Change Airspeed Altitude Hold Mode Active Reference Mode Armed Airspeed Reference Airspeed Reference Bug Figure 7-8 Flight Level Change Mode 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-11...
Page 292 Mode Active Engaged Mode Active Active ILS Frequency Tuned Glideslope Command Bars Indicator Indicate Descent on Localizer/ Glideslope Path LOC2 is Active Navigation Receiver on HSI Figure 7-10 Glideslope Mode 7-12 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 293 (i.e., with the CWS Button or NOSE UP/NOSE DN keys) result in reversion to Pitch and Roll Hold modes. Go Around Mode Active Autopilot Disconnect Annunciation Flashes Yellow 5 sec Command Bars Indicate Climb Figure 7-11 Go Around Mode 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-13...
Page 294: Roll Modes
(No Glideslope) Navigation, Backcourse Arm/Capture/Track Approach, GPS Arm/Capture/Track Approach, VOR Arm/Capture/Track VAPP APR Key Approach, ILS Arm/Capture/Track (Glideslope Mode automatically armed) Go Around GA Button Table 7-2 Roll Modes 7-14 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 295 Table 7-3 Roll Hold Mode Responses HANGING THE EFERENCE The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then releasing the CWS Button. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-15...
Page 296 340° at a time result in turn reversals. Heading Select Altitude Hold Mode Active Mode Active Command Bars Track Selected Heading Selected Selected Heading Heading Figure 7-13 Heading Select Mode 7-16 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 297 Mode Active Command Bars Indicate Left Turn to Track GPS Course and Selected Course Climb to Intercept Selected Altitude GPS is Active Navigation Receiver on HSI Figure 7-14 Navigation Mode 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-17...
Page 298 The ﬂight director remains in the active roll mode until entering capture phase, at which point Navigation or Approach Mode is annunciated as the active roll mode in green. 7-18 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 299: Autopilot Operation
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. Yaw damper operation is independent of autopilot engagement. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-19...
Page 300: Engaging The Autopilot And Yaw Damper
In most scenarios, releasing the CWS Button reengages the autopilot with a new reference. Refer to the ﬂight director modes section for CWS behavior in each mode. Control Wheel Steering Figure 7-18 CWS Annunciation 7-20 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 301: Disengaging The Autopilot And Yaw Damper
Figure 7-20 Manual Autopilot and Yaw Damper Disengagement The YD Key or AP DISC Switch can be used to disengage the yaw damper. The ‘YD’ annunciation turns yellow and ﬂashes for 5 seconds upon disengagement. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-21...
Page 302: Example Procedures
GPS ﬂight plan. On this leg, the aircraft descends to 3000 feet prior to reaching Clovis VORTAC (CZQ) and the ILS approach to R29R at KFAT is loaded. The ILS approach is ﬂown and a missed approach is executed. KRHV KFAT Figure 7-21 Flight Plan Overview 7-22 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 303 Upon reaching the Selected Altitude, the autopilot completes the capture process and levels the aircraft. From this point, the ﬂight director continues to operate in Altitude Hold Mode. � �� Figure 7-22 Departure 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-23...
Page 304 ‘VOR’ ﬂashes. 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 7-23 Intercepting a VOR 7-24 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 305 3) Once the ﬂight plan leg is intercepted, the autopilot continues to track GPS guidance to the end of the ﬂight plan. � � �� Figure 7-24 Transition to GPS Flight Plan 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-25...
Page 306 Selected Altitude. � �� Figure 7-25 FLC Descent 7-26 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 307 Use the GA Button to execute a missed approach (refer to the following procedure). Clovis V ORTA C ( CZQ ) KFAT SANGO Figure 7-26 ILS Approach to KFAT 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-27...
Page 308 4) To use the autopilot to ﬂy the hold, set the Selected Heading using the HDG Knob and press the HDG Key. Use the HDG Knob to guide the aircraft for the remainder of the hold. 7-28 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 309 AUTOMATIC FLIGHT CONTROL SYSTEM KFAT Figure 7-27 Go Around/Missed Approach 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-29...
Page 310: Afcs Annunciations And Alerts
(if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation. Preﬂight system test failed; aural alert sounds at failure Table 7-4 AFCS Status Alerts 7-30 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 311: 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 and the previous pitch mode resumes control. Airspeed Indicator Figure 7-29 Overspeed Annunciation 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 7-31...
Page 312 AUTOMATIC FLIGHT CONTROL SYSTEM LANK 7-32 Garmin G1000 Pilot’s Guide for Beechcraft A36/G36 190-00595-00 Rev. A...
Page 313: Section 8 Additional Features
If problems occur, ensure that the owner/operator of the aircraft has subscribed to XM Radio service, and that the XM subscription has been activated. If a failure still exists, elementary diagnostic checks of the system are explained in the appendix section for troubleshooting the datalink receiver. 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 314: Xm Information Page
The Weather Products Window shows the list of available weather products and indicates the selected products for the current subscription. The boxes for active weather products are ﬁlled. Before activation, all boxes are cleared. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 315: Xm Radio Page
3) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. Active Channel Channel List Categories Volume Field Field Figure 8-2 XM Radio Page 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 316 3) Press 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. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 317 3) 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 8-3 Categories List 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 318 Softkey is pressed, the volume can also be adjusted using the small FMS Knob.) 3) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to un-mute the audio. Figure 8-5 Volume Control Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 319: Annunciations And Alerts
Annunciation Figure A-1 G1000 Alerting System The G1000 Alerting System conveys alerts to the pilot using a combination of the following items: • Annunciation Window: The Annunciation window displays abbreviated annunciation text. The Annunciation Window is located to the right of the Altitude and Vertical Speed windows on the PFD display (or the MFD if system is in reversionary mode).
Page 320: Alert Level Deﬁnitions
• System Annunciations: Typically, a large red ‘X’ appears in a window when a related LRU fails or detects invalid data. A red ‘X’ is accompanied by an alert message in the Alerts Window. • Audio Alerting System: The G1000 system issues audio alert tones when speciﬁc system conditions are met. See the Alert Levels Deﬁnitions section for more information.
Page 321: A36/G36 Aircraft Annunciations & Alerts
ALT 1 INOP Alternator 1 ofﬂine. Repeating Tone ALT 2 INOP Alternator 2 ofﬂine. Repeating Tone ALT 1-2 INOP Alternators 1 and 2 ofﬂine. Repeating Tone Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 322 PFD FAN FAIL – The cooling fan for the PFD is inoperative. None MFD FAN FAIL – The cooling fan for the MFD is inoperative. None AVIONICS FAN – The cooling fan for remote avionics is inoperative. None Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 323: Afcs Alerts
Preﬂight Test Performing preﬂight system test. Upon completion, the aural alert will be heard. Preﬂight system test has failed. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 324: 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” Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 325: Taws System Status Annunciations
The following section describes various system annunciations. Refer to the POH for additional information regarding pilot responses to these annunciations. NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to 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.
Page 326 Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 327 Display is not receiving valid transponder information. A red ‘X’ through any other display ﬁeld, such as engine instrumentation Other Various Red X Indications ﬁelds, indicates that the ﬁeld is not receiving valid data. Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 328: G1000 System Alert Messages
G1000 SYSTEM ALERT MESSAGES This section describes various G1000 system alert messages. Certain messages are issued due to an LRU or an LRU function failure. Such messages are displayed in the Alerts Window and are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciation section.
Page 329 Recheck settings. The pilot may reconﬁgure the MFD & PFD with preferred settings, if desired. XTALK ERROR – A ﬂight display The MFD and PFD are not communicating with each other. The G1000 system should crosstalk error has occurred. be serviced.
Page 330 The MFD and/or PFD detected a failure in the airport terrain database. Ensure that database error exists. the data card is properly inserted. Replace data card. If problem persists, the G1000 PFD1 DB ERR – PFD1 airport terrain system should be serviced.
Page 331 The audio panel self-test has detected a problem in the unit. Certain audio functions service. Return unit for repair. may still be available, and the audio panel may still be usable. The G1000 system should be serviced when possible. BACKUP PATH – Audio panel 1 using The #1 audio panel is using a backup communication path.
Page 332 Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair.
Page 333 G1000 system should be serviced. transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced. G/S2 FAIL – G/S2 is inoperative.
Page 334 GPS information to augment the lack of airspeed. The G1000 system should be serviced. AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000 GPS source. system should be serviced when possible.
Page 335 Conﬁg service req’d. The G1000 system should be serviced. GDL69 FAIL – GDL 69 has failed. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced GDC 74A Message Advisories...
Page 336 Alerts Window Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored ﬂight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The ﬂight plan cannot ﬁnd the speciﬁed waypoint and ﬂags this message.
Page 337 The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position waypoint for navigation -[xxxx] with alternate navigation sources. TRAFFIC FAIL – Trafﬁc device has The G1000 is no longer receiving data from the trafﬁc system. The trafﬁc device failed. should be serviced. STRMSCP FAIL – Stormscope has Stormscope has failed.
Page 338 APPENDIX A LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 A-20 190-00595-00 Rev. A...
Page 339: Sd Card Use
Updating the Jeppesen aviation database: 1) With the G1000 System OFF, insert the aviation database update SD card into the top card slot of the PFD (Label of SD card facing left).
Page 340 G1000 topography, terrain, and obstacle data is stored on a Supplemental Data Card provided by Garmin. The obstacle database update cycle is every 56 days. The terrain database is updated less often, and on an irregular basis.
Page 341 1) Insert one card in the bottom card slot of the MFD and one in the bottom card slot of the PFD. 2) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the Terrain and Obstacle databases are initialized and displayed on the scrolling window of the splash screen.
Page 342 APPENDIX B LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 343: Glossary
DB, DBASE database BKSP backspace decibels ‘Z’ (Radar Return) bearing DCLTR, DECLTR declutter DEC FUEL decrease fuel Celsius degree Course to Altitude DEIC, DEICE de-icing Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 344 Estimated Time of Arrival The estimated time at which the aircraft Garmin Integrated Avionics Unit should reach the destination waypoint, based Garmin Audio Panel System upon current speed and track. Greenwich Mean Time Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 345 Initial Fix MAG VAR Magnetic Variation Instrument Flight Rules MAHP Missed Approach Hold Point Imperial gallon MAN IN manifold pressure (inches Hg) Instrument Landing System MAN SQ Manual Squelch Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 346 Procedure Turn to Course Intercept speed PIT, PTCH pitch Special Position Identiﬁcation Pilot’s Operating Handbook SPKR speaker POHS Pilot’s Operating Handbook Supplement squelch POSN position SRVC, SVC service parts per million STAL stall Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 347 Coordinated Universal Time UTM/UPS Universal Transverse Mercator / Universal XFER, XFR transfer Polar Stereographic Grid XPDR transponder XTALK cross-talk V, Vspeed velocity (airspeed) cross-track maximum landing gear extended speed Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 348 APPENDIX C LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 349: Frequently Asked Questions
APPENDIX D 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.
Page 350 BE FILED USING THE “/G” may be ﬁled for a ﬂight plan. The G1000 System meets the requirements of TSO-C129 Class A1 or A2 installation. Non-precision GPS approaches are not to be ﬂown with an expired database. See the approved Aircraft Flight Manual Supplement (AFMS) as well as the Aeronautical Information Manual (AIM) for more information.
Page 351 ﬂight plan leg. HEN DOES TURN ANTICIPATION BEGIN The G1000 smooths adjacent leg transitions based on a normal 15° bank angle (with the ability to roll up to 25°) and provides three pilot cues for turn anticipation: •...
Page 352 APPENDIX D LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 353: G1000 Map Datums
Procedures Window by highlighting “Activate Approach?” using the large FMS Knob and pressing the ENT Key. The G1000 provides navigation along the desired course to the waypoint and rejoins the approach in sequence from that point.
Page 354 NAHRWAN UNITD ARAB E United Arab Emirates GUAM 1963 Guam Island NAPARIMA BWI Trinidad and Tobago GUX 1 ASTRO Guadalcanal Island NETHERLAND TRIAG ’21 Netherlands HERAT NORTH Afghanistan NOU TRIAG FRANCE France HJORSEY 1955 Iceland Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 355 Tristan da Cunha VITI LEVU 1916 Viti Levu Island, Fiji Islands WAKE-ENIWETOK 1960 Marshal Islands WGS 72 World Geodetic System 1972 WGS 84 World Geodetic System 1984 YACARE Uruguay ZANDERIJ Surinam Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 356 APPENDIX E LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 357: General Tis Information
PFD Inset Map. Surveillance data includes all transponder-equipped aircraft within the coverage volume. The G1000 System displays up to eight trafﬁc targets within a 7.5-nm radius, from 3,000 feet below, to 3,500 feet above the requesting aircraft.
Page 358 APPENDIX F Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations WARNING: is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map. TIS is unavailable at low altitudes in many areas of the United States. This is often the case in NOTE: mountainous regions.
Page 359: Map Symbols
Symbol Item Symbol Intersection Non-Threat Trafﬁc LOM (Compass Locator at Outer Marker) Proximity Advisory NDB (Non-directional Radio Beacon) Trafﬁc Advisory, Out of Range VOR/DME Trafﬁc Advisory VOR/ILS VORTAC TACAN Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 360 Towered, Non-serviced Airport Non-towered, Serviced Airport Towered, Serviced Airport Restricted (Private) Airport Heliport NAVAIDS Item Symbol Intersection LOM (Compass Locator at Outer Marker) NDB (Non-directional Radio Beacon) VOR/DME VOR/ILS VORTAC TACAN Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 361 Interstate Highway State Highway US Highway National Highway Small City or Town Medium City Large City TRAFFIC Item Symbol Non-Threat Trafﬁc Proximity Advisory Trafﬁc Advisory, Out of Range Trafﬁc Advisory Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 362 Prohibited Area Restricted Area Training Area Unknown Area Class C Terminal Radar Service Area Mode C Area Military Operations Area (MOA) State or Province Border International Border Road Railroad Latitude/Longitude Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 363 Terrain at or within 100 ft below aircraft altitude Yellow (CAUTION) Terrain between 100 ft and 1000 ft of aircraft altitude Black Terrain more than 1000 ft below aircraft altitude Figure G-1 Terrain Colors Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 364 APPENDIX G LANK Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 365: Index
HOLD mode 4-25 Activate 5-95 NAV1 mode 4-25 Caution Missed D-2–D-4 NAV2 mode 4-25 A-19 Select 5-94 Tuning mode 4-25 CDI softkey 4-16 DME audio 4-17 CELL MOV Softkey 6-13 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 366 Map Pages (MAP) 1-21 Glideslope Indicator 2-3, 2-9 Map panning 5-17 Nearest 5-53 Glideslope Mode (GS) 7-3, 7-12, Map scale 5-16 Nearest 7-18, 7-27 Marker beacon 4-24 Global Positioning System (GPS) Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...
Page 367 4-6, 4-10, Trend Vector, Turn Rate 2-11 Procedure examples, AFCS 7-22–7-29 4-16 True airspeed Procedure Loading Pages (PROC) 1-23 Standby frequency ﬁeld True airspeed box PS1 - PS15 softkeys 190-00595-00 Rev. A Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36...
Page 368 Waypoint Pages (WPT) 1-21 Weather Data Link Page 6-6, 6-25 Weather Products weather products WIND Softkey 6-20 Wind vector Wings level 7-6, 7-13, 7- 15, 7-18, 7-25 radio XM Information Page Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 190-00595-00 Rev. A...

Garmin G1000 Pilot's Manual

Section 1 System Overview

System Description

Line Replaceable Units

Secure Digital (SD) Cards

System Power-Up

System Operation

G1000 Controls

Accessing G1000 Functionality

Display Backlighting

Section 2 Flight Instruments

Introduction

Flight Instruments

Supplemental Flight Data

PFD Annunciations and Alerting Functions

Section 3 Engine Indication System (Eis)

Introduction

Engine Display

Lean Display

System Display

Section 4 Audio Panel and Cns

Overview

COM Operation

NAV Operation

GTX 33 Mode S Transponder

Additional Audio Panel Functions

4.6 Preﬂight Procedure for the GMA 1347

Section 5 Gps Navigation

Introduction

Navigation Map (MFD)

PFD Inset Map and Windows

Direct-To-Navigation (MFD)

Direct-To-Navigation (PFD)

Airport Information (MFD)

Intersection Information (MFD)

NDB Information (MFD)

VOR Information (MFD)

User Waypoint Information (MFD)

Nearest Airports (MFD)

Nearest Intersections (MFD)

Nearest NDB (MFD)

Nearest vor (MFD)

Nearest User Waypoint (MFD)

Nearest Frequencies (MFD)

Nearest Airspaces (MFD)

Nearest Airports (PFD)

Flight Planning (MFD)

Flight Planning (PFD)

Procedures (MFD)

Procedures (PFD)

Section 6 Hazard Avoidance

XM WX Satellite Weather

Stormscope (WX-500)

Terrain Proximity

Taws

TrafﬁC Information Service (TIS)

Skywatch (Sky497)

Section 7 Automatic Flight Control System

AFCS Overview

Flight Director Operation

Flight Director Modes

Autopilot Operation

Example Procedures

AFCS Annunciations and Alerts

Section 8 Additional Features

GDL 69A Data Link Receiver - XM Digital Audio Entertainment (Optional)

Annunciations and Alerts

SD Card Use

Glossary

Frequently Asked Questions

G1000 Map Datums

General TIS Information

Map Symbols

Index

Quick Links

Related Manuals for Garmin G1000

Summary of Contents for Garmin G1000