Garmin | G1000H: Bell 505 Jet Ranger X | Garmin G1000H: Bell 505 Jet Ranger X G1000H Cockpit Ref. Guide for Bell 505

Garmin G1000H: Bell 505 Jet Ranger X G1000H Cockpit Ref. Guide for Bell 505
G1000H® Integrated Flight Deck
Cockpit Reference Guide for the Bell 505 Jet Ranger X
FLIGHT INSTRUMENTS
EICAS
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2016 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software 2472.00 or later for the Bell 505 Jet
Ranger X. Some differences in operation may be observed when comparing the information in
this manual to earlier or later software versions.
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Tel: 34-93-357-2608
Fax: 34-93-429-4484
Web Site Address: www.garmin.com
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notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® and G1000H® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are
registered trademarks of L-3 Communications.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively
“AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this
data, express or implied, including, but not limited to, the implied warranties of merchantability
and fitness for a particular purpose. The information is provided “as is” and AOPA does not
warrant or make any representations regarding its accuracy, reliability, or otherwise. Under
no circumstances including negligence, shall AOPA be liable for any incidental, special or
consequential damages that result from the use or inability to use the software or related
documentation, even if AOPA or an AOPA authorized representative has been advised of the
possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed
by law, to release and hold harmless AOPA from any causes of action, claims or losses related
to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the
limitation or exclusion of implied warranties or liability for incidental or consequential damages
so the above limitations or exclusions may not apply to you.
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”)
expressly disclaim all warranties with respect to the AC-U-KWIK information included
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do not allow the limitation or exclusion of implied warranties or liability for incidental or
consequential damages so the above limitations or exclusions may not apply to licensee.
Printed in the U.S.A.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Warnings, Cautions & Notes
WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation from terrain and obstacles. Garmin obtains
terrain and obstacle data from third party sources and cannot independently
verify the accuracy of the information.
WARNING: Always refer to current aeronautical charts and NOTAMs for
verification of displayed aeronautical information. Displayed aeronautical
data may not incorporate the latest NOTAM information.
WARNING: Do not use geometric altitude for compliance with air traffic
control altitude requirements. The primary barometric altimeter must be used
for compliance with all air traffic control altitude regulations, requirements,
instructions, and clearances.
WARNING: Do not use basemap information (land and water data) as the
sole means of navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered only an aid to
enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information to
accurately depict all of the traffic within range of the aircraft. Due to lack
of equipment, poor signal reception, and/or inaccurate information from
aircraft or ground stations, traffic may be present that is not represented on
the display.
WARNING: Do not use data link weather information for maneuvering in,
near, or around areas of hazardous weather. Information contained within
data link weather products may not accurately depict current weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather
product. Due to time delays inherent in gathering and processing weather
data for data link transmission, the weather information shown by the data
link weather product may be significantly older than the indicated weather
product age.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Warnings, Cautions & Notes
WARNING: The displayed minimum safe altitude (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts for
appropriate minimum clearance altitudes.
WARNING: Always obtain qualified instruction prior to operational use of
this equipment.
WARNING: Do not use a QFE altimeter setting with this system. System
functions will not operate properly with a QFE altimeter setting. Use only
a QNH altimeter setting for height above mean sea level, or the standard
pressure setting, as applicable.
WARNING: Do not use GPS to navigate to any active waypoint identified as
a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints
are derived from an unknown map reference datum that may be incompatible
with the map reference datum used by GPS (known as WGS84) and may be
positioned in error as displayed.
WARNING: Do not rely on information from a lightning detection system
display as the sole basis for hazardous weather avoidance. Range limitations
and interference may cause the system to display inaccurate or incomplete
information. Refer to documentation from the lightning detection system
manufacturer for detailed information about the system.
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. Garmin SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability
upon which to solely base decisions and/or plan maneuvers to avoid terrain,
obstacles, or traffic.
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the
Garmin SVT display or may appear as a partial symbol.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Warnings, Cautions & Notes
WARNING: Do not use TAWS information for primary terrain or obstacle
avoidance. TAWS is intended only to enhance situational awareness.
WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision
avoidance resolution advisories and does not under any circumstances or
conditions relieve the pilot’s responsibility to see and avoid other aircraft.
CAUTION: Do not clean display surfaces with abrasive cloths or cleaners
containing ammonia. They will harm the anti-reflective coating.
CAUTION: Repairs should only be made by an authorized Garmin service
center. Unauthorized repairs or modifications could void both the warranty
and affect the airworthiness of the aircraft.
NOTE: Do not rely solely upon data link services to provide Temporary Flight
Restriction (TFR) information. Always confirm TFR information through official
sources such as Flight Service Stations or Air Traffic Control.
NOTE: All visual depictions contained within this document, including screen
images of the system panel and displays, are subject to change and may not
reflect the most current system and aviation databases. Depictions of equipment may differ slightly from the actual equipment.
NOTE: The United States government operates the Global Positioning System
and is solely responsible for its accuracy and maintenance. The GPS system
is subject to changes which could affect the accuracy and performance of all
GPS equipment. Portions of the system utilize GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information
presented by the system can be misused or misinterpreted and, therefore,
become unsafe.
NOTE: This device complies with part 15 of the FCC Rules. Operation is
subject to the following two conditions: (1) this device may not cause harmful
interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Warnings, Cautions & Notes
NOTE: Interference from GPS repeaters operating inside nearby hangars can
cause an intermittent loss of attitude and heading displays while the aircraft
is on the ground. Moving the aircraft more than 100 yards away from the
source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
NOTE: This product, its packaging, and its components contain chemicals
known to the State of California to cause cancer, birth defects, or reproductive
harm. This notice is being provided in accordance with California’s Proposition
65. If you have any questions or would like additional information, please
refer to our web site at www.garmin.com/prop65.
NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields can cause sensor differences that may result
in nuisance miscompare annunciations during start up, shut down, or while
taxiing. If one or more of the sensed values are unavailable, the annunciation
indicates no comparison is possible.
NOTE: The system responds to a terminal procedure based on data coded
within that procedure in the Navigation Database. Differences in system
operation may be observed among similar types of procedures due to
differences in the Navigation Database coding specific to each procedure.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Warnings, Cautions & Notes
NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin databasedependent avionics of the following:
• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory
guidance and information related to the use of databases in the National Airspace
System.
• Garmin equipment will only recognize and use databases that are obtained from
Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured
compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter
of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for
each database and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA
Status.’
• Use of a current Garmin or Jeppesen database in your Garmin equipment is required
for compliance with established FAA regulatory guidance, but does not constitute
authorization to fly any and all terminal procedures that may be presented by the
system. It is the pilot’s responsibility to operate in accordance with established
AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft,
and installed equipment.
NOTE: The pilot/operator must review and be familiar with Garmin’s database
exclusion list as discussed in SAIB CE-14-04 to determine what data may be
incomplete. The database exclusion list can be viewed at www.flygarmin.
com by selecting ‘Database Exclusions List.’
NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The
database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation
Database Alerts.’
NOTE: If the pilot/operator wants or needs to adjust the database, contact
Garmin Product Support to coordinate the revised DQRs.
NOTE: Garmin requests the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or
any other displayed item used for navigation or communication in the air or
on the ground. Go to FlyGarmin.com and select ‘Aviation Data Error Report’.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Warnings, Cautions & Notes
NOTE: Lamp(s) inside this product contain mercury (HG) and must be recycled
or disposed of according to local, state, or federal laws. For more information,
refer to our website at www.garmin.com/aboutGarmin/environment/disposal.
jsp
NOTE: When operating the system with the magnetic sensor uncoupled
from the AHRS, the displayed heading and heading information used by
some system components (e.g. traffic system, AFCS, and weather radar) will
be different from the heading calculated by the AHRS. The difference is an
amount equal to the difference between the current Magnetic Field Variation
Database (MV DB) value, and the MV DB value when the magnetic sensor
was uncoupled. Due to the convergence of isogonic lines, this condition is
most noticeable at or near the north and south magnetic poles.
NOTE: Operate G1000H system power through at least one cycle in a period
of four days of continuous operation to avoid an autonomous system reboot.
NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a
resource with which to find operating instructions on the major features of
the G1000H system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000H Pilot’s Guide for this aircraft.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Record of Revisions
Part Number
190-02065-00
Change Summary
Production Release
Revision Date of Revision Affected Pages
A
October, 2016
All
190-02065-00 Rev. A
Description
Initial release at GDU 15.11
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
RR-1
Record of Revisions
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RR-2
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Table of Contents
Flight Instruments........................................................................................................................ 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Change Navigation Sources.................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS..................................................... 1
Enable/Disable OBS Mode While Navigating with GPS (If Available)............................ 2
Enable heading Preset Mode (If Available)......................................................................... 2
Disable heading Preset Mode (If Available)........................................................................ 2
Generic Timer.............................................................................................................................. 3
Set Barometric/Radar Altimeter (RA Optional) Minimum Descent Altitude................ 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 4
Engine Indication System......................................................................................................... 5
Engine Power and Speed Indications.................................................................................... 7
Power Assurance Check............................................................................................................ 8
Engine Tests................................................................................................................................ 9
Crew Alerting System (CAS).................................................................................................. 10
Nav/Com/Transponder/Audio Panel.................................................................................. 13
ADF Tuning (Optional)............................................................................................................. 13
Enter a Transponder Code..................................................................................................... 13
Selecting a COM Radio........................................................................................................... 13
Selecting a NAV Radio............................................................................................................ 14
NAV/COM Tuning...................................................................................................................... 16
Digital Clearance Recorder and Player (Optional)........................................................... 16
Intercom Volume and Squelch.............................................................................................. 17
Intercom Modes....................................................................................................................... 18
Passenger Address Mode (PA Mode)................................................................................... 22
Split-PA Mode........................................................................................................................... 23
3D Audio.................................................................................................................................... 23
Enabling 3D Audio................................................................................................................... 23
3D Audio Troubleshooting..................................................................................................... 23
Voice Recognition.................................................................................................................... 25
Automatic Flight Control System...................................................................................... 33
GPS Navigation............................................................................................................................ 35
Direct-to Navigation............................................................................................................... 35
Activate a Stored Flight Plan................................................................................................ 36
Activate a Flight Plan Leg...................................................................................................... 36
Stop Navigating a Flight Plan............................................................................................... 37
Vertical Navigation (VNAV)................................................................................................... 37
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
i
Table of Contents
Flight Planning............................................................................................................................. 41
Weight and Balance Planning............................................................................................... 41
Trip Planning............................................................................................................................. 42
Create a User Waypoint Defined by Latitude & Longitude............................................ 44
Create a User Waypoint Defined by Radials from Other Waypoints............................ 45
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 47
Delete a User Waypoint.......................................................................................................... 48
Create a Flight Plan................................................................................................................. 49
Import a Flight Plan from an SD Card................................................................................. 50
Insert a Waypoint in the Active Flight Plan....................................................................... 50
Enter an Airway in a Flight Plan........................................................................................... 51
User-Defined Holding Patterns............................................................................................. 52
Invert An Active Flight Plan................................................................................................... 54
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 54
Store a Flight Plan................................................................................................................... 55
Edit a Stored Flight Plan........................................................................................................ 55
Delete a Waypoint from the Flight Plan............................................................................. 55
Invert and Activate a Stored Flight Plan............................................................................ 56
Copy a Flight Plan.................................................................................................................... 56
Delete a Flight Plan................................................................................................................. 57
Graphical Flight Plan Creation.............................................................................................. 57
Export a Flight Plan to an SD Card...................................................................................... 58
Procedures...................................................................................................................................... 59
Load and Activate a Departure Procedure........................................................................ 59
Activate A Departure Leg...................................................................................................... 59
Load An Arrival Procedure..................................................................................................... 60
Activate An Arrival Leg.......................................................................................................... 60
Load and/or Activate an Approach Procedure.................................................................. 61
Activate An Approach in the Active Flight Plan................................................................ 62
Activate a Vector to Final Approach Fix............................................................................. 62
Activate A Missed Approach in the Active Flight Plan.................................................... 62
Temperature Compensated Altitude................................................................................... 63
Hazard Avoidance....................................................................................................................... 65
Customizing the Hazard Displays on the Navigation Map............................................. 65
Traffic Systems......................................................................................................................... 65
Helicopter Terrain Awareness & Warning System (HTAWS) Display (Optional)......... 68
Profile View Terrain................................................................................................................. 71
Additional Features................................................................................................................... 73
Synthetic Vision (Optional).................................................................................................... 73
Terminal Procedure Charts.................................................................................................... 74
ii
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Table of Contents
Airport Directory..................................................................................................................... 76
Scheduler................................................................................................................................... 77
Pilot Profiles............................................................................................................................. 78
Abnormal Operation................................................................................................................. 83
Reversionary Mode................................................................................................................. 83
Abnormal COM Operation..................................................................................................... 83
Hazard Displays with Loss of GPS Position........................................................................ 83
Unusual Attitudes.................................................................................................................... 84
Dead Reckoning....................................................................................................................... 84
Annunciations & Alerts............................................................................................................ 87
G1000H System Annunciations............................................................................................. 87
Warning Messages................................................................................................................... 89
Caution Messages.................................................................................................................... 89
Advisory Messages.................................................................................................................. 90
Status Annunciation................................................................................................................ 92
HTAWS Alerts............................................................................................................................ 92
HTAWS System Status Annunciations................................................................................. 93
TIS Alerts And Annunciations................................................................................................ 95
Voice Alerts............................................................................................................................... 96
G1000H System Message Advisories................................................................................... 97
Flight Plan Import/Export Messages................................................................................. 110
Pilot Profile Import/Export Messages............................................................................... 111
Appendix........................................................................................................................................ 113
PFD Softkey Map................................................................................................................... 113
MFD Softkey Map.................................................................................................................. 119
Loading Updated Databases............................................................................................... 121
Index............................................................................................................................................Index-1
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
iii
Table of Contents
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iv
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
EICAS
Turn the BARO Knob to select the desired setting.
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
AFCS
1)
Nav/Com/
XPDR/Audio
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Flight
Planning
Press the PFD Softkey to display the second-level softkeys.
GPS Nav
1)
Procedures
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
4)
CHANGE NAVIGATION SOURCES
2)
Press the CDI Softkey a second time to return to GPS.
Abnormal
Operation
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the cyan tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
Additional
Features
1)
Annun/
Alerts
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
Press the OBS Softkey to select OBS Mode.
Appendix
1)
1
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS (IF AVAILABLE)
Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
GPS Nav
Flight
Planning
1)
Press the SENSOR Softkey on the PFD.
2)
Press the SET HDG Softkey. The system is in Heading Preset Mode (HPM)
as indicated by displaying ‘SET’ to the left of the heading value.
3)
Press the HDG + and/or HDG - Softkeys to slew the heading value to the
desired setting.
Set the Selected Heading Bug to the desired heading value, then press the
HDG SYNC Softkey.
DISABLE HEADING PRESET MODE (IF AVAILABLE)
Hazard
Avoidance
Procedures
2)
Or:
Press the HPM OFF Softkey on the PFD to manually disable Heading Preset
Mode.
Or:
Additional
Features
Abnormal
Operation
Press the OBS Softkey to select OBS Mode.
Heading Preset Mode automatically disables after eight minutes.
If there is more than 10° difference between the Heading Preset value and the
magnetic heading when Heading Preset Mode is disabled, the heading value is
displayed in amber and ‘ALN’ will be displayed to the left of the heading. When the
magnetic heading has properly aligned, the heading value will be displayed in white
and ‘ALN’ will no longer be displayed.
Index
Appendix
Annun/
Alerts
1)
ENABLE HEADING PRESET MODE (IF AVAILABLE)
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Instruments
2
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Instruments
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
AFCS
2)
Nav/Com/
XPDR/Audio
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
EICAS
1)
Flight
Instruments
GENERIC TIMER
GPS Nav
SET BAROMETRIC/RADAR ALTIMETER (RA OPTIONAL) MINIMUM DESCENT
ALTITUDE
Flight
Planning
1) Press the TMR/REF Softkey.
Turn the large FMS Knob to highlight the Minimums field.
3)
Turn the small FMS Knob to select BARO, TEMP COMP, or RAD ALT. OFF
is selected by default. Press the ENT Key or turn the large FMS Knob to
highlight the next field.
4)
Use the small FMS Knob to enter the desired altitude (from zero to 16,000
feet for BARO, or from zero to 2,500 for RAD ALT).
5)
If TEMP COMP was selected, press the ENT Key or turn the large FMS
Knob to highlight the next field and then enter the destination airport
temperature (-59˚C to 59˚C). The temperature compensated altitude
minimum is displayed below the previously enter minimum altitude value.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Procedures
2)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DISPLAYING WIND DATA
2)
Press the WIND Softkey to display wind data to the left of the HSI.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
Appendix
Press the PFD Softkey.
Annun/
Alerts
1)
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
3
CHANGING HSI FORMAT
EICAS
Flight
Instruments
Flight Instruments
1)
Press the PFD Softkey.
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Nav/Com/
XPDR/Audio
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Press the ARC HSI Softkey to display the arc style HSI.
4
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Engine Indication & Crew Alerting System
Flight
Instruments
ENGINE INDICATION SYSTEM
EICAS
3
4
AFCS
2
Nav/Com/
XPDR/Audio
1
3
4
Flight
Planning
2
GPS Nav
1
Procedures
5
5
6
8
Hazard
Avoidance
6
8
7
Additional
Features
7
9
Abnormal
Operation
MFD EIS Display (Normal)
EIS Display (Reversionary)
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
5
1
Engine Oil Pressure
(P)
Displays pressure of oil supplied to the engine
in pounds per square inch (psi).
2
5
Oil Temperature
Indicator (T)
Transmission Oil
Pressure (P)
Transmission Oil
Temperature (T)
Ammeter (A)
Displays engine oil temperature in degrees
Celsius
Displays pressure of oil supplied to the
transmission in pounds per square inch (psi).
Displays the transmission oil temperature in
degrees Celsius
Displays the DC load in 5 amperes increments
6
Voltmeter (V)
Displays the electrical bus voltage
7
Total Fuel Quantity
8
Fuel Flow Indicator
(FF PPH)
Total Fuel Quantity
Displays the usable fuel quantity in 5 pound
increments.
Displays fuel flow in 10 pound increments.
EICAS
Flight
Instruments
Engine Indication & Crew Alerting System
Nav/Com/
XPDR/Audio
3
Procedures
Flight
Planning
GPS Nav
AFCS
4
Displays total usable fuel quantity as a bar
graph in 5 pound increments
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
9
6
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Engine Indication & Crew Alerting System
Maximum Continuous
Power Operating Limit
Box Indicates Parameter
Controlling PSI Indicator
Nav/Com/
XPDR/Audio
Power Available
Indicating Gauge
Maximum Takeoff Power Limit
Torque Readout
MGT Readout
AFCS
NG Readout
NR Indicator
NR Readout
GPS Nav
Command NP Speed
Reference Indicator
EICAS
Power Available Pointer
Flight
Instruments
ENGINE POWER AND SPEED INDICATIONS
NP Indicator
Flight
Planning
Dual Tachometer Gauge
Power Situation Indicator Gauge and Dual Tachometer Gauge
Procedures
Power Situation Indicator
Annun/
Alerts
Appendix
Index
7
Abnormal
Operation
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Additional
Features
190-02065-00 Rev. A
Hazard
Avoidance
The PSI provides the pilot with the amount of power available based on engine
torque (Q; shown as a percentage), measured gas temperature (MGT, degrees Celsius,
°C), and gas producer rotation speeds (NG; shown as a percentage) with respect to
operating limitations. A box is shown around the label for the display currently closest to its maximum continuous power (MCP) limits. This value also controls a Power
Available Pointer along a numeric scale from 0 (no power) to Takeoff Power (TOP,
shown with a red tick mark).
Power available information is displayed along the PSI scale and is adjusted dynamically in response to all parameters, to show the rate and range of pointer movement available, before any parameter reaches the Maximum Continuous Takeoff Power
limit. Green arcs indicate continuous operation ranges; amber arcs indicate transient
operating limits. A gray arc becomes red if the Power Available pointer enters this
range; it indicates an exceedance is pending or may be occurring.
In normal operations, the Power Available pointer will be the same color as the arc
it is presently within. A gray pointer is displayed when an engine failure is detected
while in-flight.
The Commanded Np Speed reference indicator is displayed in magenta circle with
a thin tick mark that extends to the arc scale in normal operations. When Np Speed
information is invalid or in autorotation mode, the Np Speed reference indicator is
white.
Takeoff Timer
After the engine has been started, if Q, MGT, and NG are within the takeoff
limitation ranges, the G1000H displays a 5-minute countdown timer inside the PSI
gauge. The timer flashes amber when 30 seconds remain, until an exceedance occurs.
The timer displays red, when an exceedance occurs and the timer reaches zero. The
timer is automatically removed when either Q, MGT and NG fall below takeoff limits.
Dual Tachometer
The dual tachometer displays rotor speed (NR) and power turbine speed (NP) as
percentages. A digital display and pointer for NR and a pointer for NP are provided.
The long pointer represents NR along the gauge scale; NP is shown with the short
pointer. Limitations are shown as colored arcs. The NR and NP pointers will be the
same color as the arc(s) they are presently within.
During autorotation with an engine failure, the NP pointer will be displayed in gray
and the dual tachometer gauge scale will display power-off limitations.
POWER ASSURANCE CHECK
NOTE: Follow the procedures in the 505 Flight Manual (FM) for configuring
the AUX-System Setup page and for information on the required conditions
to conduct a power check prior to activating the feature on the G1000H.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Engine Indication & Crew Alerting System
Performing a power assurance check:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the PWR CHK Softkey.
When the Power Assurance Check is activated, a ‘PWR CHK’ box is displayed
containing a progress meter. When the helicopter configuration for the Power
Assurance Check is successfully completed, “COMPLETE” will be displayed. When
the helicopter configuration for the Power Assurance Check is invalid, an error
message is displayed. Otherwise, the Power Assurance Check will complete after 15
seconds. Dashes are displayed if data used to perform the Power Assurance Check is
not available.
8
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Engine Indication & Crew Alerting System
Nav/Com/
XPDR/Audio
Audio Alert Test (AUD)
AFCS
Performing the audio alert test:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the TEST Softkey.
3) Press the AUD TST Softkey.
GPS Nav
Chip Detector Test
Flight
Planning
Performing the chip detector test:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the TEST Softkey.
3) Press the CHIP TST Softkey.
Procedures
Fire Detection System Test
Hazard
Avoidance
Additional
Features
Performing the fire detection system test:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the TEST Softkey.
3) Press the FIRE TST Softkey.
Abnormal
Operation
Auxiliary Control Unit Test (ACU)
Annun/
Alerts
Performing the auxiliary control unit test:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the TEST Softkey.
3) Press the ACU TST Softkey.
Appendix
Flame Out Protection System Test (FOPS)
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
Performing the flame out protection system test:
1) Press the ENGINE Softkey to display the Engine Page.
2) Press the TEST Softkey.
3) Press the FOPS TST Softkey.
EICAS
NOTE: Refer to the 505 Flight Manual (FM) for engine operating limitations
and corrective actions.
Flight
Instruments
ENGINE TESTS
9
CREW ALERTING SYSTEM (CAS)
When Crew Alerting System (CAS) messages are generated, a CAS window
containing messages appears to the right of the vertical speed indicator on the PFD. Up
to 12 messages can be displayed; when more than 12 messages accumulate, the CAS
Softkey becomes available. Pressing the CAS Softkey displays softkeys for scrolling up
and down through the messages in the PFD CAS Window. In Reversionary Mode, the
CAS Softkey takes the place of the INSET Softkey.
PFD CAS
Window
CAS Scrolling
Softkey
(Enabled when
more than 12
messages are
displayed)
Softkey Annunciation (Press to
Acknowledge CAS Message)
CAS Message Display (PFD)
CAS alerts are additionally displayed on the upper left of the EIS - Engine page.
Up to 19 messages can be displayed; when more than 19 messages accumulate, the
CAS and CAS Softkeys will become available to permit scrolling up and down
through the messages on this page.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Engine Indication & Crew Alerting System
10
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Engine Indication & Crew Alerting System
Flight
Instruments
EICAS
MFD Alerts
window
containing
CAS messages
Nav/Com/
XPDR/Audio
AFCS
CAS Scrolling
Softkeys (Enabled
when more than
19 messages are
displayed)
GPS Nav
Engine Page CAS Display (MFD)
Flight
Planning
CAS Message Prioritization
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
When a warning or caution CAS message is generated, the MSG Softkey label in
the lower right corner of the PFD changes to display the WARNING or CAUTION
annunciation. The softkey annunciation flashes and the corresponding aural alert
sounds until acknowledged by depressing the softkey..
Hazard
Avoidance
CAS messages are grouped by criticality (warning, caution, advisory, and status)
and sorted by order of appearance (most recent messages on top). The color of the
message is based on its urgency and on required action.
• Warning (red) – Immediate crew awareness and immediate crew action
required.
• Caution (amber) – Immediate crew awareness and subsequent
corrective action required.
• Advisory (white) – Crew awareness required and subsequent action
may be required.
• Status (green) – Crew awareness required.
Procedures
NOTE: Information on CAS messages in this pilot’s guide is always superseded
by the 505 Flight Manual (FM). Refer to the 505 FM for recommended pilot
actions.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
11
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Engine Indication & Crew Alerting System
Blank Page
12
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ADF TUNING (OPTIONAL)
EICAS
Tune the ADF using the remote ADF control head.
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
SELECTING A COM RADIO
Procedures
Hazard
Avoidance
Additional
Features
The COM transceiver is selected for transmitting by pressing the MIC Keys on the
Audio Panel. During reception of audio from the COM radio selected for transmission,
audio from the other COM radio (if installed) is muted.
An active COM frequency displayed in green indicates that the COM transceiver is
selected on the Audio Panel (MIC1 or MIC2 Key).
Frequencies in the standby field are displayed in either white or gray. The standby
frequency in the tuning box is white. The other standby frequency for the other COM
radio (if installed) is gray.
Flight
Planning
2)
GPS Nav
Press the XPDR Softkey to display the transponder mode selection softkeys.
AFCS
1)
Nav/Com/
XPDR/Audio
ENTER A TRANSPONDER CODE
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
13
Nav/Com/XPDR/Audio Panel
Standby
Field
Tuning Box
EICAS
Flight
Instruments
Active
Field
Nav/Com/
XPDR/Audio
COM Frequency Box Display with a single integrated COM
transceiver, and with or without a stand-alone COM transceiver
GPS Nav
AFCS
Active
Fields
Standby
Fields
Tuning Box
Procedures
Flight
Planning
COM Frequency Box Display with two integrated COM transceivers
Additional
Features
Hazard
Avoidance
COM1 Radio is Selected
on the Audio Panel
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Selecting a COM Radio for Transmit
SELECTING A NAV RADIO
A NAV radio is selected for navigation by pressing the CDI Softkey located on the
PFD. The active NAV frequency selected for navigation is displayed in green. Pressing
the CDI Softkey once selects NAV1 as the navigation radio. Pressing the CDI Softkey
a second time selects NAV2 (if equipped) as the navigation radio. Pressing the CDI
Softkey a third time activates GPS mode. Pressing the CDI Softkey again cycles back
to NAV1.
14
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Active
Field
EICAS
Standby
Field
Flight
Instruments
While cycling through the CDI Softkey selections, the NAV Tuning Box and the
Frequency Transfer Arrow are placed in the active NAV Frequency Field and the active
NAV frequency color changes to green.
The three navigation modes that can be cycled through are:
• VOR1 (or LOC1) – If NAV1 is selected, a green single line arrow (shown) labeled
either VOR1 or LOC1 is displayed on the HSI and the active NAV1 frequency
is displayed in green.
• VOR2 (or LOC2) – If NAV2 (if equipped) is selected, a green double line arrow
(not shown) labeled either VOR2 or LOC2 is displayed on the HSI and the active
NAV2 frequency is displayed in green.
• GPS – If GPS Mode is selected, a magenta single line arrow (not shown) appears
on the HSI and neither NAV radio is selected. Both active NAV frequencies are
then displayed in white.
Procedures
Tuning Box
Hazard
Avoidance
The NAV Radio is Selected
by Pressing the CDI
Softkey
Additional
Features
Selecting a NAV Radio for Navigation
Abnormal
Operation
See the Flight Instruments Section for Bearing Information windows and using
VOR as the source for the bearing pointer.
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
15
NAV radios are selected for listening by pressing the corresponding keys on the
Audio Panel. Pressing the NAV1,or NAV2 Key selects and deselects the navigation
radio source. Selected audio can be heard over the headset and the speaker (if selected).
All radios can be selected individually or simultaneously.
Selecting a NAV Radio Receiver
NAV/COM TUNING
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
1)
Press the small tuning knob to select the desired radio for tuning. A cyan
box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
DIGITAL CLEARANCE RECORDER AND PLAYER (OPTIONAL)
The Audio Panel contains a digital clearance recorder that records up to 2.5 minutes
of the selected COM radio signal. Recorded COM audio is stored in separate memory
blocks. Once 2.5 minutes of recording time have been reached, the recorder begins
recording over the stored memory blocks, starting from the oldest block.
The Play function is accessed through Voice Recognition commands. Refer to the
Voice Recognition section for more information.
Pressing the MKR/MUTE Key during play of a memory block stops play. If a COM
input signal is detected during play of a recorded memory block, play is halted.
Pressing the optional Play button while audio is playing begins playing the
previously recorded memory block. Each subsequent press of the Play button selects
the previously recorded memory block.
Powering off the unit automatically clears all recorded blocks.
16
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Nav/Com/
XPDR/Audio
AFCS
Manual Squelch Annunciator; Off for
Automatic Squelch, On for Manual
Squelch
EICAS
The VOL/CRSR Knob controls selection and volume or manual intercom squelch
adjustment for audio sources that may not be adjustable anywhere else in the system.
The small knob controls the volume or squelch. Turning the large knob activates and/
or moves the cursor (flashing green annunciator or flashing blue annunciator in BlueSelect Mode) to select the audio source to adjust. The cursor will time-out after a few
seconds and the position of the cursor will always default back to the PILOT Key.
Pressing the small knob cancels the cursor.
Flight
Instruments
INTERCOM VOLUME AND SQUELCH
Relative Volume/
Squelch Scale
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Cursor
Volume or Manual Squelch
Volume/Squelch Control
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
17
Flight
Instruments
Nav/Com/XPDR/Audio Panel
INTERCOM MODES
NOTE: When in Split-COM mode, the copilot will only hear alerts and the
All Intercom Mode
In ‘All Intercom’ mode the Pilot, Copilot, and Passengers hear each other and hear
the aircraft audio.
Aircraft Audio
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
higher numbered of the two selected COMs (COM2 or COM3).
Procedures
Flight
Planning
PILOT
COPLT
Hazard
Avoidance
PASS
Mode Operation
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
ICS Keys
18
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
In ‘Pilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft audio.
The Copilot and Passengers also hear each other.
EICAS
Aircraft Audio
Flight
Instruments
Pilot Isolate Mode
Nav/Com/
XPDR/Audio
PILOT
AFCS
COPLT
GPS Nav
PASS
Flight
Planning
ICS Keys
Mode Operation
Procedures
Passenger/Crew Isolate Mode
Aircraft Audio
Hazard
Avoidance
In ‘Passenger/Crew Isolate’ mode the Pilot and Copilot hear the aircraft audio and
each other. The Passengers hear each other.
Additional
Features
PASS
Mode Operation
Annun/
Alerts
ICS Keys
COPLT
Abnormal
Operation
PILOT
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
19
Copilot Isolate Mode
In ‘Copilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft audio.
The Pilot and Passengers also hear each other. The Copilot has the option to use SplitCOM mode.
Aircraft Audio
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
COPLT
GPS Nav
PILOT
ICS Keys
Mode Operation
All Isolate Mode
In ‘All Isolate’ mode the Pilot and Copilot hear the aircraft audio. The Copilot has
the option to use Split-COM mode. The Passengers hear each other.
Aircraft Audio
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
PASS
Annun/
Alerts
PILOT
PASS
Mode Operation
Index
Appendix
ICS Keys
COPLT
20
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Aircraft Audio
COPLT
Nav/Com/
XPDR/Audio
PILOT
EICAS
In ‘Pilot & Copilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft
audio. The Passengers hear each other. The Copilot has the option to use Split-COM
mode.
Flight
Instruments
Pilot & Copilot Isolate Mode
PASS
AFCS
Mode Operation
GPS Nav
ICS Keys
Pilot & Passenger Isolate Mode
Aircraft Audio
Flight
Planning
In ‘Pilot & Passenger Isolate’ mode the Pilot and Copilot hear the aircraft audio.
The Passengers hear each other.
Procedures
PASS
Additional
Features
ICS Keys
COPLT
Hazard
Avoidance
PILOT
Mode Operation
Copilot & Passenger Isolate Mode
COPLT
Appendix
PILOT
Annun/
Alerts
Aircraft Audio
Abnormal
Operation
In ‘Copilot & Passenger Isolate’ mode the Pilot and Copilot can hear the aircraft
audio. The Copilot has the option to use Split-COM mode. The Passengers hear each
other.
PASS
Index
ICS Keys
190-02065-00 Rev. A
Mode Operation
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
21
Blue-Select Mode (Telephone/Entertainment Distribution)
The music (MUSIC) and telephone/entertainment (
) audio are distributed
using the Blue-Select Mode. The following example indicates that the pilot, copilot,
and passengers will all hear the telephone/entertainment audio.
Blue-Select Mode (Telephone/Entertainment Distribution)
The Blue-Select Mode is entered by pressing the small knob when the volume
control cursor (flashing green annunciator) is not active. If the volume control cursor
is active, press the small knob twice. The first press will cancel the volume control
cursor, the second will activate Blue-Select Mode.
The annunciator over the
Button will be flashing blue. Any combination of
the annunciators over the PILOT, COPLT, and PASS buttons may be blue. Select the
desired button to turn the blue annunciator on or off to distribute the telephone audio
to selected crew/passenger positions. Turn the large knob to select MUSIC, and select
the crew/passenger positions to receive the music audio.
Selecting any button other than PILOT, COPLT, PASS , MUSIC or
will
cancel Blue-Select Mode. Pressing the small knob will also cancel Blue-Select Mode.
After approximately ten seconds with no input, the Blue-Select Mode will automatically
cancel.
PASSENGER ADDRESS MODE (PA MODE)
Press and hold the SPKR Key for 2 seconds to initiate Passenger Address Mode. PA
Mode is annunciated by a rapid blinking of the SPKR annunciator. When in PA Mode
the crew can use the PTT “Push-to-Talk” button to deliver announcements over the
speaker, to the passenger headsets, or both depending on configuration.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
22
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Press and hold the PILOT Key to toggle 3D audio processing on and off for all
headset positions. When 3D Audio is enabled, the aural message “3D audio left” is
heard in the left ear followed by “3D audio right” in the right ear.
GPS Nav
ENABLING 3D AUDIO
AFCS
3D Audio is useful when multiple audio sources are present. By using different
responses in each ear, 3D audio processing creates the illusion that each audio source
is coming from a unique location or seat position.
Because this feature uses different signals for left and right channels, it requires
wiring for stereo intercom and stereo headsets. If 3D audio is activated when mono
headsets are in use, the listener will still hear all audio sources; however, there is no
benefit from location separation. The baseline Bell 505 Jet Ranger X is wired for mono
headsets.
With a single COM selected and 3D Audio enabled, the listener hears the audio
source at the 12 o’clock position. If all three COMs are selected, the listener hears
the audio sources at the 11, 12 and 1 o’clock positions with the COM numbers
increasing clockwise. If two COMs are selected, the listener hears COM1 at the 11
o’clock position and COM2 at the 1 o’clock position. All other intercom positions
are processed to sound like their relative seat location. By default, the GMA 350H
assumes the pilot sits in the right seat. A Garmin authorized service center can make
changes to the default configuration.
Nav/Com/
XPDR/Audio
3D AUDIO
EICAS
During Split-PA Mode the pilot can continue to use the radio(s) while the copilot
delivers PA announcements. To initiate Split-PA Mode, first enter Split-COM Mode by
pressing more that one MIC Keys simultaneously, then press and hold the SPKR Key
for 2 seconds.
Flight
Instruments
SPLIT-PA MODE
Annun/
Alerts
3D AUDIO TROUBLESHOOTING
Appendix
If the aural messages are not heard in only the left and then the right ear respectively
the cause may be aircraft wiring or headset settings. Refer to the following table if a
headset or aircraft wiring problem is suspected.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
23
Flight
Instruments
Nav/Com/XPDR/Audio Panel
“3D audio left”
message heard
in both ears.
“3D audio right”
message not
heard
1) Mono headset in use
1) Use a stereo headset
2) Stereo headset in use
with mono/stereo switch
set to ‘mono’
2) Set mono/stereo switch on headset
to ‘stereo’
3) Aircraft wiring has left
audio wired to both left
and right channels of
stereo headset jack
3) If after checking solutions #1 and
#2 see a service center as soon as
possible to inspect/correct wiring.
This wiring fault can cause fail-safe
audio not to function.
“3D audio left”
message heard
in both ears,
followed by “3D
audio right”
message heard
in both ears
1) Mono headset in use
1) Use a stereo headset
2) Stereo headset in use
with mono/stereo switch
set to mono
2) Set mono/stereo switch on headset
to ‘stereo’
3) Incorrect aircraft wiring
(left/right shorted
together)
3) If after checking solutions #1 and
#2 see a service center as soon as
possible to inspect/correct wiring.
This wiring fault can cause fail-safe
audio not to function.
“3D audio right”
message heard
in both ears.
“3D audio left”
not heard
1) Incorrect aircraft wiring
(right channel used for
mono instead of left or
left/right swapped)
1) See a service center as soon as
possible to inspect/correct wiring.
This wiring fault can cause fail-safe
audio not to function.
“3D audio left”
message heard
in right ear only
followed by “3D
audio right”
message heard
in left ear only
1) Stereo headset is on
backwards
1) Verify correct orientation from the
left/right indication on each side of
the headset or the position of the
boom mic (usually attached on left
side). If the headset is backwards
left/right position information will be
swapped.
2) Incorrect aircraft wiring
(left/right channels
swapped)
2) See a service center as soon as
possible to inspect/correct wiring.
This wiring fault can cause fail-safe
audio not to function.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Symptom(s)
24
3D Audio Troubleshooting
Cause(s)
Solution(s)
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Symptom(s)
“3D audio right”
message heard
in right ear only,
no audio heard
in left ear
1) Incorrect aircraft wiring
(right channel used for
mono instead of left, or
left/right swapped)
1) See a service center as soon as
possible to inspect/correct wiring.
This wiring fault can cause fail-safe
audio not to function.
AFCS
1) See a service center to wire the
installation for stereo headsets.
Nav/Com/
XPDR/Audio
1) Aircraft wired for mono
intercom
EICAS
“3D audio left”
message heard
in left ear only,
no audio heard
in right ear.
Flight
Instruments
3D Audio Troubleshooting
Cause(s)
Solution(s)
GPS Nav
3D Audio Troubleshooting
VOICE RECOGNITION
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Voice Recognition allows the pilot (and optionally copilot) to control the GMA
350H using spoken commands. To activate Voice Recognition, hold the push to
command switch in the upward position while speaking a command. When the PushTo-Command switch is released, the GMA 350H will respond.
If a command is correctly interpreted by the GMA 350H, a positive acknowlegement chime will be played, and the pilot should verify that the correct button selection
is indicated by the triangular annunciator lights. Alternatively, some commands will
be indicated by a voice response from the GMA 350H. If the desired modes are not
indicated by annunciator lights or a voice response, the pilot should repeat the command by using the Push-To-Command switch, or by manually using the front panel
controls of the GMA 350H.
If a command is incorrectly interpreted by the GMA 350H, a negative acknowlegement tone will be played. The pilot should repeat the command by using the PushTo-Command switch, or by manually using the front panel controls of the GMA 350H.
In the event of any abnormal Voice Recognition operation, at any time the front panel
controls may be used manually to control the GMA 350H.
The following table lists the available Voice Recognition commands, the associated
actions, and the voice response if applicable:
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
25
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Control
Spoken Command
Action
Confirmation of Action
“COM one”
Toggles
COM1
Illuminate/Extinguish COM1
Annunciator
EICAS
“MIC one”
Nav/Com/
XPDR/Audio
“COM one MIC”
“COM two”
“MIC two”
AFCS
“COM two MIC”
GPS Nav
“COM three”
“MIC three”
Flight
Planning
“COM three MIC”
Annun/
Alerts
Illuminate/Extinguish COM2
Annunciator
Selects MIC2 Illuminate MIC2 Annunciator
Toggles
COM3
Illuminate/Extinguish COM3
Annunciator
Selects MIC3 Illuminate MIC3 Annunciator
Selects split
COM 1/2
Illuminate MIC1/MIC2
Annunciators
“Split COM one, two” or“Split
one, two”
Selects split
COM 1/2
Illuminate MIC1/MIC2
Annunciators
“Split COM one, three” or “Split
one, three”
Selects split
COM 1/3
Illuminate MIC1/MIC3
Annunciators
“Split COM two, three” or “Split
two, three”
Selects split
COM 2/3
Illuminate MIC2/MIC3
Annunciators
“Monitored COM mute” or
“Mute monitored COM”
Mutes
monitored
COM on
primary
COM
reception
Voice Response:
“Monitor mute enabled”
“Disable monitored COM mute”
or
“Monitored COM mute disable”
or
“Disable mute monitored COM”
or
“Mute monitored COM disable”
Disables
monitored
COM mute
on primary
COM
reception
Voice Response:
“Monitor mute disabled”
Index
Appendix
Toggles
COM2
“Split COM”
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
COM
Selects MIC1 Illuminate MIC1 Annunciator
26
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Confirmation of Action
“NAV one”
Toggles
NAV1
Illuminate/Extinguish NAV1
Annunciator
“NAV two”
Toggles
NAV2
Illuminate/Extinguish NAV2
Annunciator
“NAV”
Toggles NAV
Illuminate/Extinguish
Annunciator
“AUX” or
“Auxiliary”
Toggles AUX
Illuminate/Extinguish AUX
Annunciator
“Telephone” or
“Phone” or
“Jack”
Toggles
Telephone/
Jack
AFCS
Illuminate/Extinguish
Annunciator
GPS Nav
Mutes
Voice Response:
Telephone/
Jack on radio “Tel and jack mute enabled”
reception
Flight
Planning
Procedures
“Telephone mute” or
“Phone mute” or
“Jack mute”or
“Mute telephone” or
“Mute phone” or
“Mute jack”
Nav/Com/
XPDR/Audio
AUX
Action
EICAS
NAV
Spoken Command
Flight
Instruments
Control
Disables
Telephone/
Jack mute
on radio
reception
Voice Response:
“Tel and jack mute disabled”
Speaker
(SPKR)
“Speaker”
Toggles
SPKR on/off
Illuminate/Extinguish SPKR
Annunciator
PA
“P - A”
Toggles PA
on/off
SPKR Annunciator blinks in
PA mode
Hazard
Avoidance
“Disable telephone mute”
“Mute telephone disable”
“Disable phone mute”
“Mute phone disable”
“Disable jack mute”
“Mute jack disable”
“Telephone mute disable”
“Disable mute telephone”
“Phone mute disable”
“Disable mute phone”
“Jack mute disable”
OR
“Disable mute jack”
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
27
Nav/Com/XPDR/Audio Panel
EICAS
Flight
Instruments
Control
ICS Isolation
Copilot
Configuration
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
MUSIC
28
Spoken Command
Action
Confirmation of Action
“MUSIC”
Toggles
MUSIC
Illuminate/Extinguish MUSIC
Annunciator
“MUSIC mute” or
“Mute MUSIC”
Mutes
MUSIC
on radio
reception
Voice Response:
“Music mute enabled”
“Disable MUSIC mute”
“MUSIC mute disable”
“Disable mute MUSIC”
OR
“Mute MUSIC disable”
Disables
MUSIC mute
on radio
reception
Voice Response:
“Music mute disabled”
“Pilot”
Toggles
PILOT button
Illuminate/Extinguish PILOT
Annunciator
“Copilot”
Toggles
COPLT
button
Illuminate/Extinguish COPLT
Annunciator
“Passenger” or
“Pass”
Toggles
PASS button
Illuminate/Extinguish PASS
Annunciator
“Passenger mute” or
“Pass mute” or
“Mute passenger” or
“Mute pass”
Mutes
passengers
during radio
reception
Voice Response:
“Passenger mute enabled”
“Disable passenger mute” or
“Disable pass mute” or
“Disable mute passenger” or
“Disable mute pass” or
“Passenger mute disable” or
“Pass mute disable” or
“Mute passenger disable” or
“Mute pass disable”
Disables
muting of
passengers
during radio
reception
Voice Response:
“Passenger mute disabled”
“Copilot is passenger” or
“Copilot is pass”
Configures
Copilot as a
passenger
Voice Response:
“Copilot is passenger”
“Copilot is crew”
Configures
Copilot as
flight crew
Voice Response:
“Copilot is crew”
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Confirmation of Action
Marker
Beacon (MKR/
MUTE)
“Marker” or
“Mute marker” or
“Marker mute”
Marker
Beacon
audio on/
off (refer
to Marker
Beacon
section for
details)
Illuminate/Extinguish MKR/
MUTE Annunciator
Cursor
“Cursor off” or
“Cursor cancel” or
“Cancel cursor”
Cancels
cursor when
cursor is
flashing
Cursor is removed
“Manual squelch” or
“Man squelch”
Toggles
manual
squelch
Illuminate/Extinguish MAN
SQ Annunciator
“Manual squelch threshold up”
or
“Manual squelch volume up” or
“Man squelch threshold up” or
“Man squelch volume up”
Increases
manual
squelch
threshold
Manual squelch threshold
increased
“Manual squelch threshold
down” or
“Manual squelch volume down”
or
“Man squelch threshold down”
or
“Man squelch volume down”
Decreases
manual
squelch
threshold
Manual squelch threshold
decreased
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Manual
Squelch
Nav/Com/
XPDR/Audio
Action
EICAS
Spoken Command
Flight
Instruments
Control
Additional
Features
Abnormal
Operation
Annun/
Alerts
NOTE: Finer manual squelch adjustment may be made using the dual
concentric knobs on the GMA 350H. The voice command “Up” or “Down” is
equivalent to three clicks of the inner knob..
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
29
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Control
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
COM
Clearance
Recorder
Procedures
Flight
Planning
Distribution
(Blue Mode)
Action
Confirmation of Action
“Play” or
“Read back” or
“Say again”
Plays
recorded
clearance
audio (refer
to Clearance
Recorder
section for
details)
Recorded audio playing
“Distribute telephone to
(**desired position(s))” or
“Distribute phone to (**desired
position(s))” or
“Distribute jack to (**desired
position(s))”
Distributes
TEL/JACK
to desired
positions
TEL/JACK audio heard at
desired position(s)
“Distribute music to (**desired
position(s))”
Distributes
MUSIC to
desired
position(s)
MUSIC heard at desired
position(s)
Additional
Features
Hazard
Avoidance
** Desired position(s) = “All”, “none”, “pilot”, “copilot”, “passenger”, “pass”,
or any combination of pilot, copilot, passenger, or pass.
“(*Desired selection) volume up”
Increases
volume
of desired
selection
Volume of desired selection
increased
“(*Desired selection) volume
down”
Decreases
volume
of desired
selection
Volume of desired selection
decreased
Displays
the current
volume but
does not
change it
Current volume displayed
Volume
Adjustments
“(Desired selection*) volume
Appendix
NOTE: Finer volume adjustment may be made using the dual concentric knobs
on the GMA 350H. The voice command “Up” or “Down” is equivalent to three
click of the inner knob.
Index
Annun/
Alerts
Abnormal
Operation
Spoken Command
* Desired selection = “speaker”, “pilot”, “copilot”, “passenger”, “pass”,
“marker”, “aux”, “auxiliary”, “telephone”, “phone”, “jack”, or “music”.
30
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Nav/Com/XPDR/Audio Panel
Confirmation of Action
“Three-D audio”
Enables 3D
audio
Voice Response:
“Three-D audio left, three-D
audio right”
“Standard audio”
Enables
standard
audio
(disables 3D
audio)
Voice Response:
“Standard Audio”
3D Audio
Nav/Com/
XPDR/Audio
Action
EICAS
Spoken Command
Flight
Instruments
Control
AFCS
Voice Recognition Commands
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
31
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
32
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
AFCS
Flight
Instruments
AUTOMATIC FLIGHT CONTROL SYSTEM
This feature is not currently available on the Bell 505 Jet Ranger X.
EICAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
33
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
AFCS
Blank Page
34
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
EICAS
Direct-to Navigation from the MFD
2)
3)
6)
9)
12)
1)
2)
5)
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
35
Index
6)
Appendix
4)
).
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
) Key.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EICAS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the OFFSET distance field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
Press the ACT LEG Softkey on the MFD.
3)
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
4)
With ‘Activate’ highlighted, press the ENT Key.
Index
Appendix
OR
36
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION (VNAV)
AFCS
GPS Nav
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EICAS
1)
Flight
Planning
Procedures
Large White
Text
Large Cyan
Text
Hazard
Avoidance
Small Cyan
Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Additional
Features
Small Cyan
Subdued Text
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
37
Altitudes associated with approach procedures are “auto-designated”. This means
the system automatically uses the altitudes loaded with the approach for giving vertical
flight path guidance outside the FAF. Note these altitudes are displayed as small cyan
text.
Altitudes associated with arrival procedures are “manually-designated”. This
means the system does not use the altitudes loaded with the arrival for giving vertical
flight path guidance until designated to do so by the pilot. Note that these altitudes
are initially displayed as white text. These altitudes may be “designated” by placing
the cursor over the desired altitude and pressing the ENT Key. After designation, the
text changes to cyan.
Altitudes that have been designated for use in vertical navigation may also be
made “non-designated” by placing the cursor over the desired altitude and pressing
the CLR Key. The altitude is now displayed only as a reference. It will not be used
to give vertical flight path guidance. Other displayed altitudes may change due to
re-calculations or rendered invalid as a result of manually changing an altitude to a
non-designated altitude.
White Text
Cyan Text
Large Text
Altitude calculated by the
system estimating the
altitude of the aircraft as it
passes over the navigation
point. This altitude is
provided as a reference
and is not designated to
be used in determining
vertical flight path
guidance.
Altitude has been entered
by the pilot. Altitude is
designated for use in
giving vertical flight path
guidance. Altitude does
not match the published
altitude in navigation
database or no published
altitude exists.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text
Altitude is not designated
to be used in determining
vertical flight path
guidance. Altitude has
been retrieved from the
navigation database and
is provided as a reference.
Altitude is designated for
use in giving vertical flight
path guidance. Altitude
has been retrieved from
the navigation database
or has been entered by
the pilot and matches a
published altitude in the
navigation database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
GPS Navigation
38
Cyan Subdued Text
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
GPS Navigation
EICAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
The system updates vertical path guidance continuously using ground speed and
the calculated distance to the Bottom of Descent (BOD). Due to turn anticipation
guidance (turn-smoothing), distance to the BOD can be affected by course changes
greater than approximately 5 degrees. Ground speed can be affected by factors such as
shifts in wind direction, aircraft power management, pitch angle, and course changes.
Abrupt and/or substantial changes to either the distance to the BOD, ground speed, or
both can cause similarly abrupt/substantial changes in vertical path guidance.
Because of turn-smoothing, changes to both distance to the BOD and ground speed
tend to be more extreme when the BOD is also a waypoint that marks a large course
change. These speed and distance changes will be accounted for in the computed
required vertical path and reflected in the vertical guidance indications.
Flight
Instruments
NOTE: Making course changes greater than 90° during a descent with vertical
guidance may cause excessive and rapid movement of the vertical deviation
indicator, and SVS Pathways.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
39
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
GPS Navigation
Blank Page
40
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Flight
Instruments
FLIGHT PLANNING
WEIGHT AND BALANCE PLANNING
AFCS
Modifying basic empty weight:
Select the W&B CFG Softkey; or press the MENU Key, highlight ‘Weight
& Balance Configuration’, and press the ENT Key to display the Weight &
Balance Configuration Page.
2)
Press the FMS Knob to activate the cursor, and turn the large FMS Knob to
select the ‘AIRCRFT’ weight.
3)
Turn the small FMS Knob to enter the weight. The new weight will be
reflected in the Basic Empty Weight shown at the top of the page.
4)
Press the GO BACK Softkey to return to the AUX - WEIGHT & BALANCE
Page.
GPS Nav
1)
Procedures
Additional
Features
Turn the small FMS Knob to enter the weight.
4)
Press the ENT Key to confirm the entry and move the cursor to the next
field.
5)
Repeat steps 3 and 4 as necessary.
6)
Press the FMS Knob to remove the flashing cursor.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
41
Index
The ‘ZERO FUEL WEIGHT’ is calculated by adding the basic empty
weight and the aircraft load weights.
Appendix
3)
Annun/
Alerts
Turn the large FMS Knob to highlight the ‘PILOT’ field.
Abnormal
Operation
2)
Hazard
Avoidance
Entering the aircraft load weights:
Press the FMS Knob to activate the cursor.
Flight
Planning
The ‘BASIC EMPTY WEIGHT” is calculated by summing the weights of all
items marked as present.
1)
Nav/Com/
XPDR/Audio
All procedures apply to the AUX - WEIGHT & BALANCE Page on the MFD unless
otherwise stated.
EICAS
NOTE: All weight & balance page data fields display data rounded to the
nearest 5 pounds or 5 kilograms
Flight Planning
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Entering the fuel on board weight:
Press the FMS Knob to activate the cursor and highlight the ‘FUEL ON
BOARD’ field.
2)
Turn the small FMS Knob to enter the fuel on board weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Or:
AFCS
Press the FOB SYNC Softkey. The fuel on board weight is set to the current
measured fuel weight.
GPS Nav
The ‘TAKEOFF WEIGHT’ is calculated by adding the zero fuel weight and
the fuel on board weight.
Hazard
Avoidance
Procedures
Flight
Planning
Entering the hook weight:
1)
Select the HOOK WT Softkey to activate the cursor on the ‘HOOK WEIGHT’
field.
2)
Turn the small FMS Knob to enter the hook weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor.
Additional
Features
The ‘GROSS WEIGHT’ is calculated by adding the takeoff weight and the
hook weight.
Annun/
Alerts
Abnormal
Operation
Entering the fuel reserve weight:
1)
Press the FMS Knob to activate the cursor and highlight the ‘FUEL
RESERVES’ field.
2)
Turn the small FMS Knob to enter the fuel reserves weight.
3)
Press the ENT Key to confirm the entry.
4)
Press the FMS Knob to remove the flashing cursor
TRIP PLANNING
Index
Appendix
1)
42
1)
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the Trip Planning Page.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
4)
For Direct-to planning:
EICAS
The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
Nav/Com/
XPDR/Audio
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
AFCS
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
GPS Nav
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
Flight
Planning
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Procedures
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
c) Again, enter the identifier of the ending waypoint.
Hazard
Avoidance
d) Press the ENT Key to accept the waypoint.
Or:
Additional
Features
For flight plan leg planning:
a) Press the FPL Softkey (at the bottom of the display).
Abnormal
Operation
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
43
Index
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Appendix
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
Annun/
Alerts
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ is an available option to display planning data for the
remainder of the flight plan.
5)
Flight
Instruments
3)
Flight
Instruments
Flight Planning
EICAS
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
7)
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
8)
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
9)
The flashing cursor moves to the fuel onboard field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel
onboard is provided by the fuel totalizer.
Flight
Planning
GPS Nav
AFCS
6)
Nav/Com/
XPDR/Audio
NOTE: The departure time on the Trip Planning Page is used for preflight
planning. Refer to the Utility Page for the actual flight departure time.
Procedures
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
Hazard
Avoidance
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
Additional
Features
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
1)
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
44
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
EICAS
Press the ENT Key.
Flight
Instruments
5)
Nav/Com/
XPDR/Audio
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
8)
Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9)
Press the ENT Key.
GPS Nav
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
AFCS
7)
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Additional
Features
Turn the small FMS Knob to select the User WPT Information Page.
Hazard
Avoidance
2)
Procedures
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Flight
Planning
1)
Abnormal
Operation
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
8)
Turn the small FMS Knob to select RAD/RAD (radial/radial).
9)
Press the ENT Key.
Appendix
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Annun/
Alerts
7)
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
45
Flight Planning
Flight
Instruments
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
EICAS
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Nav/Com/
XPDR/Audio
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
d) Press the ENT Key.
Or:
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Additional
Features
d) Press the ENT Key.
Or:
Abnormal
Operation
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Annun/
Alerts
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Appendix
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
12) Press the ENT Key.
Index
13) Repeat step 10 to enter the next waypoint name.
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
46
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Flight
Instruments
15) Press the ENT Key.
16) Press the FMS Knob to remove the flashing cursor.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Flight
Planning
Turn the small FMS Knob to select the User WPT Information Page.
GPS Nav
2)
AFCS
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Nav/Com/
XPDR/Audio
1)
EICAS
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
Procedures
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
8)
Turn the small FMS Knob to select RAD/DIS (radial/distance).
9)
Press the ENT Key.
Additional
Features
With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Abnormal
Operation
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
b) Turn the large FMS Knob to select the desired waypoint.
Appendix
c) Press the ENT Key.
Or:
47
Index
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Annun/
Alerts
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
190-02065-00 Rev. A
Hazard
Avoidance
7)
Flight Planning
Flight
Instruments
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
EICAS
d) Press the ENT Key.
Or:
Nav/Com/
XPDR/Audio
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
AFCS
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
d) Press the ENT Key.
Or:
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
Procedures
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Hazard
Avoidance
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
12) Press the ENT Key.
Additional
Features
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Abnormal
Operation
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
Index
Appendix
Annun/
Alerts
DELETE A USER WAYPOINT
48
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
5)
Turn the small FMS Knob to highlight the desired waypoint.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
EICAS
CREATE A FLIGHT PLAN
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
49
Flight
Planning
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
GPS Nav
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Press the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
AFCS
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
3) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
4) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key. The
active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Nav/Com/
XPDR/Audio
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
190-02065-00 Rev. A
Flight
Instruments
6)
5)
Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6)
Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7)
When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
IMPORT A FLIGHT PLAN FROM AN SD CARD
NOTE: See the Annunciations & Alerts section for flight plan import message
descriptions.
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
1)
Insert the SD card containing the flight plan in the top card slot on the
MFD.
2)
Press the FPL Key on the MFD to display the Active Flight Plan Page.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn either FMS Knob to highlight an empty or existing flight plan.
6)
Press the IMPORT Softkey.
Hazard
Avoidance
If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.
Or:
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
If an existing flight plan is selected, an ‘Overwrite existing flight plan?
OK or CANCEL’ prompt is displayed. Press the ENT Key to choose to
overwrite the selected flight plan and see a list of the available flight
plans on the SD card. If overwriting the existing flight plan is not
desired, select ‘CANCEL’ using the FMS Knob, press the ENT Key, select
another existing or empty flight plan, and again press the IMPORT
Softkey.
50
1)
Press the FPL Key to display the active flight plan.
2)
If required, press the FMS Knob to activate the cursor.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5)
Enter the new flight plan waypoint by one of the following:
EICAS
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
Nav/Com/
XPDR/Audio
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
Or:
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
d) Press the ENT Key.
Or:
Hazard
Avoidance
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
Additional
Features
d) Press the ENT Key.
e) Press the ENT Key again to accept the waypoint.
Abnormal
Operation
ENTER AN AIRWAY IN A FLIGHT PLAN
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).
51
Index
2)
Appendix
Press the FPL Key.
Annun/
Alerts
1)
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
190-02065-00 Rev. A
Flight
Instruments
3)
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
USER-DEFINED HOLDING PATTERNS
A holding pattern can be defined at any active flight plan waypoint, or at the aircraft
present position.
Creating a user-defined hold at an active flight plan waypoint:
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
1)
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the waypoint for the hold.
3)
Press the MENU Key, highlight ‘Hold At Wpt’, and press the ENT Key. The
HOLD AT window appears with the course field highlighted.
4)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
Index
Appendix
10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the
flight plan.
52
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Press the MENU Key, highlight ‘Hold At Present Position’, and press the
ENT Key. The HOLD AT window appears with the Length mode highlighted.
3)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
4)
Use the FMS Knobs to edit the length, and press the ENT Key.
5)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
6)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
7)
Press the ENT Key while ‘ACTIVATE?’ is highlighted to immediately activate
the hold.
AFCS
2)
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
EICAS
1)
Flight
Instruments
Creating a user-defined hold at the aircraft present position:
GPS Nav
Flight
Planning
Creating a User-Defined Hold at a Direct-To Waypoint:
Procedures
Press a Direct-to Key and set up the Direct To waypoint as desired, but
select ‘HOLD?’ instead of ‘ACTIVATE?’ when finished.
2)
Use the FMS Knobs to edit the entry course, and press the ENT Key.
5)
Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course
direction, and press the ENT Key.
6)
Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press
the ENT Key.
7)
Use the FMS Knobs to edit the length, and press the ENT Key.
8)
Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and
press the ENT Key.
9)
Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME),
and press the ENT Key.
Hazard
Avoidance
1)
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
10) Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the Direct To
with the user-defined hold defined at the Direct To waypoint.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
53
Flight Planning
1)
Press the Direct To Key to display the DIRECT TO Window (PFD or MFD).
EICAS
2)
Press the MENU Key to display the PAGE MENU with the cursor on the
‘Cancel Direct To NAV’ selection.
Nav/Com/
XPDR/Audio
Flight
Instruments
Removing a user-defined hold (created at the aircraft present position
or at a Direct-To waypoint):
3)
Press the ENT Key. The holding pattern is removed.
Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active
Flight Plan Window (PFD).
2)
Press the FMS Knob to activate the cursor (not required on the PFD) and
turn the large FMS Knob to highlight the HOLD waypoint.
3)
Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is
displayed.
4)
Select ‘OK’ and press the ENT Key. The holding pattern is removed from
the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the
removal of the holding pattern.
Abnormal
Operation
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
4)
Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5)
With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
1)
Appendix
Annun/
Alerts
1)
INVERT AN ACTIVE FLIGHT PLAN
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Removing a user-defined hold (created at an active flight plan
waypoint):
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
Index
a) Press the FPL Key on the MFD.
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
54
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Flight
Instruments
c) Press the FMS Knob to activate the cursor.
d) Turn the large FMS Knob to highlight the desired flight plan.
e) Press the EDIT Softkey.
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
STORE A FLIGHT PLAN
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Flight
Planning
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
Press the FPL Key on the MFD, then turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
Hazard
Avoidance
1)
Additional
Features
Abnormal
Operation
Or, for a stored flight plan:
a) Press the FPL Key on the MFD.
Index
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
c) Press the FMS Knob to activate the cursor.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Appendix
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Annun/
Alerts
DELETE A WAYPOINT FROM THE FLIGHT PLAN
190-02065-00 Rev. A
Procedures
EDIT A STORED FLIGHT PLAN
1)
GPS Nav
1)
AFCS
3)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
EICAS
2)
55
Flight Planning
Flight
Instruments
d) Turn the large FMS Knob to highlight the desired flight plan.
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the
cursor.
Procedures
Hazard
Avoidance
1)
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
COPY A FLIGHT PLAN
1)
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
2)
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
e) Press the EDIT Softkey.
56
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Flight Planning
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
AFCS
EICAS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
DELETE A FLIGHT PLAN
GPS Nav
GRAPHICAL FLIGHT PLAN CREATION
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Press the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Abnormal
Operation
3)
Additional
Features
Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
Hazard
Avoidance
2)
Procedures
Press the FPL Key on the MFD to display the Active Flight Plan Page.
Flight
Planning
1)
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
57
EXPORT A FLIGHT PLAN TO AN SD CARD
NOTE: See the Annunciations & Alerts section for flight plan export message
descriptions.
1)
Insert the SD card into the top card slot on the MFD.
2)
Press the FPL Key to display the Active Flight Plan Page on the MFD.
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Flight Planning
58
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EICAS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Procedures
Hazard
Avoidance
ACTIVATE A DEPARTURE LEG
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
59
LOAD AN ARRIVAL PROCEDURE
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Press the ENT Key.
Flight
Planning
10) With ‘LOAD?’ highlighted, press the ENT Key.
11) The arrival becomes part of the active flight plan.
Procedures
12) If an altitude associated with a waypoint in an arrival procedure is to be
used to calculate vertical guidance perform the following steps:
a) Press the FMS Knob to activate the cursor.
c) Press the ENT Key to designate the altitude for use in giving vertical
guidance.
ACTIVATE AN ARRIVAL LEG
1)
Press the FPL Key to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
60
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Procedures
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
6)
Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
8)
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO, TEMP
COMP or optional RAD ALT.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
EICAS
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Flight
Instruments
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
10) Press the ENT Key. If BARO, or OFF was selected step 8, proceed to step
11. If TEMP COMP was selected in step 8, the cursor moves to the ‘TEMP
AT....” field. Turn the small FMS Knob to enter the temperature at the
destination airport. The temperature compensated altitude minimum is
displayed below the previously enter minimum altitude value.
Appendix
11) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
61
Procedures
Flight
Instruments
12) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
13) Press the ENT Key.
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
1)
ACTIVATE A VECTOR TO FINAL APPROACH FIX
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
62
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Hazard Avoidance
When temperature compensated altitude is enabled for the loaded approach, the
altitudes associated with the approach waypoints are displayed in slanted text.
Flight
Instruments
TEMPERATURE COMPENSATED ALTITUDE
EICAS
Nav/Com/
XPDR/Audio
AFCS
Altitudes Displayed With
Temperature Compensation
GPS Nav
Altitudes Displayed Without
Temperature Compensation
Procedures
Use the small FMS Knob to select the temperature at the <airport>. The
compensated altitude is computed as the temperature is selected.
Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted.
6)
Press the ENT Key. The compensated altitudes for the approach are
Additional
Features
5)
shown in the flight plan.
Abnormal
Operation
Annun/
Alerts
Disabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted.
Appendix
Press the ENT Key. The temperature compensated altitude at the FAF
is cancelled.
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
63
Index
5)
Hazard
Avoidance
4)
Flight
Planning
Enabling temperature compensated altitude:
1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is
displayed.
2) Turn the FMS Knob to highlight ‘Temperature Compensation’.
3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is
displayed.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Hazard Avoidance
Blank Page
64
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
EICAS
1)
Nav/Com/
XPDR/Audio
AFCS
TRAFFIC SYSTEMS
Procedures
Description
Flight
Planning
Traffic Symbol
GPS Nav
• If Traffic information Service (TIS) is configured, STANDBY, OPERATE, and
TNA MUTE softkeys are displayed.
• If a Traffic Advisory System (TAS) is configured, STANDBY, NORMAL, TEST,
and ALT MODE softkeys are displayed.
Non-Threat Traffic without ADS-B directional information
Hazard
Avoidance
Proximity Advisory (PA) (GTS 800 only)
Additional
Features
Traffic Advisory (TA)
Abnormal
Operation
Traffic Advisory Off Scale
Traffic Advisory (TA) arrow with ADS-B directional information. Points in
the direction of the intruder aircraft track (GTS 800 only).
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
65
Traffic Symbol
Description
Proximity Advisory (PA) arrow with ADS-B directional information. Points in
the direction of the aircraft track (GTS 800 only).
Non-threat traffic arrow with ADS-B directional information. Points in the
direction of the intruder aircraft track (GTS 800 only).
EICAS
Flight
Instruments
Hazard Avoidance
AFCS
Nav/Com/
XPDR/Audio
PA or Non-threat traffic arrow with ADS-B directional information, but
positional accuracy is degraded. Points in the direction of the aircraft
track. (Not available in all installations.) (GTS 800 only).
Traffic Symbol Description
GPS Nav
Traffic Information Service (TIS)
Flight
Planning
NOTE: If the G1000H is configured to use a Traffic Advisory System (TAS), TIS
is not available for use.
Procedures
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
66
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Hazard Avoidance
Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
EICAS
1)
Flight
Instruments
Displaying Traffic on the Navigation Map
Traffic Advisory System (TAS)(Optional)
4)
Press the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
5)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
7)
Press the FLT ID Softkey to enable or disable Flight ID displayed with the
intruder information.
Abnormal
Operation
Press the OPERATE or NORMAL Softkey to begin displaying traffic.
‘OPERATING’ is displayed in the Traffic Mode field.
Additional
Features
3)
Hazard
Avoidance
Turn the small FMS Knob to select the Traffic Map Page.
Procedures
2)
Flight
Planning
Turn the large FMS Knob to select the Map Page Group.
GPS Nav
1)
Annun/
Alerts
System Self Test
2)
Press the STANDBY Softkey.
3)
Press the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert is heard (see
Alerts and Annunciations section). If the self test fails, the system reverts to
Standby Mode and a voice alert is heard.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
67
Index
With the Traffic Map Page displayed, set the range to 2/6 nm.
Appendix
1)
190-02065-00 Rev. A
AFCS
Displaying Traffic on the Traffic Map Page
Nav/Com/
XPDR/Audio
NOTE: Radar altimeter data is optional for the Traffic Advisory System (TAS).
If radar altimeter data is detected by the TAS at the beginning of a power
cycle and that data is subsequently lost, the TAS will declare a fault and will
not provide traffic information.
Hazard Avoidance
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, press the MAP Softkey.
3)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
HELICOPTER TERRAIN AWARENESS & WARNING SYSTEM (HTAWS) DISPLAY
(OPTIONAL)
WARNING: Do not use HTAWS information for primary terrain avoidance.
HTAWS is intended only to enhance situational awareness.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Displaying Traffic on the Navigation Map
Flight
Planning
GPS Nav
NOTE: The data contained in the HTAWS databases comes from government
agencies. Garmin accurately processes and cross-validates the data but cannot
guarantee the accuracy and completeness of the data.
Procedures
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
NOTE: The terrain system is not available north of 89º North latitude and
Hazard
Avoidance
south of 89º South latitude.
Additional
Features
Displaying the HTAWS Page:
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select HTAWS Page.
Annun/
Alerts
Abnormal
Operation
Changing the HTAWS Page view:
1)
Press the VIEW Softkey.
2)
Press the 360 or ARC Softkey to select the desired view.
1)
Press the MENU Key.
2)
Select ‘View Arc’ or ‘View 360º’ and press the ENT Key to change the view.
Index
Appendix
Or:
68
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Hazard Avoidance
Aircraft Altitude +250 ft
Flight
Instruments
Red
Terrain is more than
250 ft above the
aircraft altitude
Aircraft Altitude
Aircraft Altitude -250 ft
Terrain is between 250
Green ft and 500 ft below the
aircraft altitude
Aircraft Altitude -500 ft
Terrain is more
than 500 ft below
the aircraft altitude
AFCS
Black
Nav/Com/
XPDR/Audio
Terrain is between 0 ft
Yellow and 250 ft below the
aircraft altitude
Lighted Obstacle
EICAS
Terrain is between 250
Orange ft and 0 ft above the
aircraft altitude
Terrain Altitude/Color
forindicates
HTAWSno terrain data is available.
On the Terrain Proximity
Page only, a gray Correlation
shade of purple
GPS Nav
Unlighted Obstacle
Lighted Obstacle
Obstacle Location
Flight
Planning
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL
Procedures
Red obstacle is at or
above current aircraft
altitude
Hazard
Avoidance
Yellow obstacle is
between 0’ and 250’
below current aircraft
altitude
Additional
Features
Gray obstacle is 250’
or more below current
aircraft altitude
Alert Type
Example
Annunciation
Annun/
Alerts
Potential Impact
Point Symbol
Abnormal
Operation
HTAWS Obstacle Colors and Symbology
Warning
Appendix
Caution
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
HTAWS Potential Impact Point Symbols with Alert Types
69
Hazard Avoidance
Flight
Instruments
Showing/hiding aviation information on the HTAWS Page:
1)
Press the MENU Key.
EICAS
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on
current state) and press the ENT Key.
AFCS
Nav/Com/
XPDR/Audio
Manually testing the HTAWS System:
1)
Select the HTAWS Page.
2)
Press the MENU Key.
3)
Select ‘Test HTAWS System’ and press the ENT Key to confirm the selection.
GPS Nav
Muting/Unmuting Caution Alerts:
1)
Turn the large FMS Knob to select the HTAWS Page on the MFD.
2)
Press the MUTE CTN Softkey.
Procedures
Flight
Planning
Or:
1)
Press the MENU Key.
2)
Select ‘Mute Active Caution’ or ‘Unmute Active Caution’ (choice dependent
on current state) and press the ENT Key.
1)
Select the HTAWS Page.
2)
Press the INHIBIT Softkey to inhibit or enable HTAWS (choice dependent
on current state).
Additional
Features
Hazard
Avoidance
Inhibiting/enabling PDA and FLTA alerting:
Abnormal
Operation
Or:
1)
Press the MENU Key.
2)
Select ‘Inhibit HTAWS’ or ‘Enable HTAWS’ (choice dependent on current
state) and press the ENT Key.
Index
Appendix
Annun/
Alerts
Configuring VCO alerting altitudes:
70
1)
Turn the large FMS knob to select the AUX - System Setup Page.
2)
If the Aux - System Setup 2 Page is not already displayed, press the SETUP
2 Softkey.
3)
Press the FMS Knob to activate the cursor.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Hazard Avoidance
Turn the small FMS Knob to select the maximum altitude at which VCO
alerts will be enabled from (from 50 to 500 feet), or select NONE to disable
all VCO alerts.
6)
When finished, press the FMS Knob.
Nav/Com/
XPDR/Audio
5)
PROFILE VIEW TERRAIN
Flight
Planning
Accessing Profile View:
2)
Press the MAP Softkey.
3)
Press the PROFILE Softkey to enable or disable Profile View.
Procedures
Select the Navigation Map Page.
Hazard
Avoidance
Or:
Press the MENU Key.
2)
Select ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on
current state) and press the ENT Key.
Additional
Features
1)
2)
Press the MAP Softkey.
Annun/
Alerts
Select the Navigation Map Page.
Abnormal
Operation
Enabling/Disabling Profile View Terrain on the Navigation Map (when
Profile View is enabled):
1)
GPS Nav
NOTE: Terrain data is not displayed when the aircraft is outside of the installed
terrain database coverage area.
AFCS
WARNING: Do not use Profile View Terrain data for primary terrain avoidance.
Profile View Terrain is intended only to enhance situational awareness.
1)
EICAS
Turn the large FMS Knob to highlight the altitude shown in the MAX
SELECTED field.
Flight
Instruments
4)
3) Press the TERRAIN Softkey.
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
71
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Hazard Avoidance
Blank Page
72
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION (OPTIONAL)
EICAS
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVT is intended as an aid to situational
awareness only and may not provide the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
AFCS
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Additional
Features
Enabling and disabling SVT:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the SYN TERR Softkey. The SVT display will cycle on or off with the
SYN TERR Softkey.
190-02065-00 Rev. A
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Traffic Display
Terrain and Obstacle Alerting
Airport Signs
Runway Display
Procedures
•
•
•
•
•
•
•
Flight
Planning
Synthetic Vision Technology (SVT) functionality is offered as an enhancement to
the G1000H Integrated Flight Deck System.
SVT is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVT information is shown on the primary flight display (PFD).
SVT offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVT enhancement to the PFD, the following feature enhancements
have been added to the PFD:
GPS Nav
WARNING: Do not use SVT runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
73
Additional Features
EICAS
Flight
Instruments
Enabling and disabling Pathways:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the PATHWAY Softkey. The Pathway feature will cycle on or off with
the PATHWAY Softkey.
AFCS
Nav/Com/
XPDR/Audio
Enabling and disabling Horizon Headings:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the HRZN HDG Softkey. The horizon heading display will cycle on or
off with the HRZN HDG Softkey.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Enabling and disabling Airport Signs:
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) Press the APTSIGNS Softkey. Display of airport signs will cycle on or off
with the APTSIGNS Softkey.
SafeTaxi® (Optional)
SafeTaxi® gives greater map detail as the map range is adjusted in on the airport.
The airport display on the map reveals runways with numbers, taxiways identifiers, and
airport landmarks including ramps, buildings, control towers, and other prominent
features. Resolution is greater at lower map ranges. The aircraft symbol provides
situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing the DCLTR Softkey again cycles
back to the original map detail.
74
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Additional Features
Procedures
Hazard
Avoidance
Additional
Features
1)
Flight
Planning
View Charts from the Navigation Map Page
GPS Nav
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. The selected Display Pane depiction shows the aircraft position on the moving
map in the plan view of most approach charts and on airport diagrams.
The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.
AFCS
FliteCharts® (Optional)
Nav/Com/
XPDR/Audio
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.
EICAS
ChartView (Optional)
Flight
Instruments
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
Press the SHW CHRT Softkey when displayed.
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
3)
Press the GO BACK Softkey to return to the previous page.
Appendix
Press the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
Annun/
Alerts
2)
Abnormal
Operation
Or:
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
75
Additional Features
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
View Charts from the Active Flight Plan Page
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Press the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Change Day/Night View
Additional
Features
Abnormal
Operation
Annun/
Alerts
While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
1)
While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
6)
In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
AIRPORT DIRECTORY
The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK
Airport Directory add enhanced airport information when viewing airports on the
WPT-Airport Information Page.
Both Airport Directories are available for downloading at flygarmin.com. However,
copy only one of the databases to the Supplemental Data Card. The system cannot
recognize both databases simultaneously.
Index
Appendix
1)
76
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Additional Features
Flight
Instruments
View Airport Directory Information
EICAS
While viewing the WPT-Airport Information Page, if necessary, press the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Turn the large FMS Knob to highlight the first empty scheduler message
naming field.
4)
Use the FMS Knob to enter the message text to be displayed in the
Messages Window and press the ENT Key.
5)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the field next to Type.
6)
Turn the small FMS Knob to select the message type:
Appendix
3)
Annun/
Alerts
Press the FMS Knob momentarily to activate the flashing cursor.
Abnormal
Operation
2)
Additional
Features
1) Select the AUX - Utility Page.
• Event—Message issued at the specified date/time
Index
• One-time—Message issued when the message timer reaches zero
(default setting)
• Periodic—Message issued each time the message timer reaches zero
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
AFCS
Entering a scheduler message:
190-02065-00 Rev. A
Nav/Com/
XPDR/Audio
SCHEDULER
The Scheduler feature can be used to enter and display reminder messages (e.g.,
Phase 1 Inspection, Switch fuel tanks, or Altimeter-Transponder Check) in the
Messages Window on the PFD. Messages can be set to display based on a specific date
and time (event), once the message timer reaches zero (one-time; default setting), or
recurrently whenever the message timer reaches zero (periodic). Message timers set
to periodic alerting automatically reset to the original timer value once the message is
displayed. When power is cycled, all messages are retained until deleted, and message
timer countdown is resumed.
Scheduler messages appear in the Messagess Window on the PFD. When a
scheduler message is waiting, the MSG Softkey flashes. Pressing the MSG Softkey
opens the Messages Window and acknowledges the scheduler message. The softkey
label no longer flashes after pressing the MSG Softkey. Pressing the MSG Softkey
again removes the Messages Window from the display, and the scheduler message is
deleted from the message queue.
77
EICAS
Flight
Instruments
Additional Features
7)
Press the ENT Key again or use the large FMS Knob to move the cursor to
the next field.
8)
For periodic and one-time message, use the FMS Knob to enter the timer
value (HH:MM:SS) from which to countdown and press the ENT Key.
9)
For event-based messages:
Nav/Com/
XPDR/Audio
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press
the ENT Key.
AFCS
b) Press the ENT Key again or use the large FMS Knob to move the cursor
to the next field.
c) Use the FMS Knob to enter the desired time (HH:MM) and press the
ENT Key.
GPS Nav
10) Press the ENT Key again or use the large FMS Knob to move the cursor to
enter the next message.
Flight
Planning
Deleting a scheduler message:
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3)
Turn the large FMS Knob to highlight the name field of the scheduler
message to be deleted.
4)
Press the CLR Key to clear the message text. If the CLR Key is pressed
again, the message is restored.
5)
Press the ENT Key while the message line is cleared to clear the message
text.
PILOT PROFILES
Creating a profile:
1) Use the FMS Knob to select the AUX - System Setup Page.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
1) Select the AUX - Utility Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Appendix
3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box.
4)
Press the ENT Key. A ‘Create Profile’ window is displayed.
5) Use the FMS Knob to enter a profile name up to 16 characters long and
Index
press the ENT Key. Pilot profile names cannot begin with a blank as the
first letter.
78
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Additional Features
7)
Press the ENT Key.
EICAS
In the next field, use the small FMS Knob to select the desired settings
upon which to base the new profile. Profiles can be created based on
Garmin factory defaults, default profile settings (initially based on Garmin
factory defaults unless edited by the pilot), or current system settings.
Flight
Instruments
6)
Nav/Com/
XPDR/Audio
8) With ‘CREATE’ highlighted, press the ENT Key to create the profile
Or:
9)
To cancel the process, select ‘CANCEL’ with the large FMS Knob and press
the ENT Key.
GPS Nav
Selecting an active profile:
Flight
Planning
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
Procedures
3) Turn the large FMS Knob to highlight the active profile field in the Pilot
Profile Box.
4) Turn the small FMS Knob to display the pilot profile list and highlight the
Hazard
Avoidance
desired profile.
5) Press the ENT Key. The system loads and displays the system settings for
the selected profile.
Additional
Features
Renaming a profile:
Abnormal
Operation
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box.
Press the ENT Key.
5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to
6)
Appendix
rename.
Annun/
Alerts
4)
AFCS
Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the
ENT Key to activate the new profile.
Press the ENT Key.
7) Use the FMS Knob to enter a new profile name up to 16 characters long
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
and press the ENT Key.
79
Additional Features
Flight
Instruments
8) With ‘RENAME’ highlighted, press the ENT Key.
9)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
EICAS
Deleting a profile:
Nav/Com/
XPDR/Audio
1) Use the FMS Knob to select the AUX - System Setup Page.
2)
Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box.
AFCS
4)
Press the ENT Key.
5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to
GPS Nav
delete.
6)
Press the ENT Key.
Flight
Planning
7) With ‘DELETE’ highlighted, press the ENT Key.
8)
To cancel the process, use the large FMS Knob to select ‘CANCEL’ and
press the ENT Key.
Procedures
Importing a profile:
Hazard
Avoidance
1)
Insert the SD card containing the Pilot Profile into the top card slot on the
MFD.
2) Use the FMS Knob to select the AUX - System Setup Page.
Additional
Features
3)
Press the IMPORT softkey. If the correct Pilot Profile file is selected; with
‘IMPORT’ highlighted press the ENT Key.
Abnormal
Operation
Or:
If the SD card contains more than one Pilot Profile:
Annun/
Alerts
a) Turn the large FMS Knob to highlight the select file field in the Pilot
Profile Importing Box.
Appendix
b) Turn the small FMS Knob to display the pilot profile list and highlight
the desired profile to import and press the ENT Key.
c) With ‘IMPORT’ highlighted, press the ENT Key.
Index
4)
80
“Pilot profile import succeeded.” is shown in the import results box. Press
the ENT Key. The imported profile becomes the active Pilot Profile.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Additional Features
1)
2) Use the FMS Knob to select the AUX - System Setup Page.
4)
Press the EXPORT softkey.
5)
With ‘EXPORT’ highlighted press the ENT Key.
6)
“Pilot profile export succeeded.” is shown in the export results box. Press
the ENT Key to exit the Pilot Profile Exporting Box.
AFCS
Activate the desired Pilot Profile to export. Only the active Pilot Profile can
be exported.
Nav/Com/
XPDR/Audio
3)
EICAS
Insert the SD card for storing the Pilot Profile into the top card slot on the
MFD.
Flight
Instruments
Exporting a profile:
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
81
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Additional Features
Blank Page
82
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
NOTE: The Bell 505 Flight Manual (FM) always takes precedence over the
information found in this section.
EICAS
In the event of a loss of power to the PFD with the REV switch in NORM, the
switching logic is designed to automatically transfer the MFD into composite PFD/
EICAS mode.
In the event that the switching logic does not automatically provide a composite
PFD/EICAS mode on the MFD, or the pilot wishes to manually display composite PFD/
EICAS mode on either display, the REV switch may be manually positioned to PFD
or MFD. When the REV switch is positioned to MFD, the MFD REV Crew Alerting
System (CAS) message will display.
Flight
Planning
ABNORMAL COM OPERATION
Additional
Features
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Hazard
Avoidance
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Procedures
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field. In the event
of a failure of both the PFD and MFD, the emergency frequency (121.500 MHz)
automatically becomes the active frequency on the COM radio.
Abnormal
Operation
Annun/
Alerts
Appendix
Loss of Hazard Functions with Loss of GPS
Position
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
83
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight director
Command Bars
• Inset Map
• Temperatures
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Abnormal Operation
Abnormal
Operation
Extreme Pitch Indication
While in Enroute or Oceanic phase of flight, if the G1000H detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000H uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Index
Appendix
Annun/
Alerts
DEAD RECKONING
84
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Abnormal Operation
EICAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DR Mode is indicated on the G1000H by the appearance of the letters ‘DR’
superimposed in amber over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in amber, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. Also, the CDI deviation bar is removed from the display. Lastly, but at the same
time, a ‘GPS NAV LOST’ alert message appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000H in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000H through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
Flight
Instruments
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
(OCN) phase of flight. In all other phases, an invalid GPS solution produces
a “NO GPS POSITION” annunciation on the map and the G1000H stops
navigating in GPS Mode.
Annun/
Alerts
Appendix
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
Index
Dead Reckoning Indications
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
85
As a result of operating in DR Mode, all GPS-derived data is computed based upon
an estimated position and is displayed as amber text on the display to denote degraded
navigation source information. This data includes the following:
• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
Also, while the G1000H is in DR Mode, HTAWS is disabled. Additionally, the
accuracy of all nearest information (airports, airspaces, and waypoints) is questionable.
Finally, airspace alerts continue to function, but with degraded accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Abnormal Operation
86
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
System Annunciation
EICAS
G1000H SYSTEM ANNUNCIATIONS
When an LRU or an LRU function fails, a large red “X” is typically displayed on
windows associated with the failed data. Refer to the RFM for additional information
regarding pilot responses to these annunciations
Flight
Instruments
ANNUNCIATIONS & ALERTS
Comment
AFCS
Attitude and Heading Reference System is aligning.
GPS Nav
Flight
Planning
Procedures
Display system is not receiving attitude information from the
AHRS.
Hazard
Avoidance
Additional
Features
GPS information is either not present or is invalid for
navigation use.
Note that AHRS utilizes GPS inputs during normal operation.
AHRS operation may be degraded if GPS signals are not
present (see Bell 505 FM).
Abnormal
Operation
Display system is not receiving valid transponder information.
Appendix
Display system is not receiving heading information, but track
is available.
Annun/
Alerts
Display system is not receiving valid heading input from
AHRS.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
87
System Annunciation
Comment
CDI is not receiving valid data from the GIA. Does not apply
when the CDI is set to GPS.
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
GPS Nav
AFCS
Display system is not receiving airspeed input from air data
computer.
Procedures
Flight
Planning
Display system is not receiving altitude input from the air
data computer.
Additional
Features
Hazard
Avoidance
Display system is not receiving vertical speed input from the
air data computer.
A red ‘X’ through any other display field (such as engine
instrumentation display) indicates that the field is not
receiving valid data.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Other Various Red X
Indications
88
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Annunciation Text
BATTERY HOT
ECU FAIL
Flight
Instruments
WARNING MESSAGES
See the Bell 505 Flight Manual (FM) for recommended pilot actions.
Description
AFCS
GPS Nav
Flight
Planning
Procedures
XMSN OIL PRESS
XMSN OIL TEMP
Nav/Com/
XPDR/Audio
ENG OIL TEMP
ENG OIL PSI LO
ENGINE FIRE
ENGINE OUT
FUEL PRESS
ROTOR BRAKE
RPM
EICAS
Battery is overheating.
ECU has detected a critical malfunction and reverted to fixed fuel flow
(during start or In flight).
ECU has detected high engine oil temperature.
ECU has detected low engine oil pressure.
Fire detected in the engine compartment.
Ng less than 50%.
Fuel pressure is low.
Rotor brake pad(s) not fully retracted.
With low RPM audio - NR below 97% with power on or NR below
95% with power off.
Without audio - NR above 107% power on or NR above 111% with
power off.
Transmission oil pressure is below minimum.
Transmission oil temperature is at or above red line.
Hazard
Avoidance
CAUTION MESSAGES
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
190-02065-00 Rev. A
Battery is not connected to DC Bus.
XMSN upper or lower, F/W or T/R detector(s) inoperative.
Pilot and copilot throttle switches are in FLY position.
Malfunction has been detected in the engine controls system.
ECU alternator failed. The ECU is now powered by the DC BUS only.
Appendix
BATTERY OFF
DRIVE CD INOP
DUAL FLY
ECU DEGRADED
ECU PMA FAIL
Annun/
Alerts
BATTERY FAULT
Description
Baggage door is not securely latched.
Battery temperature below -5°C.
Battery has failed and battery power unavailable.
Battery has detected a fault and battery power is temporarily
unavailable.
Abnormal
Operation
Annunciation Text
BAGGAGE DOOR
BATTERY COLD
BATTERY FAIL
Additional
Features
See the Bell 505 Flight Manual (FM) for recommended pilot actions.
89
Annunciation Text
ENG CD INOP
ENGINE CHIP
ENG OIL PSI HI
EPSU FAIL
FIRE DET INOP
FOPS TST FAIL
FUEL FILTER
FUEL LOW
GEN
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
GEN OVERLOAD
Flight
Planning
HMU AUX CTRL
Procedures
IBF CLOGGED
ADVISORY MESSAGES
See the Bell 505 Flight Manual (FM) for recommended pilot actions.
Annunciation
Text
BATT HEATER ON
ECU DATA
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
MGT EXCEED
NG EXCEED
NP EXCEED
NP SENSOR FAIL
Q EXCEED
T/R CHIP
THROTTLE INOP
XMSN CHIP
Description
One or two engine chip detector(s) inoperative.
Ferrous particles detected in engine oil.
Engine oil pressure is above maximum.
Electrical power supply unit has failed.
Engine fire detector is inoperative.
FOPS test invalid.
Fuel filter partially blocked.
Fuel low condition (75 ±5 pounds) of fuel remaining in the tank.
Generator switch is off or the generator is not providing power to the
DC bus.
Current is more than 165 amps for at least 5 seconds.
The main metering valve is frozen and the auxiliary metering valve is
controlling fuel flow.
Inlet barrier filter partially blocked. Possible reduction in engine power
available.
MGT exceeded.
NG exceeded.
NP exceeded.
One NP sensor has failed.
Engine torque exceeded.
Ferrous particles detected in T/R gearbox oil.
Throttle switches idle command is inoperative.
Ferrous particles detected in transmission or freewheeling unit oil.
90
Description
Battery internal heater is active.
One or more ECU information channel(s) is unavailable to the Garmin
system.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
ENGINE CHIP 1
FOPS TST INPRG
Fuel pressure has dropped below the filter pre-clog threshold.
Pilot has selected MFD REV.
START
Start relay is in START mode.
XMSN CHIP 1
Annun/
Alerts
XMSN CHIP 2
Abnormal
Operation
XMSN CD 2 INOP
Additional
Features
XMSN CD 1 INOP
Appendix
Illuminates upon landing and indicates that the tail rotor chip detector
has failed.
Illuminates upon landing and indicates that the transmission chip detector 1 (mast bearing) has failed.
Illuminates upon landing and indicates that the transmission chip detector 2 (lower case) has failed.
Illuminates upon landing and indicates that the transmission chip detector 1 (mast bearing) is active.
Illuminates upon landing and indicates that the transmission chip detector 2 (lower case) is active.
Hazard
Avoidance
MFD REV
T/R CD INOP
Procedures
FUEL FILTER
Flight
Planning
F/W CHIP
GPS Nav
F/W CD INOP
AFCS
ENGINE CHIP 2
Illuminates upon landing and indicates which engine chip detector has
failed.
Illuminates upon landing and indicates which engine chip detector has
failed.
Illuminates upon landing and indicates which engine chip detector is
active.
Illuminates upon landing and indicates which engine chip detector is
active.
Illuminates upon landing and indicates that the freewheeling unit chip
detector has failed.
Illuminates upon landing and indicates that the freewheeling unit chip
detector is active.
ECU is performing flame out protection system test.
Nav/Com/
XPDR/Audio
ENG CD 2 INOP
ECU Level 1 failure detected.
EICAS
ENG CD 1 INOP
Description
Flight
Instruments
Annunciation
Text
ECU MAINT
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
91
STATUS ANNUNCIATION
Annunciation Text
BATT CHARGING
CHIP TEST OK
Description
Battery is charging.
EXT POWER
FIRE TEST OK
FOPS TST OK
OK TO SHUTDOWN
PITOT ON
WOG
Test of tail rotor gearbox, transmission upper and lower, and freewheel
chip detectors successful.
External power is connected.
Test of fire detection system successful.
Flame out protection system test successful.
Engine cool down completed.
Pitot Heater is on.
Weight on gear is active and the aircraft is on ground.
HTAWS ALERTS
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Voice Message
Reduced Required
Terrain Clearance
Warning (RTC)
“Warning; Terrain, Terrain”
Imminent Terrain
Impact Warning (ITI)
“Warning; Terrain, Terrain”
Reduced Required
Obstacle Clearance
Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle
Impact Warning (IOI)
“Warning; Obstacle,
Obstacle”
Reduced Required
Terrain Clearance
Caution (RTC)
“Caution; Terrain, Terrain”
Imminent Terrain
Impact Caution (ITI)
“Caution; Terrain, Terrain”
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Hazard
Avoidance
MFD
Pop-Up Alert
(except HTAWS
Page)
Additional
Features
Alert Type
PFD/HTAWS
Page Alert
Annunciation
92
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
MFD
Pop-Up Alert
(except HTAWS
Page)
Voice Message
Imminent Obstacle
Impact Caution (IOI)
“Caution; Obstacle,
Obstacle”
None
“Five Hundred”
“Four Fifty”
“Four Hundred”
“Three Fifty”
“Three Hundred”
“Two Fifty”,
“Two Hundred”
“One Fifty”
“One Hundred”
“Fifty”
AFCS
None
Nav/Com/
XPDR/Audio
“Caution; Obstacle,
Obstacle”
EICAS
Reduced Required
Obstacle Clearance
Caution (ROC)
Voice Callout (VCO)
Flight
Instruments
Alert Type
PFD/HTAWS
Page Alert
Annunciation
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
HTAWS SYSTEM STATUS ANNUNCIATIONS
PFD/HTAWS
Page Status
Annunciation
Voice
Message
HTAWS TEST
None
None
“HTAWS Test OK”
HTAWS FAIL
“HTAWS Failure”
HTAWS Not
Available
None
“HTAWS Not
Available”
HTAWS FLTA
Alerting Inhibited
None
None
None
“HTAWS
Available”*
System Test Pass
None
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
190-02065-00 Rev. A
None
Appendix
HTAWS Availability
Restored
Annun/
Alerts
HTAWS System
Failure
Abnormal
Operation
System Test in
Progress
Additional
Features
HTAWS Page Center
Banner Annunciation
Alert Type
93
Alert Type
PFD/HTAWS
Page Status
Annunciation
Reduced Protection
Mode Enabled
MFD Terrain or
Obstacle database
unavailable or
invalid. HTAWS
operating with PFD
Terrain or Obstacle
databases
Terrain or
Obstacle database
unavailable
or invalid on
all displays,
invalid software
configuration,
HTAWS audio fault
No GPS position
None
HTAWS Page Center
Banner Annunciation
Voice
Message
None
None
TERRAIN DATABASE FAILURE
HTAWS FAIL
NO GPS POSITION
Excessively degraded
GPS signal
None
None
“HTAWS Failure”
“HTAWS Not
Available”
“HTAWS Available”
when GPS position
returns. and HTAWS
is not inhibited.
“HTAWS Not
Available”
“HTAWS Available”
when sufficient GPS
signal is received.
and HTAWS is not
inhibited.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
94
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Flight
Instruments
PFD/HTAWS
Page Status
Annunciation
Alert Type
None
“HTAWS Not
Available”
“HTAWS Available”
when aircraft enters
database coverage
area and HTAWS is
not inhibted.
Out of database
coverage area
AFCS
* Aural message not issued if HTAWS is inhibited.
Data is not being received from the transponder*
Data is being received from the transponder, but a failure is detected in
the data stream*
Procedures
The transponder has failed*
Hazard
Avoidance
FAILED
UNAVAILABLE
Description
Flight
Planning
DATA FAILED
GPS Nav
TIS ALERTS AND ANNUNCIATIONS
Traffic Map Page
Annunciation
NO DATA
TIS is unavailable or out of range
* Contact a service center or Garmin dealer for corrective action
Additional
Features
TIS Failure Annunciations
Traffic Mode Annunciation
(Traffic Map Page)
TIS Operating
OPERATING
STANDBY
(also shown in white in center of page)
Appendix
TIS Failed*
Annun/
Alerts
TIS Standby
Traffic Display Enabled Icon
(Other Maps)
Abnormal
Operation
Mode
FAIL
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
TIS Modes
190-02065-00 Rev. A
Nav/Com/
XPDR/Audio
Voice
Message
EICAS
HTAWS Page Center
Banner Annunciation
95
Annunciations & Alerts
A Traffic Advisory is outside the selected display range*
Annunciation is removed when traffic comes within the selected
display range
TA X.X ± XX ↕
System cannot determine bearing of Traffic Advisory**
Annunciation indicates distance in nm, altitude separation in
hundreds of feet, and altitude trend arrow (climbing/descending)
AGE MM:SS
Appears if traffic data is not refreshed within 6 seconds
If after another 6 seconds data is not received, traffic is removed
from the display
The quality of displayed traffic information is reduced as the age
increases
TRFC COAST
The displayed data is not current (6 to 12 seconds since last
message)
The quality of displayed traffic information is reduced when this
message is displayed
TRFC RMVD
Traffic is removed because it is too old for coasting (12 to 60
seconds since last message)
Traffic may exist within the selected display range, but it is not
displayed
Traffic data has failed
Procedures
Flight
Planning
NO TRFC DATA
Traffic has not been detected
TRFC UNAVAIL
The traffic service is unavailable or out of range
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
TIS Traffic Status Annunciations
VOICE ALERTS
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
TRFC FAIL
Appendix
Voice Alert
“One hundred fifty”*
“ECU Fail”
“Engine Fire”
Index
Description
TA OFF SCALE
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Traffic Status Banner
Annunciation
Description
Altitude is at 150 feet.
ECU has detected a critical malfunction and reverted to fixed fuel
flow (during start or in flight).
Fire detected in the engine compartment.
“Engine Out”
NG less than 50%.
*For aircraft equipped with optional GRA 55 Radar Altimeter.
96
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
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Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed. The
system should be serviced.
Vertical guidance generated by SBAS is unavailable,
use LNAV only minimums.
The system notifies the pilot that the loaded
approach is not active. Activate approach when
required.
Procedures
The #1 AHRS is operating exclusively in no-GPS
mode. The system should be serviced.
Flight
Planning
APR DWNGRADE – Approach
downgraded.
APR INACTV – Approach is not
active.
The #1 AHRS and #2 AHRS magnetic model
database versions do not match.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should be
serviced when possible.
The #1 AHRS is not receiving any or any useful GPS
information. Check AFMS limitations. The system
should be serviced.
The #1 AHRS is not receiving backup GPS information.
The system should be serviced.
GPS Nav
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
GDC is reporting that the airspeed error correction
is unavailable.
A failure has been detected in the GDC1. The
system should be serviced.
AFCS
AHRS1 GPS – AHRS1 not receiving
any GPS information.
GDC is reporting that the altitude error correction
is unavailable.
Nav/Com/
XPDR/Audio
ADC1 ALT EC – ADC1 altitude error
correction is unavailable.
ADC1 AS EC – ADC1 airspeed error
correction is unavailable.
ADC1 SERVICE – GDC1 needs
service. Return unit for repair.
AHRS MAG DB – AHRS magnetic
model database version mismatch.
AHRS1 GPS – AHRS1 using backup
GPS source.
Abort approach due to loss of GPS navigation.
EICAS
navigation. Abort approach.
Flight
Instruments
G1000H SYSTEM MESSAGE ADVISORIES
Message
Comments
ABORT APR – Loss of GPS
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
97
Message
ARSPC AHEAD – Airspace ahead
less than 10 minutes.
Comments
Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the
aircraft position.
ahead.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft
position.
than 2 nm.
AUDIO MANIFEST - Audio
The audio panel has incorrect software installed.
software mismatch, communication
The system should be serviced.
halted.
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
COM1 PTT – COM1 push-to-talk
key is stuck.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 PTT – COM2 push-to-talk
key is stuck.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
98
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
The COM1 external push-to-talk switch is stuck in the
enable (or “pressed”) position. Press the PTT switch
again to cycle its operation. If the problem persists, the
system should be serviced.
The COM1 transfer switch is stuck in the enabled
(or “pressed”) position. Press the transfer switch
again to cycle its operation. If the problem persists,
the system should be serviced.
The system has detected a failure in COM1. COM1
may still be usable. The system should be serviced
when possible.
The system has detected an over temperature
condition in COM1. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
The COM2 external push-to-talk switch is stuck in the
enable (or “pressed”) position. Press the PTT switch
again to cycle its operation. If the problem persists, the
system should be serviced.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
Procedures
DB CHANGE – Database changed.
Verify user modified procedures.
Flight
Planning
DB CHANGE – Database changed.
Verify stored airways.
The pilot profile data was lost. System reverts to
default pilot profile and settings. The pilot may
reconfigure the MFD & PFD with preferred settings,
if desired.
This occurs when a stored flight plan contains
an airway that is no longer consistent with the
navigation database. This alert is issued only after
an navigation database update. Verify use of
airways in stored flight plans and reload airways as
needed.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures in
stored flight plans are correct and up to date.
The PFDs and MFD have different navigation
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
GPS Nav
DATA LOST – Pilot stored data was
lost. Recheck settings.
AFCS
CNFG MODULE – PFD1
configuration module is inoperative.
Nav/Com/
XPDR/Audio
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
EICAS
COM2 SERVICE – COM2 needs
service. Return unit for repair.
Comments
The COM2 transfer switch is stuck in the enabled
(or “pressed”) position. Press the transfer switch
again to cycle its operation. If the problem persists,
the system should be serviced.
The system has detected a failure in COM2. COM2
may still be usable. The system should be serviced
when possible.
The system has detected an over temperature
condition in COM2. The transmitter is operating at
reduced power. If the problem persists, the system
should be serviced.
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Flight
Instruments
Message
COM2 RMT XFR – COM2 remote
transfer key is stuck.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
99
Message
DB MISMATCH – Obstacle
database mismatch.
DB MISMATCH – Terrain database
mismatch.
DIG GMA1 MANIFEST – DIG
GMA 1 software mismatch,
communication halted.
FAILED PATH – A data path has
failed.
FPL TRUNC – Flight plan has been
truncated.
FPL WPT LOCK – Flight plan
waypoint is locked.
FPL WPT MOVE – Flight plan
waypoint moved.
Comments
The PFDs and MFD have different obstacle
database installed. Install correct obstacle
database in all displays.
The PFDs and MFD have different terrain database
versions or types installed. Install correct terrain
database version or type in all displays.
The digital audio controller has incorrect software
installed. The system should be serviced.
A data path connected to the GDU, GSD 41, or the
GIA 63W has failed.
This occurs when a newly installed navigation
database eliminates an obsolete approach or arrival
used by a stored flight plan. The obsolete procedure
is removed from the flight plan. Update flight plan
with current arrival or approach.
Upon power-up, the system detects that a stored
flight plan waypoint is locked. This occurs when an
navigation database update eliminates an obsolete
waypoint. The flight plan cannot find the specified
waypoint and flags this message. This can also
occur with user waypoints in a flight plan that is
deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database,
Or
update the waypoint name/identifier to reflect the
new information.
The system has detected that a waypoint
coordinate has changed due to a new navigation
database update. Verify that stored flight plans
contain correct waypoint locations.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
100
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
101
Nav/Com/
XPDR/Audio
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
EICAS
190-02065-00 Rev. A
Flight
Instruments
Message
Comments
GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
South, no magnetic compass.
invalid.
The GIA1 temperature is too low to operate
GIA1 COOLING – GIA1
correctly. Allow units to warm up to operating
temperature too low.
temperature.
The GIA1 temperature is too high. If problem
GIA1 COOLING – GIA1 over
persists, the system should be serviced.
temperature.
GIA1 CONFIG – GIA1 audio config The GIA1 have an error in the audio configuration.
The system should be serviced.
error. Config service req’d.
GIA1 CONFIG – GIA1 config error. The GIA1 configuration settings do not match
backup configuration memory. The system should
Config service req’d.
be serviced.
GIA1 MANIFEST – GIA1 software The GIA1 has incorrect software installed. The
system should be serviced.
mismatch, communication halted.
The GIA1 self-test has detected a problem in the
GIA1 SERVICE – GIA1 needs
unit. The system should be serviced.
service. Return the unit for repair.
The GIA2 temperature is too low to operate
GIA2 COOLING – GIA2
correctly. Allow units to warm up to operating
temperature too low.
temperature.
The GIA2 temperature is too high. If problem
GIA2 COOLING – GIA2 over
persists, the system should be serviced.
temperature.
GIA2 CONFIG – GIA2 audio config The GIA2 have an error in the audio configuration.
The system should be serviced.
error. Config service req’d.
GIA2 CONFIG – GIA2 config error. The GIA2 configuration settings do not match
backup configuration memory. The system should
Config service req’d.
be serviced.
GIA2 MANIFEST – GIA2 software The GIA2 has incorrect software installed. The
system should be serviced.
mismatch, communication halted.
The GIA2 self-test has detected a problem in the
GIA2 SERVICE – GIA2 needs
unit. The system should be serviced.
service. Return the unit for repair.
GMA1 AUX MANIFEST – GMA1
The audio panel has incorrect aux software installed.
AUX software mismatch, communicaThe system should be serviced.
tion halted.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Message
GMA1 CONFIG – GMA1 config
error. Config service req’d.
Comments
The audio panel configuration settings do not
match backup configuration memory. The system
should be serviced.
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The system should
be serviced.
GMA1 MANIFEST – GMA1 software The audio panel has incorrect software installed. The
system should be serviced.
mismatch, communication halted.
The audio panel self-test has detected a problem
GMA1 SERVICE – GMA1 needs
in the unit. Certain audio functions may still be
service. Return unit for repair.
available, and the audio panel may still be usable.
The system should be serviced when possible.
GMA XTALK – GMA crosstalk error An error has occurred in transferring data between
the two GMAs. The system should be serviced.
has occurred.
GMU1 MANIFEST – GMU1
The GMU 44 has incorrect software installed. The
software mismatch, communication
system should be serviced.
halted.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to insufficient satellites.
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
A failure has been detected in the GPS1 receiver.
GPS1 SERVICE – GPS1 needs
The receiver may still be available. The system
service. Return unit for repair.
should be serviced.
GRA1 has improper calibration. The system should
GRA1 CAL – GRA1 calibration.
be serviced.
Service req’d.
GRA1 CONFIG – GRA1 config error. The GRA and GDU have incompatible
configurations.
Config service req’d.
GRA1 MANIFEST – GRA1 software The GRA has incorrect software installed. The
system should be serviced.
mismatch, communication halted.
The GRA self-test has detected a problem in the
GRA1 SERVICE – GRA1 needs
unit. The system should be serviced.
service. Return unit for repair
102
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan. Update
flight plan with current waypoint.
Flight
Planning
LOCKED FPL – Cannot navigate
locked flight plan.
GPS Nav
The aircraft is inside the airspace.
Data link avionics were not configured correctly
and therefore will not be able to communicate
with the ground network.
AFCS
INSIDE ARSPC – Inside airspace.
INVALID ADM – Invalid ADM: ATN
communication halted.
Nav/Com/
XPDR/Audio
HDG FAULT – AHRS1 magnetometer A fault has occurred in the #1 GMU 44. Heading is
flagged as invalid. The AHRS uses GPS for backup
fault has occurred.
mode operation. The system should be serviced.
The magnetometer has detected a magnetic
HDG PRESET MODE – Magnetic
anomoly detected. HPM is available. anomoly that could affect heading indications.
Heading Preset Mode may be used.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
A GIA mismatch has been detected, where only
one is SBAS capable.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
EICAS
GTS MANIFEST – GTS software
mismatch, communication halted.
Comments
The system has detected an over temperature
condition in GRA1.
The GTS and GDU have incompatible
configurations. This alert is also set when the GTS
has an invalid mode S addres sconfigured or the
mode S address does not match both XPDR mode
S addresses.
The GTS 800 has incorrect software installed. The
G1000H system should be serviced.
Flight
Instruments
Message
GRA1 TEMP – GRA1 over
temperature.
GTS CONFIG – GTS config error.
Config service req’d.
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
103
Message
LOI – GPS integrity lost. Crosscheck
with other NAVS.
LRG MAG VAR – Verify all course
angles.
Comments
GPS integrity is insufficient for the current phase
of flight.
The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
near the magnetic poles. Displayed magnetic
course angles may differ from the actual magnetic
heading by more than 2°.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
The MFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The MFD detected a failure in the Airport Directory
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists, the
system should be serviced.
The MFD detected a failure in the basemap
database.
The MFD detected a failure in the ChartView
database (optional feature). Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure that the data
card is properly inserted. Replace data card. If
problem persists, the system should be serviced.
The MFD detected a failure in the obstacle
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
MFD1 CONFIG – MFD1 config
error. Config service req’d.
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
MFD1 DB ERR – MFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
104
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
105
GPS Nav
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
AFCS
190-02065-00 Rev. A
The remote NAV1 transfer switch is stuck in the
enabled (or “pressed”) state. Press the transfer
switch again to cycle its operation. If the problem
persists, the system should be serviced.
Nav/Com/
XPDR/Audio
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
EICAS
Comments
The MFD detected a failure in the obstacle
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
The obstacle database is present on another LRU,
MFD1 DB ERR – MFD1 obstacle
but is missing on the specified LRU.
database missing
MFD1 DB ERR – MFD1 navigation The MFD detected a failure in the navigation
database. Attempt to reload the navigation
database error exists.
database. If problem persists, the system should
be serviced.
The MFD adetected a failure in the Safe Taxi
MFD1 DB ERR – MFD1 Safe Taxi
database. Ensure that the data card is properly
database error exists.
inserted. Replace data card. If problem persists,
the system should be serviced.
The terrain database is present on another LRU,
MFD1 DB ERR – MFD1 terrain
but is missing on the specified LRU.
database error exists.
MFD1 KEYSTK – MFD [key name] A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
Key is stuck.
several times. The system should be serviced if the
problem persists.
MFD1 MANIFEST – MFD1 software The MFD has incorrect software installed. The
system should be serviced.
mismatch, communication halted.
The MFD self-test has detected a problem. The
MFD1 SERVICE – MFD1 needs
system should be serviced.
service. Return unit for repair.
The MFD voltage is low. The system should be
MFD1 VOLTAGE – MFD1 has low
serviced.
voltage. Reducing power usage
System has updated the active navigation database
NAV DB UPDATED – Active
from the standby navigation database.
navigation database updated.
Flight
Instruments
Message
MFD1 DB ERR – MFD1 obstacle
database error exists.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Message
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
Comments
A failure has been detected in the NAV1 receiver.
The receiver may still be available. The system
should be serviced.
The remote NAV2 transfer switch is stuck in the
NAV2 RMT XFR – NAV2 remote
enabled (or “pressed”) state. Press the transfer
transfer key is stuck.
switch again to cycle its operation. If the problem
persists, the system should be serviced.
A failure has been detected in the NAV2 receiver.
NAV2 SERVICE – NAV2 needs
The receiver may still be available. The system
service. Return unit for repair.
should be serviced.
The position of the selected waypoint [xxxx] is not
NO WGS84 WPT – Non WGS 84
calculated based on the WGS84 map reference
waypoint for navigation -[xxxx]
datum and may be positioned in error as displayed.
Do not use GPS to navigate to the selected nonWGS84 waypoint.
NON-MAG UNITS– Non-magnetic Navigation angle is not set to MAGNETIC at
power-up.
NAV ANGLE display units are
active.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
PFD1 CONFIG – PFD1 config error.
Config service req’d.
PFD1 DB ERR – PFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
106
The PFD is overheating and is reducing power
consumption by dimming the display. If problem
persists, the system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The PFD detected a failure in the basemap
database.
The PFD detected a failure in the navigation
database. Attempt to reload the navigation
database. If problem persists, the system should
be serviced.
The PFD detected a failure in the obstacle
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Procedures
190-02065-00 Rev. A
Bad parallel track geometry.
Flight
Planning
[PFD1 or MFD1] CARD 1 ERR –
Card 1 is invalid.
[PFD1 or MFD1] CARD 2 ERR –
Card 2 is invalid.
PFD1 MANIFEST – PFD1 software
mismatch, communication halted.
PFD1 SERVICE – PFD1 needs
service. Return unit for repair.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
PTK FAIL – Parallel track
unavailable: bad geometry.
GPS Nav
[PFD1 or MFD1] CARD 2 REM –
Card 2 was removed. Reinsert card.
AFCS
[PFD1 or MFD1] CARD 1 REM –
Card 1 was removed. Reinsert card.
Nav/Com/
XPDR/Audio
PFD1 DB ERR – PFD1 terrain
database missing.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
EICAS
PFD1 DB ERR – PFD1 terrain
database error exists.
Comments
The obstacle database is present on another LRU,
but is missing on the specified LRU.
The PFD detected a failure in the Safe Taxi
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists,
the system should be serviced
The PFD detected a failure in the terrain database.
Ensure that the terrain card is properly inserted in
display. Replace terrain card. If problem persists,
the system should be serviced.
The terrain database is present on another LRU,
but is missing on the specified LRU.
A key is stuck on the PFD bezel. Attempt to free
the stuck key by pressing it several times. The
system should be serviced if the problem persists.
The SD card was removed from the top card slot of
the specified PFD or MFD. The SD card needs to be
reinserted.
The SD card was removed from the bottom card
slot of the specified PFD or MFD. The SD card
needs to be reinserted.
The SD card in the top card slot of the specified
PFD or MFD contains invalid data.
The SD card in the bottom card slot of the specified
PFD or MFD contains invalid data.
The PFD has incorrect software installed. The
system should be serviced.
The PFD self-test has detected a problem. The
system should be serviced.
The PFD1 voltage is low. The system should be
serviced.
Flight
Instruments
Message
PFD1 DB ERR – PFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
107
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Message
PTK FAIL – Parallel track
unavailable: invalid leg type.
PTK FAIL – Parallel track
unavailable: past IAF.
Comments
SCHEDULER [#] – <message>.
SLCT FREQ – Select appropriate
frequency for approach.
Message criteria entered by the user.
The system notifies the pilot to load the approach
frequency for the appropriate NAV receiver. Select
the correct frequency for the approach.
The Navigation angle is non-magnetic. Select the
MAGNETIC NAV ANGLE display units.
The system notifies the pilot to set the CDI to the
correct NAV receiver. Set the CDI to the correct
NAV receiver.
The Navigation angle is magnetic. Select the
alternate NAV ANGLE display units.
A steep turn is 15 seconds ahead. Prepare to turn.
SLCT MAG – Select MAGNETIC
NAV ANGLE display units.
SLCT NAV – Select NAV on CDI for
approach.
SLCT NON-MAG – Select alternate
NAV ANGLE display units.
STEEP TURN – Steep turn ahead.
STRMSCP FAIL – Stormscope has
failed.
SVS – SVS DISABLED: Out of
available terrain region.
SVS – SVS DISABLED: Terrain DB
resolution too low.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
TERRAIN DSP – [PFD1 or
MFD1] Terrain awareness display
unavailable.
TIMER EXPIRD – Timer has expired.
108
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been passed.
Stormscope has failed. The system should be
serviced.
Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (4.9 arc-second or
better) is not currently installed.
The MFD and PFD have different software versions
installed. The system should be service..
One of the terrain or obstacle databases required
for HTAWS in the specified PFD or MFD is missing
or invalid.
The system notifies the pilot that the timer has
expired.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
UNABLE V WPT – Can’t reach
current vertical waypoint.
The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
speed constraints. The system automatically
transitions to the next vertical waypoint.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
VNV – Unavailable. Unsupported
leg type in flight plan.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
EICAS
Comments
The system is no longer receiving data from the
traffic system. The traffic device should be serviced.
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
The current crosstrack exceeds the limit, causing
vertical deviation to go invalid.
Flight
Planning
A parallel course has been selected, causing the
vertical deviation to go invalid.
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
Procedures
Annun/
Alerts
Appendix
Index
109
Abnormal
Operation
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Additional
Features
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
ADS-B is inoperative. Other transponder functions
may be available. Transponder should be serviced
when possible.
The transponder configuration settings do not
XPDR1 CONFIG – XPDR1 config
match those of backup configuration memory. The
error. Config service req’d.
system should be serviced.
XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1
transponder.
The #1 transponder should be serviced when
XPDR1 SRVC – XPDR1 needs
possible.
service. Return unit for repair.
The MFD and PFDs are not communicating with
XTALK ERROR – A flight display
each other. The system should be serviced.
crosstalk error has occurred.
Hazard
Avoidance
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
XPDR1 ADS-B FAIL – XPDR1
unable to transmit ADS-B messages.
190-02065-00 Rev. A
Flight
Instruments
Message
TRAFFIC FAIL – Traffic device has
failed.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export
Results
EICAS
Flight
Instruments
Annunciations & Alerts
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully imported from the SD
card.
‘Flight plan partially imported.’
Some flight plan waypoints were successfully imported
from the SD card, however others had errors and were not
imported. A partial stored flight plan now exists in the
system.
‘File contained user waypoints only.’
The file stored on the SD card did not contain a flight plan,
only user waypoints. One or more of these waypoints did not
import successfully.
Hazard
Avoidance
‘Some waypoints not loaded. Waypoints
locked.’
The flight plan on the SD card contains one or more
waypoints that the system cannot find in the navigation
database. The flight plan has been imported, but must be
edited within the system before it can be activated for use.
‘User waypoint database full. Not all
loaded.’
The flight plan file on the SD card contains user waypoints.
The quantity of stored user waypoints has exceeded system
capacity, therefore not all the user waypoints on the SD
card have been imported. Any flight plan user waypoints
that were not imported are locked in the flight plan. The
flight plan must be edited within the system before it can be
activated for use.
‘One or more user waypoints renamed.’
One or more imported user waypoints were renamed when
imported due to naming conflicts with waypoints already
existing in the system.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
‘Too many points. Flight plan truncated.’ The flight plan on the SD card contains more waypoints than
the system can support. The flight plan was imported with as
many waypoints as possible.
Additional
Features
Procedures
A flight plan file stored on the SD card was successfully
imported as a stored flight plan.
‘File contained user waypoints only. User The file stored on the SD card did not contain a flight plan,
waypoints imported successfully. No
only user waypoints. These waypoints have been saved to the
stored flight plan data was modified.’
system user waypoints. No flight plans stored in the system
have been modified.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
‘Flight plan successfully imported.’
Description
110
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Annunciations & Alerts
Description
Flight
Instruments
Flight Plan Import/Export
Results
‘Flight plan export failed.’
The stored flight plan was not successfully exported to the SD
card. The SD card may not have sufficient available memory
or the card may have been removed prematurely.
PILOT PROFILE IMPORT/EXPORT MESSAGES
Description
AFCS
Pilot Profile Import/Export Results
Nav/Com/
XPDR/Audio
The stored flight plan was successfully exported to the SD
card.
EICAS
‘Flight plan successfully exported.’
Displayed if the SD card does not have one or
more valid pilot profile filenames.
‘Overwrite existing profile?’
Displayed if the profile name matches the name
of existing profile.
‘Profile name invalid. Enter a different profile
name.’
Displayed if the profile name is invalid.
‘All available pilot profiles in use. Delete a
profile before importing another.’
Displayed if the maximum number for pilot
profiles has been reached.
‘Pilot profile import failed.’
Displayed if the importing operation fails for any
other reason.
‘Pilot profile import succeeded.’
Displayed if the importing operation succeeds.
‘Overwrite existing file?’
Displayed if the filename matches the name of an
existing file on the SD card.
‘Pilot profile export failed.’
Displayed if the export operation fails.
‘Pilot profile export succeeded.’
Displayed if the export operation succeeds.
GPS Nav
‘No pilot profile plan files found to import.’
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
111
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Annunciations & Alerts
Blank page
112
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
Nav/Com/
XPDR/Audio
CAS ↑
MSG
EICAS
SENSOR
CAS
CAS ↓
AFCS
Top Level PFD Softkeys
SENSOR
MSG
MSG
Press the BACK Softkey to return to
the top-level softkeys.
TRFC-2
Hazard
Avoidance
Inset Map Softkeys
SENSOR
Additional
Features
CAS
Procedures
TRFC-1
Flight
Planning
TERRAIN
GPS Nav
CAS
MSG
(If Available)
MSG
Abnormal
Operation
SET HDG
Press the BACK Softkey to return to
the top-level softkeys.
HDG -
HDG +
HPM OFF
Annun/
Alerts
HDG SYNC
MSG
Appendix
Sensor Softkeys
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
113
Level 1
Level 2
Level 3
CAS ↓
INSET
OFF
Removes Inset Map
DCLTR (3)
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features
visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the
active flight plan
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in
the inset map window
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
CAS ↑
Additional
Features
TERRAIN
Annun/
Alerts
TOPO
Abnormal
Operation
Hazard
Avoidance
TRAFFIC
Displays/removes terrain information on
Inset Map
Displays the Set Heading Softkey
SENSOR
(If Available) Enables Heading Preset Mode
Index
Appendix
SET HDG
114
Description
Displays the scroll-up and scroll-down
softkeys when the number of CAS messages
exceeds the maximum capable of being
displayed in the window
Moves the cursor up through the displayed
messages
Moves the cursor down through the
displayed messages
Displays Inset Map in PFD lower left corner
CAS
EICAS
Flight
Instruments
Appendix
HDG
SYNC
Synchronizes heading to the selected
heading
HDG -
Slews heading counterclockwise
HDG +
Slews heading clockwise
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
Level 2
Level 3
Description
Flight
Instruments
Level 1
Manually disables Heading Preset Mode
HPM
OFF
EICAS
SENSOR
MSG
HSI FRMT
SYN VIS
MSG
ALT UNIT
BRG1(GPS)
BRG2(ADF)
BRG1(ADF)
BRG2(OFF)
Press the BACK Softkey to
return to the top-level softkeys
GPS Nav
BRG2(GPS)
AFCS
BRG1(NAV1)
Nav/Com/
XPDR/Audio
CAS
BRG1(OFF)
HPA
ARC HSI
MSG
Procedures
360 HSI
IN
Flight
Planning
METERS
MSG
MSG
SYN TERR HRZN HDG APTSIGNS
Hazard
Avoidance
PATHWAY
MSG
Additional
Features
PFD Configuration Softkeys
Level 2
PFD
Description
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Annun/
Alerts
SYN VIS
Level 3
Abnormal
Operation
Level 1
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
115
Level 1
Level 2
EICAS
Flight
Instruments
Appendix
Level 3
Description
PATHWAY
Displays rectangular boxes representing
the horizontal and vertical flight path of
the active flight plan
Enables synthetic terrain depiction
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
SYN TERR
Flight
Planning
DFLTS
Additional
Features
Hazard
Avoidance
Procedures
WIND
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings,
including changing units to standard
Displays softkeys to select wind data
parameters
Headwind/tailwind and crosswind
OPTN 1
arrows with numeric speed components
Wind direction arrow and numeric
OPTN 2
speed
Wind direction arrow with numeric
OPTN 3
direction and speed
Information not displayed
OFF
Abnormal
Operation
BRG1
Annun/
Alerts
HSI FRMT
Appendix
360 HSI
ARC HSI
Index
BRG2
116
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
Level 2
Level 3
Description
Displays softkeys for setting the altimeter
and BARO settings to metric units
ALT UNIT
Press to display the BARO setting as
inches of mercury
HPA
Press to display the BARO setting as
hectopacals
SENSOR
CAS
MSG
MSG
Transponder Softkeys
Level 2
XPDR
Displays transponder mode selection
softkeys
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Appendix
ON
Description
Annun/
Alerts
STBY
Level 3
Abnormal
Operation
Level 1
Additional
Features
Press the BACK Softkey to return
to the previous level softkeys.
Hazard
Avoidance
MSG
Procedures
Press the BACK Softkey to return
to the top-level softkeys.
Flight
Planning
ADS-B TX
GPS Nav
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
STD BARO
AFCS
IN
Nav/Com/
XPDR/Audio
When enabled, displays altimeter in
meters
EICAS
METERS
Flight
Instruments
Level 1
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
117
Level 1
Level 2
Level 3
ALT
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
VFR
CODE
Procedures
0—7
Hazard
Avoidance
IDENT
BKSP
Airborne - (Green mode indication)
Generates Mode A, Mode C, and Mode
S replies as well as transmissions of
acquisition and extended squitters,
including ADS-B out.
Automatically enters the VFR code (1200 in
the U.S.A. only)
Displays transponder code selection
softkeys 0-7
Use numbers to enter code
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Removes numbers entered, one at a time
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Enables the transmission of extended
squitters containing ADS-B out information
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
MSG
Displays Messages Window
Additional
Features
IDENT
Abnormal
Operation
ADS-B TX
Annun/
Alerts
IDENT
Index
Appendix
Description
On Ground - (White mode indication)
Generates Mode S replies to discrete
interrogations as well as transmission
of acquisition and extended squitters,
including ADS-B out. Mode A, Mode C,
and Mode S all-call replies are inhibited
EICAS
Flight
Instruments
Appendix
118
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
DCLTR
MAP
(optional)
(optional)
SHW CHRT
CHKLIST
Flight
Instruments
MFD SOFTKEY MAP
EICAS
DCLTR-1
CAS ↑
CAS ↓
PWR CHK
TEST
DCLTR-2
Nav/Com/
XPDR/Audio
DCLTR-3
AUD TST
CHIP TST
FIRE TST
ACU TST
FOPS TST
BACK
AFCS
Press the BACK Softkey on
this level to return to the previous
softkey level.
PROFILE
TOPO
TERRAIN
AIRWAYS
BACK
GPS Nav
TRAFFIC
AIRWY ON
Flight
Planning
AIRWY LO
AIRWAY HI
Level 1
Level 2
Level 3
Description
CAS ↑
TEST
Displays additional test options for
engine systems
FIRE TST
Fire Detection System Test
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index
CHIP TST
Audio Alert Test Displays
Chip Detector Test
AUD TST
Appendix
Performs a power assurance check
Annun/
Alerts
PWR CHK
Abnormal
Operation
CAS ↓
Additional
Features
Scroll up (Displayed only when
a sufficient number of items are
displayed in the Crew Alerting System
Display to warrant scrolling)
Scroll down (Displayed only when
a sufficient number of items are
displayed in the Crew Alerting System
Display to warrant scrolling)
Hazard
Avoidance
Displays the EIS-Engine Page
ENGINE
190-02065-00 Rev. A
Procedures
MFD Softkeys
119
Level 1
Level 2
Nav/Com/
XPDR/Audio
MAP
AFCS
TRAFFIC
GPS Nav
PROFILE
Flight
Planning
TOPO
Procedures
TERRAIN
Additional
Features
Hazard
Avoidance
AIRWAYS
BACK
DCLTR
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Level 3
Description
ACU TST Auxiliary Control Unit
EICAS
Flight
Instruments
Appendix
120
FOPS TST
Flame Out Protection System Test
BACK
Press BACK, to return to the previous
page
Enables second-level Navigation Map
softkeys
Displays traffic information on
Navigation Map
Displays/removes Profile View on
Navigation Map Page
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Navigation Map
Displays terrain information on Navigation Map
Displays airways on the map; cycles
through the following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are
displayed
AIRWY LO: Only low altitude
airways are displayed
AIRWY HI: Only high altitude
airways are displayed
Returns to top-level softkeys
Selects desired amount of map detail;
cycles through declutter levels:
DCLTR (No Declutter): All map
features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA
data
DCLTR-3: Removes everything
except the active flight plan
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
Level 2
Level 3
Description
CHKLIST
Nav/Com/
XPDR/Audio
LOADING UPDATED DATABASES
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
121
Hazard
Avoidance
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Procedures
Error Message
Description
Canceled
Database synchronization has been canceled by removing the bottom
SD card in display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization
process to be halted
Timeout
System timed-out prior to the database transfer completing
Flight
Planning
In some cases it may be necessary to obtain an unlock code from Garmin in order
to make the database product functional. It may also be necessary to have the system
configured by a Garmin authorized service facility in order to use some database features.
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error
message is displayed, the problem must be corrected before synchronization can be
completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
GPS Nav
NOTE: Garmin requests that the flight crew report any observed discrepancies
related to database information. These discrepancies could come in the form
of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or
any other displayed item used for navigation or communication in the air or
on the ground. Go to FlyGarmin.com and select “Aviation Data Error Report.
AFCS
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in maintenance being required to reboot the system.
190-02065-00 Rev. A
EICAS
When available, displays optional
airport and terminal procedure charts
When available, displays optional
checklists
SHW CHRT
Flight
Instruments
Level 1
Updating the active navigation database (not using the Dual
Navigation Database or Automatic Database Synchronization
Features):
Go to www.flygarmin.com or www.jeppesen.com. Download the
applicable software and install the navigation database on a blank
SD card.
2) With the system OFF, insert the SD card containing the new navigation database
version into the top card slot of the display (label of SD card facing left).
1)
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
Turn the system ON. A prompt similar to the following is displayed in the
upper left corner of the display:
4)
5)
Press the NO Softkey to proceed to loading only the active database.
A prompt similar to the following is displayed, press the YES Softkey to
update the active navigation database.
After the update completes, the display starts in normal mode. Do not
remove power while the display is starting.
Hazard
Avoidance
Procedures
Flight
Planning
6)
7)
Turn the system OFF and remove the SD card from the top card slot.
8)
Repeat steps 2 through 7 for the other display. Remove the SD card when
finished.
9)
Apply power to the system and press the ENT Key or the right-most softkey on
the MFD to acknowledge the startup screen.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Additional
Features
11) Turn the small FMS Knob to select the System Status Page.
12) Press the Display Database Selection Softkey to show active navigation
database information for each display.
13) Verify the correct navigation database cycle information is shown for each
display.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
3)
Dual Navigation Database Feature
The dual navigation database feature allows each display to store an upcoming
navigation database on the bottom SD card so that the system can automatically
load it to replace the active database when the new database becomes effective
(the next cycle becomes available seven days prior to its effective date).
The system checks the active and standby databases upon (on-ground only) powerup. If the standby database is current and the active database is out of date, the display
will upload the standby database into the active internal database location. Loading
122
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
With the system OFF, insert the SD card containing the new navigation
database version into the top card slot of the display.
3)
Verify that an SD card is inserted in the bottom slot of each display.
4)
Turn the system ON. A prompt similar to the following is displayed.
5)
Press the YES softkey. The navigation database is copied to the SD card in
the bottom of the display.
6)
After the navigation database files are copied to the bottom SD card.
7)
8)
9)
As instructed on the display, press any key to continue. .
Press any key to continue.
Press the NO Softkey. The display now starts in normal mode. Since the
database effective date is not yet valid, it should not be loaded as the
active database. The display now starts in normal mode. Do not remove
power while the display is starting.
Flight
Planning
2)
GPS Nav
Go to www.flygarmin.com or www.jeppesen.com. Download the
applicable software and install the navigation database on a blank
SD card.
AFCS
1)
Nav/Com/
XPDR/Audio
NOTE: To do this procedure, use a blank SD card to copy the navigation
database. Garmin SD Cards (bottom SD card slots) must NOT be used. The
use of SanDisk SD Card is recommended to update the navigation database
file. Before utilization, it is recommended to format the SD Card with the
FAT32 file system so that displays will read it.
EICAS
Loading a standby navigation database:
Flight
Instruments
the standby database to the active location takes approximately 45-55 seconds. During
the loading process ‘Please Wait. Navigation Database Update in Progress. Do Not
Remove Power from Displays’ will be displayed on screen. After startup is complete,
the pilot is alerted that the update is complete by a system alert message, ‘NAV DB
UPDATED’.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
10) Turn the system OFF and remove the SD card from the top card slot.
Appendix
11) Repeat steps 2 through 10 for the other display.
12) Apply power to the system and press the ENT Key on the MFD display to
acknowledge the startup screen.
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
123
Appendix
Flight
Instruments
13) Turn the large FMS Knob to select the AUX Page group on the MFD.
14) Turn the small FMS Knob to select the System Status Page.
Nav/Com/
XPDR/Audio
EICAS
15) Press the Display Database Selection Softkey to show standby navigation
database information for each display.
16) Verify the correct standby navigation database cycle information is shown
for each display.
AFCS
NOTE: Make sure that no messages related to database errors are displayed
in the Messages window of the PFD.
17) Press the MSG Softkey and determine if any message related to databases is active.
Updating Basemap, SafeTaxi, Obstacle, Airport Directory
Flight
Planning
GPS Nav
18) Remove power from the system.
Procedures
NOTE: The Basemap, SafeTaxi, Obstacle and Airport Directory databases may
be copied to one Supplemental Data Card, then automatically synchronized
to the other card(s) in the system.
With the system OFF, remove the Garmin SD Card from the bottom SD card
slot of the MFD.
2) Go to www.flygarmin.com. Download the applicable software and
install the databases on the Garmin SD card for the MFD.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
1)
3)
Put the Garmin SD Card back in the bottom SD card slot of the MFD.
4)
Turn the system ON.
5)
During MFD power-up, check the MFD Power-Up screen and make sure that
the database is initialized and shown on the database information.
6)
Press the ENT Key on MFD display to acknowledge the startup screen.
7)
Turn the large FMS Knob to select the AUX Page group on the MFD.
8)
Turn the small FMS Knob to select the System Status Page.
9)
Press the Display Database Selection Softkey to show database information
for each display.
10) Verify the correct database cycle information is shown for each display.
Index
11) Press the MSG Softkey and determine if any message related to databases is active.
12) Remove power from the system.
124
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Appendix
1)
NOTE: Label the SD cards for each display.
Go to www.flygarmin.com or www.jeppesen.com (for ChartView
only). Download the applicable software and install the databases
on the Garmin SD card for each display. (The FliteCharts or ChartView
AFCS
2)
Nav/Com/
XPDR/Audio
With the system OFF, remove the Garmin SD Cards from the bottom SD card
slot of each flight display unit.
EICAS
NOTE: Jeppesen ChartView can be updated at either www.flygarmin.com
or www.jeppesen.com, but must be purchased first from Jeppesen.
Flight
Instruments
Updating Terrain, Chartview and Flitecharts Databases
GPS Nav
database must only be installed on the MFD SD Card).
Put the Garmin SD Cards back in the bottom SD card slots of each flight
display unit.
4)
Turn the system ON.
5)
During MFD power-up, check the MFD Power-Up screen and make sure that
the database is initialized and shown on the database information.
6)
Press the ENT Key on MFD display to acknowledge the startup screen.
7)
Turn the large FMS Knob to select the AUX Page group on the MFD.
8)
Turn the small FMS Knob to select the System Status Page.
9)
Press the Display Database Selection Softkey to show database information
for each display.
Flight
Planning
3)
Procedures
Hazard
Avoidance
12) Remove power from the system.
Abnormal
Operation
11) Press the MSG Softkey and determine if any message related to databases is active.
Additional
Features
10) Verify the correct database cycle information is shown for each display.
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
125
Magnetic Field Variation Database Update
At startup, the system compares this version of the MV DB with that presently being
used by the AHRS (GRS). If the system determines the MV DB needs to be updated,
a prompt is displayed on the Navigation Map Page, as shown in the following figure.
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Appendix
GPS Nav
GRS Magnetic Field Variation Database Update Prompt
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Loading the magnetic field variation database update:
With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key
on the MFD. A progress monitor is displayed as shown in the following
figure.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Uploading Database to GRS
126
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Index
A
Additional
Features
G
H
Index
Index-1
Appendix
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Annun/
Alerts
Hazard Displays 65
Heading Preset Mode 2, 103, 114, 115
Helicopter Terrain Awareness & Warning
System (HTAWS) 68
Hook weight 42
Horizon heading 73
Horizon Headings 74
HSI double green arrow 15
HSI Format 4
Abnormal
Operation
CDI 1, 108
ChartView 74, 75
Chip Detector Test 9
Clearance player 16
Clearance Recorder 16
Code selection softkeys 13
COM 13, 16, 83
Crew Alerting System (CAS)
Messages 11–16
Hazard
Avoidance
Fire Detection System Test 9
Flame Out Protection System Test 9
Flight path marker 73
FliteCharts® 74, 75
Frequency Transfer 16
Fuel Flow (FFLOW GPH) 6
Fuel on Board 42
Fuel reserve weight 42
Gross weight 42
C
190-02065-00 Rev. A
F
Procedures
Barometric Altitude Minimums 3
Barometric pressure 117
Basic Empty Weight 41
Edit a flight plan 55
Flight
Planning
B
E
GPS Nav
Activate a flight plan 36
Active database 122
AC-U-KWIK 76
ADF 13
AHRS 97, 101, 103
Aircraft load weight 41
Aircraft load weights 41
Airport Directory 76
Airport Signs 73, 74
Airways 120
ALT 67
Altitude mode 67
Altitude volume 67
AOPA 76
Audio Alert Test 9
Auxiliary Control Unit Test 9
AFCS
Database Synchronization 122
DCLTR Softkey 74
Dead Reckoning 84
Declutter 84, 114, 120
Direct-to 35
DME 13
DR mode 84, 85, 86
Dual navigation database 122
Dual Navigation Database 122
Nav/Com/
XPDR/Audio
3D Audio 23
EICAS
D
Flight
Instruments
Symbols
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Index
HSI magenta arrow 15
HSI single green arrow 15
J
Pathways 73, 74
PFD Configuration Softkeys 115
PFD Softkey Map 113
Pilot Profile 78
Power Assurance Check 8
Power Situation Indicator 7
PSI 7
Profile View 120
Profile View Terrain 71
Jeppesen 75
R
M
Reversionary Mode 83
ROC 92, 93
I
Inset Map 113, 114
Intercom Modes 18
IOI 92, 93
Magnetic Field Variation Database 126
Message advisories 97
MFD Softkeys 119
Mode selection softkeys 13
Multi Function Display (MFD)
Softkeys 119
N
NAV 14, 16
NAV1 1
NAV1 audio 16
NAV2 audio 16
Navigation database 37, 38, 99, 100,
105, 106, 110
Navigation mode selection 15
NEXRAD 119
O
OBS 1, 2
Obstacles 100, 103
Oil Temperature (OIL °F) 6
P
Passenger Address Mode 22
Index-2
S
SafeTaxi® 74
SBAS 61, 85
Scheduler 77
Sensor Softkeys 113
Standby frequency field 13
Standby Navigation Database 123,
124, 125
Store Flight Plan 55
SVS 73, 108
Synchronization 121
Synthetic Vision 73
Synthetic Vision System 73
T
Takeoff weight 42
TAS 67, 97
Temperature Compensated Altitude 63
Terminal Procedure Charts 74
Terrain 68, 100, 114, 120
Timer 108
Topographical data 114, 120
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Index
Flight
Instruments
Traffic 65, 66, 120
Traffic advisory 66
Traffic Advisory System (TAS) 67
Traffic Information Service (TIS) 66
Traffic map page 66, 67, 68
Transponder 13, 117, 118
Transponder Softkeys 117
EICAS
Nav/Com/
XPDR/Audio
U
AFCS
Unusual Attitudes 84
Updated Databases 121
GPS Nav
V
Flight
Planning
Vertical Navigation 37
Vertical speed guidance 38
VNV 35, 84, 109
Voice Recognition 25
VOR selection 15
Procedures
W
Hazard
Avoidance
Waypoint Selection Submenu 49
Weight and Balance 41
Wind data 116
Additional
Features
Z
Zero fuel weight 41
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-02065-00 Rev. A
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EICAS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000H Cockpit Reference Guide for the Bell 505 Jet Ranger X
190-02065-00 Rev. A
Garmin International, Inc.
1200 East 151st Street
Olathe, Kansas 66062, U.S.A.
Tel: 913.397.8200
Fax: 913.397.8282
Aircraft On Ground (AOG) Hotline: 913.397.0836
Aviation Dealer Technical Support: 888.606.5482
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
Tel: +44 (0) 238 052 4000
Fax: +44 (0) 238 052 4004
Aviation Support: +44 (0) 370 850 1243
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
Tel: 503.581.8101
Fax 503.364.2138
Garmin Corporation
No. 68, Zhangshu 2nd Road
Xizhi District, New Taipei City, Taiwan
Tel: 34-93-357-2608
Fax: 34-93-429-4484
www.garmin.com
© 2016 Garmin Ltd. or its subsidiaries
190-02065-00 Rev A
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