Garmin STC for Bell 206-407, AS-350B2-B3, EC 130 B4, STC for Robinson R44, Non-Airframe Reference Guide

G500H

Cockpit
Reference Guide

© 2011-2012 Garmin Ltd. or its subsidiaries. All rights reserved.

This manual refl ects the operation of system software version 6.00 or later. Some differences in operation
may be observed when comparing the information in this manual to later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, KS 66062, U.S.A.
Tel: [phone] Fax: [phone]

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Tel: [phone] Fax: [phone]

www.garmin.com

At Garmin, we value your opinion. For comments about this guide, please e-mail:
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Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
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®

Garmin

, GDU™ 620 are trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are
registered trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the
express permission of Garmin.

NavData
Communications; and XM

®

is a registered trademark of Jeppesen, Inc.; SkyWatch® is a registered trademark of L-3

®

is a registered trademark of XM Satellite Radio, Inc.

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 fi tness for a particular
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exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to you.

January 2012 Printed in the U.S.A.

AVIATION LIMITED WARRANTY

All Garmin avionics products are warranted to be free from defects in materials or workmanship for: two
years from the date of purchase for new Remote-Mount and Panel-Mount products; one year from the
date of purchase for new portable products and any purchased newly-overhauled products; six months
for newly-overhauled products exchanged through a Garmin Authorized Service Center; and 90 days for
factory repaired or newly-overhauled products exchanged at Garmin in lieu of repair. Within the applicable
period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs
or replacement will be made at no charge to the customer for parts or labor, provided that the customer
shall be responsible for any transportation cost. This warranty does not apply to: (i) cosmetic damage, such
as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product damage has occurred
due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, fl ood,
fi re, or other acts of nature or external causes; (iv) damage caused by service performed by anyone who is
not an authorized service provider of Garmin; or (v) damage to a product that has been modifi ed or altered
without the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims
against products or services that are obtained and/or used in contravention of the laws of any country.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER
WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER
ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR
OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO
STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL
DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR
FROM DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR
CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU.

Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement
product) the product or software or offer a full refund of the purchase price at its sole discretion. SUCH
REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

Online Auction Purchases: Products purchased through online auctions are not eligible for warranty
coverage. Online auction confirmations are not accepted for warranty verification. To obtain warranty
service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace
missing components from any package purchased through an online auction.

International Purchases: A separate warranty may be provided by international distributors for devices
purchased outside the United States depending on the country. If applicable, this warranty is provided
by the local in-country distributor and this distributor provides local service for your device. Distributor
warranties are only valid in the area of intended distribution. Devices purchased in the United States or
Canada must be returned to the Garmin service center in the United Kingdom, the United States, Canada,
or Taiwan for service.

To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a
Service Center near you, visit the Garmin web site at http://www.garmin.com or contact Garmin Customer
Service at 866.739.5687.

190-01150-03 Rev E

G500H Cockpit Reference Guide

i

WARNINGS, CAUTIONS, AND NOTES

Warnings, Cautions, & Notes

WARNING: Navigation and terrain separation must NOT be predicated

upon the use of the terrain function. The G500H Terrain Proximity feature
is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of
surroundings during fl ight. The Terrain Proximity feature is only to be used
as an aid for terrain avoidance and is not certifi ed for use in applications
requiring a certifi ed terrain awareness warning system. Terrain data is
obtained from third party sources. Garmin is not able to independently
verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (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.

WARNINGS, CAUTIONS, AND NOTES

WARNING: The Garmin G500H has a very high degree of functional

integrity. However, the pilot must recognize that providing monitoring and/
or self-test capability for all conceivable system failures is not practical.
Although unlikely, it may be possible for erroneous operation to occur
without a fault indication shown by the G500H. It is thus the responsibility
of the pilot to detect such an occurrence by means of cross-checking with
all redundant or correlated information available in the cockpit.

WARNING: The altitude calculated by GPS receivers is geometric height

above Mean Sea Level and could vary signifi cantly from the altitude
displayed by pressure altimeters, such as the output from the GDC 74H
Air Data Computer, or other pressure altimeters in aircraft. GPS altitude
should never be used for vertical navigation. Always use pressure altitude
displayed by the G500H PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used

in the G500H system must be updated regularly in order to ensure that
the information remains current. Pilots using an outdated database do so
entirely at their own risk.

ii G500H Cockpit Reference Guide

190-01150-03 Rev E

WARNINGS, CAUTIONS, AND NOTES

WARNING: Do not use basemap (land and water data) information for
primary navigation. Basemap data is intended only to supplement other
approved navigation data sources and should be considered as an aid to
enhance situational awareness.

WARNING: Traffi c information shown on the G500H Multi-Function Display

is provided as an aid in visually acquiring traffi c. Pilots must maneuver
the aircraft based only upon ATC guidance or positive visual acquisition
of confl icting traffi c.

WARNING: Datalink weather radar should not be used for hazardous

weather penetration. Weather information provided by the datalink receiver
is approved only for weather avoidance, not penetration.

WARNING: Datalink weather radar data is to be used for long-range
planning purposes only. Due to inherent delays in data transmission and
the relative age of the data, datalink weather radar data should not be
used for short-range weather avoidance.

WARNING: For safety reasons, G500H operational procedures must be
learned on the ground.

WARNING: To reduce the risk of unsafe operation, carefully review and
understand all aspects of the G500H Pilot’s Guide. Thoroughly practice
basic operation prior to actual use. During fl ight operations, carefully
compare indications from the G500H to all available navigation sources,
including the information from other NAVAIDs, visual sightings, charts, etc.
For safety purposes, always resolve any discrepancies before continuing
navigation.

WARNINGS, CAUTIONS, AND NOTES

WARNING: Never use the G500H to attempt to penetrate a thunderstorm.
Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s
Information Manual (AIM) recommend avoiding “by at least 20 miles any
thunderstorm identifi ed as severe or giving an intense radar echo”.

WARNING: Exceeding 200 deg/second in pitch or roll may invalidate AHRS
attitude provided to the G500H.

190-01150-03 Rev E

G500H Cockpit Reference Guide

iii

WARNINGS, CAUTIONS, AND NOTES

WARNING: Because of anomalies in the earth’s magnetic fi eld, operating
the G500H within the following areas could result in loss of reliable attitude
and heading indications. North of 65° North latitude between longitude
75° West and 120° West. An area North of 70° North latitude between
longitude 70° West and 128° West. An area of North of 70° North latitude
between longitude 85° East and 114° East. An area South of 55° South
latitude between longitude 120° East and 165° East.

WARNING: Do not use Terrain-HSVT information for primary terrain
avoidance. Terrain-HSVT is intended only to enhance situational
awareness.

CAUTION: 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 Garmin G500H utilize
GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as
with all NAVAIDs, information presented by the G500H can be misused or
misinterpreted and therefore, become unsafe.

WARNINGS, CAUTIONS, AND NOTES

CAUTION: The Garmin G500H does not contain any user-serviceable parts.
Repairs should only be made by an authorized Garmin service center.
Unauthorized repairs or modifi cations could void both the warranty and
pilot’s authority to operate this device under FAA/FCC regulations.

CAUTION: The G500H PFD and MFD displays use a lens coated with a
special anti-refl ective coating that is very sensitive to skin oils, waxes, and
abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a
clean, lint-free cloth and an eyeglass lens cleaner that is specifi ed as safe
for anti-refl ective coatings.

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 feet away
from the source of the interference should alleviate the condition.

iv G500H Cockpit Reference Guide

190-01150-03 Rev E

WARNINGS, CAUTIONS, AND NOTES

NOTE: All visual depictions contained within this document, including
screen images of the G500H bezel displays, are subject to change and
may not refl ect the most current G500H system. Depictions of equipment
may differ slightly from the actual equipment.

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: 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.

WARNINGS, CAUTIONS, AND NOTES

NOTE: Terrain data is not displayed when the aircraft latitude is greater
than 75° North or 60° South.

NOTE: Terrain-HSVT is standard when the Synthetic Vision Technology
(SVT) option is installed. The HTAWS option will take precedence over
Terrain-HSVT.

190-01150-03 Rev E

G500H Cockpit Reference Guide

v

Record of Revisions

Part Number Revision Date Description

190-01150-03 A

B
C

D

E

Jan 2010
Mar 2010
Nov 2010

Aug 2011

Jan 2012

Production Release
Updated speed tape markings.
Update to refl ect v4.00 and v5.00
software functionality.
Update to refl ect v6.00 software
functionality.
Minor edits.

vi G500H Cockpit Reference Guide

190-01150-03 Rev E

TABLE OF CONTENTS

Contents

Warnings, Cautions, & Notes ............................................................................ ii

Introduction ...................................................................................................... 1

Primary Flight Display (PFD) ............................................................................. 2

Airspeed Tape .............................................................................................................................. 4

Altitude Tape ............................................................................................................................... 5

Barometric Pressure ..................................................................................................................... 5

Minimums Bug (Barometric or Radar Altimeter) ............................................................................ 6

Altitude Bug ................................................................................................................................ 8

Wind Vectors ............................................................................................................................... 9

Vertical Speed (V/S) ..................................................................................................................... 9

Vertical Deviation Indicator (VDI) ............................................................................................... 10

Outside Air Temperature (OAT) ................................................................................................... 10

Attitude Indicator ...................................................................................................................... 11

Horizontal Situation Indicator (HSI): Aircraft Heading .................................................................. 12

Adjusting the Course Pointer ..................................................................................................... 13

HSI Bearing Pointers .................................................................................................................. 13

TABLE OF CONTENTS

Additional Features ........................................................................................ 16

Garmin Terrain-HSVT™ (Optional) ............................................................................................... 16

Displaying Garmin Terrain-HSVT

Displaying Heading on the Horizon ............................................................................................ 17

Displaying Airport Signs ............................................................................................................. 17

Multi-Function Display (MFD) ......................................................................... 18

Page Navigation - Moving Between Pages ................................................................................. 19

Changing Settings within a Page................................................................................................ 19

Default Map Page ...................................................................................................................... 19

MFD Soft Key Map ..................................................................................................................... 20

Map Group ..................................................................................................... 21

Navigation Map 1 and Navigation Map 2 Pages ......................................................................... 21

Decluttering (DCLTR) the Map Pages .......................................................................................... 22

Split Screen Page (Optional) ....................................................................................................... 25

Traffi c Map Page (Optional) ....................................................................................................... 26

Terrain Page .............................................................................................................................. 30

WX Group ....................................................................................................... 34

XM Weather Map Pages ............................................................................................................ 34

Customizing the Weather Map ................................................................................................... 34

Displaying Surface Data and Winds Aloft .................................................................................... 36

Garmin Flight Data Services (GFDS) Map Pages .......................................................................... 37

™

Terrain ................................................................................... 17

Aux Group ...................................................................................................... 39

190-01150-03 Rev E

G500H Cockpit Reference Guide

vii

TABLE OF CONTENTS

External Video Page (Optional) ................................................................................................... 39

System Setup Page .................................................................................................................... 40

®

Information Page (Optional) .............................................................................................. 44

XM

®

Radio Page (Optional) ....................................................................................................... 45

XM

System Status Page ................................................................................................................... 47

Position Reporting Page ............................................................................................................. 48

Iridium® Phone Page ................................................................................................................ 49

Flight Plan Group ........................................................................................... 51

Active Flight Plan Page .............................................................................................................. 51

Viewing Your Active Flight Plan .................................................................................................. 51

Waypoint Information Page........................................................................................................ 52

Charts Page (Optional) .............................................................................................................. 53

Setting Minimums ..................................................................................................................... 53

Changing Day/Night View .......................................................................................................... 53

Viewing Charts and Panning ...................................................................................................... 53

Viewing NOTAMs ...................................................................................................................... 54

Selecting a Chart ....................................................................................................................... 54

Viewing Details of ChartView™ Charts ...................................................................................... 55

Selecting Other Charts ............................................................................................................... 55

Chart Information ...................................................................................................................... 56

Alerts .............................................................................................................. 57

On Screen Alerts ........................................................................................................................ 57

™

Terrain-HSVT

Alerts ................................................................................................................ 58

Symbols .......................................................................................................... 59

Map Page Symbols .................................................................................................................... 59

TABLE OF CONTENTS

SafeTaxi

®

Symbols ..................................................................................................................... 60

Traffi c Symbols .......................................................................................................................... 60

Terrain Obstacle Symbols ........................................................................................................... 61

Map Toolbar Symbols ................................................................................................................ 61

®

XM

Weather Toolbar Symbols ................................................................................................... 62

Miscellaneous Symbols .............................................................................................................. 63

viii G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Introduction

This reference guide covers the operation of the GDU 620 as integrated in
the G500H Avionics Display System. The G500H Avionics Display System is
an avionics suite that combines primary fl ight instrumentation, navigational
information, and a moving map all displayed on dual 6.5 inch color screens. The
G500H system is composed of sub-units or Line Replaceable Units (LRUs). LRUs
have a modular design. This design greatly eases troubleshooting and maintenance
of the G500H system. A failure or problem can be isolated to a particular LRU,
which can be replaced quickly and easily. Each LRU has a particular function,
or set of functions, that contributes to the system’s operation. For more details
on the G500H system, refer to the latest revision of the G500H Pilot’s Guide,
P/N 190-01150-02.

PRIMARY FLIGHT DISPLAY

PFD/MFD

NOTE: Some G500Hs have the right-side display confi gured as the PFD.

190-01150-03 Rev E

G500H Cockpit Reference Guide

1

PRIMARY FLIGHT DISPLAY (PFD)

Primary Flight Display (PFD)

1

2

19

18

20

17

PRIMARY FLIGHT DISPLAY

3

4

12

13

6

7

8

9

10

5

11

Primary Flight Display (PFD)

16

15

14

NAV Status Bar: Displays which GPS is selected as the Active Source, Active Waypoint

1

(WPT), Distance to Waypoint (DIS), Desired Track (DTK) and Current Track (TRK).

Airspeed Tape: Displays Groundspeed (GS), Overspeed Range, Maximum (Vne) Speed
with Engine On, Airspeed Trend, Current Airspeed, Max (Vne) Speed with Engine Off

2

OR Max Autorotation Speed, and True Airspeed (TAS). Markings dependent upon

confi guration at time of installation. Reference AFM or POH.

Wind Vector: Displays direction and speed of wind.

3

Outside Air Temperature (OAT): Displays the current outside air temperature.

4

2 G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Attitude Sync Soft Key: Allows the synchronization of the aircraft to the horizon in

5

level fl ight.

Heading Select Key: Press HDG and turn PFD knob to set heading bug.

6

Course Select Key: Press CRS and turn PFD knob to set the course of the selected

7

source (VOR1, VOR2, GPS1, or GPS2).

Altitude Select Key: Press ALT and turn PFD knob to set altimeter bug.

8

V/S (Vertical Speed) Select Key: Press V/S and turn PFD knob to set V/S bug.

9

Barometer Select Key: Press BARO and turn PFD knob to change barometric setting.

10

PFD Knob: Turn PFD knob to change bug settings, Heading Bug, Course, Altitude Bug,

11

V/S Bug, and Barometer setting.

Soft Keys: Used to select available options on PFD or MFD.

12

SD Card Slots, Upper and Lower: The upper slot is used for updating databases or

13

software, the lower slot is for the database card.

PRIMARY FLIGHT DISPLAY

Soft Key Labels: Located on the bottom screen of the PFD and MFD. Selection is done
by pressing the corresponding soft key. Soft keys that are available have the labels
shown as white text on a black background. Soft keys that are selected have the labels

14

shown as black text on a gray background. Soft keys that are unavailable have the
labels shown as gray text on a black background.

Horizontal Situation Indicator (HSI): Displays the Selected Heading Box, Current

15

Heading, Turn Rate Markings, and Heading Trend.

Vertical Speed Tape: Displays Vertical Speed and the Vertical Speed Bug

16

Barometric (BARO) Setting: Displays the current setting of barometric pressure.

17

Roll Pointer and Slip/Skid Indicator: The slip/skid indicator is the bar beneath the roll
pointer. The indicator moves with the roll pointer and laterally away from the pointer

18

to indicate lateral acceleration (slip/skid).

Altitude Tape: Displays Current Altitude, Altitude Trend, Altitude Bug, Altitude

19

Minimums Bug and BARO setting.

Radar Altimeter Display: Displays current height above ground from the radar

20

altimeter. Brown band in altitude tape represents the ground.

190-01150-03 Rev E

G500H Cockpit Reference Guide

3

PRIMARY FLIGHT DISPLAY (PFD)

Airspeed Tape

The upper left portion of the PFD display provides Groundspeed, Airspeed
Trend, Current Airspeed, and True Airspeed information. Current Airspeed is
normally shown in white on the black pointer. The Trend Indicator (magenta
line) indicates what the airspeed will be in six seconds, if the current acceleration
is maintained. If the current acceleration will cause the airspeed to exceed V

NE

in
six seconds, the airspeed is displayed in yellow. If the current airspeed exceeds
VNE, the pointer changes to red with white text.

NOTE: Airspeed tape markings are dependent upon confi guration at

the time of installation. Reference the POH for more details.

Overspeed

V

NE

Airspeed Tape Markings

Overspeed Indication

Groundspeed

PRIMARY FLIGHT DISPLAY

Current

Airspeed

Airspeed Tape

4 G500H Cockpit Reference Guide

Maximum (Vne) Speed
with Engine On

Trend Indicator

Maximum (Vne Power Off) Speed with
Engine Off or Maximum Autorotation

OR

True Airspeed

Speed.

One of the two markings types is selected
during the installation confi guration.

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Altitude Tape

The upper right portion of the PFD displays the Altitude Bug setting, Current
Altitude, Altitude Trend, Altitude Minimums Bug, and the current BARO Setting.
The Altitude Trend indicates what the altitude will be in six seconds if the current
vertical speed is maintained.

Altitude Bug Setting

PRIMARY FLIGHT DISPLAY

Altitude Trend

Altitude Bug

Altitude Minimums Bug

BARO Setting

Altitude Tape

Current Altitude

Barometric Pressure

The Barometric Pressure Setting (BARO setting) is displayed at the bottom of
the altitude tape. To change the BARO setting, press the BARO key and turn the
PFD knob to the desired pressure. To select standard pressure (29.92IN), press
the PFD knob.

190-01150-03 Rev E

G500H Cockpit Reference Guide

5

PRIMARY FLIGHT DISPLAY (PFD)

Minimums Bug (Barometric or Radar Altimeter)

For altitude awareness, an Altitude Minimums Bug commonly referred to as
the Minimums Bug, can be set. the source of data for minimums alerting can be
selected to either barometric altitude or radar altitude (if installed.) When active
and within 2500 feet of the selected minimums altitude, the minimums bug
setting is displayed to the bottom left of the altimeter. When set, a bug appears
parked at the bottom of the altitude tape and moves up the tape as the set altitude
comes into view.

When the aircraft altitude descends to within 2500 feet of the selected •

altitude minimums setting, the minimums box appears with the altitude
value in cyan text. Once in range, the Minimums Bug appears in cyan
on the altitude tape.

A portion of the Minimums Bug will be displayed at
the bottom of the altitude tape if the selected altitude minimums bug is off
of the tape.

When the aircraft is within 100 feet of the selected altitude minimums •

setting, the bug and the altitude text turn white.

Once the aircraft reaches the selected altitude minimums setting, the •

bug and the altitude text turn yellow and the aural alert, “Minimums,
minimums” is heard one time.

Bug and text
are yellow when
altitude reached

Minimums

Bug

Bug and text are

cyan within 2500 ft

Bug and text are

white within 100 ft

PRIMARY FLIGHT DISPLAY

Minimums

Box

Minimums Annunciations using BARO for Source

Alerting is inhibited while the aircraft is on the ground and also, if a value has
been set for altitude alerting, until the aircraft reaches 150 feet above the setting
for the alert.

6 G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

To set the altitude for the Minimums Bug:

While viewing the Active Flight Plan page of the FPL Group, press the small 1)
MFD knob to activate the cursor.

Turn the large 2) MFD knob to the ALTITUDE portion of the MINIMUMS section.
Turn the small 3) MFD knob to enter the desired altitude. Press the ENT key to

confi rm selection.
When fi nished, press the small 4) MFD knob to exit the MINIMUMS box.

The Minimums Bug can also be set from the Charts page of the FPL.

While viewing the Charts page of the FPL Group, press the 1) MNU key and
select “Set Minimums” from the Options menu.

Turn the small 2) MFD knob to select Off, BARO, or RAD ALT.

Press the ENT key to move to enter altitude. Turn the small 3) MFD knob to
enter the desired altitude. Press the ENT key to confi rm selection.

NOTE: BARO will not be available for selection on G500H models.

Radar Altimeter
Minimums Bug

PRIMARY FLIGHT DISPLAY

Radar Altimeter Value

Minimums Box

Minimums Annunciations using RAD ALT for Source

190-01150-03 Rev E

Brown band ­represents the ground.

G500H Cockpit Reference Guide

7

PRIMARY FLIGHT DISPLAY (PFD)

Altitude Bug

The Altitude Bug is displayed on the Altitude Tape at the selected altitude bug
setting. A portion of the Altitude Bug will be displayed at the top or bottom of
the altitude tape if the selected altitude bug is off of the tape.

Altitude Bug

Setting

Altitude Bug

Altitude Bug

The Altitude Bug provides visual and aural altitude alerting. Aural alerting
occurs within 200 feet (or 1000 feet, as confi gured) of the Altitude Bug setting
or when deviating beyond 200 feet of the bug.

Within 1000 ft

Altitude Bug Indications

Within 200 ft

Deviation of

+/- 200ft

PRIMARY FLIGHT DISPLAY

8 G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Wind Vectors

The PFD will display a Wind Vector Field to the left of the HSI when confi gured
by the user. There are four different styles of wind vector displays available. Refer
to the System Setup page in the AUX Group section of this guide for instructions
on selecting wind vector style. Wind Vectors can only be calculated when the
aircraft is in the air. When airspeed is less than 20 knots, the Wind Vector windows
will indicate, “No Wind Data”.

Wind Vector Field

PRIMARY FLIGHT DISPLAY

Wind Vector Display

Vertical Speed (V/S)

The Vertical Speed Tape and Vertical Speed Bug are displayed below the Altitude
Tape. For rotorcraft with vertical speed operating limitations, red bands showing
Vertical Speed Maximum and Minimum ranges will be shown on the left side of
the Vertical Speed tape.

Vertical Speed Maximum

Current Vertical Speed

Vertical Speed Bug

Vertical Speed Minimum

Vertical Speed Bug Setting

190-01150-03 Rev E

Vertical Speed

G500H Cockpit Reference Guide

Vertical Speed - Rotorcraft

9

PRIMARY FLIGHT DISPLAY (PFD)

Vertical Deviation Indicator (VDI)

The Vertical Deviation Indicator is displayed for GPS and ILS approaches
with vertical guidance. The GPS approach glidepath is shown in magenta
(G and indicator), while the ILS approach glideslope is shown in green
(G and indicator.)

Vertical Deviation Source

Vertical Deviation Indicator

GPS Approach

ILS Approach

Outside Air Temperature (OAT)

The Outside Air Temperature, as sensed from the temperature probe on the
aircraft, is displayed to the left of the HSI. This static air temperature is used in

PRIMARY FLIGHT DISPLAY

calculating the true airspeed.

10 G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Attitude Indicator

Ground/Sky Pointer mode is confi gured during installation and can not be
changed by the pilot.

In an aircraft with an Attitude Indicator that has a Ground Pointer, the pointer
above the roll scale shifts with the roll or bank angle of the aircraft to keep the
Roll Scale Zero Pointer pointing towards the ground.

Roll Pointer

Roll Scale Zero Pointer

Roll Scale

PRIMARY FLIGHT DISPLAY

G500H Attitude Indicator with a Ground Pointer Confi guration in a Left Turn

In an aircraft with an Attitude Indicator that has a Sky Pointer, the pointer
below the roll scale shifts with the roll or bank angle of the aircraft to keep the
Roll Pointer pointing towards the sky.

Roll Scale Zero Pointer

Roll Pointer

Roll Scale

G500H Attitude Indicator with a Sky Pointer Confi guration in a Left Turn

190-01150-03 Rev E

G500H Cockpit Reference Guide

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PRIMARY FLIGHT DISPLAY (PFD)

The Trim Ball Indicator is the bar beneath the roll pointer. The indicator moves
with the roll pointer and moves laterally away from the pointer to indicate lateral
acceleration. Trim is indicated by the location of the bar relative to the pointer.
One bar displacement as shown below is equivalent to one ball displacement on
a traditional Trim Ball Indicator.

Roll Pointer Trim Ball IndicatorRoll Scale Zero

Trim Indication

Horizontal Situation Indicator (HSI): Aircraft Heading

The top of the HSI displays current heading, current GPS track (magenta
diamond), heading trend, and turn rate markings. The heading trend indicates
what the aircraft heading will be in six seconds if the heading rate remains
unchanged. The turn rate markings, along with the heading trend, display standard
and half-standard rate turns.

Current Heading Turn Rate Markings

PRIMARY FLIGHT DISPLAY

Heading TrendCurrent GPS Track

HSI Heading Markings

NOTE: If magnetic heading is lost, GPS ground track will be displayed

in place of heading.

12 G500H Cockpit Reference Guide

190-01150-03 Rev E

PRIMARY FLIGHT DISPLAY (PFD)

Adjusting the Course Pointer

Press the CRS key and turn the PFD knob to select a course for a VOR/ILS or
OBS mode course.

HSI Bearing Pointers

NOTE: The Bearing Pointer for navigation source 1 (BRG1) will be an

arrow with a single line. The Bearing Pointer for navigation source 2
(BRG2) will be an arrow with a double line.

To toggle between the available bearing pointers, press the PFD soft key followed
by the BRG1 or BRG2 soft keys.

The BRG1 soft key cycles through modes NAV1 and GPS1. Additionally, ADF
is available if an ADF source is installed.

The BRG2 soft key cycles through modes, NAV2 and GPS2 if a second NAV
or GPS source is available. Additionally, ADF is available if an ADF source is
installed.

NAV2 Bearing Pointer

NAV1 Bearing Pointer

PRIMARY FLIGHT DISPLAY

Selected source for

BRG 1 bearing pointer

190-01150-03 Rev E

Selected source for

BRG 2 bearing pointer

Bearing Pointers on the HSI

G500H Cockpit Reference Guide

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