3D Connexion GNS 530A User Manual

GNS 530(A)

Pilot’s Guide and Reference

RECORD OF REVISIONS

Revision Date of Revision Description

A 5/00 Initial Release B 5/01 Update to reﬂect software changes through 2.06 C 4/03 Update to reﬂect software changes through 4.0 D 2/07 Updated layout, added TAWS, TERRAIN, TIS, and

Weather information, per SW v6.02

E 7/07 Updated per Main SW v6.03

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

This manual reﬂects the operation of Main System Software version 6.03 or later. Some differences may be observed when comparing the information in this manual to other software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062 USA p: 913.397.8200 f: 913.397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, Oregon 97302 USA p: 503.391.3411 f: 503.364.2138

Garmin (Europe) Ltd., Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. p: 44/ (0) 0870.8501241 f: 44/ (0) 870.85012

Garmin (Asia) Corp., No. 68, Jangshu 2nd Road., Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f : 886/2.2642-9099

Web Site Address: www.garmin.com Visit the Garmin website for the latest updates and supplemental information concerning the operation of this and other Garmin

products.

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin®, AutoLocate®, and PhaseTrac12® are registered trademarks of Garmin Ltd. or its subsidiaries and may not be used without the express permission of Garmin.

GNS™ and Spell’N’Find™ are trademarks of Garmin Ltd. or its subsidiaries and may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.

July 2007 190-00181-00 Rev. E Printed in the U.S.A.

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

TABLE OF CONTENTS

SECTION 1: INTRODUCTION ........................................... 1-1

1.1 Accessories and Packing List ................................. 1-1

1.2 Key and Knob Functions ......................................... 1-2

1.3 Takeoff Tour ............................................................... 1-5

SECTION 2: COM .................................................................. 2-1

2.1 Communicating using the GNS 530 ...................... 2-1

SECTION 3: NAV PAGES .................................................. 3-1

3.1 Main Page Groups .................................................... 3-1

3.2 NAV Page Group ....................................................... 3-2

3.3 Default NAV Page .....................................................3-2

3.4 Map Page ...................................................................3-6

3.5 TERRAIN Page .......................................................... 3-15

3.6 TAWS Page ............................................................... 3-18

3.7 NAV/COM Page ........................................................ 3-21

3.8 Satellite Status Page ............................................. 3-23

SECTION 4: DIRECT-TO NAVIGATION .........................4-1

4.1 Overview .................................................................... 4-1

SECTION 5: FLIGHT PLANS .............................................5-1

5.1 Flight Plan Catalog Page ........................................ 5-1

5.2 Active Flight Plan Page ........................................... 5-8

SECTION 6: PROCEDURES ............................................... 6-1

6.1 Approaches, Departures, and Arrivals ................. 6-1

6.2 Non-Precision Approach Operations .................... 6-3

6.3 ILS Approaches ....................................................... 6-25

6.4 Points to Remember for All Approaches ..........6-32

SECTION 7: WPT PAGES .................................................... 7-1

7.1 WPT Page Group ....................................................... 7-1

7.2 Airport Location Page ............................................. 7-4

7.3 Airport Runway Page .............................................. 7-6

7.4 Airport Frequency Page .......................................... 7-8

7.5 Airport Approach Page .........................................7-10

7.6 Airport Arrival Page ............................................... 7-12

7.7 Airport Departure Page ........................................ 7-14

7.8 Intersection Page ................................................... 7-16

7.9 NDB Page .................................................................. 7-16

7.10 VOR Page ................................................................7-17

7.11 User Waypoint Page ............................................7-18

SECTION 8: NRST PAGES ................................................. 8-1

8.1 NRST Page Group .....................................................8-1

8.2 Nearest Airport Page ............................................... 8-3

8.3 Nearest Intersection Page ...................................... 8-5

8.4 Nearest NDB Page .................................................... 8-6

8.5 Nearest VOR Page ....................................................8-6

8.6 Nearest User Waypoint Page ................................. 8-8

8.7 Nearest Center (ARTCC) Page ................................ 8-8

8.8 Nearest Flight Service Station (FSS) Page ..........8-9

8.9 Nearest Airspace Page .......................................... 8-11

SECTION 9: VLOC RECEIVER ........................................... 9-1

9.1 VLOC (VOR/LOCALIZER/GLIDESLOPE) Receiver

Operations ......................................................................... 9-1

SECTION 10: AUX PAGES ...............................................10-1

10.1 AUX Page Group ................................................... 10-1

10.2 Flight Planning Page ...........................................10-2

10.3 Utility Page ..........................................................10-10

10.4 Setup Page ........................................................... 10-18

SECTION 11: VERTICAL NAVIGATION (VNAV) ..... 11-1

SECTION 12: TERRAIN ..................................................... 12-1

12.1 INTRODUCTION ...................................................... 12-1

12.2 TERRAIN Page ........................................................ 12-3

12.3 TERRAIN Alerts ...................................................... 12-4

12.4 Database Information for TERRAIN .................. 12-9

SECTION 13: TAWS ............................................................ 13-1

13.1 INTRODUCTION ...................................................... 13-1

13.2 TAWS Page .............................................................13-3

13.3 TAWS Alerts ............................................................ 13-4

13.4 Database Information for TAWS ..................... 13-11

SECTION 14: ADDITIONAL FEATURES ..................... 14-1

14.1 Trafﬁc Information Service (TIS) Interface ..... 14-1

14.2 Weather Data Link Interface ........................... 14-12

SECTION 15: FAULT DETECTION and

EXCLUSION ............................................................................ 15-1

15.1 Detection and Exclusion ..................................... 15-1

15.2 Pre-Departure Veriﬁcation of FDE ....................15-2

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

iii

TABLE OF CONTENTS

SECTION 16: MESSAGES, ABBREVIATIONS, and

TERMS ............................................................................ 16-1

NAV

16.1 Messages ................................................................ 16-1

16.2 Abbreviations ........................................................16-9

16.3 Navigation Terms ...............................................16-12

Appendix A: Data Card Use ..........................................A-1

Appendix B: Speciﬁcations ........................................... B-1

Appendix C: Troubleshooting Q & A ........................C-1

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

WARNINGS,

CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the TAWS function. The TAWS 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 ﬂight. The TAWS feature is only to be used as an aid for terrain avoidance and is not certiﬁed for use in applications requiring a certiﬁed terrain awareness system. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The terrain data should be used only as an aid for situational awareness. Terrain data must not

be used as the sole basis for decisions or maneuvers to avoid terrain or obstacles. Terrain data must not be used for navigation.

WARNING: The altitude calculated by GNS 530 GPS receivers is geometric height above Mean Sea Level and could vary signiﬁcantly from the altitude displayed by pressure altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by pressure altimeters in the aircraft.

WARNING: The Jeppesen database used in the GNS 530 system must be updated regularly in order to ensure that its information remains current. Updates are released every 28 days. A database information packet is included in the GNS 530 package. Pilots using an outdated database do so entirely at their own risk.

WARNING: The basemap (land and water data) must not be used for navigation, but rather only for nonnavigational situational awareness. Any basemap indication should be compared with other navigation sources.

WARNING: For safety reasons, GNS 530 operational procedures must be learned on the ground.

WARNING: 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 GNS 530 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the GNS 530 can be misused or misinterpreted and, therefore, become unsafe.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

WARNINGS,

CAUTIONS, AND NOTES

WARNING: Use the GNS 530, Weather Data Link Interface, TIS, and TAWS at your own risk. To reduce the risk of unsafe operation, carefully review and understand all aspects of the GNS 530 Pilot’s Guide documentation and the GNS 530 Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During ﬂight operations, carefully compare indications from the GNS 530 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.

CAUTION: The GNS 530 display lens is coated with a special anti-reﬂective 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 speciﬁed as safe for anti-reﬂective coatings.

CAUTION: The Garmin GNS 530 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: All visual depictions contained within this document, including screen images of the GNS 530 panel and displays, are subject to change and may not reﬂect the most current GNS 530 system. Depictions of equipment may differ slightly from the actual equipment.

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.

NOTE: Unless otherwise speciﬁed within this manual, the term ‘GNS 530’ applies to the GNS 530, GNS 530A, and GNS 530(A) w/TAWS models. Please note that the difference between the GNS 530 and the GNS 530A models is indicated under ‘VHF COM Performance’ in the Speciﬁcations section of this manual (Appendix B).

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 website at www.garmin.com/prop65.

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

WARRANTY

LIMITED WARRANTY

This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this 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 and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR 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 THIS 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 the unit or software, or to 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.

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 800-800-1020.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

vii

WARRANTY

Blank Page

viii

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

SECTION 1: INTRODUCTION

1.1 ACCESSORIES AND PACKING LIST

Congratulations on choosing the ﬁnest, most advanced panel mount IFR navigation/communication system available. The GNS 530 represents Garmin’s commitment to provide accurate, easy-to-use avionics.

Before installing and getting started with the GNS 530, please check to see that the package includes the following items. If any parts are missing or damaged, please contact a Garmin dealer immediately.

Standard Package:

• GNS 530 Unit

• NavData® Card

• Terrain Data Card

• Installation Rack

• Connectors

The Garmin dealer performs the installation and conﬁguration of the GNS 530. The GNS 530 is secured in the installation rack with the proper wiring connections performed. After installation, the NavData Card and the Terrain Data Card (if applicable) are installed into their correct slots on the front of the unit (Appendix A). A Garmin dealer can answer questions about the installation such as location of antennas or any connections to other equipment in the panel.

NOTE: Help Garmin provide better support by

completing on-line registration. Registration ensures notiﬁcation of product updates, new products, and provides for lost or stolen unit tracking. Have the serial number of the GNS 530 available and connect to the website (www. garmin.com). Look for the product registration link on the home page.

• GPS Antenna

• Pilot’s Guide

• Quick Reference Guide

• 400/500 Series Display Interface Pilot’s Guide Addendum

• Database Subscription Packet

• Warranty Registration Card

• GNS 530 Simulator CD-ROM

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

1-1

SECTION 1

INTRODUCTION

1.2 KEY AND KNOB FUNCTIONS

The GNS 530 is designed to make operation as simple as possible. The key and knob descriptions (Figure 1-1) provide a general overview of the primary function(s) for each key and knob. The takeoff tour (Section 1.3) is intended to provide a brief overview of the primary functions of the GNS 530.

Experiment with the unit and refer to the reference

sections for more information.

Data is entered using the large and small knobs. Experiment with them to become efﬁcient at entering data. This greatly reduces the amount of time spent operating the GNS 530 in ﬂight.

1-2

COM Flip-ﬂop

COM Power/Volume

VLOC Flip-ﬂop

VLOC Volume

Small left knob

Figure 1-1 Keys and Knobs

Large left knob

RNG (map range)

Direct-to

CLR (clear)

GNS 530(A) Pilot’s Guide and Reference

ENT (enter)

12 17

Small right knob

13 18

Large right knob

14 19

CDI

OBS

MSG (message)

FPL (ﬂight plan)

VNAV

PROC (procedures)

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

Left-hand Keys and Knobs

(1) COM Flip-ﬂop Key – Swaps the active and standby COM frequencies. Press and hold to select emergency channel (121.500 MHz). (2) COM Power/Volume Knob – Controls unit power and communications radio volume. Press momentarily to disable automatic squelch control. (3) VLOC Flip-ﬂop Key – Used to swap the active and standby VLOC frequencies (i.e., make the selected standby frequency active). (4) VLOC Volume Knob – Controls audio volume for the selected VOR/Localizer frequency. Press momentarily to enable/disable the ident tone. (5) Small Left Knob (COM/VLOC) – Used to tune the kilohertz (kHz) value of the standby frequency for the communications transceiver (COM) or the VLOC receiver, whichever is currently selected by the tuning cursor. Press this knob momentarily to toggle the tuning cursor between the COM and VLOC frequency ﬁelds. (6) Large Left Knob (COM/VLOC) – Used to tune the megahertz (MHz) value of the standby frequency for the communications transceiver (COM) or the VLOC receiver, whichever is currently selected by the tuning cursor.

Right-hand Keys and Knobs

(7) RNG Key – Allows the pilot to select the desired map range. Use the up arrow to zoom out to a larger area, or the down arrow to zoom in to a smaller area. (8) Direct-to Key – Provides access to the direct-to function, which allows the pilot to enter a destination waypoint and establishes a direct course to the selected destination (Section 4). (9) MENU Key – Displays a context-sensitive list of options. This options list allows the pilot to access additional features or make settings changes which relate to the currently displayed page. (10) CLR Key – Used to erase information, remove map detail, or to cancel an entry. Press and hold the CLR key to immediately display the Default NAV Page. (11) ENT Key – Used to approve an operation or complete data entry. It is also used to conﬁrm information during power on. (12) Small Right Knob – Used to select pages within one of the page groups. Press this knob momentarily to display the on-screen cursor. The cursor allows the pilot to enter data and/or make a selection from a list of options. When entering data, the small right knob is used to select the desired letter or number and the large right knob is used to move to the next character space. The small right knob is also used to move the target pointer up (turn clockwise) or down (counterclockwise) when the map panning function is active. (13) Large Right knob – Used to select page groups: NAV, WPT, AUX, or NRST. With the on-screen cursor enabled, the large right knob allows the pilot to move the cursor about the page. The large right knob is also used to move the target pointer right (turn clockwise) or left (counterclockwise) when the map panning function is active.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

1-3

SECTION 1

INTRODUCTION

` NOTE: Data is entered using the large and

small right knobs (Figure 1-2). Experiment with them to become efﬁcient at entering data. This will greatly reduce the amount of time spent operating the GNS 530 in ﬂight.

Figure 1-2 Blank Direct-to Page

NOTE: When the GNS 530 is displaying a list

of information that is too long for the display screen, a scroll bar appears along the right-hand side of the display (Figure 1-3). The scroll bar graphically indicates the number of additional items available within the selected category. To scroll through the list, press the small right knob to activate the cursor, then turn the large right knob.

Scroll Bar

Bottom Row Keys

(14) CDI Key – Used to toggle which navigation source (GPS or VLOC) provides output to an external HSI or CDI. (15) OBS Key – Used to select manual or automatic sequencing of waypoints. Pressing the OBS mode, which retains the current ‘active to’ waypoint as the navigation reference even after passing the waypoint (i.e., prevents sequencing to the next waypoint). Pressing the OBS Key again returns the unit to normal operation, with automatic sequencing of waypoints. When OBS mode is selected, the pilot may set the desired course to/from a waypoint using the Select OBS Course pop-up window, or an external OBS selector on the HSI or CDI. (16) MSG Key – Used to view system messages and to alert the pilot to important warnings and requirements. See Section 16.1 for more information on messages. (17) FPL Key – Allows the pilot to create, edit, activate, and invert ﬂight plans, as well as access approaches, departures, and arrivals. A closest point to ﬂight plan feature is also available from the FPL Key. See Section 5 for more information on ﬂight plans. (18) VNAV (Vertical Navigation) Key – Allows the pilot to create a three-dimensional proﬁle which provides guidance to a ﬁnal (target) altitude at a speciﬁed location See Section 11. (19) PROC Key – Allows the pilot to select and remove approaches, departures, and arrivals from the ﬂight plan. When using a ﬂight plan, available procedures for the departure and/or arrival airport are offered automatically. Otherwise, the pilot may select the desired airport, then the desired procedure.

OBS Key selects

1-4

Figure 1-3 Scroll Bar

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

1.3 TAKEOFF TOUR

reading within this Pilot’s Guide includes:

Overview

The Garmin GNS 530 provides the pilot accurate navigational data and communication capability, along with non-precision and precision approach certiﬁcation in the IFR environment. The takeoff tour is designed to familiarize the pilot with:

• Powering up the unit

• Changing frequencies

• Entering data

• Performing a simple direct-to

• Selecting IFR procedures

• Using some limited ﬂight plans

In addition, this section brieﬂy covers the Default NAV Page, the Map Page, and the NAV/COM Page, which are available as part of the NAV Page Group. These pages are used for most of the in-ﬂight navigation.

The takeoff tour assumes that the unit and antennas have been properly installed and that the GNS 530’s default settings have not been changed. If any of the factory default settings (position format, units of measure, selectable ﬁelds, etc.) have been changed, the pictures shown here may not exactly match what is shown on the GNS 530. Prior to using the GNS 530 for the ﬁrst time, Garmin recommends that the aircraft be moved to a location that is well away from buildings and other aircraft so the unit can collect satellite data without interruption.

This takeoff tour is intended to provide a brief introduction of the GNS 530’s major features. Sections 2 through 14 of this manual describe these features and others in additional detail. Refer to these sections, as needed to learn or review the details regarding a particular feature.

Service staff is available during normal business hours (U.S. Central time zone) at the phone and fax numbers listed on page ii. Garmin can also be reached by mail (page ii) or at our website address, www.garmin.com.

Powering up the GNS 530

using the COM Power/Volume knob at the top left corner of the unit. Turning it clockwise turns unit power on and increases the COM radio volume. After turning the unit on, a welcome page is displayed while the unit performs a self test, followed sequentially by the Unit Type Page (Figure 1-4) and the Software Version Page. Then (depending on conﬁguration) the Weather Page, the Trafﬁc Page, the Aviation Database Page, and the Land/Terrain/ Obstacles Database Page are sequentially displayed.

After becoming familiar with the basics, some suggested

• Flight plan features - Section 5

• IFR procedures - Section 6

• Waypoint information pages (database information) - Section 7

• Unit settings (conﬁguring the unit to the pilot’s preferences) - Section 10

If more information is needed, Garmin’s Customer

The GNS 530’s power and COM volume are controlled

Figure 1-4 Unit Type Page

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

1-5

SECTION 1

INTRODUCTION

The Database Versions Page (Figure 1-5) appears next, which shows the current database information on the NavData and Terrain Data Cards. Database information highlighted in yellow indicates the database is not within its effective dates. The NavData database is updated every 28 days and must be current for approved instrument approach operations. Information on database subscriptions is available inside the GNS 530 package.

Figure 1-5 Database Versions Page

Acknowledging the database information:

Press the

Check CDI/HSI, RMI, and

Other Instruments to verify

these Indications

Should Match Current

OBS Course Selection

ENT Key.

Fuel Capacity is

entered manually

Fuel On-Board and Fuel Flow are Provided by Sensors, if Installed

Select to Set Fuel Level to Full Capacity

Select to display Checklists Page

Instrument Panel Self-test Page

Once the database has been acknowledged, the

Instrument Panel Self-test Page appears (Figure 1-6).

To ensure that the GNS 530 and any connected instruments are working properly, check for the following indications on the CDI/HSI, RMI, external annunciators, and other connected instruments:

• Course deviation - Half left/no ﬂag

• TO/FROM ﬂag - TO

• Bearing to destination - 135°

• Distance to destination - 10.0 nm

• All external annunciators (if installed) - On

• Glideslope - Half up/no ﬂag

• Time to destination - 4 minutes

• Desired

• Ground speed - 150 knots

The Instrument Panel Self-test Page indicates the currently selected OBS course, fuel capacity (CAP), fuel on board (FOB), and fuel ﬂow (FF). The fuel capacity, fuel on board, and fuel ﬂow may be manually entered if the installation does not include connection to sensors which automatically provide these ﬁgures.

Entering fuel capacity, fuel on board, or fuel ﬂow ﬁgures (if not provided by sensors):

1) Turn the large

2) Turn the small and large

track - 149.5°

right knob to select the Fuel

Capacity, Fuel on Board, or Fuel Flow ﬁeld.

right knobs to enter

the desired ﬁgure (Figure 1-7) and press the ENT Key.

1-6

Figure 1-6 Instrument Panel Self-Test Page

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

INTRODUCTION

Viewing the Checklists Page:

SECTION 1

Figure 1-7 Fuel Flow Selected

The Instrument Panel Self-test Page includes selections to set fuel on board to full capacity and access the Checklists Page. This allows the pilot to quickly set fuel to full limits and display any checklists that have been entered, such as start up or takeoff checklists.

Setting fuel on board to full (if not provided by sensor):

1) Turn the large

right knob to highlight ‘Set Full

Fuel?’ (Figure 1-8).

1) Turn the large

right knob to highlight ‘Go To

Chklist?’ (Figure 1-9) and press the ENT Key.

Figure 1-9 ‘Go To Chklist?’ Highlighted

2) Turn the large right knob to select the desired

checklist, then execute each step (Section

10.3, Utility Page: Checklists) in the selected checklist.

3) Once the pilot completes the desired checklist(s), press the small

right knob to return to the

Checklists Page. Press the small right knob again to return to normal operation on the Satellite Status Page or the Map Page.

Figure 1-8 ‘Set Full Fuel?’ Highlighted

2) Press the ENT Key and verify that fuel on board

now matches the fuel capacity ﬁgure. Fuel on board is reduced, over time, based on the fuel ﬂow ﬁgure.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

4) Once instrument operation has been veriﬁed with the Instrument Panel Self-test Page displayed, highlight ‘OK?’, and press the

ENT

Key.

NOTE: The GNS 530 can hold up to nine checklists

with up to 30 entries in each checklist.

1-7

SECTION 1

INTRODUCTION

Satellite Status Page

The Satellite Status Page (Figure 1-10) appears as the

GNS 530 attempts to collect satellite information.

When an ‘Acquiring’ status is displayed on the Satellite Status Page, the signal strengths of any satellites received appear as ‘bar graph’ readings. This is a good indication that the unit is receiving signals and a position ﬁx is being determined. Following the ﬁrst-time use of the GNS 530, the time required for a position ﬁx varies, usually from one to two minutes.

Figure 1-10 Satellite Status Page

The Satellite Status Page displays a ‘Search Sky’ status, and the message annunciator (MSG), above the MSG Key also ﬂashes to alert the pilot of system message, ‘Searching the Sky’.

Viewing a system message:

Press the

MSG Key (Figure 1-11).

The Message Page appears and displays the status or warning information applicable to the receiver’s current operating condition.

Figure 1-11 Message Page

1-8

If the unit can only obtain enough satellites for 2D navigation (no altitude), the unit uses the altitude provided by the altitude encoder (if one is connected).

The ‘INTEG’ annunciator (bottom left corner of the screen) indicates that satellite coverage is insufﬁcient to pass built-in integrity monitoring tests. In the example above, not enough satellites are being received to determine a position. The Satellite Status Page shows the ID numbers for the satellites and the relative signal strength of each satellite received (as a bar graph reading).

‘Searching Sky’ indicates that satellite almanac data is not available or has expired (if the unit hasn’t been used for six months or more). This means the unit is acquiring satellite data to establish almanac and satellite orbit information, which can take ﬁve to ten minutes. The data is recollected from the ﬁrst available satellite.

GNS 530(A) Pilot’s Guide and Reference

Returning to the previous page after viewing a message:

Press the

NOTE: The GNS 530 utilizes certain software

algorithms to ensure reliable GPS receiver operation. Receiver Autonomous Integrity Monitoring (RAIM) and Fault Detection and Exclusion (FDE) are two examples. These features allow navigation during Oceanic/Remote legs of a ﬂight using the GNS 530. For further details, please refer to Sections 10.3, 10.4, and 14.

MSG Key again.

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

Selecting COM and VLOC Frequencies

While the GNS 530 is acquiring a position, take a minute to dial in the active and standby frequencies to be used for the ﬁrst phase of the ﬂight. The GNS 530’s display is divided into separate windows (or screen areas), including a COM Window, VLOC Window, and the GPS Window (Figure 1-12).

COM Window

Active

Frequency

Standby

Frequency

VLOC

Window

Figure 1-12 Standby Frequency 135.325 MHz

Changing the standby communication frequency:

1) Press the small the tuning cursor to the COM Window (Figure 1-12).

2) Turn the large

left knob to select the MHz,

and the small left knob to select the kHz of the desired frequency.

GPS Window

left knob if needed, to move

Placing the standby communication frequency in the active ﬁeld:

Press the COM Flip-ﬂop Key

Figure 1-13 Active Frequency 135.325 MHz

(Figure 1-13).

Once the active frequency has been entered, repeat steps 1 and 2 to enter the standby frequency. After both communication frequencies have been entered, the COM Window may be kept ‘hot’ by leaving the cursor on the standby frequency. Move the cursor to the VLOC Window by pressing the small left knob.

NOTE: When selecting VLOC frequencies, the

tuning cursor automatically returns to the COM Window after 30 seconds of inactivity.

Changing the standby VLOC frequency:

1) Press the small left knob if needed, to activate

the tuning cursor in the VLOC Window.

2) Turn the large

left knob to select the MHz,

and the small left knob to select the kHz of the desired frequency.

190-00181-00 Rev. E

Placing the standby frequency in the active ﬁeld:

Press the NAV Flip-ﬂop Key.

GNS 530(A) Pilot’s Guide and Reference

1-9

SECTION 1

INTRODUCTION

Page Groups

NAV Group WPT Group AUX Group NRST Group

see Section 3 see Section 7 see Section 10 see Section 8

Table 1-1 Page Groups

The bottom right corner of the screen (Figure 1-14) indicates which page group (Table 1-1) is currently being displayed, the number of pages available within that group (indicated by square icons), and the placement of the current page within that group (indicated by a highlighted square icon).

In addition to the NAV Page Group, additional page groups are available for waypoint information (WPT), auxiliary (AUX) functions such as ﬂight planning or unit settings, and listings for nearest (NRST) airports or other facilities.

NAV Pages

There are ﬁve pages available under the NAV Page

Group*:

• Default NAV Page

• Map Page

• TAWS Page

• NAV/COM Page

• Satellite Status Page

The Default NAV Page, the Map Page, and the NAV/

COM Page are used for most of the in-ﬂight navigation.

Selecting the NAV Page Group and displaying the Default NAV Page:

Press and hold the

Selecting the desired NAV Page:

Turn the small right knob until the desired

page is displayed.

CLR Key.

1-10

Current Page Group Number of Pages in

Current Page Group

Figure 1-14 Current Page and Page Group

Position of

Current Page

within Current

Page Group

Selecting the desired page group and page:

Turn the large right knob until a page from the

desired page group is displayed.

Turn the small right knob until the desired page

is displayed.

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

Map Page

After the GNS 530 acquires satellites and computes a position, the Map Page (Figure 1-15) appears automatically.

Map Display

Present

Position

Map Range

Figure 1-15 Map Page

The Map Page displays the present position (using an airplane symbol) relative to nearby airports, VORs, NDBs, intersections, user waypoints, and airspace boundaries. The route is displayed as a solid line.

Optional data ﬁelds for destination waypoint (WPT), desired track (DTK), track (TRK), distance to waypoint (DIS), and ground speed (GS) appear on the right-hand side of the display. These ﬁelds are user selectable (Section

3.4, Selecting Desired On-screen Data) to allow the pilot to conﬁgure the unit. Available settings include: altitude, bearing, enroute safe altitude, estimated time of arrival, minimum safe altitude, and ground track.

A Map Setup Page is provided to designate the maximum range at which each map feature appears. These settings provide an automatic decluttering of the map (based upon preferences) while adjusting the range. See Section 16.3 for deﬁnitions of these navigation terms.

Data

Fields

Desired Track

While viewing the Map Page, the pilot can quickly declutter and remove many of the background map details by pressing the

CLR Key (repeatedly) until the desired

detail is depicted.

To change the map range, press the up arrow (to zoom out) or the down arrow (to zoom in) of the RNG (map range) Key. The current map range is depicted in the lower left corner of the Map Display.

Direct-to Navigation

The GNS 530 can use direct point-to-point navigation to provide guidance from takeoff to touchdown, even in the IFR environment. Once a destination is selected, the unit provides speed, course, and distance data based upon a direct course from the present position to the destination. A destination can be selected from any page with the Direct-to Key.

Selecting a direct-to destination:

1) Press the Direct-to Key. The Select Direct-to

Waypoint Page appears with the destination ﬁeld highlighted.

2) Turn the small letter of the destination waypoint identiﬁer. The destination waypoint may be an airport, VOR, NDB, intersection, or user waypoint, as long as it is in the database or stored in memory as a user waypoint.

3) Turn the large the cursor to the next character position.

right knob to enter the ﬁrst

right knob to the right to move

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

1-11

SECTION 1

INTRODUCTION

4) Repeat steps 2 and 3 to spell out the rest of the waypoint identiﬁer (Figure 1-16).

Figure 1-16 Direct-to Waypoint Page

5) Press the ENT Key to conﬁrm the identiﬁer. The ‘Activate?’ function ﬁeld is highlighted (Figure 1-17).

Figure 1-17 ‘Activate?’ Highlighted

6) Press the ENT Key to activate a direct-to course to the selected destination.

Default NAV Page

During most ﬂights, the Default NAV Page, the Map Page, and the NAV/COM Page are the primary pages used for navigation.

Selecting the Default NAV Page:

Press a nd hold the CL R Ke y (Figu re

1-18).

User-Selectable Data Fields (all four corners)

Active Leg

Course

Deviation

Indicator

(CDI)

Figure 1-18 Default NAV Page

of Flight Plan, or Direct-to Destination

The Default NAV Page (Figure 1-18) displays a graphic course deviation indicator (CDI), the active leg of the ﬂight plan (as deﬁned by the current ‘from’ and ‘to’ waypoints), and four user-selectable data ﬁelds. The default settings for these ﬁelds are desired track (DTK), distance to waypoint (DIS), ground speed (GS), and estimated time enroute (ETE). See Section 16.3 for deﬁnitions of these navigation terms.

1-12

Once a direct-to destination is selected, press and hold

the CLR Key to display the Default NAV Page.

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

Changing the data ﬁelds:

1) From the Default NAV page, press the MENU

Key and select ‘Change Fields?’ (Figure 1-19).

Figure 1-19 Default NAV Page Menu

2) Turn the large right knob to select the data

ﬁeld to be changed.

3) Turn the small

right knob to display a list of

data options (Figure 1-20).

NAV/COM Page

From the Default NAV Page, turn the small right knob until the NAV/COM Page (Figure 1-21) is displayed.

Departure, Enroute, or

Frequency

Type

Arrival Airport

Frequency List

Figure 1-21 NAV/COM Page

The NAV/COM Page displays the available frequencies (communications and navigation) for the departure airport, any enroute airports which are included in the ﬂight plan, and the ﬁnal destination airport. When using the directto function, frequencies are listed for the airport nearest to the starting position and the destination airport.

Figure 1-20 ‘Select Field Type’ Window

4) Press the ENT Key to select the desired data

item and return to the Default NAV Page.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

Displaying the frequency list for the desired ﬂight plan or direct-to airport:

1) Press the small right knob to activate the

cursor on the airport identiﬁer ﬁeld (in the GPS Window).

2) Turn the small

right knob to display the list

of airports (departure, arrival, and enroute) for the ﬂight plan or direct-to. Continue to turn the small right knob until the desired airport is selected.

3) Press the

ENT Key to display the frequency list

for the selected airport.

1-13

SECTION 1

INTRODUCTION

A frequency listed on the NAV/COM Page can be quickly transferred to the standby ﬁeld of the COM Window or the VLOC Window. This time-saving process prevents having to ‘re-key’ a frequency already displayed elsewhere on the screen.

Selecting a communication or navigation frequency:

1) Press the small right knob to activate the

cursor in the GPS Window.

2) Turn the large

right knob to select the desired

frequency from the list.

3) Press the ENT Key to transfer the selected

frequency to the standby ﬁeld in the COM or VLOC Window. COM frequencies automatically go to the standby ﬁeld of the COM Window and navigation frequencies automatically go to the standby ﬁeld of the VLOC Window, regardless of which window is currently highlighted by the cursor.

4) To activate the selected frequency, press the

COM or VLOC Flip-ﬂop Key.

Displaying frequencies for a different airport along the ﬂight plan.

1) Press the small right knob to highlight the

airport identiﬁer ﬁeld.

2) Turn the small

right knob to display the list of

airports within the ﬂight plan (Figure 1-22).

Figure 1-22 Airport Window

3) Continue turning the small right knob to select the desired airport and press the ENT Key.

1-14

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

IFR Procedures

Once the direct-to or ﬂight plan is conﬁrmed, the whole range of instrument procedures is available. Departures (SIDs), arrivals (STARs), non-precision and precision approaches are stored within the NavData card and are available using the PROC (procedures) Key.

To display the Procedures Page (Figure 1-23), press the PROC Key.

Figure 1-23 Procedures Page

The steps required to select and activate an approach, departure, or arrival are identical. This introductory section shows examples of the steps required to select an approach, but keep in mind the same process also applies to departures and arrivals.

Selecting an approach, departure, or arrival:

1) Turn the large option (‘Select Approach?’, ‘Select Arrival?’, or ‘Select Departure?’) from the Procedures Page.

right knob to select the desired

4) For approaches, a window appears (Figure 1-24) to select the desired initial approach ﬁx (IAF) or provide a ‘vectors’ option to select just the ﬁnal course segment of the approach. Turn the small right knob to select the desired option and press the

ENT Key. (The ‘vectors’

option extends the ﬁnal inbound course beyond the ﬁnal approach ﬁx, allowing the pilot to intercept the ﬁnal course segment beyond its normal limits.)

Figure 1-24 Approach Window

5) For departures and arrivals, a window appears to select the desired transition. Turn the small right knob to select the desired option and press the ENT Key.

In the ﬂight plan or direct-to, the departure or arrival airport is replaced with the sequence of waypoints contained within the selected procedure.

2) Press the ENT Key to display a list of

available procedures for the arrival (when using approaches or STARs) or departure (when using SIDs) airport.

3) Turn the small right knob to select the desired procedure and press the ENT Key.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

1-15

SECTION 1

INTRODUCTION

Nearest (NRST) Pages

The NRST Page Group provides detailed information on the nine nearest airports, VORs, NDBs, intersections, and user-created waypoints within 200 nm of the current position. In addition, pages are also provided to display the ﬁve nearest center (ARTCC/FIR) and Flight Service Station (FSS) points of communication, plus alert the pilot to any nearby special-use or controlled airspaces.

There are eight pages available in the NRST group:

• Nearest Airport Page

• Nearest NDB Page

• Nearest User Waypoints Page

• Nearest FSS Page

• Nearest Intersection Page

• Nearest VOR Page

• Nearest ARTCC Page

• Nearest Airspace Page

The communication frequencies and information may both be examined directly from the Nearest Airport Page. As discussed earlier for the NAV/ COM Page, the pilot may also place any displayed frequency into the standby COM or VLOC ﬁeld by highlighting the frequency with the cursor and pressing the ENT Key.

runway

Displaying the NRST pages:

1) If necessary, press and hold the

CLR Key to

select the NAV group and display the Default NAV Page.

2) Turn the large

right knob to select the NRST

Page Group, as indicated by ‘NRST’ appearing in the lower right corner of the screen.

3) Turn the small right knob to select the desired

NRST Page.

Displaying a list of nearby airports:

1) Turn the large

right knob to select the NRST

Page Group and (if needed) the small right knob to select the Nearest Airport Page (Figure 1-25).

Figure 1-25 Nearest Airport Page

2) To scroll through the list, press the small right

knob, then turn the large

right knob (Figure

1-26)

1-16

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

The Nearest Airport Page may be used in conjunction with the Direct-to Key to quickly set a course to a nearby facility in an in-ﬂight emergency. Selecting a nearby airport as a direct-to destination overrides the ﬂight plan or cancels a previously selected direct-to destination. (The pilot still has the option of returning to the ﬂight plan by cancelling the direct-to; see Section 4.1, Cancelling Direct-to Navigation.)

Figure 1-26 Scrolling the Nearest Airport List

Viewing additional information for a nearby airport:

1) Press the small right knob to activate the

cursor.

2) Turn the large

right knob to select the desired

airport from the list.

3) Press the

ENT Key to display waypoint (WPT)

information pages for the selected airport (Figure 1-27).

Selecting a nearby airport as a direct-to destination from the Nearest Airport Page:

1) From the Nearest Airport Page, press the small

right knob to activate the cursor.

2) Turn the large

right knob to select the desired

airport from the list.

3) Press the Direct-to Key.

4) Press the

5) Press the

ENT Key.

ENT Key (again) to navigate to the

nearby airport.

Selecting a nearby airport as a direct-to destination from an Airport Information Page:

1) Press the Direct-to Key.

2) Press the

ENT Key (Figure 1-28).

Figure 1-27 Airport Location Page

4) To display runway and frequency information,

press the small right knob to remove the cursor and turn the small right knob to display the desired information page.

190-00181-00 Rev. E

GNS 530(A) Pilot’s Guide and Reference

Figure 1-28 ‘Activate?’ Highlighted

3) Press the ENT Key again to navigate to the

nearby airport.

1-17

SECTION 1

INTRODUCTION

Nearest (NRST) Airspace Page

The last page in the NRST group, the Nearest Airspace Page (Figure 1-29), provides information for up to nine controlled or special-use airspaces near or in the ﬂight path. Airspace information appears on this page based on the same criteria used for airspace alert messages:

• If the projected course will take the aircraft inside an airspace within the next ten minutes, the message ‘Airspace ahead -- less than 10 minutes’ appears.

• If the aircraft is within 2 nm of an airspace and the current course will take it inside of the airspace, the message ‘Airspace near and ahead’ appears.

• If the aircraft is within 2 nm of an airspace and the current course will not take it inside of the air space, the message ‘Near airspace less than 2nm’ appears.

• If the aircraft has entered an airspace, the message ‘Inside airspace’ appears.

By default, airspace alert messages are turned off. When turned on, the message (MSG) annunciator located directly above the MSG Key ﬂashes to alert the pilot to the airspace message. See Section 10.4, Setup Page: Airspace Alarms for information on enabling airspace alert messages.

Viewing an airspace alert message:

1) Press the MSG Key. The Messages Page

appears with the alert message (Figure 1-30).

Figure 1-30 Messages Page

2) Press the MSG Key again to return to the

previous display.

1-18

Figure 1-29 Nearest Airspace Page

GNS 530(A) Pilot’s Guide and Reference

Note that the airspace alerts are based upon threedimensional data (latitude, longitude, and altitude) to avoid nuisance alerts. The alert boundaries for controlled airspace are also sectorized to provide complete information on any nearby airspace. Additional information about a nearby airspace—such as controlling agency, frequency, and ﬂoor/ceiling limits—is available from the Nearest Airspace Page (Section 8.9).

Viewing additional airspace information:

1) Press the small right knob to activate the

cursor.

2) Turn the large

right knob to select the desired

airspace from the list.

3) Press the ENT Key to view the airspace

information.

190-00181-00 Rev. E

SECTION 1

INTRODUCTION

Flight Plans (FPL)

The GNS 530 lets the pilot create up to 20 ﬂight plans with up to 31 waypoints in each ﬂight plan. Flight plans are created, edited, and activated using the FPL Key. The FPL Page Group includes two pages: the Active Flight Plan Page and the Flight Plan Catalog Page (Figures 1-31 and 1-32). The Active Flight Plan Page provides information and editing features for the ﬂight plan currently in use (referred to as ‘ﬂight plan 00’). The Flight Plan Catalog Page serves as the main page for creating new ﬂight plans, as well as editing or activating previously created ﬂight plans.

Since using ﬂight plans is arguably one of the more complex features of the GNS 530, it will be discussed only brieﬂy here, with focus on creating a new ﬂight plan and activating it to use for navigation. Answers to additional questions about ﬂight plans not found in this brief introduction can be found in Section 5, Flight Plans.

Creating a new ﬂight plan:

1) Press the

2) Turn the small

FPL Key.

right knob to select the Flight

Plan Catalog Page.

3) Press the

MENU Key to display the Flight Plan

Catalog Page Menu (Figure 1-33).

Figure 1-31 Active Flight Plan Page

Figure 1-32 Flight Plan Catalog Page

190-00181-00 Rev. E

Figure 1-33 Flight Plan Catalog Page Menu

4) Turn the large right knob to select ‘Create New Flight Plan?’ and press the ENT Key.

5) The cursor appears on the ﬁrst waypoint identiﬁer ﬁeld (located directly below ‘WAYPOINT’). Use the large and small identiﬁer of the ﬁrst waypoint in the ﬂight plan. (The small knob is used to select the desired letter or number and the large knob is used to move to the next character space.)

6) Press the ENT Key once the identiﬁer has been selected. The cursor moves to the next blank waypoint identiﬁer ﬁeld.

GNS 530(A) Pilot’s Guide and Reference

right knobs to enter the

1-19

SECTION 1

INTRODUCTION

7) Repeat steps 5 and 6, above, until all waypoints for the ﬂight plan have been entered (Figure 1-34).

Figure 1-34 Enter Flight Plan Waypoints

Once the ﬂight plan is created, it may be activated from the Flight Plan Catalog Page Menu. Activating the ﬂight plan places it into ‘ﬂight plan 00’ (a copy of it still resides in the original catalog location) and replaces any ﬂight plan which currently exists in ‘ﬂight plan 00’.

Activating the new ﬂight plan:

1) Press the

MENU Key to display the Flight Plan

Catalog Page Menu.

2) Turn the small

right knob to select ‘Activate

Flight Plan?’ (Figure 1-35) and press the Key

Figure 1-35 Flight Plan Catalog Page Menu

ENT

1-20

GNS 530(A) Pilot’s Guide and Reference

190-00181-00 Rev. E

+ 252 hidden pages