Гармин 430 инструкция по применению на русском - Инструкции, руководства, мануалы

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Page 1
GNS 430/430A P i l o t ’ s G u i d e a n d R e f e r e n c e…
Page 3: Foreword

Web Site Address: www.garmin.com Visit the Garmin web site for the latest © 1998-2003 Garmin Ltd. or its subsidiaries. All rights reserved. Except as expressly updates and supplemental information provided herein, no part of this manual may be reproduced, copied, transmitted, dis- concerning the operation of this and other Garmin products.
Page 4
Garmin GNS 430 is a precision electronic NAVigation AID (NAVAID), any NAVAID can be misused or misinterpreted and therefore become unsafe. Use the GNS 430 at your own risk. To reduce the risk of unsafe operation, carefully review and understand all aspects of this Owner’s Manual and the Flight Manual Supplement, and thoroughly practice basic operation prior to actual use.
Page 5
GNS 430. After installation, the NavData® card will already be installed into the cor- Help us to better support you by completing our rect slot on the front of the unit (see Appendix A). The GNS 430 will be secured in the on-line registration today! Registration ensures you installation rack with the proper wiring connections performed.
Page 6
This Garmin product is warranted to be free from defects in materials or workmanship for one year from the date of purchase. Within this period, Garmin will at its sole option, INTRODUCTION 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 the customer shall be responsible for any transportation costs.
Page 7: Table Of Contents

PART TWO: REFERENCE CONVENTIONS USED IN THIS MANUAL Section 1: Communicating with the GNS 430 ….21 COM and VLOC frequencies A circled number (e.g.,“…
Page 8: Table Of Contents

Section 6: WPT Page Group (Waypoint/database information) ….94 Finding and viewing airport location, runway and frequency data INTRODUCTION Finding and viewing navaid information Creating user-defined waypoints Table of Contents Section 7: NRST Page Group (Nearest airports, etc.).
Page 9: Takeoff Tour

Key and Knob Functions TAKEOFF TOUR The GNS 430 is designed to make operation as simple as possible. The key and knob descriptions on the next three pages provide a general overview of the primary function(s) Key and Knob for each key and knob. This Takeoff Tour section is intended to provide a brief overview Functions of the primary functions of your GNS 430.
Page 10
It is also used to confirm information, such as during power on. reduce the amount of time spent operating the GNS 430 in flight. The large right knob (CRSR) is used to select between the various page groups: NAV, WPT, AUX or NRST. With the on-screen cursor enabled, the large right knob allows you to move the cursor about the page.
Page 11: Bottom Row Keys

OBS mode is selected, you may set the desired course to/from a waypoint using the OBS Page, or an external OBS selector on your HSI or CDI. Whenever the GNS 430 is displaying a list The message key is used to view system messages and to alert you to impor- of information that is too long for the display tant warnings and requirements.
Page 12
GNS 430. Prior to using your GNS 430 for the ﬁ rst time, we recommend that you taxi to a location that is well away from buildings and other aircraft so the unit can collect satellite data without interruption.
Page 13
Checklists Page Once the database has been acknowledged, the instrument panel self-test page will appear. To ensure that your GNS 430 and any connected instruments are working prop- erly, check for the following indications on your CDI/HSI , RMI, external annunciators and other connected instruments: •…
Page 14
“bar graph” readings. This is a good indication that you are receiving signals and a position ﬁ x will be determined. Following the ﬁ rst-time use of your GNS 430, the time required for a position ﬁ x will vary—usually from one to two minutes.
Page 15
(if one is connected). TAKEOFF TOUR If the GNS 430 has not been operated for a period of six months or more, it may have to ‘Search the Sky’ to collect new data. This means the unit is acquiring satellite data to Acquiring Satellites &…
Page 16
While the GNS 430 is acquiring a position, let’s take a minute to dial in the active and standby frequencies you’ll be using for the ﬁ rst phase of your ﬂ ight. The GNS 430’s TAKEOFF TOUR display is divided into separate ‘windows’ (or screen areas), including a COM window,…
Page 17
) to select the Map Page kHz of the desired frequency. To place the standby frequency in the active field, press After the GNS 430 acquires satellites and computes a position, the map page will appear automatically. Data Fields Map Display…
Page 18
To select the desired page within the group, rotate the small right knob ( ) until the * Seven NAV Pages are available when the GNS 430 installation includes connection to desired page is displayed. traffic and/or weather information sources.
Page 19: Aux Group

TAKEOFF TOUR Page Groups (Small right knob to select pages within the group) NAV Group Default NAV NAVCOM Satellite Status VNAV Position WPT Group Airport Frequency User Waypoint Airport Location Airport Runway Airport Approach Airport Arrival Airport Departure Intersection AUX Group Flight Planning Utility Setup 1…
Page 20
Identifier Field Select Direct-To Waypoint Page The GNS 430 can use direct point-to-point navigation to guide you from takeoff to touchdown, even in the IFR environment. Once a destination is selected, the unit will provide speed, course and distance data based upon a direct course from your pres- ent position to your destination.
Page 21
Course Deviation Indicator (CDI) TAKEOFF TOUR User- selectable Active Leg of Default NAV Page Data Fields Flight Plan Default NAV Page During most ﬂ ights, the default NAV, map and NAVCOM pages will be the primary pages used for navigation. The default NAV page displays a graphic course deviation indicator (CDI), the active leg of your ﬂ…
Page 22
2. Rotate the small right knob ( ) to display the list of airports (departure, arrival and en route) for your flight plan or direct-to. Continue to rotate the small right knob ( ) until the desired TAKEOFF TOUR airport is selected. 3.
Page 23
Once the direct-to or ﬂ ight plan is conﬁ rmed, the whole range of instrument pro- cedures is available to you. Departures (SIDs), arrivals (STARs), non-precision and TAKEOFF TOUR precision approaches are stored within the NavData card and available using the (procedures) key.
Page 24: Nearest Airports

From page 10 you may recall that one of the main page groups, NRST, provides list- ings for nearest airports or other facilities. The NRST group provides detailed information TAKEOFF TOUR on the nine nearest airports, VORs, NDBs, intersections and user-created waypoints within 200 nautical miles of your current position.
Page 25
TAKEOFF TOUR To view additional information for a nearby airport: 1. Press the small right knob ( ) to activate the cursor. Nearest Airports: Additional Information and Direct-to 2. Rotate the large right knob ( ) to select the desired airport from the list. 3.
Page 26: Special-Use/Controlled Air Space

The last page in the NRST group, the nearest airspace page, provides information for up to nine controlled or special-use airspaces near or in your ﬂ ight path. Airspace TAKEOFF TOUR information appears on this page based upon the same criteria used for airspace alert mes- sages.
Page 27
The GNS 430 lets you create up to 20 ﬂ ight plans, with up to thirty-one waypoints in each ﬂ ight plan. Flight plans are created, edited and activated using the key. The TAKEOFF TOUR FPL page group includes two pages: the active ﬂ ight plan page and the ﬂ ight plan catalog.
Page 28
2. Rotate the small right knob ( ) to select “Activate Flight Plan?” and press This Takeoff Tour is intended to provide a brief introduction of the GNS 430’s major features. The Reference section of this manual describes these features, and others, in additional detail.
Page 29: Section 1: Communicating With The Gns 430

ﬂ ying together in one panel-mounted unit. The GNS 430’s COM radio operates in the aviation voice band, from 118.000 to 136.975 MHz, in 25 kHz steps (default). For Euro- pean operations, a COM radio conﬁ…
Page 30
COM Window and Tuning Communication frequencies are selected with the tuning cursor in the standby COM Tuning Cursor frequency ﬁ eld, and using the small ( ) and large ( ) left knobs to dial in the desired Active/Standby Freqs frequency.
Page 31
Sections 5 and 8 (beginning on pages 66 and 131). Auto-Tuning The GNS 430’s auto-tune feature allows you to quickly select any database frequency Cursor in VLOC window allows for VOR and ILS operations. See Section 8, starting on in the GPS window as your standby frequency.
Page 32
2. Press the small right knob ( ) momentarily to place the cursor on the airport identifier field of the first airport in the list. If you wish to select another airport, rotate the large right knob ( to highlight the desired airport. 3.
Page 33
To select a COM frequency for any airport in your flight plan: 1. Select the NAVCOM page from the NAV page group. (See page 27, or press and hold then rotate the small right knob, , until the NAVCOM page appears.) Auto-Tuning from 2.
Page 34: Emergency Channel

Stuck Microphone As mentioned earlier, whenever the GNS 430 is transmitting, a ‘TX’ indication will appear in the COM window. If the microphone is stuck or accidentally left in the keyed position, or continues to transmit after the key is released, the COM transmitter will automatically timeout (or cease transmitting) after 35 seconds of continuous broadcasting.
Page 35: Section 2: Nav Page Group (Gps Navigation)

Page Groups Main Page Groups NAV Page Group The GNS 430’s main pages are divided into groups: NAV, WPT, AUX and NRST. While viewing any of these pages, selection of another page is a simple selection process using the small ( ) and large ( ) right knobs.
Page 36
(an up arrow) the waypoint or if you have passed the waypoint (a down arrow). DME Arc to the right The GNS 430 always navigates TO a waypoint unless the OBS Left-hand Holding Pattern switch is set (preventing automatic waypoint sequencing), or you have passed the last waypoint in your flight plan.
Page 37
Directly below the CDI appears the active leg of your ﬂ ight plan, or the direct-to des- tination when using the D key. This will automatically sequence to the next leg of your NAV PAGES ﬂ ight plan as you reach each interim waypoint. If no ﬂ ight plan or direct-to destination has been selected, the destination ﬁ…
Page 38: Restoring Factory Settings

A “Crossﬁ ll?” option is also provided for the default NAV page. This option allows you to transfer a direct-to destination or ﬂ ight plan to a second Garmin 400 Series unit. See page 58 and 142 for additional details on using the “Crossﬁ ll?” option.
Page 39
Different symbols are used to distinguish between waypoint types. The identiﬁ ers for any on-screen waypoints can also be displayed. (By default the identiﬁ ers are enabled). NAV PAGES Special-use and controlled airspace boundaries appear on the map, showing the indi- vidual sectors in the case of Class B or Class C airspace.
Page 40
An autozoom feature is available which will automatically adjust from an en route scale of 2000 through each lower scale, stopping at a scale of 1.0 as you approach your destina- NAV PAGES tion waypoint. The autozoom feature is turned on/off from the map setup page described on page 36.
Page 41: Map Panning

Map Panning Another map page function is panning, which allows you to move the map beyond its NAV PAGES current limits without adjusting the map scale. When you select the panning function — by pressing the small right knob — a target pointer will ﬂ ash on the map display. Map Page A window will also appear at the top of the map display showing the latitude/longitude position of the pointer, plus the bearing and distance to the pointer from your present…
Page 42: Airspace Information On The Map

Map Direct-To To designate an on-screen airport, navaid or user waypoint as your direct-to NAV PAGES destination: 1a. Use the panning function (see previous page) to place the target pointer on a waypoint. Map Page 2. Press to display the select direct-to waypoint page, with the selected waypoint already listed.
Page 43
Many of the GNS 430’s functions are menu driven. Each of the main pages has an options menu, allowing you to custom tailor the corresponding page to your preferences NAV PAGES and/or select special features which speciﬁ cally relate to that page. A map page options menu provides additional settings to customize the map page and additional features related speciﬁ…
Page 44
To change a map setup feature: 1. Rotate the large right knob ( ) to highlight “Setup Map?” and press NAV PAGES 2. To change map orientation, rotate the small right knob ( ) to select “Map” and press Rotate the large right knob ( ) to highlight the “Orientation”…
Page 45: Distance Measurements

Distance Measurements The “Measure Dist?” option provides a quick, easy method for determining the bear- NAV PAGES ing and distance between any two points on the map display. To measure bearing and distance between two points: Map Page Options 1. Rotate the large right knob ( ) to highlight “Measure Dist?”…
Page 46
The on-screen traffic information will occupy two data fields, leaving room to display only two additional data types. Traffic information is only available when the GNS 430 installation includes connection to traffic information sources. See 400 Series Pilot’s Guide Addendum, part number 190-00140-13.
Page 47: Navcom Page

NAVCOM Page NAV PAGES Assigned Departure, Frequency and Enroute or Usage Information NAVCOM Page Arrival Airport (when applicable) Frequency Type Third Page in NAV group The third NAV page is the NAVCOM (navigation communications) page. The NAV- COM page provides a list of the airport communication and navigation frequencies at your departure, enroute and arrival airports.
Page 48
2a. Rotate the large right knob ( ) to move the cursor through the list of frequencies. If there are more frequencies in the list that can be displayed on the screen, a scroll bar along the right- NAV PAGES hand side of the screen will indicate which part of the list is currently being displayed.
Page 49: Position Page

Position Page NAV PAGES The position page (the fourth NAV page) displays your present position (by default, in latitude and longitude) and altitude. The position page also displays your current track, Position Page ground speed, time and a reference waypoint ﬁ eld. These ﬁ elds are user-selectable to conﬁ…
Page 50
NAV PAGES To change the user-selectable data fields: 1. Press to display the position page options menu. Position Page 2a. Rotate the large right knob ( ) to highlight “Change Fields?” and press 3a. Rotate the large right knob ( ) to highlight the data field you wish to change.
Page 51
6. To select between “bearing FROM” or “bearing TO” to the reference waypoint, rotate the small NAV PAGES right knob ( ) to select the desired bearing reference and press 7. Press the small right knob ( ) momentarily to remove the cursor from the page. Position Page 8.
Page 52: Satellite Status Page

Satellite Status Page The satellite status page (the ﬁ fth NAV page) provides a visual reference of GPS NAV PAGES receiver functions, including current satellite coverage, GPS receiver status and position accuracy. The satellite status page is helpful in troubleshooting weak (or missing) signal Satellite Status Page levels due to poor satellite coverage or installation problems.
Page 53
(solid signal strength bar). NAV PAGES Once the GPS receiver has determined your position, the GNS 430 will indicate your position, track and ground speed on the other navigation pages. The GPS receiver status ﬁ…
Page 54: Vertical Navigation Page

Section 10 on page 163. Vertical Navigation Page The GNS 430’s vertical navigation page (the last NAV page) allows you to create a three-dimensional proﬁ le which guides you from your present position and altitude to a ﬁ nal (target) altitude at a speciﬁ ed location. This is helpful when you’d like to descend to a certain altitude near an airport or climb to an altitude before reaching a route or direct-to waypoint.
Page 55
NAV PAGES Vertical Navigation TIME AND DISTANCE TO PROFILE (VNAV) CURRENT ALTITUDE AND POSITION TARGET ALTITUDE AND POSITION DISTANCE TO TARGET AIRPORT To create a vertical navigation profile: 1. Press the small right knob ( ) to activate the cursor. 2.
Page 56
8. The default profile utilizes a 400 foot-per-minute descent rate. To change the rate, rotate the large right knob ( ) to highlight the “VS Profile” field and use the small ( ) and large ( NAV PAGES right knobs to enter a new rate. Press when finished.
Page 57: Section 3: Direct-To Navigation

DIRECT-TO Direct-To Navigation Selecting a The GNS 430’s direct-to function provides a quick method of setting a course to a Destination destination waypoint. Once a direct-to is activated, the GNS 430 will establish a point- to-point course line (great circle) from your present position to the selected direct-to destination.
Page 58: Selecting A Destination By Facility Name Or City

) right knobs to enter the facility name or city location of the identifier(s) for any matching entries will appear desired destination waypoint. As you spell the facility name or city, the GNS 430’s Spell’N’Find on the top line of the page.
Page 59: Using The

Selecting a Destination from the Active Flight Plan DIRECT-TO If you’re navigating an active ﬂ ight plan, any waypoint contained in the ﬂ ight plan may be selected as a direct-to destination from the select direct-to waypoint page. (See section 4, beginning on page 54, for more information on ﬂ…
Page 60
Shortcuts DIRECT-TO Shortcuts are available when using the key, allowing you to bypass the use of Direct-To the small ( ) and large ( ) right knobs to enter the destination waypoint’s identiﬁ er. A direct-to can be performed from any page displaying a single waypoint identiﬁ er (such as Shortcuts the WPT pages for airports and navaids) by simply pressing .
Page 61: Specifying A Course To A Waypoint

430 will resume navigating the flight plan along the closest leg. Specifying a Course to a Waypoint Whenever you perform a direct-to, the GNS 430 will set a direct great circle course to your selected destination. You can also manually deﬁ ne the course to your destination, using the “CRS”…
Page 62: Section 4: Flight Plans ( Key And Fpl

Flight Plans FLIGHT PLANS The GNS 430 lets you create up to 20 different ﬂ ight plans, with up to 31 waypoints in Creating Flight Plans each ﬂ ight plan. The ﬂ ight plan page group consists of two pages, accessed by pressing the key.
Page 63: Flight Plan Editing

Flight Plan Editing To add a waypoint to an existing flight plan: FLIGHT PLANS 1. Press and rotate the small right knob ( ) to display the flight plan catalog. Editing Flight Plans 2. Press the small right knob ( ) to activate the cursor.
Page 64: Activating Flight Plans

To change the comment line for an existing flight plan: FLIGHT PLANS 1. From the flight plan catalog, press the small right knob ( ) to activate the cursor. 2. Rotate the large right knob ( ) to highlight the desired flight plan and press 3a.
Page 65: Copying Flight Plans

Copying Flight Plans FLIGHT PLANS If you want to save a ﬂ ight plan currently located in “ﬂ ight plan 0”, be sure to copy it to an open catalog location (1-19) before the ﬂ ight plan is cancelled, overwritten or erased. Copying/Deleting To copy a flight plan to another flight plan catalog location: Flight Plans…
Page 66: Flight Plan Catalog Options

Crossfill? allows you to transfer a direct-to destination, the active flight plan, any stored flight plan or user waypoints to a second 400-Series or 500-Series Garmin unit. Some crossfill operations can be done automatically. If both units are set to “auto”, a change in the direct-to destination or active flight plan on one unit will also…
Page 67: Active Flight Plan

Copy Flight Plan? allows you to copy the selected flight plan to a new flight plan location, as described on page 57. The copy function is useful for duplicating an exist- FLIGHT PLANS ing flight plan before making changes. Delete Flight Plan? allows you to remove the selected flight plan from memory, as Active Flight Plan described on page 57.
Page 68: Active Flight Plan Options

3. A confirmation window will appear. With “Activate?” highlighted, press Crossfill? allows you to transfer the active flight plan between two 400- or 500-series Garmin units in a dual unit installation. See pages 58 and 142 for additional information on this feature.
Page 69
Copy Flight Plan? copies the active flight plan to a flight plan catalog location, as described on page 57. The copy function is useful for duplicating the active flight FLIGHT PLANS plan before making changes. Invert Flight Plan? reverses the active flight plan. See description of “Invert & Active Flight Activate FPL”…
Page 70
(SID) for the departure airport, or replace the current departure with a new selection. When using a direct-to, the GNS 430 will use the nearest airport as a reference when displaying available departures. See page 66 for information on selecting departures using the key.
Page 71
4. The GNS 430 will display the bearing (BRG) and distance (DIST) to the closest point along the flight plan, from the selected reference waypoint.To create a user waypoint at this location and add it to the flight plan, highlight “Load?” and press .
Page 72
Shortcuts FLIGHT PLANS A number of shortcuts are available to save time when using the active ﬂ ight plan page. These shortcuts speed the process of removing approaches, departures and arrivals, and aid in selecting a speciﬁ c ﬂ ight plan leg for navigation guidance. Active Flight On the preceding page, options to remove approaches, departures and arrivals were Plan Editing…
Page 73
On page 60 the “Activate Leg?” option is discussed, which allows you to specify which leg of the ﬂ ight plan will currently be used for navigation guidance. A shortcut also exists FLIGHT PLANS for this operation, using the key. To activate a specific leg of the active flight plan: Active Flight Plan Leg Selection…
Page 74: Section 5: Approaches, Departures And Arrivals ( Key)

All available approaches are stored on your Jeppesen NavData® card, and are automatically updated when you replace the card with a new one. Subscription information for NavData cards is included in your GNS 430 package.
Page 75
Not all approaches in the database are approved for GPS use. As you select an approach, a “ ” designation to the right of the proce- PROCEDURES dure name indicates the procedure can be ﬂ own using the GPS re- ceiver.
Page 76: Basic Approach Operations

ﬁ x (IAF) — or may be ﬂ own with a the approach vectors-to-ﬁ nal transition. Approach operations on the GNS 430 will typically begin with the same basic steps: 1. Select the destination airport using the key, or as the last waypoint in the active flight plan.
Page 77: Approaches With Procedure Turns

The procedure turn portion of an approach is stored as one of the legs of the approach. For this reason, the GNS 430 requires no special operations from the pilot — other than ﬂ ying the procedure turn itself — beyond what is required for any other type of approach.
Page 78: Flying The Procedure Turn

Flying the Procedure Turn PROCEDURES 1. Within 30 nautical miles of the destination airport, the GNS 430 will switch from “enroute” mode to “terminal” mode (as indicated in the Procedure Turn lower left corner of the screen). The switch to…
Page 79
8. As the CDI needle starts to center, make a right turn to 025°—the final approach course. 9. Within 2.0 nautical miles of the FAF (LYH), the GNS 430 will switch from terminal mode to “approach” mode. CDI scaling will be tightened from 1.0 to 0.3 nautical mile, full scale deflection.
Page 80: Flying The Missed Approach

MAP and MAHP are the same waypoint. 2. Follow the missed approach procedures, as published on your approach plate, for proper climb and heading instructions. The GNS 430 will guide you to the holding pattern, along the 053° radial from LYH VOR.
Page 81: Flying An Approach With A Hold

Example 4a. The GNS 430 will provide course guidance only on the inbound side of the holding pattern. When leaving the holding pattern to re-fly the approach (or another approach) press the key to “Select…
Page 82
As you make the turn inbound, “SUSP” will be cancelled and the GNS 430 will return to automatic sequencing. If you need to lose extra altitude or speed by going around the…
Page 83
12. At 2.0 nautical miles from the FAF (DEPOY intersection), the Approach with Hold GNS 430 will switch from terminal mode to approach mode. CDI Example scaling will be tightened from 1.0 to 0.3 nautical mile, full scale deflection.
Page 84
Flying a DME Arc Approach Billard Muni (Topeka, KS) PROCEDURES VOR or GPS Rwy 22 The GPS overlay for a DME arc approach uses additional Jeppesen- provided waypoints to deﬁ ne the arc. DME Arc These waypoints are indicated by “D” Approach Example as the ﬁ…
Page 85
CDI (or HSI) using the OBS knob and initiate a standard rate turn to this course heading. 8. At 2.0 nautical miles from the FAF (TOP VOR), the GNS 430 will switch from terminal mode to approach…
Page 86
{continued} DO NOT USE FOR PROCEDURES NAVIGATION 9. As you approach the FAF , “NEXT DTK 214°” will appear in the lower right corner of the screen. Select this course on the DME Arc CDI (or HSI) using the OBS knob and turn Approach Example to the final course segment (FAF to MAP) heading.
Page 87: Vectors To Final

Let’s take a second look at the “VOR 22” approach into Billard Municipal. Instead of following the DME arc, ATC tells you to expect vectors onto the ﬁ nal approach course. There are several ways to select “vectors to ﬁ nal” with the GNS 430. The ﬁ rst two op- Vectors-To-Final…
Page 88
ATC vectors result in a rectangular course to intercept ﬁ nal, as follows: 1. Within 30 nautical miles of KTOP, the GNS 430 will switch from enroute mode to terminal mode and the CDI scale will transition from 5.0 to 1.0 nautical miles, full scale deflection.
Page 89
PROCEDURES approach course. At 2.0 nautical miles from the FAF (TOP VOR), the GNS 430 will switch from terminal mode to approach mode. CDI scaling will be tightened from 1.0 Vectors-To-Final to 0.3 nautical mile, full scale deflection.
Page 90: Course From Fix Flight Plan Legs

Certain approach, departure, and arrival procedures in the Jeppesen database contain course from ﬁ x ﬂ ight plan legs. The GNS 430 is able to load these legs into the ﬂ ight plan along with the rest of the procedure data, and to provide navigation along these legs.
Page 91
PROCEDURES 5. Within 2.0 nautical miles of the FAF (THERO), the GNS 430 will switch from terminal mode to approach mode. (“APR” will appear in the lower left corner of the screen—replacing “TERM”.) CDI scaling will be Course From Fix tightened from 1.0 to 0.3 nautical mile, full scale deflection.
Page 92
NAV page. The timer automatically resets on each outbound and inbound portion of the holding pattern. 7. Note that the GNS 430 again displays “SUSP” above the key. Automatic waypoint sequencing is suspended at the missed approach holding point.
Page 93
(HFD VOR). The actual desired track (DTK) will depend on your ground speed and distance from HFD VOR. 4. Once the key is pressed, the GNS 430 will automatically sequence to each waypoint along the remainder of the departure route, including the selected transition.
Page 94: Ils Approaches

VLOC as you intercept the ﬁ nal approach course. When the ILS approach is activated, the GNS 430 will automatically switch within 1.2 nautical miles left or right of the ﬁ nal approach course. This switch can take place anywhere from 2.0 to 15.0 nautical miles from the FAF.
Page 95
Selecting an ILS Approach Flagstaff (AZ) Pulliam PROCEDURES ILS DME Rwy 21 For this example, we’ll use a ﬂ ight from Laughlin Bullhead (Arizona) International to Flagstaff ILS Approach Pulliam (KFLG) and select Example the ILS runway 21 approach. “SHUTR” intersection will be selected as the IAF, which will include an outbound leg and a procedure turn.
Page 96
(step #4 below), automatic selection of “VLOC” will not occur. 1. Within 30 nautical miles of KFLG, the GNS 430 will switch from enroute mode to terminal mode and the CDI scale will transition from 5.0 to 1.0 nautical miles, full scale deflection.
Page 97
NAVIGATION PROCEDURES 8. Turn right to a heading of 075° to initiate the procedure turn. The GNS 430 will not guide you through the turn. (The procedure turn is displayed ILS Approach on the map page and indicated as the active leg on the default NAV and active flight plan pages.)
Page 98
{continued} 12. Also as you approach SHUTR, a DO NOT USE FOR PROCEDURES waypoint alert (“NEXT DTK 210°”) will NAVIGATION appear in the lower right corner of the screen. ILS Approach 13. As you cross SHUTR, the destination Example sequences to the MAP (“RW21”, the runway threshold).
Page 99
• The active leg (or the portion of the approach currently in use) is depicted in Information magenta on the Map Page. As you ﬂ y the approach, the GNS 430 will automati- cally sequence through each leg of the approach unless “SUSP” appears above the OBS key.
Page 100
• When an ILS approach is ﬁ rst selected and “loaded” (or “activated”), the ILS frequency is automatically placed in the standby ﬁ eld. In order to ﬂ y the ﬁ nal course PROCEDURES segment of the ILS approach, you must place the ILS frequency in the active fre- quency ﬁ…
Page 101
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Page 102: Section 6: Wpt Page Group (Waypoint/Database Information)

WPT Page Group WPT Page Group Section 2 introduced the GNS 430’s main page groups—NAV, WPT, AUX, NRST— and described each page in the NAV group. This second page group (WPT) provides in- formation for the thousands of airports, VORs, NDBs, intersections, runways, frequencies and procedures stored on your Jeppesen NavData®…
Page 103
The WPT page group includes ten pages. While viewing any WPT page, rotate the small right knob ( ) to select a different WPT page. The ﬁ rst six pages provide detailed WPT PAGES information for the selected airport: location, runways, frequencies, approaches, arrivals, and departures.
Page 104: Duplicate Waypoints

) and large ( ) right knobs, the GNS 430’s Spell’N’Find feature will select the first entry in the database based upon the charac- ters you have entered up to that point. 3a. Continue rotating the small right knob ( ) to scroll through any additional database listings for the selected facility name or location.
Page 105: Airport Location Page

Airport Location Page Airport Identifier, WPT PAGES Facility Name and Symbol and Type Location (city) Airport Location Field Elevation, Latitude/Longitude Available Fuels and Position Airspace Type Best Available First Page Approach and in WPT group Radar Coverage The airport location page displays the latitude, longitude, and elevation of the selected airport.
Page 106: Airport Runway Page

Airport Runway Page Airport Identifier, Runway WPT PAGES Symbol and Type Designations Airport Runways Runway Length Map Image and Width Runway Surface Second Page and Lighting in WPT group The airport runway page displays runway designations, length, surface type and lighting for the selected airport.
Page 107: Airport Frequency Page

The following descriptions and abbreviations are used on the airport runway page: • Type— Usage type: Public, Military or Private WPT PAGES • Surface— Runway surface types include: Hard, Turf, Sealed, Gravel, Dirt, Soft, Unknown or Water Airport Frequencies • Lighting— Runway lighting types include: No Lights, Part Time, Full Time, Unknown or Frequency (for pilot-controlled lighting) Airport Frequency Page…
Page 108
2a. Rotate the large right knob ( ) to scroll through the list, placing the cursor on the desired WPT PAGES frequency. If there are more frequencies in the list than can be displayed on the screen, a scroll bar along the right-hand side of the screen will indicate where you are within the list. 3a.
Page 109
The following descriptions and abbreviations are used on the airport frequency page: • Type— Usage type: Public, Military or Private WPT PAGES • Frequency— Communication frequencies which may include restrictions: Approach Arrival Class B Airport Frequencies Class C Departure Terminal TRSA Communication frequencies without restrictions: ATIS…
Page 110: Airport Approach Page

Airport Approach Page Approach WPT PAGES Airport Identifier, Procedure Name Symbol and Type Airport Approaches Transitions: IAFs, Feeder Routes and Map Image Vectors-to-Final Fourth Page in WPT group The airport approach page shows the available approach procedures for the selected airport.
Page 111: Airport Approach Page Options

Not all approaches in the database are approved for GPS use. As you select an approach, a “ ” designation to the right of WPT PAGES the procedure name indicates the procedure can be flown using the GPS receiver. Some procedures will not have this designa- Airport Approaches tion, meaning the GPS receiver may be used for supplemental navigation guidance only.
Page 112: Airport Arrival Page

Airport Arrival Page Arrival Procedure WPT PAGES Airport Identifier, Name Symbol and Type Airport Arrivals Transitions Map Image Runways Associated with Arrival Fifth Page in WPT group The airport arrival page shows the available Airport Standard Terminal Arrival (STAR) procedures for the selected airport. Where multiple transitions or runways are associ- ated with the arrival procedure, that information may also be displayed.
Page 113: Airport Arrival Page Options

7. Rotate the small right knob ( ) to display a window of available runways. Continue rotating the small right knob ( ) to select the desired runway. (“ALL” may appear in the runway field, WPT PAGES indicating the arrival procedure applies to all runways. For airports with parallel runways, “B” may appear at the end of the runway designation to indicate the arrival procedure applies to both runways.) Airport Arrivals…
Page 114: Airport Departure Page

Airport Departure Page Departure WPT PAGES Procedure Name Airport Identifier, Symbol and Type Airport Departures Runways Associated with Departure Map Image Transitions Sixth Page in WPT group The airport departure page shows the available Airport Standard Instrument Depar- ture (SID) procedures for the selected airport. Where multiple runways or transitions are associated with the departure procedure, that information may also be displayed.
Page 115: Airport Departure Page Options

{continued} 5. Rotate the small right knob ( ) to display a window of available runways. Continue rotating WPT PAGES the small right knob ( ) to select the desired runway. (“ALL” may appear in the runway field, indicating the departure procedure applies to all runways. For airports with parallel runways, “B” may appear at the end of the runway designation to indicate the departure procedure applies to Airport Departures both runways.)
Page 116: Intersection Page

Intersection Page WPT PAGES Nearest VOR Intersection and Symbol Identifier and Symbol Intersections Radial and Region/Country Distance from Nearest VOR Latitude/Longitude Position Seventh Page in WPT group The intersection page displays the latitude, longitude, region and country for the selected intersection. The intersection page also displays the identiﬁ er, radial and distance from the nearest VOR, VORTAC or VOR/DME.
Page 117
NDB Page Facility Name, WPT PAGES City and Region/ NDB Identifier Country and Symbol NDBs Frequency and Weather Broadcast Latitude/Longitude Indication Position Eighth Page in WPT group The NDB page displays the facility name, city, region/country, latitude and longitude for the selected NDB. The NDB page also displays the frequency and a weather broad- cast indication (if applicable).
Page 118
VOR Page WPT PAGES Magnetic Variation VOR Identifier VORs and Symbol Frequency and Facility Name, Weather Broadcast City and Region/ Indication Country Latitude/Longitude Ninth Page Position in WPT group The VOR page displays the facility name, city, region/country, magnetic variation, latitude and longitude for the selected VOR.
Page 119: User Waypoint Page

In addition to the airport, VOR, NDB and intersection information contained in your Jeppesen NavData® card, the GNS 430 allows you to store up to 1,000 user-defined waypoints. The user waypoint page displays the waypoint name (up to five characters long), identifier and radial from two reference waypoints, distance from one reference waypoint, along with the user waypoint’s latitude/longitude position.
Page 120: Creating User Waypoints

The following descriptions and abbreviations appear on the user waypoint page: WPT PAGES • REF WPT— Reference waypoint identiﬁ er (name) • RAD— Radial from reference waypoint, in degrees magnetic or degrees true (depending upon unit conﬁ guration) Creating User Waypoints •…
Page 121
8. Press the small right knob ( ) to remove the flashing cursor. The GNS 430 allows you to create a new user waypoint at a defined radial and distance from your present position. To reference your pres- ent position, follow the steps above, but press c in step #4. “P.POS”…
Page 122: Modifying User Waypoints

Creating User Waypoints from the Map Page WPT PAGES The map page and panning target pointer (see page 33) provide a quick means of sav- ing your present position as a user-deﬁ ned waypoint. Creating / Modifying To capture and save your present position as a user waypoint: User Waypoints 1a.
Page 123
If you attempt to modify or delete a waypoint which is currently a direct-to waypoint or the current “from” or “to” waypoint in the active flight plan, the GNS 430 will alert you with the “Can’t change an active waypoint” or “Waypoint is active and can’t be deleted” message. You must first cancel the direct-to or remove the waypoint(s) from the active flight plan before modifying or deleting the waypoint(s).
Page 124: User Waypoint Page Options

User Waypoint Page Options WPT PAGES The following user waypoint page options are available by pressing the m key: View User Waypoint List? displays a list of all user waypoints currently stored in mem- Deleting Waypoints ory. User Waypoint List To view a list of all user waypoints: 1.
Page 125
To review and/or modify a user waypoint from the user waypoint list: WPT PAGES 1. Select the user waypoint list, as described on page 116. 2. Rotate the large right knob ( ) to highlight the desired user waypoint. Modifying / Deleting 3a.
Page 126
To delete all user waypoints from memory: WPT PAGES 1. Select the user waypoint list, as described on page 116. 2. Press to display an options window for the user waypoint list. Deleting All 3. With “Delete All User Waypoints” highlighted, press User Waypoints 4.
Page 127: Section 7: Nrst Page Group (Nearest Airports, Etc.)

NRST Page Group NRST Page Group Section 2 introduced the GNS 430’s main page groups—NAV, WPT, AUX, NRST— and described each page in the NAV group. This fourth page group (NRST) provides detailed information for the nine nearest airports, VORs, NDBs, intersections and user waypoints within 200 nm of your current position.
Page 128
Not all nine nearest airports, VORs, NDBs, intersections or user waypoints can be displayed on the corresponding NRST page at one time. The nearest airport page displays NRST PAGES detailed information for three nearest airports, with a scroll bar along the right-hand side of the page indicating which part of the list is currently being viewed.
Page 129: Navigating To A Nearby Waypoint

Navigating to a Nearby Waypoint The NRST pages can be used in conjunction with the GNS 430’s direct-to NRST PAGES function to quickly set a course to a nearby facility. This feature can be a real time saver compared to retrieving information from the database using the WPT pages. More Nearest Airports importantly, it instantly provides navigation to the nearest airport in case of an in-ﬂ…
Page 130
The nearest airport page can be conﬁ gured to exclude shorter runways or undesirable runway surface types, so that the corresponding airports do not appear on the list. You NRST PAGES may wish to use this feature to exclude seaplane bases or runway lengths which would be difﬁ…
Page 131: Nearest Intersection Page

To view additional information for a nearby airport: NRST PAGES 1. Select the nearest airport page, using the steps outlined on page 119. 2. Press the small right knob ( ) to activate the cursor. Nearest VORs, NDBs 3. Rotate the large right knob ( ) to scroll through the list, highlighting the identifier of the desired airport.
Page 132
VOR Frequency VOR Identifier NRST PAGES and Symbol Scroll Bar Nearest VORs Bearing To and Fourth Page Distance To in NRST group To quickly tune a VOR’s frequency from the nearest VOR page: 1. Select the nearest VOR page, using the steps outlined on page 119. 2.
Page 133: Nearest User Waypoint Page

Nearest User Waypoint Page The nearest user waypoint page displays the name, bearing and distance to the nine NRST PAGES nearest user waypoints (within 200 nautical miles of your present position). Nearest Center (ARTCC) Page Nearest ARTCC The nearest center page displays the facility name, bearing to and distance to the ﬁ ve nearest ARTCC points of communication (within 200 nautical miles of your present posi- tion).
Page 134
Nearest Flight Service Station (FSS) Page The nearest flight service station page displays the facility name, bearing to and NRST PAGES distance to the five nearest FSS points of communication (within 200 nautical miles of your present position). For each FSS listed, the nearest flight service station page also Nearest FSS indicates the frequency(s) and may be used to quickly tune the COM transceiver to the FSS’s frequency.
Page 135: Nearest Airspace Page

5. Press to place the selected frequency in the standby field of the COM or VLOC window. 6. Press , as appropriate, to activate the selected frequency. NRST PAGES 7. Press the small right knob ( ) to remove the flashing cursor. Nearest Airspaces Nearest Airspace Page The last page in the NRST group, the nearest airspace page, will alert you to as many…
Page 136
To view an airspace alert message: 1a. When the message annunciator above the key flashes, press NRST PAGES 2. Press again to return to the previous page. Nearest Airspaces Once you have been provided an airspace alert message, detailed information con- cerning the speciﬁ…
Page 137
“Done?” Field (return to Airspace Name NRST PAGES previous page) and Type “Frequency?” Field Nearest Airspaces Status and (display frequency page) Time to Entry Floor/Ceiling Limits To view and quickly tune the frequency for a controlling agency: 1. Follow steps #1 through #4 on the previous page to display the airspace page for the desired controlled or special use airspace.
Page 138
The airspace page displays (and airspace alert messages are provided for) the following airspace types: NRST PAGES • Alert • Caution • Class B • Class C Nearest Airspaces • CTA • Danger • MOA • Prohibited • Restricted • TMA •…
Page 139: Section 8: Vloc (Vor/Localizer/Glideslope) Receiver Operations

Receiver Operations Ident, Volume and Tuning The GNS 430 includes digitally-tuned VOR/localizer and glideslope receivers with the desired frequency selected on a VLOC window, along the left-hand side of the display. Frequency selection is performed by pressing the small left knob…
Page 140
The tuning cursor will normally appear in the COM VLOC RECEIVER window, unless placed in the VLOC window by press- . When the tuning cursor is in the VLOC window, it will automatically return to the COM window after 30 Auto-tuning seconds of inactivity.
Page 141
When selecting a VOR or ILS approach, manual tuning of the VLOC receiver is not required. Once the approach procedure is “Loaded” or “Activated”, the GNS 430 will au- tomatically place the proper frequency in the standby ﬁ eld of the VLOC window. If you wish to use this frequency, simply press to activate the frequency.
Page 142
“Yes?” and press CDI Key The GNS 430’s C key is used to couple the GPS or VLOC receiver to the external CDI (or HSI). When the external CDI (or HSI) is being driven by the GPS receiver, “GPS” will appear at the bottom left corner of the page, directly above the C key.
Page 143: Section 9: Aux Page Group (Flight Planning And Unit Settings)

AUX Page Group AUX Page Group Section 2 introduced the GNS 430’s main page groups—NAV, WPT, AUX, NRST— and described each page in the NAV group. The third page group (AUX) allows you to change unit settings, customizing operation to your preferences. The AUX pages also pro- vide E6B functions—such as trip planning, fuel planning, density altitude, true airspeed…
Page 144: Flight Planning Page

The ﬂ ight planning page provides access (via “menu options”) to E6B functions for fuel planning, trip planning, density altitude/true airspeed/winds aloft calculations and a “Crossﬁ ll” function to transfer ﬂ ight plans/user waypoints to a second GNS 430. When a menu option is selected, the corresponding page will appear providing additional infor- mation and features.
Page 145
Scheduler— displays reminder messages (such as “Change oil”, “Switch fuel tanks”, “Overhaul”, etc.). One-time, periodic, and event-based messages are allowed. One-time messages will appear once the timer expires and will reappear each time the GNS 430 is powered on, until the message is deleted. Periodic messages will automatically reset to The “Flight Plan?”…
Page 146
AUX PAGES Flight Planning Page: Fuel Planning To perform fuel planning operations: Flight Planning 1. Select “Fuel Planning” from the flight planning page, using the steps described on page 136. 2. The current fuel planning “mode” is displayed at the top of the page: “POINT TO POINT” or “FPL”…
Page 147
8. With all variables entered, the following information will be provided: AUX PAGES • REQ— Quantity of fuel required • LFOB— Left-over fuel on board Flight Planning • LRES— Left-over fuel reserve time • EFF— Efficiency, expressed in distance per fuel units (e.g. nautical miles per gallon) •…
Page 148
Flight Planning Page: Trip Planning AUX PAGES To perform trip planning operations: Flight Planning 1. Select “Trip Planning” from the flight planning page, using the steps described on page 136. 2. The current trip planning “leg mode” is displayed at the top of the page: “POINT TO POINT” or “FPL LEG”…
Page 149
Flight Planning Page: Density Alt / TAS / Winds AUX PAGES To calculate density altitude, true airspeed, winds aloft: 1. Select “Density Alt / TAS / Winds” from the flight planning page, using the steps described on page 136. Flight Planning 2.
Page 150
“Auto” or “Manual”. “Auto” will automatically transfer any selection of (or any change to) a direct-to destination or active flight plan to a second 400 or 500 Series Garmin unit. Crossfill requires both 400 and/or 500 Series units to have the same…
Page 151
• Active Flight Plan—transfer the active flight plan to/from a second 400- Flight Planning Series Garmin unit (GNS 430/GNC 420/GPS 400) in a dual unit installa- tion. This option is the default when selecting “Crossfill” from the flight planning page.
Page 152
) right knobs to enter the message text. Press when finished. (The GNS 430 will store up to nine scheduled messages holding 20 characters each.) 4a. The flashing cursor moves to the type field under the new message. Rotate the small right knob ( ) to display a window of available options: (Event, One Time, Periodic).
Page 153: Utility Page

Flight Timers— provides count up/down timers, plus automatic recording of depar- ture time and total trip time. Departure and total trip time recording can be conﬁ gured to run either any time GNS 430 power is on, or only when your ground speed exceeds 30 knots.
Page 154
ﬂ ying some approaches. The GNS 430 will automatically monitor RAIM during ap- proach operations and warn you if RAIM is not available. In such cases, use the GNS 430’s VLOC receiver instead for many of the non-precision and precision approaches stored on your Jeppesen NavData®…
Page 155
Utility Page: Checklists (cont.) AUX PAGES To execute a checklist: 1b. With the checklists page displayed, rotate the large right knob ( ) to select the desired checklist and press Utility Page 2b. As you complete each checklist item, press to move to the next item on the list.
Page 156
3b. Rotate the small right knob ( ) to select the desired reset mode. (“Pwr-on” will record a departure time when the GNS 430 is turned on. “GS>30 k t” will record a departure time once the GPS-computed ground speed exceeds 30 knots.) 4.
Page 157
3. Rotate the small right knob ( ) to select the desired reset mode. (“Pwr-on” will record trip time, in hours/minutes/seconds, any time the GNS 430 is turned on. “GS>30 k t” will record trip time any time the GPS-computed ground speed exceeds 30 knots.) 4.
Page 158
5. The flashing cursor moves to “Compute RAIM?”. Press to begin RAIM prediction. Once calculations are complete, the GNS 430 will display one of the following in the RAIM status field: • RAIM Not Available— Satellite coverage is predicted to NOT be suffi-…
Page 159
The software / database version page displays software version information for each of the various subsystems contained within the GNS 430, as well as database versions for the Jeppesen NavData® card and built-in land data. This page is for information purposes…
Page 160: Setup 1 Page

Setup 1 Page AUX PAGES Menu Options: to Setup 1 select, highlight with cursor and press Third Page in AUX group The setup 1 page provides access (via “menu options”) to airspace alarms, CDI scale adjustment, an arrival alarm, units of measure settings, position formats, map datums and settings for local or UTC time display.
Page 161
(i.e., 1.0 nm or 0.3 nm) the higher scale settings will not be selected during ANY phase of ﬂ ight. For example, if 1.0 nm is selected, the GNS 430 will use this for the enroute and terminal phase and ramp down to 0.3 nm during an approach. Note that the…
Page 162
If you are using a chart based on another datum, you must set the GNS 430 to use the same datum. Using a map datum that does not match the charts you are using can result in signiﬁ cant differences in Setup 1 position information.
Page 163
Setup 1 Page: CDI Scale / Alarms AUX PAGES To change the CDI scale: 1. Select “CDI / Alarms” from the setup 1 page, using the steps described on page 152. Setup 1 2. The flashing cursor highlights the “Selected CDI” field. Rotate the small right knob ( ) to select the desired CDI scale.
Page 164
Setup 1 Page: Units / Mag Var AUX PAGES To set the magnetic variation: 1. Select “Units / Mag Var” from the setup 1 page, using the steps described on page 152. Setup 1 2a. The flashing cursor highlights the heading mode field. Rotate the small right knob ( ) to select the desired heading mode: Auto, True or User.
Page 165
Setup 1 Page: Position Format / Map Datum AUX PAGES To change the position format: 1. Select “Position Format / Map Datum” from the setup 1 page, using the steps described on page 152. Setup 1 2a. The flashing cursor is on the position format field. Rotate the small right knob ( ) to select the desired position format.
Page 166
Setup 1 Page: Date / Time AUX PAGES To display local time or UTC: 1. Select “Date / Time” from the setup 1 page, using the steps described on page 152. Setup 1 2a. The flashing cursor highlights the time format field. Rotate the small right knob ( ) to display a window of available time formats: Local 12hr, Local 24hr, or UTC.
Page 167
You may also select manual control of the display contrast and backlighting to tailor the GNS 430’s display to your needs. Display backlighting changes are not saved when the GNS 430 is turned off. Backlighting will revert to the “Auto” setting the next time the unit is turned on.
Page 168
Nearest Airport Criteria— deﬁ nes the minimum runway length and surface type used when determining the nine nearest airports to display on the nearest airport page. A AUX PAGES minimum runway length and/or surface type may be entered to prevent airports with small runways, or runways that are not of appropriate surface, from being displayed.
Page 169
Setup 2 Page: Nearest Airport Criteria AUX PAGES To set the minimum runway length and runway surface: 1. Select “Nearest Airport Criteria” from the setup 2 page, using the steps described on page 159. Setup 2 2a. The flashing cursor highlights the runway surface field. Rotate the small right knob ( ) to select the desired surface.
Page 170
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Page 171: Section 10: Fde (Fault Detection Exclusion)

Navigation for Oceanic/Remote Operations” per FAA Notice N8110.60. The oceanic ﬂ ight phase is used by the GNS 430 when you are more than 200 nautical miles from the nearest airport. There are two main aspects to address in the FDE system. The ﬁ rst relates to the unit’s software side, in regard to detection and exclusion of faulty satellites.
Page 172
ﬂ ight involving Oceanic/Remote operations where GPS is to be the sole source of navigation. All operators using the GNS 430 as a primary means of navigation in oceanic/ remote areas under FAR parts 91, 121, 125 and 135 are required to utilize the FDE Pre- diction Program prior to conducting a ﬂ…
Page 173: Section 11: Messages, Abbreviations & Navigation Terminology

Messages, Abbreviations and Navigation Terminology aBBREVIATIONS & nav tERMS Messages The GNS 430 uses a flashing “MSG” annunciator at the bottom of the screen (directly above the key) to alert you of any important information or warnings. While most messages are advisory in nature, warning messages may require your intervention.
Page 174
—An attempt has been switch again to cycle its operation. If the message persists, contact your made to delete the active “to” or “from” waypoint. The GNS 430 will not GARMIN dealer for assistance. allow you to delete user waypoints currently being utilized for COM transfer key stuck navigation guidance.
Page 175
Data transfer error, please re-transmit —The GNS 430 has detected a failure in the —An error was detected display backlighting. The unit should be taken to your GARMIN dealer during unit-to-unit crossfill of user data (user waypoints and/or flight for service.
Page 176
NavData® card was installed (data- base change). MESSAGES, G/S has failed —The GNS 430 has detected a failure in its glideslope aBBREVIATIONS receiver. The glideslope receiver is not available and the unit should & nav tERMS be returned to your GARMIN dealer for service.
Page 177
No altitude input is being received —No altitude data is being failure in the main system processor. The GNS 430 is not usable and received from RS-232 (Serializer: Icarus, Rosetta or Shadin) or grey code should be taken to your GARMIN dealer for service.
Page 178
Other unit functions will continue to work normally, how- navigation. ever the GNS 430 should be taken to your GARMIN dealer for service at your earliest convenience. RAIM is not available —Receiver Autonomous Integrity Monitoring…
Page 179
3 nautical miles of the FAF; and the active approach is not a GPS- Searching the sky —The GNS 430 is searching the sky for GPS approved approach. Verify that the VLOC receiver is tuned to the proper satellite almanac data or the GPS receiver is in AutoLocate Mode.
Page 180
—You have used all 1000 user waypoint components may be unusable. Try cycling power off and back on. If the locations in the GNS 430’s memory. Delete unwanted waypoint to message persists, contact your GARMIN dealer for make room for new entries.
Page 181
Abbreviations MESSAGES, The following is a list of abbreviations used on the GNS 430 and aBBREVIATIONS their meanings: & nav tERMS ACTV — Active — Altitude APPRCHING —Approaching — Approach — Communications Transceiver — Airport CRSR — Cursor ARSPC — Airspace —…
Page 182
— Flight Plan — Kilograms — Feet Per Minute — Kilohertz MESSAGES, FREQ — Frequency — Kilometers aBBREVIATIONS & nav tERMS — Flight Service Station — Kilometers Per Hour — Feet — Knots LAT/LON — Glideslope —Latitude/Longitude — gallons — Pounds —…
Page 183
— Radial — Meters Per Minute RAIM — Receiver Autonomous Integrity — Meters Per Second MESSAGES, Monitoring — Minimum Safe Altitude aBBREVIATIONS — Reference & nav tERMS — Message — Required / Requirements — Mean Sea Level RESTRICTD —Restricted — Multicom —…
Page 184
MESSAGES, aBBREVIATIONS & nav tERMS VLOC — VOR/Localizer Receiver VNAV — Vertical Navigation — Volume — VHF Omnidirectional Radio Range — Vertical Speed — Vertical Speed Required — Waypoint — Weather — Crosstrack Error…
Page 185
The following navigation terms are used MESSAGES, on the GNS 430 and in this Pilot’s Guide: CUM(cumulative) —The total of all legs in aBBREVIATIONS a flight plan (such as “cumulative distance”).
Page 186
Vertical MESSAGES, Navigation aBBREVIATIONS & nav tERMS TIME AND DISTANCE TO PROFILE CURRENT ALTITUDE AND POSITION TARGET ALTITUDE HDG(heading) AND POSITION —The direction an aircraft DISTANCE TO TARGET is pointed, based upon indications from a magnetic compass or a properly set direc- AIRPORT tional gyro.
Page 187: Appendix A: Navdata Card Use

NAVDATA ® removed when the GNS 430 is on or off. Insert the card with the swing arm handle at the CARD USE bottom and the label facing to the left (see illustration right). If the NavData card is not present when the unit is turned on, you will receive a “No Jeppesen Aviation Database…
Page 188: Appendix B: Specifications

* Earlier versions of the 430 were designed to be used with 28 Vdc power only. Acquisition Time: 12 seconds (warm) Please refer to your Garmin authorized service center if you have questions on your particular installation. 45 seconds (cold) ** Subject to accuracy degradation to 100m 2DRMS under the U.S.
Page 189: Appendix C: Map Datums

Appendix C: Map Datums APPENDIX Adindan Ethiopia, Mali, (New Zealand) DATUMS Chua Astro Senegal, Sudan Paraguay Afgooye Corrego Alegre Brazil Somalia AIN EL ABD 1970 DANISH GI 1934 Denmark Bahrain Island, Djakarta (BATAVIA) Sumatra Island Saudi Arabia Anna 1 Astro 1965 Cocos Islands (Indonesia) Dos 1968…
Page 190
Central America, Santo (Dos) Espirito Santo CONUS, Mexico Island Nahrwan Masirah Is Masirah Island Sao Braz Sao Miguel, Santa APPENDIX (Oman) Maria Islands Nahrwan Saudi Arabia Saudi Arabia (Azores) DATUMS Nahrwan Unitd Arab E United Arab Sapper Hill 1943 East Falkland Emirates Island Naparima BWI…
Page 191: Appendix D: Troubleshooting Q & A

During oceanic, en route and terminal phases of flight, RAIM will be available nearly 100% of the time. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The GNS 430 automatically monitors RAIM and will warn you with an alert message (see Section 10) when it is not available, and the INTEG annunciator ( ) will appear at the bottom left corner of the screen.
Page 192
Can I file slant Golf (“/G”) using my GPS? Yes, you may file your flight plan as /G if your GNS 430 is a certified A1 or A2 installation. If you are flying en route, you may file /G with an expired database only after you have verified all route waypoints.
Page 193
Cannot be set for final approach course or published holding patterns Whenever OBS mode is active, the GNS 430 allows you to select the desired course to/from a waypoint using the HSI (much like a VOR) and display a to/from ﬂ ag for the active-to waypoint. If an external course input is not available, you may select the OBS course on-screen, via a “Select OBS Course pop-up window.
Page 194
When does turn anticipation begin, and what bank angle is expected? The GNS 430 will smooth adjacent leg transitions based upon a nominal 15º bank angle (with the ability to roll up to 25º) and provide three pilot cues for turn anticipation: 1) A waypoint alert (“NEXT DTK ###°”) will ﬂ ash in the lower right corner of the screen 10 seconds before the turn point.
Page 195
When does the CDI scale change, and what does it change to? APPENDIX TROUBLE- The GNS 430 will begin a smooth CDI scale transition from the 5.0 nm (enroute/oceanic mode) to the 1.0 nm (terminal mode) scale 30 nm from the destination airport (see left). The CDI scale will SHOOTING further transition to 0.3 nm (approach mode) at 2 nm prior to the FAF during an active approach.
Page 196
“Activate Approach?” and then pressing E . The GNS 430 will provide navigation along the desired course to the waypoint and rejoin the ap- proach in sequence from that point on. See page 65 for information on activating a speciﬁ c ﬂ ight plan leg.
Page 197: Appendix E: Index

COM squelch ….. .21 Addresses, GARMIN ….i, iv Backlighting .
Page 198
Direct-to navigation .12, 17, 34, 49-53, 121 Flight plan catalog options ..58-59 Display backlighting … 159-160 Flight plan comments ….56 APPENDIX Display contrast .
Page 199
Main page groups ….10, 11 Manual conventions ….v Hold (in an approach) … . 72-75 APPENDIX Manual sequence (course from fix legs) .85 Holding patterns .
Page 200
Sorting flight plans ….59 Radar coverage information ..101 Specifications ….178 Reference waypoint .
Page 201
Waypoint entry … . 95, 112-114 Turn advisories ….70-87, 187 Waypoint holding … . . 184-186 Turn anticipation .
Page 202
Notes…
Page 204
© 1998- 2003 Garmin Corporation Garmin International, Inc., 1200 East 151st Street Olathe, KS 66062 Garmin (Europe) Ltd., Unit 4, The Quadrangle, Abbey Park Industrial Estate, Romsey, SO51 9DL, UK Garmin (Asia) Corp., No. 68, Jangshu 2nd Road., Shijr, Taipei County, Taiwan Website Address: www.garmin.com…

Источник

Page 1: Garmin GNS 430

GNS 430 Shown GARMIN International, Inc. 1200 E. 151 st Street Olathe, KS 66062 USA 190-00140-05, Revision C October 2002 400 SERIES MAINTENANCE MANUAL (GNS ¥ 430, GNC ¥ 420, GPS 400)[…]
Page 2: Garmin GNS 430

Page A 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 © Copyright 1999-2002 GARMIN Ltd. or its subsidiaries All Rights Reserved GARMIN International, Inc. 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. GARMIN (Europe) Ltd. Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, SO51 9AQ, U.K. GARMIN Corporation No. 68, Jangshu 2[…]
Page 3: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page i P/N 190-00140-05 Rev. C LIST OF EFFECTIVE PAGES Page Revision Page Revision Page Revision Page Revision A C 4-8 C 5-54 BLANK F7-24 BLANK i C 5-1 C 6-1 C A-1 C i i C5 — 2 C6 — 2 CA — 2 C i i i C5 — 3 C6 — 3 CB — 1 C i v C5 — 4 C6 — 4 CB — 2 C v C 5-5 C 6-5 C B-3 C v i C5 — 6 C6 — 6 CB — 4 C vii C 5-7 C 6-7 C B-5 […]
Page 4: Garmin GNS 430

Page ii 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C The following are General Safety Precautions that are not related to any specific procedure and therefore do not appear elsewhere in this maintenance manual. These are recommended precautions that personnel should understand and apply during the many phases of maintenance and repair. KEE[…]
Page 5: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page iii P/N 190-00140-05 Rev. C TABLE OF CONTENTS SECTION 1 DESCRIPTION AND OPERATION Paragraph Page 1.1 INTRODUCTION ………………………………………………………………………………………. 1-1 1.1.1 Versions Covered by this Manual ………………………………………………….[…]
Page 6: Garmin GNS 430

Page iv 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C SECTION 3 TROUBLESHOOTING Paragraph Page 3.1 TROUBLESHOOTING EQUIPMENT …………………………………………………………… 3-1 3.2 TROUBLESHOOTING ORDER …………………………………………………………………… 3-1 3.3 TROUBLESHOOTING PROCEDURES …[…]
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400 SERIES MAINTENANCE MANUAL Page v P/N 190-00140-05 Rev. C SECTION 5 ALIGNMENT, CALIBRATION, AND TESTING Paragraph Page 5.1 INTRODUCTION ……………………………………………………………………………………. 5-1 5.2 RECOMMENDED TEST EQUIPMENT ……………………………………………………… 5-1 5.3 TEST S[…]
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Page vi 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C SECTION 5 ALIGNMENT, CALIBRATION, AND TESTING (continued) 5.7.2.8 Sidetone ………………………………………………………………………………………….. 5-18 5.7.2.9 MIC Intercom Test …………………………………………………………………..[…]
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400 SERIES MAINTENANCE MANUAL Page vii P/N 190-00140-05 Rev. C SECTION 5 ALIGNMENT, CALIBRATION, AND TESTING (continued) 5.7.4 Navigation Assembly I/O Tests ………………………………………………………….. 5-32 5.7.4.1 Localizer Course Deviation Test …………………………………………………………. 5-32 5.7.4.[…]
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Page viii 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C SECTION 5 ALIGNMENT, CALIBRATION, AND TESTING (continued) 5.7.6.14 MAIN Vertical UP, DOWN Outputs………………………………………………………. 5-47 5.7.6.15 MAIN To/From Output ……………………………………………………………………….. 5-47 5[…]
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400 SERIES MAINTENANCE MANUAL Page ix P/N 190-00140-05 Rev. C APPENDIX A GNC 420A AND GNS 430A A.1 DESCRIPTION ……………………………………………………………………………………….A-1 A.2 ‘A’ VERSION PART NUMBERS ………………………………………………………………..A-1 A.3 TROUBLESHOOTING ….[…]
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Page x 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C LIST OF FIGURES Figure Page 2-1 Com Chassis Nut ……………………………………………………………………………………. 2-1 2-2 Signal And Load Drawing-J1 (Sheet 1 of 2) ……………………………………………….. 2-3 2-3 Signal And Load Drawing-J1 ([…]
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400 SERIES MAINTENANCE MANUAL Page xi P/N 190-00140-05 Rev. C LIST OF TABLES Table Page 1-1 Unit Configuration …………………………………………………………………………………… 1-1 3-1 Unit Board Power Supply Max Current Allowed ………………………………………….. 3-5 3-2 Com Board Power Supply Toleranc[…]
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Page xii 400 SERIES MAINTENANCE MANUAL P/N 190-00140-05 Rev. C LIST OF TABLES (con’t.) Table Page 6-25 Sub-Assy, CDU, GNC 420, Black (Unit P/N 011-00281-01, Figure 7-4) ……….. 6-23 6-26 Sub-Assy, CDU, GNC 420, Gray (Unit P/N 011-00281-05, Figure 7-4) ………… 6-24 6-27 Sub-Assy, CDU GNC 420A, Black (Unit P/N 011-00281-01, Figure 7-4) …[…]
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400 SERIES MAINTENANCE MANUAL Page 1-1 P/N 190-00140-05 Rev. C SECTION 1 DESCRIPTION AND OPERATION 1.1 INTRODUCTION References made to the GNS 430 and the GNC 420 throughout this manual equally apply to the GNS 430A and the GNC 420A except where specifically noted. This manual provides board-level maintenance inform ation for the GARMIN 400 Series […]
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Page 1-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 GPS 400: UNIT P/N COLOR 011-00504-00 Black 011-00504-10 Gray GNC 420: UNIT P/N COLOR OPERATING VOLTAGE MINIMUM XMIT PWR 011-00506-00 BLACK 28 V 10 W 011-00506-10 BLACK 14 or 28 V 10 W 011-00506-30 GRAY 14 or 28 V 10 W GNS 430: UNIT P/N COLOR OPERATING VOLTAGE MINIMUM XMIT PWR 011-00280-[…]
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400 SERIES MAINTENANCE MANUAL Page 1-3 P/N 190-00140-05 Rev. C Each of the configurations includes a color display providing graphical moving map capability. Navigation, communication, and m apping functions are supported by a navigation database provided by a removable database card. The mapping function has additional support provided by a built-[…]
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Page 1-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 1.3 REPAIR PLAN This manual is designed to allow the user to perform board-level repair. If necessary, the unit can be returned to GARMIN for complete service work. Contact GARMIN at the address given on Page A (inside cover) for further service information. 1.4 SPECIFICATIONS Technical[…]
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400 SERIES MAINTENANCE MANUAL Page 1-5 P/N 190-00140-05 Rev. C 1.5.2 Com Board The Com Board contains the VHF COM Transceiver that provides voice comm unication in the 118.000 to 136.992 MHz general aviation band. The transceiver consists of a 10 or 16 watt (“A” versions) amplitude modulated transm itter (see the unit matrix tables on page 1-1)[…]
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Page 1-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 1.5.5 Glideslope Board The Glideslope Board contains a processor controlled Glideslope Receiver which operates from 329.15 MHz to 335.00 MHz in 150 kHz increments for 40 Glideslope channels. 1.5.6 Inverter Board The Inverter Board supplies high voltage for display operation. 1.5.7 CDU A[…]
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400 SERIES MAINTENANCE MANUAL Page 2-1 P/N 190-00140-05 Rev. C SECTION 2 SPECIAL TOOLS AND TEST EQUIPMENT 2.1 INTRODUCTION This section identifies the special tools and test equipment needed to maintain the 400 Series Units. Standard equipment is not listed. For any questions regarding special tools and test equipment contact GARMIN at the followin[…]
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400 SERIES MAINTENANCE MANUAL Page 2-3 (Page 2-4 blank) P/N 190-00140-05 Rev. C Figure 2-2. J1 Signal and Load Drawing (Sheet 1 of 2)[…]
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400 SERIES MAINTENANCE MANUAL Page 2-5 (Page 2-6 blank) P/N 190-00140 Rev. C Figure 2-3. J1 Signal and Load Drawing (Sheet 2 of 2)[…]
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400 SERIES MAINTENANCE MANUAL Page 2-7 (Page 2-8 blank) P/N 190-00140-05 Rev. C Figure 2-4. J2 Signal and Load Drawing[…]
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400 SERIES MAINTENANCE MANUAL Page 2-9 (Page 2-10 blank) P/N 190-00140-05 Rev. C Figure 2-5. J6 Signal and Load Drawing[…]
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400 SERIES MAINTENANCE MANUAL Page 3-1 P/N 190-00140-05 Rev. C SECTION 3 TROUBLESHOOTING Each unit in the 400 Series contains static sensitive components. Observe proper anti-static procedures when testing the unit. Hazardous voltages exist on the Inverter Board (all units). Under normal operating conditions the voltages range up to 2500 Vac peak t[…]
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Page 3-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 3.3 TROUBLESHOOTING PROCEDURES 3.3.1 Fuses Check for blown fuses on the Main Board, Com Board, and Nav Board as shown in Figures 3-1 through 3-4. If blown fuses are found, try to determine the cause of the fuse failure before installing a new fuse. F 8 5 0 5A F853 0.75A F851 3A F852 2A […]
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400 SERIES MAINTENANCE MANUAL Page 3-3 P/N 190-00140-05 Rev. C LOCA TION OF F600 (7A FUSE ) ON -00/-02/-03 COM BOARDS Figure 3-2. Com Board Fuse Location/F600 LOCATION OF F600 ON -04 REV C COM BOARDS TO PRES ENT (F600 REPLACED WITH R611, EXCEPT ON -0 4 REV A AND B BOARD) Figure 3-3. Com Board Fuse Location/F600 (Replaced by R611)[…]
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Page 3-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 F501 1 AMP J6 F502 1 AMP Figure 3-4. Nav Board Fuse Locations 3.3.2 Power Supply Checks 3.3.2.1 Current Measurements Taking intra-board and external current measureme nts is one way of determining a faulty board. To measure the currents, use a spare ribbon cable and spread the cable wir[…]
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400 SERIES MAINTENANCE MANUAL Page 3-5 P/N 190-00140-05 Rev. C The values listed in Table 3-1 are with the display backlight at maximum brightness. Table 3-1. Unit Board Power Supply Max Current Allowed Unit (Main Board) Unit Status Max Current (A) @ 27.5 V Max Current (A) @ 13.8 V (Optional) GPS 400 ON 0.66 1.32 GNC 420 ON RX—0.99 TX—3.36 RX?[…]
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Page 3-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 3.3.2.3 Glideslope Board Replace the Main Board if any voltage on the G/S Board is not within tolerance. Replace the G/S Board if excessive current is measured. Table 3-3. Glideslope Board Power Supply Tolerances Connector/Pin Voltage (V) Tolerance (V) Max Current (mA) Comments J25 Pin […]
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400 SERIES MAINTENANCE MANUAL Page 3-7 P/N 190-00140-05 Rev. C I — 111 0 I-1 00 Figure 3-5. Processor Location (Main Board) 3.4 STATIC MESSAGES The unit informs the user of operational status using the messages listed in Table 3-5. These messages can help in isolating a faulty assembly. Table 3-5 also shows the recommended action for each message. […]
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Page 3-8 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 3-5. Static Messages MESSAGE RECOMMENDED ACTION Stored data was lost Replace Main Board (see paragraph 4.5.5) Main processor requires service Replace Main Board (see paragraph 4.5.5) Memory battery low Replace Memory Battery (see paragraph 4.7.1) No differential GPS position Repla[…]
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400 SERIES MAINTENANCE MANUAL Page 3-9 P/N 190-00140-05 Rev. C Table 3-5. Static Messages (continued) COM remote transfer key stuck Verify that Remote Transfer Key Line is not stuck before replacing COM Board Replace Com Board (see paragraph 4.5.4) Heading input failure Replace Main Board (see paragraph 4.5.5) CDI key stuck Replace Flex Cable (see […]
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Page 3-10 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 3.5 TESTING FAILURES Another approach in troubleshooting is to perform testing on a unit according to the test procedures given in Section 5. To save time, only perform the minim um amount of testing in order to isolate the suspect board. Table 3-6 lists recommended actions based on fa[…]
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400 SERIES MAINTENANCE MANUAL Page 3-11 P/N 190-00140-05 Rev. C Table 3-6. Testing Failures  Main Board (continued) TEST FAILURE TEST PARAGRAPH RECOMMENDED ACTION GPS Antenna Bias 5.7.6.10 Replace GPS Module (see paragraph 4.5.5) GPS Noise 5.7.6.11 Replace GPS Module (see paragraph 4.5.5) Replace Main Board (see paragraph 4.5.5) Satellite Tracki[…]
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Page 3-12 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 3-7. Testing Failures  COM Board TEST FAILURE TEST PARAGRAPH RECOMMENDED ACTION Power Input Check 5.7.2.1 Replace Main Board (see paragraph 4.5.5) Replace Com Board (see paragraph 4.5.4) RF Power Out 5.7.2.2 Replace Com Board (see paragraph 4.5.4) Frequency Stability and Toler[…]
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400 SERIES MAINTENANCE MANUAL Page 3-13 P/N 190-00140-05 Rev. C Table 3-8. Testing Failures  NAV Board TEST FAILURE TEST PARAGRAPH RECOMMENDED ACTION Localizer Course Deviation Test 5.7.4.1 Replace Nav Receiver Board (see paragraph 4.5.6) To/From Deflection Output Characteristic Test 5.7.4.2 Replace Nav Receiver Board (see paragraph 4.5.6) To/Fr[…]
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Page 3-14 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 3-10. Testing Failures  NAV Receiver TEST FAILURE TEST PARAGRAPH RECOMMENDED ACTION Voice/Ident Audio Output Level 5.7.3.1 Replace Nav Receiver Board (see paragraph 4.5.6) Voice/Ident Audio Frequency Response 5.7.3.2 Replace Nav Receiver Board (see paragraph 4.5.6) Voice/Ident[…]
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400 SERIES MAINTENANCE MANUAL Page 3-15 P/N 190-00140-05 Rev. C 3.6 EXTERNAL CONNECTORS Figure 3-6 shows the external connectors and their corresponding pin numbers for each unit. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 1 2 34 5 67 89 10 11 12 14 15 16 17 18 19 20 21[…]
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400 SERIES MAINTENANCE MANUAL Page 3-17 (Page 3-18 blank) P/N 190-00140-05 Rev. C Figure 3-7. 400 Series Block Diagarm[…]
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400 SERIES MAINTENANCE MANUAL Page 4-1 P/N 190-00140-05 Rev. C SECTION 4 DISASSEMBLY AND ASSEMBLY 4.1 INTRODUCTION Repairing the unit is accomplished by removing and replacing defective boards. To help disassemble and reassemble the unit in order to access the boards, look at the assembly drawings in Section 7 and the parts lists in Section 6. Each[…]
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Page 4-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 4.3 NAV DATA CARD REMOVAL AND INSERTION Before disassembly begins, remove the Jeppesen NavData® card supplied with the unit. The card can be installed or removed when the unit is on or off. Insert the card with the swing arm handle at the bottom and the label facing to the left (see Fi[…]
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400 SERIES MAINTENANCE MANUAL Page 4-3 P/N 190-00140-05 Rev. C 4.4 UNIT DESIGN Each unit consists of a Main and Nav Chassis, CDU Assembly, and a Top Cover. The Main Chassis has a Top and Underside Cavity which contains replaceable boards. The following is a typical order of disassembly: 1. Remove the Top Cover. 2. Remove the CDU Assembly. 3. Disass[…]
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Page 4-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 4.5.2.1 Disassemble the CDU Assembly x Remove the Flex Assemblies (Figure 7-4) 1. Remove the VOL w/’C’ and VOL w/’V’ Knobs (18 and 19). 2. Remove the Push ‘CRSR’ and Push ‘C/V’ knobs (21, 22, 20, and 28). 3. Remove the Hex Nuts holding the Push ‘CRSR’ and Push ‘C/V[…]
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400 SERIES MAINTENANCE MANUAL Page 4-5 P/N 190-00140-05 Rev. C 4.5.4 Remove Faulty Boards from the Main Chassis Top Cavity Remove the Top Cover (see paragraph 4.5.1) to access the Main Chassis Top Sub-assemblies. x COM Board (Figure 7-2) Steps 5 and 6 apply to 28V/10W units only. 14/28V and 28V/16W units have no posistor, no brass spacers, and use […]
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Page 4-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 x GPS Module (Figure 7-2) 1. Disconnect the Ribbon Cable from the GPS Module (011-00474-XX). 2. Remove screw (211-60234-11) attaching the Map Board (012-00296-00) to the Main Chassis (125-00034-01). Remove 3 of 5 screws (211-63234-10) attaching GPS Module (011-00474-XX) to the Main Chas[…]
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400 SERIES MAINTENANCE MANUAL Page 4-7 P/N 190-00140-05 Rev. C x Glideslope Board (Figure 7-3) 1. Remove the Glideslope Board Cover (115-00221-00). 2. Disconnect the Ribbon Cable (325-00063-01) from the Glideslope Board (012- 00212-XX). 3. Unsolder the connector wire from the Coax Connector (330-00070-03). 4. Remove the three screws (211-60234-04) […]
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Page 4-8 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 1. Remove the Main Board (paragraph 4.5.5). 2. Remove all electrical grounds from the unit, so if using a grounded tip soldering iron, the battery will not be shorted upon removal. 3. Unsolder the battery leads from the bottom side of the Main Board. 4. Carefully remove the battery by p[…]
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400 SERIES MAINTENANCE MANUAL Page 5-1 P/N 190-00140-05 Rev. C SECTION 5 ALIGNMENT, CALIBRATION, AND TESTING 5.1 INTRODUCTION This section provides unit-level alignment, calibration, and testing information for the 400 Series units. The procedures in this section can be performed before troubleshooting begins to help identify a faulty board, or as […]
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Page 5-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05  Avionics Signal Generator  IFR or Marconi 2030 w/options one and six.  BF Goodrich Precision Track Selector  Digital Voltmeter—HP 34401A  GPS Antenna—GARMIN GA56 (P/N 010-10040-01)  Power Supply capable of 10-33 Volts @ 10 Amps—HP 6267B  Radio Test Set—HP 8[…]
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400 SERIES MAINTENANCE MANUAL Page 5-3 P/N 190-00140-05 Rev. C UNIT UNDER TEST BIRD WA TT M E T E R 30 dB 50 W A TT A TTENUA TOR 50 OHM LOAD RF INPUT AT T E N U AT E D RF OUTPUT NOTE 5 0 O H M L O A D IS N O T R E Q U IR E D I F 30 dB A T TE N U A TO R I S U S ED . THE 30 dB A TTE NU A TOR W I LL L OWE R T H E V S WR T O < 1 . 1 : 1 EVEN I F L E[…]
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Page 5-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.4.1.2 Standard Signals  COM RF Level Units All specifications given for the com transceiver are in HARD units. To arrive at these units adjust the RF generator to the level specified and insert a 6 dB pad at the output of the RF generator.  Standard Mic Input Signal A 1000 Hz to[…]
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400 SERIES MAINTENANCE MANUAL Page 5-5 P/N 190-00140-05 Rev. C  Standard Glideslope Centering Test Signal Standard Glideslope centering test signal is a standard Glideslope test signal in which the difference in depth of modulation of the 90 and 150 Hz signals is less than 0.002 ddm.  Standard Glideslope Deviation Test Signal Standard Glidesl[…]
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Page 5-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05  G/S Super Flag Load (G/S SUPER FLAG OUT) One standard super flag load shall be 56 ohms connected between G/S SUPER FLAG OUT J6-38 and GND J6-41.  ARINC 429 Transmitter Load (VLOC 429 OUTA/OUTB) The standard ARINC 429 transmitter load shall be 2.4K ohms resistance and 250 pF capac[…]
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400 SERIES MAINTENANCE MANUAL Page 5-7 P/N 190-00140-05 Rev. C  Standard VOR Audio Test Signal Standard VOR audio test signal is a standard VOR test signal to which is added a 1000 Hz signal, amplitude modulating the carrier 30%.  Standard Audio Test Signal Standard audio test signal is a RF carrier amplitude modulated 30% at 1000 Hz. The RF […]
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Page 5-8 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05  Standard Localizer Centering Test Signal Standard localizer centering test signal is a standard localizer test signal in which the difference in depth of modulation of the 90 and 150 Hz signals is less than 0.001.  Standard Localizer Deviation Test Signal Standard localizer devia[…]
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400 SERIES MAINTENANCE MANUAL Page 5-9 P/N 190-00140-05 Rev. C 5.5 ALIGNMENT Board alignment is not recommended on any of the 400 Series units. Alignment is performed on individual boards at the factory before being shipped as replacement items. 5.6 CALIBRATION Calibration can be performed for the following:  COM Frequency  Frequency Spacing […]
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Page 5-10 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.6.1 Com Setup Page Fields 5.6.1.1 Com Frequency The Com Frequency field selects a VHF communication frequency. For purposes of setting the squelch, sidetone levels and mic gain, only the frequencies 118.000, 127.000, and 136.975 MHz can be used. If any adjustment is made at one of th[…]
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400 SERIES MAINTENANCE MANUAL Page 5-11 P/N 190-00140-05 Rev. C 5.6.1.5 Sidetone The sidetone audio output level is independent of the COM volume knob on the unit. The SIDETN field sets the sidetone audio output level. The sidetone can be set to any value between zero and 63. The higher the number, the greater the sidetone volume.  SIDETN ______[…]
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Page 5-12 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7 TEST PROCEDURES 5.7.1 Test Mode In order to perform certain tests in the following section, the GNS 430 must be put into test m ode, which allows access to the Test Pages (Figure 5-4). To put the unit in the test mode, ground Test Pin (J1-76) and turn the unit on. When in test mode[…]
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400 SERIES MAINTENANCE MANUAL Page 5-13 P/N 190-00140-05 Rev. C Figure 5-4. Test Pages[…]
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Page 5-14 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.2 Com Testing Before starting com testing, note the following: 1. Disable the audio compressor unless otherwise specified. The compressor can be disabled for testing purposes by manually grounding the SQUELCH/COMPRESSOR TEST input at Pin 3 of J2 . 2. The 8.33 kHz channel mode uses […]
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400 SERIES MAINTENANCE MANUAL Page 5-15 P/N 190-00140-05 Rev. C 3. Transmit Mode: +14/+28 Volt Radios (J2-11 and 12):  Voltage _________ (+ 13.75 V)  Tolerance _________ ( r 0.2 V)  Max Current Avg 1 _________ (6.0 A) 5.7.2.2 RF Power Out 1. Set input voltage to 27.5 VDC (10 W, 28V units only) in TX mode at Pins J2-11 and 12. 2. Connect a […]
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Page 5-16 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Figure 5-5. Modulation Measurement Figure 5-5 shows the output of the Narda Crystal Detector display ed on an oscilloscope. The oscilloscope must be DC coupled in order for the modulation signal to be displayed correctly. 5.7.2.3 Frequency Stability and Tolerance Verify the RF carrier […]
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400 SERIES MAINTENANCE MANUAL Page 5-17 P/N 190-00140-05 Rev. C 5.7.2.5 Carrier Noise Level 1. Apply a standard MIC input signal. 2. The demodulated noise on the transmitter output, without audio m odulation, shall be at least 45 dB below the demodulated audio level obtained when the transmitter is m odulated with a standard mic input signal.  1[…]
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Page 5-18 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.2.8 Sidetone 1. Apply a standard mic input signal. Measure com audio out and while transmitting, verify sidetone level is 1.4 Vrms  0.2 Vrms.  118.50 MHz ______ Vrms  127.50 MHz ______ Vrms  136.50 MHz ______ Vrms 5.7.2.9 MIC Intercom Test 1. Remove RF input from the un[…]
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400 SERIES MAINTENANCE MANUAL Page 5-19 P/N 190-00140-05 Rev. C 5.7.2.11 TX Interlock 1. Apply an 10 P V, 30% modulated, 1000 Hz RF signal. 2. Measure SNR at rated audio ( a 7.07 Vrms).  Sensitivity Reading 1______ 3. Enable TX interlock line. 4. Measure SNR again.  Sensitivity Reading 2______  NLT 15dB difference between sensitivity readi[…]
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Page 5-20 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 7. Adjust the RF level to 20 µV. 8. Verify the DMM reading is greater than the AGC reference voltage.  DMM reading ________VDC (NLT AGC Reference Voltage) 9. Adjust the signal generator frequency to 127.008 MHz. 10. Verify the DMM reading is greater than the reference AGC voltage. […]
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400 SERIES MAINTENANCE MANUAL Page 5-21 P/N 190-00140-05 Rev. C 11. Verify the DMM reading is greater than the reference AGC voltage.  127.002778 MHz ______VDC (NLT AGC reference voltage)  126.997222 MHz ______VDC (NLT AGC reference voltage) 12. Adjust signal level to 10 mV.  127.00737 MHz ______VDC (NGT AGC reference voltage)  126.9926[…]
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Page 5-22 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.2.17 Audio Frequency Response 1. With compression disabled, apply a 30% modulated, 1 mV signal to the unit. 2. Verify the audio output does not change more than 6 dB from 350 Hz to 2.5 kHz. 3. Verify the audio-frequency response above 2500 Hz decreases, and at all frequencies above[…]
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400 SERIES MAINTENANCE MANUAL Page 5-23 P/N 190-00140-05 Rev. C 5.7.2.19 Squelch Test Note: Opened squelch—Audio Closed Squelch—No Audio 1. Enable compressor (see Section 5.7.2). 2. Set the unit and the RF signal generator to 127.000 MHz, 30% modulated with a 1 kHz tone. 3. Turn the RF level down below 1µV. 4. Turn the power/volume control on […]
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Page 5-24 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.2.20 Frequency Modulation FM deviation is to be measured with an average responding detector, which is RMS sine wave calibrated. The result is to be divided by 0.707 to yield the mathematical peak deviation. 1. Modulate the transmitter with a standard modulator input signal. 2. Ver[…]
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400 SERIES MAINTENANCE MANUAL Page 5-25 P/N 190-00140-05 Rev. C 5.7.3 Navigation Receiver Final Tests 5.7.3.1 Voice/Ident Audio Output Level 1. Apply a standard audio test signal having a RF level of -93 dBm. 2. Select maximum audio (volume control turned fully clockwise), and turn off the ident filter. 3. Measure 500 : VOR/ILS AUDIO HI J6-16 with […]
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Page 5-26 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.3.3 Voice/Ident Audio Distortion 1. Apply an input level from the RF generator of -79 dBm. 2. Modulate a standard VOR audio test signal at 350 Hz, 1000 Hz, and 2500 Hz (must be in IDENT mode to pass 1000 Hz tone). 3. Measure 500 : VOR/ILS AUDIO HI J6-16 with respect to 500 : VOR/IL[…]
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400 SERIES MAINTENANCE MANUAL Page 5-27 P/N 190-00140-05 Rev. C 5.7.3.6 Receiver Quieting 1. Apply a -86 dBm RF level to the RF input. 2. Apply a Standard VOR Audio Test signal at 108.00 MHz. 3. Measure at the 500 : VOR/ILS AUDIO HI J6-16 and 500 : VOR/ILS AUDIO LO J6-17 outputs. 4. Verify the Audio SINAD or SNR is greater than 25 dB.  Audio SIN[…]
Page 79: Garmin GNS 430

Page 5-28 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.3.9 VOR Flag Sensitivity A VOR/LOC +FLAG output voltage of greater than 260 mV fully conceals the indicator flag (‘HIDE’) and a VOR/LOC +FLAG output voltage of less than 125 m V fully reveals the indicator flag (IN VIEW). This test requires a Precision Track Selector or similar[…]
Page 80: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page 5-29 P/N 190-00140-05 Rev. C 5.7.3.12 VOR Course Deviation Sensitivity 1. Apply a standard VOR deviation signal at 108.00 MHz, –103.5 dBm RF level to the RF input. at a radial of 160 degrees ‘FROM’. 2. Apply a Precision Test Selector or similar device at 150 degrees in course angle. 3. Measure at the VOR/LOC[…]
Page 81: Garmin GNS 430

Page 5-30 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.3.16 Course Deviation Accuracy Test Apply a standard localizer deviation test signal, 90 Hz greater than 150Hz. Verify the deviation measured at VOR/LOC +LEFT with respect to VOR/LOC +RIGHT (VOR/LOC COMMON) is 90 mV r 9 m V. _____OK 5.7.3.17 VOR OBS Bearing Accuracy 1. Apply a stan[…]
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400 SERIES MAINTENANCE MANUAL Page 5-31 P/N 190-00140-05 Rev. C 5.7.3.19 Spurious Response—VOR/LOC 1. Tune the VOR receiver to 117.95 MHz. 2. Verify the input signal level of an undesired image frequency of 77.15 MHz required to produce a detector-carrier (AGC) level obtained at the VOR/LOC IF AGC J6-7 output with a -93 dBm Standard VOR Audio Tes[…]
Page 83: Garmin GNS 430

Page 5-32 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.4 Navigation Assembly I/O Tests 5.7.4.1 Localizer Course Deviation Test 1. Display the VOR/LOC/GS CDI Test Page (Figure 5-6). Figure 5-6. VOR/LOC/GS CDI Test Page 2. Display the following on the VOR/LOC/GS CDI Test Page and verify the following voltages, measuring across VOR/LOC +L[…]
Page 84: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page 5-33 P/N 190-00140-05 Rev. C 6. Verify the following output:  TO/FROM (VOR/LOC +TO) ______(-225 r 75 mV) 7. Display HIDE. 8. Measure VOR/LOC +TO (J6-1) with respect to VOR/LOC +FROM (J6-2). 9. Verify the following output:  TO/FROM (VOR/LOC +TO) ______ mV (0 mV r 5 mV) 5.7.4.4 Course Deviation Flag Output Cha[…]
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Page 5-34 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5. Verify the VOR/LOC SUPER FLAG OUT output voltage with respect to ground is 0 r 250 mV (50 ohm load).  VOR/LOC SUPER FLAG OUT ______ mV 5.7.4.7 NAV Input Lines Monitor the “VOR DISCRETE INPUTS” Test Page and verify that toggling the below listed inputs between their active and[…]
Page 86: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page 5-35 P/N 190-00140-05 Rev. C 5.7.4.9 NAV Serial DME Outputs Monitor the “VOR DISCRETE OUTPUTS” Test Page and verify that toggling the below listed outputs between their active and inactive states causes the output voltage on the appropriate line to switch between low (<.01 V) and high (>8.0 V) states. ?[…]
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Page 5-36 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05  PAR DME 2 MHz Low____ High ____ (Input Switch must not be grounded for this test)  PAR DME 4 MHz Low____ High ____ (Input Switch must not be grounded for this test)  PAR DME 8 MHz Low____ High ____[…]
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400 SERIES MAINTENANCE MANUAL Page 5-37 P/N 190-00140-05 Rev. C 5.7.5 Glideslope Final Tests 5.7.5.1 Glideslope Course Deviation Output Characteristic Test 1. Apply a standard course deviation input signal to the unit. 2. Measure GLIDESLOPE +UP (J6-32) with respect to GLIDESLOPE +DOWN (J6-31). 3. Verify the deviation output voltages (GLIDESLOPE +UP[…]
Page 89: Garmin GNS 430

Page 5-38 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.5.4 Glideslope Superflag Output Test 1. Select flag ‘HIDDEN’. 2. Verify GLIDESLOPE superflag output voltage is not less than PWR_IN minus 1.5 V.  GLIDESLOPE Superflag Output ______ (NLT Power_IN minus 1.5 V) 3. Select Flag ‘IN VIEW’. 4. Verify GLIDESLOPE superflag output[…]
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400 SERIES MAINTENANCE MANUAL Page 5-39 P/N 190-00140-05 Rev. C 5.7.5.6 Centering Accuracy 1. Apply a standard glideslope test signal to the unit. 2. Measure GLIDESLOPE +UP (J6-32) with respect to GLIDESLOPE +DOWN (GLIDESLOPE Common) (J6-31). 3. Verify the centering accuracy is 0 mV r 7.8 mV.  Centering Accuracy _________mV 5.7.5.7 AGC 1. Apply […]
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Page 5-40 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.5.9 Nose Bandwidth 1. Apply standard glideslope test signal to the unit (-56dBm). 2. Find the AGC voltage and use it as a reference. 3. Vary the input signal frequency over the range of r 17 kHz from the assigned channel frequency. 4. Verify the input signal level needed to maintai[…]
Page 92: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page 5-41 P/N 190-00140-05 Rev. C 5.7.5.12 Status Tests 1. The following status bits shall be good with or without a standard glideslope test signal:  GLIDESLOPE ROM_______OK  GLIDESLOPE EEPROM _____OK  GLIDESLOPE Synthesizer Lock__________OK 2. The following status bits shall be good when a standard glideslop[…]
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Page 5-42 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.6 Main Board Final Tests GNC 420 versions 011-00506-10 or 011-00506-30, and GNS 430 versions 011-00280-10 or 011-00280-30 m ust be verified operational with dual power switch in both positions (1 and 2). The “A” versions of the GNC 420 and the GNS 430 must be verified also. See[…]
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400 SERIES MAINTENANCE MANUAL Page 5-43 P/N 190-00140-05 Rev. C 5.7.6.4 Photocell 1. Turn the unit on in the test mode and verify brightness control is in photo mode, using the main lighting page. 2. With photocell uncovered, ensure display and keyboard backlight LED brightness is proper under normal conditions. _____OK 3. Cover the photocell and v[…]
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Page 5-44 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Figure 5-7. Main Lighting and Main Analog Test Pages B. Lighting Bus DC 1. Using the Main Lighting Test Page, change source to 14 VDC in both the DISPLAY and KEY fields. 2. Attach 12.0 VDC to unit pin J1-39. Ensure the power supply ground is connected to unit ground (J1-77, 78). 3. Mon[…]
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400 SERIES MAINTENANCE MANUAL Page 5-45 P/N 190-00140-05 Rev. C 5.7.6.7 Display Pattern Test Starting from the display pattern test page, use the “RNG” buttons to cycle through all of the display patterns to verify all pixels are driven and color contrast is acceptable. _____OK 5.7.6.8 Fan Test 1. Verify fan blade is not moving or air is not be[…]
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Page 5-46 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 1. Put the unit into Test Mode. 2. Turn the small right knob (CRSR) until you see the GPS Test Page (Figure 5-7). 3. Terminate GPS receiver into a 50 ohm load. 4. The “sgnl” number represents the receiver noise level. Verify this number is within the range of 1450 to 1750. _____OK […]
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400 SERIES MAINTENANCE MANUAL Page 5-47 P/N 190-00140-05 Rev. C Figure 5-9. Main CDI/OBS Configuration Test Page 5.7.6.13 MAIN Lateral LEFT, RIGHT Outputs Measure J1-21 (output) relative to J1-22 (output) [Load—333 ohms (three 1000 ohm loads) across J1-21 and J1-22]. Note that full left/right ( r 150 m V) are also available selections but are not[…]
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Page 5-48 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.6.16 MAIN Lateral Flag Output Measure J1-23 relative to J1-24. Load—333 ohms (Three 1000 ohm loads) across J1-23 and J1-24.  ‘HIDE’______ (+375 r 80 mV)  IN VIEW ______ (0 r 25 mV ) 5.7.6.17 MAIN Vertical Flag Output Measure J1-29 relative to J1-30. Load—333 ohms (Thr[…]
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400 SERIES MAINTENANCE MANUAL Page 5-49 P/N 190-00140-05 Rev. C 5.7.6.20 Annunciate Outputs Both the OBS and the AUTO outputs are switched by toggling the OBS selection on the Test Page. For: ANNUCIATOR PIN NAV (VLOC) (J1-1) GPS (J1-2) WAYPOINT (J1-3) TERMINAL (A) (J1-4) APPROACH (B) (J1-5) MESSAGE (J1-6) OBS (J1-7) AUTO (J1-8) INTEGRITY (C) (J1-9)[…]
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Page 5-50 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 2. Measure at applicable pin. Load—Resistor to external voltage source such that it will source 275 mA when grounded. Note: applicable output will sink this current when active (18 ohms/2W when pulled up to 5V).  ACTIVE______ (0.3 VDC max)  INACTIVE ______ (NLT pull-up voltage […]
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400 SERIES MAINTENANCE MANUAL Page 5-51 P/N 190-00140-05 Rev. C 5.7.6.22 Discrete Switch and Altitude Inputs For: INPUT NAME PIN ALTITUDE C4 (J1-61) ALTITUDE C2 (J1-62) ALTITUDE C1 (J1-63) ALTITUDE B4 (J1-64) ALTITUDE B2 (J1-65) ALTITUDE B1 (J1-66) ALTITUDE A4 (J1-67) ALTITUDE A2 (J1-68) ALTITUDE A1 (J1-69) ALTITUDE D4 (J1-70) OBS MODE SELECT (J1-7[…]
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Page 5-52 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.6.23 ARINC 429 Transmitter and Receivers Unit outputs both HIGH and LOW speed signals at the same time in test mode while on the Main Status/Loopback Test Page, thus both speeds are tested simultaneously. For: GPS ARINC 429 OUT A (J1-46). GPS ARINC 429 OUT B (J1-47). GPS ARINC 429 […]
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400 SERIES MAINTENANCE MANUAL Page 5-53 P/N 190-00140-05 Rev. C 5.7.6.24 RS232 Ports For: GPS RS232 OUT 1 (J1-56) GPS RS232 IN 1 (J1-57) GPS RS232 OUT 2 (J1-58) GPS RS232 IN 2 (J1-59) GPS RS232 OUT 3 (J1-41) GPS RS232 IN 3 (J1-42) GPS RS232 OUT 4 (J1-54) GPS RS232 IN 4 (J1-55) A. GPS RS232 1 1. Test both receiver and transmitter. 2. Connect the tra[…]
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Page 5-54 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 5.7.6.25 OBS The load used in the OBS test consists of a calibrated OBS resolver, Precision Track Selector or equivalent, and must be connected to the GPS OBS inputs. The OBS bearing must be consistent to within r 2 degrees of the bearing setting. If this output requires an alignment, […]
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400 SERIES MAINTENANCE MANUAL Page 6-1 P/N 190-000140-05 Rev. C SECTION 6 PARTS AND ASSEMBLIES 6.1 INTRODUCTION This section lists major parts of the 400 Series. The part numbers listed in this section of the manual are given to aid in assembly and disassembly of the unit only, not for identifying orderable parts. For orderable part information, se[…]
Page 107: Garmin GNS 430

Page 6-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 GNC420/420A Table Part Description Unit P/N Figure 6-15 Sub-Assy, GNC420, 28V, Black 011-00506-00 7-5 6-16 Sub-Assy, GNC420, 14/28V, Black 011-00506-10 7-5 6-17 Sub-Assy, GNC420, 14/28V, Gray 011-00506-30 7-5 6-18 Sub-Assy, GNC420A, 28V, Black 011-00837-00 7-8 6-19 Sub-Assy, GNC420A, 28[…]
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400 SERIES MAINTENANCE MANUAL Page 6-3 P/N 190-000140-05 Rev. C Miscellaneous Parts Part Part Description Unit P/N Figure F600 Fuse, Submini, Axial, 7 Amp 350-00003-15 3-2 F850 Fuse, SMT, Fast, 5 Amp 350-B0500-01 3-1 F853 Fuse, 1206, 0.75 Amp 350-B1075-00 3-1 F852 Fuse, 1206, 2 Amp 350-B1200-00 3-1 F851 Fuse, 1206, 3 Amp 350-B1300-00 3-1 R611 Resis[…]
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Page 6-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 6.2.1 GNS 430/430A Tables Table 6-1. Sub-Assy, GNS 430, 28V, Black (Unit P/N 011-00280-00, Figure 7-1) Part Number Part Name Qty 011-00281-00 Sub-Assy,CDU,GNS430 1 011-00282-00 Sub-Assy,Nav Chassis,GNC400 1 011-00283-00 Sub-Assy,Main Chas,GNS430,28V 1 011-00460-40 Sub-Assy,Memory Card,D[…]
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400 SERIES MAINTENANCE MANUAL Page 6-5 P/N 190-000140-05 Rev. C Table 6-3. Sub-Assy, GNS 430, 14/28V, Gray (Unit P/N 011-00280-30, Figure 7-1) Part Number Part Name Qty 011-00281-04 Sub-Assy,CDU,GNS430,Gray 1 011-00282-00 Sub-Assy,Nav Chassis,GNC400 1 011-00283-30 Sub,Mn Chassis,GNS430,14/28V,DO 1 011-00460-40 Sub-Assy,Memory Card,Dummy 1 115-00218[…]
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Page 6-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-5. Sub-Assy GNS 430A, 28V, Gray (Unit P/N 011-00836-10, Figure 7-1) Part Number Part Name Qty 011-00281-04 Sub-Assy,CDU,GNS430,Gray 1 011-00282-00 Sub-Assy,Nav Chassis,GNC400 1 011-00283-20 Sub,Main Chassis,GNS430A 1 011-00460-40 Sub-Assy,Memory Card,Dummy 1 115-00218-00 SMP,Cov[…]
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400 SERIES MAINTENANCE MANUAL Page 6-7 P/N 190-000140-05 Rev. C Table 6-6. Main Chassis Assy, GNS 430, 14/28V (Unit P/N 011-00283-10, Figure 7-2) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-05 PCB Assy,Comm,10W 14/28V 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-32[…]
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Page 6-8 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-7. Main Chassis Assy, GNS 430, 14/28V, DO (Unit P/N 011-00283-30, Fig. 7-2) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-05 PCB Assy,Comm,10W 14/28V 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-3[…]
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400 SERIES MAINTENANCE MANUAL Page 6-9 P/N 190-000140-05 Rev. C Table 6-8. Main Chassis Assy, GNS 430, 28V (Unit P/N 011-00283-00, Fig. 7-2) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-03 PCB Assy,Comm,2.5ppm TCXO 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-32 PCB[…]
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Page 6-10 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-9. Main Chassis Assy, GNS 430A, 28V (Unit P/N 011-00283-20, Figure 7-2) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-32 PCB Assy,GNS430 Main Bd,DO 1 012-00611-00[…]
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400 SERIES MAINTENANCE MANUAL Page 6-11 P/N 190-000140-05 Rev. C Table 6-10. Nav Chassis Sub-Assy, GNS 430/430A (Unit P/N 011-00282-00, Figure 7-3) Part Number Part Name Qty 012-00195-20 PCB Assy,Nav Rcvr,GNC400/500 1 012-00212-10 PCB Assy,GNC400 Glide Slope 1 115-00209-00 SMP,Cover,Cont,GNC400 Nav Bd 1 115-00213-00 SMP,Cover,RF,GNC400 Nav Bd 1 115[…]
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Page 6-12 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-11. Sub-Assy, CDU, GNS 430, Black (Unit P/N 011-00281-00, Figure 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 6 210-00021-00 Nut,Hex,Reduced 1 7 211-00030-00 Pivot Pin,Power Switch 1 8 117-00028-00 Shaft,Pot,Machined,GNC4XX 1 20 430-00013-01 […]
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400 SERIES MAINTENANCE MANUAL Page 6-13 P/N 190-000140-05 Rev. C Table 6-12. Sub-Assy, CDU, GNS 430, Gray (Unit P/N 011-00281-04, Figure 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 6 210-00021-00 Nut,Hex,Reduced 1 7 211-00030-00 Pivot Pin,Power Switch 1 8 117-00028-00 Shaft,Pot,Machined,GNC4XX 1 20 430-00013-01 […]
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Page 6-14 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-13. Sub-Assy, CDU, GNS 430A, Black (Unit P/N 011-00281-00, Figure 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 6 210-00021-00 Nut,Hex,Reduced 1 7 211-00030-00 Pivot Pin,Power Switch 1 8 117-00028-00 Shaft,Pot,Machined,GNC4XX 1 20 430-00013-01[…]
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400 SERIES MAINTENANCE MANUAL Page 6-15 P/N 190-000140-05 Rev. C Table 6-14. Sub-Assy, CDU, GNS 430A, Gray (Unit P/N 011-00281-04, Figure 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 6 210-00021-00 Nut,Hex,Reduced 1 7 211-00030-00 Pivot Pin,Power Switch 1 8 117-00028-00 Shaft,Pot,Machined,GNC4XX 1 20 430-00013-01[…]
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Page 6-16 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 6.2.3 GNC 420/420A Tables Table 6-15. Sub-Assy, GNC 420, 28V, Black (Unit P/N 011-00506-00, Figure 7-5) Part Number Part Name Qty 011-00281-01 Sub-Assy,CDU,GNC420 1 011-00282-01 Sub-Assy,Nav Chassis,w/o Nav 1 011-00283-01 Sub-Assy,Main Chas,GNC420,28V 1 011-00460-40 Sub-Assy,Memory Car[…]
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400 SERIES MAINTENANCE MANUAL Page 6-17 P/N 190-000140-05 Rev. C Table 6-17. Sub-Assy, GNC 420, 14/28V, Gray (Unit P/N 011-00506-30, Figure 7-5) Part Number Part Name Qty 011-00281-05 Sub-Assy,CDU,GNC420,Gray 1 011-00282-01 Sub-Assy,Nav Chassis,w/o Nav 1 011-00283-31 Sub,Mn Chassis,GNC420,Gray,DO 1 011-00460-40 Sub-Assy,Memory Card,Dummy 1 115-0021[…]
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Page 6-18 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-19. Sub-Assy, GNC 420A, 28V Gray (Unit P/N 011-00837-10, Figure 7-8) Part Number Part Name Qty 011-00281-05 Sub-Assy,CDU,GNC420,Gray 1 011-00282-01 Sub-Assy,Nav Chassis,w/o Nav 1 011-00283-21 Sub,Main Chassis,GNC420A 1 011-00460-40 Sub-Assy,Memory Card,Dummy 1 115-00218-00 SMP,[…]
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400 SERIES MAINTENANCE MANUAL Page 6-19 P/N 190-000140-05 Rev. C Table 6-20. Main Chassis Assy, GNC 420, 28V (Unit P/N 011-00283-01, Figure 7-6) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-03 PCB Assy,Comm,2.5ppm TCXO 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-22[…]
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Page 6-20 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-21. Main Chassis Assy, GNC 420, 14/28V (Unit P/N 011-00283-11, Fig. 7-6) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-05 PCB Assy,Comm,10W 14/28V 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-22 […]
Page 126: Garmin GNS 430

400 SERIES MAINTENANCE MANUAL Page 6-21 P/N 190-000140-05 Rev. C Table 6-22. Main Chassis Assy, GNC 420, 14/28V, DO, (P/N 011-00283-31, Figure 7-6) Item Description Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00214-05 PCB Assy,Comm,10W 14/28V 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-22 PC[…]
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Page 6-22 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-23. Main Chassis Sub-Assy, GNC 420A, 28V (Unit P/N 011-00283-21, Figure 7-6) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00611-00 PCB Assy,Comm Xcvr,16 Watt 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-003[…]
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400 SERIES MAINTENANCE MANUAL Page 6-23 P/N 190-000140-05 Rev. C Table 6-25. Sub-Assy, CDU, GNC 420, Black (Unit P/N 011-00281-01, Figure 7-4) Bub Number Item Description Qty 32 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 28 430-00013-01 Knob Assy,Outer,GNC400/500 1 20 430-00013-01 Knob Assy,Outer,GNC400/500 1 1 011-00340-00 Sub-Assy,Inc Dec Push S[…]
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Page 6-24 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-26. Sub-Assy, CDU, GNC 420, Gray (Unit 011-00281-05, Figure 7-4) Bub Number Part Number Part Name Qty 32 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 28 430-00013-01 Knob Assy,Outer,GNC400/500 1 20 430-00013-01 Knob Assy,Outer,GNC400/500 1 1 011-00340-00 Sub-Assy,Inc Dec Push Sw[…]
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400 SERIES MAINTENANCE MANUAL Page 6-25 P/N 190-000140-05 Rev. C Table 6-27. Sub-Assy, CDU, GNC 420A, Black (Unit P/N 011-00281-01, Figure 7-4) Bub Number Item Description Qty 32 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 28 430-00013-01 Knob Assy,Outer,GNC400/500 1 20 430-00013-01 Knob Assy,Outer,GNC400/500 1 1 011-00340-00 Sub-Assy,Inc Dec Push […]
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Page 6-26 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-28. Sub-Assy, CDU, GNC 420A, Gray (Unit 011-00281-05, Figure 7-4) Bub Number Part Number Part Name Qty 32 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 28 430-00013-01 Knob Assy,Outer,GNC400/500 1 20 430-00013-01 Knob Assy,Outer,GNC400/500 1 1 011-00340-00 Sub-Assy,Inc Dec Push S[…]
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400 SERIES MAINTENANCE MANUAL Page 6-27 P/N 190-000140-05 Rev. C 6.2.4 GPS 400 Tables Table 6-29. Sub-Assy, GPS 400, 14/28V, Black (Unit P/N 011-00504-00, Figure 7-10) Part Number Part Name Qty 011-00281-03 Sub-Assy,CDU,GPS400 1 011-00282-01 Sub-Assy,Nav Chassis,w/o Nav 1 011-00283-33 Sub,Main Chassis,GPS400,DO 1 011-00460-40 Sub-Assy,Memory Card,D[…]
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Page 6-28 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-31. Main Chassis Assy, GPS 400 14/28V, (Unit P/N 011-00283-03, Figure 7-9) Part Number Part Name Qty 011-00474-01 Sub-Assy,GPS Module,GNC TSOII 1 012-00256-00 PCB Assy,GNC400 Inverter Bd 1 012-00296-00 PCB Assy,GNC400 Map Bd 1 012-00347-02 PCB Assy,GPS400 Main Bd,DO 1 115-00337[…]
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400 SERIES MAINTENANCE MANUAL Page 6-29 P/N 190-000140-05 Rev. C Table 6-34. Sub-Assembly, CDU, GPS 400, Black (Unit P/N 011-00281-03), Fig 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 2 211-60232-06 Screw,2-56x.187,PHP,SS/P,w/NYL 6 3 410-00012-01 Rtry Sw,Pot,w/Mom Push Sw, 1 5 012-00258-00 PCB Assy,GNC400 Interf[…]
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Page 6-30 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table 6-35. Sub-Assembly, CDU, GPS 400, Gray (Unit P/N 011-00281-06, Fig 7-4) Bub Part Number Part Name Qty 1 011-00340-00 Sub-Assy,Inc Dec Push Switch 1 2 211-60232-06 Screw,2-56x.187,PHP,SS/P,w/NYL 6 3 410-00012-01 Rtry Sw,Pot,w/Mom Push Sw, 1 5 012-00258-00 PCB Assy,GNC400 Interface[…]
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400 SERIES MAINTENANCE MANUAL Page 7-1 P/N 190-00140-05 Rev. C SECTION 7 ASSEMBLY DRAWINGS 7.1 INTRODUCTION This section contains assembly drawings to aid in assembly and disassembly of the 400 Series units. Part numbers and drawing notes can be used as reference information during disassem bly and assembly. Note: The revision levels of the drawing[…]
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Page 7-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 GPS 400: x GPS 400 Assy Drawing (Dwg. No. 015-00504-XX, Rev. G, Figure 7-10) x Figure 7-9—Main Chassis Assembly, GPS 400 (Dwg. No. 015-00283-03, Rev. J) x GPS 400 Sub-Assy, Nav Chassis, W/O Nav (Use Figure 7-7) x GPS 400 CDU Assembly Drawing (Use Figure 7-4)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-3 (page 7-4 blank) P/N 190-00140-05 Rev. C Figure 7-1. Sub-Assy, GNS 430 (Dwg. No. 015-00280-XX, Rev. P)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-5 (page 7-6 blank) P/N 190-00140-05 Rev. C Figure 7-2. Main Chassis Assy, GNS 430(A) (Dwg. No. 015-00283-00, Rev. R)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-7 (page 7-8 blank) P/N 190-00140-05 Rev. C Figure 7-3. Nav Chassis Assy, GNC 400 (Dwg. No. 015-00282-00, Rev. K)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-9 (Page 7-10 blank) P/N 190-00140-05 Rev. C Figure 7-4. GNC 4XX CDU Assy (Sheet 1 of 2) (Dwg. No. 015-00281-XX, Rev. F )[…]
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400 SERIES MAINTENANCE MANUAL Page 7-11 (Page 7-12 blank) P/N 190-00140-05 Rev. C Figure 7-4. GNC 4XX CDU Assy (Sheet 2 of 2) (Dwg. No. 015-00281-XX, Rev. F )[…]
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400 SERIES MAINTENANCE MANUAL Page 7-13 (page 7-14 blank) P/N 190-00140-05 Rev. C Figure 7-5. Sub-Assy, GNC 420 (Dwg. No. 015-00506-XX, Rev. N)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-15 (page 7-16 blank) P/N 190-00140-05 Rev. C Figure 7-6. Main Chassis Assy, GNC 420(A) (Dwg. No. 015-00283-01, Rev. K)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-17 (page 7-18 blank) P/N 190-00140-05 Rev. C Figure 7-7. Nav Chassis Assy, W/O Nav (Dwg. No. 015-00282-01, Rev. E)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-19 (page 7-20 blank) P/N 190-00140-05 Rev. C Figure 7-8. Sub-Assy, GNC 420A (Dwg. No. 015-00837-XX, Rev. A)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-21 (page 7-22 blank) P/N 190-00140-05 Rev. C Figure 7-9. Main Chassis Assy, GPS 400 (Dwg. No. 015-00283-03, Rev. J)[…]
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400 SERIES MAINTENANCE MANUAL Page 7-23 (Page 7-24 blank) P/N 190-00140-05 Rev. C Figure 7-10. Assy Dwg, GPS 400 (Dwg. No. 015-00504-XX, Rev. G)[…]
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400 SERIES MAINTENANCE MANUAL Page A-1 P/N 190-00140-05 Rev. C APPENDIX A GNC 420A AND GNS 430A A.1 DESCRIPTION This appendix describes version A of the GNC 420 and the GNS 430. The ‘A’ versions contain a 16 watt VHF Com Transmitter as opposed to a 10 watt transm itter. There is one Com Board part number for the GNC 420 and GNS 430 ‘A’ vers[…]
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Page A-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 The Com Voltage and Current requirements for the GNS 420A and GNS 430A are listed in Table A-2. Table A-2. Voltage and Current Supply Requirements Connector / Pin DC Voltage Tolerance(V) Max Current (DC) Conditions J2, Pins 11 & 12 +27.5 r .4 3.0 A Transmit Mode A.4 DISASSEMBLY AND […]
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400 SERIES MAINTENANCE MANUAL Page B-1 P/N 190-00140-05 Rev. C APPENDIX B CONNECTOR I/O DESCRIPTIONS B.1 I/O DESCRIPTION This appendix contains tables describing various I/O information used in the 400 Series. Table B-1. I/O Descriptions IO Code Description I INPUT O OUTPUT B BI-DIRECTIONAL B.2 INTERNAL AND EXTERNAL CONNECTORS Table B-2. Internal a[…]
Page 152: Garmin GNS 430

Page B-2 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table B-2. Internal and External Connections (continued) INVERTER BOARD J13 Main Board J26 Display Module CCTF J27 Display Module Heater GPS MODULE ( ALL UNITS) J101 J3 Main Board Antenna In INTERFACE BOARD J19 Data Card Flex J20 Left Data Card J21 Right Data Card DISPLAY MODULE J22 LCD[…]
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400 SERIES MAINTENANCE MANUAL Page B-3 P/N 190-00140-05 Rev. C Table B-3. J1 Descriptions (continued) AIRCRAFT POWER 20 I MAIN +LEFT 21 O MAIN +RIGHT (2.5V Common) 22 O MAIN LATERAL +FLAG 23 O MAIN LATERAL -FLAG (2.5V Common) 24 O MAIN +TO 25 O MAIN +FROM (2.5V Common) 26 O MAIN +UP 27 O MAIN +DOWN (2.5V Common ) 28 O MAIN VERTICAL +FLAG 29 O MAIN […]
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Page B-4 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table B-3. J1 Descriptions (continued) GPS RS232 IN4 55 I GPS RS232 OUT1 56 O GPS RS232 IN1 57 I GPS RS232 OUT2 58 O GPS RS232 IN2 59 I ALTITUDE COMMON (Ground) 60 O ALTITUDE C4 61 I ALTITUDE C2 62 I ALTITUDE C1 63 I ALTITUDE B4 64 I ALTITUDE B2 65 I ALTITUDE B1 66 I ALTITUDE A4 67 I AL[…]
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400 SERIES MAINTENANCE MANUAL Page B-5 P/N 190-00140-05 Rev. C B.3.3 J9 Table B-5. J9 Descriptions Pin Name Pin # I/O Description 12V 1 O 12 volt Supply to NAV board and G/S board from Main CPU board. 5V_NAV 2 O +5 volt Supply to NAV board and G/S board from Main CPU board. GND 3 O Ground. -12V 4 O -12 volt Supply to NAV board and G/S board from Ma[…]
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Page B-6 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.3.5 J12 Table B-7. J12 Descriptions Pin Name Pin # I/O Description LD1 through LD8 46-50 3-5 O LOWER half display DATA output. CLK_ROW 6 O Pulse high for typically 310 ns at a period of 33.236 us (30.088 kHz). This line loads the next row of data in the display drivers. There are 66 C[…]
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400 SERIES MAINTENANCE MANUAL Page B-7 P/N 190-00140-05 Rev. C Table B-7. J12 Descriptions (continued) NOT USED 25 ROT_R_LRGA ROT_R_LRGB ROT_R_LRGC 64 26 27 I I I Rotor Right Large A to C are the contacts of a single pole triple throw switch. The common of the switch is ground. Only one of the 3 is low at a time. ROT_R_SMLA ROT_R_SMLB ROT_R_SMLC 61[…]
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Page B-8 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 Table B-8. J14 Descriptions (continued) 36 37 38 ROT_L_SMLC ROT_L_SMLB ROT_L_SMLA I I I Rotor Left Small A to C are the contacts of a single pole triple throw switch. The common of the switch is ground. Only one of the 3 is low at a time. 39 ROT_L_SW I Push switch on left rotary. Active[…]
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400 SERIES MAINTENANCE MANUAL Page B-9 P/N 190-00140-05 Rev. C B.3.7 J16 Table B-9. J16 Descriptions Pin Name Pin # I/O Description CS_MAPN 1 O Chip Select Map Not. Output pulses low ty pically for 240 ns when map is accessed. RDN 2 O Read Not. Output pulses low for typical times of 90, 150, and 210 ns, depending on wait states. WRN 3 O Write Not. […]
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Page B-10 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.3.8 J17 Table B-10. J17 Descriptions Pin Name Pin # I/O Description FAN_HI 1 O Approx. 5 V. FAN_LO 2 O Used to switch fan off and on. B.3.9 P13 Table B-11. P13 Descriptions Pin Name Pin # I/O Description 12V 1 O 12 V dc output. CCFT_TA_NOT 2 O Cold Cathode Transmit A Not logic level […]
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400 SERIES MAINTENANCE MANUAL Page B-11 P/N 190-00140-05 Rev. C B.4 COM BOARD CONNECTORS B.4.1 J2 Table B-12. J2 Descriptions Pin # Name I/O 1 RESERVED 2 COM IF AGC TEST O 3 SQUELCH / COMPRESSOR TEST I 4 COM MIC KEY I 5 INTERCOM MIC HI I 6 COM MIC AUDIO HI I 7 500 : COM AUDIO HI O 8 RESERVED I 9 RESERVED I 10 RESERVED I 11 AIRCRAFT POWER I 12 AIRCR[…]
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Page B-12 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.4.2 J26 Table B-13. J26 Descriptions Pin # Pin Name I/O Description 1 +12 VDC I 2 -12 VDC I 3 + 5 VDC I 4 SERIAL_IN I Asynchronous serial input. 5 SERIAL_OUT O Asy nchronous serial output. 6 DC_VOL_CONT I High impedance A/D input. In the unit it is fed by the center tap of a 20K pot […]
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400 SERIES MAINTENANCE MANUAL Page B-13 P/N 190-00140-05 Rev. C Table B-14. J6 Descriptions (continued) 16 500 : VOR/ILS AUDIO HI O 17 500 : VOR/ILS AUDIO LO (GND) O 18 SERIAL DME CLOCK O 19 SERIAL DME DATA O 20 SER DME — CHAN REQ /PAR DME — 4MHZ I/O 21 SER DME — RNAV MODE /PAR DME — 2MHZ I/O 22 VOR/ILS DME COMMON I 23 VOR/ILS 429 OUTB O 24 VOR/ILS[…]
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Page B-14 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.5.2 J10 Table B-15. J10 Descriptions Pin # Pin Name I/O Description 1 +12VDC I 2 +5VDC I 3 GND I 4 -12VDC I 5 VLOC SERIAL IN I Serial input from the Main CPU board to the NAV Board. 6 KEY — This pin is not used. 7 G/S SERIAL IN I Serial input from the Main CPU board to the G/S board.[…]
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400 SERIES MAINTENANCE MANUAL Page B-15 P/N 190-00140-05 Rev. C B.6 GLIDESLOPE BOARD CONNECTORS B.6.1 J25 Table B-17. J25 Descriptions Pin # Pin Name I/O DESCRIPTION 1 +12VDC I 2 +5VDC I 3 GND I Ground. 4 -12VDC I 5 G/S IF AGC O The IF AGC output. 10K output impedance. 6 G/S Composite O Not Used. 7 G/S SERIAL_IN I Serial input from Main Board. 8 G/[…]
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Page B-16 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.8 INVERTER BOARD CONNECTORS B.8.1 J13 Table B-18. J13 Description Pin # Pin Name I/O Description 1 12V I 11 to 14 V dc. 2 CCFT_TA_NOT I Cold Cathode Transmit A Not input. Occurs at 58.5 kHz and is active low. Inverter is capacitor coupled. 3 CCFT_TB_NOT I Cold Cathode Transmit B Not […]
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400 SERIES MAINTENANCE MANUAL Page B-17 P/N 190-00140-05 Rev. C B.8.3 J27 Table B-20. J27 Description Pin # Pin Name I/O DESCRIPTION 1 HEATER VIN O Heater high. The heater typical resistance is 16 ohms. 2 HEATER GND I Heater low. B.9 GPS MODULE CONNECTORS B.9.1 J101 Table B-21. J101 Descriptions Pin # Pin Name I/O DESCRIPTION TRAP 1 I 0 to 12 V dc […]
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Page B-18 400 SERIES MAINTENANCE MANUAL Rev. C P/N 190-00140-05 B.11 DISPLAY MODULE CONNECTORS B.11.1 J22 See LCD Flex description (J12). B.12 DATA BASE CARD CONNECTORS J20 and J21 are the Data Base Card Connectors. B.13 MAP BOARD CONNECTORS B.13.1 P16 Table B-22. P16 Descriptions Pin Name Pin # I/O DESCRIPTION CS_MAPN 1 O Chip Select Map Not. Outp[…]

Источник

Посмотреть инструкция для Garmin Astro 430 бесплатно. Руководство относится к категории GPS-устройства, 7 человек(а) дали ему среднюю оценку 9.3. Руководство доступно на следующих языках: русский, английский. У вас есть вопрос о Garmin Astro 430 или вам нужна помощь? Задайте свой вопрос здесь

Не можете найти ответ на свой вопрос в руководстве? Вы можете найти ответ на свой вопрос ниже, в разделе часто задаваемых вопросов о Garmin Astro 430.

Инструкция Garmin Astro 430 доступно в русский?

Да, руководствоGarmin Astro 430 доступно врусский .

Не нашли свой вопрос? Задайте свой вопрос здесь

Источник

Garmin Astro 430 — это передовая система для отслеживания местоположения собак, которая позволяет контролировать и получать информацию о своем питомце в реальном времени. Эта надежная и простая в использовании система особенно полезна для охотников, у которых есть охотничьи собаки.

Настройка Garmin Astro 430 может показаться сложной задачей для тех, кто впервые сталкивается с этой технологией, но на самом деле она достаточно проста. В этой статье мы рассмотрим пошаговую инструкцию, которая поможет вам быстро и легко настроить вашу систему и быть готовым к использованию ее в полевых условиях.

Примечание: перед настройкой системы Garmin Astro 430 вам нужно установить приложение Garmin Connect на свое мобильное устройство, чтобы связаться с устройством и использовать все его функции.

Содержание

Покупка и распаковка
Загрузка программного обеспечения
Подготовка устройства к использованию
Настройка параметров
Сопряжение с другими устройствами
Начало трекинга

Покупка и распаковка

При покупке Garmin Astro 430 вам потребуется обратить внимание на несколько важных моментов. Во-первых, убедитесь, что вы покупаете товар у официального дилера или надежного продавца, чтобы избежать подделок. Во-вторых, проверьте, что в комплекте есть все необходимые компоненты, такие как приемник, ошейник, зарядное устройство и документация.

Когда вы получите посылку, внимательно рассмотрите ее перед началом распаковки. Убедитесь, что коробка целая и не повреждена. Если вы заметите какие-либо повреждения или отсутствие каких-либо компонентов, обратитесь к продавцу с претензией.

Когда вы готовы начать распаковку, аккуратно разрежьте скотч, который держит коробку закрытой. Откройте коробку и аккуратно извлеките все компоненты. Возможно, их будут держать на месте пенопластовые или картонные вставки. Постепенно извлекайте компоненты и убедитесь, что ничего не потерялось или не пострадало во время транспортировки.

Также обратите внимание на наличие инструкций по установке и использованию. Ознакомьтесь с ними перед тем, как начать настраивать устройство. Если инструкции отсутствуют, вы можете найти их на официальном сайте Garmin, загрузив соответствующую версию для модели Astro 430.

После того как вы убедились, что все компоненты на месте и не повреждены, вы готовы переходить к настройке вашего Garmin Astro 430. Следуйте дальнейшим инструкциям, чтобы настроить устройство и начать его использование.

Загрузка программного обеспечения

Перед началом использования Garmin Astro 430 необходимо загрузить и установить программное обеспечение на компьютере. Это позволит вам взаимодействовать с устройством и получать актуальные данные о местонахождении ваших собак.

Для загрузки программного обеспечения выполните следующие шаги:

Перейдите на официальный сайт Garmin и найдите раздел загрузок.
В списке продуктов найдите Garmin Astro 430 и выберите соответствующую модель.
Нажмите на ссылку для скачивания программного обеспечения.
Сохраните загруженный файл на компьютере и запустите его для начала установки.
Следуйте инструкциям на экране, чтобы завершить установку программного обеспечения.

После успешной установки программного обеспечения вы сможете подключить Garmin Astro 430 к компьютеру и начать настройку устройства с помощью специального приложения.

Подготовка устройства к использованию

Прежде чем начать использовать Garmin Astro 430, необходимо выполнить несколько шагов подготовки.

1. Зарядка аккумулятора

Убедитесь в том, что аккумулятор Garmin Astro 430 полностью заряжен перед использованием. Если аккумулятор не заряжен, подключите устройство к зарядному устройству при помощи кабеля USB и дождитесь полной зарядки.

2. Установка карты памяти

Если вы планируете использовать дополнительную карту памяти для сохранения данных или загрузки карт, убедитесь, что она установлена в устройство. Для установки карты памяти откройте крышку слота карты памяти на задней части устройства, вставьте карту памяти в открытый слот и закройте крышку.

3. Подключение к компьютеру

Если вам требуется подключение Garmin Astro 430 к компьютеру для загрузки данных или обновления программного обеспечения, используйте кабель USB, включив его в USB-порт компьютера и соединив его с устройством. Убедитесь, что компьютер распознает устройство.

4. Установка ошейника на собаку

Перед использованием Garmin Astro 430 убедитесь, что ошейник системы установлен на вашу собаку и надежно крепится. Запустите процесс сопряжения устройства с ошейником, следуя инструкциям в руководстве пользователя.

Следуя этим простым шагам подготовки, вы готовы начать использовать Garmin Astro 430.

Настройка параметров

После установки и активации Garmin Astro 430 вы можете настроить различные параметры устройства для оптимального использования. Вот пошаговая инструкция:

Включите устройство, нажав кнопку питания.
Нажмите на кнопку «Меню» для доступа к главному меню.
Выберите пункт «Настройки» и нажмите кнопку «Enter».
В меню «Настройки» выберите нужные параметры:

Дисплей: здесь вы можете настроить яркость экрана, тему оформления и ориентацию дисплея.
Единицы измерения: выберите метрическую или американскую систему измерений для расстояний, скорости и высоты.
Автоматическое выключение: установите время неактивности, после которого устройство автоматически выключится.
Язык: выберите язык, на котором будут отображаться тексты на устройстве.
Сообщения: настройте параметры отображения сообщений, такие как автоматическое поднятие звука при получении нового сообщения.

Для сохранения изменений нажмите кнопку «Enter».

После настройки параметров вы можете начать использовать Garmin Astro 430 с оптимальными настройками для вас.

Сопряжение с другими устройствами

Garmin Astro 430 может быть сопряжен с другими устройствами, такими как ошейник для собаки или дополнительные приемники, чтобы обеспечить синхронизацию и обмен данными. Сопряжение позволяет получить точные данные о местоположении вашей собаки и передавать их на другие устройства для отображения или дополнительной обработки.

Для сопряжения Garmin Astro 430 с другими устройствами нужно выполнить следующие шаги:

1. Включите Garmin Astro 430 и устройство, с которым вы хотите его сопрячь.

Убедитесь, что оба устройства находятся в радиусе действия друг друга. Они должны находиться на расстоянии не более нескольких метров для оптимальной связи.

2. Откройте меню на Garmin Astro 430.

Используя кнопки навигации, прокрутите список меню и выберите пункт «Сопряжение устройств» или аналогичный пункт, который указывает на сопряжение с другими устройствами.

3. Выберите тип устройства для сопряжения.

На Garmin Astro 430 могут быть представлены различные типы устройств для сопряжения, такие как ошейники для собаки или дополнительные приемники. Используя кнопки навигации, выберите нужный тип устройства из списка.

4. Следуйте инструкциям на экране для завершения сопряжения.

В зависимости от типа устройства, вам могут быть предложены дополнительные настройки или шаги для завершения сопряжения. Следуйте инструкциям на экране и выполните все необходимые шаги.

После успешного сопряжения вы увидите подтверждающее сообщение на Garmin Astro 430 и другом устройстве. Теперь устройства готовы к обмену данными и синхронизации местоположения собаки.

Используя эту пошаговую инструкцию, вы сможете легко сопрячь Garmin Astro 430 с другими устройствами и настроить связь для передачи данных о вашей собаке. Убедитесь, что вы следуете инструкциям производителя для каждого устройства, чтобы обеспечить правильное сопряжение и настройку.

Начало трекинга

После того, как вы настроили Garmin Astro 430 и установили все необходимые компоненты, вы можете начать трекинг вашей собаки. Для этого выполните следующие шаги:

1. Включите устройство

Нажмите и удерживайте кнопку включения на главной панели устройства, пока не появится логотип Garmin. После этого ваш Garmin Astro 430 будет включен и готов к использованию.

2. Проверьте связь с ошейником собаки

Убедитесь, что ошейник собаки находится в пределах диапазона действия устройства и соединен с ним через радиосигнал. Вы должны видеть индикатор связи на главном экране вашего устройства, который показывает качество связи с ошейником.

3. Установите параметры трекинга

Настройте желаемые параметры трекинга на вашем Garmin Astro 430. Вы можете задать такие параметры, как область и время обновления данных о местоположении собаки.

4. Начните трекинг

После настройки всех параметров вы можете начать трекинг вашей собаки. Вы увидите на экране карту с указанием местоположения собаки и вашего текущего местоположения. Настройки трекинга будут автоматически обновляться в соответствии с вашими предпочтениями.

5. Следите за треком собаки

В течение трекинга вы можете наблюдать за местоположением вашей собаки на экране устройства. Вы также можете получать уведомления о изменении местоположения или статусе собаки через звуковые или вибрационные сигналы.

Обратите внимание, что для успешного трекинга необходима достаточная зарядка батареи как у вашего Garmin Astro 430, так и у ошейника собаки.

Источник

Garmin Astro 430 — это передовая система отслеживания местонахождения вашей собаки. Она позволяет вам всегда знать, где находится ваш питомец, и следить за его передвижениями в реальном времени. Но чтобы полностью использовать все возможности этой системы, необходимо правильно ее настроить.

В этом пошаговом руководстве мы расскажем, как настроить Garmin Astro 430, чтобы получить максимальную отдачу от данной системы. Мы покажем, как правильно настроить устройство, связаться с ним с помощью приложения на вашем смартфоне, а также дадим несколько полезных советов по использованию Astro 430.

Шаг 1: Зарядите устройство

Перед началом настройки Garmin Astro 430 важно убедиться, что устройство полностью заряжено. Подключите Astro 430 к зарядному устройству или компьютеру с помощью USB-кабеля и дайте ему полностью зарядиться. Обычно это занимает около 2-3 часов.

Шаг 2: Подключите устройство к приложению

После того, как ваш Astro 430 полностью зарядился, вам необходимо подключить его к приложению на вашем смартфоне. Скачайте и установите приложение Garmin Connect на ваш телефон. Затем откройте приложение и следуйте инструкциям для добавления устройства. Когда Astro 430 обнаружит ваш телефон, подтвердите соединение и введите пароль, если это требуется.

Содержание

Подготовка к использованию Garmin Astro 430: что вам понадобится
Выбор места и времени
Настройка пульта управления
Настройка приемника
Тестирование и настройка дальности сигнала

Подготовка к использованию Garmin Astro 430: что вам понадобится

Перед тем, как приступить к использованию Garmin Astro 430, вам понадобится несколько вещей:

Гармин Astro 430 приемник с GPS-навигацией для охоты с собаками
Комплект зарядных устройств для приемника и ошейника
Ошейник для собаки, оснащенный модулем для GPS-отслеживания
Антенна для улучшения качества сигнала
Компьютер с доступом в интернет
USB-кабель для подключения приемника к компьютеру

Также рекомендуется иметь следующие предметы:

Дополнительный комплект батарей для приемника и ошейника
Футляр или сумка для удобной транспортировки и хранения устройств
Руководство пользователя для ознакомления с функциональностью приемника
Дополнительные аксессуары, такие как защитные чехлы или хомуты для ошейника

Проверьте наличие всех необходимых компонентов и убедитесь, что они находятся в исправном состоянии перед началом использования Garmin Astro 430. Это поможет вам избежать возможных проблем при охоте или тренировке с вашими собаками.

Выбор места и времени

Выбор правильного места и времени для настройки Garmin Astro 430 является важным шагом в процессе его использования. Вот несколько рекомендаций:

Выберите спокойное место. При выборе места для настройки убедитесь, что это тихое и спокойное место, где вас и вашего питомца не будут отвлекать посторонние звуки и движения.
Выберите погодно-климатические условия. Проверьте прогноз погоды перед настройкой Garmin Astro 430. Убедитесь, что погода не будет слишком жаркой или сильно дождливой, чтобы ваш питомец был комфортным и удобно проводил время во время настройки.
Выберите удобное время. Выберите время, когда ваш питомец будет наиболее спокоен и настроен на сотрудничество. Лучше всего проводить настройку в течение дня, когда ваш питомец сыт, активен и не спит.

Убедитесь, что место и время настройки Garmin Astro 430 соответствуют вашим требованиям и потребностям вашего питомца. Таким образом, вы сможете добиться лучшей эффективности от использования устройства.

Настройка пульта управления

Чтобы настроить пульт управления Garmin Astro 430, выполните следующие шаги:

Убедитесь, что пульт управления включен и находится в пределах радиуса действия с базовой станцией.
Нажмите на кнопку «Меню» на пульте управления.
Используя кнопки навигации, выберите пункт «Настройки» и нажмите кнопку «Выбор».
Выберите пункт «Система» и нажмите кнопку «Выбор».
В меню «Система» выберите пункт «Настройки радиосвязи» и нажмите кнопку «Выбор».
Выберите пункт «Основные настройки» и нажмите кнопку «Выбор».
Настройте необходимые параметры радиосвязи, такие как частота и мощность передачи. Используйте руководство пользователя для получения подробных инструкций по этим параметрам.
Нажмите кнопку «Готово» для сохранения настроек.

После выполнения этих шагов пульт управления должен быть готов к использованию и связан с базовой станцией. Убедитесь, что пульт управления корректно отображает информацию о подключенных приемниках и установленных настройках радиосвязи. Если у вас возникли проблемы с настройкой пульта управления, обратитесь к руководству пользователя или свяжитесь с технической поддержкой Garmin.

Настройка приемника

Приступая к настройке Garmin Astro 430, необходимо убедиться, что у вас есть все необходимые компоненты:

Приемник Garmin Astro 430
Антенна для GPS сигнала
Антенна для радиосигнала
Комплект зарядного устройства и аккумуляторов
Компьютер с установленным программным обеспечением BaseCamp

После того как вы убедились, что у вас есть все необходимое оборудование, приступайте к настройке приемника:

Установите антенну для GPS сигнала на соответствующий порт приемника. Убедитесь, что антенна установлена надежно и никакие провода не повреждены.
Установите антенну для радиосигнала на соответствующий порт приемника.
Подключите зарядное устройство к приемнику и подключите его к розетке для зарядки. Убедитесь, что приемник начал заряжаться.
Включите приемник, нажав и удерживая кнопку питания. Приемник должен включиться и показать экран приветствия.
Установите программное обеспечение BaseCamp на компьютер, следуя инструкциям производителя. Подключите приемник к компьютеру, используя кабель USB, и запустите программу BaseCamp.
В программе BaseCamp выберите опцию «Настройки приемника» и следуйте инструкциям на экране, чтобы настроить свой приемник и установить необходимые параметры.

После завершения настройки приемника вы будете готовы использовать Garmin Astro 430 для отслеживания своих домашних животных или других объектов. Убедитесь, что вы правильно установили и настроили все компоненты, чтобы обеспечить максимальную точность и надежность при использовании системы.

Тестирование и настройка дальности сигнала

Правильная настройка дальности сигнала для Garmin Astro 430 — важный аспект работы с устройством, который позволяет определить максимальное расстояние, на котором вы сможете отслеживать свою собаку.

Для начала вам понадобится надежное пространство без помех, например, открытая поляна или пустырь. Затем выполните следующие шаги, чтобы протестировать и настроить дальность сигнала:

Установите ошейник с Garmin T 5 Mini на шею собаки и убедитесь, что он надежно закреплен.
Включите приемник Astro 430 и перейдите в меню настройки дальности сигнала.
Выберите опцию «Тестирование дальности сигнала» и следуйте инструкциям на экране для начала тестирования.
Позвольте собаке свободно передвигаться на заданном расстоянии. Убедитесь, что она находится в пределах видимости.
Измерьте расстояние, на котором вы все еще получаете сигнал от ошейника. Это значение является вашей дальностью сигнала.

На основе этого теста вы сможете настроить дальность сигнала в соответствии с вашими потребностями и условиями эксплуатации.

Обратите внимание, что фактическая дальность сигнала может быть ограничена различными факторами, такими как препятствия (например, деревья или здания), территория (открытая или закрытая), типы почвы и т. д. Поэтому тестирование и настройка дальности сигнала должны проводиться в условиях, близких к тем, в которых вы планируете использовать Garmin Astro 430 на практике.

Помните, что правильная настройка дальности сигнала поможет вам контролировать свою собаку на расстоянии, минимизируя риск потери и обеспечивая ее безопасность.

Источник

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Page 3: Foreword

Page 7: Table Of Contents

Page 8: Table Of Contents

Page 9: Takeoff Tour

Page 11: Bottom Row Keys

Page 19: Aux Group

Page 24: Nearest Airports

Page 26: Special-Use/Controlled Air Space

Page 29: Section 1: Communicating With The Gns 430

Page 34: Emergency Channel

Page 35: Section 2: Nav Page Group (Gps Navigation)

Page 38: Restoring Factory Settings

Page 41: Map Panning

Page 42: Airspace Information On The Map

Page 45: Distance Measurements

Page 47: Navcom Page

Page 49: Position Page

Page 52: Satellite Status Page

Page 54: Vertical Navigation Page

Page 57: Section 3: Direct-To Navigation

Page 58: Selecting A Destination By Facility Name Or City

Page 59: Using The

Page 61: Specifying A Course To A Waypoint

Page 62: Section 4: Flight Plans ( Key And Fpl

Page 63: Flight Plan Editing

Page 64: Activating Flight Plans

Page 65: Copying Flight Plans

Page 66: Flight Plan Catalog Options

Page 67: Active Flight Plan

Page 68: Active Flight Plan Options

Page 74: Section 5: Approaches, Departures And Arrivals ( Key)

Page 76: Basic Approach Operations

Page 77: Approaches With Procedure Turns

Page 78: Flying The Procedure Turn

Page 80: Flying The Missed Approach

Page 81: Flying An Approach With A Hold

Page 87: Vectors To Final

Page 90: Course From Fix Flight Plan Legs

Page 94: Ils Approaches

Page 102: Section 6: Wpt Page Group (Waypoint/Database Information)

Page 104: Duplicate Waypoints

Page 105: Airport Location Page

Page 106: Airport Runway Page

Page 107: Airport Frequency Page

Page 110: Airport Approach Page

Page 111: Airport Approach Page Options

Page 112: Airport Arrival Page

Page 113: Airport Arrival Page Options

Page 114: Airport Departure Page

Page 115: Airport Departure Page Options

Page 116: Intersection Page

Page 119: User Waypoint Page

Page 120: Creating User Waypoints

Page 122: Modifying User Waypoints

Page 124: User Waypoint Page Options

Page 127: Section 7: Nrst Page Group (Nearest Airports, Etc.)

Page 129: Navigating To A Nearby Waypoint

Page 131: Nearest Intersection Page

Page 133: Nearest User Waypoint Page

Page 135: Nearest Airspace Page

Page 139: Section 8: Vloc (Vor/Localizer/Glideslope) Receiver Operations

Page 143: Section 9: Aux Page Group (Flight Planning And Unit Settings)

Page 144: Flight Planning Page

Page 153: Utility Page

Page 160: Setup 1 Page

Page 171: Section 10: Fde (Fault Detection Exclusion)

Page 173: Section 11: Messages, Abbreviations & Navigation Terminology

Page 187: Appendix A: Navdata Card Use

Page 188: Appendix B: Specifications

Page 189: Appendix C: Map Datums

Page 191: Appendix D: Troubleshooting Q & A

Page 197: Appendix E: Index

Page 1: Garmin GNS 430

Page 2: Garmin GNS 430

Page 3: Garmin GNS 430

Page 4: Garmin GNS 430

Page 5: Garmin GNS 430

Page 6: Garmin GNS 430

Page 7: Garmin GNS 430