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 2nd Road, Shijr, Taipei County, Taiwan
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express prior
written consent of GARMIN. GARMIN hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to be
viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or
printed copy of this manual or revision must contain the complete text of this copyright notice and
provided further that any unauthorized commercial distribution of this manual or any revision hereto is
strictly prohibited.
Information in this document is subject to change without notice. GARMIN reserves the right to change or
improve its products and to make changes in the content without obligation to notify any person or
organization of such changes or improvements.
GARMIN International, Inc.
1200 E. 151
st
Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
Aviation Panel-Mount Technical Support Line (Toll Free): 1-888-606-5482
www.garmin.com
RECORD OF REVISIONS
REVISIONREVISION
DATE
A07/06/99Initial Release-----
B01/26/01Redraw15007
C10/22/02Redraw19319
DescriptionECO #Insertion DateBy
GNC and GNS are trademarks of GARMIN Ltd. or its subsidiaries and may not be used without the express permission of GARMIN.
Page A400 SERIES MAINTENANCE MANUAL
Rev. C P/N 190-00140-05
400 SERIES MAINTENANCE MANUAL Page i
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.
KEEP AWAY FROM LIVE CIRCUITS.
Maintenance personnel shall observe all safety
regulations at all times. Do not replace components inside the equipment when potentially lethal
voltages are present. Turn off system power before making or breaking electrical connections.
Regard any exposed connector, terminal board, or circuit board as a possible shock hazard.
Components which retain a charge shall be discharged only when such grounding does not result
in equipment damage. If a test connection to energized equipment is required, make the test
equipment ground connection before probing the voltage or signal to be tested.
DO NOT SERVICE ALONE.
Personnel shall not under any circumstances reach into or enter
any enclosure for the purpose of servicing or adjusting the equipment without immediate
presence or assistance of another person capable of rendering aid.
INFORMATION SUBJECT TO EXPORT CONTROL LAWS
This document may contain information which is subject to the Export Administration
Regulations (“EAR”) issued by the United States Department of Commerce (15 CFR, Chapter
VII, Subchapter C) and which may not be exported, released, or disclosed to foreign nationals
inside or outside of the United States without first obtaining an export license. A violation of the
EAR may be subject to a penalty of up to 10 years imprisonment and a fine of up to
US $1,000,000 under Section 2410 of the Export Administration Act of 1979. Include this notice
with any reproduced portion of this document.
400 SERIES HARDWARE MOD LEVEL HISTORY
The following table identifies hardware modification (Mod) Levels for the 400 Series.
Mod Levels are listed with the associated service bulletin number, service bulletin date, and the
purpose of the modification. The table is current at the time of publication of this manual (see
date on front cover) and is subject to change without notice. Authorized GARMIN Sales and
Service Centers are encouraged to access the most up-to-date bulletin and advisory information
on the GARMIN Dealer Resource web site at www.garmin.com using their GARMIN-provided
user name and password.
Mod
Level
1SB0019Nov 7, 200014/28V only, Comm Transmitter Fuse
2SB0101Feb 16, 200114/28V only, Remote COM Transfer
3SB0203Feb 1, 2002430/420; 14/28V only (-10 and –30), Receiver Audio
4SB0207Apr 2, 2002430/420; Remove excessive solder from Comm Board vias
Service
Bulletin
Number
Service
Bulletin Date
Purpose of Modification
Compressor (recommended only if problem exists)
Page ii 400 SERIES MAINTENANCE MANUAL
P/N 190-00140-05 Rev. C
Page xii 400 SERIES MAINTENANCE MANUAL
P/N 190-00140-05 Rev. C
SECTION 1
DESCRIPTION AND OPERATION
1.1INTRODUCTION
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 information for the GARMIN 400 Series of
products. Table 1-1 shows each unit in the 400 series and their configurations. The system allows
the Main Processor software to recognize which of the optional components (VHF
Communications Transceiver, VOR/LOC receivers, and Glideslope receiver) are present.
Table 1-1. Unit Configuration
GPS 400GNC 420GNS 430
Main Processor
GPS Receiver
VHF Com Transceiver
VOR/ILS Localizer Receivers
ILS Glideslope Receiver
1.1.1Versions Covered by this Manual
This manual applies to the GPS 400, GNC 420, and the GNS 430. It also applies to the
GNC 420A and the GNS 430A. The “A” identifies the 16 watt VHF COM transmitter as opposed
to the 10 watt version. Appendix A describes the GNC 420A and the GNS 430A. For ease of
identification, the following tables contain part number information relative to the different
versions of the 400 Series:
400 SERIES MAINTENANCE MANUALPage 1-1
P/N 190-00140-05Rev. C
GPS 400:
GNC 420:
UNIT P/NCOLOR
011-00504-00Black
011-00504-10Gray
GNS 430:
GNC 420A:
UNIT P/NCOLOROPERATING
VOLTAGE
011-00506-00BLACK28 V10 W
011-00506-10BLACK14 or 28 V10 W
011-00506-30GRAY14 or 28 V10 W
UNIT P/NCOLOROPERATING
VOLTAGE
011-00280-00BLACK28 V10 W
011-00280-10BLACK14 or 28 V10 W
011-00280-30GRAY14 or 28 V10 W
UNIT P/NCOLOROPERATING
VOLTAGE
011-00837-00BLACK28 V only16 W
MINIMUM
XMIT PWR
MINIMUM
XMIT PWR
MINIMUM
XMIT PWR
011-00837-10GRAY28 V only16 W
GNS 430A:
UNIT P/NCOLOROPERATING
VOLTAGE
011-00836-00BLACK28 V only16 W
011-00836-10GRAY28 V only16 W
Page 1-2400 SERIES MAINTENANCE MANUAL
Rev. CP/N 190-00140-05
MINIMUM
XMIT PWR
Each of the configurations includes a color display providing graphical moving map capability.
Navigation, communication, and mapping functions are supported by a navigation database
provided by a removable database card. The mapping function has additional support provided
by a built-in ground features base map which may be supplemented by a detailed map provided
on a second removable database card.
Information relative to the installation and operation of the 400 Series is found in the 400 Series
Installation Manual, P/N 190-00140-02.
1.2FUNCTIONAL SUMMARY
1.2.1GPS 400
ƒPosition and velocity determination using signals transmitted by Global Positioning
System (GPS) Satellites.
ƒ Display of the stored navigation and map database for use by the pilot/flight crew.
ƒ Area navigation functions using the determined position/velocity and stored
navigation data.
ƒ Approach navigation functions and the associated database.
ƒ Interfacing with other flight instruments such as a moving map, autopilot, CDI/HSI
(including OBS), indicators, altitude encoder/serializer, fuel management system, and
annunciators.
ƒ14 or 28 volt operation.
1.2.2 GNC 420
ƒ Performs all functions of a GPS 400.
ƒ Communications transceiver tuning from 118.000 to 136.9916 MHz in 25 kHz or
8.33 kHz increments.
ƒ Com audio output.
ƒ 10 or 16-watt transmitter.
ƒ 14 or 28 volt operation for 10 watt transmitter;
28 V only for 16 watt transmitter.
1.2.3GNS 430
ƒ Performs all functions of a GNC 420.
ƒ VOR and ILS Localizer Receivers.
ƒ ILS Glideslope Receiver.
400 SERIES MAINTENANCE MANUALPage 1-3
P/N 190-00140-05Rev. C
1.3REPAIR 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.
1.4SPECIFICATIONS
Technical specifications for each unit are given in the 400 Series Installation Manual,
P/N 190-00140-02.
1.5GENERAL DESCRIPTION
To help understand the general description, Appendix B lists all
external and internal I/O signal descriptions for each unit. Also,
see Figure 3-7 for a block diagram, which shows all of the
external and internal connectors for each board.
1.5.1 Main Board
The Main Board is the functional center of the unit. The Main Board communicates with all the
components of the unit, and provides the interface with the pilot and other avionics installed in
the aircraft.
The Main Board performs the following functions:
1. Communicates with all components of the unit.
2. Displays and controls interface with the pilot.
3. Displays the navigation database via a removable memory card for use by the
pilot/flight crew.
4. Area navigation functions using the determined position/velocity and stored
navigation data.
5. Interfaces with other flight instruments such as a moving map autopilot, CDI/HSI,
indicators, altitude encoder, fuel management system, and annunciators.
Page 1-4400 SERIES MAINTENANCE MANUAL
Rev. CP/N 190-00140-05
1.5.2Com Board
The Com Board contains the VHF COM Transceiver that provides voice communication in the
118.000 to 136.992 MHz general aviation band. The transceiver consists of a 10 or 16 watt (“A”
versions) amplitude modulated transmitter (see the unit matrix tables on page 1-1), and a single
conversion superhetrodyne AM receiver. The 10 watt transmitters are Class 4 and 6 devices as
described in RTCA DO-186A, indicating that they have channel spacing modes of 25 kHz and
8.33 kHz, and are intended for a communications range of 100 nautical miles. The 16 watt
transmitters are class 3 and 5 devices as described in RTCA DO-186A, indicating that they have
channel spacing modes of 25 kHz and 8.33 kHz and are intended for a communications range of
200 nautical miles.
The receiver is a Class C and E device as described in RTCA DO-186A, indicating that it has
channel spacing modes of 8.33 kHz and 25 kHz, with offset carrier capability in 25 kHz mode.
The Com Board contains connectors J2 and J26. J4 is the Com BNC antenna connector.
1.5.3Nav Board
The Nav Board contains the processor controlled navigation receiver for VOR and Localizer
signals from 108.00 MHz to 117.95 MHz in 50 kHz increments providing 200 channels.
Functionally, the Nav Board performs the following:
1. Tunes a VOR or localizer frequency as commanded by the Main Board.
2. Communicates VOR/LOC receiver sub-system status to the Main Board.
3. Communicates VOR radial or localizer deviation, TO/FROM flag state and
navigation flag state to the Main Board.
4. Drives horizontal deviation, flag and TO/FROM electrical outputs.
5. Receives glideslope data from the Main Board to be sent out in ARINC 429 format.
6. Toggles the VOR/LOC identifier filter as commanded by the Main Board.
7. Communicates to the Main Board the detection of a remote frequency transfer key
press.
8. Drives electrical outputs for OBI.
9. Channels a remote DME if connected to the VOR/LOC Receiver Board.
10. Transmits ARINC 429 labels.
11. Receives ARINC 429 labels.
12. Provides signal pass-through for G/S flags and drivers to NAV Board Connectors.
1.5.4 GPS Module
The GPS Module contains a twelve channel parallel receiver that is capable of tracking and using
up to twelve visible satellites for position, velocity, and time calculations. The GPS Receiver is
designed to operate with the GARMIN GA 56 antenna (P/N 011-00134-00). The GPS Module
interfaces with the Main Board via connector J101.
400 SERIES MAINTENANCE MANUALPage 1-5
P/N 190-00140-05Rev. C
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 Assembly
The main components of the CDU Assembly are the Liquid Crystal Display (LCD), Keyboard
Assembly, and the Interface Board. The display portion consists of a 3-color RGB DSTN type
LCD, 128 x 240 pixels. The keyboard assembly consists of the snap-dome keys, photocell and
LED’s for backlighting display operation. The Interface Board is simply an interconnect
containing no active components. Unit switches and volume pots are mounted in the CDU.
1.5.8 Map Board
The Map Board is physically connected to the Main Board via P16. The Map Board consists of a
map data storage device (ROM or flash). The map storage device contains base map data used to
store topographical information (highways, lakes, rivers, and railroads).
Page 1-6400 SERIES MAINTENANCE MANUAL
Rev. CP/N 190-00140-05
SECTION 2
SPECIAL TOOLS AND TEST EQUIPMENT
2.1INTRODUCTION
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 following address:
GARMIN
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
Aviation Panel Mount Technical Support Line (Toll Free): 1-888-606-5482
Website Address: www.garmin.com
2.2SPECIAL TOOLS AND TEST EQUIPMENT
x Test Panel—See paragraph 2.3.
x Test Cables—See paragraph 2.3.
x Thinly Ground Open End Wrench for removing COM BNC Chassis Nut (on units
with serial numbers of approximately 96303300 and lower).
Figure 2-1. COM Chassis Nut
2.3TEST PANELS AND CABLES
Test panels and cables are to be supplied by the repair facility. Load and signal information
given in Figures 2-2 through 2-5 and the information listed in Appendix B can help in their
fabrication.
400 SERIES MAINTENANCE MANUALPage 2-1
P/N 190-00140-05Rev. C
This page left intentionally blank.
Page 2-2 400 SERIES MAINTENANCE MANUAL
Rev. CP/N 190-00140-05
400 SERIES MAINTENANCE MANUALPage 2-3 (Page 2-4 blank)
P/N 190-00140-05Rev. C
Figure 2-2. J1 Signal and Load Drawing (Sheet 1 of 2)
400 SERIES MAINTENANCE MANUALPage 2-5 (Page 2-6 blank)
P/N 190-00140Rev. C
Figure 2-3. J1 Signal and Load Drawing (Sheet 2 of 2)
400 SERIES MAINTENANCE MANUALPage 2-7 (Page 2-8 blank)
P/N 190-00140-05Rev. C
Figure 2-4. J2 Signal and Load Drawing
400 SERIES MAINTENANCE MANUALPage 2-9 (Page 2-10 blank)
P/N 190-00140-05 Rev. C
Figure 2-5. J6 Signal and Load Drawing
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 to peak. Under open circuit conditions voltages
can range over 8000 Vac peak to peak. Exercise extreme
caution during unit troubleshooting. Death or serious injury
could result from electrical shock. See other general
maintenance warnings and cautions on page ii.
3.1TROUBLESHOOTING EQUIPMENT
The equipment used in testing a unit can be used to troubleshoot a faulty unit. See Sections 2 and
5.
3.2TROUBLESHOOTING ORDER
Start troubleshooting a unit by following steps one through three listed below (not necessarily in
the order listed). Once it has been determined that these three items are not the cause of failure,
proceed with troubleshooting using the static messages and performance testing (paragraphs 3.4
and 3.5). To help in the troubleshooting process, a block diagram and external connectors are
shown at the end of this section. In addition, Appendix B describes all of the input/output signals
for all of the unit’s internal and external connectors.
1. Fuses (Paragraph 3.3.1).
2. Power Supply Checks (Paragraph 3.3.2).
3. Processor Clock Check (Paragraph 3.3.3).
400 SERIES MAINTENANCE MANUAL Page 3-1
P/N 190-00140-05 Rev. C
3.3 TROUBLESHOOTING PROCEDURES
0
3.3.1Fuses
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.
F85
5A
F852
2A
F854
5A
F853
0.75A
F851
3A
Figure 3-1. Main Board Fuse Locations
Page 3-2 400 SERIES MAINTENANCE MANUAL
Rev. C P/N 190-00140-05
LOCATION 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 PRESENT
(F600 REPLACED
WITH R611, EXCEPT
ON -04 REV A AND B
BOARD)
Figure 3-3. Com Board Fuse Location/F600 (Replaced by R611)
400 SERIES MAINTENANCE MANUAL Page 3-3
P/N 190-00140-05 Rev. C
F501
1 AMP
F502
1 AMP
Figure 3-4. Nav Board Fuse Locations
3.3.2Power Supply Checks
3.3.2.1Current Measurements
J6
Taking intra-board and external current measurements is one way of determining a faulty board.
To measure the currents, use a spare ribbon cable and spread the cable wires, then use a DC probe
to measure the current in the appropriate wire (connector pin). The following external and
intra-board current measurements can be taken during troubleshooting (the intra-board currents
are given as reference):
x Com Board (Tables 3-2 and 3-3):
J26: Intra-board (Main Board to Com Board)
J2: External Connector
x Glideslope Board (Table 3-4):
J25: Intra-board (Nav Board to Glideslope Board)
x Nav Board (Table 3-4):
J10: Intra-board (Main Board to Nav Board)
J6: External Connector
Page 3-4 400 SERIES MAINTENANCE MANUAL
Rev. C P/N 190-00140-05
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