GNC 300
INSTALLATION MANUAL
GARMIN INTERNATIONAL, INC.
1200 E. 151st STREET
PART NUMBER: 190-00067-02
REVISION J, 30 MARCH 1998
OLATHE, KANSAS 66062-3426
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 1
Download from Www.Somanuals.com. All Manuals Search And Download.
TABLE OF CONTENTS
SECTION 1
GENERAL DESCRIPTION
1.1
INTRODUCTION
1.2
TECHNICAL CHARACTERISTICS
PHYSICAL CHARACTERISTICS
OPERATIONAL CHARACTERISTICS
INTERFACES
1.2.1
1.2.2
1.2.3
1.3
LICENCE REQUIREMENTS
SECTION 2
INSTALLATION CONSIDERATIONS
2.1
ANTENNA CONSIDERATIONS
GPS ANTENNA LOCATION
COMM ANTENNA LOCATION
ELECTRICAL BONDING
2.1.1
2.1.2
2.1.3
2.1.4
2.1.5
2.1.6
2.2
ANTENNA LIMITATIONS
VHF COMM INTERFERENCE OF GPS
COMM ANTENNA INSTALLATION CONSIDERATIONS
RACK CONSIDERATIONS
2.2.1
2.3
ACCESSIBILITY
CABLING AND WIRING
2.4
COOLING AIR
2.5
2.6
MINIMUM INSTALLATION REQUIREMENTS
EXTERNAL ALTITUDE INPUT
SECTION 3
INSTALLATION PROCEDURE
3.1
3.2
3.3
3.4
3.5
3.6
INSTALLATION ACCESSORIES
ANTENNA INSTALLATION
CABLE INSTALLATION
RACK INSTALLATION
GNC 300 INSTALLATION AND REMOVAL
COMM ANTENNA INSTALLATION CHECK
SECTION 4
POST INSTALLATION CONFIGURATION &
CHECKOUT PROCEDURE
SECTION 5
SECTION 6
CERTIFICATION
CONTINUED AIRWORTHINESS
APPENDIX A
APPENDIX B
APPENDIX C
CERTIFICATION DOCUMENTS
CONNECTOR CHANGES
STC PERMISSION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 3
Download from Www.Somanuals.com. All Manuals Search And Download.
LIST OF ILLUSTRATIONS
FIGURE
1-1
1-2
PINOUT DEFINITION, 37 PIN DSUB
PINOUT DEFINITION, 26 PIN HD-DSUB
INTERCONNECT SCHEMATIC
1-3
1-4
2-1
2-2
2-3
3-1
3-2
3-3
INTERCONNECT SCHEMATIC NOTES
GPS ANTENNA INSTALLATION CONSIDERATIONS
GNC 300 INSTALLATION CONSIDERATIONS
SWITCH/ANNUNCIATOR LAYOUT
STUD MOUNT GA 56 INSTALLATION
FLANGE MOUNT GA 56 INSTALLATION
COAX CABLE INSTALLATION
3-4
AVIATION RACK DIMENSIONS
3-5
AVIATION RACK INSTALLATION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 4
Download from Www.Somanuals.com. All Manuals Search And Download.
SECTION 1 GENERAL DESCRIPTION
1.1 INTRODUCTION
This manual describes the physical, mechanical, and electrical characteristics and
the installation requirements for the GNC 300 Aviation Kit.
After installation of the GNC 300 system, FAA Form 337 must be completed by an
appropriately certificated agency to return the aircraft to service.
1.2 TECHNICAL CHARACTERISTICS
TheGNC300offerstheversatilityoffixedinstallationinapanelmountedaviationrack
as well as complete portability.
For TSO Compliance, see Appendix A.
The conditions and tests required for TSO approval of this article are minimum
performance standards. It is the responsibility of those desiring to install this article
either on or within a specific type or class of aircraft to determine that the aircraft
installationconditionsarewithintheTSOstandards. Thearticlemaybeinstalledonly
if further evaluation by the applicant documents an acceptable installation and is
approved by the Administrator.
1.2.1 PHYSICAL CHARACTERISTICS
Width:
Height:
Depth:
6.25 inches
2 inches
5.65 inches
2.4 lbs.
4 oz.
10 oz.
GNC 300 Weight:
GA 56 Antenna Weight:
Aviation Rack Weight:
Max Air Speed:
(Structural rating for antenna)
Subsonic
1.2.2 OPERATIONAL CHARACTERISTICS
Operating Temperature Range:
Humidity:
Altitude Range:
-20oC to +55oC
95% non-condensing
-1,500 to 50,000 ft.
Power Range
10 to 15.1 VDC
Power Requirements:
1.2A @ 13.8v (not transmitting)
5.5A @ 13.8V (transmitting)
1.2.3 INTERFACES
The GNC 300 provides interfaces to various general aviation instruments. Figure 1-
1 defines the function of each pin on the 37 pin DSUB connector located at the back
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 5
Download from Www.Somanuals.com. All Manuals Search And Download.
of the rack. Figure 1-2 defines the function of each pin in the 26 pin HD-DSUB
connector (J102) located above the 37 pin connector at the back of the rack. Figures
1-3 and 1-4 defines the interconnects between the rack and other instruments. The
following interfaces are provided.
1.2.3.1 37 PIN CONNECTOR (J101)
CDI:
(Pins 1 and 4)
Capable of driving up to three 1000 ohm parallel
loads, +150 millivolts full scale deflection with a
maximum output of +300 millivolts.
To/From:
(Pins 2 and 4)
Capable of driving up to three 200 ohm parallel
loads, +82 millivolts full scale deflection.
Units with Mod Status 1: +190 millivolts full scale deflec-
tion.
Nav Flag:
(Pins 3 and 4)
Capable of driving up to three 1000 ohm parallel
loads, 375 millivolts for flag out-of-view, and
+40 millivolts for flag in-view.
OBI data:
(Pins 7, 8, and 23)
Output providing bearing to waypoint data for a
Bendix/King RMI (KI 229 or equivalent).
Message annunciator:
(Pin 20)
Output capable of driving negative logic message
annunciators by sinking up to 500mA.
RS232 chan 1 output data:Output capable of driving devices as listed in Section 4.
(Pin 24) Conforms to the EIA specification RS-232C.
RS232 chan 2 output data:Output capable of driving devices as listed in Section 4.
(Pin 19) Conforms to the EIA specification RS-232C.
RS232 chan 1 input data: Input capable of receiving data from devices listed in
(Pin 17)
Section 4. Conforms to the EIA specification RS-232C.
Arrival annunciator:
(Pin 12)
Output capable of driving negative logic annunciator
by sinking up to 500mA.
GPS approach active ann: Output capable of driving negative logic annunciator
(Pin 13)
by sinking up to 500mA. See GNC 300 Pilot's Guide,
(GPN 190-00067-00), for more information.
GPS approach arm ann:
(Pin 28)
Output capable of driving negative logic annunciator
by sinking up to 500mA. See GNC 300 Pilot's Guide,
(GPN 190-00067-00), for more information.
ARINC 429 Output A & B: Output capable of interfacing with any device that has
(Pins 15 and 16)
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 6
an input conforming to the GAMA ARINC 429 (low
speed) specification.
Download from Www.Somanuals.com. All Manuals Search And Download.
NAV Super Flag Output: Output capable of driving positive logic NAV Super
(Pin 10)
Flag by sourcing up to 500mA for flag out of view (NAV
valid).
RS422 input:
(Pins 11 & 27)
Input capable of receiving serial OBS data from
Collins Pro Line 2 EFIS DSP unit.
GPS approach arm low:
(Pin 9)
Input, when grounded, controls approach mode.
Capable of interfacing with a standard OBS resolver.
GPS OBS:
(Pins 4,14,35 and 37)
ARINC 429 Input A & B:
(Pins 32 & 33)
Input capable of receiving data from ARINC 429 (low
speed) devices as listed in Section 4.
Battery +,-, Charge Enable Connection for GARMIN remote battery accessory.
(Pins 30, 34, 29)
1.2.3.2 26 PIN CONNECTOR (J102)
MIC Audio Hi and Lo::
(Pins 2 and 3)
Input requiring 275mV RMS into 470 ohm load.
(Standard carbon or dynamic MIC containing
transistorized pre-amp.)
MIC Key:
(Pin4)
Input, when grounded, keys the transmitter.
COMM Audio Hi and Lo:
(Pins 5 and 6)
Output capable of driving a 500 ohm load with
100mW.
MIC Intercomm:
(Pin 8)
Input requiring 125mV RMS into 470 ohm load.
(Standard carbon or dynamic MIC containing
transistorized pre-amp.)
Remote Transfer:
(Pin 10)
Input, when grounded, swaps the active and
standby COMM frequencies.
TX Interlock:
(Pin 12)
Input, when grounded, reduces receiver sensitivity
so squelch will not break when another transceiver is
keyed.
Altimeter input:
(Pins 14-24)
Capable of receiving encoded output data from any
parallel altimeter device.
Remote Enter:
(Pin 26)
Input, when ground, functions the same as the enter
key on the GNC 300 front panel.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 7
Download from Www.Somanuals.com. All Manuals Search And Download.
Sequence Hold Low:
(Pin 13)
Input, when grounded, activates HOLD mode. See
the GNC 300 Pilot's Guide (GPN 190-00067-00) for
more information.
1.2.3.3 COMM Antenna Connector (J4)
Capableofproviding5watts, minimum, at13.8V. Sensitivityof6dBSNR, minimum,
at 2 uV hard. The COMM antenna shall be approved to TSO C37( ) and C38( ).
1.3 LICENCE REQUIREMENTS
The transmitter, as installed in the aircraft, requires an Aircraft Radio Station
Licence. This licence is obtained by filing the FCC Form 404. While awaiting the
receipt of the station licence, a copy of FCC Form 404 is kept in the aircraft.
This equipment has been type accepted by the FCC and entered on the type ac-
cepted equipment list, as GARMIN GNC 300 and must be identified as GARMIN
GNC 300 on your Form 404, Aircraft Radio Station Licence application.
CAUTION
THE VHF TRANSMITTER IN THIS EQUIPMENT IS GUARANTEED TO MEET
FEDERAL COMMUNICATIONS COMMISSION ACCEPTANCE OVER THE OPER-
ATING TEMPERATURE RANGE. MODIFICATIONS NOT EXPRESSLY APPROVED
BY GARMIN COULD VOID THE LICENCES' AUTHORITY TO OPERATE THE
EQUIPMENT.
SECTION 2 INSTALLATION CONSIDERATIONS
Careful planning and consideration of the suggestions in this section are required to
achieve the desired performance and reliability from the GNC 300.
2.1 ANTENNA CONSIDERATIONS
2.1.1 GPS ANTENNA LOCATION
The GNC 300 GA 56 Antenna must be mounted on top of the aircraft. For best
performance select a location with an unobstructed view of the sky above the aircraft
when in level flight. Figure 2-1 illustrates a typical GPS antenna installation.
For rotorcraft, locate the GA 56 antenna:
1) As far from the main rotor hub as possible. This reduces the percentage of time
the blade blocks the antenna.
2) Asfarbelowthebladesurfaceaspossibleifinstallingtheantennaundertheblade.
This reduces signal distortion caused by the blades.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 8
Download from Www.Somanuals.com. All Manuals Search And Download.
Theantennashouldbelocatedatleast3feetfromtransmittingantennassuchasVHF
Comm, HF transmitter, DME, Transponder, and Radar.
2.1.2 COMM ANTENNA LOCATION
The COMM antenna should be well removed from all projections, engines and
propellers. Thegroundplanesurfacedirectlybelowtheantennashouldbeaflatplane
over as large an area as possible (18 inches square minimum).
The antenna should be mounted a minimum of 6 feet away from any DME antennas,
4 feet from any ADF sense antennas, and a minimum of 3 feet from the GNC 300 and
its GPS antenna.
TheGNC300COMMantennaconnectorisspecifiedtohaveinstalledGPN330-00067-
00 (1.57542 GHz notch filter) to minimize interfering harmonics.
2.1.3 ELECTRICAL BONDING
No special precautions need to be taken to provide a bonding path between the GPS
antenna and the aircraft structure.
Follow the manufacturers instructions for the COMM antenna.
2.1.4 ANTENNA LIMITATIONS
GARMIN'S GA 56 Antennas are recommended for installations where the airspeed of
the aircraft will be subsonic.
GARMIN's GA 56, Mod 1 or later, must be used.
See the COMM antenna specification for its limitations.
2.1.5 VHF COMM INTERFERENCE OF GPS
On many panel-mounted aircraft, VHF COMM's can radiate strong harmonics from
the unit and antenna. The GNC 300 COMM section will not interfere with its GPS
section. However, placement of the GNC 300 GPS antenna relative to all COMM's and
COMM antenna, including its own, is critical.
Usethefollowingguidelines, inadditiontoothersinthisdocument, whenlocatingthe
GNC 300 and its antennas.
GPS Antenna:
Locate as far as possible from all COMM antennas
and all COMMs (including the GNC 300). The GPS
antenna will be much less sensitive to COMM antennas that
use a 1.57542 GHz notch filter.
GNC 300:
Locate as far as possible from all COMM antennas.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 9
Download from Www.Somanuals.com. All Manuals Search And Download.
If a COMM antenna is found to be the problem, a 1.57542 GHz notch filter (GPN 330-
00067-00)maybeinstalledintheVHFCOMMcoax, asclosetotheCOMMaspossible.
This filter (GPN 330-00067-00) is required for the GNC 300 transmitter).
If a COMM is found to be radiating, the following can be done:
1)
2)
3)
ReplaceorcleanVHFCOMMrackconnectortoassuregoodcoaxground.
Place a grounding brace between the GNC 300, VHF COMM, and ground.
Shield the VHF COMM wiring harness.
2.1.6 COMM ANTENNA INSTALLATION INSTRUCTIONS
The COMM antenna should be installed according to the manufacturer's
recommendations.
2.2 RACK CONSIDERATIONS
2.2.1 ACCESSIBILITY
Plan a location which gives the pilot complete and comfortable access to the entire
keypad and which is plainly visible from the pilot’s perspective. Check that there is
adequate depth for the rack in the instrument panel. A location away from heating
vents or other sources of heat generation is optimal. Figure 2-2 illustrates a typical
aviation rack installation.
2.3 CABLING AND WIRING
The recommended antenna cable type for both antennas is M17/155-0001 (RG-58A/
U) per MIL-C-17. Maximum allowable length for the GPS antenna using this cable
typeis40feet. Othercabletypeswith50 ohmsnominalimpedanceandlongerlengths
can be used for the GPS antenna, provided the installer insures that the attenuation
does not exceed 10dB at 1.5 GHz for the specific installation. Check that there is
ample space for the cabling and mating connectors. Avoid sharp bends in cabling,
particularly the COMM antenna cable, and routing near aircraft control cables.
Cabling for the GNC 300 should not be routed near components or cabling which are
sources of electrical noise.
Do not route the COMM antenna cable near any ADF antenna cables.
Route the GPS antenna cable as far as possible away from all COMMs and COMM
antenna cable.
2.4 COOLING AIR
Cooling air is not required for the GNC 300 but is highly recommended because, as
with any electronic equipment, reduced operating temperature can contribute to
increased reliability. Additionally, location of the GNC 300 in a stack of other power
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 10
Download from Www.Somanuals.com. All Manuals Search And Download.
dissipating equipment can produce unacceptably high ambient air temperatures
aroundtheunit. A5/8inchdiameterairfittingisprovidedontherearofthemounting
rack for the purpose of admitting cooling air under such conditions.
2.5 MINIMUM INSTALLATION REQUIREMENTS
Below is a list of required devices for A1 and A2 certification. Figure 1-3 shows
various equipment that can be used. For a specific list of equipment used in the
initial STC see GPN 190-00067-06. Deviations from this equipment should be
approved by the FAA or the governing organization.
Pressure Altitude Device
This device delivers pressure altitude data to the GNC 300. This data
can come from an encoder or serializer.
Manual Course Device
This device delivers the manual course selected to the GNC 300.
Course information can come from an analog resolver or from an EFIS
via the ARINC 429 bus or RS-422 bus.
HSI/CDI Device
This device displays Nav Flag, Left/Right and To/From. This can be
displayed on the EFIS or HSI.
External Annunciators and Switches
NAV
GPS
NAV/GPS
HOLD
AUTO
Annunciator
Annunciator
Switch
Annunciator
Annunciator
GPS Sequence Switch
Approach Actv Annunciator (not required for A2)
Approach Arm
GPS Approach
Message
Annunciator (not required for A2)
Switch (not required for A2)
Annunciator
Arrival
Annunciator
The installer is advised to ensure that the switches and annunciators
are the functional equivalent to and perform at least as well as the
GARMIN devices used in the initial STC. The GARMIN switches and
annunciators are sunlight readable and in the primary view of the
pilot. Figure 2-3 shows what the GARMIN switch/annunciators look
like. For other information concerning switch/annunciators see the
Generic Airplane Flight Manual Supplement (190-00067-04) as well
as current FAA directives.
Qualified GPS Antenna
This antenna must be one of those listed in the accessories list.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 11
Download from Www.Somanuals.com. All Manuals Search And Download.
2.6 EXTERNALALTITUDEINPUT
Pressure altitude input from an external source may be derived from a RS-232
compatible serial altitude input or Parallel Gray Code/Gillham Altitude as described
in Section 4 of this manual. Gillham Altitude is not required when serial altitude is
used.
SECTION 3 INSTALLATION PROCEDURE
3.1 INSTALLATION ACCESSORIES
The following installation accessories are available:
ANTENNA AND RACK OPTIONS
010-10040-01
Includes:
GA 56 ANTENNA KIT, W/O CABLE (Mod 1, or later)
011-00134-00
115-00031-00
GA56 ANTENNA SUB-ASSEMBLY
BACKING PLATE
1
1
4
1
210-10004-09
253-00002-00
NUT, SELF-LOCKING, #8-32
ANTENNA GASKET
010-10040-02
Includes:
GA 56 FLANGE MOUNT ANTENNA (Mod 1, or later)
011-00147-00 FLANGE MOUNT GA56 ANTENNA SUB-ASSEMBLY
115-00080-00
1
1
4
1
NUT PLATE
211-62212-14
253-00011-00
SCREW, #10-32 X 5/8
ANTENNA GASKET
320-00003-00 15 FT LOW-LOSS AVIATION ANT. EXTENSION CABLE WITH RIGHT ANGLE BNC CONNECTOR
320-00003-02 30 FT LOW-LOSS AVIATION ANT. EXTENSION CABLE WITH RIGHT ANGLE BNC CONNECTOR
330-00087-00 CONNECTOR, BNC, MALE, CLAMP
Note: One cable assembly and one BNC connector are required to make the antenna cable, or it can
be fabricated by the installer from materials meeting the requirements of paragraph 2.3.
011-00154-00
MOUNTING RACK, (WITHOUT CONNECTORS)
Note: A mounting rack is required for approved installations. The following hardware is required for installa-
tion of the mounting rack, but is not provided:
#6-32 Flat Head Screw (4 ea.)
#6-32 Self-locking Nut (4 ea.)
011-00313-00 CONNECTOR, (J1 and J2) Kit
DATA BASE OPTIONS
010-10051-00
010-10051-01
010-10051-02
010-10032-03
MEMORY CARD - WORLDWIDE DATABASE
MEMORY CARD - AMERICAS DATABASE
MEMORY CARD - INTERNATIONAL DATABASE
MEMORY CARD - USER
ANNUNCIATOR OPTIONS
GPN
MID-CONTINENT P/N
DESCRIPTION
013-00029-10
013-00029-11
013-00029-12
013-00029-15
013-00029-16
013-00029-17
MD41-448
MD41-444
MD41-448 (5V)
MD41-458
MD41-454
INTEGRATED SW/ANN UNIT, HOR, 28V
INTEGRATED SW/ANN UNIT, HOR, 14V
INTEGRATED SW/ANN UNIT, HOR, 28V (5V LIGHTING)
INTEGRATED SW/ANN UNIT, VERT, 28V
INTEGRATED SW/ANN UNIT, VERT, 14V
INTEGRATED SW/ANN UNIT, VERT, 28V (5V LIGHTING)
MD41-458 (5V)
MISCELLANEOUS OPTIONS
010-10075-00
190-00067-00
190-00067-01
190-00067-06
330-00067-00
362-00014-00
010-10057-00
010-10074-00
PC KIT
GNC 300 PILOT'S GUIDE
GNC 300 QUICK REFERENCE GUIDE
GNC 300 IN MOONEY M20J DOCUMENTED INSTALLATION
GPS 1.57542 GHZ NOTCH FILTER
WALL ADAPTER - 110/220VAC
28 TO 14V CONVERTER (Consists of 011-00181-00)
REMOTE BATTERY PACK (Consists of 011-00182-00)
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 12
Download from Www.Somanuals.com. All Manuals Search And Download.
The following installation accessories are required but not provided:
COMM ANTENNA: BROAD BAND 50 OHM VERTICALLY POLARIZED WITH COAXIAL CABLE.
HEADPHONES:
MICROPHONE:
500 OHM NOMINAL IMPEDANCE
LOW IMPEDANCE CARBON OR DYNAMIC WITH TRANSISTORIZED PRE-AMP.
3.2 ANTENNA INSTALLATION
For the COMM antenna, follow the manufacturers instructions.
The remainder of this section applies to the GPS antenna. The GA 56 Antenna outline
and footprint dimensions are shown in Figures 3-1 and 3-2.
A. Using the backing plate as a template, mark the location of the mounting holes
and the through hole for coax cable. Drill or punch the holes.
B.Theantennainstallationmustprovideadequatesupportfortheantennaconsidering
a maximum drag load of 5 lbs. for the GA 56 antennas (at subsonic speed). Install
a doubler plate to reinforce thin skinned aircraft. Observe guidelines for
acceptable installation practices as outlined in AC 43.13-2A.
C. Seal the antenna and gasket to the fuselage using a good quality electrical grade
sealant. Use caution to insure that the antenna connector is not contaminated
with sealant. Insure that the mounting screws are fully tightened and that the
antennabaseiswellseatedagainstthegasket. CAUTION: Donotuseconstruction
grade RTV sealant or sealants containing acetic acid. These sealants may damage
the electrical connections to the antenna. Use of these type sealants may void the
antenna warranty.
3.3 CABLE INSTALLATION
A. Route the coax cable to the rack location keeping in mind the recommendations
of Section 2. Secure the cable in accordance with good aviation practice.
B. Trim the coaxial cable to the desired length and install the BNC connector (330-
00087-00) per the cabling instructions on Figure 3-3. If the connector is provided
by the installer, follow the connector manufacturer's instructions for cable
preparation.
C. Contacts for the 37 and 26 pin connectors must be crimped into the individual
wires of the aircraft wiring harness. The following tables list contact part numbers
(for reference) and recommended crimp tools:
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 13
Download from Www.Somanuals.com. All Manuals Search And Download.
Contacts
Standard Density Connectors
37 socket connector (J1 on unit)
Hi Dens. Connector
9 pin connector (on battery pack)
26 pin connector (J2 on unit)
20-24 AWG socket contact
18 AWG socket contact 20-24 AWG pin contact
18 AWG pin contact 22-28 AWG pin contact
Garmin p/n 336-00022-00
military p/n M39029/63-368
336-00023-00
n/a
336-00024-00
M39029/64-369
205089-1
336-00025-00 336-00021-00
n/a
M39029/58-360
204370-2
Amp
205090-1
n/a
n/a
Positronic M39029/63-368
ITTCannon 031-1007-042
FC6018D
see note
M39029/64-369
330-5291-037
MC6018D
see note
M39029/58-360
030-2042-000
Tools
Hand
Crimping
Standard Density Connectors (size 20 contacts)
Hi Dens. Connector (size 22D)
pin or socket contacts (20-24 AWG)
pin or socket contacts (18 AWG)
pin contacts (22-28 AWG)
Tool
positioner
M22520/2-08
9502-5
insert/extract
M81969/1-02
M81969/1-02
positioner insert/extract
positioner
M22520/2-09
9502-3
insert/extract
M81969/1-04
M81969/1-04
military p/n M22520/2-01
n/a
M81969/1-02
M81969/1-02
Positronic
9507
9502-11
ITTCannon 995-0001-584 995-0001-604 980-2000-426* see note
274-7048-000* 995-0001-739 n/a
Amp
601966-1
AFM8
601966-5
K13-1
91067-2
n/a
n/a
601966-6
K42
91067-1
Daniels
Astro
M24308/1-02
M81969/1-02
K774
M24308/1-02
M81969/1-02
M24308/18-1
M81969/1-04
615717
615725
see note
615724
* Insert/extract tools from ITT Cannon are all plastic, others are plastic with metal tip.
Non- GARMIN part numbers shown are not maintained by GARMIN and
consequently are subject to change without notice.
NOTE: Alternate contacts for 18 AWG wire: As an alternate to the Positronic
contacts listed (and provided in the install kit), the installer may use contacts
made by ITT Cannon as follows: Socket contact - ITT Cannon p/n: 031-10007-
001, Pin contact - ITT Cannon p/n: 330-5291-055. These contacts require the
use of a different crimp tool positioner than that shown in the table, with part
numbers as follows: Daniels p/n: K250, Astro p/n: 616245, or ITT Cannon p/
n: 980-00005-722.
See Appendix B for information regarding obsolete stamped type contacts.
3.4 RACK INSTALLATION
A. Figure 3-4 shows outline dimensions for the aviation rack. Install the rack in
a rectangular 6.320" x 2.000" hole in the instrument panel. Exercise caution
when installing the rack into the instrument panel. The rack is designed to
facilitate removal of the GNC 300 for portable use. Deformation of the rack may
make it difficult to install and remove the GNC 300.
B. Install the rack in the aircraft panel using four #6-32 countersunk screws and
four self-locking nuts or other FAA approved methods as per Advisory Circular
43.13-1A. The screws are inserted from the inside through the holes in the sides
of the rack (see Figure 3-5).
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 14
Download from Www.Somanuals.com. All Manuals Search And Download.
3.5 GNC 300 INSTALLATION AND REMOVAL
The GNC 300 is installed in the rack by gently sliding it straight in until it rests
against the back of the rack. A 3/32 inch hex drive tool is then inserted into the
access hole at the bottom of the unit face. Rotate the hex tool clockwise while
pressing on the left side of the Bezel until the unit is firmly seated in the rack.
To remove the unit from the rack, insert the hex drive tool into the access hole on the
unit face and rotate counter-clockwise until the mounting screw turns freely and the
unit protrudes about 3/8 inch from the panel.
Be sure not to over tighten the unit into the rack. The application of hex drive tool
torque exceeding 15 in*lbs can damage the locking mechanism.
3.6 COMM ANTENNA INSTALLATION CHECK
Check for insertion loss and VSWR. VSWR should be checked with an in-line type
wattmeter inserted in the coaxial transmission line between the transceiver and
the antenna. Any problem with the antenna installation will most likely be seen
as a high reflected power. A VSWR of 3:1 will result in a 25% loss in power.
SECTION 4 POST INSTALLATION CONFIGURATION & CHECKOUT
PROCEDURE
Before starting the below operations, unit initialization must occur. Do this by first
removing any data cards and then turning the unit on. Press enter in response to
“Select operating mode Normal ok?”. Press enter in response to “No Jeppesen
database rte/prx limited to user wpts ok?”. After the satellite status page is displayed
for 5 seconds the unit may be turned off. Proceed with the following steps.
4.1 TEST MODE OPERATIONS
With power applied to the aviation rack and the GNC 300 unit off, depress and hold
the ENT key and turn the unit on (release the ENT key when the display activates).
The first page displayed is the Display Test Page. While in TEST MODE, test pages
can be selected by ensuring the cursor is off and rotating the outer knob either
direction. To change data on the displayed test page, depress the CRSR key and the
cursor will highlight the standby COMM frequency. Press cursor again to move to
configuration selections. The inner knob will change the data on the selected field.
The ENT key or the outer knob will advance to the next field on the page. Pressing the
CRSR key again will stop the current field from flashing, allowing the outer knob to
select the next test page. The ENT key is used to enter a new value into the OBI data
field after selecting the desired value using the inner and outer knobs (see the
appropriate chapter of the Pilot's Guide for more information on page and data
selection). Note that some pages found in test mode are intended for bench testing
and are not discussed here.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 15
Download from Www.Somanuals.com. All Manuals Search And Download.
4.2 INSTALLATION CONFIGURATION
Note that the below pages are in the order found when rotating the outer knob
clock-wise starting at the Display Test Page. See Section 4.1 to get to this page.
4.2.1 DISPLAY ADJUSTMENT
This page allows the setting of display parameters that affect the display brightness
in automatic mode.
“response time” sets the speed with which the brightness responds to ambient light
changes.
The higher the number the slower the display responds.
“min” sets the minimum brightness of the display. The higher the number the
brighter the minimum brightness.
“slope” sets the sensitivity the brightness of the display has to changes in ambient
light. The higher the number the brighter the display will be for a given increase
in ambient lighting.
4.2.2 I/O CHANNEL 1
Select the I/O CHANNEL 1 Test Page. Change the selectable input and output to
match that of the installed equipment. The available options are:
Input:
Field
Description
off
icarus-alt
No units connected to Channel 1 input
Serial altitude received from:
Icarus, Model 3000, Mode C Serializer
Serial altitude received from:
shadin-alt
Shadin 9000T Serializer System (Non-TSO'd)
Shadin 9200T Series Serializer System (Non-TSO'd)
Shadin 8800T Series Encoder System (TSO'd)
Fuel information received from:
shadin-fuel
Shadin91204XTSeriesDigitalFuelManagementSystem
(TSO'd)
Shadin91053XTSeriesDigitalFuelManagementSystem
(TSO'd)
arnav/ei-fuel
Fuel information received from:
Arnav, Model FC-10, Fuel Computer (TSO'd)
Arnav, Model FT-10, Fuel Totalizer (TSO'd)
Electronics International, Model FP-5L, Fuel Flow
Computer (Non-TSO'd)
shadin-adc
shadin-fadc
Air data information received from:
Various models from the 9628XX-X family
Fuel/Air data information received from:
Various models from the 9628XX-X family
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 16
Download from Www.Somanuals.com. All Manuals Search And Download.
Note: Verify with manufacturer of data input device that unit supports GARMIN
interface.
Output: Field
off
Description
No units connected to Channel 1 output
Serial position, velocity and navigation data to:
Argus, Model 3000, Moving Map
Argus, Model 5000, Moving Map
Argus, Model 7000, Moving Map
Stormscope, Series II with Navaid, Moving Map
Shadin, 91204X[T] Digital Fuel Management System
(TSO'd)
aviation
Shadin, 91053X[T] Digital Fuel Management System
Electronics International, Model FP-5L, Fuel Flow
Computer (Non-TSO'd)
Shadin, Model 9628XX-X Fuel/Airdata Computer
(TSO'd)
GARMIN, GPS 195
GARMIN, GPS III
4.2.3 RS-422 CHANNEL
Select the RS-422 Channel Test Page. Change the selectable input and output to
match that of the installed equipment. The available options are:
Input:
Field
off
Description
No units connected to the RS-422 input
Collins PL2 DSP Collins Pro Line 2 Display Select Panel connected
Output: Field
off
Description
NO AVAILABLE SELECTIONS
4.2.4 ARINC 429 CHANNEL
Select the ARINC 429 Channel Test Page. Change the selectable output to match that
of the installed equipment. The available options are:
Input:
Field
Description
off
No units connected to ARINC 429 input
Any ARINC 429 compatible unit that transmits the
“Selected Course” word (label 100)
Selected Course
Course/heading Any ARINC 429 compatible unit that transmits the
“Selected Course” (label 100), as well as the “True
heading” (label 314) and/or “Magnetic heading” (label
320) words
Heading
Any ARINC 429 compatible unit that transmits the
“True heading” (label 314) and/or “Magnetic heading”
(label 320) words
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 17
Download from Www.Somanuals.com. All Manuals Search And Download.
Output: Field
off
Description
No units connected to ARINC 429 output
Collins PL2 EFS Collins Pro Line 2 EFIS connected (w/ GAMA)
King EFS 40/50 King Radio EFIS 40 or 50 connected (w/ GAMA)
w/o GAMA labels Any unit that receives standard 429 output
Below is a list of labels output by the GNC 300:
Navigation/position data
Label
(octal)
Description
100
114
115
116
121
251
252
310
311
312
313
314
320
147*
261*
275*
326*
351*
352*
Selected course
Desired track
Bearing to waypoint
Cross track error
Horizontal command (to autopilot)
Distance to go
Time to go
Present position latitude
Present position longitude
Ground speed
Ground track
True heading
Magnetic heading
Magnetic variation
GPS navigation mode
Navigation status
Lateral scale factor
Distance to destination
Time to destination
Flight plan data
Label
(octal)
074*
075*
113*
300*
303*
304*
305*
306*
307*
Description
Flight plan header
Active from/to waypoints
Message checksum
Station magnetic variation/type/class
Message length/type/number
Waypoint identifier characters 1-3
Waypoint identifier characters 4-6
Waypoint latitude
Waypoint longitude
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 18
Download from Www.Somanuals.com. All Manuals Search And Download.
Identificationdata
Label
(octal)
Description
377
Equipment identifier
371*
General Aviation equipment identifier
*These labels are formatted per the General Aviation Manufacturers Association
(GAMA) definition. Note that the use of a 429 device w/o GAMA will cause the loss
of the above asterisked labels. Some may be required for A1 certification. For
example, label 326 changes the CDI scale for approach.
4.2.5 CDI CALIBRATION
Select the test page displaying CDI output calibration. Place the cursor on the
alignment field by using the outer knob. Use the inner knob to adjust the CDI needle
until it is centered. Once centered, turn the cursor off to complete the calibration
process.
4.2.6 SELECTED COURSE CALIBRATION
Selectthetestpagedisplayingtheselectedcourseinput. Usinganextremelyaccurate
input source, input 150° to the GNC 300. The input course will indicate close to 150
and a “Calib?” field will appear in the lower right corner. Selecting the “Calib?” field
will calibrate the GNC 300 to match the input source. Verify OBS operation by
checking that the bearing displayed on the GNC 300 is within 2° of the selected
bearing. Do this for every multiple of 30° around the OBS.
4.2.7 APPROACH SETTINGS
Select the Approach Settings Test Page. Move the cursor over the approach switch
field to change the installation state.
The available options are:
Appr switch: Field
Description
none
instld
The approach switch is not present
The approach switch is installed
NOTE: To verify the installation of the approach switch, the “instld”
setting requires the approach switch to be pressed to confirm its
presence. The following prompt is displayed in this case: “press appr
switch to confirm” along with a “?” following “instld”. When the switch
press is recognized the prompts are cleared and the “instld” setting is
confirmed.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 19
Download from Www.Somanuals.com. All Manuals Search And Download.
4.2.8 CONFIGURATION
Select the Configuration Test Page. Change the selectable Strap and Fuel selections
to match that of the aircraft. The available options are:
Strap:
Field
Description
Lnav 1
Lnav 2
common
Number 1 (Pilot) long range NAV
Number 2 (Co-Pilot) long range NAV
Common long range NAV
NOTE: ThestrapoptionaffectstheinterpretationofRS-422andARINC429
input data
For RS-422 input data the following applies:
Lnav 1
Lnav 2
common
Only data marked for Lnav 1 is used
Only data marked for Lnav 2 is used
Data marked for either Lnav 1 or Lnav 2 is used
For ARINC 429 input data the following applies:
Lnav 1
Lnav 2
common
Only data with SDI=0 or SDI=1 is used
Only data with SDI=0 or SDI=2 is used
Only data with SDI=0 is used
NOTE: SDI=0 is an “all call”.
Fuel:
av gas
Jet A
Jet B
Using Aviation gas (5.8 lbs/gal)
Using Jet A/Jet A-1 fuel (6.7 lbs/gal)
Using Jet B (JP-4) fuel (6.5 lbs/gal)
NOTE: The Fuel option is used to designate the type of fuel used so that the
correct fuel density will be used in calculations.
4.2.9 REMOTE BATTERY SETTINGS
Remote Battery: none
instld
NOTE: If “instld” is selected when a battery is not installed erroneous
voltages will be shown on the Power Test page and invalid battery messages
will be issued in normal operating modes.
Low Battery:
selectable between 8.0 volts and 9.6 volts by 0.2 volt steps
NOTE: In normal operating modes, The “Battery Low” message will be
issued when the battery voltage is below the low battery value. The default
value is 9.0 volts.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 20
Download from Www.Somanuals.com. All Manuals Search And Download.
4.2.10 I/O CHANNEL 2
Note: This page is not found in the Test Pages but is included here to aid installation.
For more information see SET pages in the Pilot's Guide (GPN 190-00067-00).
SelecttheI/OCHANNEL2SetPage. Changetheselectableinputandoutputtomatch
that of the installed equipment. The available options are:
Input:
Field
off
Description
NO AVAILABLE SELECTIONS
Output: Field
off
Description
No units connected to Channel 2 output
Serialposition,velocity,navigationandsatellitedatato:
NMEA 0183 Version 2.0 compatible mapping device or
GARMIN PC software.
plotting
NOTE: Below is a list of the NMEA 0183 sentences (with maximum number of
characters) that the GNC 300 transmits.
RMC
GGA
-70 characters
-72 characters
GSA
-57 characters
GSV
-140 characters (70 characters x 2 sentences)
-70 characters
-35 characters
RMB
BOD
WPL
-38 characters
*PGRME
-35 characters
*GARMIN proprietary accuracy error sentence that is not a part of the NMEA
0183 standard.
4.3 GROUND TEST
TheGNC300groundtestprocedureincorporatesaseriesofdisplaypagestotestCDI/
flag,OBI,annunciators,externalswitches,altitudeinputs,andpowerfunctionsofthe
unit.
Notethatthebelowpagesareintheorderfoundwhenrotatingtheouterknobcounter-
clockwise starting at the Display Test page. See Section 4.1 to get to this page.
4.3.1 POWER TEST
SelectthePowerTestpage. ThispagereportsthestatusoftheGNC300externalpower
source, remote battery and internal memory battery.
In the below “voltage”
represents the voltage currently measured for that function.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 21
Download from Www.Somanuals.com. All Manuals Search And Download.
The first line, below the COMM frequencies, shows the source of external power as
shown below:
External Power “voltage”
Battery Power
Wall Adapter
The presence of a Wall Adapter will override the other two sources. Battery Power will
not be shown unless on the Remote Battery Settings Page the Remote Battery is
selected as “instld”. The higher voltage of External Power or Battery Power will
determine which is shown.
The next line shows the status of the Remote Battery as shown below:
Rmt Bat none (If on the Remote Battery Settings Page Remote Battery is selected as
none)
Rmt Bat “voltage” “mode” “auto status”
“mode” represents the mode of the charger enable to the remote battery pack and is
selectable. “On” enables the charger. “Off” disables the charger. “Auto” enables the
charger if the External Power is the current source and its voltage is high enough.
When in “Auto” mode “auto status” will be either “on” or “off” reflecting whether the
charger is enabled or disabled.
The next line reports the status of the internal memory battery as shown below:
Mem Bat ok/low.
Note that the “TX” field will light on the display but the transmitter will not actually
transmit when the GNC 300 is powered from the wall charger.
4.3.2 CDI AND FLAG TEST
Select the CDI Test Page. Using the controls on the GNC 300 front panel, make the
selections indicated below and verify the interfaces as appropriate:
CDI
Full scale left
Full scale right
Centered
Ensure the CDI is deflected full scale left (5 dots)
Ensure the CDI is deflected full scale right (5 dots)
Ensure the CDI is centered
TO/FROM/FLAG
TO
Ensure TO flag is visible
FROM
FLAG
Ensure FROM flag is visible
Ensure TO and FROM are NOT visible
CDI FLAG
IN VIEW
Ensure CDI flag is in view
OUT OF VIEW
Ensure CDI flag is out of view
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 22
Download from Www.Somanuals.com. All Manuals Search And Download.
SUPERFLAG
IN VIEW
Ensure superflag in view
OUT OF VIEW
Ensure superflag out of view
4.3.3 ANNUNCIATOR TEST
SelecttheAnnunicatorTestPage. UsingthecontrolsontheGNC300frontpanelmake
the selections indicated below and verify the interfaces as appropriate:
MSG Annunciator
OFF
ON
Ensure the Message Annunciator is OFF
Ensure the Message Annunciator is ON
Arrival Annunciator
OFF
ON
Ensure the Arrival Annunciator is OFF
Ensure the Arrival Annunciator is ON
Approach Annunciator
OFF
ACTV
Ensure all Approach Annunciators are OFF
Ensure the Approach Active Annunciator is ON (Arm
is OFF)
ARM
Ensure the Approach Arm Annunciator is ON (Active
is OFF)
4.3.4 EXTERNAL SWITCH TEST
Select the External COM Switches Page. For each of the following installed remote
switches perform the following:
Press Remote Enter and verify the Rmt ent field changes from off to on.
Press PTT and verify the PTT field changes from off to on.
Press Remote Transfer and verify the Rmt xfr field changes from off to on.
Next, select the External Switches Page. For each of the following installed remote
switches perform the following:
Press GPS Appr and verify the “appr” field changes from off to on.
Press GPS Sequence and verify the “hold” field changes from off to on.
4.3.5 COMMUNICATIONS LOOPBACK TEST
This page displays the results of communication loop back tests. Four channels are
tested: RS232channels1and2, RS422andARINC429. Resultsofthetestareeither
“OPEN” or “OK”. Open means the channel's transmitter and receiver are not
connected or the test failed. The tests are performed continuously while on this page
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 23
Download from Www.Somanuals.com. All Manuals Search And Download.
except for RS232 channel 2. This channel is only tested at power on and the results
displayed on this page. Therefore the unit must be turned off and the receiver/
transmitter connected or disconnected and then turn the unit on to perform the test.
To test the channels:
RS232 channel 1:
RS232 channel 2:
RS422:
Connect RS232 channel 1 receiver and transmitter
Connect RS232 channel 2 receiver and transmitter
Connect RS232 channel 1 to RS422 LOW (pin 27) and
ground RS422 HI (pin 11)
ARINC 429:
Connect ARINC 429 receiver and transmitter
4.3.6 ALTITUDE INPUT TEST
Select the Gray Code Altitude Test Page if this input is used. Verify that the altitude
input is reading the correct altitude. NOTE: This does not display serial altitude.
4.3.7 OBI TEST
Select the OBI Test Page. Using the controls on the GNC 300 front panel, make the
selections indicated below and verify the interfaces as appropriate:
OBI Data
VALID
INVALID
Ensure that the OBI indicates the proper value
Ensure the OBI is invalid
OBI Value
Ensure that the OBI displays the value entered when
the VALID option is selected
NOTE: The 3 lines that make up the OBI interface may be toggled individually. This
may be done from the “Value” field. Cycle this field to the desired line (either CLOCK,
DATA or SYNC) and toggle the output to HIGH or LOW.
4.3.8 SIGNAL ACQUISITION TEST
The Self Test Page will be displayed followed by the Data Base Page. Upon approval
of the Data Base Page, the Satellite Status Page will be displayed. If unable to acquire
satellites, relocate the aircraft away from obstructions which might be shading
reception. If the situation does not improve, check the antenna installation.
Once GPS position information is available, use the DIRECT-TO key to activate the
navigation function to a nearby NAVAID, intersection, or airport. Ensure any
connected equipment is transmitting data to and/or is receiving data from the GNC
300 and is functioning properly (see the Pilot's Guide for more information on the
DIRECT-TO function).
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 24
Download from Www.Somanuals.com. All Manuals Search And Download.
4.3.9 VHF COMM INTERFERENCE CHECK
a) Go to the Satellite Status Page, verify that 7 to 8 satellites have been
acquired
b) See that the “NAV” flag is out of view
c) Select 121.15 MHZ on COMM1
d) Transmit for a period of 20 seconds
e) Verify that the flag does not come into view
f) Repeat steps d) and e) for the following frequencies:
121.175, 121.20, 131.250, 131.275 and 131.300
g) Repeat steps c-f for all COMMs installed in the aircraft
h) Ifthe“NAV”flagcomesintoview,refertoSection2.1.5foroptionstoimprove
performance.
4.3.10 VHF COMM CHECK
A flight test is recommended after the installation is completed to insure satisfactory
performance. To check the communications transceiver, maintain an appropriate
altitude and contact a ground station facility at a range of at least 50 nautical miles.
Contact a ground station close in. Press the squelch disable button to defeat the
automatic squelch feature and listen for any unusual electrical noise which would
reducetheCOMMreceiversensitivitybyincreasingthesquelchthreshold. Ifpossible,
verify the communications capability on both the high and low end of the VHF COMM
band.
SECTION 5 CERTIFICATION
The GNC 300 is certified for IFR enroute, terminal and non-precision approaches.
The GNC 300's initial certification was accomplished via a STC by GARMIN in a
Mooney M20J. See Appendix C for a copy of the STC.
All installations must be certified. For more information, see FAA Advisory Circular
“AirworthinessApprovalofGlobalPositioningSystem(GPS)NavigationEquipmentfor
use as a VFR and IFR Supplemental Navigation System”, Appendix 1. All new
certifications after GARMIN's Mooney installation will be “Follow-On”.
SECTION 6 CONTINUED AIRWORTHINESS
Maintenance of the GNC 300 is on condition only. Periodic maintenance of the GNC
300 is not required.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 25
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-1 PINOUT DEFINITION, 37 PIN DSUB
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 26
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-2 PINOUT DEFINITION, 26 PIN HD-DSUB
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 27
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-3A INTERCONNECT SCHEMATIC
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 28
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-3B INTERCONNECT SCHEMATIC
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 29
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-3C INTERCONNECT SCHEMATIC
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 30
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 1-4 INTERCONNECT SCHEMATIC NOTES
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 31
Download from Www.Somanuals.com. All Manuals Search And Download.
Ante nna m a ske d b y ve rtic a l fin,
ta il, o r d o rsa l fin
T
OK
Ante nna m ust b e o n
to p o f a irc ra ft.
FIG 2-1
GPS ANTENNA INSTALLATION CONSIDERATIONS
Maintain 6"(16 cm)
compass safe distance
ACTV
STBY
GARMIN GNC 250
CLR ENT
CRSR
SQ
D
NRST
RTE
NAV
MSG
WPT
FIG 2-2
GNC 300 INSTALLATION CONSIDERATIONS
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 32
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 2-3 SWITCH/ANNUNCIATOR LAYOUT
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 33
Download from Www.Somanuals.com. All Manuals Search And Download.
FIG 3-1
STUD MOUNT GA 56 ANTENNA INSTALLATION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 34
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 3-2
FLANGE MOUNT GA 56 ANTENNA INSTALLATION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 35
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 3-3 COAX CABLE INSTALLATION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 36
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 3-4 AVIATION RACK DIMENSIONS
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 37
Download from Www.Somanuals.com. All Manuals Search And Download.
FIGURE 3-5 AVIATION RACK INSTALLATION
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 38
Download from Www.Somanuals.com. All Manuals Search And Download.
APPENDIX A CERTIFICATION DOCUMENTS
(19,5210(17$/ꢀ48$/,),&$7,21ꢀ)250
120(1&/$785(ꢁ
*1&ꢀꢂꢃꢃꢄꢀ*36ꢀ$,5%251(ꢀ51$9ꢀꢅꢀ&200ꢀ6<67(0
7<3(ꢅ02'(/ꢅ3$57ꢀ12ꢁ ꢃꢆꢆꢇꢃꢃꢆꢈꢉꢇꢃꢃ
*36ꢀ762ꢁꢀ&ꢆꢈꢊꢀ&/$66ꢀ$ꢀꢋꢆꢌ
9+)ꢀ&200ꢀ75$160,77(5ꢀ762ꢁꢀꢀ&ꢂꢍGꢀ&/$66ꢀꢎ
9+)ꢀ&200ꢀ5(&(,9(5ꢀ762ꢁꢀꢀ&ꢂꢉGꢀ&/$66ꢀ&
0$18)$&785(5ꢏ6ꢀ63(&,),&$7,21ꢀ$1'ꢅ25ꢀ27+(5ꢀ$33/,&$%/(ꢀ63(&,),&$7,21ꢁ ꢃꢃꢎꢇꢃꢃꢃꢆꢎꢇꢃꢃ
0$18)$&785(5ꢁ
$''5(66ꢁ
*$50,1ꢀ,17(51$7,21$/ꢄꢀ,1&ꢐ
ꢆꢈꢃꢃꢀ(ꢐꢀꢆꢑꢆVWꢀ675((7ꢄꢀ2/$7+(ꢄꢀ.$16$6ꢀꢒꢒꢃꢒꢈ
&RQGLWLRQVꢀꢆꢅ
6HFWLRQ
ꢎꢐꢃ
'HVFULSWLRQꢀRIꢀ&RQGXFWHGꢀ7HVWV
7HPSHUDWXUHꢀDQGꢀ$OWLWXGH
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRULHVꢀ$ꢆꢀ ꢀ'ꢆꢀH[FHSWꢀDV
QRWHG
/RZꢀ7HPSHUDWXUH
ꢎꢐꢑꢐꢆ
ꢎꢐꢑꢐꢈꢐꢀ ꢀꢎꢐꢑꢐꢂ
ꢎꢐꢑꢐꢎ
+LJKꢀ7HPSHUDWXUH
,Qꢇ)OLJKWꢀ/RVVꢀRIꢀ&RROLQJ
&RROLQJꢀDLUꢀQRWꢀUHTXLUHG
$OWLWXGH
ꢎꢐꢒꢐꢆ
ꢎꢐꢒꢐꢈ
ꢎꢐꢒꢐꢂ
'HFRPSUHVVLRQ
2YHUSUHVVXUH
7HPSHUDWXUHꢀ9DULDWLRQ
+XPLGLW\
ꢑꢐꢃ
ꢒꢐꢃ
ꢍꢐꢃ
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ&
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ$
6KRFN
(TXLSPHQWꢀWHVWHGꢀSHUꢀ'2ꢇꢆꢒꢃ&ꢄꢀ3DUꢐꢀꢍꢐꢈꢐꢆ
2SHUDWLRQDO
&UDVKꢀ6DIHW\
ꢍꢐꢈ
ꢍꢐꢂ
9LEUDWLRQ
ꢉꢐꢃ
(TXLSPHQWꢀWHVWHGꢀZLWKRXWꢀVKRFNꢀPRXQWVꢀWR
&DWHJRULHVꢀ%ꢄꢀ0ꢀDQGꢀ1ꢀꢋ7DEOHꢀꢉꢇꢆꢌ
([SORVLRQ
ꢊꢐꢃ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
:DWHUSURRIQHVV
)OXLGVꢀ6XVFHSWLELOLW\
ꢆꢃꢐꢃ
ꢆꢆꢐꢃ
Download from Www.Somanuals.com. All Manuals Search And Download.
ꢆꢅ
7KHꢀLQIRUPDWLRQꢀOLVWHGꢀEHORZꢀSURYLGHVꢀH[DPSOHVꢀRQO\ꢐꢀꢀ,WꢀLVꢀQRWꢀLQWHQGHGꢀWRꢀEHꢀDꢀFRPSUHKHQVLYH
OLVWLQJꢀRIꢀDOOꢀWHVWꢀFRQGLWLRQVꢐ
&RQGLWLRQVꢀꢆꢅ
6HFWLRQ
ꢆꢈꢐꢃ
ꢆꢂꢐꢃ
ꢆꢎꢐꢃ
ꢆꢑꢐꢃ
ꢆꢒꢐꢃ
ꢆꢍꢐꢃ
ꢆꢉꢐꢃ
'HVFULSWLRQꢀRIꢀ&RQGXFWHGꢀ7HVWV
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀWHVWHGꢀLVꢀ&ODVVꢀ=
6DQGꢀDQGꢀ'XVW
)XQJXV
6DOWꢀ6SUD\
0DJQHWLFꢀ(IIHFW
3RZHUꢀ,QSXW
9ROWDJHꢀ6SLNH
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ%
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ$
$XGLRꢀ)UHTXHQF\
6XVFHSWLELOLW\
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ%
,QGXFHGꢀ6LJQDO
6XVFHSWLELOLW\
ꢆꢊꢐꢃ
ꢈꢃꢐꢃ
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ$
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ7
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ=
5DGLRꢀ)UHTXHQF\
6XVFHSWLELOLW\
5DGLRꢀ)UHTXHQF\ꢀ(PLVVLRQ
ꢈꢆꢐꢃ
ꢈꢈꢐꢃ
/LJKWQLQJꢀ,QGXFHꢀ7UDQVLHQW
6XVFHSWLELOLW\
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;;;;ꢄꢀQRꢀWHVW
UHTXLUHG
/LJKWQLQJꢀ'LUHFWꢀ(IIHFWV
,FLQJ
ꢈꢂꢐꢃ
ꢈꢎꢐꢃ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
2WKHUꢀ7HVWV
5HPDUNVꢁ
6RIWZDUHꢁꢀ'2ꢇꢆꢍꢉ&ꢄꢀ/HYHOꢀ&ꢀꢋ0DMRUꢌ
Download from Www.Somanuals.com. All Manuals Search And Download.
(19,5210(17$/ꢀ48$/,),&$7,21ꢀ)250
*$ꢀꢂꢃꢄꢀ*36ꢀ$9,$7,21ꢀ$17(11$
ꢇꢈꢈꢉꢇꢇꢈꢊꢋꢉꢇꢇꢅꢇꢈꢅꢇꢌ
120(1&/$785(ꢁ
7<3(ꢅ02'(/ꢅ3$57ꢀ12ꢆꢁ
762ꢀ180%(5ꢁꢀ&ꢈꢌꢍ
&/$66ꢀ$ꢎꢈꢏ
0$18)$&785(5ꢐ6ꢀ63(&,),&$7,21ꢀ$1'ꢅ25ꢀ27+(5ꢀ$33/,&$%/(ꢀ63(&,),&$7,21ꢁ ꢇꢇꢋꢉꢇꢇꢇꢈꢂꢉꢇꢇ
0$18)$&785(5ꢁ
$''5(66ꢁ
*$50,1ꢀ,17(51$7,21$/ꢄꢀ,1&ꢆ
ꢈꢌꢇꢇꢀ(ꢆꢀꢈꢂꢈVWꢀ675((7ꢄꢀ2/$7+(ꢄꢀ.$16$6ꢀꢃꢃꢇꢃꢌ
&RQGLWLRQVꢀꢈꢅ
6HFWLRQ
ꢋꢆꢇ
'HVFULSWLRQꢀRIꢀ&RQGXFWHGꢀ7HVWV
7HPSHUDWXUHꢀDQGꢀ$OWLWXGH
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ)ꢌ
/RZꢀ7HPSHUDWXUH
ꢋꢆꢂꢆꢈ
ꢋꢆꢂꢆꢌꢆꢀ ꢀꢋꢆꢂꢆꢊ
ꢋꢆꢂꢆꢋ
+LJKꢀ7HPSHUDWXUH
,Qꢉ)OLJKWꢀ/RVVꢀRIꢀ&RROLQJ
&RROLQJꢀDLUꢀQRWꢀUHTXLUHG
$OWLWXGH
ꢋꢆꢃꢆꢈ
ꢋꢆꢃꢆꢌ
ꢋꢆꢃꢆꢊ
'HFRPSUHVVLRQ
2YHUSUHVVXUH
1RWꢀWHVWHG
1RWꢀWHVWHG
7HPSHUDWXUHꢀ9DULDWLRQ
+XPLGLW\
ꢂꢆꢇ
ꢃꢆꢇ
ꢑꢆꢇ
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ$
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ&
6KRFN
(TXLSPHQWꢀWHVWHGꢀSHUꢀ'2ꢉꢈꢃꢇ&ꢄꢀ3DUꢆꢀꢑꢆꢌꢆꢈ
2SHUDWLRQDO
&UDVKꢀ6DIHW\
ꢑꢆꢌ
ꢑꢆꢊ
1RWꢀDSSOLFDEOH
9LEUDWLRQ
ꢒꢆꢇ
(TXLSPHQWꢀWHVWHGꢀZLWKRXWꢀVKRFNꢀPRXQWVꢀWR
&DWHJRULHVꢀ&ꢄꢀ/ꢄꢀ0ꢀDQGꢀ<ꢀꢎ7DEOHꢀꢒꢉꢈꢏ
([SORVLRQ
ꢍꢆꢇ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ6
:DWHUSURRIQHVV
)OXLGVꢀ6XVFHSWLELOLW\
ꢈꢇꢆꢇ
ꢈꢈꢆꢇ
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ)ꢀZLWKꢀ(WK\OHQHꢀ*O\FRO
'Hꢉ,FLQJꢀ)OXLG
Download from Www.Somanuals.com. All Manuals Search And Download.
ꢈꢅ
7KHꢀLQIRUPDWLRQꢀOLVWHGꢀEHORZꢀSURYLGHVꢀH[DPSOHVꢀRQO\ꢆꢀꢀ,WꢀLVꢀQRWꢀLQWHQGHGꢀWRꢀEHꢀDꢀFRPSUHKHQVLYH
OLVWLQJꢀRIꢀDOOꢀWHVWꢀFRQGLWLRQVꢆ
&RQGLWLRQVꢀꢈꢅ
6HFWLRQ
ꢈꢌꢆꢇ
ꢈꢊꢆꢇ
ꢈꢋꢆꢇ
ꢈꢂꢆꢇ
ꢈꢃꢆꢇ
ꢈꢑꢆꢇ
ꢈꢒꢆꢇ
'HVFULSWLRQꢀRIꢀ&RQGXFWHGꢀ7HVWV
6DQGꢀDQGꢀ'XVW
)XQJXV
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
6DOWꢀ6SUD\
0DJQHWLFꢀ(IIHFW
3RZHUꢀ,QSXW
9ROWDJHꢀ6SLNH
$XGLRꢀ)UHTXHQF\
6XVFHSWLELOLW\
,QGXFHGꢀ6LJQDO
6XVFHSWLELOLW\
ꢈꢍꢆꢇ
ꢌꢇꢆꢇ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ$ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ7ꢄꢀQRꢀWHVWꢀUHTXLUHG
5DGLRꢀ)UHTXHQF\
6XVFHSWLELOLW\
5DGLRꢀ)UHTXHQF\ꢀ(PLVVLRQ
ꢌꢈꢆꢇ
ꢌꢌꢆꢇ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ=ꢄꢀQRꢀWHVWꢀUHTXLUHG
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀ;ꢄꢀQRꢀWHVWꢀUHTXLUHG
/LJKWQLQJꢀ,QGXFHꢀ7UDQVLHQW
6XVFHSWLELOLW\
/LJKWQLQJꢀ'LUHFWꢀ(IIHFWV
ꢌꢊꢆꢇ
ꢌꢋꢆꢇ
(TXLSPHQWꢀLGHQWLILHGꢀDVꢀ&DWHJRU\ꢀꢌ$ꢄꢀQRꢀWHVW
UHTXLUHG
,FLQJ
(TXLSPHQWꢀWHVWHGꢀWRꢀ&DWHJRU\ꢀ&
2WKHUꢀ7HVWV
5HPDUNVꢁ
Download from Www.Somanuals.com. All Manuals Search And Download.
APPENDIX B CONNECTOR CHANGES
STAMPED CONTACT CONNECTOR USAGE
Garmin panel mount GPS radios have previously been shipped with stamped crimp type contacts. All
products are now being shipped with machined mil-spec contacts with color-coded barrels. The following
figures can be used to identify which type contact you have:
Some contacts are pins as shown, while others are the socket type. The type used will vary with the
installation. When working with the stamped crimp type contacts, the following tools should be used:
Tools
37 and 9 position connectors
26 position connector
supplier
Amp
Crimp Tool
58448-2
Extraction Tool
91067-22
Crimp Tool
90430-1
Extraction Tool
91285-1
ITT Cannon
Cinch
995-2000-000
HTD-544
980-0008-124
CIET-20-HDB
995-2000-022
HTD-544
980-00004-804
HTD-520
Part numbers shown are not maintained by Garmin and consequently are subject to change without notice.
Special considerations must be made for aircraft power and remote battery (optional) connections, as shown
in the following diagram:
Download from Www.Somanuals.com. All Manuals Search And Download.
REMOTE BATTERY PIN ASSIGNMENTS
A change was made to the remote battery connectors starting with serial numbers 33050055. Units with
lower serial numbers have pin contacts on the battery pack. Units 33050055 and up use socket contacts on
the battery and the pin number assignments are different, however the individual contact locations are
unchanged. The following table shows the pin assignments for the two different types of connectors:
Serial Number
remote batt.
below 33050055
pins
33050055 and up
sockets
mating plug
sockets
pins
function
contact number
contact number
battery +
battery +
1
2
3
4
5
6
7
8
9
5
4
3
2
1
9
8
7
6
charge enable
aircraft power
aircraft power
no connection
no connection
ground
ground
Download from Www.Somanuals.com. All Manuals Search And Download.
APPENDIX C STC PERMISSION
Consistent with N8110.69 or Order 8110.4, Aviation Authority approved installers
are hereby granted permission to use STC# SA00372WI data to modify aircraft.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 45
Download from Www.Somanuals.com. All Manuals Search And Download.
Av. Kit Install. Manual
190-00067-02 Rev. J
Page 46
Download from Www.Somanuals.com. All Manuals Search And Download.
|