Garmin Flight Stream 110/210 User manual

190-01700-00 October 2014 Revision B
Flight Stream 110/210
TSO Installation Manual

190-01700-00 Flight Stream 110/210 TSO Installation Manual
Rev. B Page A
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Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
Telephone: [phone]
Aviation Dealer Technical Support Line (Toll Free): [phone]
Web Site Address: www.garmin.com
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Fax: [phone] RECORD OF REVISIONS
Revision Revision Date Description
A 6/13/2014 Initial Release.
B 10/8/14 Added software update procedure.

190-01700-00 Flight Stream 110/210 TSO Installation Manual
Rev. B Page B
CURRENT REVISION DESCRIPTION
DOCUMENT PAGINATION
Section Number Description of Change
1.4.3 Corrected Bluetooth Version.
3.3.2 Updated yaw, pitch, and roll mounting limitations.
4.4 Added software update procedures.
Section Pagination
Table of Contents iii through vi
Section 1 1-1 through 1-8
Section 2 2-1 through 2-3
Section 3 3-1 through 3-8
Section 4 4-1 through 4-1
Section 5 5-1 through 5-1
Section 6 6-1 through 6-2
Section 7 7-1 through 7-1
Section 8 8-1 through 8-1
Appendix A A-1 through A-1
Appendix B B-1 through B-7

190-01700-00 Flight Stream 110/210 TSO Installation Manual
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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 $1,000,000 under Section 2410 of the Export Administration Act of
1979. Include this notice with any reproduced portion of this document.
DEFINITIONS OF WARNINGS, CAUTIONS, AND NOTES
WARNING
This product, its packaging, and its components contain chemicals known to the State of
California to cause cancer, birth defects, or reproductive harm. This notice is being
provided in accordance with California's Proposition 65. If you have any questions or
would like additional information, please refer to our web site at
www.garmin.com/prop65.
WARNING
Perchlorate Material – special handling may apply, visit
www.dtsc.ca.gov./hazardouswaste/perchlorate.
WARNING
Warnings indicate that immediate attention must be given to avoid potential
equipment damage and personal injury should the instructions be
disregarded.
CAUTION
Cautions indicate an alert to potential damage to the equipment if the
procedural step is not directly followed.
NOTE
Notes indicate that additional information is required to explain the
applicable step, providing further understanding as to the reason for that
particular operation.

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Aviation Limited Warranty
All Garmin avionics products are warranted to be free from defects in materials or workmanship for: two
years from the date of purchase for new Remote-Mount and Panel-Mount products; one year from the date
of purchase for new portable products and any purchased newly-overhauled products; six months for
newly-overhauled products exchanged through a Garmin Authorized Service Center; and 90 days for
factory repaired or newly-overhauled products exchanged at Garmin in lieu of repair. Within the
applicable period, Garmin will, at its sole option, repair or replace any components which fail in normal
use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided the
customer will be responsible for any transportation cost. This warranty does not apply to: (i) cosmetic
damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product damage
has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse,
water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by
anyone who is not an authorized service provider of Garmin; or (v) damage to a product which has been
modified or altered without the written permission of Garmin. In addition, Garmin reserves the right to
refuse warranty claims against products or services which are obtained and/or used in contravention of the
laws of any country.
WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL
OTHER WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY
LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU
SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.
IN NO EVENT WILL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR
CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR
INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT. SOME STATES DO
NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES, SO THE
ABOVE LIMITATIONS MAY NOT APPLY TO YOU.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement
product) the product or software or offer a full refund of the purchase price at its sole discretion. SUCH
REMEDY WILL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF
WARRANTY.
Online Auction Purchases: Products purchased through online auctions are not eligible for warranty
coverage. Online auction confirmations are not accepted for warranty verification. To obtain warranty
service, an original or copy of the sales receipt from the original retailer is required. Garmin will not
replace missing components from any package purchased through an online auction.
International Purchases: A separate warranty may be provided by international distributors for devices
purchased outside the United States depending on the country. If applicable, this warranty is provided by
the local in-country distributor and this distributor provides local service for your device. Distributor
warranties are only valid in the area of intended distribution. Devices purchased in the United States or
Canada must be returned to the Garmin service center in the United Kingdom, the United States, or Canada
for service.

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TABLE OF CONTENTS
1 GENERAL DESCRIPTION ............................................................................................................1-1
1.1 Introduction ................................................................................................................................1-1
1.2 Equipment Description ..............................................................................................................1-1
1.3 Interface Summary and Equipment ...........................................................................................1-3
1.4 Technical Specifications ............................................................................................................1-4
1.5 Certification ...............................................................................................................................1-6
1.6 Limitations .................................................................................................................................1-8
1.7 Reference Documents ................................................................................................................1-8
2 INSTALLATION OVERVIEW ......................................................................................................2-1
2.1 Introduction ................................................................................................................................2-1
2.2 Installation Material Required but Not Supplied .......................................................................2-1
2.3 Special Tools Required ..............................................................................................................2-2
2.4 Cabling and Wiring ....................................................................................................................2-2
2.5 Mounting Requirements ............................................................................................................2-2
3 INSTALLATION PROCEDURE ....................................................................................................3-1
3.1 Wiring Harness Installation .......................................................................................................3-1
3.2 Flight Stream Backshell Assembly and D-sub Connector .........................................................3-1
3.3 Equipment Mounting .................................................................................................................3-5
4 POST-INSTALLATION CONFIGURATION AND CHECKOUT ............................................4-1
4.1 Mounting, Wiring, and Power Checks .......................................................................................4-1
4.2 Bluetooth Setup ..........................................................................................................................4-1
4.3 Ground Checks ..........................................................................................................................4-2
4.4 Software Updates .......................................................................................................................4-3
5 CONTINUED AIRWORTHINESS .................................................................................................5-1
5.1 Flight Stream 110 .......................................................................................................................5-1
5.2 Flight Stream 210 .......................................................................................................................5-1
6 CONNECTOR PINOUT INFORMATION ...................................................................................6-1
6.1 Flight Stream Pin Out List .........................................................................................................6-1
7 TROUBLESHOOTING ...................................................................................................................7-1
APPENDIX A OUTLINE AND INSTALLATION DRAWING ....................................................A-1
APPENDIX B INTERCONNECT DRAWINGS .............................................................................B-1

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LIST OF FIGURES
Figure 1-1. Flight Stream Transceiver Unit View .....................................................................................1-2
Figure 1-2. Flight Stream Interface Block Diagram ..................................................................................1-3
Figure 3-1. Connector and Backshell Assembly .......................................................................................3-2
Figure 3-2. Shielded Cable Preparation .....................................................................................................3-3
Figure 3-3. Suggested Mounting Locations ...............................................................................................3-5
Figure 3-4. Flight Stream Mounting ..........................................................................................................3-6
Figure 3-5. Mounting Orientation ..............................................................................................................3-7
Figure 3-6. Mounting Orientation Side View ............................................................................................3-8
Figure A-1. Flight Stream Transceiver Dimensions .................................................................................A-1
Figure B-1. Flight Stream 110/210 Power Interconnect ...........................................................................B-2
Figure B-2. Flight Stream - GDL 69/69A Interconnect ........................................................................... B-3
Figure B-3. Flight Stream - GDL 88 Interconnect ................................................................................... B-4
Figure B-4. Flight Stream 210 - GNS Interconnect .................................................................................. B-5
Figure B-5. Flight Stream 210 - GTN 6XX/7XX Interconnect ................................................................ B-6
Figure B-6. Flight Stream 210 - ARINC 429 Interconnect ...................................................................... B-7

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LIST OF TABLES
Table 1-1. Flight Stream Interfaces ...........................................................................................................1-3
Table 1-2. Flight Stream Interfaced Equipment List .................................................................................1-4
Table 1-3. Flight Stream Transceiver Dimensions ....................................................................................1-4
Table 1-4. Flight Stream Transceiver Specifications ................................................................................1-5
Table 1-5. Bluetooth Specifications ..........................................................................................................1-5
Table 1-6. Flight Stream Transceiver ........................................................................................................1-5
Table 1-7. TSO Compliance ......................................................................................................................1-6
Table 1-8. Non-TSO Functions .................................................................................................................1-6
Table 1-9. Referenced Publications ...........................................................................................................1-8
Table 2-1. Units and Part Numbers ...........................................................................................................2-1
Table 2-2. Pin Contact Numbers ...............................................................................................................2-2
Table 2-3. Recommended Crimp Tools .....................................................................................................2-2
Table 3-1. Connector and Backshell Assembly .........................................................................................3-1
Table 6-1. Flight Stream Pin Out List .......................................................................................................6-1
Table 6-2. Aircraft Power. .........................................................................................................................6-1
Table 6-3. RS-232 ......................................................................................................................................6-2
Table 6-4. RS-422 ......................................................................................................................................6-2
Table 6-5. ARINC 429 ..............................................................................................................................6-2
Table 6-6. Discrete Inputs ..........................................................................................................................6-2
Table 7-1. Flight Stream Troubleshooting Guide ......................................................................................7-1

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HARDWARE MOD LEVEL HISTORY
The following table identifies hardware modification (Mod) Levels. 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
SERVICE
BULLETIN
NUMBER
SERVICE
BULLETIN
DATE PURPOSE OF MODIFICATION

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1 GENERAL DESCRIPTION
1.1 Introduction
This manual is intended to provide physical, mechanical, and electrical information for use in the planning
and design of a Flight Stream 110/210 unit installation into an aircraft. It is not a substitute for an approved
airframe-specific maintenance manual, installation design drawing, or complete installation data package.
Attempting to install equipment by reference to this manual alone and without first planning or designing
an installation specific to your aircraft, is not recommended. The content of this manual assumes use by
competent and qualified avionics engineering personnel and/or avionics installation specialists using
standard aviation maintenance practices in accordance with Title 14 of the Code of Federal Regulations
and other relevant accepted practices, and is not intended for use by individuals who lack the competencies
set forth above.
For additional information, see section 1.6 Limitations.
NOTE
Except where specifically noted, references made to Flight Stream will equally apply to the
Flight Stream 110 and the Flight Stream 210.
NOTE
Features may vary due to the many configurations available.
NOTE
Garmin™ recommends installation of the Flight Stream units by a Garmin-authorized
installer. To the extent allowable by law, Garmin will not be liable for damages resulting
from improper or negligent installation of the Flight Stream units. For questions, contact
Garmin Aviation Product Support at 1-888-606-5482.
1.2 Equipment Description
The Flight Stream units bring Bluetooth®technology to the cockpit, allowing portable electronics to
stream data to and from the installed avionics.
The Flight Stream 110 provides the following data from the listed wired interfaces to portable electronics
using Bluetooth technology:
GDL 69
SiriusXM Radio Volume/Channel Control
XM WX Aviation Weather
GDL 88
FIS-B Weather
ADS-B Traffic
GPS Position

190-01700-00 Flight Stream 110/210 TSO Installation Manual
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The Flight Stream 210 includes all of the features of the Flight Stream 110, an internal AHRS and pressure
sensor, as well as the following data from the listed wired interface to portable electronics, using Bluetooth
technology:
GNS 430W/530W
GPS Position
Flight Plan Input/Output
GTN 6XX/7XX
GPS Position
Flight Plan Input/Output
Attitude (forwarded from a G500/G600 system, when connected)
ARINC 429 Transmitters
ARINC 429 Receiver
CAUTION
Bluetooth devices and other non-aviation transmitters require separate authorization for
use in an aircraft. If they are present, note interference from such devices may degrade the
performance of the Flight Stream wireless remote system. The Flight Stream wireless
remote system may also degrade the performance of other wireless transceiver systems
which use Bluetooth or IEEE 802.11 operating in the same frequency band, though
functional testing suggests these protocols are robust enough to maintain acceptable
performance in the presence of the Flight Stream system.
Figure 1-1. Flight Stream Transceiver Unit View
(Flight Stream 210 shown)
NOTE
Flight Stream 210 looks identical to the Flight Stream 110, but includes a direction of
flight sticker.

190-01700-00 Flight Stream 110/210 TSO Installation Manual
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1.3 Interface Summary and Equipment
figure 1-2 shows a block diagram of the possible interfaces for the Flight Stream products.
Figure 1-2. Flight Stream Interface Block Diagram
Notes:
1. FLIGHT STREAM 210 ONLY
2. THE FLIGHT STREAM 210 ONLY SUPPORTS A CONNECTION TO ONE GARMIN NAVIGATOR AT A
TIME. IT IS RECOMMENDED TO CONNECT IT TO THE #1 NAVIGATOR OR THE GTN IN GTN/GNS
INSTALLATIONS.
Table 1-1. Flight Stream Interfaces
Interface Description Number of Ports
ARINC 429 In (Flight Stream 210 Only) 1
Bluetooth N/A
RS-232 In/Out 3
RS-422 In/Out 1
*16
56
)OLJKW6WUHDP 0RELOH$SSV
*71
56
*'/
56
*'/
56
$5,1&
7UDQVPLWWHU
5656$5,1& %OXHWRRWK
)OLJKWSODQLQRXW
*36397LQ
$WWLWXGH
)OLJKWSODQLQRXW
*36397LQ
$XGLRFRQWUROLQRXW
:HDWKHULQ
$'6%7UDIILF),6%,Q
*36397LQ
$5,1&
/DEHOV
$'6%2XW
$5,1&/DEHOV2XW
$WWLWXGH
$XGLR&RQWURO,Q2XW
)OLJKWSODQLQRXW
*36397RXW
:HDWKHURXW






190-01700-00 Flight Stream 110/210 TSO Installation Manual
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Table 1-2. Flight Stream Interfaced Equipment List
[1] The Flight Stream must be connected to RS-232 Port 1 of the GDL 69.
[2] The Flight Stream does not directly interface to the GDU 620. However, attitude information
may be forwarded from the GDU 620 through a GTN 6XX/7XX with GDU 620 software version
7.00.
1.4 Technical Specifications
The Flight Stream is TSO authorized under TSO-C157. It is the responsibility of those desiring to install
this equipment either on or within a specific type of class of aircraft to determine the aircraft installation
standards are within the prescribed standards. The following sections present general environmental
specifications. For detailed specifications, refer to the Environmental Qualification Form.
1.4.1 Environmental Qualification Form (EQF)
It is the responsibility of the installing agency to obtain the latest revision of the Flight Stream EQF. For
the latest EQF visit the Dealer Resource Center. The Flight Stream 110 and Flight Stream 210 use the same
EQF.
The EQF is available directly from Garmin under the following name and part number:
Garmin Flight Stream 110/210 Environmental Qualification Form, P/N 005-00818-03.
1.4.2 Physical Characteristics
Table 1-3. Flight Stream Transceiver Dimensions
Description Software Version (or later FAA approved version)
GTN 6XX/7XX Navigator 5.10
GNS 400W Series Navigator 5.20
GNS 500W Series Navigator 5.20
GDL 88 3.00
GDL 69 [1] 3.30
GDU 620 [2] 7.00
Characteristic Specification
Width 2.74" (7.0 cm)
Height 0.92" (2.3 cm)
Length (excluding connector kit) 3.93" (10.0 cm)
Unit Weight (excluding connector kit) 0.156 lbs (0.07 kg)
Unit Weight (including connector kit) 0.27 lbs (0.12 kg)

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1.4.3 General Specifications
Table 1-4. Flight Stream Transceiver Specifications
Table 1-5. Bluetooth Specifications
1.4.4 Power Specifications
Table 1-6. Flight Stream Transceiver
NOTE
Circuits should be protected in accordance with guidelines in AC 43.13-1B, Chapter 11,
Section 4.
Flight Stream Transceiver Characteristics Specification
Operating Temperature Range -20° C to +70° C
Input Voltage Range 9.5 to 33.0 VDC
Software Compliance RTCA DO-178B Level E
Environmental Compliance RTCA DO-160F
Characteristics Specification
Bluetooth Version 3.0
Bluetooth Class 2
Maximum Transmitter Power 4 dBm (2.5 mW)
Effective Unimpeded Range 33 feet (10 m)
Unit Status Max Current @ 28 VDC Max Current @ 14 VDC
On 50 mA 100 mA

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1.5 Certification
The conditions and tests required for TSO approval of this article are minimum performance standards. It
is the responsibility of those installing this article either on or within a specific type or class of aircraft to
determine the aircraft installation conditions are within the TSO standards. TSO articles must have
separate approval for installation in an aircraft. The article may be installed only in compliance under
14 CFR part 43 or the applicable airworthiness requirements.
1.5.1 TSO Compliance
The Flight Stream is TSO-C157 authorized as an incomplete system.
Table 1-7. TSO Compliance
1.5.2 TSO Deviations
None.
1.5.3 Non-TSO Functions
The Flight Stream includes the following non-TSO functions.
Table 1-8. Non-TSO Functions
1.5.4 Design Assurance Levels
This device complies with DO-178B design assurance Level E.
TSO Function TSO/SAE/RTCA/
EUROCAE Applicable LRU SW P/Ns
XM Radio Weather Data TSO-C157
DO-267A 006-B1779-00 through 006-B1779-( )
Function Applicable SW P/N
Remote Audio Entertainment 006-B1779-00 through 006-B1779-( )
Conversion of serial data from the GDL 69 to
Bluetooth wireless signals

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1.5.5 Transmitter Grant of Equipment Authorization
FCC ID: IPH-02318
IC: 1312A-02318
IC M/N: GMN-01194
NOTE
This device complies with Part 15 of the FCC Rules. Operation is subject to the following
conditions: (1) This device may not cause harmful interference, and (2) this device must
accept any interference received, including interference which may cause undesired
operation.
NOTE
This device does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could result
in permanent damage to the equipment, and void your warranty and your authority to
operate this device under Part 15 regulations.
Industry Canada Statement:
This device complies with Industry Canada license-exempt RSS standard(s). Operation is subject to the
following two conditions: (1) this device may not cause interference, and (2) this device must accept any
interference, including interference that may cause undesired operation of the device.
Cet appareil est conforme aux normes RSS sans licence d’Industrie Canada. Son fonctionnement est
soumis aux conditions suivantes: (1) cet appareil ne doit pas causer d’interférences et (2) doit accepter
toute interférence,y compris les interférences pouvant entraîner un fonctionnement indésirable de
l’appareil.
European Union Declaration of Conformity:
“Hereby, Garmin, declares that this Flight Stream product is in compliance with the essential requirements
and other relevant provisions of Directive 1999/5/EC. To view the full Declaration of Conformity, see the
Garmin Web site for your Garmin product: www.garmin.com”.

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1.6 Limitations
1.6.1 Operation
The optional Flight Stream wireless remote system has been tested for interference. Its operation must not
interfere with the proper operation of any required aircraft equipment or systems. The installation requires
the installer to verify there is no interference using the post-installation check-out procedure, see section 4.
1.6.2 Installation
For preservation of essential equipment in aircraft with multiple power busses, the Flight Stream should be
powered from a non-essential bus.
1.7 Reference Documents
The following publications are sources of additional information for installing the Flight Stream wireless
remote system. Before installing the Flight Stream, the technician should read all referenced materials
applicable to the installation along with this manual.
Table 1-9. Referenced Publications
Document P/N
FAA Advisory Circular, Acceptable Methods, Techniques, and Practices
– Aircraft Inspection and Repair FAA AC 43.13-1B
FAA Advisory Circular, Acceptable Methods, Techniques, and Practices
– Aircraft Alterations FAA AC 43.13-2B
GDL 69 Series TSO Installation Manual 190-00355-07
GDL 88 TSO Installation Manual 190-01122-00
GNS 400W Series Installation Manual 190-00356-08
GNS 500W Series Installation Manual 190-00357-08
GTN 625/635/650 TSO Installation Manual 190-01004-02
GTN 725/750 TSO Installation Manual 190-01007-02

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2 INSTALLATION OVERVIEW
2.1 Introduction
This section provides the equipment information for installing the Flight Stream and related optional
accessories. Installation of the Flight Stream should follow the data detailed in this manual. Cabling is
typically fabricated by the installing agency to fit each particular aircraft. Always follow acceptable
avionics installation practices per advisory circulars AC 43.13-1B and AC 43.13-2B or later FAA
approved revisions.
2.1.1 Unit Configurations
The Flight Stream is available with the following part numbers.
Table 2-1. Units and Part Numbers
2.2 Installation Material Required but Not Supplied
The Flight Stream units are intended for use with standard aviation accessories. The following items are
required for installation but not supplied:
Wire (MIL-W-22759/16 or MIL-W-22759/18 or equivalent). If MIL-W-22759/18 wire is utilized,
extra care must be taken to adequately support and protect the wiring due to its thinner insulation.
Shielded Wire (MIL-C-27500 cable utilizing M22759/18 wire (TG) or ETFE jacket (14), or
equivalent).
Aircraft hardware for installation, including #6 screws, nuts/nutplates, washers, and rivets
Push/Pull (manually resettable) Circuit Breaker
Tie Wraps or Lacing Cord
Ring Terminals (MS25036 or equivalent)
Shield Terminators (MIL-S-83519 or equivalent)
Silicon Fusion Tape (Garmin P/N 249-00114-00 or equivalent)
Compatible portable electronic device (PED)
Garmin Pilot™ App
Model Unit P/N Unit Only Kit P/N
Flight Stream 110 011-03257-00 010-01194-00 010-01194-01
Flight Stream 210 011-03257-40 010-01194-40 010-01194-41
Connector Kit 011-03258-00 N/A N/A

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2.3 Special Tools Required
Table 2-2. Pin Contact Numbers
Table 2-3. Recommended Crimp Tools
NOTE
Non-Garmin part numbers shown are not maintained by Garmin and are subject to
change without notice.
2.4 Cabling and Wiring
Wiring should be installed in accordance with AC 43.13-1B Chapter 11. When wire separation cannot be
achieved, the following issues should be addressed:
• The cable harness should not be located near flight control cables, high electrical capacity lines, or
fuel lines.
• The cable harness should be located in a protected area of the aircraft.
• Do not route cable near high-energy sources.
See the interconnection diagrams in appendix B for the appropriate wiring. Once the cable assemblies have
been made, attach the cable connector. Route the wiring bundle as appropriate. Avoid sharp bends.
For the Flight Stream, use 22 AWG wire for all connections including power/ground.
CAUTION
Check wiring connections for errors before connecting the 15-pin D-sub to the Flight
Stream. Incorrect wiring could cause component damage.
2.5 Mounting Requirements
The Flight Stream may be mounted in a pressurized or unpressurized location. To achieve optimal
Bluetooth reception, mount the Flight Stream as close as possible to the cockpit.
Wire Gauge 15-pin connectors
20-24 AWG
Garmin P/N 336-00021-00
Military P/N M39029/58-360
Wire Gauge Hand Crimping Tool 20-24 AWG
Positioner Insertion/Extraction
Tool
Military P/N M22520/2-01 M22520/2-09 M81969/1-04
Positronic 9507 9502-4 M81969/1-04
AMP 601966-1 601966-6 91067-1
Daniels AFM8 K42 DAK95-22MB/
DRK95-22MB
Astro 615717 615725 M81969/1-04

190-01700-00 Flight Stream 110/210 TSO Installation Manual
Rev. B Page 3-1
3 INSTALLATION PROCEDURE
This section provides hardware equipment information for installing the Flight Stream. For interconnects
with interfaced equipment, see appendix B.
3.1 Wiring Harness Installation
Allow adequate space for installation of cables and connectors. All electrical connections are made
through a 15-pin D-sub connector provided by Garmin. Construct the wiring harness according to the
information contained in this and the following sections. Cable lengths will vary depending upon
installation.
1. Strip all wires going to the D-sub connectors 0.17".
2. Insert the wire into the pin and crimp with one of the recommended (or equivalent) crimping tools.
3. Insert the pin into the D-sub connector housing locations as specified by the interconnect drawing
in appendix B.
4. Verify the pin is properly engaged into the connector by gently tugging on the wire.
5. Route and secure the cable run from the Flight Stream to the other units away from sources of
electrical noise.
section 6 defines the electrical characteristics of all input and output signals. Required connectors and
associated hardware are supplied with the connector kit. See appendix B for interconnect wiring diagrams.
3.2 Flight Stream Backshell Assembly and D-sub Connector
3.2.1 Flight Stream Connector Assembly
Table 3-1. Connector and Backshell Assembly
See figure 3-1 Description Garmin P/N
1 Screw, 4-40x.187, FLHP100, SS/P with Nylon 211-63234-06
2 Cover, Backshell, Jackscrew 115-01079-00
3 Screw, 4-40x.375, PHP, SS/P with Nylon 211-60234-10
4 Clamp, Backshell, Jackscrew 115-01078-00
5 Backshell, Jackscrew, 15 Pin 125-00171-00
6 Conn, HD D-Sub, 15 Pin 330-00626-15