Garmin | GSB 15 | Garmin GSB 15 GSB 15 Installation Manual

Garmin GSB 15 GSB 15 Installation Manual
GSB 15
USB Database and
Charging Hub
Installation Manual
190-00303-A3
July, 2019
Revision 2
© 2019
Garmin Ltd. or its subsidiaries
All Rights Reserved
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.
Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062 USA
www.garmin.com
Garmin (Europe) Ltd.
Liberty House, Hounsdown Business Park
Southampton, Hampshire SO40 9LR U.K.
AVIATION LIMITED WARRANTY
GSB 15 warranty information is available at garmin.com/aviationwarranty.
RECORD OF REVISIONS
Revision
Revision
Date
1
07/10/19
Initial Release
2
07/18/19
Added mounting kit info
190-00303-A3
Rev. 2
Description
GSB 15 Installation Manual
Page A
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 the United States
without first obtaining an export license. The preceding statement is required to be included on any and all
reproductions in whole or in part of this manual.
CURRENT REVISION DESCRIPTION
Revision
Page
Number
Section
Number
ii
Front
Added Qualcomm® information
1-2
1.2.2
Added mounting kit info in Tables 1-4 & 1-5
1-3
1.2.3
Added mounting weight info to Table 1-7
1-6
1.5.2
Added Qualcomm® information
2-1
2.3
Added info regarding mounting kits
2-3
2.8
Updated Figure 2-1
3-1
3.2
Added mounting instructions for new mounting kits
A-2, A-3
Appdx A
Updated figure titles for Figure A-2 and Figure A-3
A-4–A-6
Appdx A
Added Figure A-4, Figure A-5, and Figure A-6
2
Description of Change
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 http://www.garmin.com/
prop65.
190-00303-A3
Rev. 2
GSB 15 Installation Manual
Page i
SOFTWARE LICENSE AGREEMENT
BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN
(“THE GARMIN PRODUCT”), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS
OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT
CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the
software embedded in the Garmin Product (the “Software”) in binary executable form in the normal
operation of the Garmin Product. Title, ownership rights, and intellectual property rights in and to the
Software remain with Garmin and/or its third-party providers. You acknowledge that the Software is the
property of Garmin and/or its third-party providers and is protected under the United States of America
copyright laws and international copyright treaties. You further acknowledge that the structure,
organization, and code of the Software are valuable trade secrets of Garmin and/or its third-party providers
and that the Software in source code form remains a valuable trade secret of Garmin and/or its third-party
providers. You agree not to reproduce, decompile, disassemble, modify, reverse assemble, reverse
engineer, or reduce to human readable form the Software or any part thereof or create any derivative works
based on the Software. You agree not to export or re-export the Software to any country in violation of the
export control laws of the United States of America.
Qualcomm® is a trademark of Qualcomm Incorporated, registered in the United States and other
countries. Quick Charge™ is a trademark of Qualcomm Incorporated. All Qualcomm Incorporated
trademarks are used with permission.
Qualcomm Quick Charge is a product of Qualcomm Technologies, Inc. and/or its subsidiaries.
190-00303-A3
Rev. 2
GSB 15 Installation Manual
Page ii
TABLE OF CONTENTS
PARAGRAPH
PAGE
Section 1 Declaration of Design and Performance ..........................................1-1
1.1 Introduction...................................................................................................................... 1-1
1.2 Description and Identification ......................................................................................... 1-1
1.3 Certification Statement .................................................................................................... 1-4
1.4 Interface Summary........................................................................................................... 1-5
1.5 Performance Technical Specifications............................................................................. 1-6
1.6 Limitations ....................................................................................................................... 1-7
1.7 Operating Instructions...................................................................................................... 1-7
1.8 License Requirements...................................................................................................... 1-7
1.9 Reference Documents ...................................................................................................... 1-7
Section 2 Installation Overview .........................................................................2-1
2.1 Introduction...................................................................................................................... 2-1
2.2 Installation Materials Required but not Supplied ............................................................ 2-1
2.3 Installation Configurations .............................................................................................. 2-1
2.4 Special Tools Required .................................................................................................... 2-1
2.5 Cabling and Wiring.......................................................................................................... 2-2
2.6 Shielding and Electrical Bonding Considerations ........................................................... 2-2
2.7 Cooling Requirements or Considerations ........................................................................ 2-2
2.8 Mounting Requirements .................................................................................................. 2-3
Section 3 Installation Procedure........................................................................3-1
3.1 Wiring Harness Installation ............................................................................................. 3-1
3.2 Equipment Mounting ....................................................................................................... 3-1
Section 4 Post Installation Configuration & Checkout ...................................4-1
4.1 Mounting, Wiring, and Power Checks............................................................................. 4-1
4.2 Configuration Setup ......................................................................................................... 4-1
4.3 Diagnostic Information .................................................................................................... 4-1
4.4 Ground Checks ................................................................................................................ 4-1
4.5 Software Loading Procedure ........................................................................................... 4-1
Section 5 Continued Airworthiness...................................................................5-1
Section 6 Connector Pinout Information..........................................................6-1
6.1 Pin Function List.............................................................................................................. 6-1
Appendix A Outline and Installation Drawings .............................................A-1
Appendix B Interconnect Drawings................................................................. B-1
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Page iii
1 DECLARATION OF DESIGN AND PERFORMANCE
1.1 Introduction
The Declaration of Design and Performance section contains the definition and statement of compliance of
the GSB 15. The section is written in accordance with European Aviation Safety Agency (EASA)
Commission Regulation (EU) No 748/2012 date 3 August 2012.
The full manual is intended to provide mechanical and electrical information for use in the planning and
design of an installation of the GSB 15 into an aircraft. This manual 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 may compromise your safety and it is not recommended. The
content of this manual assumes use by competent and qualified avionics engineering personnel and/or
avionics installation specialist using standard maintenance practices in accordance with Title 14 of the
Code of Federal Regulation and other relevant accepted practices. This manual is not intended for use by
individuals who do not possess the competencies and abilities set forth above.
NOTE
Garmin recommends installation of the GSB 15 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 GSB 15. For questions, please contact Garmin Aviation
Product Support at 1-888-606-5482.
NOTE
Except where specifically noted, references to GSB 15 apply equally to all GSB 15
variants.
1.2 Description and Identification
The GSB 15 functions as a USB Database and Charging Hub that provides:
•
•
•
Two (2) - USB Type A charging ports (low-current with data transfer or high-current without data
transfer)
Optional software and database loading to compatible Garmin devices via USB
Halo backlighting to facilitate nighttime usability
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1.2.1
Unit Identification
The GSB 15 can be identified by the part numbers listed in Table 1-1.
Table 1-1 GSB 15 Unit Identification
API
Marketing Label
Garmin P/N
(Unit Only)
Garmin P/N
(Shipping Level)
GMN-02201
GSB 15
011-04937-0( )
through
011-04937-1( )
010-02201-0( )
through
010-02201-1( )
The GSB 15 is currently available in the following configurations.
Table 1-2 GSB 15 Part Numbers
Model
Unit Only P/N
Unit Only Shipping P/N
Standard P/N [1]
GSB 15 (vertical)
011-04937-00
010-02201-00
010-02201-10
GSB 15 (right angle)
011-04937-01
010-02201-01
010-02201-11
[1] Includes connector kit (011-05044-00)
1.2.2
Accessories
The following accessories are provided separately from the GSB 15.
Table 1-3 Equipment Available
Item
Garmin P/N
GSB 15 2.25” Mounting Kit
011-05043-00
GSB 15 3.125” Mounting Kit
011-05043-01
GSB 15 Connector Kit
011-05044-00
Table 1-4 Contents of 2.25” Mounting Kit (011-05043-00)
Item
Garmin P/N
Quantity
DCP, Adapter Plate, 2.25”
125-00581-02
1
Screw, 4-40 x .250, FLHP 100, SS/BO
211-63304-08
2
Table 1-5 Contents of 3.125” Mounting Kit (011-05043-01)
Item
Garmin P/N
Quantity
DCP, Adapter Plate, 3.125”
125-00581-12
1
Screw, 4-40 x .250, FLHP 100, SS/BO
211-63304-08
2
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Table 1-6 Contents of Connector Kit (011-05044-00)
Item
Garmin P/N
Quantity
Screw, 4-40x.125, PHP, SS/P, w/NYL
211-60234-04
1
Screw, 4-40x.250, PHP-STD, SS/BO
211-60304-08
2
Term, Ring, Ins, #4, 22-26 AWG
235-00117-01
1
Conn, Hsg, Rcpt, 3mm P, Single Row, Locking, 6 CKT, Nylon
330-00771-05
1
Contact, Female, Crimp, 20-24 AWG, 15u Gold
336-00065-05
6
1.2.3
Physical Characteristics
Table 1-7 Unit and Accessory Weights
Model
Part Number
Weight
GSB 15, Vertical
011-04937-00
0.16 lbs (0.07 kg)
GSB 15, Right Angle
011-04937-01
0.16 lbs (0.07 kg)
GSB 15 2.25” Mounting Kit
011-05043-00
0.11 lbs (0.05 kg)
GSB 15 3.125” Mounting Kit
011-05043-01
0.20 lbs (0.09 kg)
GSB 15 Connector Kit
011-05044-00
0.01 lbs (0.005 kg)
1.2.4
Mod Level History
The following tables identify hardware modification (Mod) Levels for the GSB 15. 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-todate bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using
their Garmin-provided user name and password.
Table 1-8. MOD Level History
Applicable LRU
Part Number
MOD
Level
Service Bulletin
Number & Date
Purpose of Modification
011-04937-00
N/A
N/A
N/A
011-04937-01
N/A
N/A
N/A
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1.3 Certification Statement
The GSB 15 has been shown to meet compliance with the claimed TSO(s) when interfaced with the equipment defined in this installation manual, and installed in
accordance with the requirements and limitations as defined in this installation manual.
The installer must verify that non-Garmin devices to be interfaced meet the installation requirements identified in this manual to assure the installed system will
comply with the Garmin TSO Authorization. Garmin installation requirements will usually specify that the interfaced device has appropriate TSO authorization, and
in some cases, such as for TSO-C144 antennas, may also require that the non-Garmin device meet additional Garmin specifications.
The conditions and tests required for TSO approval of this article are minimum performance standards. Those installing this article either on or within a specific type
or class of aircraft must determine that the aircraft installation conditions are within the TSO standards which include any accepted integrated non-TSO functions.
TSO articles and any accepted integrated non-TSO function(s) must have separate approval for installation in an aircraft. The article may be installed only according
to 14 CFR part 43 or the applicable airworthiness requirements.
In accordance with the Bilateral Oversight Board, Decision 006, for the Agreement Between the United States of America and the European Union on Cooperation
in the Regulation of Civil Aviation Safety, the FAA TSO authorization makes this an approved article within the respective EASA system. This article was tested to
additional standards (see section 1.3.4) that may demonstrate additional airworthiness specification performance standards required by the European Aviation Safety
Agency (EASA).
The Appliance Project Identifier (API) for the GSB 15 is GMN-02201. The API has been used for project identification with the FAA.
1.3.1
GSB 15 TSO Compliance
Table 1-9 GSB 15 (011-04937-00, -01) TSO Compliance
TSO/MOPS*
TSO-C71
Function Design
Airborne Static (DC to DC) Electrical Power Converter
Class/Type
System SW
Part Numbers
Boot Block SW
Part Numbers
CLD Part Numbers
N/A
N/A
N/A
N/A
*The Minimum Performance Standards in this table are the conditions and tests used to achieve FAA TSO authorization. See Section 1.3.4 for additional standards.
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1.3.2
GSB 15 (011-04937-00, -01) TSO/ETSO Deviations
Table 1-10 GSB 15 (011-04937-00, -01)TSO Standard Deviations
TSO
TSO-C71
Deviation
Garmin was granted a deviation to include only product name, part number, serial
number, and this statement on the unit's nameplate label: "TSO-C71 See IM for Add'l
Appliance Apprvls”.
Garmin was granted a deviation to use RTCA/DO-160F as the standard for
Environmental Qualification and Test Procedures of Airborne Equipment.
1.3.3
Non-TSO Functions
The GSB 15 has no non-TSO functions.
1.3.4
Additional Standards
The GSB 15 has no Additional Standards.
The conditions and tests required for approval of this article are minimum performance standards. Those
installing this article either on or within a specific type or class of aircraft must determine that the aircraft
installation conditions are within the standards which include any accepted integrated functions not
specified by the standard. Articles approved with 14 CFR part 21.8(d) and any accepted integrated
function(s) not specified in the standard must have separate approval for installation in an aircraft. The
article may be installed only according to 14 CFR part 43 or the applicable airworthiness requirements.
1.3.5
Design Assurance Levels
The GSB 15 contains no software or airborne electronic hardware with related design assurance levels.
The GSB 15 COTS module provides no design assurance for pass-through data. Those installing this
article with other articles utilizing pass-through data must determine means for detecting misleading or
corrupt data.
1.3.6
Database
For information on certification compliance for databases, refer to Garmin Document P/N 190-01999-00
posted at flyGarmin.com.
1.4 Interface Summary
The following list is an interface summary for the GSB 15 unit:
•
•
Two (2) - USB Type A connectors for charging and data transfer
A USB interface through the rear connector for database/SW loads to compatible Garmin units.
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1.5 Performance Technical Specifications
1.5.1 Environmental Qualification Form Reference
It is the responsibility of the installing agency to obtain the latest revision of the GSB 15 Environmental
Qualification Form. To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site
(www.garmin.com).
This form is available directly from Garmin under the following part number:
GSB 15 Environmental Qualification Form, Garmin part number 005-01380-03
1.5.2
General Specifications
Table 1-11 General Specifications
Characteristic
Qualcomm® Quick Charge™
Technology
Specification
Qualcomm® Quick Charge™ Technology delivers up to 75%
faster charging vs. conventional USB charging
Output Voltage
Output Power (each port)
5-12V out (5V nominal)
5.0V/3A, 9.0V/2A, 12V/1.5A (18W MAX)
Operating Temperature Range
-20 to 55 C
Altitude
55,000 ft
Humidity
95% non-condensing
1.5.3
Power Specifications
Maximum power while charging both ports (18W each) and backlight enabled: 40W
28V: 1.43A
14V: 2.86A
Maximum power with no devices connected: 500mW
28V: 17mA
14V: 35mA
1.5.4
Over-Temperature Protection
The GSB 15 is equipped with over-temperature detection and may re-negotiate to 5V, 1.5A (MAX) output
current. Once the device has cooled, normal output current will resume.
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GSB 15 Installation Manual
Page 1-6
1.6 Limitations
This article meets the minimum performance and quality control standards required by a technical
standard order (TSO). Installation of this article requires separate approval.
1.7 Operating Instructions
The GSB 15 has a configurable backlight. Grounding pin 5 will de-activate the backlight, allowing pin
5 to float enables the backlight.
It is acceptable and preferred to install only the pins that are needed.
CAUTION
Do not apply power to the unit until after the rear connector is completely seated.
Connecting the unit while power is applied may cause damage to the device, and to other
LRUs that are connected to the data lines.
1.8 License Requirements
There are no license requirements applicable to the GSB 15.
1.9 Reference Documents
There are no applicable reference documents for installation of the GSB 15.
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GSB 15 Installation Manual
Page 1-7
2 INSTALLATION OVERVIEW
2.1 Introduction
This section provides the equipment information for installing the GSB 15 and related optional
accessories. Installation of the GSB 15 must 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.
2.2 Installation Materials Required but not Supplied
•
•
All wiring required for installation
Circuit breaker
2.3 Installation Configurations
The GSB 15 can be installed in either a rear connector or side connector configuration. Refer to the outline
and installation drawings in Appendix A.
Optional 2.25” and 3.125” mounting kits are also available (see Table 1-3) to mount the GSB 15 in
existing instrument panel holes.
NOTE
At least 2 of the 4 provided mounting holes must be used (diagonally from each other) to
mount the GSB 15.
2.4 Special Tools Required
A crimp tool is required for the GSB 15 installation. Recommended and optional crimp tools are as
follows:
Recommended Crimp tool:
•
Molex Hand Crimp Tool, P/N 638190000
Optional:
•
Molex Insertion Tool for Micro-Fit 3.0 and CRC Male and Female Crimp Terminals, 20-30 AWG,
P/N 638120800
•
Molex Extraction Tool, P/N 11030043
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Rev. 2
GSB 15 Installation Manual
Page 2-1
2.5 Cabling and Wiring
Wiring must be installed in accordance with AC 43.13-1B Chapter 11, Sections 8 through 13. The
following issues must be addressed:
•
•
•
•
•
•
Do not expose cabling and wiring to chafing
Do not route cabling and wiring harnesses near flight cables
Do not route cabling and wiring near high-energy sources. (e.g. DC motors, high heat sources)
Wiring indicated as shielded in Appendix B must be shielded
Pigtail lengths must be less than 3.0 inches.
Use 22 AWG or larger for power and ground wires, 25 ft max.
2.6 Shielding and Electrical Bonding Considerations
Electrical equipment, supporting brackets, and racks must be electrically bonded to the aircraft’s main
structure or a designated aircraft groundplane. Refer to the following documents for applicable bonding
techniques:
•
•
•
AC 43.13-1B CHG 1, "Acceptable Methods, Techniques, and Practices - Aircraft Inspection and
Repair", Chapter 11, "Aircraft Electrical Systems"
SAE ARP 1870A, "Aerospace Systems Electrical Bonding and Grounding for Electromagnetic
Compatibility and Safety"
A bonding procedure developed and supplied by the aircraft manufacturer (if available)
The electrical bond must achieve direct current (DC) resistance less than or equal to 2.5 milliohms to local
structure where the equipment is mounted. Compliance must be verified by inspection using a calibrated
milliohm meter.
2.7 Cooling Requirements or Considerations
The GSB 15 has no cooling requirements or considerations. Forced air cooling will reduce the internal
temperature of the unit and prolong the life of the product.
The GSB 15 is equipped with over-temperature detection that may reduce output current to 1.5A (max) .
After the device has cooled, normal output current 3A (max) will resume.
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GSB 15 Installation Manual
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2.8 Mounting Requirements
The small size of the GSB 15 allows it to be installed in many places. It is intended to be installed to the
instrument panel or other suitable cabin surface. There are no special requirements for viewing, reach, or
proximity. See drawings in Appendix A for details.
VERTICAL CONNECTOR (-00 CONFIG) WITH
CONNECTOR KIT (011-05044-00)
RIGHT-ANGLE CONNECTOR (-01 CONFIG) WITH
CONNECTOR KIT (011-05044-00)
GSB 15 UNIT
011-04937-00
GSB 15 UNIT
011-04937-01
AIRCRAFT
PANEL
AIRCRAFT
PANEL
VERTICAL CONNECTOR (-00 CONFIG)
WITH 3.125" MOUNTING KIT (011-05043-01)
VERTICAL CONNECTOR (-00 CONFIG)
WITH 2.25" MOUNTING KIT (011-05043-00)
AIRCRAFT
PANEL
GSB 15 UNIT
011-04937-00
GSB 15 UNIT
011-04937-00
AIRCRAFT
PANEL
2" NOMINAL
ADAPTER PLATE (Ø 2.25")
125-00581-02
3" NOMINAL OR 3 ATI
ADAPTER PLATE (Ø 3.125")
125-00581-12
Figure 2-1. GSB 15 Mounting Examples
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GSB 15 Installation Manual
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3 INSTALLATION PROCEDURE
3.1 Wiring Harness Installation
Allow adequate space for installation of cables and connectors. The installer shall supply and fabricate all
of the cables. All electrical connections are made through a single connector.
Section 6 defines the electrical characteristics of all input and output signals. Required connectors and
associated hardware are provided in the connector kit (Section 1.2.2).
CAUTION
Do not apply power to the unit until after the rear connector is completely seated.
Connecting the unit while power is applied may cause damage to the device, and to other
LRUs that are connected to the data lines.
NOTE
For data transfer installations, the ring terminal is required. If used, torque the ring
terminal screw to 4-6 in-lbs.
3.2 Equipment Mounting
For final installation and assembly, refer to the outline and installation drawings shown in Appendix A of
this manual.
1. Assemble connector per instructions in Section 2.
2. Install the unit from the back side of the desired installation surface with the circular surface
protruding through the hole.
3. Attach the unit to the installation surface using a minimum of two screws (oriented diagonally).
Rotation orientation of the unit within the mounting location is at the installer’s discretion.
4. Attach the cable harness to the connector, paying attention to the keying and latching features of
the connector.
5. If using mounting kit 011-05043-00 or 011-05043-01, mount adapter plate to desired mounting
surface using specified screws (see Figure A-4) and attach unit to adapter plate using included
screws.
CAUTION
Be careful to not damage the unit or connector during installation. Avoid over torquing
mounting screws.
NOTE
For vertical unit (011-04937-00) installations, ensure the portion of the panel that mates
to the GSB 15 is electrically conductive to ensure proper grounding.
3.2.1
Unit Replacement
Make sure that power is removed before removing the GSB 15.
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4 POST INSTALLATION CONFIGURATION & CHECKOUT
4.1 Mounting, Wiring, and Power Checks
Verify all cables are properly secured and shields are connected to the ground lug located on the back of
the unit. Check the movement of the flight and engine controls to verify there is no interference between
the cabling and control systems. Verify all wiring is installed as described in this manual. Prior to installing
and powering up the GSB 15, the wiring harness must be checked for proper connections to the aircraft
systems and other avionics equipment. Point to Point continuity must be checked to expose any faults such
as shorting to ground or wiring discrepancies. Any faults or discrepancies must be corrected before
proceeding. After accomplishing a continuity check, perform power and ground checks to verify proper
power distribution to the GSB 15. Any faults or discrepancies must be corrected at this time. The GSB 15
can be installed after completion of the continuity and power checks.
4.2 Configuration Setup
Not applicable.
4.3 Diagnostic Information
Not applicable.
4.4 Ground Checks
Not applicable.
4.5 Software Loading Procedure
The GSB 15 does not use or load its own operating software.
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Page 4-1
5 CONTINUED AIRWORTHINESS
Maintenance of the GSB 15 is “on condition” only.
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GSB 15 Installation Manual
Page 5-1
6 CONNECTOR PINOUT INFORMATION
6.1 Pin Function List
6.1.1
P201/202 Connector
NOTE
P201 is the rear connector designation for the GSB 15 (vertical) part number
011-04937-00.
NOTE
P202 is the rear connector designation for the GSB 15 (right angle) part number
011-04937-01.
6
1
1
P201, GSB 15 Vertical (011-04937-00) Unit
6
P202, GSB 15 Right Angle (011-04937-01) Unit
Figure 6-1. Unit View of P201/P202.
Table 6-1 J201/J202 Connector
Pin
Pin Name
I/O
1
AIRCRAFT POWER
IN
14V/28V Aircraft Power Input
2
USB DN
I/O
May use shielded CAT-5 ethernet cable.
3
USB DP
I/O
May use shielded CAT-5 ethernet cable.
4
USB GND
--
May use shielded CAT-5 ethernet cable.
5
BACKLIGHT ENABLE
IN
Deactivated-Low configuration strap. Do not
connect for backlight ON. Ground connection for
backlight OFF.
6
POWER GROUND
--
Ground
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COMMENTS
GSB 15 Installation Manual
Page 6-1
APPENDIX A OUTLINE AND INSTALLATION DRAWINGS
VERTICAL CONNECTOR (-00 CONFIG), UNIT ONLY
1.50 38.1
RIGHT-ANGLE CONNECTOR (-00 CONFIG), UNIT ONLY
.92 23.5
.84 21.4
1.50 38.1
.438±.005 11.11±0.13
1.55 39.3
1.50 38.1
.438±.005 11.11±0.13
0 0.00
0 0.00
VERTICAL CONNECTOR (-00 CONFIG), WITH CONNECTOR KIT (011-05044-00)
.438±.005 11.11±0.13
0 0.00
.4 10
.438±.005 11.11±0.13
.438±.005 11.11±0.13
.438±.005 11.11±0.13
0 0.00
.438±.005 11.11±0.13
.438±.005 11.11±0.13
.4 10
RIGHT-ANGLE CONNECTOR (-00 CONFIG), WITH CONNECTOR KIT (011-05044-00)
1.02 25.9
.64 16.2
1.85 47.0
.80 20.24
BACK OF MOUNTING SURFACE
BACK OF MOUNTING SUFACE
NOTES:
1.
DIMENSIONS: INCHES[mm]. METRIC VALUES ARE FOR REFERENCE ONLY.
2.
DIMENSIONS ARE NOMINAL AND TOLERANCES ARE NOT IMPLIED UNLESS SPECIFICALLY STATED.
Figure A-1 GSB 15 Outline Drawing
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-1
VERTICAL CONNECTOR (-00 CONFIG) WITH CONNECTOR KIT (011-05044-00)
RIGHT-ANGLE CONNECTOR (-01 CONFIG) WITH CONNECTOR KIT (011-05044-00)
GSB 15 UNIT
011-04937-00
GSB 15 UNIT
011-04937-01
AIRCRAFT
PANEL
AIRCRAFT
PANEL
CRIMP PIN
336-00065-05
6 PLACES
4-40 x .125" PAN HEAD SCREW
211-60234-04
CRIMP PIN HOUSING
330-00771-05
16-22 AWG RING TERMINAL
235-00117-00
MOUNTING SCREWS
#4-40 x .25[6.4], PHP
211-60304-08
2 PLACES
,
KIT
B
GS
4-40 x .125" PAN HEAD SCREW
211-60234-04
15
R
TO
EC -00
N
4
N
4
CO -050
1
01
16-22 AWG RING TERMINAL
235-00117-00
CRIMP PIN
336-00065-05
6 PLACES
CRIMP PIN HOUSING
330-00771-05
MOUNTING SCREWS
#4-40 x .25[6.4], PHP
211-60304-08
2 PLACES
Panel Thickness
.000-.050[0.00-1.27]
.050-.125[1.27-3.18]
.125-.188[3.18-4.76]
SB
,G
KIT
15
OR
CT
NE 4-00
N
4
CO -050
1
01
in Connector Kit
Recommended Screw Length Included
(011-05044-00)?
.188[4.76]
.250[6.35]
.313[7.95]
No
Yes, Qty. 2
No
Figure A-2 GSB 15 Installation Drawing (011-05044-00 Mounting Kit)
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-2
RECOMMENDED PANEL CUTOUT DIMENSIONS FOR UNIT
+.030
+0.76
1.000 - .005 25.40 - 0.13
.438±.005 11.11±0.13
.129±.003 3.26±0.08
45°
0 0.00
OR
OR
.438±.005 11.11±0.13
0 0.00
.438±.005 11.11±0.13
.438±.005 11.11±0.13
COUNTERSUNK HOLES
(FOR 100° FLAT HEAD SCREWS)
STANDARD HOLES
(FOR PAN HEAD SCREWS)
2X
2X
.129±.003 3.26±0.08 THRU ALL
.225 5.72 X 100°
OR
OR
Figure A-3 GSB 15 Panel Cutout Drawing (Pan Head and Flat Head Screws)
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-3
VERTICAL CONNECTOR (-00 CONFIG) WITH 2.25" MOUNTING KIT (011-05043-00)
VERTICAL CONNECTOR (-00 CONFIG)WITH 3.125" MOUNTING KIT (011-05043-01)
GSB 15 UNIT
011-04937-00
AIRCRAFT
PANEL
GSB 15 UNIT
011-04937-00
AIRCRAFT
PANEL
2" NOMINAL
ADAPTER PLATE (Ø 2.25")
125-00581-02
MOUNTING SCREWS,
#6-32
4 PLACES
MOUNTING SCREWS,
15
SB
#4-40 x .25[6.4], FLHP100
,G
"
5
211-63304-08
.2
,2
2 PLACES
KIT
G
TIN 00
UN 43MO -050
1
01
3" NOMINAL OR 3 ATI
ADAPTER PLATE (Ø 3.125")
125-00581-12
MOUNTING SCREWS,
#6-32
4 PLACES
5
MOUNTING SCREWS,
B1
GS
,
#4-40 x .25[6.4], FLHP100
"
5
.12
211-63304-08
,3
KI T
2 PLACES
G
TIN 01
UN 043O
5
M -0
1
01
Panel Thickness
Recommended Screw Length
Panel Thickness
Recommended Screw Length
.000-.050[0.00-1.27]
.050-.125[1.27-3.18]
.125-.188[3.18-4.76]
.188[4.76] Minimum
.250[6.35] Minimum
.313[7.95] Minimum
.000-.050[0.00-1.27]
.050-.125[1.27-3.18]
.125-.188[3.18-4.76]
.188[4.76] Minimum
.250[6.35] Minimum
.313[7.95] Minimum
Figure A-4 GSB 15 Assembly Drawing (011-05043-00 and -01 Mounting Kits)
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-4
011-05043-00 STANDARD HOLES (FOR PAN HEAD SCREWS)
011-05043-01 STANDARD HOLES (FOR PAN HEAD SCREWS)
+0.76
+.030
3.125 - .005 79.38 - 0.13
4X
+0.76
+.030
2.250 - .005 57.15 - 0.13
2.475 62.86
.150±.003 3.80±0.08
1.856 47.15
4X
.150±.003 3.80±0.08
45°
1.856 47.15
2.475 62.86
45°
1.313 33.34
1.750 44.45
2.625 66.68
3.500 88.90
Figure A-5 GSB 15 Panel Cutout Drawing w/Pan Head Screws (011-05043-00 and -01 Mounting Kits)
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-5
011-05043-00 COUNTERSUNK HOLES (FOR 100° FLAT HEAD SCREWS)
011-05043-01 COUNTERSUNK HOLES (FOR 100° FLAT HEAD SCREWS)
4X
4X
.150 3.80 THRU ALL
.279 7.09 X 100°
.150 3.80 THRU ALL
.279 7.09 X 100°
Figure A-6 GSB 15 Panel Cutout Drawing w/Flat Head Screws (011-05043-00 and -01 Mounting Kits)
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page A-6
APPENDIX B INTERCONNECT DRAWINGS
GSB 15
P201/ J201/
P202 J202
AIRCRAFT POWER
1
USB DN
2
USB DP
3
USB GROUND
4
BACKLIGHT ENABLE
5
POWER GROUND
6
5A
TO AIRCRAFT POWER
SEE NOTE 3
SEE NOTES 1 AND 2
SEE NOTE 4
SEE NOTE 3
NOTES:
1. TERMINATE SHIELDING 0.01” [0.0254 cm] FROM CONNECTOR
2. USE TWISTED SHIELDED PAIR WIRING, 6 ft MAX.
3. USE 22 AWG OR LARGER FOR POWER AND GROUND WIRES, 25 ft MAX.
4. RING TERMINAL P/N 235-00117-00
5. SYMBOL DESIGNATIONS:
AIRCRAFT GROUND
TWISTED SHIELDED PAIR
Figure B-1 GSB 15 Example Interconnect
190-00303-A3
Rev 2
GSB 15 Installation Manual
Page B-1
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