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JA34-BT1
Installation And Operating Manual
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Jupiter Avionics JA34-BT1 Installation And Operating Manual

Download
Rev
JA34-BT1
Universal Radio Adapter
With Bluetooth®
Rev D
Jupiter Avionics Corporation
1959 Kirschner Road
Kelowna BC
Canada V1Y 4N7
Tel: +1 778 478 2232
Toll-Free: 1 855 478 2232
www.jupiteravionics.com
B Page i
JA34-BT1 Universal Radio Adapter with Bluetooth
Revision
A
B
C
D
Prepared:
Checked:
Approved:
IMPORTANT:
Installation and Operating Manual
Copyright 2014 Jupiter Avionics Corp.
All rights reserved
Jupiter Avionics Corporation (JAC) permits a single copy of this manual to be printed or downloaded for the express use of an installing agency. Any such electronic or printed copy of this manual must contain the complete text of this copyright notice. Any unauthorized commercial distribution of this manual is strictly prohibited. Except as described above, 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 JAC.
Information in this document is subject to change without notice.
To confirm the current revision status of this manual, visit the JAC website:
®
www.jupiteravionics
.com
RECORD OF REVISIONS
Rev Date Description ECR
Apr 2014 Initial release, Serial number 1001 and higher. 2452 Nov 2014 Removed product Certification references. 3173 Mar 2015 Changes to ProCS Settings 3449 Sep 2019
Updated manual; added iPhone Connectivity Configuration 3699
Rev D Page ii
MPB
JAC
09-23-19
SRM
JAC
09-23-19
KDV
JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual

Table of Contents

SECTION 1 - DESCRIPTION ................................................................................................................................................. 1
1.1 System Overview .................................................................................................................................................... 1
1.2 Features Overview .................................................................................................................................................. 1
1.3 Inputs and Outputs .................................................................................................................................................. 1
1.3.1 Inputs ............................................................................................................................................................... 1
1.3.2 Outputs ............................................................................................................................................................ 1
1.4 Specifications .......................................................................................................................................................... 2
1.4.1 Electrical Specifications................................................................................................................................... 2
1.4.2 Mechanical Specifications ............................................................................................................................... 3
1.4.3 Flammability of Materials ................................................................................................................................ 3
1.4.4 Product Configuration Version......................................................................................................................... 3
1.4.5 FCC Compliance Statement ............................................................................................................................ 3
1.4.6 IC Compliance Statement................................................................................................................................ 3
1.4.7 Co-location with Other Transmitters................................................................................................................. 3
SECTION 2 – INSTALLATION ............................................................................................................................................... 4
2.1 Introduction .............................................................................................................................................................. 4
2.2 Continued Airworthiness ......................................................................................................................................... 4
2.3 Unpacking and Inspecting Equipment..................................................................................................................... 4
2.3.1 Warranty .............................................................................................................................................................. 4
2.4 Installation Procedures ............................................................................................................................................ 4
2.4.1 Installation Limitations ......................................................................................................................................... 4
2.4.2 Cabling and Wiring .............................................................................................................................................. 4
2.4.3 Mechanical Installation ........................................................................................................................................ 5
2.4.4 Post Installation Checks ...................................................................................................................................... 5
2.5 System Operation.................................................................................................................................................... 5
2.5.1 Configuration Operation .................................................................................................................................. 5
2.5.2 Receive Operation ........................................................................................................................................... 6
2.5.3 Sidetone Operation ......................................................................................................................................... 6
2.5.4 Relay Operation .............................................................................................................................................. 6
2.5.5 Microphone Operation ..................................................................................................................................... 6
2.6 Adjustments and Configuration using ProCS™ ...................................................................................................... 6
2.6.1 Configuration Cabling Requirements .............................................................................................................. 6
2.6.2 ProCS™ Setup ................................................................................................................................................ 6
2.6.3 Configurable Settings ...................................................................................................................................... 7
2.6.4 JA34-BT1 Settings .......................................................................................................................................... 7
2.6.5 Aircraft Audio Systems List ............................................................................................................................. 8
2.6.6 Non-Aircraft Radios List .................................................................................................................................. 9
2.6.7 JA34-BT1 Connector Maps ............................................................................................................................. 9
2.6.8 Other Configuration Features .......................................................................................................................... 9
2.7 Installation Kit .......................................................................................................................................................... 9
2.7.1 Recommended Crimp tools ............................................................................................................................. 9
2.8 Installation Drawings ............................................................................................................................................... 9
SECTION 3 – OPERATION .................................................................................................................................................. 10
3.1 Introduction ............................................................................................................................................................ 10
3.2 Bluetooth® Operation ............................................................................................................................................ 10
3.3 Bluetooth® Pairing ................................................................................................................................................. 10
3.4 Bluetooth® Status Indicator ................................................................................................................................... 11
Appendix A - Installation Drawings ................................................................................................................................... A1
A1 Introduction ............................................................................................................................................................ A1
A2 Installation Drawings ............................................................................................................................................. A1
Appendix B - Installation Documents ............................................................................................................................... B1
B1 Airworthiness Approval ......................................................................................................................................... B2
B2 Instructions for Continued Airworthiness .............................................................................................................. B2
®
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JA34-BT1 Universal Radio Adapter with Bluetooth
®

SECTION 1 - DESCRIPTION

Name
Qty
Type
CONFIG DATA TO JA34-BT1
1
Data signal
MODE SELECT TO JA34-BT1
1
Discrete signal
RECEIVE INPUT
1
Audio signal
MIC INPUT
1
Audio signal
+28 VDC POWER
1
Power Supply
RELAY KEY INPUT
1
Discrete signal
Name
Qty
Type
CONFIG DATA FROM JA34-BT1
1
Data signal
RECEIVE OUT
1
Audio signal
MIC OUTPUT
1
Audio signal
RELAY CONTACTS
6
Audio signal

1.1 System Overview

The JA34-BT1 Universal Radio Adapter with Bluetooth® allows the aircraft audio management system access to a non-aviation radio and Bluetooth from the radio to allow a noise free installation. Microphone biasing and artificial sidetone generation are selectable for radios without them.
The JA34-BT1 is setup on a per installation basis using a Configuration Cable and downloading the system configuration settings from a PC into non-volatile control devices.
®
enabled devices. The JA34-BT1 provides fully isolated audio signal paths to and

1.2 Features Overvi e w

The JA34-BT1 unit features an industry standard D-Sub connector pin-out to allow easy field upgrades.
All internal settings are quickly adjusted using the proprietary ProCS (Product Configuration Software).
Two configuration ports are provided for configuration loading, one beside the main connector and one on the rear.
All audio outputs
The JA34-BT1 provides relay contact keying, artificial sidetone generation and microphone voltage biasing.
The JA34-BT1 contains a Bluetooth range.
The JA34-BT1 is a Bluetooth® compliant device with the following supported profiles:
- HFP (Hands Free Profile) for cell phone interface.
- A2DP (Advanced Audio Distribution Profile) for music interface.
are floating and balanced.
®
Audio Module and is a Bluetooth® class 3 device with a <10 meters operating

1.3 Inputs and Outputs

Refer to the JA34-BT1 connector map for the mating connector designators and contact assignments for the input and output signals.

1.3.1 Inputs

1.3.2 Outputs

Rev D Page 1
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.4.1
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.4.1.1
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Specifi
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Receive o Micropho Micropho
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28 Vdc
30.3 Vdc
22.0 Vdc
18.0 Vdc
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7.75 Vrm 250 mVr
2.50 Vrm 250 mVr 50 mVrm
≤3dB fro ≤3dB fro
10% s 10%
10% s10% 10%
300 to 600 300 to 600
Hz Hz
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≥60 dB
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Page
JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual
®
1.4.2

Mechanical Specifications

Height
Depth
Width
Weight
Material
Connectors (3):
Mounting
Bonding
Installation kit part number
J2, J3 J1
1.27 in [32.3 mm] maximum
2.42 in [61.5 mm] maximum
4.52 in [114.8 mm] maximum
0.43 lb [0.20 kg] maximum
brushed aluminum with conversion coating
Two 4 pole 3.5mm jack One 25-pin D-Sub male V5 locking
4 x 10-32 fasteners
≤ 2.5 mΩ
INST-JA34

1.4.3 Flammability of Materials

The JA34-BT1 complies with the flammability testing of materials and the Small Parts Exemption.
requirements of RTCA/DO-160G Sec 26.3.3 "Flammability", through equivalent
1.4.4 Product Configuration Software Version
Configuration of the JA34-BT1 requires the Product Configuration Software (ProCS) version v0.16.4 or later. Refer to the release notes from http://www.jupiteravionics.com/productsoftware.php or contact Jupiter Avionics to ensure the correct version is used.
1.4.5 FCC Compliance Statement
Contains Transmitter Module FCC ID: QOQWT32AE
This device complies with Part 15 of the FCC Rules. Operation is subject to the following two conditions:
(1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.
1.4.6 IC Compliance Statement
Contains Transmitter Module Industry Canada ID: 5123A-BGTWT32AE
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
llllll l'appareil.
1.4.7
Co-location with Other Transmitters
Ensure all JA34-BT1 units are installed with at least 20 cm between other JA34-BT1 units and antennae from other transmitting equipment.
Rev D Page 3
JA34-BT1 Universal Radio Adapter with Bluetooth
®

SECTION 2 – INSTALLATION

2.1 Introduction

This section contains unpacking and inspection procedures, installation information, and post-installation checks.

2.2 Continued Airworthiness

Maintenance of the JA34-BT1 is on condition only. Scheduled inspection and/or periodic maintenance of this unit is not required.

2.3 Unpacking and Inspecting Equipment

Unpack the equipment carefully. Check for shipping damage and report any problems to the relevant carrier. Confirm that the Authorized Release Certificate or Certificate of Conformance is included. Complete the on-line warranty card from the Jupiter Avionics Corporation (JAC) website - www.jupiteravionics.com/warranty

2.3.1 Warranty

This product manufactured by JAC is warranted to be free of defects in workmanship or performance for 2 years from the date of installation by an approved JAC dealer or agency. This warranty covers the cost of all materials and labour to repair or replace the unit, but does not include the cost of transporting the defective unit to and from JAC or its designated warranty repair centre, or of removing and replacing the defective unit in the aircraft. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alteration or repairs.
THIS WARRANTY IS VOID IF THE PRODUCT IS NOT INSTALLED BY AN AUTHORIZED JAC DEALER. If the on­line warranty card is not completed, the product will be warranted from the date of manufacture.
Contact JAC for return authorization, and for any questions regarding this warranty and how it applies to your unit(s). JAC is the final arbiter concerning warranty issues.

2.4 Installation Procedures

WARNING: Loud noise can cause hearing damage. Set the headset volume to minimum before conducting tests, and slowly increase the volume to a comfortable listening level.
CAUTION: The power input circuitry of the unit may be damaged if the installation does not conform to the wiring instructions in this manual.

2.4.1 Installation Limitations

The JA34-BT1 may be installed only by following the applicable airworthiness requirements.

2.4.2 Cabling and Wiring

All wire shall be selected in accordance with the original aircraft manufacturer’s maintenance instructions, or AC43.13­1B Change 1, Paragraphs 11-76 through 11-78. Unshielded wire types shall qualify to MIL-W-22759 as specified in AC43.13-1B Change 1, Paragraphs 11-85, 11-86, and listed in Table 11-11. For shielded wire applications, use Tefzel MIL-C-27500 shielded wire with tag ring or equivalent (for shield terminations) to make the most compact and easily
terminated interconnect. Follow the Connector Map in Appendix A of this manual.
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JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual
Allow 3” from the end of the shielded wiring to the shield termination to allow the connector hood to be easily installed. Refer to the Interconnect drawing in Appendix A of this manual for shield termination details. Note that this unit has a ‘clamshell’ hood that is installed after the wiring is complete.
Maintain wire segregation and route wiring in accordance with the original aircraft manufacturer’s maintenance instructions.
Unless otherwise noted, all wiring shall be a minimum of 24 AWG, except power and ground lines, which shall be a minimum of 22 AWG. Refer to the Interconnect drawing for additional specifications. Check that the ground connection is clean and well secured, and that it shares no path with any electrically noisy aircraft accessories such as blowers, turn-and-bank instruments, or similar loads.

2.4.3 Mechanical Installation

The JA34-BT1 can be mounted in any attitude and location with adequate space and sufficient clearance for the connector and wiring harness. It requires no direct cooling. Ensure all JA34-BT1 units are installed with at least
20 cm between other JA34-BT1 units and antennae from other transmitting equipment.

2.4.4 Post Installation Checks

2.4.4.1 Voltage/Resistance checks.
®
Do not attach this unit until the following conditions are met:
a) Check P1 pin 1 for +28 Vdc power. b) Check P1 pin 14 (Power Ground) for continuity to ground (les c) Check P1 pin 15 (Chassis Ground) for continuity to ground (less than 0.5 Ω).
d) Check all pins for shorts to ground or adjacent pins.
2.4.4.2 Configuration
Ensure that the JA34-BT1 contains the correct configuration settings. This may be done at the factory, on the maintenance bench or in the aircraft before the power on checks are performed. Refer to section 2.5.
2.4.4.3 Power on Checks.
Power up the aircraft’s systems and confirm normal operation of all functions of the JA34-BT1 (see section 2.5).
a) Confirm radio operation for both receive and transmit. Do not proceed until the radio is functioning correctly.
b) Unusual buzzes, hums or other background audio are symptomatic of multiple grounds, or noisy external
systems such as blowers or pumps sharing wiring with the audio system. If a transmitter fails to key or correctly modulate it is often the result of not connecting all required grounds to the radio or external audio system.
c) Check that all configurations settings are correct.
s than 0.5 Ω).
When all performance checks are satisfied, complete the necessary regulatory documentation before releasing the aircraft for service. Refer to Appendix B.

2.5 System Operation

The JA34-BT1 is a remote mount unit and has no user accessible controls.

2.5.1 Configuration Operation

The JA34-BT1 accepts commands on the Configuration connector via the configuration cable and the configuration tool ProCs™. (See section 2.6 Adjustments and Configuration)
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JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual

2.5.2 Receive Operation

The RECEIVE INPUT is level controlled and summed with the MIC INPUT (Sidetone) and routed to the RECEIVE OUTPUT.
®
When Bluetooth OUTPUT.
operation is enabled, the Bluetooth® received audio is level controlled and routed to the RECEIVE

2.5.3 Sidetone Operation

The MIC INPUT audio is level controlled (sidetone level) and routed to the RECEIVE OUTPUT.

2.5.4 Relay Operation

When the RELAY KEY INPUT is inactive, the RELAY COMMON contacts are connected to the RELAY N.C. contacts.
When the RELAY KEY INPUT is active (connected to POWER GROUND), the RELAY COMMON contacts are connected to the RELAY N.O. contacts.

2.5.5 Microphone Operation

The MIC INPUT audio is level controlled and routed to the MIC OUTPUT.
®
®
When Bluetooth controlled and routed to the Bluetooth
operation is enabled and the Hands Free Profile (HFP) is selected, the MIC INPUT audio is level
®
transmit audio.

2.6 Adjustments and Configuration using ProCS™

All the JA34-BT1 internal adjustments are set from the Product Configuration Software ProCS™. Configuration data is sent to the JA34-BT1 via the front panel connector (♫/io), using the Configuration Cables and a computer running the ProCS™ software. For configuration requirements, see section 2.5.1.
For full information on the configuration process, and for installation of ProCS™ on your computer, refer to the
ProCS™ manual on the Jupiter Avionics website - www.jupiteravionics.com/productsoftware.

2.6.1 Configuration Cabling Requirements

To configure the JA34-BT1, it is necessary to load the Product Configuration Software ProCS™ onto a Windows- based computer as described in the ProCS™ manual.
The cables required to configure the JA34-BT1 are not included with the unit.
Cabling option 1:
Quantity Description JAC Part #
1 USB A to RS232 9-Pin Cable CAB-USB-0002 1 Configuration Cable JA99-001
Cabling option 2:
Quantity Description JAC Part #
1 USB A Male to RS232 3.5mm Plug CAB-USB-0006

2.6.2 ProCS™ Setup

The JA34-BT1 menu items 'ProCS Setup' provide drawings showing the cabling arrangement (using JA99 or CAB-USB-0006) for connecting the JA34-BT1 to a computer to allow configuration using ProCS™.
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JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual

2.6.3 Configurable Settings

A standard unit is shipped from the factory with all internal adjustments configured to the default levels. At installation, it may be desirable to change some of these settings to suit the local operating environment.
Note: To configure the JA34-BT1, power must be applied to the unit.
Within ProCS™, the configurable settings are grouped together into the following sections:

2.6.4 JA34-BT1 Settings

The Settings window is divided into three sections: the Aircraft Audio System; the Universal Radio Adapter; and the
Non-Aircraft Radio. Each section is colour-coded to keep the relevant information together.
The Settings window is divided into five sections:
• the Aircraft Audio System
• the JA34-BT1 Universal Radio Adapter Adjustments
®
• the Bluetooth
• the Non-Aircraft Radio Selection.
Each section is colour-coded to keep the relevant information together.
Transceiver
®
2.6.4.1 Aircraft Audio System Selection (Green block)
The appropriate aircraft audio system is selected from a drop-down list at the top of the block, and all relevant configuration information is added automatically. Other aircraft Audio systems can be added to the list (see section 2.6.5).
Rev D Page 7
JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual
2.6.4.2 JA34-BT1 Universal Radio Adapter Adjustments (Blue block)
The blue block refers to the adjustments and settings for the JA34-BT1 Universal Radio Adapter.
Receive Input The level of the RECEIVE INPUT may be adjusted from 1.50 to 10.00 Vrms. (Default 7.75 Vrms) Artificial Sidetone
The Artificial Sidetone may be selected as ON or OFF. When selected ON, the level of the MIC INPUT sidetone may
be adjusted from -12 to 0 dB. (Default -10 dB) (When OFF, the level is -35 dB)
Mic Bias The MIC Bias may be ON or OFF. (Default ON) Mic Output The level of the MIC OUTPUT signal may be adjusted from 0.010 to 0.625 Vrms. (Default 0.250mVrms) Mic Output Load Impedance The MIC OUTPUT impedance may be set to 8 Ohms or 150 Ohms. (Default 150 Ohm s) Bluetooth® Transceiver
A custom Bluetooth® device name identifies the JA34-BT1 in the user's cell phone. The volume can be set to suit the user's preference. The Bluetooth® Profile is configured to provide both A2DP (Advanced Audio Distribution Profile) for playing audio from a smartphone or other music source, and HFP (Hands Free Profile) for connecting to a cell phone. If a device is attached, the 'Edit Name', 'Clear Pairing' and 'Set Defaults' buttons will be available for use.
®
2.6.4.3 Non-Aircraft Radio Selection (Orange block)
The appropriate Non-Aircraft Radio is selected from a drop-down list at the top of the block, and all relevant configuration information is added automatically. Other Non-Aircraft Radios can be added to the list (see section 2.6.6).

2.6.5 Aircraft Audio Systems List

This is a list of Aircraft Audio Systems, and shows the configuration information that will be added to the JA34-BT1 Settings page.
If it is desirable to add other Audio systems, click on the Aircraft Audio Systems List. A new audio system and its parameters can be added by clicking on (the ‘New Aircraft Audio System' button). A new line will be added to
the bottom of the list, and double clicking on each part of the line will highlight it to allow changes. When the relevant
details have been added, use the (‘Save Changes’) or (‘Cancel All Changes’) button as required. The added
system will then appear on the appropriate drop-down menu list.
Rev D Page 8
JA34-BT1 Universal Radio Adapter with Bluetooth
Standard D-Sub Crimp Tool Chart
Tool Type
Hand crimping tool
Positioner
Insertion/extractor tool
POSITRONIC
9507-0-0-0
9502-5-0-0
4711-2-0-0
DANIELS
AFM 8
K13-1
91067-2
MIL-SPEC
M22520/2-01
M22520/2-08
M81969/1-02
Installation and Operating Manual

2.6.6 Non-Aircraft Radios List

This is a list of Non-Aircraft Radios and the configuration information that will be added to the JA34-BT1 Settings
page. The list is similar to the Aircraft Audio Systems list, and new radios can be added in the same way.

2.6.7 JA34-BT1 Connector Maps

JA34-BT1 Connector Maps and Interconnects are included here for information only.

2.6.8 Other Configuration Features

®
In the JA34-BT1 Product Information Window, the model number, serial number and check sum of the JA34-BT1 Universal Radio Adapter with Bluetooth
®
can be viewed.

2.7 Installation Kit

The kit required to install this unit is not included with the unit.
The installation kit (Part # INST-JA34) consists of the following:
Quantity Description JAC Part #
1 1
1
TAG ring D-Sub 25-pin connector, hood and 25 crimp pins Heat Shrink Tubing
CON-5500-0625 CON-3420-0025 WIR-HTSK-1000

2.7.1 Recommended Crimp tools

2.8 Installation Drawings

The drawings and documents required for Installation can be found in Appendix A of this manual.
Rev D Page 9
JA34-BT1 Universal Radio Adapter with Bluetooth
®

3.1 Introduction

SECTION 3 – OPERATION

The JA34-BT1 Universal Radio Adapter with Bluetooth® allows the aircraft audio management system access to a non-aviation radio and Bluetooth
®
enabled devices.

3.2 Bluetooth® Operation

The JA34-BT1 is a remote mount unit and has no user accessible controls. However, when a Bluetooth® enabled device such as a cell phone is introduced into the aircraft, it can be paired with the JA34-BT1.
®
The Bluetooth Avionics Corporation ProCS™ configuration software. At that time, the Bluetooth
transceiver can be configured at installation or in the field by a dealer or installer, using the Jupiter
®
volume and the device name can
be chosen.
®
The default Bluetooth
device name is JA34-BT1-xxxx where xxxx is the unit's serial number.

3.3 Bluetooth® Pairing

Pairing is i Bluetooth operating manual for full pairing information.
Typically, from the phone 'Settings' screen, select 'Bluetooth' and ensure that it is turned on. Then confirm
that the list of discoverable devices includes JA34-BT1
or the selected device name. Select this device.
nitiated using your cellphone or other
®
enabled device. Refer to your cellphone
The cellphone will pair with the JA34-BT1 in the mode selected via ProCS™ - HFP (Hands-Free Profile), SPP (Serial Port Profile) - A2DP Sink - A2DP Source. If necessary, confirm the mode with the installer.
Note: Some cell phones may not support A2DP
audio streaming. Refer to your cellphone manual for
more information.
Note: If the Bluetooth
®
mode of the JA34-BT1 is changed at a later date, it may be necessary to un-pair the
cellphone and repeat the pairing process to reset to the updated mode of operation.
Rev D Page 10

3.3.1 iPhone Connectivity Configuration

JA34-BT1 Universal Radio Adapter with Bluetooth
Installation and Operating Manual
®
The default setting for Call Audio Routing allows the iPhone to select where to route calls; either to the built-in speaker or a Bluetooth
To ensure that the paired
when answering incoming calls.
default
®
headset. This can cause response delays and possible 'dropped calls'.
iPhone works more consistently, it should be configured to use the Bluetooth
®
device as a
Example from the iPhone 5:
• Select
• Select
• Select
• Choose
Settings Accessibility Call Audio Routing
Headset
Example from the iPhone 6:
• Select
• Select
• Select
• Select
• Choose
hanging the setting to Headset ensures that the iPhone selects the Bluetooth
C
Settings General Accessibility Call Audio Routing
Headset
®
device as its first option, but will
revert to the iPhone's built-in speaker if no device is found.

3.4 Bluetooth® Status Indicator

If an optional Bluetooth various stages of the connection process.
®
Status Indicator is installed, the table below describes how an indicator lamp will behave at
Light
Bluetooth
Flashing Waiting for connection
Steady Connected
Off
Bluetooth
®
Connection Status
®
off
Rev A Page 11
JA34-BT1 Universal Radio Adapter with Bluetooth
®
Installation and Operating Manual

Appendix A - Installation Drawings

A1 Introduction

The drawings necessary for installation and troubleshooting of the JA34-BT1 Universal Radio Adapter with Bluetooth are in this Appendix, as listed below.

A2 Installation Drawings

DOCUMENT Rev
JA34-BT1 Connector Map A
JA34-BT1 Interconnect C
JA34-BT1 Mechanical Installation C
Rev D Page A1
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 1/1
JA34-BT1 Connector Map Rev A.dwg
TAT
1 2 3 4 5
14 15 16 17
+28 VDC POWER
SPARE
MIC INPUT HI
RECEIVE OUTPUT HI
POWER GROUND
CHASSIS GROUND
MIC INPUT LO
RECEIVE OUTPUT LO
P1
25 PIN FEMALE DMIN
MATING CONNECTOR
VIEW IS FROM REAR OF MATING CONNECTOR
6 7 8
19 2018
OUTPUT GROUND
MIC OUTPUT HI
RECEIVE INPUT HI
RELAY KEY INPUT
MIC OUTPUT LO
RECEIVE INPUT LO
OUTPUT GROUND
9 102211 12 13
24 2523
RELAY N.O. 1
JUMPER
RELAY COMMON 1
RELAY N.O. 2
RELAY COMMON 2
OUTPUT GROUND
RELAY N.C. 1
OUTPUT GROUND
RELAY N.C. 2
JUMPER
21
P2-P3
4 POLE MALE 3.5MM STEREO
TIP: TX DATA 1ST RING: RX DATA 2ND RING: GROUND 3RD RING: MODE SELECT
JA99 CONFIGURATION CABLE
MATING PLUG NAMES JA34 SIGNAL NAMES
CONFIG DATA TO JA34 CONFIG DATA FROM JA34 GROUND MODE SELECT
CONFIGURATION CONNECTOR
04-23-14
04-23-14
JAC
DS
JAC
KDV
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 1/6
JA34-BT1 Interconnect Rev C.dwg
TAT
JA34-BT1 INTERCONNECT WIRING NOTES
NOTES
All wire size should be 24 AWG min unless otherwise specified. Unshielded wire should be selected per FAA AC43.13-1B change 1 para 11-76 TO 11-78. Wire types should be in accordance with MIL-W-22759 as described in FAA AC43.13-1B change 1 para 11-85 and 11-86 and listed in table
11-11 or 11-12. All shielded cable should be in accordance with MIL-DTL-27500 (Revision H or later). Jumper for a ground to key radio. Jumper for a floating contact closure. Input/Outputs are transformer coupled (Balanced), 'LO' wires require one termination to ground
(usually at the source). Connection to airframe ground should be made with 20 AWG wire. Length not to exceed 3 FT (0.9 M). Cable shields at the JA34-BT1 connector pins should be terminated to airframe ground using a tag ring
P/N: MS27741-3 or equivalent. Optional resistors for routing music to audio controller. Optional switch to disable transceiver PTT during phone call.
2
1.
3 4
5 6
7 8
02-13-19
02-13-19
JAC
SRM
JAC
KDV
MIC INPUT HI
MIC INPUT LO
MIC AUDIO OUT MIC AUDIO LO
AUDIO CONTROLLER
3
16
JA34-BT1 J1
P1 25 PIN FEMALE DMIN MATING CONNECTOR
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 2/6
JA34-BT1 Interconnect Rev C.dwg
TAT
RECEIVE OUTPUT HI
RECEIVE OUTPUT LO
4
17
RX AUDIO IN RX AUDIO LO
MIC OUTPUT HI
MIC OUTPUT LO
5
18
RECEIVE INPUT HI
RECEIVE INPUT LO
6
19
RELAY KEY INPUT MIC KEYLINE7
MIC AUDIO HI MIC AUDIO LO
MOBILE TRANSCEIVER
RX AUDIO OUT RX AUDIO LO
RELAY N.O. 1 KEYLINE9
RELAY COMMON 1 KEYLINE RETURN10
RELAY N.C. 1
22
11
12
24
OUTPUT GROUND
23
JUMPER
25
JUMPER 13
OUTPUT GROUND 8
OUTPUT GROUND
21
OUTPUT GROUND
20
+28 VDC POWER +28 VDC POWER
1
SPARE 2
POWER GROUND 14
CHASSIS GROUND
15
POWER GROUND
22 AWG.
22 AWG.
2
4
4
4
3
RELAY N.O. 2
RELAY COMMON 2
RELAY N.C. 2
1A
5
20 AWG.
6
02-13-19
02-13-19
JAC
SRM
JAC
KDV
JA34-BT1 J1
P1 25 PIN FEMALE DMIN MATING CONNECTOR
MIC INPUT LO
MIC INPUT HI163
AUDIO CONTROLLER
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 3/6
JA34-BT1 Interconnect Rev C.dwg
TAT
RECEIVE OUTPUT HI
RECEIVE OUTPUT LO
4
17
MUSIC HI MUSIC LO
MIC OUTPUT HI
MIC OUTPUT LO
5
18
RECEIVE INPUT HI
RECEIVE INPUT LO
6
19
RELAY KEY INPUT 7
USING ADVANCED
MUSIC SOURCE
RELAY N.O. 1 9
RELAY COMMON 1 10
RELAY N.C. 1
22
11
12
24
OUTPUT GROUND
23
JUMPER
25
JUMPER 13
OUTPUT GROUND 8
OUTPUT GROUND
21
OUTPUT GROUND
20
+28 VDC POWER +28 VDC POWER
1
SPARE 2
POWER GROUND 14
CHASSIS GROUND
15
POWER GROUND
22 AWG.
22 AWG.
4
RELAY N.O. 2
RELAY COMMON 2
RELAY N.C. 2
1A
5
20 AWG.
6
OPTIONAL: BLUETOOTH MUSIC INPUT
BLUETOOTH
AUDIO DISTRIBUTION
PROFILE (A2DP)
02-13-19
02-13-19
JAC
SRM
JAC
KDV
JA34-BT1 J1
P1 25 PIN FEMALE DMIN MATING CONNECTOR
MIC INPUT LO
MIC INPUT HI163
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 4/6
JA34-BT1 Interconnect Rev C.dwg
TAT
RECEIVE OUTPUT HI
RECEIVE OUTPUT LO
4
17
MIC OUTPUT HI
MIC OUTPUT LO
5
18
RECEIVE INPUT HI
RECEIVE INPUT LO
6
19
RELAY KEY INPUT 7
USING HANDS
WITH BLUETOOTH
RELAY N.O. 1 9
RELAY COMMON 1 10
RELAY N.C. 1
22
11
12
24
OUTPUT GROUND
23
JUMPER
25
JUMPER 13
OUTPUT GROUND 8
OUTPUT GROUND
21
OUTPUT GROUND
20
+28 VDC POWER +28 VDC POWER
1
SPARE 2
POWER GROUND 14
CHASSIS GROUND
15
POWER GROUND
22 AWG.
22 AWG.
4
RELAY N.O. 2
RELAY COMMON 2
RELAY N.C. 2
1A
5
20 AWG.
6
OPTIONAL: BLUETOOTH CELL PHONE
CELL PHONE
FREE PROFILE
(HFP)
MIC AUDIO OUT MIC AUDIO LO
AUDIO CONTROLLER
RX AUDIO IN RX AUDIO LO
N/C
02-13-19
02-13-19
JAC
SRM
JAC
KDV
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter With Bluetooth
J2 and J3 Interconnect
JA34-BT1 5/6
JA34-BT1 Interconnect Rev C.dwg
TAT
PART OF
CONFIGURATION CABLE
CAB-USB-0006
or JA99-001
JA34-BT1 CONFIGURATION CONNECTOR
4 POLE MALE 3.5MM STEREO
MATING CONNECTOR
CONFIGURATION CONNECTOR
J2 or J3
CONFIG DATA TO JAxx
CONFIG DATA FROM JAxx
GROUND
MODE SELECT CONFIG DATA TO JA34 CONFIG DATA FROM JA34 GROUND
3RD RING
TIP 1ST RING 2ND RING
MODE SELECT/CONFIG AUDIO
02-13-19
02-13-19
JAC
SRM
JAC
KDV
JA34-BT1 J1
P1 25 PIN FEMALE DMIN MATING CONNECTOR
MIC INPUT LO
MIC INPUT HI163
AUDIO CONTROLLER
MIC AUDIO LO
MIC AUDIO OUT
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY TO JUPITER AVIONICS CORP.
Universal Radio Adapter
With Bluetooth
JA34-BT1 6/6
JA34-BT1 Interconnect Rev C.dwg
TAT
RECEIVE OUTPUT HI
RECEIVE OUTPUT LO
4
17
RX AUDIO IN RX AUDIO LO
MIC OUTPUT HI
MIC OUTPUT LO
5
18
RECEIVE INPUT HI
RECEIVE INPUT LO
6
19
RELAY KEY INPUT
MIC KEYLINE
7
MIC AUDIO HI MIC AUDIO LO
MOBILE TRANSCEIVER
RX AUDIO OUT RX AUDIO LO
RELAY N.O. 1 KEYLINE
9
RELAY COMMON 1 KEYLINE RETURN10
RELAY N.C. 1 22
11
12
24
OUTPUT GROUND 23
JUMPER
25
JUMPER
13
OUTPUT GROUND
8
OUTPUT GROUND 21
OUTPUT GROUND
20
+28 VDC POWER +28 VDC POWER
1
SPARE 2
POWER GROUND 14
CHASSIS GROUND
15
POWER GROUND
22 AWG.
22 AWG.
2
4
4
4
3
RELAY N.O. 2
RELAY COMMON 2
RELAY N.C. 2
1A
5
20 AWG.
6
MUSIC HI MUSIC LO
kOhms
2.7
kOhms
2.7
8
AUX TX MODE SWITCH
PHONE
AUX
7
WITH HANDSFREE AND
ADVANCED AUDIO
DISTRIBUTION PROFILES
MOBILE PHONE
OPTION: JA34-BT1 Interconnect to a Transceiver and a Mobile Phone with music.
02-13-19
02-13-19
JAC
SRM
JAC
KDV
4.52in MAX
114.8mm MAX
2.42in MAX
1.80in
61.5mm MAX
45.7mm
2.06in
52.3mm
89.4mm MAX
4.00in
101.6mm
3.52in MAX
0.53in
13.5mm
66.5mm MAX
29.2mm
2.62in MAX
1.15in
4 x 0.21in 5.4mm
32.3mm MAX
1.27in MAX
UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES ANGLES ARE IN DEGREES TOLERANCES: 1 DEC PLACE: 0.1 2 DEC PLACE: 0.01 3 DEC PLACE: 0.005 ANGLES:
MATERIAL:
JUPITER AVIONICS TEMPLATE SOLIDWORKS PORT R AI T SI Z EA REVB . D RW D O T
FINISH:
0.5 DEG
N/A
N/A
PREPARED
TAT
JAC
CHECKED
06-05-15
DS
JAC
APPROVED
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
DRAWING NOT TO SCALE
06-05-15
KDV
CENTER OF GRAVITY
0.03in [0.8mm]
WEIGHT: 0.43 lbs [0.20 kg] MAX.
TITLE
Universal Radio Adapter with Bluetooth
NCAGE CODE
L00N3
DOC. NO.
PART NO.
JA34-BT1
JA34-BT1 Mechanical Installation Rev C.SLDDRW
SHEET
1/1
JA34-BT1 Universal Radio Adapter with Bluetooth®
Installation and Operating Manual

Appendix B - Installation Documents

Rev D Page B1
JA34-BT1 Universal Radio Adapter with Bluetooth
®
Installation and Operating Manual

B1 Airworthiness Approval

Airworthiness approval of the JA34-BT1 may require completion of a TCCA Major Modification Report per CAR STD (AWM) 571 Appendix L, or a FAA Form 337. The sample wording for a description of the work is provided to assist the Installing Agency in preparing Instructions for Continued Airworthiness (ICA) when replacing an existing radio adapter with a Jupiter Avionics JA34-BT1 Universal Radio Adapter with Bluetooth. This sample may be modified appropriately for new installations. It is the installer’s responsibility to determine the applicability of the method used. Installations performed outside the USA and Canada must follow the applicable aviation authority’s regulations.
Sample Wording:
Removed the existing [model] radio adapter and replaced with a Jupiter Avionics JA34-BT1 Universal Radio Adapter with Bluetooth in [aircraft location].
Installed in accordance with the JA34-BT1 Installation & Operating Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JA34-BT1 interfaces with existing aircraft radios per the Installation & Operating Manual instructions.
The JA34-BT1 Installation & Operating Manual provides detailed installation instructions and wiring diagrams (Section 2, and Appendices A and B).
Power is supplied to the JA34-BT1 through a 1.0-Amp circuit breaker.
Aircraft equipment list, weights and balance amended. Compass compensation checked and found to conform to applicable regulations.

B2 Instructions for Continued Airworthiness

Maintenance of the JA34-BT1 Universal Radio Adapter with Bluetooth is “on condition” only. Refer to the JA34-BT1 Maintenance Manual. Periodic maintenance of the JA34-BT1 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the Jupiter Avionics JA34-BT1 unit installation as part of a Type Certificate (TC) or Supplemental Type Certificate (STC) project to comply with CAR STD (AWM) 523/527/525/529.1529 or FAR 23/25/27/29.1529 “Instructions for Continued Airworthiness”.
Items that may vary by aircraft make and model are shown in brackets (“[ ]”) and should be filled in as appropriate. Some of the checklist items do not apply, in which case they should be marked “N/A” (Not Applicable).
Instructions for Continued Airworthiness, Jupit er Avionics JA34-BT1 Universal Radio Adapter in an [Aircraft Make and Model]
1. Introduction
[Aircraft that has been altered: Registration number, Make, Model and Serial Number]
Content, Scope, Purpose and Arrangement: This document identifies the Instructions for Continued
Airworthiness for a Jupiter Avionics JA34-BT1 installed in an [aircraft make and model].
Applicability: Applies to a Jupiter Avionics JA34-BT1 installed in an [aircraft make and model]. Definitions/Abbreviations: None, N/A. Precautions: None, N/A. Units of Measurement: None, N/A. Referenced Publication s: JA34-BT1 Installation & Operating Manual
JA34-BT1 Maintenance Manual STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution: This document should be a permanent aircraft record.
2. Description of the System/Alteration
Jupiter Avionics JA34-BT1 Universal Radio Adapter with Bluetooth interfaces to external transceivers and [include other equipment/systems as appropriate]. Refer to Appendix A of this manual for interconnect information. Refer to aircraft manufacturer approved interconnect for actual installation.
Rev D Page B2
JA34-BT1 Universal Radio Adapter with Bluetooth
®
Installation and Operating Manual
3. Control, Operation Information
Refer to section 3 of this manual.
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JA34-BT1 is ‘on condition’ only. Periodic maintenance is not required. Refer to the JA34-BT1 Maintenance Manual.
6. Troubleshooting Information
Refer to the JA34-BT1 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JA34-BT1 Installation & Operating Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted.
8. Diagrams
Refer to Appendix A of this manual - the JA34-BT1 Installation & Operating Manual - for installation drawings and interconnect examples.
9. Special Inspection Requirements
N/A
10. Application of Protective Treatments
N/A
11. Data: Relative to Structural Fasteners
JA34-BT1 and appropriate mounting hardware installation, removal and replacement should be in accordance with applicable provisions of AC 43.13-1B and AC 43.13-2A.
12. Special Tools
N/A
13. This Section is for Commuter Category Aircraft Only
A. Electrical loads: Refer to Section 1 of the JA34-BT1 Installation and Operating Manual. B. Methods of balancing flight controls: N/A. C. Identification of primary and secon d ary structures: N/A. D. Special repair methods applicable to th e airplane: N/A.
14. Overhaul Period
No additional overhaul time limitations.
15. Airworthiness Limitation Section
N/A
Rev D Page B3
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