JA34-001
Universal Radio Adapter
Installation and Operating Manual
Rev. A
Jupiter Avionics Corporation
1959 Kirschner Road
Kelowna BC
Canada V1Y 4N7
Tel: 778-478-2232
Toll-Free: 855-478-2232
www.jupiteravionics.com
RECORD OF REVISIONS
Revision
Rev Date
Description
ECR
A
Nov 2014
Initial release, Serial number 1001 and higher.
2628
Prepared:
Checked:
Approved:
IMPORTANT:
JA34-001 Audio Controller
Installation 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
MPB
Rev A Page ii
JAC
11-06-14
SRM
INVALID!
JAC
11-07-14
KDV
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JA34-001 Audio Controller
Installation 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 Sp ec ifications ............................................................................................................................ 2
1.4.2 Mechanical Specifications ........................................................................................................................ 3
1.4.3 Flammability of Materials .......................................................................................................................... 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 Cabling and Wiring ....................................................................................................................................... 4
2.4.2 Mechanical Installation ................................................................................................................................. 5
2.4.3 Post Installation Checks ............................................................................................................................... 5
2.5 System Operation ............................................................................................................................................. 5
2.5.1 Configuration Operation ............................................................................................................................ 5
2.5.2 Receive Operation .................................................................................................................................... 5
2.5.3 Sidetone Operation ................................................................................................................................... 5
2.5.4 Relay Operation ........................................................................................................................................ 6
2.5.5 Microphone Operation .............................................................................................................................. 6
2.6 Adjustments and Configuration using ProCS™ ............................................................................................... 6
2.6.1 ProCS™ Setup ......................................................................................................................................... 6
2.6.2 Configurable Settings ............................................................................................................................... 6
2.6.3 JA34-001 Settings .................................................................................................................................... 6
2.6.4 Aircraft Audio Systems List ....................................................................................................................... 8
2.6.5 Non-Aircraft Radios List ............................................................................................................................ 8
2.6.6 Other Configuration Features ................................................................................................................... 8
2.7 Installation Kit ................................................................................................................................................... 8
2.7.1 Recommended Crimp tools ...................................................................................................................... 8
2.8 Installation Drawings ......................................................................................................................................... 8
SECTION 3 – OPERATION ............................................................................................................................................. 9
3.1 Introduction ....................................................................................................................................................... 9
3.2 Operation .......................................................................................................................................................... 9
Appendix A - Installation Drawings ........................................................................................................................... A1
A1 Introduction ..................................................................................................................................................... A1
A2 Installation Drawings ....................................................................................................................................... A1
Appendix B - Installation Documents ........................................................................................................................ B1
B1 Airworthiness .................................................................................................................................................. B2
B2 Instructions for Continued Airworthiness ........................................................................................................ B2
Rev A Page iii
JA34-001 Universal Radio Adapter
Name
Qty
Type
CONFIG DATA TO JA34
1
Data signal
MODE SELECT TO JA34
1
RECEIVE INPUT
1
Audio signal
MIC INPUT
1
Audio signal
+28 VDC POWER
1
Electrical power input
POWER GROUND
1
Power supply
RELAY KEY INPUT
1
Name
Qty
Type
CONFIG DATA FROM JA34-001
1
Data signal
RECEIVE OUT
1
Audio signal
MIC OUTPUT
1
Audio signal
RELAY CONTACTS
6
Audio signal
SECTION 1 - DESCRIPTION
1.1 System Overview
The JA34-001 Universal Radio Adapter allows the aircraft audio management system access to a non-aviation radio.
The JA34-001 provides fully isolated audio signal paths to and from the radio to allow a noise-free installation.
Microphone biasing and artificial sidetone generation are selectable for radios without them.
The JA34-001 is setup on a 'per installation' basis using cable CAB-USB-0002 and the JA99-001 Configuration Cable,
or cable CAB-USB-0006, and downloading the system configuration settings from a PC into non-volatile control
devices.
1.2 Features Overvi e w
The JA34-001 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 is beside the main connector and one is on the
back of the unit.
All audio outputs are balanced.
The JA34-001 provides relay contact keying, artificial sidetone generation and microphone voltage biasing.
1.3 Inputs and Outputs
Refer to the JA34-001 connector map for the mating connector designators and contact assignments for the
input and output signals.
1.3.1 Inputs
'LVFUHWHsignal
'LVFUHWH6LJQDO
1.3.2 Outputs
Rev A Page 1
1.4 Specifications
1.4.1 Electrical Specifications
Power Input
Nominal voltage 28 Vdc
Maximum voltage 30.3 Vdc
Minimum voltage 22.0 Vdc
Emergency voltage 18.0 Vdc
Input current 0.5 A max
1.4.1.1 Audio Performance
Rated Input Level
Receive audio rated input leve l 7.75 Vrms ± 10%
Microphone input le vel 250 mVrms ± 10%
Rated Output Power
JA34-001 Universal Radio Adapter
Installation Manual
Rated output power 7.75 Vrms ± 10%
Microphone rated output (150 Ohm mode) 250 mVrms ± 10%
Microphone rated output (8 Ohm mode) 50 mVrms ± 10%
Audio Frequency Response
Receive output audio frequency response ≤ 3dB from 300 to 6000 Hz
Microphone audio output audio frequency response ≤ 3dB from 300 to 6000 Hz
Distortion Characteristics
Audio output distortion at rated power ≤ 10%
Input Impedance
Microphone input impedance 150 Ω ± 10%
Receive Audio input impedance 600 Ω ± 10%
Output Load
Receive load 600 Ω ± 10%
Microphone load (150 Ohm mode) 150 Ω ± 10%
Microphone load (8 Ohm mode) 8 Ω ± 20%
Input to Input Crosstalk Level
Input to Input crosstalk ≤ 60 dB
Audio Noise Level without Signal
Noise level below the rated output ≥ 60 dB
1.4.1.2 Audio Performance, Other
MIC input designed for MIC type amplified dynamic/electret
MIC input bias voltage 12 Vdc ±10%
MIC input circuitry type differential
RECEIVE AUDIO input circ uitry type Transformer Coupled
RECEIVE output circuitry type Transformer Coupled
MIC output circuitry type Transformer Coupled
Rev A Page 2
JA34-001 Universal Radio Adapter
1.4.1.3 Discrete Signals
RELAY KEY INPUT, active signal level ≤ +3 Vdc
RELAY KEY INPUT, inactive signal level ≥ +10 Vdc
Relay contacts shall pass ≤ 1
1.4.2 Mechanical Specifications
Height 1.27 in [32.3 mm] maximum
Depth 2.61 in [66.3 mm] maximum
Width 4.52 in [114.8 mm] maximum
Installation Manual
ADC @ ≤ 30V, Resistive Load
Weight 0.38 lb
erial brushed aluminum with conversion
Mat
[0.17 kg] maximum
coating
Connectors (3): J2, J3 Two 4 pole 3.5mm jack
J1 One 25-pin D-Sub male V5 locking
Mounting 4 x 10-32 fasteners
Bonding ≤ 2.5 mΩ
Installation kit part number INST-JA34
1.4.3 Flammability of Materials
The JA34-001 complies with the requirements of RTCA/DO-160G Sec 26.3.3 "Flammability", through equivalent
flammability testing of materials and the Small Parts Exemption.
Rev A Page 3
JA34-001 Universal Radio Adapter
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 JA34-001 is on condition onl y. Schedu led ins p ectio n and/or p er iodic 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 Certificate of Conformance is included. Complete the on-line warranty card from the Jupiter Avionics
Corporation (JAC) website – www.jupiteravionics.com.
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 u n it may be damaged if the installation does not conform
to the wiring instructions in this manual.
2.4.1 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.
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.
Rev A Page 4
JA34-001 Universal Radio Adapter
Installation Manual
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.
2.4.2 Mechanical Installati on
The JA34-001 can be m ounted in any attitude and location with adequate space and sufficient clearance for the
connector and wiring har ne s s. It requires no direct cooling.
2.4.3 Post Installation Checks
2.4.3.1 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 (less than 0.5 Ω).
c) Check P1 pin 15 (Chassis Ground) for continuity to ground (less than 0.5 Ω).
d) Check P1 pins 8, 20, 21 and 23 (Output Ground) for continuity to ground (less than 0.5 Ω).
e) Check all pins for shorts to ground or adjacent pins.
2.4.3.2 Configuration
Ensure that the JA34-001 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.
2.4.3.3 Power on Checks.
Power up the aircraft’s systems and confirm normal operation of all functions of the JA34-001 (see section 2.4.5).
a) Begin with only the pilot’s headset attached. Confirm radio operation for both receive and transmit. Check the
radio selection and inputs. Do not proceed until the radios are 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.
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 JA34-001 is a remote mount unit and has no user accessible controls.
2.5.1 Configuration Operation
The JA34-001 accepts commands on the Configuration connector via the configuration cable (JA99-001) and the
configuration tool (ProCs™). (See section 2.6 Adjustments and Configuration)
2.5.2 Receive Operation
The RECEIVE INPUT is level controlled and summed with the MIC INPUT (Sidetone) and routed to the RECEIVE
OUTPUT.
2.5.3 Sidetone Operation
The MIC INPUT audio is level controlled and summed with the Receive Audio and routed to the RECEIVE OUTPUT.
Rev A Page 5
JA34-001 Universal Radio Adapter
Installation Manual
2.5.4 Relay Operation
The RELAY KEY INPUT selects the connection of both of the relay common contacts to either their normally closed
contact or their normally open contact.
2.5.5 Microphone Operation
The MIC INPUT audio is level controlled and routed to the MIC OUTPUT.
2.6 Adjustments and Configuration using ProCS™
The JA34-001 has no internal mechanical adjustments. Configuration data is sent to the JA34-001 via the
programming port input, using the ProCS™ configuration tool and configuration cables (JA99-001 and CAB-USB0002, or CAB-USB-0006).
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.
2.6.1 ProCS™ Setup
The JA34-001 menu items 'ProCS Setup' provide Setup drawings showing the cabling arrangement for
connecting the JA34-001 to a computer to allow configuration using ProCS™.
2.6.2 Configurable Settings
A standard unit is shipped from the factory with all internal adjustments configured to the default levels shown in bold
on the JA34-001 Settings page. At installation, it may be desirable to change some of these settings to suit the local
operating environment.
The Aircraft Audio Selection and Non-Aircraft Radio Selection choices are made from drop-down boxes as shown. For
further information, refer to sections 2.6.3.1 and 2.6.3.3. All input, output, MIC bias information etc. is automatically
added to suit the selected radios.
The required radios can be selected
from the dropdown boxes at the top of
the 'Aircraft Audio System' and 'Non-
Aircraft Radio' sections.
New radios may be added (see
sections 2.6.4 and 2.6.5 below).
2.6.3 JA34-001 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.
Rev A Page 6
JA34-001 Universal Radio Adapter
Installation Manual
2.6.3.1 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 aut omati cally. O ther air craft Au dio sy stems can be added to the li st (see se ction 2.5.4).
2.6.3.2 JA34-001 Universal Rad io Ada pter Adjus tments (Blue block)
The blue block refers to the adjustments and settings for the JA34-001 Universal Radio Adapter.
Receive Input
The level of the RECEIVE INPUT can 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 -35 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 0.625 Vrms)
Mic Output Load Impedance
The MIC OUTPUT impedance may be set to 8 Ohms or 150 Ohms. (Default 150 Ohms)
2.6.3.3 Non-Aircraft Radio Selection (Orange bloc k)
The appropriate Non-Aircraft Radio is selected from a drop-down list at the top of the block, and al l relevan t configur atio n
information is added aut omati cally. O ther Non -Ai rcra ft Radi os can be ad ded t o the l i st (s e e sectio n 2 .6.5).
Rev A Page 7
Connector Type
Hand crimp tool
Positioner
Insertion/extraction tool
Positronic
9507
9502-3
M81969/1-04
Positronic
AFM8 (Daniels)
M22520/2.08 KB-1
JA34-001 Universal Radio Adapter
Installation Manual
2.6.4 Aircraft Audio Systems List
This is a list of Aircraft Audio Systems, and shows the configuration information that will be added to the JA34-001
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.
2.6.5 Non-Aircraft Radios List
This is a list of Non-Aircraft Radios and the configuration information that will be added to the JA34-001 Settings
page. The list is similar to the Aircraft Audio Systems list, and new radios can be added in the same way.
2.6.6 Other Configuration Features
In the JA34-001 Product Information Window, the model number, serial number and check sum of the JA34-001
Universal Radio Adapter 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 TAG ring CON-5500-0375
1 D-Sub 25-pin connector, hood and 25 crimp pins CON-3420-0025
1 Heat Shrink Tubing WIR-HTSK-0750
2.7.1 Recommended Crimp tool s
2.8 Installation Drawings
The drawings and documents required for Installation can be found in Appendix A of this manual.
Rev A Page 8
JA34-001 Universal Radio Adapter
SECTION 3 – OPERATION
3.1 Introduction
The JA34-B001 Universal Radio Adapter allows the aircraft audio management system access to a non-aviation
radio.
3.2 Operation
The JA34-001 is a remote mount unit and has no user accessible controls.
Rev A Page 9
JA34-001 Universal Radio Adapter
Installation Manual
Appendix A - Installation Drawings
A1 Introduction
The drawings necessary for installation and troubleshooting of the JA34-001 Universal Radio Adapter are in this
Appendix, as listed below.
A2 Installation Drawings
DOCUMENT Rev
JA34-001 Connector Map A
JA34-001 Interconnect A
JA34-001 Mechanical Installation C
Rev A Page A1
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JA34-001 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
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JA34-001 1/3
JA34-001 Interconnect Rev A.dwg
TAT
JA34-001 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 JA34-001 connector pins should be terminated to airframe ground using a tag ring
P/N: MS27741-3 or equivalent.
2
1.
3
4
5
6
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MIC INPUT HI
MIC INPUT LO
MIC AUDIO OUT
MIC AUDIO LO
AUDIO CONTROLLER
3
16
JA34-001 J1
P1
25 PIN FEMALE DMIN
MATING CONNECTOR
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JA34-001 Interconnect Rev A.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
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Universal Radio Adapter
J2 and J3 Interconnect
JA34-001 3/3
JA34-001 Interconnect Rev A.dwg
TAT
PART OF
CONFIGURATION CABLE
CAB-USB-0006
or JA99-001
JA34-001 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
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4.52in MAX
114.8mm MAX
2.42in MAX
61.5mm MAX
1.80in
45.7mm
2.40in
61mm
4.00in
101.6mm
3.52in MAX
89.4mm MAX
0.45in
11.4mm
66.3mm MAX
2.61in MAX
29.2mm
1.15in
0.21 5.4 THRU ALL
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
CHECKED
APPROVED
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TO JUPITER AVIONICS CORP.
DRAWING NOT TO SCALE
CENTER OF GRAVITY
0.03in [0.8mm]
WEIGHT: 0.38 lbs [0.17 kg] MAX.
TITLE
Universal Radio Adapter
NCAGE CODE
L00N3
DOC. NO.
PART NO.
JA34-001
JA34-001 Mechanical Installation Rev C.SLDDRW
SHEET
1/1
JA34-001 Universal Radio Adapter
Installation Manual
Appendix B - Installation Documents
Rev A Page B1
JA34-001 Universal Radio Adapter
Installation Manual
B1 Airworthiness
Airworthiness approval of the JA34-001 requires completion of a TCCA Major Modificat ion Rep or t per CAR ST D
(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 JA34-001 Universal Radio Adapter. This sample may be modified
appropriately for ne w insta llatio ns .
Sample Wording:
Removed the existing [model] radio adapter and replaced with a Jupiter Avion ics JA34-001 Universal Radio
Adapter in [aircraft location].
Installed in accordance with the JA34-001 Installation Manual, Revis ion [ ], and AC 43.13-2, Chapters 2, and 3.
The JA34-001 interfaces with existing aircraft radios per the Installation Manual instructions.
The JA34-001 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JA34-001 through a 1-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 JA34-001 Universal Radio Ad apter is “on condition” only. Refer to the JA34-001 Maintenance
Manual. Periodic maintenance of the JA34-001 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA34-001 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, Jupiter Avionics JA34-001
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 JA34-001 installed in an [aircraft make and model].
Applicability: Applies to a Jupiter Avionics JA34-001 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: JA34-001 Installation Manual
Distribution: This document should be a permanent aircraft record.
Rev A Page B2
JA34-001 Maintenance Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
JA34-001 Universal Radio Adapter
Installation Manual
2. Description of the System/Alteration
Jupiter Avionics JA34-001 Universal Radio Adapter with interface 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.
3. Control, Operation Information
N/A
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JA34-001 is ‘on condition’ only. Periodic maintenance is not required. Refer to the
JA34-001 Maintenanc e Ma nua l.
6. Troubleshooting Information
Refer to the JA34-001 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JA34-001 Installation 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 JA34-001 Installation 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
JA34-001 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 JA34-001 Installation 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 A Page B3
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