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:
1.1 System Overview .................................................................................................................................................... 1
1.2 Features Overview .................................................................................................................................................. 1
1.3 Inputs and Outputs .................................................................................................................................................. 2
1.4.4Flammability of Materials ................................................................................................................................ 5
2.2 Continued Airworthiness ......................................................................................................................................... 6
2.3 Unpacking and Inspecting Equipment..................................................................................................................... 6
2.4.6 Post Installation Checks .................................................................................................................................. 7
2.5 Adjustments and Configuration using ProCS™ ...................................................................................................... 8
2.5.4 Other Configuration Features ........................................................................................................................ 14
(3)AUX and PA Receive Select Switches and Legends .................................................................................... 17
(4)VOX Threshold Control ................................................................................................................................. 17
(7) (10) RX/ICS Volume control and legend .............................................................................................................. 19
3.3.7 Direct Audio Operation .................................................................................................................................. 21
3.3.8 Music Operation ............................................................................................................................................ 21
3.3.9 Rear Hand Mic Operation ............................................................................................................................. 21
3.4.1 Left User Emergency Mode .......................................................................................................................... 22
3.4.2 Right User Emergency Mode ........................................................................................................................ 22
3.4.3 Auto Emergency Mode .................................................................................................................................. 22
B2 Instructions for Continued Airworthiness .............................................................................................................. B2
The JA94-N44A dual audio controller is a centralized management system for two independent users that distributes
and controls all transceiver, receiver and warning source audio in an aircraft. It enables the selected transmission of
microphone audio to one or more transceivers and distributes all intercom audio. The JA94-N44A dual audio
controller can be used in a standalone configuration or a star configuration to prevent the loss of the entire system
due to the failure of one controller. It provides a passive emergency mode that directs the Right User to the COM1
transceiver and NAV1 receiver, and the Left User to COM2 transceiver and NAV2 receiver.
The JA94-N44A is set up on a per-installation basis using a configuration cable and a PC running the product
configuration tool to download system configuration settings via the front panel music / configuration connector. To
facilitate future customizations and certification, neither software nor complex electronic devices are used in the JA94N44A design.
1.2 Features Overview
The JA94-N44A may be configured as a drop-in replacement for the Cobham/NAT AA92, AMS42 & AMS44.
The JA94-N44A supports up to 6 transceivers, each selectable from two rotary switches.
The JA94-N44A supports up to 4 selectable receivers in two banks of 4 switches.
The JA94-N44A provides intercom functions for up to 2 users and up to 6 passengers.
The JA94-N44A has individual VOX gating for each user and passenger.
The JA94-N44A supports two Direct Audio inputs at a fixed level to two users in Normal and Emergency mode.
The Direct audios may be routed to both Left and Right User phones or Direct Audio 2 routed to Right User and Direct
Audio 1 to Left User.
The JA94-N44A supports a third Direct Audio input in Normal mode only.
The JA94-N44A allows the receive audios to be disconnected from the Passenger Phones.
The JA94-N44A supports two CVR outputs.
The JA94-N44A allows transmit access for five crew members (Right User, Left User, Passenger 1, Passenger 2, and
Passenger 6).The JA94-N44A allows ICS PTT access for all users and passengers.
The JA94-N44A features a Music / Configuration connector on the faceplate for configuration of audio levels and
routing. The port can also be used as a music input and is compatible with most music players.
The JA94-N44A has three modes of operation: Normal Mode, Emergency Mode and ICS Isolate Mode.
The JA94-N44A supports radio simulcast.
The JA94-N44A supports a remote transmit select input.
The JA94-N44A supports selection of Normal Mode and Emergency Mode from a front panel control and selection of
ICS Isolate Mode from an external switch.
Primary nominal voltage 28 Vdc
Maximum voltage 32.2 Vdc
Minimum voltage 22.0 Vdc
Emergency voltage 18.0 Vdc
Power Off Voltage ≤ 15.0 Vdc
Input current 0.95 A max
1.4.1.1 Audio Performance
Rated Input Level
Receive audio rated input level 7.75 Vrms ± 10%
Direct audio rated input level 7.75 Vrms ± 10%
Music rated input level 400 mVrms ± 10%
Microphone input level 250 mVrms ± 10%
Intercom Tie Line type 1 input level 340 mVrms ± 10%
Intercom Tie Line type 2 input level 1.20 Vrms ± 10%
Installation and Operating Manual
Rated Output Level
Phone rated output 8.7 Vrms ± 10%
Left or Right User Phone rated output in emergency mode 3.00 Vrms ± 20%
Phone rated output level, with MUSIC input 4.35 Vrms ± 10%
COM MIC rated output 250 mVrms ± 10%
CVR rated output 500 mVrms ± 10%
CVR rated output with MUSIC INPUT 250 mVrms ± 10%
CVR rated output with MIC INPUT 1.00 Vrms ± 10%
CVR rated output, in emergency mode, 500 mVrms ± 10%
Receive Composite rated output 2.50 Vrms ± 10%
Intercom Tie Line type 1 rated output 340 mVrms ± 10%
Intercom Tie Line type 2 rated output 1.20 Vrms ± 10%
Audio Frequency Response
Audio output audio frequency response ≤ 3 dB from 300 to 6000 Hz
Receive Composite Audio load 600 Ω ± 10%
Intercom Tie Line type 1 rated load 2000 Ω ± 10%
Intercom Tie Line type 2 rated load 2000 Ω ± 10%
Intercom Tie Line type 1 maximum load 666 Ω max (3 loads)
Intercom Tie Line type 2 maximum load 285 Ω max (7 loads)
Volume Controls
Receive Audio control variation 32 ± 3 dB min
ICS Audio control variation 42 ± 3 dB min
Crosstalk Level
Input to Output crosstalk ≤ 55 dB
Input to Input crosstalk ≤ 60 dB
Station to Station crosstalk ≤ 65 dB
Audio Noise Level without Signal
Noise level below the rated output ≥60 dB
1.4.1.2 Audio Performance, Other
Installation and Operating Manual
CVR HI / LO output circuitry type (Normal) differential
CVR HI / LO output circuitry type (Emergency) single ended
Microphone inputs designed for MIC type amplified dynamic/electret
Microphone inputs bias voltage 12 Vdc ± 10%
Microphone inputs circuitry type single ended
MUSIC LEFT / RIGHT HI / LO audio input circuitry type differential
FRONT MUSIC LEFT / RIGHT audio input circuitry type: single ended
MUSIC attenuation 38 dB max
RECEIVE AUDIO input circuitry type differential
PHN HI / LO output circuitry type single ended
MIC output circuitry type differential
RX Composite Audio output circuitry type differential
ICS TIE HI / LO Circuitry Type differential
PHN HI / LO output music fade in duration 2.5 ± 1.0 seconds
VOX Threshold level range relative to rated MIC input -28 to +6 dB
VOX off Delay Time range 0.5 to 2.0 seconds
Transmit Timeout Timer 90 ± 10 seconds
1.4.1.2 Lights Input
LIGHTS INPUT ranges 0 to 28, 0 to 14 and 0 to 5 Vdc
LIGHTS INPUT current 10 mA max.
The JA94-001A Dual Audio Controller has been qualified to the environmental conditions listed below. Environmental
categories for which TSO compliance has been demonstrated are listed in the Environmental Qualification Form in
Appendix B of this manual.
Temperature:
Operating
Ground Survival
Altitude
Humidity
Shock, Crash Safety
J1 One 37-pin D-Sub male, V5 locking
J2 One 50-pin D-Sub male, V5 locking
J3 One 15-pin D-Sub male, V5 locking
J4 One 4 pole 3.5mm stereo jack
J5 One 4-40, 0.5 in. max
1.875 in [47.63 mm] max
5.48 in [139.2 mm] max
5.75 in [146.1 mm] max
5.00 in [127 mm] max
1.99 lbs. [0.91 kg] max
brushed aluminum with conversion
coating
4 Dzus fasteners
≤ 2.5 mΩ
INST-JA94
-45 °C to +70 °C
-55 °C to +85 °C
50,000 ft
Cat A (48 hours)
6 g, 20 g for 11 ms
1.4.4 Flammability of Materials
The JA94-N44A complies with the requirements of RTCA/DO-160G Sec 26.3.3 "Flammability", through equivalent
flammability testing of materials and the Small Parts Exemption.
This section contains unpacking and inspection procedures, installation information, and post-installation checks.
2.2 Continued Airworthiness
Maintenance of the JA94-N44A 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
All products manufactured by JAC are 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 conditions and tests for CAN TSO approval of the JA94-N44A are minimum performance standards. Those
installing the JA94-N44A, on or in a specific type or class of aircraft, must determine that the aircraft installation
conditions are within TSO standards. The JA94-N44A 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.
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.
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 JA94-N44A can be mounted in any attitude and location with adequate space for the front panel and sufficient
clearance for the connector and wiring harness. It requires no direct cooling.
Note: During bench test set up, it is normal for the JA94-N44A chassis to become warm to the touch.
2.4.4 In-Line PTT Cordsets
If in-line PTT cordsets (drop cords) are used, be aware that incorrectly configured or improperly shielded in-line PTT
cordsets can lead to significant audio problems.
2.4.5 Legend Replacement
The JA94-N44A illuminated legends are field replaceable. For further information, refer to the ‘Legend Replacement’
document in Appendix A of this manual.
2.4.6 Post Installation Checks
2.4.6.1 Voltage/Resistance checks.
Do not attach this unit until the following conditions are met:
a) Check P1 pin 19 for lights buss voltage +28 Vdc +14 Vdc or +5 Vdc.
b) Check P2 pin 17 for +28 Vdc power relative to ground.
c) Check P2 pin 34 for continuity to ground (less than 0.5 Ω).
d) Check P2 pins 6 thru 10 for continuity to ground (less than 0.5 Ω) when the relevant switch is closed.
e) Check P3 all pins for continuity to ground (less than 0.5 Ω) when the relevant switch is closed or selection
made.
f)Check all pins for shorts to ground or adjacent pins.
2.4.6.2 Configuration
Ensure that the JA94-N44A contains the correct configuration settings. This may be done at the factory, on the
maintenance bench or in the aircraft before or during the power on checks. Refer to section 2.5.1.
2.4.6.3 Power on Checks.
Power up the aircraft’s systems and confirm normal operation of all functions of the JA94-N44A. Refer to
Section 3 (Operation) for specific operational details.
a) Begin with only the Right user headset attached. Confirm correct ICS and radio operation for both receive and
transmit. Check yoke or cyclic switch action. Check the radio selection and inputs. Do not proceed until the
radios are functioning correctly.
b) If there is a music source in the system, turn it on and check for proper mute operation.
c) 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.
d) Check the ICS operation and Emergency operation.
e) Plug in the Left user headset. Check for correct ICS operation. Check yoke or cyclic switch functions.
f) Plug in any remaining headsets, and check for correct ICS operation. Note that an incorrect cordset (drop cord)
or improper jack wiring may cause a wide range of problems, from loss of audio to a tone heard in the headset.
g) 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 Adjustments and Configuration using ProCS™
All the JA94-N44A internal adjustments are set from the Product Configuration Software ProCS™. Configuration data
is sent to the JA94-N44A 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.
2.5.1 Configuration Cabling Requirements
To configure the JA94-N44A, 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 JA94-N44A 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
2.5.2 ProCS™ Setup
The ProCS™ JA94-N44A menu item 'ProCS Setup' provides Setup drawings showing the cabling
arrangement for connecting the JA94-N44A to a computer running the ProCS™.
2.5.3 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.
The receive and direct audio input level of each of the eight RX and the three
DIRECT AUDIO inputs can be adjusted from 1 to 10 Vrms. (Default 7.75 Vrms)
Rev A Page 10
The Receive Audio Detector threshold can be adjusted from
-36 to -12 dB of rated input level. (Default -24 dB)
The level of the receive composite audio output (RX COMP OUT)
can be adjusted from 0.25 to 2.5 Vrms. (Default 1.00 Vrms)
Note: When Legacy Passenger ICS Mode is selected, the Passenger Mics are controlled by the VOX control
until the fully cw (PTT) position is reached. Then the Passenger Mics are automatically set to the minimum
VOX level and should be controlled by in-line PTT drop-cords.
2.5.3.8 Connector Pin Configuration
Several of the connector pins can be configured to meet the requirements of specific installations. Refer to JA94N44A Interconnect sheet 5 of 6. Direct Audio routing can also be selected in this section.
he rated input and output levels of the intercom tie line can be selected as Type 1 or Type 2 (Default Type 2).
The quantity of external loads for a Type 1 intercom tie line can be selected from 0 to 3 (Default 0).
The quantity of external loads for a Type 2 intercom tie line can be selected from 0 to 7 (Default 0).
2.5.3.13 Lighting Voltage Selection
2.5.3.14 VOX
2.5.3.15 Connector Maps
The rated input level for the lighting
voltage may be selected from
+5 Vdc, +14 Vdc or +28Vdc
(Default +28 Vdc).
from 0.50 to 2.00 sec (Default 1 sec).
This section contains connector maps and interconnects that are automatically generated to show changes that affect
the installation of the JA94-N44A, such as switch labels and voltages. See section 2.7.1.
2.5.4 Other Configuration Features
In the JA94-N44A Product Information Window, the model number, serial number and check sum of the JA94-N44A
Dual Audio Controller can be viewed.
The drawings and documents required for Installation can be found in Appendix A of this manual.
2.7.1 Generation of Custom Drawings
The interconnects and connector maps in Appendix A of this manual are generic drawings based on the standard
version of the JA94-N44A. However, if a unit has been configured using JAC’s ProCS™ software to change switch
legends or lighting voltages, the software can be used to generate fully customized interconnects and connector
maps for use by the installer.
(1) (2)NAV1 - FM2 Receive Select Switches and Legends
Each User has four white two-position centre-off toggle
switches for the NAV1/COM1 to DME/FM2
receivers/transceivers. When a left or right switch is set
to the 'up' position, audio from the receiver associated
with the legend above the switch is routed to the phones
of that side's user (and passengers if configured.) In the
'down' position, audio from the transceiver associated
with the legend below the switch is routed to the phones
of that side's user (and passengers if configured.)
The backlit legends are interchangeable to allow
customization. The default legends are NAV1, NAV2,
ADF and DME above the switches, and COM1, COM2,
FM1 and FM2 below the switches.
(3)AUX and PA Receive Select Switches and Legends
The AUX/PA switches are two white two-position centre-off
toggle switches. The left-hand switch is associated with the Left
User, and the right-hand switch is for the Right User.
Installation and Operating Manual
To select AUX, the appropriate switch is set to the 'up' position,
and for PA it is in the 'down' position. Audio from the associated
receiver is routed to the phones of that side’s user (and
passengers if configured).
The backlit legends are interchangeable to allow customization.
The default legends are AUX above the switches and PA below
the switches.
(4)VOX Threshold Control
The VOX Threshold Control is an unlit rotary knob in the
centre top of the panel that is used to set the VOX
threshold level of the unit for all users and passengers.
When rotated fully clockwise (cw), the threshold will be
at maximum, VOX ICS operation is disabled and ICS
PTT input is required for ICS operation.
When rotated fully counterclockwise (ccw), the threshold
will be at minimum (almost live).
To adjust the unit for VOX (Voice activated) use, the
VOX control should be set fully ccw and then slowly
rotated cw to the point where no intercom audio can be
heard. The VOX control may require adjustment for
proper operation as ambient noise changes.
eft User Controls (11) TX Annunciators (12)Right User Controls
The Right User TX selector is an unlit rotary seven-position knob that is used to select transmission for one of the six
transceivers, or the RMT (remote) position. Below the knob is a 'TX' deadfront annunciator (12) which will illuminate
during transmission. For Remote operation, refer to section 3.3.11.
Each of the transmit selector positions is linked by a white line to the corresponding
transceiver switch and legend, and each transceiver has a transmit select annunciator
pointing to the associated switch or legend. The appropriate annunciator will light green to
show which transceiver is selected for transmit (right user PA in the example above).
T
he Left User TX selector is an unlit rotary
seven-position knob that operates in the
same manner as the Right User selector,
except that position 7, marked PULL TO
TURN (extreme ccw) is used to select
Emergency (EMER) mode.
Below the knob is a 'TX' deadfront
annunciator (11) which will illuminate during
transmission.
For full information on Emergency mode see
section 3.4.
Note: To prevent accidental selection of Emergency mode, the knob must be pulled towards the user before
it can be rotated to the EMER position.
(6)EMER legend
he backlit EMER (Emergency) legend is associated with the Left User TX control only. For full information on
These are two unlit dual rotary knobs that adjust
the receive(RX) volume ((the smaller, top knob
marked RX) and the ICS volume (the larger,
bottom knob).
Each user can adjust the volumes individually.
Rotating the knobs clockwise (cw) will increase the
volume, and counterclockwise (ccw) will reduce it
Individual radio volume controls should be set to a
nominal level, and then adjusted for changing
flight conditions using this control.
Legend
(9)Music/Configuration Connector cover (♫/io)
This cover is located between the Right User RX/ICS and TX
controls. It protects a music input port compatible with most
music players, and accepts a 3 pole 3.5mm stereo plug with a
slim diameter connector housing.
Installation and Operating Manual
Side View
(This connector is also used during installation to change
configuration settings.)
CAUTION:
device, or both.
Attempting to connect an incompatible plug or device could damage the
If in doubt, check with your installing agency.
unit
, the attached
3.3 Normal Operation Mode
The JA94-N44A is in Normal mode unless EMER mode has been selected via the Left User TX control, or if the
power input is off.
Note: Numbers in parentheses refer to the front panel controls shown in section 3.2.
3.3.1 Panel Lighting
The JA94-N01A NVIS Type I Class B compliant legends and annunciators will be illuminated (when appropriate) and
dim through the aircraft lighting buss.
3.3.2 Receiving
When the JA94-N44A receives an incoming transmission on a transceiver or receiver that has been selected, either
by the white transceiver receive switches (1) (2) or (3) or a transmit selector (5) or (8), the incoming audio will be
directed to the user’s phones.
The audio level of any incoming transmission will depend upon the level selected by the user's front panel RX volume
control – (7) or (10). It will be muted if the unit is transmitting and muting of receive audio during transmit is enabled.
ProCS™ can be configured to route no receive audio, Right User receive audio, or Left User receive audio to
passengers.
To select a transceiver, rotate the Transmit Select Switch (5) or (8) until it aligns with the line leading to the
Transceiver Select switch legend (1) (2) or (3) - default legends COM1, COM2, FM1, FM2, AUX or PA. The
corresponding Transmit Select annunciator will illuminate green.
When the user’s TX PTT is activated, the unit will transmit on the selected transceiver, and the deadfront Transmit
Annunciator will illuminate ‘TX’. All MIC and sidetone audio will be routed to the user’s phones, and any music (and
RX and/or ICS audio if selected by ProCS™) will be muted for the duration of the transmission.
Passengers 1, 2 and 6 (designated at installation) will transmit on the radio selected by either the Right User or Left
User, as configured by ProCS™.
3.3.3.1 Simulcast Operation
Note: It is important to be aware of the Simulcast configuration of the aircraft.
The ProCS™ configuration program allows the selection of Simulcast Mode. This can be for the left user or the right
user or both, and for each user the simulcast radio selections can be selected separately.
If simulcast has been enabled via ProCS™ and the user's Transmit Selector Switch is set to PA (simulcast position),
the user will transmit on multiple radios as configured by ProCS™.
3.3.3.2 Transmit Timeout Operation
Note: It is important to be aware of the Transmit Timeout configuration of the aircraft.
The ProCS™ configuration program allows the selection of Transmit Timeout. If selected, transmissions will timeout
after 90 seconds.
3.3.3.3 FM2 PTT Operation
Note: If the FM2 transceiver has been configured as duplex, it can be used with a cellphone or
sat-phone. Check your configuration with the installing agency.
If the unit has been configured for cellphone or sat-phone use and FM2 has been selected for transmit, momentarily
activating the TX PTT (either from the faceplate or by some other method) will keep FM2 transmitting. A second
momentary activation of the TX PTT, or moving the Transmit Selector away from FM2, will stop FM2 from
transmitting.
3.3.4 VOX Operation
A user’s MIC audio is routed to the ICS when the MIC audio level exceeds the VOX threshold (3).
A user’s MIC audio is disconnected from the ICS when the MIC audio level falls below the VOX threshold for 0.5 to 2
seconds.
3.3.5 ICS Operation
ICS audio is the sum of all the MIC audio from users with ICS KEY active or with MIC audio level exceeding the VOX
Threshold level.
The ICS audio also includes the audio input on the ICS TIE from other audio controllers.
The ICS audio is output on the phones of each user.
The ICS audio is muted during transmit as configured by ProCS™.
The ICS audio level at the phones is controlled by the ICS volume control (7) or (10).
Note: If Legacy Passenger ICS Mode has been selected, the Passenger Mics are controlled by the VOX
control until the fully cw (PTT) position is reached. Then the Passenger Mics are automatically set to the
minimum VOX level and should be controlled by in-line PTT drop-cords.
Note: It is important to be aware of the ICS Isolation configuration of the aircraft.
When the external control signal ICS ISOLATE is active: the LEFT or RIGHT User, as configured by ProCS™, are
isolated from the ICS signal of the passengers and the other User; when configured as both the LEFT and RIGHT
user, the LEFT and RIGHT Users will be connected to each other via an ICS but are isolated from the Passengers
ICS.
In Isolate Mode, the selected user's MIC audio input is disconnected from the ICS TIE output, the user's phones are
disconnected from the ICS TIE input circuit, and the music to the user’s PHN output will be muted.
3.3.7 Direct Audio Operation
DIRECT AUDIO 1 and, when configured by ProCS™, the DIRECT AUDIO 2 & 3, are routed to the LEFT USER
Phones.
DIRECT AUDIO 2 and, when configured by ProCS™, the DIRECT AUDIO 1 & 3 are routed to the RIGHT USER
Phones.
3.3.8 Music Operation
Music to the phones will be muted by incoming audio (ICS, Receive, or Direct Audio) or if the unit is transmitting.
When the incoming audio has ended, the music will gradually return to the previous level.
3.3.9 Rear Hand Mic Operation
When configured by ProCS™, the Rear Hand MIC audio and PTT signal are connected to the Transceiver as
selected by the left or right TX Select switch. The Rear Hand MIC is assigned to left or right user's controls by
ProCS™ in the Passenger and Rear Hand MIC settings.
3.3.10 Cockpit Voice Recorder (CVR) Operation
The RIGHT CVR output consists of the sum of the RIGHT USER MIC input (independent from VOX control setting)
and the RIGHT USER PHONE output, and the LEFT CVR output is the sum of the LEFT USER MIC input
(independent from VOX control setting) and the LEFT USER PHONE output.
3.3.11 Remote RMT Operation
A remote transmit selector may be linked to the JA94-N44A to allow remote selection for transmission via the right
user controls. (This remote selector could be on the right user's cyclic control.) When a remote transmit selector is
installed and the RIGHT USER TX SELECT switch is in the RMT position, then the RIGHT USER will transmit on the
radio or radios as selected by the remote transmit selector.
Note: It is important to be aware of the Remote Operation configuration of the aircraft.
The JA94-N44A operates in Emergency Mode automatically (Auto Emergency Mode) when the power to the unit is
off, or when the left Transmit Selector Switch is in the EMER position (Selected Emergency Mode).
3.4.1 Left User Emergency Mode
In emergency mode, the Left User phone and MIC signals are connected by mechanical relay contacts to the COM2
transceiver and the NAV2 receiver. Left User PTT is routed directly to COM2 PTT and the LEFT USER MIC is routed
to the COM 2 MIC. The Left User is disconnected from the ICS.
The sum of COM 2 RX, NAV 2 RX and Direct Audio 1 (and Direct Audio 2 if configured by ProCS™) is routed to the
LEFT USER PHN output. The LEFT USERPHN is routed to the LEFT CVR output.
3.4.2 Right User Emergency Mode
In emergency mode, the Right User phone and MIC signals are connected by mechanical relay contacts to the COM1
transceiver and the NAV1 receiver. Right User TX PTT is routed directly to COM1 PTT, and the RIGHT USER MIC is
routed to the COM 1 MIC. The Right User is disconnected from the ICS.
The sum of COM 1 RX, NAV 1 RX and Direct Audio 2 (and Direct Audio 1 if configured by ProCS™) is routed to the
RIGHT USER PHN output. The RIGHT USERPHN is routed to the RIGHT CVR output.
3.4.3 Auto Emergency Mode
The unit will enter emergency mode automatically if power to the unit is off.
Other than Emergency operation described above, no functions of the JA94-N44A will operate when power is lost.
Legends and annunciators will not be illuminated.
3.4.4 Selected Emergency Mode
If the JA94-N44A retains power, the unit can be placed into emergency mode by rotating the Left User TX control to
the EMER position (pull to turn).
Emergency mode conditions will apply (see above) but all other functions of the JA94-N44A will operate. The LEDs,
legends and annunciators will retain normal functionality
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
Dual Audio Controller - AMS44 Compatible - NVG
Interconnect Notes
JA94-N44A1/6
JA94-N44A Interconnect Rev A.dwg
TAT
JA94-N44A 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).
CONNECTION TO AIRFRAME GROUND SHOULD BE MADE WITH 20 AWG WIRE. LENGTH NOT TO
EXCEED 3 FT (0.91 M).
CABLE SHIELDS AT THE JA94-N44A CONNECTOR PINS SHOULD BE TERMINATED TO AIRFRAME
GROUND USING A TAG RING P/N: MS27741-5 OR EQUIVALENT.
CONNECTOR PIN HAS MORE THAN ONE FUNCTION. SEE THE OPTIONS SECTION OF THIS
DRAWING FOR ALTERNATE INTERCONNECT WIRING.
ONLY +28 VDC OR +14 VDC OR +5 VDC LIGHTS INPUT VOLTAGE MAY BE APPLIED AT ONE TIME.
THE FRONT PANEL MUSIC INPUT SHALL NOT BE CONNECTED TO ANY OTHER AUDIO INPUT.
Jupiter Avionics Corporation (JAC) products have field-replaceable illuminated
To facilitate legend removal, JAC provides a legend extractor tool - part #
To remove a legend, hold the extractor firmly between
Pull the legend away from the faceplate as shown in figure 3.
Figure 1
Figure 2
Legend
Extractor tool
recess
Legend Replacement
Field-Replaceable Legends
legends. This permits easy customization, and allows the same units to be used
in multiple different configurations with only minimal changes.
The internal circuitry ensures that, although the legends are individually
illuminated, the illumination is consistent and uniform throughout all legends, and
never needs to be balanced. This means that if it is a requirement to change the
labelling due to damage or for a different project, there is no need for costly and
time-consuming illumination checks.
Legend Removal
Caution: Take care not to scratch or otherwise damage the faceplate or the legend.
TOL-CUST-EXTR (figure 1) that fits into the recesses on the legend.
the forefinger and thumb, and use a tweezer-like action
to grip the legend (figure 2).
Figure 3
Legend Replacement
To replace a legend, align the text correctly, and then apply gentle pressure until the body of the legend support seats
firmly into the faceplate.
Once the new legend is in place, ensure that it has seated correctly by checking that it illuminates. The unit is now
ready for use.
Airworthiness approval of the JA94-N44A 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
audio panel with a Jupiter Avionics JA94-N44A Dual Audio Controller. 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 Canada must follow the applicable aviation authority’s regulations.
Sample Wording:
Removed the existing [model] audio panel and replaced with a Jupiter Avionics JA94-N44A Dual Audio Controller
in [aircraft location].
The JA94-N44A is approved to CAN-TSO-C139. The JA94-N44A meets RTCA DO-160G environmental
qualifications for this installation. See Section 1 of the JA94-N44A Installation Manual.
Installed in accordance with the JA94-N44A Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JA94-N44A interfaces with existing aircraft systems per the Installation Manual instructions.
The JA94-N44A Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).).
Power is supplied to the JA94-N44A through a 2 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 JA94-N44A Dual Audio Controller is “on condition” only. Refer to the JA94-N44A Maintenance
Manual. Periodic maintenance of the JA94-N44A is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA94-N44A 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 JA94-N44A Dual
Audio Controller 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 JA94-N44A installed in an [aircraft make and model].
Applicability: Applies to a Jupiter Avionics JA94-N44A installed in an [aircraft make and model].
Definitions/Abbreviations: None, N/A.
Precautions: None, N/A.
Units of Measurement: None, N/A.
Referenced Publications: JA94-N44A Installation and Operating Manual
Distribution: This document should be a permanent aircraft record.
Rev A Page B2
JA94-N44A Maintenance Manual
JA94-N44A Operating Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Jupiter Avionics JA94-N44A Dual Audio Controller 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
Refer to section 3 of this manual or to the Jupiter Avionics JA94-N44A Operating Manual.
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JA94-N44A is ‘on condition’ only. Periodic maintenance is not required. Refer to the
JA94-N44A Maintenance Manual.
6. Troubleshooting Information
Refer to the JA94-N44A Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JA94-N44A Installation and 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 JA94-N44A Installation and 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
JA94-N44A 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 JA94-N44A Installation and Operating Manual.
B. Methods of balancing flight controls: N/A.
C. Identification of primary and secondary structures: N/A.
D. Special repair methods applicable to the airplane: N/A.
Equipment tested to Category B
Equipment tested to Category B, (6 g for 11 ms)
Equipment tested to Category B, (20 g for 11 ms)
Equipment tested to Category B, (20 g for 3 sec)
Vibration
1
Fixed Wing - Sine
Fixed Wing - Random
Helicopter - Random, unknown
8.0
8.5.1
8.5.2
8.8.3
Equipment tested to Categories: [(SBM)(U2FF1)]
Equipment tested to Category SM
Equipment tested to Category SB
Equipment tested to Category U2FF1
Explosive Atmosphere
9.0
Equipment identified as Category X, no test performed
Waterproofness
10.0
Equipment identified as Category X, no test performed
Fluids Susceptibility
11.0
Equipment identified as Category X, no test performed
Sand and Dust
12.0
Equipment identified as Category X, no test performed
Fungus
13.0
Equipment identified as Category X, no test performed
Salt Fog Test
14.0
Equipment identified as Category X, no test performed
Magnetic Effect
15.0
Equipment tested to Category Z (≤ 0.3 m)
Power Input
DC Equipment
DC Current Ripple
DC Inrush
16.0
Equipment tested to Category: Z(XX)
Equipment tested to Category Z (+28 Vdc equipment),
X, no test to be performed
X, no test to be performed
Voltage Spike
17.0
Equipment tested to Category A, (600Vp, 10 us)
Audio Frequency Susceptibility
18.0
Equipment tested to Category Z, (+28 Vdc equipment)
Induced Signal Susceptibility
Magnetic Fields into Equipment
Magnetic Fields into Interconnect
Electric Fields into Interconnect
Voltage Spikes into Interconnect
19.0
19.3.1
19.3.3
19.3.4
19.3.5
Equipment tested to Category [ZC]
20 A at 400 Hz
30 A·m at 400 Hz
1800 V·m from 380 to 420 Hz
3.0 m
Radio Frequency Susceptibility
2
Radiated
Conducted
20.0
Equipment tested to Category [RR]
Category R, (20 V/m CW&SW) and (150 V/m PM)
Category R, (30 mA)
Radio Frequency Emission
2
21.0
Equipment tested to Category H
Environmental Qualification Form
Environmental Qualification Form Rev A Page 2 of 3
Equipment tested to Category [A3J3L3]
Equipment tested to Waveform Set A, Test Level 3
Equipment tested to Waveform Set J, Test Level 3
Equipment tested to Waveform Set L, Test Level 3
Icing
24.0
Equipment identified as Category X, no test performed
Electrostatic Discharge
25.0
Equipment identified as Category X, no test performed
Fire, Flammability
26.0
Equipment identified as Category C.
Other Tests
N/A
N/A
1
Orientation
Initial Freq. [Hz]
Final Freq. [Hz]
Longitudinal Axis
312
318
Vertical Axis
765
752
1165
1144
2
Environmental Qualification Form
REMARKS
This product is a derivative of the JA94-001A. All tests were performed on the JA94-001A.
A similarity analysis between the two products is detailed in the Jupiter Avionics Corporation document:
JA94-N44A CAN-TSO Design Change Assessment Rev A
Test information can be found in the Jupiter Avionics Corporation documents:
JA94-001A Test Report (Qualification - Final) Rev A
During exposure to vibration test conditions all critical resonances changed frequency greater than 1.5%:
Testing performed at CKC Laboratories in Bothell, WA, USA.
Reference report: JA94-001A Test Report (CKC Labs - DO-160G Section 20, 21, 22 - 20170911) Rev A
Environmental Qualification Form Rev A Page 3 of 3
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