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
2.2 Continued Airworthiness ................................................................................................................................... 4
2.3 Unpacking and Inspecting Equipment .............................................................................................................. 4
(3)Receive Volume Control ............................................................................................................................... 9
(9)VOX Threshold Control ............................................................................................................................... 11
B2 Instructions for Continued Airworthiness ........................................................................................................ B2
Music Operation ...................................................................................................................................... 13
Rev A Page iv
JCP3-N01 Control Panel - NVG
SECTION 1 - DESCRIPTION
1.1 System Overview
The JCP3-N01 Control Panel - NVG is part of an aircraft audio system consisting of the control panel and a remote
audio controller.
Figu
re 1-1 Aircraft Audio System
The control panel has the switches and level controls that allow the user to operate the remote audio controller.
Control commands are sent to the remote audio controller via a serial data bus from the control panel. The control
commands manage the user selectable functions of the audio system. The control panel provides a locking toggle
switch with a discrete output that places the remote audio controller in emergency operating mode.
The JCP3-N01 front panel music / configuration connector provides a discrete path to the JRAC music / configuration
connections. Configuration settings can be sent to the JRAC using a configuration cable and a PC running the product
configuration application ProCS
electronic devices are used in the JCP3-N01 design.
TM
. To facilitate future customizations and certification, neither software nor complex
1.2 Features Overview
The JCP3-N01 features a 15 pin D-Min connector, which interfaces to the JRAC-001. The JCP3-N01 input power is
derived from the JRAC-001.
The JCP3-N01 is NVIS Type I Class B compliant.
The JCP3-N01 has 1 rotary 6-position transmit selector switch.
The JCP3-001 has 6 transmit select annunciators
The JCP3-001 has a transmit active annunciator
The JCP3-N01 has 6 toggle transceiver monitor switches
The JCP3-001 has a CALL annunciator
The JCP3-N01 has 2 center-off toggle receiver monitor switches.
The JCP3-N01 has 1 rotary 16-position VOX threshold control.
The JCP3-N01 has 1 rotary 16-position ICS volume control.
The JCP3-N01 has 1 rotary 16-position RX volume control.
The JCP3-N01 has 1 locking toggle Emergency / Normal mode select switch.
The JCP3-N01 has 1 spring load center off toggle switch, nominally for ICS and TX PTT control.
A 3.5mm Music / Configuration connector is provided on the faceplate of the JCP3-N01 for downloading configuration
data to the JRAC-001 Remote Audio Controller. The connector can also be used as a music input and is compatible
with most music players.
Rev A Page 1
JCP3-N01 Control Panel - NVG
Name
Qty
Type
CALL ANNUNCIATOR
1
Active low discrete
CONFIG DATA TO JCP3
1
Data signal
CONTROL DATA TO JCP3
1
Data signal
MUSIC LEFT/ CONFIG DATA TO
REMOTE AUDIO CONTROLLER
+5/+28 VDC LIGHTS INPUT
2
Analog control signal
MODE SELECT / CONFIG AUDIO
1
Multi format signal
MODE SELECT
1
Multi format signal
POWER INPUT
1
power supply
RESET INPUT
1
Active low discrete
TX ANNUNCIATOR
1
Active low discrete
Name
Qty
Type
CONFIG DATA FROM JCP3
1
Data signal
CONTROL DATA FROM JCP3
1
Data signal
MODE SELECT / CONFIG AUDIO
1
Multi format signal
MUSIC LEFT/ CONFIG DATA TO
REMOTE AUDIO CONTROLLER
NORM MODE SELECT
1
Active low discrete
Name
Qty
Type
MUSIC RIGHT/CONFIG DATA FROM
MUSIC RIGHT/CONFIG DATA FROM
REMOTE AUDIO CONTROLLER
Installation and Operating Manual
1.3 Inputs and Outputs
Refer to the JCP3-N01 connector maps for the mating connector designators and pin assignments for the
input and output signals.
1.3.1 Inputs
1 Audio signal
1.3.2 Outputs
1.3.3 Bi-directional Signals
REMOTE AUDIO CONTROLLER
1.4 Specifications
1.4.1 Electrical Specifications
Power Input
Primary nominal voltage (from JRAC) 13.5 Vdc
Input current ≤ 0.5 A at 13.5 Vdc
1 Audio signal
1 Data signal (Main connector)
1 Data signal (Configuration connector)
1.4.1.1 Audio Performance
Rated Input Level
Music rated input 400 mVrms ±10%
Rated Output Power
Music rated output level 400 mVrms ±10%
Rev A Page 2
Output Load
Music load 1000 Ω ±10%
1.4.1.4 Discrete Signals
Active low control input, active signal level ≤ +3 Vdc
Active low control input, inactive signal level ≥ +9 Vdc
Active low control input signals, when active, source 0.1 to 10 mA
Active low control output, active output ≤ +2 Vdc
Active low control output signals, when active, sink ≤ 100 mA
Active low control input signals have an internal pull-up resistor
1.4.1.5 Lights Input
LIGHTS INPUT current 10 mA max.
1.4.2 Mechanical Specifications
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
Height
Behind panel depth
In front of panel depth
Faceplate width
Behind panel width
Weight
Enclosure material
Connectors (4):
Mounting
Bonding
Installation kit part number
1.4.3 Environmental Specifications
1.875 in [47.6 mm] max
1.65 in [41.9 mm] max
1.22 in [31.0 mm] max
5.75 in [146.1 mm] max
4.95 in [125.7 mm] max
0.84 lb [0.38 kg] max
5052-H32 brushed aluminum with
conversion coating
J1 (System) One 15-pin D-Sub male, V5 locking
J2 (Music /configuration) One 4 pole 3.5mm stereo jack
J3 (Configuration)
J4 (Rear stud fastener)
One 4 pole 3.5mm stereo jack
One 4-40, 0.5 in. max
4 Dzus fasteners
≤ 2.5 mΩ
INST-JCPX
The JCP3-N01 Control Panel 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.
This section contains unpacking and inspection procedures, installation information, and post-installation checks.
2.2 Continued Airworthiness
Maintenance of the JCP3-N01 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/warrantyregistration.
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 JCP3-N01 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.
Rev A Page 4
JCP3-N01 Control Panel - NVG
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.
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 JCP3-N01 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.
2.4.4 Legend Replacement
The JCP3-N01 illuminated legends are field replaceable. For further information, refer to the ‘Legend Replacement’
document in Appendix A of this manual.
2.4.5Post Installation Checks
2.4.5.1Voltage/Resistance checks.
Do not attach this unit until the following conditions are met:
a) Check P1 between pins 1 and 9 for 13 Vdc power.
b) Check P1 pin 14 for +5 Vdc lights voltage or P1 pin 15 for +28 Vdc lights voltage.
c) Check P1 pin 10 (Chassis ground) for continuity to ground (less than 0.5 Ω).
d) Confirm P1 pin 13 (RESET INPUT) is connected to the Remote Audio Controller
P3 pin 13 (RESET OUTPUT)
e) Check all pins for shorts to ground or adjacent pins.
2.4.5.2Power on Checks.
Power up the aircraft’s systems and confirm normal operation of all functions of the JCP3-N01. Refer to
Section 3 (Operation) for specific operational details.
a) Begin with only the pilot’s 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 co-pilot’s 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.
Rev A Page 5
JCP3-N01 Control Panel - NVG
Among the options is ‘- - - -‘ which signifies that
Clicking on a customizable legend will open a drop-
Installation and Operating Manual
2.5 Legend Text Selection using ProCS™
The configuration program ProCS™ can be used to customize the text for each legend either at the time of ordering
the unit, or if text changes are required after installation. The JCP3-N01 need not be connected to a computer to
select the legend text.
For information on ordering customized legends, refer to the ProCS™ Ordering Instructions on the JAC website.
2.5.1 Virtual Front Panel
The Virtual Front Panel window is used to specify the text for each legend.
down menu listing the options for that label. The
currently selected option will be highlighted. To escape
from the menu, click on the desired option, or right-click
in the window. A 'Print…’ box will appear. Click outside
the box to escape, or select it to print the 'Virtual Front Panel window showing the current label selections.
In t
he example shown here, the option ‘New…’ has been selected. A
pop-up ‘New Label’ window will appear, allowing the user to create a
customized legend – in this case, JAC. The new legend name will
now be shown in the appropriate position on the faceplate
representation in the software program, and will be used in the
connector maps and interconnect.
Note: If the name of a front panel switch is changed using this software, the change will be incorporated in
the connector maps and interconnect, to give truly customized installation diagrams.
2.5.2 Connector Maps
This section contains connector maps and interconnects that are automatically generated to show changes to switch
labels that affect the installation of the JCP3-N01.
the legend will be left blank, and ‘New…’ which
allows the user to enter a completely new
legend of up to five characters. If a ‘new’
legend has been added, the option ‘Edit …’ is
added to the menu to enable changes to the
newly created label.
Rev A Page 6
2.6 Adjustments and Configuration using ProCS™
Connector Type
Hand crimp tool
Positioner
Insertion/extraction tool
Positronic
9507
9502-3
M81969/1-04
Positronic
AFM8 (Daniels)
M22520/2.08 KB-1
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
2.6.1
The JCP3-N01 has no internal adjustments; however, configuration data for the JRAC-001 Remote Audio
Controller can be sent via the JCP3-N01 front panel connector (♫/io), using the configuration program ProCS™.
For full information on configuring the JRAC-001, refer to the JRAC-001 manual on the JAC website.
For full information on the configuration process, refer to the ProCS™ manual on the Jupiter Avionics website. .
2.6.2
The JCP3-N01 menu items 'ProCS Setup' provide Setup drawings showing different cabling
arrangements for connecting the JCP3-N01 to a computer and other equipment.
ProCS Setup - JA99,ProCS Setup - CAB-USB-0006 and ProCS Setup - Virtual Panel show the connections used
for testing the JCP3-N01. These setup drawings would not be used in normal operation.
Configuring the JRAC-xxx-Remote Audio Controller via the JCP3-N01-N01
The front panel Music/Configuration port
(♫/io) is protected by a urethane rubber
cover, which can be lifted upwards or
rotated round (as shown) to provide
access to the port
♫♫/io port
Port cover
ProCS™ Setup
ProCS Setup - JRAC-001 shows the cabling for using the JCP3-N01 for configuring the JRAC-xxx using P
(see section 2.6.1 above).
2.7 Installation Kit
The kit required to install this unit is not included with the unit.
The installation kit (Part # INST-JCPx) consists of the following:
Quantity Description JAC Part #
1 0.375" Inside Diameter TAG ring CON-5500-0375
1 D-Sub 15-pin connector, hood and 15 crimp pinsCON-3420-0015
1 3/4" I/D Heat Shrink TubingWIR-HTSK-0750
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.
roCS™
Rev A Page 7
JCP3-N01 Control Panel - NVG
SECTION 3 – OPERATION
1 2 3
10
6
5
4
7
8
11
9
3.1 Introduction
This section contains the operating instructions for the JCP3-N01.
The JCP3-N01 acts as a control panel for a remote Audio controller such as the Jupiter Avionics JRAC-001.
The JCP3-N01 commands the remote audio controller, and this manual is written to describe the results of any
operation of the JCP3-N01 controls.
3.2 Front Panel Controls
Note: The 15 legends and two annunciators are removable and may be replaced with custom ordered parts.
For the purpose of this manual the controls will be referred to by the default legend and annunciator names as
shown below. The JCP3-N01 legends and annunciators are NVIS Type I Class B compliant.
1.Transceiver switches and associated legends
2.Receiver switches and associated legends
3.Receive volume control
4.EMER/NORM switch
5.Pilot’s Transmit/ICS (Multi-function) switch
6.Music/configuration port cover and legend (♫/io)
Rev A Page 8
ransmit annunciator (deadfront)
7.T
8.Transmit selector
9.V
OX threshold control
10. CA
11. IC
LL annunciator (deadfront)
S volume control
(1)Transceiver Switches
These are six white two-position toggle switches.
When a switch is set to the ‘up’ position, audio from
the associated transceiver is routed to the phones.
The legends (above the switches) are
interchangeable to allow customization.
(Default – COM1, COM2, COM3, COM4, COM5
and COM6)
(2)Receiver Switches
These are two blue two-position centre-off
toggle switches. When a switch is set to the ‘up’
or ‘down’ position audio from the selected
receiver is routed to the phones.
egends (two above and two below the
The l
switches) are interchangeable to allow
customization. (Default – NAV1, NAV2, NAV3,
N4&5.)
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
(3)Receive Volume Control
This is a rotary knob that adjusts the phones volume of
the receive audio from minimum - fully counterclockwise
(ccw) to maximum - fully clockwise (cw). Individual radio
volume controls should be set to a nominal level, and
then adjusted for changing flight conditions using this
control.
(4)EMER/NORM Mode Switch
This is a red two-position locking toggle switch. When set to the ‘up’
position, the unit is Emergency mode, and when set to the ‘down’
position, the unit is in Normal mode. The legends are
interchangeable to allow customization. (Default – EMER, NORM.)
The switch is lockable to prevent accidental changing of the mode.
The switch must be lifted to release the lock.
For full information on Emergency and Normal Mode operation, see
sections 3.3 and 3.4 below.
(5) Multi-function (Transmit/ICS) Switch
This is a green two-position centre-off momentary toggle switch.
When in the default XMIT/ICS configuration, this switch acts as the pilot’s
‘Press-to-talk’ (PTT) button. The unit will transmit on the selected
transceiver when the switch is held in the ‘up’ position, and when held in
the ‘down’ position, it will transmit on the intercom.
See section 3.3.6below for Multi-function Switch operation.
Note: At installation, this switch may be configured to operate in default (XMIT/ICS) or alternative mode.
Check with your installing agency for confirmation of the operation of this switch. The legends are
interchangeable to allow customization.
Rev A Page 9
(6) Music/Configuration Connector Cover (♫/io)
This is a music input that is compatible with most music players.
It accepts a 3 pole 3.5mm stereo plug with a slim diameter
connector housing.
(This connector is also used during installation to change
configuration settings for the JRAC-001.)
The port (♫/io) is protected by a urethane rubber cover, which can be
lifted upwards or rotated round (as shown) to provide access to the
port.
♫♫/io port
Port
cover
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
CAUTION: If an unapproved connector or cable is used, damage to the unit or to any attached device may
occur. If in doubt, contact JAC for a list of approved cables, music sources and devices.
(7)Transmit Annunciator - TX
This is a deadfront annunciator that will illuminate
when the JRAC-001 is transmitting.
The default legend is ‘TX’, but it is interchangeable
to allow customization.
(8)Transmit Selector
This is a rotary six-position control that is used to
select transmission via one of the six transceivers.
Each of the transmit selector positions is linked by a
white line to the corresponding transmit select
annunciator, transceiver switch and legend.
The appropriate annunciator will light green to show
which transceiver is selected for transmit - ‘COM4’ in
this example.
Rev A Page 10
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
(9)VOX Threshold Control
This is a rotary knob that is used to select the VOX threshold of
the unit. See below.
When rotated fully clockwise (cw), the threshold will be at
maximum and 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 should be adjusted for proper operation according
to the ambient noise.
(10)CALL Annunciator
This is a customizable deadfront annunciator activated by
an external switch.
When enabled, it will illuminate when a call is received from
another user’s audio controller, or by a remote ‘call’ button
within the aircraft.
Note: Check with your installing agency for confirmation of the operation of this annunciator. The legends
are interchangeable to allow customization.
(11)ICS Volume Control
This is a rotary control used to adjust the volume of all
ICS audio to suit the ambient conditions. Rotating the
control fully cw gives rated level, and fully ccw reduces
the output to minimum level.
Rev A Page 11
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
3.3 Normal Operation Mode
Note: Numbers in parentheses refer to the front panel controls shown in section 3.2.
The Audio System is in Normal mode when the front panel EMER / NORM switch (4) is in the NORM position and
suitable electrical power is supplied to the audio system (Control Panel and Remote Audio Controller).
All operation described is for an Audio System consisting of a JCP3 Control Panel and a JRAC Remote Audio
Controller.
3.3.1 Panel Lighting
The control panel legends and annunciators will be illuminated and dim (when appropriate) through the aircraft lighting buss.
3.3.2 Receiving
When the Audio System receives an incoming transmission on a transceiver or receiver that has been selected, either
by the white transceiver receive switches (1) or the transmit selector (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 front panel RX volume control
(3). It will be muted if the unit is transmitting and muting of receive audio during transmit is enabled.
3.3.3 Transmitting (Transmit Operation)
To select a transceiver, rotate the Transmit Select Switch until it aligns with the line leading to the Transceiver Select
switch legend - see (1) - default legends COM 1 through COM 6. The corresponding Transmit Select annunciator will
illuminate.
When the user’s TX PTT is activated, the Audio System will transmit on the selected transceiver, and the deadfront
Transmit Annunciator (7) will illuminate ‘TX’. All MIC and sidetone audio will be routed to the user’s phones, and any
music will be muted for the duration of the transmission.
V
3.3.4
A user’s MIC audio is routed to the ICS when the MIC audio level exceeds the VOX threshold.
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. The VOX level is controlled by the VOX knob (9).
3.3.5
ICS audio routed to the PHONES 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 routed to the PHONES also includes the audio input on the ICS TIE from other audio controllers.
The sum of all the MIC audio from users with ICS KEY active or with MIC audio level exceeding the VOX
Threshold level is output on the ICS TIE line.
OX Operation
ICS Operation
The ICS audio is muted during transmit (if selected via ProCS™).
The ICS audio level at the phones is controlled by the ICS volume control (11).
Note: At installation, this switch may be configured to operate in default or alternative mode. Check with
your installing agency for confirmation of the operation of this switch.
Default Operation
When in the default XMIT/ICS configuration, this switch acts as the pilot’s ‘Press-to-talk (PTT) button. The Audio
System will transmit on the selected transceiver when the switch is set to the ‘up’ position, and when set to the ‘down’
position, it will transmit on the intercom.
Alternative Operation
This switch may be configured to provide a ground signal to operate other equipment.
3.3.7Music Operation
Music to the phones will be muted by incoming audio (ICS, Receive, Direct or Alert Audio) or if the Audio System is
transmitting. When the incoming audio has ended, the music will gradually return to the previous level.
3.4 Emergency Operation Mode
Emergency mode can be selected by the EMER / NORM switch on the control panel.
Refer to the controlled device operating manual for information on operation during emergency mode.
Rev A Page 13
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
Appendix A - Installation Drawings
A1 Introduction
The drawings necessary for installation and troubleshooting of the JCP3-N01 Control Panel - NVG are in this
Appendix, as listed below.
Note: A fully customized set of Connector Maps
software. Refer to the ProCS™ manual for further information.
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
Control Panel - NVG
Interconnect Notes
JCP3-N011/3
JCP3-N01 Interconnect Rev A.dwg
TAT/CPM
JCP3-N01 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 CONNECTOR PINS SHOULD BE TERMINATED TO AIRFRAME GROUND
USING A TAG RING P/N: MS27741-5 OR EQUIVALENT.
GROUND PIN TO ILLUMINATE ANNUNCIATOR ON FACEPLATE.
MOMENTARILY GROUND PIN TO RESET CONTROL PANEL.
ONLY CONNECT ONE OF EITHER +28 VDC OR +5 VDC LIGHTS INPUT.
FOR MUSIC INPUT, CONNECT MODE SELECT TO GROUND THROUGH 3.5MM MALE CABLE
CONNECTOR RING 2.
THE FRONT PANEL MUSIC INPUT SHALL NOT BE CONNECTED TO ANY OTHER AUDIO INPUT.
2
1.
3
4
CONNECTOR PIN LEGENDS
LEGEND
SPAREINTERNAL CIRCUITS MAY EXIST AND MAY BE ACTIVATED FOR FUTURE USE. NO EXTERNAL
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:
Control Panel - NVG
qu
`^ii
J2
5.75in MAX
146.1mm MAX
1.875in MAX
47.6mm MAX
JAC
CPM
09-14-17
JAC
KDV
09-14-17
Jupiter Avionics Corporation Audio Controllers
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.
TOL-CUST-EXTR – Legend Replacem ent Page 1 of 1
JCP3-N01 Control Panel - NVG
Installation and Operating Manual
Appendix B - Certification Documents
Rev A Page B1
JCP3-001 Control Panel - NVG
Installation and Operating Manual
B1 Airworthiness Approval
Airworthiness approval of the JCP3-N01 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 JCP3-N01 Control Panel - NVG. 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 J
[aircraft location].
The JCP3-N01 is approved to CAN-TSO-C139. The JCP3-N01 meets RTCA DO-160G environmental qualifications
for this installation. See Section 1 of the JCP3-001 Installation and Operation Manual.
Installed in accordance with the JCP3-N01 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JCP3-N01 interfaces with the Remote Audio Controller per the Installation Manual instructions.
The JCP3-N01 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JCP3-N01 from the Remote Audio Controller.
Aircraft equipment list, weights and balance amended. Compass compensation checked and found to conform to
applicable regulations.
upiter Avionics JCP3-N01 Control Panel - NVG in
B2 Instructions for Continued Airworthiness
Maintenance of the JCP3-N01 Control Panel - NVG is “on condition” only. Refer to the JCP3-N01 Maintenance
Manual. Periodic maintenance of the JCP3-N01 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JCP3-N01 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 JCP3-N01 Control
Panel - NVG 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 JCP3-N01 installed in an [aircraft make and model].
Applicability: Applies to a Jupiter Avionics JCP3-N01 installed in an [aircraft make and model].
Definitions/Abbreviations: None, N/A.
Precautions: None, N/A.
Units of Measurement: None, N/A.
Referenced Publications: JCP3-N01 Installation and Operating Manual
JCP3-N01 Maintenance Manual
JCP3-N01 Operating Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution: This document should be a permanent aircraft record.
A Page B2
Rev
JCP3-001 Control Panel - NVG
Installation and Operating Manual
2. Description of the System/Alteration
Jupiter Avionics JCP3-N01 Control Panel - NVG with interface to a remote Audio Controller 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 JCP3-N01 Operating Manual.
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JCP3-N01 is ‘on condition’ only. Periodic maintenance is not required. Refer to the
JCP3-N01 Maintenance Manual.
6. Troubleshooting Information
Refer to the JCP3-N01 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JCP3-N01 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 JCP3-N01 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
JCP3-N01 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 JCP3-N01 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.
14.Overhaul Period
No additional overhaul time limitations.
15.Airworthiness Limitation Section
N/A
B3Environmental Qualification Form
See next pages
Rev A P
age B3
JCP3-N01 Control Panel - NVG
Prepared:
KV
Checked:
Approved:
Nomenclature
Control Panel - NVG
Type/Model/ Part No.:
JCP3-N01
TSO No.:
CAN-TSO-C139
Manufacturer’s Build Configuration:
JCP3-N01 Build Configuration Rev A
Manufacturer’s Test Report:
JCP3-001 Test Report (Qualification - Final) Rev A
JCP3-N01 CAN-TSO Design Change Assessment Rev A
Manufacturer’s Specification
and/or Other Applicable Specification:
JCP3-001 Declaration of Design and Performance Rev B
JCP3-N01 Derivative Declaration of Design and Performance Rev A
Manufacturer:
Jupiter Avionics Corporation
Address:
1959 Kirschner Road, Kelowna, BC, Canada, V1Y 4N7
Revision & Change No of DO-160:
Rev. G dated December 8, 2010
Dates Tested:
2016 July 26 to 2017 Jul 07
CONDITIONS
SECTION
DESCRIPTION OF TESTS CONDUCTED
Temperature
4.5
Equipment tested to Category C4
Ground Survival Low Temperature
4.5.1
Equipment tested to Category C4 (-55 °C)
Short-Time Operating Low
Temperature
4.5.1
Equipment tested to Category C4 (-45 °C)
Operating Low Temperature
4.5.2
Equipment tested to Category C4 (-45 °C)
Ground Survival High Temperature
4.5.3
Equipment tested to Category C4 (+85 °C)
Short-Time Operating High
Temperature
4.5.3
Equipment tested to Category C4 (+70 °C)
Operating High Temperature
4.5.4
Equipment tested to Category C4 (+70 °C)
In-Flight Loss of Cooling
4.5.5
Equipment identified as Category X, no test performed
Altitude
4.6
Equipment tested to Category (A1)(D1)
Altitude
4.6.1
Equipment tested to Category D1 (55,000 ft)
Decompression
4.6.2
Equipment tested to Category A1 (8,000 to 55,000 ft)
Equipment identified as 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)
Vibration1
Fixed Wing - Sine
Fixed Wing - Random
Helicopter - Random, unknown
8.0
8.5.1
8.5.2
8.8.3
Equipment tested to Categories:
SM
SB
U2FF1
Environmental Qualification Form
JAC
09-19-17
CPM
JAC
09-19-17
KDV
Environmental Qualification Form Rev A Page 1 of 3
JCP3-N01 Control Panel - NVG
CONDITIONS
SECTION
DESCRIPTION OF TESTS CONDUCTED
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 2
DC Equipment
DC Current Ripple
DC Inrush
16.0
JRAC-001 Remote Audio Controller
tested to Category: (ZXX)(BXX)
Z (+28 Vdc equipment),
B (+14 Vdc and + 28 Vdc equipment)
X, no test performed
X, no test performed
Voltage Spike 2
17.0
JRAC-001 Remote Audio Controller
tested to Category A (600Vp, 10 us)
Audio Frequency Susceptibility 2
18.0
JRAC-001 Remote Audio Controller
tested to Category Z (+28 Vdc equipment)
JRAC-001 Remote Audio Controller
tested to Category B (+14 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 ZCX
20 A at 400Hz
30 A·m at 400Hz
1800 V·m at 400Hz
3.0 m
Radio Frequency Susceptibility 3
Radiated
Conducted
20.0
Equipment tested to Category RR
R (20 V/m CW&SW) and (150 V/m PM)
R (30 mA)
Radio Frequency Emission
Radiated3
Conducted
21.0
Equipment tested to Category H
Lightning Induced Transient Susceptibility
Pin Injection
Cable Bundle Single
and Multiple Stroke3
Cable Bundle Multiple Burst3
22.0
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
Lightning Direct Effects
23.0
Equipment identified as Category X, no test performed
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
Environmental Qualification Form
Environmental Qualification Form Rev A Page 2 of 3
JCP3-N01 Control Panel - NVG
Environmental Qualification Form
REMARKS
This product is a derivative of the JCP3-001. All tests were performed on the JCP3-001. A similarity analysis
between the two products is detailed in the Jupiter Avionics Corp. document JCP3-N01 CAN-TSO Design
Change Assessment Rev A.
Test information can be found in the Jupiter Avionics Corp. document: JCP3-001 Test Report (Qualification -
Final) Rev A
1
During exposure to vibration test conditions all critical resonances changed frequency less than 1.5%.
2
The JCP3-001 Control Panel was operating a JRAC-001 Remote Audio Controller during the power input, voltage
spike and audio frequency conducted susceptibility tests. During these tests, the JRAC-001 Remote Audio
Controller was exposed to the test conditions.
3
Testing performed at CKC Laboratories in Bothell, WA, USA.
See report JRAC-001 Test Report Signed (CKC Labs - DO-160G Section 20, 21, 22 - 20161107 to 10) Rev A
Environmental Qualification Form Rev A Page 3 of 3
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