Jupiter Avionics JA74-410 User manual
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page ii
Copyright 2022 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.
RECORD OF REVISIONS
Revision
Rev Date
Description
ECR
A
Jul2022
Initial release, Serial number 1001 and higher.
7716
Prepared:
MPB/DGB
Checked:
Approved:
IMPORTANT:
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
JAC
SDB
07-25-22 JAC
KDV
07-25-22
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page iii
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 Output ....................................................................................................................................................... 1
1.3.3 Bi-Directional ............................................................................................................................................ 1
1.3.4 Grounds/Spares........................................................................................................................................ 1
1.4 Specifications.................................................................................................................................................... 2
1.4.1 Electrical Specifications ............................................................................................................................ 2
1.4.2 Mechanical Specifications ........................................................................................................................ 2
SECTION 2 – INSTALLATION ........................................................................................................................................ 3
2.1 Introduction ....................................................................................................................................................... 3
2.2 Continued Airworthiness................................................................................................................................... 3
2.3 Unpacking and Inspecting Equipment .............................................................................................................. 3
2.3.1 Warranty ....................................................................................................................................................... 3
2.4 Installation Procedures ..................................................................................................................................... 3
2.4.1 Installation Limitations .................................................................................................................................. 3
2.4.2 Cabling and Wiring ....................................................................................................................................... 3
2.4.3 Mechanical Installation ................................................................................................................................. 4
2.4.6 Post Installation Checks ............................................................................................................................... 4
2.5 Installation Kit ................................................................................................................................................... 4
2.5.1 Recommended Crimp tools ...................................................................................................................... 4
2.6 Installation Drawings......................................................................................................................................... 4
SECTION 3 – OPERATION ............................................................................................................................................. 5
3.1 Introduction ....................................................................................................................................................... 5
3.2 Front Panel Connectors.................................................................................................................................... 5
3.2.1 USB-C Power Output................................................................................................................................ 5
3.2.2 USB-A Power Output................................................................................................................................ 5
3.3 Compatibility ..................................................................................................................................................... 5
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 1
JA74-410 USB-A and USB-C Charger
SECTION 1 - DESCRIPTION
1.1 System Overview
The JA74-410 USB-A and USB-C Charger allows the aircraft owner/operator to use an unused portion of the
instrument panel (3 Dzus high) for charging two devices simultaneously.
1.2 Features Overview
One USB 2.0 Type A receptacle is provided to supply 5 Vdc power up to 2.1 Amps.
One USB 2.0 Type C receptacle is provided to supply up to 45 Watts.
1.3 Inputs and Outputs
Refer to the JA74-410 connector map for the mating connector designators and contact assignments for the input and
bi-directional signals.
1.3.1 Inputs
Name
Qty
Type
POWER INPUT
1
Power
CC1
1
CC1 input
CC2
1
CC2 input
1.3.2 Output
Name
Qty
Type
+5VDC
1
USB power output
V BUS
4
USB power output
1.3.3 Bi-Directional
Name
Qty
Type
D+
1
Charge sense
D-
1
Charge sense
D+
3
Data
D-
3
Data
1.3.4 Grounds/Spares
Name
Qty
Type
POWER GROUND
1
Power ground
GROUND RETURN
4
Ground return
CHASSIS GROUND
1
Chassis ground
SPARE
3
Spares (Main connector)
SPARE
10
Spares (USB-C connector)
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page 2
1.4 Specifications
1.4.1 Electrical Specifications
Power Input
Primary nominal voltage 28.0 Vdc
Maximum voltage 32.2 Vdc
Minimum voltage 22.0 Vdc
Emergency voltage 18.0 Vdc
Power Input - Off ≤ 15 Vdc
Input current at 28 Vdc ≤ 3.2 A
1.4.1.1 USB-A Output Performance
Output rated current ≤2.1 A
Output rated voltage +5 Vdc ± 10 %
Ripple ≤ 5 mVpp
Short circuit ≥ 1 min
1.4.1.2USB-C Output Performance
Output rated current 2.25 A for +20 V output
3.00 A for all other voltages
Output rated voltage +5 Vdc ± 5 %
+9 Vdc ± 5 %
+12 Vdc ± 5 %
+15 Vdc ± 5 %
+20 Vdc ± 5 %
Ripple
Short circuit
1.4.2 Mechanical Specifications
Height
Behind panel depth (not including connectors)
Width
Weight
Enclosure:
Faceplate
Connector (3): J1 Main
J2 USB C
J3 USB A
Mounting
Bonding
Installation kit part number
≤ 5 mVpp for +5 V output
≤ 9 mVpp for +9 V output
≤ 12 mVpp for +12 V output
≤ 15 mVpp for +15 V output
≤ 20 mVpp for +20 V output
≥ 1 min for all voltages
1.25 in [28.6 mm] maximum
5.46 in [138.7 mm] maximum
5.75 in [146.1 mm] maximum
0.89 lb [0.40 kg] maximum
5052-H32 aluminum; brushed
texture and black anodized
6061-T651 Aluminum with flat black
urethane paint; white legends
One 9-pin D-Sub male, V5 locking
One USB Type C Female
One USB Type A Female
2 Dzus fasteners
≤2.5 mΩ
INST-JA74
Rev A Page 3
JA74-410 USB-A and USB-C Charger
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 JA74-410 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 on-
line 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
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
Those installing the JA74, on or in a specific type or class of aircraft, must determine that the aircraft installation
conditions meet standards. The JA74 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 AC43.13-
1B Change 1, Paragraphs 11-76 through 11-78. Follow the Connector Map in Appendix A of this manual.
Note that this unit has a ‘clamshell’ hood that is installed after the wiring is complete.
Maintain wire segregation and route wiring in accordance with the original aircraft manufacturer’s maintenance
instructions.
Unless otherwise noted, all wiring shall be a minimum of 20 AWG. Refer to the Interconnect drawing for additional
specifications.
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page 4
2.4.3 Mechanical Installation
The JA74-410 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.
2.4.6 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 1for +28 Vdc relative to ground.
b) Check P1 pin 6(power ground) for continuity to ground (less than 0.5 Ω).
c) Check P1 pin 7 (chassis ground) for continuity to ground (less than 0.5 Ω).
d) Check all pins for shorts to ground or adjacent pins.
2.4.6.2 Power on Checks
Power up the aircraft’s systems and confirm normal operation of all functions of the JA74. Refer to
Section 3 (Operation) for specific operational details.
When all performance checks are satisfied, complete the necessary regulatory documentation before releasing the
aircraft for service. Refer to Appendix B.
2.5 Installation Kit
The kit required to install this unit is not included with the unit.
The installation kit (Part # INST-JA74) consists of the following:
Quantity Description JAC Part #
1 D-Sub 9-pin connector, hood and 9 crimp pins CON-3420-0009
1 JA74 Assembly Notes, Installation Kit DOC-INST-JA74
2.5.1 Recommended Crimp tools
Standard D-Sub Crimp Tool Chart
Tool Type
Hand crimping tool
Positioner
Insertion/extractor tool
POSITRONIC
9507-0-0-0
9502-5-0-0
4711-2-0-0
DANIELS
AFM 8
K13-1
91067-2
MIL-SPEC
M22520/2-01
M22520/2-08
M81969/1-02
2.6 Installation Drawings
The drawings and documents required for Installation can be found in Appendix A of this manual.
Rev A Page 6
JA74-410 USB-A and USB-C Charger
SECTION 3 – OPERATION
3.1 Introduction
This section contains the operating instructions for the JA74-410.
The JA74-410 provides charging for two phones or other devices.
3.2 Front Panel Connectors
The JA74-410 has one front panel USB-A Power output connector and one front panel USB-C Power output
connector.
3.2.1 USB-C Power Output
This Power Output is a USB Type C connector.
This connector has a USB PD Type C receptacle with an auto-adjustable supply which can deliver +5 Vdc @ 3 A, +9
Vdc @ 3 A, +12 Vdc @ 3 A, +15 Vdc @ 3 A, or +20 Vdc @ 2.25 A for charging cell phones and similar devices.
3.2.2 USB-A Power Output
This Power Output is a USB Type A connector.
Note: The USB-A port is not designed to be used for data transfer.
This connector is provided to supply +5 Vdc up to 2.1 Amps for charging cell phones and similar devices.
3.3 Compatibility
CAUTION: Attempting to connect an incompatible plug or device could damage the JA74, the
attached device, or both.
If in doubt regarding compatibility of a specific item, contact Jupiter Avionics (www.jupiteravionics.com).
USB-C
Power Output
USB-A Power
Output
Rev A Page A1
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Appendix A - Installation Drawings
A1 Introduction
The drawings necessary for installation and troubleshooting of the JA74-410 USB-A and USB-C Charger are in this
Appendix, as listed below.
A2 Installation Drawings
DOCUMENT Rev
JA74-410 Connector Map A
JA74-410 Interconnect A
JA74-410 Mechanical Installation A
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
USB-A and USB-C Charger
Connector Map
JA74-410 1/1
JA74-410 Connector Map Rev A.dwg
TAT
1 2 3 4 5
6 7 8 9
POWER INPUT
GROUND RETURN
SPARE 2
D-
D+
POWER GROUND
CHASSIS GROUND
SPARE 3
SHIELD
P1
9 PIN FEMALE DMIN
MATING CONNECTOR
VIEW IS FROM REAR OF MATING CONNECTOR
P3
USB TYPE A MALE
MATING CONNECTOR
+5V
D+
D-
4 3 2 1
View is from front of mating connector
USB A Connector
GROUND
Main Connector
P2
USB TYPE C MALE
MATING CONNECTOR
USB C Connector
B2B1
View is from front of mating connector
B3 B4 B5 B6 B7 B8 B9 B10 B11 B12
A2 A1A3A4A5A6A7A8A9A10A11A12
SPARE 6
SPARE 7
SPARE 5
V BUS
SPARE 3
SPARE 4
V BUS
CC1
SPARE 1
SPARE 2
GROUND RETURN
GROUND RETURN
SPARE 9
SPARE 8
CC2
V BUS
SPARE 11
SPARE 10
V BUS
SPARE 12
SPARE 14
SPARE 13
GROUND RETURN
SPARE 1
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
USB-A and USB-C Charger
JA74-410 1/2
JA74-410 Interconnect Rev A.dwg
TAT
JA74-410 INTERCONNECT WIRING NOTES
NOTES
ALL WIRE SIZE SHOULD BE 22 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 22 AWG WIRE. LENGTH NOT
TO EXCEED 3 FT (0.91 M).
CABLE LENGTH NOT TO EXCEED 6 FT (1.82 M).
2
1.
3
JAC
SDB
06-02-22
JAC
KDV
06-02-22
POWER INPUT 1
CHASSIS GROUND 7
JA74-410 MAIN
P1
9 PIN FEMALE DMIN
MATING CONNECTOR
CHASSIS GROUND
22 AWG
2
JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT
TITLE
APPROVED
PREPARED
CHECKED
L00N3
NCAGE CODE PART NO. SHEET
DOC NO.
CONFIDENTIAL & PROPRIETARY
TO JUPITER AVIONICS CORP.
USB-A and USB-C Charger
JA74-410 2/2
JA74-410 Interconnect Rev A.dwg
TAT
+ 28 VDC POWER
4A
POWER GROUND 6
GROUND RETURN A1
P2
USB TYPE C MALE
MATING CONNECTOR
VBUS A4
CC1 A5
VBUS A9
22 AWG
22 AWG
JA74-410 USB C
J2
J1
CHARGEABLE USB DEVICE
2
3
GROUND RETURN A12
GROUND RETURN B1
VBUS B4
CC2 B5
VBUS B9
GROUND RETURN B12
GROUND RETURNA1
VBUSA4
CC1A5
VBUSA9
GROUND RETURNA12
GROUND RETURNB1
VBUSB4
CC2B5
VBUSB9
GROUND RETURNB12
+5V 1
P3
USB TYPE A MALE
MATING CONNECTOR
D- 2
D+ 3
GROUND 4
VBUS1
D-2
D+3
GROUND4
JA74-410 USB A
J3
CHARGEABLE USB DEVICE
3
20 AWG
20 AWG
SPARE 3
SHIELD
8
9
D+ 5
D- 4
SPARE 2 3
SPARE 1 2
USB DEVICE
D-
D+
JAC
SDB
06-02-22
JAC
KDV
06-02-22
CENTER OF GRAVITY
WEIGHT: 0.89 lbs [0.40 kg] MAX.
0.05in [0.8mm]
0.5in
11.9mm
5.71in MAX
145.0mm MAX
2.4in
60.2mm
2.1in
52.1mm
CONFIDENTIAL & PROPRIETARY
0.5 DEG
JUPITER AVIONICS TEMPLATE SOLIDWORKS LANDSCAPE SIZEB REV B.DRWDOT
JA74-410 Mechanical Installation Rev A.SLDDRW
DOC. NO.
1/1
SHEET
JA74-410
PART NO.
TITLE
DRAWING NOT TO SCALE
TO JUPITER AVIONICS CORP.
APPROVED
CHECKED
TATPREPARED
N/A
N/A
MATERIAL:
FINISH:
NCAGE CODE
L00N3
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: USB-A and USB-C Charger
J2 J3
1.125in MAX
28.6mm MAX
5.75in MAX
146.1mm MAX
5.46in MAX
138.7mm MAX
0.45in MAX
11.4mm MAX
4.82in MAX
122.4mm MAX
JAC
SDB
07-22-22
JAC
KDV
07-22-22
Rev A Page B1
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Appendix B - Installation Documents
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page B2
B1 Airworthiness
Airworthiness approval of the JA74-410 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 installing a Jupiter
Avionics JA74-410 USB-A and USB-C Charger. 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:
Installed the Jupiter Avionics JA74-410 USB-Aand USB-CCharger [aircraft location].
Installed inaccordance with the JA74-410 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JA74-410 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JA74-410 through a 4-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 JA74-410 USB-A and USB-C Charger is “on condition” only. Periodic maintenance of the
JA74-410 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA74-410 unit installation as partof 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 JA74-410 USB-A
and USB-CCharger 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 JA74-410 installed in an [aircraft make and model].
Applicability: Applies to a Jupiter Avionics JA74-410 installed in an [aircraft make and model].
Definitions/Abbreviations: None, N/A.
Precautions: None, N/A.
Units of Measurement: None, N/A.
Referenced Publications: JA74-410 Installation and Operating Manual
JA74-410 Maintenance Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution: This document should be a permanent aircraft record.
JA74-410 USB-A and USB-C Charger
Installation and Operating Manual
Rev A Page B3
2. Description of the System/Alteration
Jupiter Avionics JA74-410 USB-A and USB-C Charger.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.
4. Servicing Information
N/A
5. Maintenance Instructions
Maintenance of the JA74-410 is ‘on condition’ only. Periodic maintenance is not required. Refer to the
JA74-410 Maintenance Manual.
6. Troubleshooting Information
Refer to the JA74-410 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual - the JA74-410 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 JA74-410 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
JA74-410 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 JA74-410 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
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