True blue power TA202 Series Documento técnico
Installation Manual and Operating Instructions
TA202 Series
High Power USB Charging Port
True Blue Power® is a division of Mid-Continent Instrument Co., Inc.
Mid-Continent Instrument Co., Inc.
dba Mid-Continent Instruments and Avionics
9400 E. 34th Street N.
Wichita, KS 67226 Manual number 9017899
PH (800) 821-1212 FX (316) 630-0723 Revision G, June 6, 2019
Rev G, June 6, 2019 2 Manual Number 9017899
FOREWORD
This manual provides information intended for use by persons who, in accordance with current
regulatory requirements, are qualified to install this equipment. If further information is required,
please contact:
True Blue Power
c/o Mid-Continent Instrument Co., Inc.
Attn: Customer Service Dept.
9400 E. 34th Street N.
Wichita, KS 67226 USA
PH (316) 630-0101
FX (316) 630-0723
www.truebluepowerusa.com
www.mcico.com
We welcome your comments concerning this manual. Although every effort has been made to
keep it free of errors, some may occur. When reporting a specific problem, please describe it
briefly and include the manual part number, the paragraph/figure/table reference and the page
number. Send your comments to:
True Blue Power
c/o Mid-Continent Instrument Co., Inc.
Attn: Technical Publications
9400 E. 34th Street N.
Wichita, KS 67226 USA
PH (316) 630-0101
FX (316) 630-0723
All products produced by Mid-Continent Instrument, Co., Inc., including those identified as Mid-
Continent Instruments and Avionics or True Blue Power, are designed and manufactured in
Wichita, KS, USA.
© Copyright 2019
Mid-Continent Instrument Co., Inc.
Rev G, June 6, 2019 3 Manual Number 9017899
REVISION HISTORY
Rev. Date Approved Detail
A 03/14/16 BAW Initial release.
B 04/25/16 CAS Updated formatting, added AEH statement to table 1.3
C 05/10/16 BAW Added single port unit mounting options, removed
configurations table.
D 06/23/16 ScH Added two screws (1/4”) to included connector kit.
E 01/04/17 BAW Updated to include new mounting option. Added 1.2.4.
F 05/07/19 VAA Added single rear mount with cover plate option.
G 06/06/19 VAA Updated figure 3.9 and added rear mount with circular cover
plate options.
Rev G, June 6, 2019 4 Manual Number 9017899
TABLE OF CONTENTS
SECTION 1 GENERAL DESCRIPTION
1.1 INTRODUCTION
1.2 TECHNICAL SPECIFICATIONS
1.2.1 ELECTRICAL ATTRIBUTES
1.2.2 PHYSICAL ATTRIBUTES
1.2.3 QUALIFICATIONS
1.2.4 CONFIGURATIONS
SECTION 2
PRE-INSTALLATION CONSIDERATIONS
2.1 COOLING
2.2 EQUIPMENT LOCATION
2.3 ROUTING OF CABLES
2.4 LIMITATIONS
2.5 MODIFICATIONS
SECTION 3
INSTALLATION PROCEDURES
3.1 GENERAL INFORMATION
3.2 UNPACKING AND INSPECTING
3.3 CABLE HARNESS
3.3.1 WIRE GAUGE SELECTION
3.3.2 PIN ASSIGNMENT INFORMATION
3.3.3 HARNESS VERIFICATION
3.4 MOUNTING
3.5 INSTALLATION COMPLETION
SECTION 4
OPERATION
4.1 ELECTRICAL PERFORMANCE
4.2 PROTECTIVE FEATURES
4.2.1 SHORT CIRCUIT PROTECTION
4.2.2 OVER-CURRENT PROTECTION
4.2.3 LOW INPUT VOLTAGE SHUTDOWN
4.2.4 OVER-TEMPERATURE
SECTION 5
CONFORMANCE
5.1 CONTINUED AIRWORTHINESS STATEMENT
5.2 ENVIRONMENTAL QUALIFICATION STATEMENT
Rev G, June 6, 2019 5 Manual Number 9017899
SECTION 1 GENERAL DESCRIPTION
1.1 INTRODUCTION
The TA202 Series High Power USB Charging Port is a certified accessory that converts 10 to 32 volts of
DC electrical input from the aircraft to standard 5 volt power for any electronic product that charges using
a USB connector. The TA202 provides one or two Universal Serial Bus-A or C (USB-A or USB-C) ports
and can be rear mounted or front mounted in a variety of locations throughout the aircraft. The new
“Type-C” USB port design is a smaller port that accommodates the latest consumer electronic devices on
the market. Among other features, the Type-C connector accepts reversible cable plugging with no ‘up’ or
‘down’ requirement for cable orientation. The unit is certified to FAA TSO C71 and qualified to multiple
RTCA DO-160 requirements, providing confidence and allowing installation in the cockpit or cabin.
This High Power USB Charging Port is designed as a DCP (Dedicated Charging Port) to industry-
standard protocol per the USB Battery Charging 1.2 Compliance Plan. It also complies with the higher
power requirements of USB Power Delivery 2.0. Newer electronics, such as the Apple iPad
®
, other tablets
and larger devices can accept or may require 2.1 amps or more to charge and operate. As a high power
DCP, the TA202 can provide up to 3.0 amps of power to charge USB devices, including the higher
demand products. Most dual USB chargers typically provide 1.0 amp on one port and 2.1 amps on the
second port, but the TA202 can provide 3.0 amps to both ports simultaneously (for dual port units). The
unit has built-in protections for short circuit, over-current, and low voltage conditions. It is designed to
protect against reverse polarity installation and has temperature monitoring and shutdown capability,
allowing the unit to handle unforeseen conditions safely.
Small, compact and powerful, with plenty of installation flexibility, the TA202 is an ideal choice as a highly
useful and effective addition to any aircraft.
Rev G, June 6, 2019 6 Manual Number 9017899
1.2 TECHNICAL SPECIFICATIONS
1.2.1 Electrical Attributes
Input Voltage: 10-32 VDC
Input Power: 35 watts max; 2.5 amps @ 14 VDC / 1.25 amps @ 28 VDC
Output Voltage: 5 VDC ±0.25 per port
Output Power: 3.0 amps max per port
Efficiency: ~90% nominal
Table 1.1
1.2.2 Physical Attributes
Weight: 1.3 oz. (38 g) (dual port), 0.8 oz. (23 g) (single port)
Dimensions (Dual Port Units): (not
including connector)
1.50 inches wide X 1.03 inches high X 1.25 inches deep
Dimensions (Single Port Units): (not
including connector)
1.50 inches wide X 0.52 inches high X 1.25 inches deep
Charging Ports Type: USB Standard-A or USB Standard-C
Connector Kit: MCIA P/N 9017960
Mounting: Panel mount; rear or front
Table 1.2
1.2.3 Qualifications
Certification: FAA TSO-C71
EASA ETSO-C71
Environmental Qualification: RTCA DO-160G Environmental Category
F1S2BB[(RCC1)(UG)]XXXXXXY[B(XX)]BRXXMXXXAX
Airborne Electronic Hardware: RTCA DO-254, Design Assurance Level E
Table 1.3
1.2.4 Versions
Non Lighted Lighted Power Input
Location USB Connector
Part Numbers
6430202-1 6430202-11 Rear Dual: Type A+Type C
6430202-2 6430202-12 Bottom
6430202-3 6430202-13 Rear Dual: Type C+Type C
6430202-4 6430202-14 Bottom
6430202-5 6430202-15 Rear Dual: Type A+Type A
6430202-6 6430202-16 Bottom
6430202-7 6430202-17 Rear Single: Type C
6430202-8 6430202-18 Bottom
6430202-9 6430202-19 Rear Single: Type A
6430202-10 6430202-20 Bottom
Table 1.4
Rev G, June 6, 2019 7 Manual Number 9017899
SECTION 2 PRE-INSTALLATION CONSIDERATIONS
2.1 COOLING
No external cooling is required. The unit will become warm when in use. This is normal and within
operational parameters. No special mounting considerations are required; however, mounting to a metal
surface can help dissipate any heat generated and extend the life of the product.
2.2 EQUIPMENT LOCATION
The TA202 High Power USB Charging Port is designed for mounting flexibility, allowing for installation in
the cockpit or in the cabin. It is designed for panel mounting and can be installed in a rectangular
configuration or, with an available installation kit, can be front mounted with a cosmetic cover plate. An
instrument mounting adapter bracket is also available to easily mount the unit in a standard 2-inch round
instrument opening that may already exist in the cockpit panel. There are two versions to choose from
which allow the input connector to be located either on the rear of the unit or from the bottom.
The unit can be mounted in any orientation. Clearance should be provided for the mating connector which
may require an additional inch beyond the rear of the unit.
2.3 ROUTING OF CABLES
Avoid sharp bends in cabling and routing near aircraft control cables. Avoid close proximity and contact
with aircraft structures, avionics equipment or other obstructions that could chafe wires during flight and
cause undesirable effects.
2.4 LIMITATIONS
Environmental qualifications were verified per RTCA DO-160, Revision G in lieu of those identified within
the minimum performance standards (MPS) of the TSO.
The conditions and tests for TSO approval of this article are minimum performance standards. Those
installing this article, on or in a specific type or class of aircraft, must determine that the aircraft installation
conditions are within the TSO standards, specification of the article and deviations as listed above. TSO
articles must have separate approval for installation in an aircraft. The article may be installed only
according to 14 CFR part 43 or the applicable airworthiness requirements.
The USB Type-C interface is an exciting new connector for electronic devices. Beyond the physical
format of the Type-C connector, it also allows for a variety of interface options when communicating with
compatible devices. This device-to-charger communication is defined within the USB 3.1 Specification
and Power Delivery 2.0 standards. However, manufacturers of consumer electronic devices and/or cables
may choose to implement proprietary versions or modifications of the USB standards to operate
specifically with their own charging equipment. The TA202 has been tested with and supports a wide
variety of devices now emerging on the open market. However, compatibility with all devices may not be
guaranteed. True Blue Power continues to be proactive in evaluating new devices and strives to
continually improve the product as needed to serve the vast majority of USB Type-C electronic products.
Rev G, June 6, 2019 8 Manual Number 9017899
2.5 MODIFICATIONS
Each TA202 series High Power USB Charging Port (part number 6430202-( )) has a nameplate that
identifies the manufacturer, model, part number, description, certifications and technical specifications of
the unit. The nameplate also includes the “MOD” or modification status representing notable changes in
the design of the unit. The following identifies each “MOD” or modification.
Modification (MOD) 0 is the initial release of the TA202 series High Power USB Charging Port and is
identified on the nameplate by the lack of marking on the MOD numbers 1 through 9 (i.e. 1-9 are visible).
All subsequent modifications are identified on the nameplate by the marking/blacking out of that particular
MOD number (i.e. for MOD 1, the number 1 is not visible and 2-9 are visible). See Figure 2.1 for examples.
For additional details regarding design changes to the TA202 series High Power USB Charging Port,
refer to individual Service Bulletins associated with each MOD.
MOD 0 MOD 1
Figure 2.1
Nameplate and MOD Status Examples
Rev G, June 6, 2019 9 Manual Number 9017899
SECTION 3 INSTALLATION PROCEDURES
3.1 GENERAL INFORMATION
This section contains interconnect diagrams, mounting dimensions and other information pertaining to the
installation of the TA202 Single and Dual USB Charger. After installation of cabling and before installation
of the equipment, ensure that power and ground are applied to the proper pins specified in Section 3.3.2,
Pin Assignment Information.
3.2 UNPACKING AND INSPECTING EQUIPMENT
When unpacking this equipment, make a visual inspection for evidence of any damage that may have
occurred during shipment. The following parts should be included:
a. High Power USB Charging Port MCIA P/N 6430202-( )
b. Installation Manual MCIA P/N 9017899
c. Connector Kit MCIA P/N 9017960
i. Mating Connector, 2-pin
ii. Pins (4) (2 required, 2 spares)
iii. Screws, #4-40 x 1/4 flat-head (2)
iv. Screws, #4-40 x 5/16 flat-head (2)
Optional Equipment Available:
a. Front Mount Installation Kit MCIA P/N 9017897
b. Instrument Mount Adapter Kit MCIA P/N 9017947
c. Dual Rear Mount Installation Kit MCIA P/N 9017958
d. Single Rear Mount Installation Kit MCIA P/N 9019351-1
e. Dual Rear Mount Circular Cover Plate MCIA P/N 9019384-2
f. Single Rear Mount Circular Cover Plate MCIA P/N 9019384-1
Equipment Not Provided:
a. Cable Harness Wire See Section 3.3.1 for specifications
b. Circuit Breaker Recommendation 3 amp (2 amp may be sufficient for 28V aircraft)
3.3 CABLE HARNESS
Construct the cable harness following the instructions outlined below and per Figure 3.1.
Refer to Section 2: Pre-Installation Considerations, for routing precautions.
3.3.1 Wire Gauge Selection
Use of PTFE, ETFE, TFE, Teflon or Tefzel insulated wire is recommended for aircraft use.
The wire harness should utilize 20-24 AWG stranded wire. Refer to table 3.1 below.
Wire Gauge Wire Length
20 AWG stranded wire 35 ft
22 AWG stranded wire 22 ft
24 AWG stranded wire 14 ft
Table 3.1
Wire Gauge and Length
Note: Pins should be crimped using Molex Hand Crimp Tool 63819-0000 (Preferred), 63811-2800
(obsolete) or 11-01-0200 (obsolete). See the Molex Hand Crimp Tool User Manual for crimp
procedures.
Rev G, June 6, 2019 10 Manual Number 9017899
3.3.2 Pin Assignment Information
INPUT POWER:
Pin A (keyed) – Positive DC input +10 to 32 VDC power
Pin B – Negative DC input / ground
3.3.3 Harness Verification
Note:
The TA202 has built-in reverse polarity protection for the
power connector. If Pins A and B are swapped, the unit will not
be damaged, but will also not function.
Once the cable harness is prepared, prior to connecting the
TA202, activate the aircraft power bus and use a multimeter to
verify that aircraft power and ground is supplied with appropriate
voltage on the proper pins within the mating harness.
3.4 MOUNTING
The TA202 can be installed in one of five ways:
rear mount, rectangular
instrument mount
1 2 3
front mount, decorative cover plate
1 2 4
rear mount, decorative cover plate
1 4
rear mount, circular cover plate
1 3
1
Installation kit required. See Section 3.2, Optional Equipment Available for part
number reference
2
Dual port units only
3
Black anodized
4
Brushed aluminum, bare (appropriate for additional plating/finish)
Prepare the panel cutout as shown in Figures 3.4 thru 3.11 per the selected mounting option.
Countersinks shown in the panel cutouts for flat head screws are optional. However, flat head
screws are provided for flush appearance. For Rear Mount Cover Plate Installations, countersinks in
the panel are required.
For Rear Mount Installations:
Mounting screws length MUST be between (PT +0.150”) and (PT +0.210”). [PT = panel thickness]
Mounting screws provided with the unit are 0.24” and 0.31”. (accommodates 0.030” to 0.160” PT)
For PT greater than 0.125, the USB connector will be below the surface of the panel (below flush).
For Front Mount Installations: Minimum panel thickness is 0.04”. Maximum panel thickness is 0.20”.
For Rear Mount Installation with Cover Plate: Panel thickness greater than 0.065 will cause the USB
connector to be below the surface of the Cover Plate (below flush).
3.5 INSTALLATION COMPLETION
Prior to operating the unit in the aircraft, it is recommended to verify the output and functionality of the
unit. In order to prevent accidental damage to other systems, it is not recommended to attach the output
to other equipment prior to verification. Verify the output of the unit at the terminating end of the cable with
a multimeter to ensure proper voltage and polarity. Once verified, installation can be completed and
functionality should be checked.
Figure 3.1
Power Input
Pin B
(bottom input versions)
Pin
A
Pin A
(rear input versions)
Pin B
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