Audio Authority BM-AIK2A Airframe Interface Kit Installation Guide
- May 15, 2024
- Audio Authority
Table of Contents
BM-AIK2A
**and BM-AIK1*
Installation Instructions
Airframe Interface Kit for
Battery MINDer®
Maintenance Charger-Desulfator
**
BM-AIK2A Airframe Interface Kit
One BM-AIK1 harness ships with each BatteryMINDer-equipped GPU. BM-AIK2A is identical except that it also includes the 802-694A SAE “trailer plug” adapter, and the BM-AIK1 does not.
Background and Regulatory Information
Read Completely Before Beginning Installation
Some non-aviation BatteryMINDer models are supplied with an automotivegrade
battery connection harness and a battery-mounted temperature sensor. However,
these are not eligible for installation on FAA-certified aircraft, under
Federal Aviation Regulations 14 CFR §21.9. They are suitable only for
temporary connection or bench charging but cannot be legally installed on the
aircraft. Aviation-specific BatteryMINDer models are supplied with a battery
clip harness for temporary connections for a battery that is removed from the
airframe.
This kit provides standard aircraft parts acceptable under 14 CFR §21.9 for an
FAA certificated mechanic to fabricate and install a fused, 2-wire harness
toaccess a certified aircraft’s lead-acid storage battery or related battery
electrical bus, for the purpose of connecting an aviation-specific
BatteryMINDer brand of low-current (8A or less), continuous-duty, maintenance-
type battery charger. The finished harness typically has ring terminals at the
battery relay & ground, connecting to an Anderson SB50 polarized plug at the
opposite end via MIL-spec unshielded 16-gauge aircraft wire, with a 15-amp in-
line protective fuse. An insulating dust cover protects the plug when not
connected to the charger. This product is not designed or intended for
chargers greater than 8-amperes.
This kit can be installed as a minor alteration under 14 CFR §1.1 and
§21.93(a) as it has “no appreciable effect on the weight, balance, structural
strength, reliability, operational characteristics, or other characteristics
affecting the airworthiness” of the aircraft. No Form 337 submittal or FSDO
field approval is required per FAA Order 8900.1 Figure 4-67. A §43.9 airframe
maintenance logbook entry is required and sufficient for return to service.
These instructions are advisory only. Aircraft models and configurations vary
widely, so an airworthy installation depends on the judgment of a competent
mechanic to determine the best option. This kit provides commonly used
installation parts. Some airframe configurations may require different parts
that are not supplied. Similarly, a length of protective fiberglass MIL-spec
sleeve is provided to protect the harness from airframe chafing, as needed in
the judgment of the installing mechanic. Other protective and security
measures not included in this kit may be needed and employed at the discretion
of the installing mechanic, who is ultimately responsible for the
airworthiness of the installation.
This kit also includes an adapter harness to convert the charger’s SAE
(trailer plug) output connector to a mating Anderson SB50 plug. This harness
is connected to and remains with the charger; it is not installed on the
aircraft. Finally, temperature sensing for aviation BatteryMINDers is
accomplished by use of VDC’s Ambient Temperature Sensor (ATS-1), a small plug
connected to the short pigtail on the charger, not installed on the battery or
airframe.
IMPORTANT: This harness is designed only for maintenance battery
charging, not for supplying ground power for airframe operations. Disconnect
the charger before turning on airframe electrical power. Reconnect the charger
after turning airframe electrical power off to recharge and then
maintain/desulfate the battery.
Installation Procedures
-
Determine best electrical access to the aircraft battery. See installation examples in a variety of airframes at www.audioauthority.com/bmaik. Since batteries are regularly removed for inspection, maintenance and replacement, we recommend attaching the positive ring terminal to the battery relay post or stud that is connected to the positive battery cable and the negative to a convenient airframe ground (see Figure 1). Plastic or composite airframes that do not have battery busses may require direct connection to battery terminals. The best method to access the battery varies by aircraft type and must be determined by the installing mechanic.
-
Determine a safe location to secure the red SB50 plug where it can be readily accessed for connecting the charger. Keep the distance from the plug to the battery as short as possible. If wire length required is longer than 6’ supplied in this kit, do not splice. Run a continuous length of wire as required.
-
Assemble SB50 plug to wiring. Take care to observe proper orientation when inserting the contacts into the enclosure (Figure 2). Fill the plug’s wire cavities with RTV for strain relief and allow it to set (Figure 3).
Figure 1. Simplified example of connection to battery solenoid. For more examples, see www.audioauthority.com/bmaik. -
Route and secure the wiring harness and trim to length. Use protective sleeve as necessary to prevent chafing against airframe or other components.
-
Assemble the fuse holder:
a) Cut wire leads, remove springs (use smallest spring — discard others).
b) Assemble fuse and holder as shown in Figure 4.
c) Install cap to provide positive contact pressure with the fuse. -
Position the assembled fuse holder so it is accessible and close to the battery relay or unswitched battery bus.
-
Crimp the appropriate terminals to harness leads and attach to the battery relay terminals, red wire to the positive terminal and black to negative or ground. If required, use alternate approved terminal hardware.
-
Placard the SB50 plug/cover using the supplied label or equivalent.
-
Verify continuity and proper polarity to battery.
-
Connect the SB50 harness (or SAE-to-SB50 adapter harness) to the BatteryMINDer’s output.
-
Connect the BatteryMINDer SB50 output to the airframe SB50 and test for proper operation.
-
Make appropriate entry in airframe maintenance logbook to document installation and return aircraft to service. Sample text below, edit as required for specific installation:
“Fabricated & installed 2-wire battery charger connection harness using MIL-W-22759/16 wire with 15A inline circuit protection fuse. Attached to battery relay and airframe ground with ring terminals. Terminated opposite end with Anderson SB50 plug with protective cover and mounted in forward baggage compartment. All work [AW AC43.13/1B. Verified continuity, polarity, tested with charger and for proper aircraft electrical system operation. No defects noted at this time.”
Parts List
Weight of all installed items is negligible.
Part # | Description | Qty |
---|---|---|
6331 G2 | Anderson SB50 polarized plug (red) w/solder contacts | 1 |
716-367 | Elastomeric insulating dust cover for SB50 | 1 |
761-451 | Cover Label “BATTERY MAINTENANCE CHARGER ONLY” | 1 |
852-2225 | MIL-W-22759/16 16-gauge unshielded wire, red (250°C) | 6 |
852-0005 | MIL-W-22759/16 16-gauge unshielded wire, black (250°C) | 6 |
882-014 | MIL-I-3190E silicone-coated fiberglass sleeve | 6 |
908-059 | Fuse-holder, phenolic in-line bayonet w/15″ wire loop (125°C) | 1 |
031-061 | Fuse, 15-amp 3AG style glass cartridge, 32VAC/VDC | 1 |
910-111 | Terminal, 5/16″ ring, 14-16 AWG insulated (MS25036-109) | 2 |
910-110 | Terminal, #10 ring, 14-16 AWG insulated (MS25036-108) | 2 |
910-035 | Butt splice 14-16 AWG insulated, crimp | 2 |
802-694A* | SAE to SB50 adapter harness* | 1 |
- The adapter harness attaches to the charger, not the aircraft. BM-AIK1 harness kit does not include 802-694A because the GPU includes its own charger harness, and does not require the SAE adapter.
Audio Authority® Corporation
2048 Mercer Road, Lexington, KY 40511-1071 USA
800-322-8346 •
859-233-4599 • Fax:
859-233-4510
support@audioauthority.com •
www.WhiteLightningGPU.com
References
Read User Manual Online (PDF format)
Read User Manual Online (PDF format) >>