JA33-001 Bluetooth
®
Transceiver
Installation and Operating Manual
Rev C
Page 5
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.
Unless otherwise noted, all wiring shall be a minimum of 24 AWG, except power and ground lines, which shall be a
minimum of 22 AWG. 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 JA33-001 can be mounted in any attitude and location with adequate space and sufficient clearance for the
connector and wiring harness. It requires no direct cooling.
2.4.4
Post Installation Checks
2.4.4.1
Voltage/Resistance checks.
Do not attach this unit until the following conditions are met:
a) Check P1 pin
1
for +28 Vdc power.
b) Check P1 pin
9
(Power Ground) for continuity to ground (less than 0.5
Ω
).
c) Check P1 pin
10
(Chassis Ground) for continuity to ground (less than 0.5
Ω
).
d) Check P1 pin
13
(Bluetooth disable) for continuity to ground when switch is closed (less than 0.5
Ω
).
e) Check all pins for shorts to ground or adjacent pins.
2.4.4.2
Configuration
Ensure that the JA33-001 contains the correct configuration settings. This may be done at the factory, on the
maintenance bench or in the aircraft before the power on checks are performed. Refer to section 2.5.
2.4.4.3
Power on Checks.
Power up the aircraft’s systems and confirm normal operation of all functions of the JA33-001 (see section 2.5).
a) 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.
b) 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
2.5
System Operation
The JA33-001 is a remote mount unit and has no user accessible controls.
2.5.1
Configuration Operation
The JA33-001 accepts commands on the Configuration connector via the configuration cable (JA99-001) and the
configuration tool (ProCS™). Refer to
Adjustments and Configuration.
2.5.2
Bluetooth
®
Audio Receive Operation
The Bluetooth
®
Audio Input is level controlled and routed to the MUSIC LEFT HI/LO and MUSIC RIGHT HI/LO
outputs.
