True Blue Power, Wichita, KS
REV. E August 29, 2012
10
Manual Number 9017039
3.3.3
HARNESS VERIFICATION
With the TI500 Static Inverter disconnected, activate the aircraft power bus that supplies the
unit and use an multi-meter to verify that aircraft power and ground with appropriate voltage
is on the pins within the mating harness.
3.4
MOUNTING
Refer to Section 2: Pre-Installation Considerations in regards to equipment location.
The TI500 Static Inverter is designed for base mounting only. Four #10-32 mounting holes should be
provided in the aircraft in accordance with Figure 3.5. If installing the TI500 as a replacement for legacy
static inverters, an optional Mounting Adapter Kit adapter plate is available to utilize the same mounting
hole locations. See figure 3.6 for mounting hole locations using the Mounting Adapter Kit and Section 3.2
for the Mounting Adapter Kit part number. Secure the unit with four #10-32 pan head phillips screws or
equivalent. A lock washer under the head of each screw is recommended.
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 best not attach the output to other
equipment or power busses 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 of the remote on/off feature (if used) should be checked.
