User Manual Part 3

Page D-12
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
D. KANDU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 2-26
Electrical wiring Electrically wire and interconnect in
accordance with Figure 2-26 and
Figure 2-34, Figure 2-35, or Figure 2-36.
Mounting
Install location of KANDU is airframe
specific.
The KANDU is installed inside a
pressurized location, the KANDU to
KRFU and KANDU to FMA interconnect
are routed through a Bulkhead Interface
connectors.
Electrical wiring
- KANDU -FMA
Refer to KANDU (1).
Electrical
bonding
Electrically bond in accordance with
page 2-7.
KANDU bonding to the aircraft must be
achieved through the mounting
structure (fasteners) and KANDU
A3J1-A.
The bulkhead interface connectors
should be electrically bonded to the
aircraft.
E. KRFU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 2-27, Figure 2-28, or Figure 2-29
depending on configuration used.
Install the thermal pad in accordance with
KRFU Thermal Pad Kit on page 2-9.
The KRFU is installed with the FMA. refer
to FMA Installation Procedure on
page 2-29.
Section Parameter Item NA √ Value