User's Manual Part 6

Page C-12
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
4.3 KANDU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 4-25 or Figure 4-26.
Electrical
wiring
Electrically wire and interconnect in
accordance with Figure 4-25 or
Figure 4-26 and Figure 4-34, thru
Figure 4-37, depending on the
configuration being used.
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 4-10.
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.
4.6 KRFU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 4-27, Figure 4-28, or Figure 4-29
depending on configuration used.
Install the thermal pad in accordance
with KRFU on page 4-16.
The KRFU is installed with the FMA.
refer to FMA Installation Procedure on
page 4-24.
Section Parameter Item NA √ Value
Draft as of 31 May 2017