User's Manual Part 6

Page C-8
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
NOTE: Input signal
range: -79 to -5 dBm.
Output signal range -30
to +5 dBm. Incross talk
requirement: -25 dBc.
Output cross talk
requirement: -40 dBc.
(Cont)
Electrical
wiring - APM to
Modman
APM to Modman interconnect cable
shall use ARINC 664 compliant 2
Shielded Twisted Pair 24 AWG (or
Aerospace Grade Shielded Cat 5/Cat
5E Minimum). Part No. ECS 922404 or
Equivalent, with a maximum length of
9.8 feet (3 m).
4.3 KANDU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 4-25 or Figure 4-26.
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 JetWave™ System Internal
LRU Installation, KANDU on page 4-8.
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.
The KRFU feet are configured differently
depending on the part number ordered.
Make sure feet are in the correct
configuration for the aircraft application.
Waveguide Make sure the waveguide is connected
before powering the KRFU.
Waveguide -
KRFU to FMA
Connection must be WR28 for TX and
coaxial cable for RX.
The TX interconnect path loss
Section Parameter Item NA √ Value
Draft as of 31 May 2017