User's Manual Part 6

Page C-3
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
Electrically wire and interconnect in
accordance with Figure 4-24 and
Figure 4-34.
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 and Figure 4-26
Electrical
wiring
Electrically wire and interconnect in
accordance with Figure 4-25,
Figure 4-26, and Figure 4-34.
Mounting
Install location of KANDU is airframe
specific. KANDU could be installed in
unpressurized area near the tail
empennage of the aircraft or inside
pressurized area of the aircraft.
In case of KANDU install location is
inside pressurized location, the KANDU
to KRFU and KANDU to TMA
interconnect may be routed through a
Bulkhead Interface connector.
Electrical
wiring -
KANDU to
TMA
Refer to JetWave™ System Internal
LRU Installation, KANDU on page 4-8.
Electrical
wiring -
KANDU
bulkhead
interface
Refer to JetWave™ System Internal
LRU Installation, KANDU on page 4-8.
Section Parameter Item NA √ Value
Draft as of 31 May 2017