User Manual Part 1

Page 2-28
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Install the LAIM to the Aircraft Fuselage
(a) Make sure that all the fittings are oriented vertically with the alignment tools, to help
when you lower the LAIM onto aircraft fittings.
(b) Put the LAIM assembly onto aircraft install location. Refer to Figur
e 2-13 for a generic
LAIM installation on airframe structure.
Figure 2-13. LAIM Assembly
(c) The LAIM gets attached to aircraft structure at six machined
fitting locations. Forward
four fittings each have four attachment points, through the aircraft skin to the
intercostals. The two aft fittings each have four attachment points through aircraft skin
to the stringer rivet hole locations. Machined brackets will get attached to intercostals
with fasteners.
Refer to the airframe specific kits and assembly for fastener
specifications to install LAIM
to airc
raft.
Install the Radome Skirt Fairing
(a) Before mounting the radome skirt fairing assembly onto aircraft, make sure that all the
fittings are or
iented vertically with the alignment tools, to help when you lower the
radome skirt fairing assembly onto the aircraft fittings.
(b) Put the radome skirt fairing assembly onto the aircraft. Ref
er to the airframe specific kits
and assembly for fastener specifications to install radome skirt fairing assembly to
aircraft. Figure 2-14 shows the radome skirt assembly along with LAIM.
(c) The radome skirt fairing assembly is mounted firmly with 39 fastener points through
aircraft skin into
gusset attached to the outer flange of the intercostals and into gusset
attached to the inner flange of the intercostals (1 at the forward center and 19 on each
side).
NOTE: Consult airframe manufacturer for choosing the correct torque values.