User's Manual Part 1
Table Of Contents
- TRANSMITTAL INFORMATION
- SECTION 1 INTRODUCTION
- SECTION 2 DESCRIPTION
- SECTION 3 SYSTEM PRE-CONFIGURATION
- SECTION 4 INSTALLATION
Page 4-13
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
4.5 Installation Guidelines for the LAIM (If applicable)
NOTE: Please see Figure 4-33 LAIM outline and installation drawing, 90404861, for installation
details.
The installation sequence suggested for mounting the LAIM is as follows:
• Install the LAIM and radome skirt fairing bonding straps.
• Install the LAIM to the aircraft fuselage.
• Install the radome skirt fairing.
A. Install the LAIM and Radome Skirt Fairing Bonding Straps
(1) Before mounting the LAIM assembly onto the aircraft, install bonding s
traps to aircraft fittings.
There are eight bonding straps. Six of the bonding straps are installed between the bonding
points and the radome skirt fairing. Two bonding straps are installed between the bonding
points and the LAIM structure.
(2) Refer to the airframe specific kits and assembly drawings for fastener details.
B. Install the LAIM to the Aircraft Fuselage
(1) Put the LAIM assembly onto aircraft install location.
Refer to Figure 4-5 for a generic LAIM
installation on airframe structure.
Figure 4-5. LAIM Assembly
(2) 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.
Draft as of 31 May 2017