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 4-11
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
The aircraft coordinate system orientation and fitting layout are shown in Figure 4-2.
Figure 4-2. Aircraft Coordinate System Orientation and Fitting Layout
(1) Position and install the A791 based AIM fittings onto aircraft fittings for fittings #1, #2, #5, #6,
and #7.
(
2) Use the alignment tools to make sure that the fitting s
lip in X-direction is centered for fittings
#2, #6, and #7.
(3) Make sure that all the fittings are oriented vertically with
the alignment tools to help when you
lower the A791 based AIM onto aircraft fittings and the installed fittings pass through
openings in A791 based AIM.
(4) Put the A791 based AIM assembly onto aircraft wit
h an aircraft servicing hoist. Attach the
hoist to the A791 based AIM adapter plate at three locations labeled “Hoist Point”. Make sure
that the previously installed fittings on aircraft are still oriented vertically so that they will pass
through the openings in the adapter plate as AIM assembly is lowered onto aircraft. Refer to
Figure 4-3.
(5) Refer to the airframe specific kits and assem
bly
for fastener specifications to install A791
complaint AIM fittings to aircraft fittings.
NOTE: Consult airframe manufacturer for choosing the correct torque values.
(6) Wet the fuselage skin with water on skirt seal contact area before you put the AIM assembly
on ai
rcraft.
Draft as of 31 May 2017