Honeywell International Inc. KXP2290 Manuale Utente

Pagina di 62
n
 KXP 2290
 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA
Page 2-1
SECTION II
INSTALLATION
2.1
GENERAL INFORMATION
This section contains suggestions and factors to consider before installing the KXP 2290 Mode S 
Transponder.  Close adherence to these suggestions will assure a more satisfactory performance 
from the equipment.
The conditions and test required for the TSO and MOPS approval of this article are minimum per-
formance standards. It is the responsibility of those installing this article either on or with a speci-
fied type or class of aircraft to determine that the aircraft installation conditions are within the TSO 
and MOPS standards.  These articles must have separate approval for installation in an aircraft.  
Any features in this equipment outside the requirements of this applicable TSO and MOPS must 
be evaluated and approved as part of the installation approval.  The article may be installed only 
if performed under 14 CFR part 43 or the applicable airworthiness requirements. 
2.2
UNPACKING AND INSPECTING EQUIPMENT
Exercise extreme caution when unpacking the unit.  Make a visual inspection of the unit for evi-
dence of damage incurred during shipment.  If a claim for a damage is to be made, save the ship-
ping container to substantiate the claim.  When all equipment is removed, place all packing mate-
rials in the shipping container for future storage or reshipment of the unit.
2.3
EQUIPMENT INSTALLATION
2.3.1
GENERAL
The following paragraphs contain information pertaining to the initial installation of the KXP 2290 
Mode S Transponder, including instructions concerning the location and mounting of the support-
ing antenna(s).
The equipment should be installed in the aircraft in a manner consistent with acceptable workman-
ship and engineering practices and in accordance with the instructions set forth in this publication.  
To ensure that the system has been properly and safely installed in the aircraft, the installer should 
make a through visual inspection and conduct an overall operational check of the system on the 
ground prior to flight.
CAUTION:
AFTER INSTALLATION OF THE CABLING
AND BEFORE INSTALLATION OF THE
EQUIPMENT, A CHECK SHOULD BE MADE
WITH THE AIRCRAFT PRIMARY POWER
SUPPLIED TO THE MOUNTING CONNEC-
TOR TO ENSURE THAT POWER IS APPLIED
ONLY TO THE PINS SPECIFIED IN THE IN-
TERCONNECTION DRAWING, 
.