Honeywell International Inc. KTR2280A Manuale Utente

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SYSTEM INSTALLATION MANUAL
KTR 2280A
Page 1-7 
15 May 2017
© Honeywell International Inc. Do not copy without express permission of Honeywell.
 l'utilisateur de l'appareil doit accepter tout brouillage radioélectrique subi, même si le brouillage 
est 
susceptible d'en compromettre le fonctionnement.
1.7               CONTINUED AIRWORTHINESS INSTRUCTIONS
1.7.1             Equipment
The instructions for continued airworthiness given in the TC or STC approvals for this product supplements or 
supersedes the instructions for continued airworthiness in this manual.
The KTR 2280A is designed and manufactured to allow "on-condition maintenance". On condition maintenance
 
is described as follows; There are no periodic service requirements necessary to maintain continued
 
airworthiness. No maintenance is required until the equipment does not properly perform its intended function. 
When service is required, a complete performance test must be accomplished following any repair action. 
Consult the KTR 2280A CMM, Pub. No. D201610000050, for complete performance test information. All 
maintenance must be performed by a Honeywell approved repair center
14 CFR Part 23.1529 and 25.1529, Instructions for Continued Airworthiness is met per the following instructions:
The removal of the equipment is on the condition of failure. There is no required periodic  maintenance for the 
KTR 2280A.
NOTE:                Upon completion of maintenance or repair, the post-installation checkout procedures must be
 
performed. Refer to 2.4 POST-INSTALLATION CHECKS for the procedures.
1.7.2               Wires and Coaxial Cables
During on-condition or regularly scheduled maintenance, inspect the wires and coax cables following the
 
guidelines listed in AC 43.13-1B Chapter 11, 12 as necessary.
1.8               ANTENNA RF EXPOSURE
WARNING:                       TO MINIMIZE RF EXPOSURE TO PERSONNEL, INSTALL THE ANTENNA
 
GENERALLY AWAY FROM AREAS WHERE PEOPLE ARE LOCATED. IN
 
SITUATIONS WHERE A PERSON WOULD BE DIRECTLY EXPOSED TO ANTENNA
 
RADIATION, SUCH AS IN A COMPOSITE AIRCRAFT, A MINIMUM SEPARATION OF
 
1.97 FT (60 CM) IS GENERALLY REQUIRED BETWEEN ANY PART OF THE
 
ANTENNA AND ANY LOCATION WHERE A PERSON MAY BE PERMANENTLY
 
SEATED IN THE AIRCRAFT. LESSER SEPARATION IS ACCEPTABLE IN AN
 
AIRCRAFT WHERE METAL SKIN SHIELDS THE OCCUPANTS FROM THE
 
ANTENNA