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KTR 2280 Preliminary H 08/17/06
Rev. 0, Aug/2006
©Honeywell International Inc. Do not print without express permission of Honeywell
Page 2-7
(4)
The cables should be supported firmly enough to prevent movement. They
should be carefully protected wherever one may chafe against another or
against some other object. Extra protection should be provided in all loca-
tions where the cables may be subject to abuse. Shields on shielded wires
should be grounded in accordance with the system interconnection informa-
tion.
(5)
Shields should be carried through any obstruction via a thru-bulkhead con-
nector. If shielding cannot be carried through by use of a bulkhead/connec-
tor pin, precautions should be taken to ensure each segment of the shielded
lead be grounded at only one point. A ground connection of not more than
two inches in length should be used. The preceding discussion does not ap-
ply to coaxial and quadraxial cable.
(6)
Avoid routing cabling near high noise and high power sources.
2.3.5.2 PRIMARY POWER AND CIRCUIT BREAKER REQUIREMENTS
The KTR 2280 MMDR receives primary power from the aircraft power circuit breakers.
Power connections, wire sizes, and circuit breaker requirements may be found in the
APEX system installation manual and/or engineering bulletin (EB) for a specific
installation.
Содержание BENDIX/KING KTR 2280
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